U.S. Department of Transportation

Federal Aviation Administration

Washington, D.C.

 

Master Minimum Equipment List

 

 

 

 

Revision: 49

Date: 06/06/2012

 

 

 

 

Boeing

B-727-100/200

 

 

 

 

 

 

John N. LaBrow

Flight Operations Evaluation Board (FOEB)

 

 

Federal Aviation Administration

Flight Standards Division

AIRCRAFT EVALUATION OFFICE,  SEA-AEG

1601 Lind Ave. S.W.

Renton, Washington 98057-4056

 

 

 

 

 

Telephone:   (425) 917-6600

                                                              Fax:   (425) 917-6638

 

 

 

                                                 FEDERAL AVIATION ADMINISTRATION             Page: I

                                                                                                                        Revision: 49

                                                  MASTER MINIMUM EQUIPMENT LIST              Date: 06/06/2012

 

                                                            (BOEING B-727-100/200)

 

 

Table of Contents

 

 

         SYSTEM                                           PAGES                        REVISION                    DATE

 

Title Page                                                                                          49                        06/06/2012

Table of Contents                                   I                                            49                        06/06/2012

Highlights of Change                              II thru III                                 49                        06/06/2012

Definitions                                             IV                                          49                        06/06/2012

Preamble                                              IV                                          49                        06/06/2012

21 Air Conditioning                                 21-1 thru 21-17                       49                        06/06/2012

22 Auto Flight                                        22-1 thru 22-4                         49                        06/06/2012

23 Communications                               23-1 thru 23-17                       49                        06/06/2012

24 Electrical Power                                24-1 thru 24-3                         49                        06/06/2012

25 Equipment/Furnishings                      25-1 thru 25-13                       49                        06/06/2012

26 Fire Protection                                  26-1 thru 26-10                       49                        06/06/2012

27 Flight Controls                                   27-1 thru 27-5                         49                        06/06/2012

28 Fuel                                                 28-1 thru 28-18                       49                        06/06/2012

29 Hydraulic Power                                29-1 thru 29-3                         49                        06/06/2012

30 Ice and Rain Protection                      30-1 thru 30-13                       49                        06/06/2012

31 Indicating/Recording Systems            31-1 thru 31-2                         49                        06/06/2012

32 Landing Gear                                    32-1 thru 32-5                         49                        06/06/2012

33 Lights                                               33-1 thru 33-8                         49                        06/06/2012

34 Navigation                                         34-1 thru 34-24                       49                        06/06/2012

35 Oxygen                                            35-1 thru 35-3                         49                        06/06/2012

36 Pneumatic                                        36-1 thru 36-5                         49                        06/06/2012

38 Water/Waste                                    38-1 thru 38-2                         49                        06/06/2012

46 Information Systems                          46-1 thru 46-2                         49                        06/06/2012

47 Inert Gas System                              47-1                                      49                        06/06/2012

49 Airborne Auxiliary Power                    49-1 thru 49-2                         49                        06/06/2012

52 Doors                                               52-1 thru 52-8                         49                        06/06/2012

56 Windows                                          56-1                                      49                        06/06/2012

73 Engine Fuel & Control                        73-1 thru 73-2                         49                        06/06/2012

74 Ignition                                             74-1                                      49                        06/06/2012

77 Engine Indicating                               77-1 thru 77-3                         49                        06/06/2012

78 Engine Exhaust                                 78-1 thru 78-3                         49                        06/06/2012

79 Engine Oil                                         79-1 thru 79-2                         49                        06/06/2012

80 Starting                                            80-1                                      49                        06/06/2012

 

 

 

                                                 FEDERAL AVIATION ADMINISTRATION             Page: II

                                                                                                                            Revision: 49

                                                     MASTER MINIMUM EQUIPMENT LIST               Date: 06/06/2012

 

                                                            (BOEING B-727-100/200)

 

 

Highlights of Change

 

EFFECTIVE ABOVE DATE, the Boeing 727 Master Minimum Equipment List has been revised.  The changes in this revision were made to increase flexibility and improve consistency.  All changes are reflected in the highlights of change listed below and are indicated by revision bars. For any change affecting an ATA section, all pages in the associated ATA section are dated for the current revision.

 

GLOBAL CHANGES

Updated entire MMEL to current template

 

ATA 21 AIR CONDITIONING

ITEM -37 Sub Item1) PL31 R3 Removed (if installed)

 

ATA 22 AUTO FLIGHT

ITEM -01 Sub Item 1) PL93 R1

 

ATA 23   COMMUNICATIONS

ITEM -03 Sub Item 2) PL106 R4

ITEM -08 & Sub Item 1) PL117 R0

ITEM -12 Sub Item 1) & 2) PL120 R1

ITEM -13 & Sub Item 1) & 2) PL58 R4

ITEM -17 PL58 R4

ITEM -18 Sub Item 1) b) & c)  PL9 R10

ITEM -20 Sub Item 2) a) PL9 R10

 

ATA 25   EQUIPMENT/FURNISHINGS

ITEM -02 PL47 R2

ITEM -06 Sub Item 2) PL100 R2

ITEM -12 PL116 R2

ITEM -13 Sub Item 1),3) a) & b) PL79 R7 and 4) a) & b) PL 79 R8

ITEM -21 Sub Item 1) & 2) Global Alternative Method of Compliance (AMOC) to Airworthiness

                Directive (AD).74-08-09 R3.

ITEM -22 Sub Item 1),2) & 3) PL73 R5

ITEM -24 PL104 R5

 

ATA 26 FIRE PROTECTION

ITEM -15 Sub Item 2) PL24 R4

ITEM -17 Sub Item 2) PL24 R4

 

ATA 31

ITEM -02 Sub Item 1) PL87 R5

 

ATA 33

ITEM -01 PL77 R2

ITEM -03 & sub Item 2) PL123 R1

 

ATA 34   NAVIGATION

ITEM -24, Sub Item 1) & 2) PL76 R5

ITEM -27, Sub Item 2) & 3) PL39 R5

ITEM -29 ALL PL 54 R10

ITEM -41 Sub Item 4) & 5) PL32 R7

ITEM -58 Sub Item 1),3) & 5) PL105 R1

 

                        FEDERAL AVIATION ADMINISTRATION      Page: III

                                                            Revision: 49

                         MASTER MINIMUM EQUIPMENT LIST       Date: 06/06/2012

 

                                      

                                                                 (BOEING B-727-100/200)

 

 

 

 

 

 

 

 

ATA 35   OXYGEN

ITEM -06 PL43 R2

 

ATA 38   WATER/WASTE

ITEM -02 Sub Item 2) PL83 R5

 

ATA 46 INFORMATION SYSTEMS

ITEM -01 PL45 R0

 

ATA 47 INERT GAS SYSTEM

ITEM -01 PL118 (archived)

 

ATA 52   DOORS

ITEM -14 Operator requested relief

 

 

                        FEDERAL AVIATION ADMINISTRATION             Page: IV

                                                                                                                            Revision: 49

                                                     MASTER MINIMUM EQUIPMENT LIST               Date: 06/06/2012

 

(BOEING B-727-100/200)

 

 

Definitions

 

For the Master Minimum Equipment List, Definitions addendum, refer to the current FAA MMEL Policy Letter PL-25, Policy Concerning MMEL Definitions, as well as, the current FAA MMEL Policy Letter PL-70, Definitions Required in MELs, as found on the Flight Standards Information Management System (FSIMS) website.

 

 

FSIMS - Publications - MMEL Policy Letters

 

 

 

 

 

Preamble

 

For the Master Minimum Equipment List, Preamble addendum as used for operations under 14 CFR Parts 121, 125, 129, and 135, refer to the current FAA Policy Letter PL-34, MMEL and MEL Preamble, as found on the Flight Standards Information Management System (FSIMS) website,.

 

FSIMS – Publications - MMEL and MEL Preamble

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

21-1

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

21 AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

21-01

Air Conditioning Packs

 

 

 

 

 

 

 

 1) All Models Except

     727-100 in Class

     “E” Cargo  

     Configuration

 

C

2

1

(O) One may be inoperative provided altitude is limited to FL 250 or below.

 

 

   2) All Models Except

       Class “E”

       Configurations

 

C

2

0

(M)(O) One or both may be inoperative for

unpressurized flight.

 

 

  3) 727-100 All  

      Models in Class 

      “E” Cargo

      Configuration

 

C

2

1

(O) Left pack may be inoperative provided:

a)       Right pack operates normally, and

b)       Altitude is limited to FL 250 or below.

 

 

 

    4) 727-200 Air Cycle

        Machines (ACM)

C

2

1

(O) One may be inoperative provided:

a)       Bleed air to the associated pack is not turned on at TAT above +19 degrees C,

b)       Air is not supplied to an inoperative ACM,

c)       Associated pack is operated in MANUAL with mix valve operated from 3/8 full cold toward hot as required, and

d)       Ram air doors remain fully open during pack operation.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

21-2

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

21 AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

21-02

Pack Air Shut-Off     Valves

 

 

 

 

 

 

 

 

 

 1) All Models Except

 727-100 And 727-

   100QF Class “E”

 Cargo    

 Configuration

 

C

2

0

(M) One or both may be inoperative closed provided associated pack is considered inoperative.

 

 

 2) 727-100 All

   Models in Class

   “E” Cargo

       Configuration

 

C

2

1

(M)(O) Left system valve may be inoperative closed provided left pack is considered inoperative.

 

 

 3) 727-200

C

2

0

(M)(O) One or both may be inoperative open, and pack(s) may be used provided:

a)       Associated flow control and shutoff

      valve operates normally, and

b)       APU air is not used.

 

 

   21-03

Pack Air Flow

Control Systems

 

 

 

 

 

 

 

 1) 727-100, 100QF

       Except Class

       “E” Cargo

     Configuration

C

2

0

(O) May be inoperative provided:

a)       Associated pack is considered inoperative, and

b)       Reference is made to AFM

       Performance Data for auto-pack trip

       system inoperative when appropriate.

 

 

 

 2) 727-100 All

       Models in Class

       “E” Cargo

       Configuration

C

2

1

(O) Left system may be inoperative provided:

a)       Reference is made to AFM Performance Data for auto-pack trip system inoperative when appropriate, and

b)       Left pack is considered inoperative.

 

 

 

 

 

 

(Continued)

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

21-3

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

21 AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

221-03

Pack Air Flow

Control Systems

(Cont’d)

 

 

 

 

 

 

 

 3) 727-200

C

2

0

(M)(O) One or both may be inoperative provided an associated pack is considered inoperative.

 

 

 

 

C

2

0

(M)(O) One or both may be inoperative provided:

a)       Associated pack may be utilized by using the override plunger on the flow control valve to open the valve, and

b)       Reference is made to AFM Performance Data for autopack trip system inoperative when appropriate.

 

 

 

 4) 727-200F

C

2

1

(O) One may be inoperative provided:

a)       Reference is made to AFM Performance Data for auto-pack trip system inoperative when appropriate,

b)       Override plunger on flow control valve is not used, and

c)       Associated pack is considered inoperative.

 

 

21-04

Pack Trip System

 

 

 

 

 

 

 

 1) All Models

C

2

0

(O) One or both warning light(s) may be inoperative provided associated overheat switches, duct pressure, and pack temperature gauges operate normally.

 

 

 

 2) 727-200

C

2

1

(O) One pack trip system may be inoperative provided associated duct pressure and pack temperature gauges operate normally, and associated pack is operated as follows:

a)       It is not turned on at TAT above

      19 degrees C,

b)       It is operated with MANUAL mix valve

      at least 3/8 from full cold position before

      and after supplying  bleed air, and

c)       Cooling doors are full open during pack operation.

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

21-4

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

21 AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

21-05

Pack Cooling Fans

 

 

 

 

 

 

 

 1) 727-100 Except

     Class “E” Cargo

     Configuration

C

2

0

(M)(O) One or both may be inoperative provided the associated pack is operated only in flight with the landing gear retracted.

 

 

 

 2) 727-100 All

     Models in Class  

     “E” Cargo

     Configuration

 

C

2

1

(M)(O) Left pack cooling fan may be inoperative provided the associated pack is operated only in flight with the landing gear retracted.

 

 

 

   3) 727-200

C

2

0

(M)(O) One or both may be inoperative provided the associated pack is operated only in flight with the landing gear and flaps retracted.

 

 

 

   4) 727-200F and

       727-200 Cargo

       Conversions

       Operated In Class

       “E” Configurations

C

2

1

(M)(O) Either pack cooling fan may be inoperative provided:

a)       Associated pack is operated only in

      flight with landing gear and flaps

      retracted, and

b)       On airplanes with Smoke Control 

      System: Normal, Abnormal, and

      Emergency Procedures are developed

      and used requiring the associated pack

      to be shut OFF before selecting the

      Smoke Control Switch ON.

 

 

21-06

Cooling Fan Air Inlet Door Actuators

 

 

 

 

 

 

 

   1) All Models Except

       Class “E” Cargo

       Configuration

C

2

0

(O) One or both may be inoperative CLOSED provided associated pack(s) are operated only

in flight with flaps retracted.

 

 

 

   2) 727-100 All

       Models in Class

       “E” Cargo

       Configuration

 

C

2

1

(O) Left door actuator may be inoperative CLOSED or partially CLOSED provided associated pack is considered inoperative.

 

 

 

 

(Continued)

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

21-5

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

21 AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

21-06

Cooling Fan Air Inlet Door Actuators

(Cont’d)

 

 

 

 

 

 

 

   2) 727-100 All

        Models in Class

        “E” Cargo

        Configuration

        (Cont’d)

 

C

2

1

(O) Left door actuator may be inoperative CLOSED or partially CLOSED provided associated pack is operated only in flight with

the flaps retracted.

 

 

 

   3) 727-200F and

       727-200 Cargo

       Conversions

       Operated In Class

       “E” Configurations

 

C

2

1

(O) Either door actuator may be inoperative CLOSED provided associated pack is

considered inoperative.

 

 

 

C

2

1

(O) Either door actuator may be inoperative CLOSED provided:

a)       Associated pack is operated only in

      flight with flaps retracted, and

b)       On airplanes with Smoke Control System: Normal, Abnormal, and Emergency Procedures are developed and used requiring the associated pack to be shut OFF before selecting the Smoke Control Switch ON.

 

NOTE: With an approved inlet cover, door is 

            considered closed.

 

 

 

   4) 727-100 and

       727-100QF

 

C

2

0

(O) One or both may be inoperative OPEN.

 

 

 

   5) 727-200 Except

       Class “E” Cargo

       Configuration

C

2

0

(O) One or both may be inoperative OPEN or PARTIALLY OPEN provided associated pack(s) is considered inoperative.

 

 

 

 

   6) 727-200F and

       727-200 Cargo

       Conversions

       Operated in Class

       “E” Configurations

C

2

1

Either may be inoperative OPEN or PARTIALLY OPEN provided associated pack is considered inoperative.

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

21-6

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

21 AIR CONDITIONING

 

 

 

 

21-07

Pack Cooling Air Modulation System

 

 

 

 

 

 

 

   1) Pack Cooling 

       Doors Manual

       Control System

 

C

2

0

(M)(O) One or both may be inoperative provided associated systems are secured fully open.

 

 

 

 

C

2

0

(O) One or both may be inoperative provided an Automatic control mode operates normally.

 

 

 

 

C

2

1

(M)(O) One may be inoperative other than fully open provided:

a)       Pack cooling door is deactivated,

b)       Pack is operated in MANUAL, and in flight only with landing gear and flaps retracted,

c)       Pack startup is made with mix valve set at 1/3 from full cold, or warmer, and

d)       Pack temperature is monitored

      continuously.

 

 

 

 

C

2

1

(M)(O) One may be inoperative other than

fully open provided an Automatic control

mode operates normally.

 

 

 

   2) Pack Cooling

       Doors Automatic

       Control System

 

C

2

0

(O) One or both may be inoperative provided Manual control mode operates normally.

 

 

 

 

C

2

0

(M)(O) One or both may be inoperative provided associated system(s) are secured fully open.

 

 

 

 

C

2

1

(M)(O) One may be inoperative other than fully open provided Manual control mode operates normally.

 

 

 

 

 

 

 

(Continued)

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

21-7

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

21 AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

21-07

Pack Cooling Air Modulation System

(Cont’d)

 

 

 

 

 

 

 

 2) Pack Cooling

       Doors Automatic

       Control System

     (Cont’d)

C

2

1

(M)(O) One may be inoperative other than fully open provided:

a)       Pack cooling door is deactivated,

b)       Pack is operated in MANUAL, and in flight only with landing gear and flaps retracted,

c)       Pack startup is made with mix valve

      set 1/3 from full cold, or warmer, and

d)       Pack temperature is monitored continuously.

 

 

21-08

Pack Cooling Door Position Indicators

C

2

0

(O) One or both may be inoperative provided associated pack trip warning system or pack temperature gauge operates normally.

 

 

 

 

C

2

0

(O) One or both may be inoperative provided associated pack cooling door(s) remain full open.

 

 

21-09

Pack Cooling Air Modulation System Temperature Limit Switches

C

2

0

(O) One or both may be inoperative provided:

a)       Associated pack temperature indicator and pack trip warning system operate normally, and

b)       Manual operations of pack cooling

      doors are confirmed.

 

 

 

 

C

2

0

(O) One or both may be inoperative provided associated pack cooling door(s) remain fully open during pack operation.

 

 

 

 

21-10

Pack Temperature Gauges

C

2

0

(O) One or both may be inoperative provided associated pack trip warning system operates normally.

 

 

 

 

C

2

0

(O) One or both may be inoperative provided associated pack cooling door(s) remain fully open during pack operation.

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

21-8

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

21 AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

21-11

Air Mix Valves

 

 

 

 

 

 

 

   1) All models Except

       Class “E” Cargo

       Configuration(s)

 

C

2

0

(M) May be inoperative provided associated

pack is considered inoperative and is not used.

 

 

  2) 727-100C In Class

      “E” Cargo

      Configuration

 

 

 

 

 

 

 

    a) Right Valve

C

1

0

(M) May be inoperative provided:

a)       Valve is deactivated in the full cold position,

b)       Right pack operates with the valve in the full cold position for smoke removal procedure, and

c)       Left pack operates normally.

 

 

 

     b) Left Valve

C

1

0

(M)(O) May be inoperative provided:

a)       Right pack operates normally, and

b)       Left pack is considered inoperative and is not used.

 

 

 

   3) 727-200F

C

2

1

Either Left or right valve may be inoperative provided associated pack is considered inoperative and is not used.

 

 

21-12

Air Mix Valve

Position Indicators

 

C

2

0

 

 

21-13

Cabin Rate of

Climb Indicator

C

1

0

May be inoperative provided all other instruments and functions of the pressurization system operate normally.

 

 

 

 

C

1

0

(O) May be inoperative provided flight is conducted in an unpressurized configuration.

 

 

21-14

Cabin Altitude Warning System

C

1

0

May be inoperative provided flight remains at or below 10,000 feet MSL.

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

21-9

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

21 AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

21-15

Cabin Altitude Indicator

C

1

0

(O) May be inoperative provided:

a)       Cabin differential pressure indicator operates normally, and

b)       A chart is provided for the flight crew to convert differential pressure to cabin altitude.

 

 

 

 

C

1

0

(O) May be inoperative provided flight is conducted in an unpressurized configuration.

 

 

21-16

Cabin Pressure Control System

 

 

 

 

 

 

 

   1) Pneumatic System

 

 

 

 

 

 

 

    a) Automatic Mode

C

1

0

May be inoperative provided Manual Mode operates normally.

 

 

 

    b) Manual Mode

C

1

0

May be inoperative provided Automatic Mode operates normally.

 

 

 

    c) Automatic and

        Manual Modes

C

2

0

(M)(O) Both modes may be inoperative for   unpressurized flight provided:

a)       Outflow valve remains open, or is removed, and

b)       Extended overwater flight is prohibited.

 

 

 

 2) Electric System

 

 

 

 

 

 

 

a) Automatic

    and/or Standby

        Modes

 

C

2

0

May be inoperative provided both Manual

Modes, AC and DC, operate normally.

 

 

 

    b) Automatic and

        Manual AC

        Modes

A

2

0

(O) May be inoperative provided:

a)       Standby and Manual DC Modes operate normally,

b)       Aircraft is operated at FL 250 or below, and

c)       Operations are limited to not more than three flight days before repair is made.

 

 

(Continued)

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

21-10

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

21 AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

21-16

Cabin Pressure Control System

(Cont’d)

 

 

 

 

 

 

 

 2) Electric System

     (Cont’d)

 

 

 

 

 

 

 

    c) Standby and

        Manual DC

        Modes

A

2

0

(O) May be inoperative provided:

a)       Automatic and Manual AC Modes operate normally,

b)       Aircraft is operated at FL250 or below, and

c)       Operations are limited to not more than three flight days before repair is made.

 

 

 

    d) All Modes

C

4

0

(M)(O) May be inoperative for unpressurized flight provided:

a)       Outflow valve remains open, and

b)       Extended overwater flight is prohibited.

 

 

21-17

Ground Venturi Fan

 

C

1

0

 

 

21-18

Outflow/Safety Valves

 

 

 

 

 

 

 

   1) Pneumatic System

 

 

 

 

C

2

0

(M)(O) One or both may be inoperative provided:

a)       Airplane is operated unpressurized with the inoperative valve(s) remaining open, or removed, and

b)       Extended overwater flight is prohibited.

 

 

 

   2) Outflow Valve

       (Electric System)

 

 

 

 

 

 

 

     a) AC Powered

         Actuator

         System

A

1

0

(M)(O) May be inoperative provided:

a)       DC Powered Actuator System operates normally,

b)       Inoperative AC System does not restrict DC System,

c)       Aircraft is operated at FL250 or below, and

d)       Operations are limited to not more than three flight days before repair is made.

(Continued)

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

21-11

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

21 AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

21-18

Outflow/Safety Valves

(Cont’d)

 

 

 

 

 

 

 

   2) Outflow Valve

       (Electric System)

     (Cont’d)

 

 

 

 

 

 

 

     b) DC Powered

         Actuator

         System

A

1

0

(M)(O) May be inoperative provided:

a)       AC Powered Actuator System operates normally,

b)       Inoperative DC System does not restrict AC System,

c)       Aircraft is operated at FL250 or below, and

d)       Operations are limited to not more than three flight days before repair is made.

 

 

 

 

C

1

0

(M)(O) May be inoperative for unpressurized flight provided:

a)       Outflow valve remains open, and

b)       Extended overwater flight is prohibited.

 

 

 

  3) Safety Valves

      (With Electric

     Outflow Valves)

 

C

2

1

One may be inoperative closed for pressurized flight.

 

 

 

C

2

0

(M)(O) One or both may be inoperative for unpressurized flight provided:

a)       Outflow valve remains open, and

b)       Extended overwater flight is prohibited.

 

 

21-19 

 ***

Ram Air Shutoff Valve

 

 

 

 

 

 

 

   1) 727-100/-100C

       (Except Class “E”

       Cargo

       Configuration)

 

C

1

0

(M)(O) May be inoperative open for left pack operation only, during either pressurized or unpressurized flight.

 

 

 

 

D

1

0

(M) May be inoperative closed.

 

 

(Continued)

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

21-12

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

21 AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

21-19 

 ***

Ram Air Shutoff Valve

(Cont’d)

 

 

 

 

 

 

 

   2) 727-100C

       (Class “E” Cargo

       Configuration)     

 

C

1

0

(M) May be inoperative open provided right

pack operates normally.

 

 

 

   3) 727-200

C

1

0

(M)(O) May be inoperative open for

unpressurized flight.

 

 

 

 

D

1

0

(M) May be inoperative closed.

 

 

21-20

Passenger Cabin Temperature Control System

 

 

 

 

 

 

 

   1) Automatic Mode

C

1

0

May be inoperative provided Manual Mode operates normally.

 

 

 

 

   2) Manual Mode

C

1

0

May be inoperative provided Automatic Mode operates normally.

 

 

 

   3) Automatic And

       Manual Modes

 

 

 

 

 

 

 

a)   Except for

     727-100C In

     Class “E” Cargo

     Configuration

 

C

2

0

(M)(O) Both modes may be inoperative

provided Right Pack is considered inoperative.

 

 

 

 

 

b)   727-100C In

     Class “E” Cargo

     Configuration

C

2

0

(M) May be inoperative provided:

a)       Right Air Mix Valve is secured in the full cold position,

b)       Right pack operates with the valve in the full cold position for smoke removal procedure, and

c)       Left pack operates normally.

 

NOTE: This item may be identified as Main

            Cabin Temperature Control System on

            all cargo configurations.

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

21-13

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

21 AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

21-21

Cabin Temperature Gauge

 

C

1

0

 

 

21-22

Flight Deck Temperature Control System

 

 

 

 

 

 

 

   1) Automatic Mode

C

1

0

May be inoperative provided Manual Mode operates normally.

 

 

 

   2) Manual Mode

C

1

0

May be inoperative provided Automatic Mode operates normally.

 

 

 

   3) Automatic and

       Manual Modes

C

2

0

(M)(O) Both modes may be inoperative

provided Left Pack is considered inoperative.

 

 

21-23

Forward Cargo Heat Outflow Valve

C

1

0

May be inoperative open for two pack

operations only.

 

 

 

 

C

1

0

May be inoperative closed for all-passenger operations only.

 

 

21-24

***

Gasper Fan

D

1

0

 

 

21-25

Water Separator

Anti-Icing Systems

 

 

 

 

 

 

 

 1) Passenger

      Configurations

 

C

2

1

One may be inoperative provided the other

pack operates normally.

 

  

 2) Class “E” Cargo

       Configurations

 

 

 

 

 

 

 

     a) 727-100, And

        100QF

C

2

1

(O) Left system may be inoperative provided

right pack operates normally.

 

 

 

     b) 727-200

C

2

1

(O) Either left or right system may be inoperative provided the other pack operates normally.

 

 

 

 3) All Models Except

     For Class “E”

     Cargo

       Configuration

 

C

2

0

(O) One or both may be inoperative provided associated pack(s) is considered inoperative.

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

21-14

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

21 AIR CONDITIONING

 

 

 

 

21-26

Cabin Differential Pressure Gauge

C

1

0

(O) May be inoperative provided:

a)       Cabin altitude indicator operates normally, and

b)       A chart is provided to the crew to convert cabin altitude to differential pressure.

 

 

 

 

C

1

0

(O) May be inoperative provided flight is conducted in an unpressurized configuration.

 

 

21-27

***

Zone Control Protection System

 

 

 

 

 

 

 

  1) 727-200

      Passenger

       and Combi

     Configuration

C

1

0

(O) May be inoperative provided associated valves remain closed.

 

 

 

 

 

  2) 727-200 Cargo

  Configuration

        From STC

 

C

1

0

(M)(O) May be inoperative provided associated valves are deactivated closed.

 

 

 

C

1

0

(M)(O) May be inoperative provided:

a)       Zone Control Indicating System

       operates normally, and

b)       Associated valves remain closed.

 

 

21-28

***

Zone Temperature Control Valves

(727-200)

 

C

2

0

(M) One or both may be inoperative closed.

 

 

 

C

2

0

(M)(O) One or both may be inoperative fully or partially open provided a blocking plate is installed.

 

 

 

 

C

2

0

(M)(O) One or both may be inoperative fully or partially open provided right pack valve remains closed.

 

 

21-29

***

Zone Control Indicating System (727-200)

 

 

D

1

0

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

21-15

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

21 AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

21-30

Auto-Pack Trip System

C

1

0

(O) May be inoperative provided AFM performance data and procedures are followed.

 

 

21-31

Auto-Pack Trip

Armed Light

C

1

0

(O) May be inoperative provided AFM performance data and procedures are followed.

 

 

21-32

Airflow Multiplier Bypass Valve

 

C

1

0

 

 

21-33

Airflow Multiplier

(727-200 Only)

 

C

1

0

 

 

21-34

Ram Cooling Inlet Check Valves

C

2

0

(O) One or both may be inoperative open provided associated pack is operated only in flight with the landing gear retracted.

 

 

21-35

Air Conditioning Ground Connection Check Valve

 

 

 

 

 

 

 

   1) All Configurations

D

1

0

(M) May be inoperative closed for pressurized flight.

 

 

 

   2) All Passenger

       Configurations

       Only

 

C

1

0

(O) May be inoperative open provided flight is conducted in an unpressurized configuration.

 

 

21-36

Outflow Valve Position Indicator

 

 

 

 

 

 

 

 

 

 

 

 

 

 

C

1

0

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

21-16

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

21 AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

21-37

Equipment Cooling Fan (Or Flow Control Valve)

 

 

 

 

 

 

 

 1) All Configurations

       Except Class “E”

       Cargo

       Configurations

C

1

0

(O) May be inoperative provided:

a)       Icing conditions do not exist below 1,000 feet AGL (proportional window heat only),

b)       Airplane is not equipped with draw-through NI-CAD battery case (solid battery cover),

c)       Ground use of radio equipment is limited to that necessary for checkout and clearance procedures, not to exceed 30 minutes,

d)       DME and Radio Altimeter circuit breakers remain open until not more than five minutes prior to takeoff,

e)       Both air conditioning packs operate normally, and pressurization is normal,

f)         INS is not operated,

g)       NO. 2 forward panel blower fan operates normally,

h)       Tape reproducer and proportional window heat ONLY remain off until reaching 1,000 feet AGL,

i)         Cabin and flight deck temperature is maintained at or below 75 degrees F   (24 degrees C),

j)         Airplane is not operated in all-

      cargo Class “E” configuration,

k)       When INS provides primary attitude information, dispatch is prohibited, and

l)         De-Fog system operates normally.

 

 

 

 

 

 

 

(Continued)

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

|

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

21-17

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

21 AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

21-37

Equipment Cooling Fan (Or Flow Control Valve)

(Cont’d)

 

 

 

 

 

 

 

2) No Equipment/ No

      Rack Cooling Fan

      Light

 

C

1

0

(M) May be inoperative provided Equipment/Rack Cooling Fan operates normally.

 

 

 

 

C

1

0

May be inoperative provided Equipment/Rack Cooling Fan is considered inoperative.

 

NOTE: Light will illuminate on the ground with

            an inoperative Rack Cooling Fan, but

            will extinguish in flight.

 

 

21-38

Main Cargo Smoke Control System

(727-200F)

C

1

0

(O) May be inoperative provided procedures are established and used to ensure the associated compartment remains empty, or is verified to contain only empty cargo handling equipment, ballast (ballast may be loaded in ULDs), and/or Fly Away Kits.

 

NOTE: Operate MELs must define which items

            are approved for inclusion in the Fly

            Away Kits, and which materials can be

            used as ballast.

 

 

21-39

Supply Duct Temperature Gauge

C

1

0

May be inoperative provided both duct overheat warning systems operate normally.

 

 

21-40

Duct Overheat Warning Systems

C

2

0

One or both may be inoperative provided the supply duct temperature gauge operates normally.

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

22-1

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

22 AUTO FLIGHT

 

 

 

 

 

 

 

 

 

 

 

22-01

Autopilot System

B

1

0

(O) May be inoperative provided approach minimums or operations do not require its use.

 

NOTE: Any mode which operates normally may be used.

 

 

 

   1) Disengage

       Switches   

 

    

C

2

1

One may be inoperative provided:

a)       No autopilot is used below 1,500 feet

      AGL, and

b)       Approach minimums do not require

      autopilot use.        

 

|
|
|
|
|

 

   2) Heading Select

       Mode

C

1

0

May be inoperative provided manual mode

and altitude hold operate normally.

 

 

 

  3) Altitude Select

      Mode

 

C

1

0

May be inoperative provided altitude alert operates normally.

 

 

 

   4) IAS Hold Mode

 

C

1

0

 

 

 

   5) Mach Hold Mode

 

C

1

0

 

 

 

   6) Aux Nav Mode

 

C

1

0

 

 

 

   7) VOR/LOC Mode

C

1

0

May be inoperative provided approach

minimums do not require its use.

 

 

 

 8)  ILS Auto

       Glideslope Mode

     

C

1

0

May be inoperative provided approach

minimums do not require its use.

 

 

 

   9) G/A Mode

C

1

0

May be inoperative provided approach

minimums do not require its use.

  

 

 

   10) Land Mode

C

1

0

May be inoperative provided approach

minimums do not require its use.

 

 

 

 

 

 

(Continued)

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

22-2

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

22 AUTO FLIGHT

 

 

 

 

 

 

 

 

 

 

 

22-01

Autopilot System (Cont’d)

 

 

 

 

 

 

 

   11) Elevator Servo

         System

 

 

 

 

 

 

 

      a)  Mode A or B

C

2

1

(M) Either Mode A or B may be inoperative provided autopilot will engage when operative system A or B is selected.

 

 

 

      b)  Mode AB

C

1

0

May be inoperative provided autoland operations are not conducted.

 

 

22-02

***

  Autopilot Pitch

  Monitor System

 

D

1

0

 

 

22-03

 DELETED

 

 

 

 

Deleted prior to Rev. 27.

 

22-04

 

  Autopilot Disengaged

  Warning System

 

 

 

 

 

 

 

   1) Lights

 

C

2

1

 

 

 

 

B

2

0

Both may be inoperative provided autopilot is

not engaged.

 

 

 

   2) Aural Warning

C

1

0

May be inoperative provided approach minimums do not require its use.

 

 

22-05

DELETED

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Deleted prior to Rev. 27.

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

22-3

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

22 AUTO FLIGHT

 

 

 

 

 

 

 

 

 

 

 

22-06

Yaw Dampers (Excluding -100 airplanes with configurations

65DT-78001-511, 65DT-78001-513 or 65DT-78001-515 of STC ST00488SE, and excluding -100 airplanes with

STC SA5938NM)

 

C

2

0

One or both may be inoperative provided:

a)       AFM Limitations are complied with, and

b)       Switch associated with inoperative system remains OFF.

 

 

NOTE: Autopilot is inoperative when both yaw

            dampers are inoperative or OFF.

 

 

22-07

Yaw Damper Engage Lights or Warning Flags

C

2

0

(O) One or both may be inoperative provided:

a)       Proper motion of the rudder position indicators are verified before each departure, and

b)       AFM yaw damper inoperative limitations are observed.

 

 

22-08

Yaw Damper Ground Test Circuit

(727-200 Only)

C

2

0

(O) One or both may be inoperative provided proper motion of the rudder position indicators are verified before each departure.

 

 

22-09

***

Autothrottle Systems

D

1

0

May be inoperative provided approach procedures do not require its use.

 

 

22-10

***

A/P Approach Progress Display Panel

 

 

 

 

 

 

 

   1) Flare

       Annunciations

       (Arm and Capture)

C

2

0

(O) Arm and Capture functions may be inoperative provided Autoland is not used.

 

 

 

 

   2) Glideslope

       Annunciations

      (Arm and Capture)

C

2

0

(O) Arm and Capture functions may be inoperative provided Autopilot is not coupled to the Glide Slope (G/S) during approach.

 

 

 

   3) VOR/LOC

       Annunciations

       (Arm and Capture)

C

2

0

(O) Arm and Capture functions may be inoperative provided Autopilot is not used in the NAV/LOC Mode.

 

(Continued)

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

22-4

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

22 AUTO FLIGHT

 

 

 

 

22-10

***

A/P Approach Progress Display Panel

(Cont’d)

 

 

 

 

 

 

 

 4) Nav Annunciations

       (ARM and

       Capture)

C

2

0

(O) Arm and Capture functions may be inoperative provided the autopilot is not used in the AUX NAV mode.

 

 

 

 5) Altitude Hold 

       Annunciations

 

 

 

A

2

0

May be inoperative provided:

a)       Altitude alert operates normally, and

b)       Operations are limited to not more than three flight days before repair is made.                                                                          

  

 

 

 6) ALT SELECT

       Annunciations

C

2

0

May be inoperative provided the ARM ENG annunciator of the ALT SEL switch on the autopilot control panel operates normally.

 

 

 

 7) HDG

Annunciations

C

2

0

May be inoperative provided the ENG annunciator of the HDG Select on the autopilot control panel operates normally.

 

 

22-11

***

Single Auto-Pilot Interface Unit (AIU) (STC SA3093SO)

C

1

0

(M)(O) May be inoperative provided:

a)       AIU is deactivated,

b)       Autopilot is operated uncoupled from

      the AIU, and

c)       Operations do not require its use.

 

 

 

  1) AIU Fail

      Annunciator

C

2

1

One may be inoperative provided autopilot is operated and engaged from the operating side.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

C

2

0

Both may be inoperative provided AUI is considered inoperative.

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

23-1

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

23 COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

23-01

Flight Deck Speaker System

 

C

1

0

May be inoperative provided procedures do not require its use.

 

23-02

Passenger Address System

 

 

 

 

 

 

 

 1) Passenger

       Configuration

 

 

 

 

 

B

1

0

(O) May be inoperative provided:

a)       Alternate, normal and emergency procedures and/or operating restrictions are established and used, and

b)       Flight attendant alerting system (audio

      and visual) operates normally.

 

NOTE: Any station function(s) that operate

            normally may be used.

 

 

 

 

 

 

 

 

 

C

1

0

(O) May be inoperative provided:

a)       PA not required by FAR, and

b)       Alternate, normal and emergency procedures, and/or operating restrictions are established and used.

 

NOTE: Any station function(s) that operate

            normally may be used.

 

 

 

     a) Lavatory

         Speakers

C

-

0

(O) May be inoperative provided alternate procedures are established and used.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

(Continued)

  

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

23-2

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

23 COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

23-02

Passenger Address System (Cont’d)

 

 

 

 

 

 

 

2) Cargo

      Configuration

     (Courier/

     Supernumerary

     Address System)

 

C

1

0

(O) May be inoperative provided alternate, normal and emergency procedures and/or operating restrictions are established and

used.

 

 

 

D

1

0

May be inoperative provided procedures do

not require its use.

 

 

 

    a)  Lavatory

         Speakers

C

1

0

(O) May be inoperative provided alternate procedures are established and used.

 

 

 

 

D

1

0

May be inoperative provided procedures do

not require its use.

 

 

***

 3) Cockpit Volume

     Level Indicator

 

C

-

0

 

 

***

 4) Cockpit PA

     Monitor/Speaker

     Switch

 

C

1

0

May be inoperative in OFF (not selected) position.

 

***

 5) Cockpit PA In Use

     Light

 

C

1

0

 

 

23-03

Communications System (VHF,HF,UHF)

 

 

 

 

 

 

 

 1) Very High

     Frequency (VHF)

     Communication

     System

D

-

-

Any in excess of those required by FAR may be inoperative provided it is not powered by the Emergency AC Bus, Emergency DC Bus, Battery Direct Bus, or the DC Transfer Bus and not required for emergency procedures.

 

 

***

    a) Frequency

        Transfer Light

 

C

-

0

 

 

 

(Continued)

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

23-3

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

23 COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

23-03

Communications System (VHF,HF,UHF)

(Cont’d)

 

 

 

 

 

 

 

 1) Very High

     Frequency (VHF)

     Communication

     System

     (Cont’d)

 

 

 

 

 

 

***

    b) Frequency

        Transfer Switch

 

C

-

0

 

 

 

    c) Frequency

        Selectors

C

-

-

One per each VHF Comm required by FAR

must operate normally.

 

 

 

d) Frequency

  Indicators

C

-

-

One per each VHF Comm required by FAR

must operate normally.  

      

 

 

 2) High Frequency

     (HF)    

     Communication

     System

 

 

 

 

 

 

 

 

 

 

 

 

 

 

C

-

1

(O) May be inoperative while conducting operations that require two Long Range Communication Systems (LRCS) provided:

a)       SATCOM Voice or Data Link operates normally,

b)       Alternate procedures are established

      and used,

c)       SATCOM Voice coverage is available over the intended route of flight, and

d)       If SATCOM Voice is to be used over the intended route of flight, STACOM Voice short codes (INMARSAT) or direct dial commercial numbers (IRIDIUM) must be available. If not available, prior coordination with the appropriate ATS (FIR) facility is required.

 

NOTE: SATCOM is to be used only as a backup

            to normal HF communication unless

            otherwise authorized by the appropriate

            ATS facilities.

 

(Continued)

 

 

 

 

|
|

 

 

|

 

|
|
|
|
|
|
|

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

23-4

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

23 COMMUNICATIONS

 

 

 

 

23-03

Communications System (VHF,HF,UHF)

(Cont’d)

 

 

 

 

 

 

 

 2)  High Frequency

      (HF)

      Communication

      System

      (Cont’d)

 

D

-

-

Any in excess of those required by FAR may be inoperative.

 

 

 

 3) Ultra High

     Frequency (UHF)

     Communication

     System

 

D

-

-

Any in excess of those required by FAR, and not powered by a Standby Bus, may be inoperative.

 

 

23-04

Flight Interphone System

 

 

 

 

Deleted, Rev. 46. (Included in Item 23-6.)

 

23-05

Audio Selector Panels

 

 

 

 

 

 

 

 1) Flight Deck Audio

     Selector Panels

 

 

 

 

 

 

***

a)   Receive/

    Transmit

    Function of

    Receive/

    Transmit and

    Intercom

    Switches

 

C

-

0

(M) May be inoperative provided:

a)       A separate push-to-talk (PTT) switch operates normally at affected crew stationed, and

b)       Affected switch is electrically failed open.

 

***

    b) Amplifiers

        (Panels

        equipped

        with dual

        amplifiers)

 

C

-

-

One amplifier in each panel may be inoperative provided one amplifier operates normally at each required crew station.

 

 

 

 

 

 

(Continued)

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

23-5

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

23 COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

23-05

Audio Selector Panels

(Cont’d)

 

 

 

 

 

 

 

 1) Flight Deck Audio

     Selector Panels

     (Cont’d)

 

 

 

 

 

 

 

    c) Mixer Switches

        (ADF, HF, NAV,

        MKR, VOICE,

        RANGE)

 

 

 

 

 

 

C

-

-

(O) One switch on each audio panel may be inoperative provided:

a)       The flight interphone function operates normally,

b)       Alternate procedures for monitoring radios are identifying stations are established and used, and

c)       Associated function operates normally

      at other required crew stations.

 

***

 2) Other Than On

     Flight Deck

 

D

-

0

 

 

23-06

Crewmember Interphone System

 

 

 

 

 

 

 

 1) Passenger  

     Configuration

 

 

 

 

 

 

 

    a) Flight Deck to

        Cabin, Cabin

         to Flight Deck

         Functions

B

-

-

(O) May be inoperative provided:

a)       Flight deck to cabin and cabin to flight deck interphone functions operate normally on at least fifty percent of the cabin handsets, and

b)       Alternate communication procedures between the affected flight attendant stations are established and used.

 

NOTE: Any station function(s) that operate

            normally may be used.

 

 

 

(Continued)

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

23-6

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

23 COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

23-06

Crewmember Interphone System (Cont’d)

 

 

 

 

 

 

 

 1) Passenger  

     Configuration

     (Cont’d)

 

 

 

 

 

 

 

     b) Cabin to Cabin

   Function

 

B

2

0

(O) May be inoperative provided alternate communication procedures between the affected flight attendant stations are established and used.

 

NOTE: Any station function(s) that operate

            normally may be used.

 

 

 

 

B

-

-

(O) May be inoperative provided:

a)       Cabin to cabin interphone functions operate normally on at least fifty perfect of the cabin handsets, and

b)       Alternate communications procedures between affected flight attendant stations are established and used.

 

NOTE: Any station function(s) that operate

            normally may be used.

 

 

 

     c) Flight Deck to

         Ground

         Function

         (Airplanes

         Operating

         Under

         FAR Part 121)

C

1

0

(O) Flight interphone flight deck to

ground/ground to flight deck function may be inoperative provided:

a)       Alternate procedures are established

      and used, and

b)       Nose gear service interphone jack operates normally.

 

 

 

 

C

1

0

(O) Service interphone flight deck to ground/ground to flight deck function may be inoperative provided:

a)       Alternate procedures are established

      and used, and

b)       Nose gear flight interphone jack operates normally.

  (Continued)

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

23-7

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

23 COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

23-06

Crewmember Interphone System (Cont’d)

 

 

 

 

 

 

 

c) Flight Deck to

         Ground

         Function

         (Airplanes

         Operating

         Under

         FAR Part 121)

        (cont’d)

 

B

-

0

(O) May be inoperative provided alternate procedures are established and used.

 

 

 

     d) Flight Deck to

         Ground

         Function

         (All Other

         Aircraft

         Operations)

 

C

-

0

(O) May be inoperative provided alternate procedures are established and used.

 

 

 

 

D

-

0

May be inoperative provided procedures do not require its use.

  

 

 

 2) Cargo

      Configuration

 

 

 

 

 

 

 

     a) Flight Deck to

         Cabin, Cabin to

         Flight Deck

         Functions

 

C

1

0

(O) May be inoperative provided alternate, normal and emergency procedures, and/or operating restrictions are established and used.

 

 

 

 

D

1

0

May be inoperative provided procedures do not require its use.

 

 

 

      b) Cabin to Cabin

           Function

D

1

0

 

 

 

 

 

 

 

(Continued) 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

23-8

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

23 COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

23-06

Crewmember Interphone System (Cont’d)

 

 

 

 

 

 

 

 2) Cargo

      Configuration

      (Cont’d)

 

 

 

 

 

 

 

     c) Flight Deck to

        Ground Function

        (Airplanes

        Operating Under

        FAR Part 121)

C

1

0

(O) Flight interphone flight deck to

ground/ground to flight deck function may be inoperative provided:

a)       Alternate procedures are established

      and used, and

b)       Nose gear service interphone jack operates normally.

 

 

 

 

C

1

0

(O) Service interphone flight deck to ground/ground to flight deck function may be inoperative provided:

a)       Alternate procedures are established and used, and

b)       Nose gear flight interphone jack operates normally.

 

 

 

 

B

-

0

(O) May be inoperative provided alternate procedures are established and used.

 

 

 

     d) Flight Deck to

         Ground

         Function

         (All Other

         Aircraft

         Operations)

 

C

-

0

(O) May be inoperative provided alternate procedures are established and used.

 

 

 

 

D

-

0

May be inoperative provided procedures do not require its use.

 

 

23-07

DELETED

 

 

 

 

 

 

 

 

Deleted prior to Rev. 27.

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

23-9

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

23 COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

23-08

***

Selective Call System (SELCAL)

 

C

-

0

(O) May be inoperative provided alternate procedures are established and used.

|
|

 

 

D

-

0

May be inoperative provided procedures do not require its use.

 

|
|

 

1) Channels

C

-

0

(O) May be inoperative provided alternate procedures are established and used.

 

|
|

 

 

D

-

0

May be inoperative provided procedures do not require its use.

 

|
|

23-09

DELETED

 

 

 

Deleted, Rev. 29.

 

 

 

 

 

23-10

Cockpit Voice

Recorder System (CVR)

 

A

1

0

May be inoperative provided:

a)       Flight Data Recorder (FDR) operates normally, and

b)       Repairs are made within three flight days.

 

 

23-11

***

ARINC Communications Addressing and Reporting System (ACARS)

 

D

1

0

 

 

***

 1) ACARS Printer

 

 

 

 

 

 

 

 

 

 

 

 

 

D

1

0

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

23-10

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

23 COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

23-12

Emergency Locator Transmitter (ELT)

 

 

 

 

 

 

***

1) Survival Type

    ELTs

D

-

-

Any in excess of those required by FAR may be inoperative or missing.

 

|
|

***

 2) Fixed ELTs

A

-

0

(M) May be inoperative provided:

     a)  System is deactivated, and

     b)  Repairs are made within 90 days.

 

|
|
|

 

 

A

-

0

May be missing provided repairs are made

within 90 days.

 

|
|

 

 

D

-

-

(M) Any in excess of those required by FAR may be inoperative provided system is deactivated.

 

|
|

 

 

D

-

0

Any in excess of those required by FAR may be missing.

 

|
|

23-13

Flight Deck Headsets Earphones/ Headphones and Boom Microphones

 

(HOLDER OF AN AIR CARRIER OR COMMERCIAL OPERATOR CERTIFICATE)

 

 

 

 

 

|
|
|

 

 

|
|
|
|
|

 

 1) Headset Boom

     Microphones

 

 

A

-

0

May be inoperative provided:

a)       Associated hand microphone is installed and operates normally, and

b)       Repairs are made within three flight days.

 

|
|

|

 

 

 

 

D

-

-

Any in excess of those required by regulation may be inoperative.

 

 

(Continued)

|
|

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

23-11

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

23 COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

23-13

Flight Deck Headsets Earphones/ Headphones and Boom Microphones

 

(HOLDER OF AN

 AIR CARRIER OR COMMERCIAL OPERATOR CERTIFICATE)

(cont’d)

 

 

 

 

 

|
|
|
|
|
|
|
|
|
|
|

 

 2) Headset   Earphones/ Headphones

C

-

1

May be inoperative provided associated flight deck speaker operates normally.

 

|
|
|

 

 

D

-

-

Any in excess of those required by regulation may be inoperative.

|
|

 

(OPERATOR OTHER THAN A HOLDER OF AN AIR CARRIER OR COMMERCIAL OPERATOR CERTIFICATE)

 

D

-

-

Any in excess of those required by regulation may be inoperative.

|
|
|
|
|
|
|
|
|

 

 1) Headset Boom  Microphones

A

-

0

May be inoperative provided:

a)  Associated hand microphone is installed and operates normally, and

b)   Repairs are made in accordance with applicable regulations.

|
|
|
|
|

|

 

 

D

-

0

Any in excess of those required by regulation may be inoperative.

|
|

 

 2) Headset Earphones/Head-phones

C

-

1

May be inoperative provided associated flight deck speaker operates normally.

 

 

 

|
|
|

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

23-12

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

23 COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

23-14

***

Pre-recorded Passenger Announcement System

 

C

1

0

(O) May be inoperative provided alternate procedures are established and used.

 

23-15

 ***

Cockpit Speaker Audio Integrating System

(Add on System)

C

2

0

(M) May be inoperative provided:

a)       Associated speaker isolation amplifier operates normally,

b)       Associated headset(s) receive all

      normal selections, and

c)       Associated headset operates normally and is worn during all operations.

 

 

23-16

Control Wheel

 Push-to-Talk (PTT)  

 Switches

C

2

1

(M)(O) One may be inoperative provided:

a)       Alternate PTT switch is installed and operates in normal communications

      and with oxygen mask,

b)       Alternate procedures are established

      and used, and

c)       Affected switch is either verified failed open or is deactivated.

 

 

23-17

Flight Deck Hand Microphones

C

-

0

May be inoperative provided associated boom microphone operates normally.

 

|

|

 

 

D

-

0

Any in excess of those required by regulation may be inoperative.

|
|

***

 1) Dual Tone Multi-

     Frequency (DTMF)

     Telephone Dialing

     Feature

D

-

0

(O) May be inoperative provided:

a)       Voice Mode operates normally, and

b)       Alternate procedures are established

      and used.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

23-13

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

23 COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

23-18

Alerting Systems

(Audio/Visual)

 

 

 

 

 

 

|

 

 1) Passenger    Configuration

 

 

 

 

 

 

 

     a) Flight Deck Call

         Visual Alerting

         System

B

1

0

May be inoperative provided the flight deck

audio alerting system operates normally.

 

NOTE: The flight deck audio alerting must

            always be operative.

 

 

 

     b) Flight

   Attendant

   Visual Alerting

   System

B

1

0

(O) May be inoperative provided:

a)       PA system operates normally,

b)       If affected visual alerting system is used for lavatory smoke detector alerting, an  alternate lavatory smoke detector alert (audio or visual) is installed and operates normally, and

c)       Alternate procedures for contacting flight attendants are established and used.

 

NOTE 1: Passenger to Attendant Call System

               (excluding wheelchair accessible

                lavatory call system required by

               14 CFR) is considered Non-Essential

               Equipment and Furnishing (NEF).

 

NOTE 2: Any visual alerting system function

               that operates normally may be used.

 

 

 

 

 

 

 

 

 

 

(Continued)

 

 

 

 

 

 

 

 

 

 

 

 

|

|

|

|

|

    

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

23-14

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

23 COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

23-18

Alerting Systems (Audio/Visual)

(Cont’d)

 

 

 

 

 

 

 

 1) Passenger Configuration

     (Cont’d)

 

 

 

 

 

 

 

c)  Flight Attendant Audio Alerting System

 

B

-

0

(O) May be inoperative provided:

a)       PA system operates normally,

b)       If affected audio alerting system is used for lavatory smoke detector alerting, an alternate lavatory smoke detector alert (visual or audio) is installed and operates normally, and

c)       Alternate procedures for contacting flight attendants are established and used.

 

NOTE 1:  Passenger to Attendant Call System (excluding wheelchair accessible lavatory call system required by 14 CFR) is considered Non-Essential Equipment and Furnishing (NEF).

 

NOTE 2:  Any audio alerting system function

                that operates normally may be used.

 

 

 

 

 

 

 

 

 

 

 

 

|
|
|
|
|

 

  2) Cargo

      Configuration

 

 

 

 

 

 

 

 

a) Flight Deck

    Call Visual

     Alerting

     System

 

B

1

0

May be inoperative provided the flight deck

audio alerting system operates normally.

 

 

 

b) Flight Deck

    Call System

D

1

0

May be inoperative provided courier/supernumerary compartment remains unoccupied.

 

 

(Continued)

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

23-15

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

23 COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

23-18

Alerting Systems (Audio/Visual)

(Cont’d)

 

 

 

 

 

 

 

 

  2) Cargo

      Configuration

     Cont’d)

 

 

 

 

 

 

 

c) Courier

    Supernumerary

    Visual Alerting

    System

B

1

0

May be inoperative provided:

a)       Courier/supernumerary address system operates normally, and

b)       Alternate procedures are established and used.

 

 

 

 

D

1

0

May be inoperative provided courier/supernumerary compartment remains unoccupied.

 

NOTE: Any visual alerting system function that

            operates normally may be used.

 

 

 

d) Courier

    Supernumerary

    Audio Alerting

     System

       

B

1

0

May be inoperative provided:

a)       Courier/supernumerary address system operates normally, and

b)       Alternate procedures are established

      and used.

 

 

 

 

D

-

0

May be inoperative provided courier/supernumerary compartment remains unoccupied.

 

NOTE: Any audio alerting system function that

            operates normally may be used.

 

 

23-19

***

Satellite Communication (SATCOM) System

 

C

-

0

(O) May be inoperative provided alternate procedures are established and used.

 

 

 

 

D

-

0

May be inoperative provided operations or procedures do not require its use.

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

23-16

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

23 COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

23-20

Handset Systems

 

 

 

 

 

 

 

 1) Passenger

     Configuration

 

 

 

 

 

 

 

     a) Flight Deck

C

-

0

(O) May be inoperative provided:

a)       Flight deck to cabin communication operates normally, and

b)       Alternate procedures are established

      and used.

 

 

 

 

D

-

0

May be inoperative provided procedures do

not require its use.

 

 

 

     b) Cabin

B

-

-

(O) May be inoperative provided:

a)       Fifty percent of cabin handsets operate normally, and

b)       Alternate communications procedures between the affected Flight Attendants stations(s) are established and used.

 

NOTE 1: An operative handset at an inoperative

               flight attendant seat shall not be

               counted to satisfy the fifty percent

               requirement.

 

NOTE 2: Any handset function(s) that operate

               normally may be used.

 

 

 

 2) Cargo

     Configuration

 

 

 

 

 

 

 

 

     a) Flight Deck

C

-

0

May be inoperative provided flight deck to courier/supernumerary communication

operates normally.

 

 

 

 

D

-

0

May be inoperative provided procedures do not require its use.

 

 

 

 

(Continued)

|

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

23-17

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

23 COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

23-20

Handset Systems

(Cont’d)

 

 

 

 

 

 

 

 2) Cargo

     Configuration

     (Cont’d)

 

 

 

 

 

 

 

     b) Courier

         Supernumerary

 

D

-

1

 

 

 

 

D

-

0

May be inoperative provided courier/supernumerary compartment remains unoccupied.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

24-1

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

24 ELECTRICAL POWER

 

 

 

 

 

 

 

 

 

 

 

24-01

Generators and Constant Speed

Drive Units

B

3

2

(M)(O) One generator or CSD may be inoperative provided:

a)       Electrical loads are monitored,

b)       Two generators operate normally,

c)       All TRs operate normally, and

d)       One air conditioning pack fan is deactivated.

 

 

24-02

CSD Low Pressure Lights

C

3

0

Any or all may be inoperative provided the associated generator functions and indicators operate normally.

 

 

24-03

CSD Oil Temperature Gauges

C

3

0

Any or all may be inoperative provided the associated KW/KVAR meter and generator

drive low pressure lights operate normally.

 

 

24-04

Automatic Generator Paralleling System

C

1

0

(O) May be inoperative provided manual paralleling procedures are followed.

 

 

24-05

Generator Synchronization Lights

C

2

0

One or both may be inoperative provided auto-paralleling operates normally for parallel generator operation.

 

 

24-06

Transformer Rectifiers

B

3

2

No.1 or No.2 TR may be inoperative provided

all generators, DC busses and essential TR operate normally.

 

 

24-07

DELETED

 

 

 

 

 

 

24-08

AC Voltmeter

 

 

 

 

 

 

 

 1) Residual Voltage

     Function

 

C

1

0

 

 

24-09

DELETED

 

 

 

 

 

 

24-10

DELETED

 

 

 

 

 

 

24-11

DELETED

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

24-2

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

24 ELECTRICAL POWER

 

 

 

 

 

 

 

 

 

 

 

24-12

Generator System Annunciator Panel

 

C

1

0

 

 

24-13

DELETED

 

 

 

 

 

 

24-14

External Power System

 

C

1

0

 

 

 

24-15

KW/KVAR Meters

 

 

 

 

 

 

 

 1) KW Meters

C

3

2

One KW meter may be inoperative provided:

a)       Associated CSD oil temperature gauge operates normally, and

b)       All generators operate normally.

 

 

 

 

C

3

2

One KW meter may be inoperative for an associated inoperative generator.

 

 

 

 2) KVAR Meters

C

3

0

 

 

 

24-16

***

Constant Speed Drive Ejector Valves

C

-

-

(M)(O) One may be inoperative open provided:

a)       All limit EPRS on associated engine are reduced by .03, and

b)       Performance limited gross weight is reduced by: - Takeoff and Landing – 2,500 lbs. (1,134 kg.). – En route climb (1 or 2 engines inoperative) – 4,800 lbs. (2,177 kg.).

 

 

24-17

 

Essential Power Generator Selector Position

C

3

2

(M)(O) One generator position may be inoperative provided:

a)       Essential power can be provided through the two remaining generator positions,

b)       Remaining generator channels operate normally,

c)       All AC busses are paralleled, and

d)       Three-phase circuit breaker for the inoperative position is opened and secured, as prescribed by the operators appropriate procedures.

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

24-3

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

24 ELECTRICAL POWER

 

 

 

 

 

 

 

 

 

 

 

24-18

 

Automatic Standby Bus Transfer System (Auto Standby Switching)

 

 

 

 

 

 

 

 1) Automatic

     Transfer

      Function

B

1

0

(M) May be inoperative provided:

a)       Normal, Abnormal, and Emergency Procedures are established and used

      for manual transfer, and

b)       Manual transfer operates normally and

      is verified once each flight day.

 

 

***

 2) Ground Test

      Function

C

1

0

(O) May be inoperative provided system

integrity is verified once each flight day.

 

 

24-19

Master Warning Light (WARN)

(Pilot Center Panel)

 

C

1

0

May be inoperative provided the essential

power failure light on the F/E panel operates normally.

 

 

24-20

***

Standby Battery System

(STC SA8821SW)

 

 

 

 

 

 

 

 1) Batteries

C

2

1

(M)(O) One may be inoperative provided:

a)       Parallel operation is deselected, and

b)       Operating battery is selected.

 

 

 

 2) Test Annunciator

C

1

0

(O) May be inoperative provided all indicators in the select switches are verified to be functioning normally prior to each departure. 

 

 

 

  3) Parallel Feature

 

C

1

0

 

 

 

 

 4) Battery Chargers

C

2

1

One may be inoperative provided battery on

the inoperative charger is considered

inoperative and is not used.

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

25-1

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

25 EQUIPMENT/FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

25-01

DELETED

 

 

 

 

Deleted Prior to Rev. 33.

 

25-02

Megaphones

 

 

D

-

-

Any in excess of those required by FAR may be inoperative or missing provided:

a)       Inoperative megaphone is removed

      from the passenger cabin,

b)       Associated placard is removed or obscured, and

c)       Required distribution is maintained.

 

 

 

 

 

|

|

 

25-03

Rear Entrance Door Strap

C

1

0

May be inoperative provided a passenger announcement is made to stay clear until the door is opened.

 

NOTE 1: Not required for -200 series, or -100

              series airplanes with two type I rear

              exits.

 

NOTE 2: Not required for all cargo operations.

 

 

25-04

Crewmember Shoulder Harness (Flight Deck)

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Deleted, Rev. 35.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

25-2

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

25 EQUIPMENT/FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

25-05

Flight Attendant Seat Assembly (Single or Dual Position)

 

 

 

 

 

 

 

 1) Required Flight

      Attendant Seats

B

-

-

(M)(O) One seat position or assembly (dual position) may be inoperative provided:

a)       Affected seat position or seat assembly is not occupied,

b)       Flight attendant(s) displaced by inoperative seat(s) occupies either an adjacent flight attendant seat or the passenger seat which is most accessible to the inoperative seat(s), so as to most effectively perform assigned duties,

c)       Alternate procedures are established and used as published in crewmember manuals,

d)       Folding type seat stows automatically or is secured in the retracted position,

e)       Passenger seat assigned to flight attendant is placarded “FOR FLIGHT ATTENDANT USE ONLY”, and

f)         If the ventral door attendant’s seat

      (727-100 without two TYPE I exits only)

      is inoperative, the aft entry restraint aisle

      strap will not be used, and a passenger

      announcement will be made to stay

      clear until the door is opened.

 

NOTE 1: An automatic folding seat that will not

               stow is considered inoperative.

 

NOTE 2: A seat position with an inoperative or

               missing restraint system is considered

               inoperative.

 

 

 

 

 

 

(Continued) 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

25-3

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

25 EQUIPMENT/FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

25-05

Flight Attendant Seat Assembly (Single or Dual Position)

(Cont’d)

 

 

 

 

 

 

 

 1) Required Flight

     Attendant Seats

     (Cont’d)

 

 

 

NOTE 3: Individual operators, when operating

               with inoperative seats, will consider

               the locations and combinations of

               seats to ensure that the proximity to

               exits and distribution requirements of

               the applicable FAR are met.

 

NOTE 4: If one side of a dual seat assembly is

               inoperative and a flight attendant is

               displaced to the adjacent seat, the

               adjacent seat must operate normally.

 

 

 

 2) Excess Flight

     Attendant Seats

C

-

-

(M) May be inoperative provided:

a)       Affected seat position or seat assembly is not occupied, and

b)       Folding type seat stows automatically or is secured in the retracted position.

 

NOTE 1: An automatic folding seat that will not

               stow automatically is considered

               inoperative.

 

NOTE 2: A seat position with an inoperative or

               missing restraint system is considered

               inoperative.

 

 

 

 3) All Cargo

     Configuration

 

 

 

 

 

 

 

 

 

 

D

-

-

May be inoperative provided affected seat or

seat assembly is not occupied.

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

25-4

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

25 EQUIPMENT/FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

25-06

Pallet Locks/Cargo Restraint Systems

 

 

 

 

 

 

 

 1) Passenger Pallet

     Locks

C

-

-

A maximum of one per pallet may be inoperative provided:

a)       Three seats in the group associated

       with that lock are blocked by folding

       and securing the backrests in a forward

       position, and

b)       If more than one lock is inoperative open the pallet must be removed.

 

 

 

 

 

 

 

 

 

 

 2) Cargo Restraint

     Systems

 

 

A

-

-

(M) May be inoperative, or missing provided:

      a)  Acceptable cargo loading limits from an

           approved source, i.e., an approved Cargo

           Loading Manual, Cargo Handling Manual,

           or Weight and Balance Document are

           observed, and

b)  Repairs are made prior to the

     completion of the next heavy

     maintenance visit.    

 

 

|

|

|

|

|

|

|

|

 

 

C

-

-

May be inoperative, or missing provided cargo compartment remains empty.

 

 

25-07

Passenger Cabin Window Shades

D

-

0

May be inoperative in a compartment used for cargo provided AFM Limitations are observed.

 

NOTE: Passenger Cabin Window Shades in

            compartments configured for passengers

            only are considered a passenger

            convenience item.

 

 

25-08

“FASTEN SEAT BELT WHILE SEATED” Sign or Placard

 

C

-

-

One or more signs or placards may be illegible

or missing provided a legible sign or placard is visible from each occupied passenger seat.

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

25-5

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

25 EQUIPMENT/FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

25-09

Flight Attendant Flashlight Holders/ Flashlights

 

 

 

 

 

 

 

 1) Passenger and

     Mixed

     Configurations

C

-

-

May be inoperative or missing provided the crewmember assigned to the associated position has a normally operating flashlight of equivalent lighting characteristics readily available.

 

 

***

 2) Cargo

     Configuration

 

 

D

-

0

 

 

25-10

AFT Airstair

Access Panels

 

 

 

 

Deleted, Rev. 39.

 

25-11

 ***

Flight Crew Power Seat Adjustment System

 

D

-

0

May be inoperative provided manual seat adjustment system operates normally.

 

25-12

Non-Essential Equipment and Furnishings (NEF)

 

 

 

  

 

-

0

May be inoperative, damaged or missing provided that the item(s) is deferred in accordance with the NEF deferral program. The NEF program, procedures and processes are outlined in the operator’s (insert name) Manual. (M) and (O) procedures, if required, must be available to the flight crew and included in the operator’s appropriate document.

 

NOTE: Exterior lavatory door ash trays are not

            NEF items.

 

 

 

 

 

 

 

 

 

 

 

 

|

|

|

|

|

|

|

|

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

25-6

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

25 EQUIPMENT/FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

25-13

Passenger Seat(s)

 

 

 

 

 

 

 

 

D

-

-

May be inoperative provided:

a)       Seat does not block an Emergency Exit,

b)       Seat does not restrict any passenger from access to the main aircraft aisle, and

c)       The affected seat(s) are blocked and placarded “DO NOT OCCUPY”.

 

NOTE 1: A seat with an inoperative seat belt

               is considered inoperative.

 

NOTE 2: Inoperative seats do not affect the

               required number of Flight Attendants.

 

NOTE 3: Affected seat(s) may include the

              seat(s) behind and/or adjacent

              outboard seats.

 

|

 

 1) Recline

     Mechanism

D

-

-

(M) May be inoperative and seat occupied provided seat back is secured in the full

up-right position.

 

|

|

 

 

D

-

-

May be inoperative and seat occupied provided seat back is immovable in full upright position.

 

|

|

 

 2) Underseat

     Baggage

     Restraining Bars

 

 

 

 

 

 

 

C

-

-

(O) May be inoperative provided:

a)       Baggage is not stowed under seat with inoperative restraining bar,

b)       Associated seat is placarded “DO NOT STOW BAGGAGE UNDER THIS SEAT”, and

c)       Procedures are established to alert Cabin Crew of inoperative restraining bar.

  

 

 

 

 

 

 

(Continued)

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

25-7

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

25 EQUIPMENT/FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

25-13

Passenger Seat(s)

(Cont’d)

 

 

 

 

 

 

 

 3) Armrest

 

 

 

 

 

 

 

a)  Armrest with

     Recline

     Mechanism

 

 

 

 

D

-

-

(M)(O) May be inoperative or missing and seat occupied provided:

       a)  Armrest does not block an Emergency

            Exit,

       b)  Armrest does not restrict any passenger

            from access to the main aircraft aisle,

            and

       c)  If armrest is missing, seat is secured in

            the full upright position.

  

|

|

|

|

|

|

|

|

|

 

b)  Armrest

     without

     Recline

     Mechanism

 

 

 

D

-

-

May be inoperative or missing and seat

occupied provided:

      a)  Armrest does not block an Emergency

           Exit, and

      b)  Armrest does not restrict any passenger

           from access to the main aircraft aisle.

 

|

|

|

|

 

 4) Seat Belt Air Bag

     Restraint System

 

 

 

 

 

|

|

 

a)  Seat Belt Air

     Bags Required

      by CFR  

 

D

-

-

May be inoperative provided affected seat is blocked and placarded  “DO NOT OCCUPY”.

|

|

|

 

b)  Seat Belt Air

     Bags Not

     Required by

     CFR

 

 

 

 

 

 

 

 

 

 

D

-

-

May be inoperative or disconnected provided  seat belt operates normally.

|

|

|

|

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

25-8

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

25 EQUIPMENT/FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

25-14

Observer Seat(s)

 

 

 

 

 

 

 

 1) Primary Observer

     Seat (Including

     associated

     equipment)

 

 

A

-

-

May be inoperative provided:

a)       A passenger seat in the passenger cabin is made available to an FAA inspector for the performance of official duties, and

b)       Repairs are made within two flight days.

 

 

 

 

 

 

 

 

A

-

-

May be inoperative provided:

a)       Secondary observer’s seat is available to the FAA inspector for performance of official duties, and

b)       Repairs are made within two flight days.

 

 

 

 

 

 

 

 

 

 

 

 

A

-

-

May be inoperative provided:

a)       Required minimum safety equipment (safety belt and oxygen) is available,

b)       Seat is acceptable to the FAA inspector for performance of official duties, and

c)       Repairs are made within two flight days.

 

NOTE 1: These provisos are intended to provide

               for occupancy of the above seats by an

               FAA inspector when the minimum

               safety equipment (oxygen and safety

               belt) is functional and the inspector

               determines the conditions to be

               acceptable.

 

  NOTE 2:  The pilot-in-command will determine if

                  the minimum safety equipment is

                functional for other persons authorized

                to occupy any observer seat(s).

 

 

***

 2) Additional 

     Observer

     Seat(s) (Including

     associated

     equipment)

 

D

-

0

NOTE: The Pilot-in Command will determine if

             the minimum safety equipment is

             functional for other persons authorized

             to occupy any observer seat(s).

 

 

25-15

Flight Attendant

Call System

 

 

 

 

Deleted, Rev. 38. (Included in Item 25-12.)

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

25-9

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

25 EQUIPMENT/FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

25-16

Lower Cargo Door Barrier Curtain

C

-

0

May be inoperative or may be dysfunctional and not perform its intended function provided interior netting system is utilized to keep cargo free of cargo door.

 

 

 

 

 

 

 

See NOTE below.

 

 

 

 

C

-

0

May be inoperative or may be dysfunctional and not perform its intended function provided “pod” cargo containers are utilized to keep cargo free of cargo door.

 

 

 

 

 

 

 

See NOTE below.

 

 

 

 

C

-

0

May be inoperative or dysfunctional and not perform its intended function provided cargo compartment remains empty.

 

NOTE: Lower Cargo Door Barrier Curtain may

            have two torn non-contiguous ribs and/or

            be missing two non-contiguous support

            clips and still be considered to provide its

            intended function.

 

 

25-17

***

Interior Cargo Hold Nets And Net Support Fittings

C

-

0

All may be inoperative or missing provided

Lower Cargo Door Barrier Curtain is functional and operates normally.

 

 

 

 

C

-

0

All may be inoperative or missing provided “Pod” cargo containers are utilized to keep cargo free of cargo door.

 

 

 

 

C

-

0

All may be inoperative or missing provided cargo compartment remains empty.

 

 

25-18

***

Onboard Cargo Container System

C

1

0

(M) May be inoperative provided the system is deactivated and secured.

 

 

25-19

Flotation Equipment (Crew and Passenger)

 

 

C

-

-

Any in excess of that required by FAR may be inoperative or missing.

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

25-10

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

25 EQUIPMENT/FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

25-20

Flight Crew Seats

 

 

 

 

 

 

 

 1) Armrests

B

6

0

(M) May be inoperative in the up position or removed provided seat is acceptable to the affected crewmember.

 

 

 

 2) Lumbar/Thigh

     Supports

     Adjustments

 

C

-

0

May be inoperative provided seat is acceptable to the affected crewmember.

 

 

 

 3) Recline System

A

-

0

May be inoperative provided:

a)       Seat is secured in an upright position acceptable to the affected crewmember, and

b)       Repairs are made within three landings.

 

 

25-21

Exterior Lavatory

Door Ashtrays

 

 

 

 

 

 

 

 1) Airplanes with

     more than one

     exterior lavatory

     door ashtray

     installed

 

A

-

-

Up to and including fifty percent may be inoperative or missing provided repairs are

made within 10 calendar days.

|

|

|

 

 

A

-

0

More than fifty percent may be inoperative or missing provided repairs are made within 3 calendar days.

 

 NOTE: Both crew and passenger lavatories are

             included in the total aircraft lavatory

             count.

 

|

|

 

 

|

|

|

 

 2) Airplanes with

     only one exterior

     lavatory door

     ashtray installed

 

A

1

0

May be inoperative or missing provided repairs are made within 10 calendar days.

 

 

 

 

 

 

 

 

|

|

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

25-11

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

25 EQUIPMENT/FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

25-22

Emergency Medical Equipment

 

 

 

 

 

 

 

 1) Emergency

     Medical Kit (EMK)

     and/or Associated

     Equipment

A

-

0

(O) May be inoperative provided:

     a)  EMK is sealed in a manner that will

          identify it as a unit that can not be

          mistaken for a fully serviceable unit, and

     b)  Repairs or replacements are made within

          1 flight.  

 

|

|

|

|

|

|

 

 

D

-

-

Any in excess of those required by FAR may be incomplete, missing, or inoperative.

 

 

 

 2) First Aid Kit  (FAK)

     and/or Associated

     Equipment

A

-

-

(O) If more that one is required by FAR, only one of the required first aid kits may be incomplete, missing or inoperative provided:

     a)  FAK is sealed in a manner that will

          identify it as a unit that can not be

          mistaken for a fully serviceable unit, and

     b)  Repairs or replacements are made within

          1 flight.  

 

|

|

|

|

|

|

 

 

D

-

-

Any in excess of those required by FAR may be incomplete, missing, or inoperative.

 

 

 

 3) Automatic External

     Defibrillator (AED)

     and/or Associated

     Equipment

 

A

-

0

(O) May be incomplete, missing or inoperative provided:

     a)  AED is sealed in a manner that will

          identify it as a unit that can not be

          mistaken for a fully serviceable unit, and

     b)  Repairs or replacements are made within

          1 flight.  

 

|

|

|

|

|

|

 

 

 

 

D

-

-

Any in excess of those required by FAR may be incomplete, missing, or inoperative.

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

25-12

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

25 EQUIPMENT/FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

25-23

Galley Waste Receptacles Access Doors/Covers

 

 

 

 

 

 

C

-

-

(M)(O) May be inoperative provided:

a)       The container is empty and the access

       is secured to prevent waste introduction

       into the compartment, and

b)       Procedures are established to ensure that sufficient galley waste receptacles are available to accommodate all waste that may be generated on a flight.

 

 

25-24

Overhead Storage Bin(s)/Cabin and Galley Storage Compartment/Closets

 

(Limited relief for 14 CFR Part 382 items)

 

 

 

 

 

 

 

 

 

 

C

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

-

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

-

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

(M) May be inoperative provided:

a)       Procedures are established to secure the affected bin, compartment or closet in the CLOSED position,

b)       Affected bin, compartment or closet is prominently placarded DO NOT USE,

c)       Any emergency equipment located in the affected compartment is considered inoperative, and

d)       Affected bin, compartment or closet is not used for storage of any item(s) except for those permanently affixed.

 

 NOTE: For overhead bins, if no partitions are             installed, the entire overhead storage             compartment is considered inoperative.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

(Continued)

 

 

 

|

|

|

|

|

|

|

|

|

 

 

 

|

 

|

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

25-13

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

25 EQUIPMENT/FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

25-24

Overhead Storage Bin(s)/Cabin and Galley Storage Compartment/Closets

(Cont’d)

 

(Limited relief for 14 CFR Part 382 items)

 

C

-

-

(M)(O) May be inoperative provided:

a)        For non-retractable doors, affected                 door is removed,

b)        For retractable doors, affected door is removed or secured in the retracted (fully open) position,

c)        Affected bin, compartment or closet is not used for storage of any items, except those permanently affixed,

d)        Affected bin, compartment or closet is prominently placarded DO NOT USE,

e)        Procedures are established and used to alert crew members and passengers of inoperative bins, compartments or closets and

f)          Passengers are briefed that affected bin, compartment or closet is not used.

 

NOTE 1:  For overhead bins, if no partitions are installed, the entire overhead bin is considered inoperative.

 

NOTE 2:  Any emergency equipment located in the affected bin, compartment or closet (permanently affixed) is available for use.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

|

|

|

|

|

|

|

|

|

|

|

|

|

|

|

|

|

|

|

|

|

|

|

|

|

|

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

26-1

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

26 FIRE PROTECTION

 

 

 

 

 

 

 

 

 

 

 

26-01

 Engine Fire

 Extinguisher 

 Discharge Lights

 

C

2

0

 

 

26-02

 Engine Fire

 Extinguisher

 Thermal/ Discharge

 Discs

 

C

3

0

(M) May be missing provided gauge readings

or other acceptable procedures are used to

verify adequate charge.

 

26-03

 DELETED

 

 

 

 

 

 

26-04

 DELETED

 

 

 

 

 

 

26-05

 Engine Fire

 Detection

 Test System

C

1

0

(M) Flight deck test feature may be inoperative

provided an alternate procedure is established

to assure integrity of the system before first

flight of the day.

 

 

26-06

 Engine Overheat

 and Fire Detection

 System

 (Kidde System)

 

C

6

3

 One complete system (A or B) on each 

 engine may be inoperative.

 

26-07

 Portable Fire

 Extinguishers

 

 

 

 

 

 

 

 

D

-

-

 Any in excess of those required by FAR

 may be inoperative or missing provided:

a)       The inoperative fire extinguisher is

tagged inoperative, removed from

installed location, and placed out of

sight so it cannot be mistaken for a functional unit, and

b)       Required distribution is maintained.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

26-2

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

26 FIRE PROTECTION

 

 

 

 

 

 

 

 

 

 

 

26-08

 Wheel Well Fire 

 Detection System

C

1

0

 (O) May be inoperative provided:

a)       Brakes are inspected and are cool to the touch immediately before starting engines, and

b)       After takeoff, landing gear remains extended for 10 minutes to avoid the possibility to retracting a wheel overheated by a dragging brake.

 

NOTE 1: Performance is the prime

               consideration. When an engine fails at

               V1 or later, landing gear should be

               retracted until performance penalties

               associated with gear extended are not

               a problem.

 

NOTE 2: Pilots should consider the effects

               associated with delayed raising or

               lowering of the landing gear during

               winter operations from contaminated

               runways.

 

 

26-09

 Fire Warning

 Ground Fault

 Detector Systems

 

C

3

0

 

 

26-10

 Overheat Detection

 System

 (Strut and Body)

 

 

 

 

 

 

 

 1) Lower Aft Body

     System

C

1

0

(M)(O) May be inoperative provided:

a)       No bleed air is used the airplane, and

b)       Both packs are considered inoperative.

 

 

 

 2) Flight Deck Test

     Feature

C

1

0

(M) May be inoperative provided system

 integrity is verified by an approved alternate 

 procedure once each flight day.

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

26-3

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

26 FIRE PROTECTION

 

 

 

 

26-11

 APU Fire

 Protection/Detection

 System

C

1

0

 (M)(O) May be inoperative and APU

 used provided:

a)       APU is used for starting of  one engine only, and          

b)       A fire guard is stationed on the

ground adjacent to the APU at

at all times while it is operating,

and for at least 5 minutes

following APU shutdown.

 

 

 

 

C

1

0

 May be inoperative provided APU is not

 used.

 

 

 

 1) APU Test Feature

C

1

0

 (M) May be inoperative provided an

 approved procedure is established to

 verify integrity of the system.

 

 

 

 2) External Warning

     Horn and/or

     Warning Light

C

1

0

 May be inoperative provided during the

 entire period of APU operation, the

 system is monitored at the flight deck

 APU control panel.

 

 

26-12

 APU Fire

 Exitinguisher

 Discharge Disc

C

1

0

 (M)(O) May be missing provided gauge

 reading is used to verify adequate

 charge.

 

 

 

 

C

1

0

 (M)(O) May be missing provided HTL  

 type bottle is installed, and integrity is

 verified by weighing the bottle once

 each flight day.

 

 

 

 

C

1

0

 (M)(O) May be missing provided APU

 Fire Protection/Detection System is

 considered Inoperative.

 

 

 

 

C

1

0

 May be missing provided APU is not

 operated.

 

 

26-13

 Engine Fire Detector

 Inoperative Lights

 

C

-

0

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

26-4

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

26 FIRE PROTECTION

 

 

 

 

26-14

 Main Deck Cargo

 Compartment Smoke

 Detection System

 (Including STC

 SA1798SO)

 

 

 

 

 

 

 

 

 

 

 

C

-

0

 (O) May be inoperative provided procedures

 are established and used to ensure the

 associated compartment remains empty, or is

 verified to contain only empty cargo handling

 equipment, ballast (ballast may be loaded in

 ULDS), and/or Fly Away Kits.

 

NOTE 1: Class E cargo compartments require

               only the installation of smoke or fire

               detection systems, not suppression.

 

NOTE 2: Operator MELs must define which

               items are approved for inclusion in

               the Fly Away Kits, and which materials

               can be used as ballast.

 

 

 

 1) Passenger and

     Combi 

     Configurations

C

1

1

 Those lamps corresponding to pickup

 points in the passenger compartment

 may be inoperative.

 

 

 

 2) 727-200F

 

 

 

 

 

 

 

     a) Amplifier A

C

1

0

 May be inoperative provided Amplifier B

 operates normally.

 

 

 

     b) Amplifier B

C

1

0

  May be inoperative provided Amplifier A

 operates normally.

 

 

 

 3) 727-100

     (STC # SA189650

     Conversion)

C

1

0

 May be inoperative provided restrictions

 in AFM Supplement are observed.

 

 

 

 

  4) Fault(s) Indicated

      by Illumination of

      the “MX” Indicator

     (STC ST3123SE-T

     and ST1600SE-T)

 

 

 

 

 

 

B

-

-

 Dispatch with the “MX” indicator illuminated is

 permitted provided the green “SYS OK”

 indicator remains illuminated.

 

NOTE: This is a fault tolerant system and the

             unit will continue to perform its intended

             function as long as the green “SYS OK”

             Indicator remains Illuminated.

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

26-5

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

26 FIRE PROTECTION

 

 

 

 

 

 

 

 

 

 

 

26-15

 Lavatory Fire

 Extinguisher

 Systems

 

 

 

 

 

 

 

 

 1) Passenger

     Configuration

C

-

-

For each lavatory, the lavatory fire extinguisher system may be inoperative provided the associated lavatory Smoke Detection System operates normally.

 

 

 

 

C

-

-

(M)(O) For each lavatory, the lavatory fire extinguisher system may be inoperative provided:

       a) Lavatory waste receptacle is empty,

       b) Associated lavatory door is locked closed

           and placarded, "INOPERTIVE - DO NOT

           ENTER", and

       c) Lavatory is used only by crewmembers.

 

NOTE: These provisos are not intended to

            prohibit lavatory use or inspections by

            crewmembers.

 



 

 

 2) Cargo  

     Configuration

 

D

-

0

 

|

|

26-16

Master Fire Warning

Bell Cutout Switches

C

-

1

(O) When multiple switches are installed,

 may be inoperative provided:

a)       One operates normally at a pilot station, and

b)       All other components of the fire warning system, both visual and aural, operate normally.

 

 

 

 

 

 

 

 




 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

26-6

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

26 FIRE PROTECTION

 

 

 

 

 

 

 

 

 

 

 

26-17

 Lavatory Smoke

 Detection Systems

 

 

 

 

 

 

 

 1) Passenger

     Configuration

C

-

-

(M)(O) For each lavatory, the lavatory smoke detection system may be inoperative provided:

a)       Lavatory waste receptacle is empty,

b)       Associated lavatory door is locked

      closed and placarded, “INOPERATIVE-

      DO NOT ENTER”, and

c)       Lavatory is used only by crewmembers.

 

NOTE: These provisos are not intended to

            prohibit lavatory use or inspections by

            crewmembers.

 

 

 

2) Cargo  

    Configuration

D

-

0

 

|

|

 

26-18

***

 Passenger

 Compartment Smoke

 Detection System  

 (Add On System)

 

 

 

 

 

 

 

 1) Pick Points

 

 

 

 

 

 

 

      a) Smoke

          Detectors

C

-

-

Sensing lamps within passenger compartments occupied by passengers or flight attendants may be inoperative.

 

 

 

      b) Flame

          Detectors

 

C

-

-

 

 

 

 2) Smoke Test 

     System

C

1

0

May be inoperative provided flame (heat) test system operates normally.

 

 

 

 3) Flame (Heat)

     Test System

C

1

0

May be inoperative provided smoke test system operates normally.

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

26-7

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

26 FIRE PROTECTION

 

 

 

 

 

 

 

 

 

 

 

26-19

***

 

 Lower Cargo 

 Compartment Fire

 Detection/

 Suppression

 System

C

-

0

(O) May be inoperative provided procedures are established and used to ensure the associated compartment remains empty, or is verified to contain only empty cargo handling equipment, ballast (ballast may be loaded in ULDS), and/or Fly Away Kits.

 

NOTE 1: Class E cargo compartments require

            only the installation of smoke or fire

            detection systems,  not suppression.

 

NOTE 2: Operator MELs must define which

            items are approved for inclusion in

            the Fly Away Kits, and which

            materials can be used as ballast.

 

 

 

 1) Fault(s) Indicated

     by llumination of

     the “MX” Indicator

  (STC ST00399LA-D,

   ST00765LA-D, and

   ST00991LA-D only)

 

B

-

-

Dispatch with the “MX” indicator illuminated is permitted provided the green “SYS OK” indicator remains illuminated.

 

NOTE: This is a fault tolerant system and the

            unit will continue to perform its intended

            function as long as the green “SYS OK”

         indicator remains illuminated.

      

 

 

     a) Display of FWD

    INOP and /or

    AFT INOP

    messages

 

 

 

 

 

 

 

B

-

-

(O) May be displayed provided:

a)  The green “SYS OK” indicator

        remains illuminated, and

   b)  Procedures are established and

     used to ensure the associated

     compartment remains empty, or

     is verified to contain only empty

     cargo handling equipment,

     ballast (ballast may be loaded in

     ULDS), and/or Fly Away Kits.

 

 NOTE: Operator MELs must define which

          items are approved for inclusion in

          the Fly Away Kits, and which

          materials can be used as ballast.

 

(Continued)

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

26-8

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

26 FIRE PROTECTION

 

 

 

 

 

 

 

 

 

 

 

26-19

***

 

 Lower Cargo 

 Compartment Fire

 Detection/

 Suppression

 System

 (Cont’d)

 

 

 

 

 

 

 

 1) Fault(s) Indicated

     by llumination of

     the “MX” Indicator

  (STC ST00399LA-D,

   ST00765LA-D, and

   ST00991LA-D only)

   (Cont’d)

 

 

 

 

 

 

 

      b) Smoke

          Detectors

C

-

-

(O) One smoke detector may be inoperative in each compartment provided the “SYS OK” indicator on the CDU remains illuminated.

 

 NOTE: The “MX” indicator on the CDU will 

             remain illuminated.

 

 

 

 2) Smoke Detection

     Channels (STC

     ST00387LA-D and

     ST01285LA)

C

4

2

(O) One channel for each cargo compartment may be inoperative provided the operative channel in the associated compartment is selected and verified to operate normally prior

to each departure.

 

 

 

a)  Control panel 

    ALARMS OFF

    Switch

C

1

0

(M)(O) May be inoperative provided the master Fire Warning Bell cutout switch silences the Cargo Bay Fire Protection Fire Warning Bell.

 

 

 

 

 

 

 

 

 

 

(Continued)

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

26-9

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

26 FIRE PROTECTION

 

 

 

 

26-19

***

 

 Lower Cargo 

 Compartment Fire

 Detection/

 Suppression

 System

 (Cont’d)

 

 

 

 

 

 

 

 3) Smoke Detection

      Loops

      (STC ST01742AT

      and ST02144AT)

 

C

4

2

(O) One loop (A or B) in each compartment may be inoperative provided the opposite loop is checked to operate normally.

 

 

      a) DET Lights

C

4

2

(O) One light in each compartment may be inoperative provided the opposite loop in the associated compartment is checked to operate normally before each departure.

 

 

 

      b) FAIL Lights

C

4

2

(O) One light in each compartment may be inoperative provided the remaining loop in the associated compartment is checked to operate normally before each departure.

 

 

 

      c) Fault Panel

          (E & E

          Compartment)

 

D

1

0

 

 

 

 

 

 

      d) Smoke

           Detectors

 

 

 

 

 

 

 

 

          1) Single

              Optical

              (Single  

              Chamber)

              Detectors

 

C

-

-

(O) One detector in each detector enclosure may be inoperative provided the remaining detector enclosure is verified to operate normally before each departure.

 

 

 

          2) Dual Sensor

              (Dual

              Chamber)

              Detectors

 

 

 

 

C

-

-

(O) One chamber may be inoperative provided the remaining chamber is verified to operate normally before each departure.

 

 

 

(Continued)

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

26-10

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

26 FIRE PROTECTION

 

 

 

 

 

 

 

 

 

 

 

26-19

***

 

 Lower Cargo 

 Compartment Fire

 Detection/

 Suppression

 System

 (Cont’d)

 

 

 

 

 

 

 

 4) “FAULT” Light on

      Cargo Fire Flight

      Deck Unit (CFFU)

     (STC ST00089BO)

 

 

 

C

1

0

(M) May be inoperative provided:

        a)  All other CFFU annunciators

    illuminate during test, and

        b)  Cargo Fire Maintenance Unit (CFMU)

             self test is performed prior to each

             departure.    

    

 

 

a)  Smoke

    Detectors

 

C

12

6

(M) May be inoperative provided defective

smoke detectors are not in the same zone.

 

 

     b) Glareshield

         “CARGO FIRE”

         Annunciator

 

C

1

0

(M)(O) May be inoperative provided all CFFU annunciators are operative.

 

 

 5) Smoke Detection

     Loops

     (STC ST01979AT)

C

4

2

(O) One loop for each cargo compartment may be inoperative provided the remaining loop in

the associated compartment is verified to

operate normally prior to each departure.

 

 

26-20

***

 Lower Cargo 

 Compartment Fire

 Suppression System

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Deleted Rev.42, combined with Item 19.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

27-1

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

27 FLIGHT CONTROLS

 

 

 

 

 

 

 

 

 

 

 

27-01

 DELETED

 

 

 

 

 

 

27-02

 Stabilizer Main

 Electric Trim   

 Operating Light

 

C

1

0

 

 

27-03

 Trailing Edge Flap

 Position Indicating

 Systems (Outboard)

 

 

 

 

Deleted, Rev.38

 

27-04

 DELETED

 

 

 

 

 

 

27-05

 DELETED

 

 

 

 

 

 

27-06

 Leading Edge

 Device Position

 Light System

 

 

C

2

1

(O) F/E annunciator panel lights may be inoperative provided forward instrument

panel L.E.D. position indicator lights operate normally.

 

 

 

C

2

1

(O) Forward instrument panel L.E.D. position indicator lights may be inoperative provided the F/E annunciator lights are used to confirm proper L.E.D. position after each movement of the flap handle to position UP, 2 and 5 degrees as follows:

          1)  Flaps UP – ALL

               L.. E. D. ‘s  UP,

          2)  Flaps  2  degrees –

               No’s. 2, 3,     6, 7

          3)  Flaps  5  degrees - ALL

               Extended.

 

 

27-07

 DELETED

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

27-2

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

27 FLIGHT CONTROLS

 

 

 

 

 

 

 

 

 

 

 

27-08

 Rudder Position 

 Indicators

 

 

 

 

 

 

 

 

 C

2

0

(M)(O) One or both may be inoperative provided:

a)   Rudder is visually checked for

     proper movement before each 

     departure,

b)   AFM yaw damper limitations are

     observed, and

c)   Associated power control unit

        low pressure lights operate

        normally.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

C

2

0

(M)(O) One or both may be inoperative provided:

a)   Rudder is visually checked for

     proper movement before each

     departure,

b)   Associated power control unit

      low pressure lights operate

      normally, and

c)   Associated yaw damper is

     verified to operate normally prior

     to each departure using the test

     function.

 

 

27-09

 DELETED

 

 

 

 

 

 

27-10

 Elevator Position

 Indicators

 

C

2

1

One may be inoperative provided remaining indicator operates normally.

 

 

 

C

2

0

(M) Both may be inoperative provided elevator is visually checked for proper movement once each flight day.

 

 

27-11

 DELETED

 

 

 

 

 

 

27-12

 DELETED

 

 

 

 

 

 

27-13

 DELETED

 

 

 

 

 

 

27-14

 DELETED

 

 

 

 

 

 

27-15

 DELETED

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

27-3

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

27 FLIGHT CONTROLS

 

 

 

 

 

 

 

 

 

 

 

27-16

 PCU Low

 Pressure Lights

 (A and B Systems)

 

C

6

3

One light on each control may be inoperative provided all other flight deck hydraulic pressure and quantity gauges, and warning lights operate normally.

 

 

27-17

 Stabilizer Cruise

 Trim System

 

 

 

 

 

 

 

 1) 727-100, 100QF

 

    C

1

0

 

 

 

 2) 727-200

 

C

1

0

(O) May be inoperative provided:

a)   Altitude is limited to 15,000 feel

      MSL or less,

b)   Airspeed is limited to 250 KIAS

      or less,

c)   Aft CG is limited to 32% MAC,

     and

d)   Pilot’s panel is placarded to

     indicate airspeed and altitude

     limitations.

 

 NOTE: Autopilot pitch axis will be

             inoperative on all models.

 

 

27-18

 Stall Warning

 Systems

C

-

1

(M)(O) Systems in excess of one may be inoperative provided remaining system is verified to operate normally before each departure.

 

 

 

 1) Vane Heater/

     Power Failure

     Light

C

1

0

 May be inoperative provided:

a)   Stall warning system operates

     normally, and

b)   Airplane is not operated in known or

      forecast icing conditions.

 

 

 

 2) Test Indicator 

     Rotating Card

 

C

-

0

(O) May be inoperative provided stall warning system operates normally.

 

 

27-19

 DELETED

 

 

 

 

 

 

27-20

 Stabilizer Actuated

 Elevator Trim

 (Neutral Shift)

C

1

0

May be inoperative provided autopilot is not

used below 1,500 feet AGL during approach

and landing.

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

27-4

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

27 FLIGHT CONTROLS

 

 

 

 

 

 

 

 

 

 

 

27-21

***

 

 

 Auto Spoiler System

D

1

0

(M)(O) May be inoperative provided:

   a)  System is electrically 

         deactivated, and

 b)  AFM performance decrements

      are observed.

 

 

27-22

 Rudder Load

 Limiter System

 (Lower Rudder)

C

1

0

(M)(O) Low pressure mode (800 psi)

             may be inoperative provided:

a)   Rudder load limiter circuit

     breaker is pulled and collared,

b)   Altitude is limited to 10,000 feet

     MSL or below, and

c)   Airspeed does not exceed 240

     KIAS.

 

 

 

 

C

1

0

Low pressure mode (800 psi) may be inoperative provided:

a)  System “A” (lower rudder)

     switch is turned off after flaps

     have been retracted, and on

     before flaps are extended, and

b)   AFM yaw damper inoperative

     speed and altitude limitations are

     complied with.

 

NOTE: Failure to restore power to the lower

         rudder before approach may reduce

         crosswind landing capability.

 

 

27-23

 Control Wheel Trim

 Switches

C

2

1

Copilots may be inoperative provided stabilizer trim system (including pilot’s control wheel

switch and cruise trim switch) operates normally.

 

 

27-24

 Flap Load

 Relief System

C

1

0

(O) May be inoperative provided flaps 40 setting is not used above landing weight of 142,500 lbs. (64,637 kg).

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

27-5

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

27 FLIGHT CONTROLS

 

 

 

 

 

 

 

 

 

 

 

27-25

***

 Stabilizer Main Trim

 Heater System

 (Add on System)

 

 

 

C

 

 

 

 

 

1

 

 

 

 

 

0

 

 

 

 

 

(M) May be inoperative provided system is deactivated and secured.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

28-1

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

28 FUEL

 

 

 

 

 

 

 

 

 

 

 

28-01

 Pressure Fueling

 System

C

1

0

(M) May be inoperative provided alternate procedures are established and used.

 

NOTE: Any portion of the system which

            operates normally may be used.

 

 

 

 1) Volumetric Top

     Off (VTO Units)

A

3

0

(M) May be inoperative provided:

a)  An alternate means to determine

     fuel quantity during the fueling

     process is used, and

b)  Operations are limited to not more then

      three flight days before repair is made.

 

 

 

 

C

3

0

May be inoperative provided associated fuel quantity gauge on refueling panel operates normally and is monitored during refueling.

 

 

 

 

C

3

0

May be inoperative provided:

a)       Associated fuel quantity gauge on Flight Engineer’s panel operates normally,

b)       Communications procedures are established between the flight deck and the person refueling, and

c)       Fuel quantity is monitored from the flight deck during refueling.

 

 

28-02

 Refueling Control

 Panel Quantity

 Gauges

C

-

0

(M) Any or all may be inoperative providing an 

      acceptable alternate procedure is used to

      verify fuel quantity during fueling.

 

 

28-03

 Manually Operated

 Defueling Valve

 

 

 

 

 

 

 

 

 

C

1

0

(M) May be inoperative provided it remains closed.

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

28-2

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

28 FUEL

 

 

 

 

 

 

 

 

 

 

 

28-04

 Fuel Boost Pumps

 (Tanks 1, 2, and 3)

 

 

 

 

 

 

 

 1) All Models Except 

     727-100QF

 

C

8

-

(O) May be inoperative provided AFM

Limitations are observed.

 

 

 2) 727-100QF

A

8

-

(M)(O) May be inoperative provided:

a)       AFM Limitations are observed,

b)       Continuous ignition is verified to operate normally one each flight day, and

c)       Operations are limited to not

      more then three flight days

      before repair is made.

 

 

28-05

 DELETED

 

 

 

 

 

 

28-06

 Fuel Boost Pump

 Low Pressure

 Warning Lights

B

-

-

(M)(O) One may be inoperative provided:

a)       All pumps in associated tank operate normally, and

b)       During takeoff, initial climb and landing, the tank with the inoperative warning light is manifolded to another tank where all boost pumps operate normally.

 

 

 

 

C

-

-

May be inoperative provided associated pump

is inoperative.

 

 

28-07

 Fuel Crossfeed

 Manifold Valves

C

3

2

(M)(O) One may be inoperative provided the valve is secured open.

 

 

28-08

 Fuel Valve

 In-Transit Lights

 

 

 

 

 

 

 

 1) Manifold Valve

     Lights

C

3

2

(M)(O) One may be inoperative provided

associated valve is verified to operate

normally before each departure.

 

 

 

 

C

3

2

(M)(O) One may be inoperative provided

 associated valve is locked open.

 

(Continued)

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

28-3

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

28 FUEL

 

 

 

 

 

 

 

 

 

 

 

28-08

 Fuel Valve

 In-Transit Lights

 (Cont’d)

 

 

 

 

 

 

 

 2) Fuel Shutoff Valve

     Lights

C

3

2

(M) One may be inoperative provided proper valve operation is verified by use of the fire switch, start lever, or flight engineer panel

switch prior to each takeoff.

 

 

 

 3) Fuel Dump Valve

     Lights

 

 

 

 

 

 

 

     a) 727-100/JT8D-1

C

4

0

(O) May be inoperative provided:

a)       Takeoff gross weight does not exceed 105% of the authorized maximum landing weight, and

b)       Performance is not dependent upon fuel dumping for en route engine(s) out procedures.

 

 

 

 

C

4

0

(M) May be inoperative provided operations of the nozzle valve and fuel transfer capability through the fuel dump system is verified once each flight day.

   

 

 

       b) All Other 727

           Models

C

4

0

(O) May be inoperative provided:

a)       Takeoff gross weight does not exceed maximum landing weight climb limit plus 1,850 lbs. (839 kg) for the 727-100 and 100QF, or 2,200 lbs. (998 kg) for the 727-200, and

b)       Performance is not dependent upon fuel dumping for en route engine(s) out procedures.

 

 

 

 

C

4

0

(M) May be inoperative provided operation of the nozzle valve and fuel transfer capability through the fuel dump system is verified once each flight day.

 

(Continued)

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

28-4

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

28 FUEL

 

 

 

 

 

 

 

 

 

 

 

28-08

 Fuel Valve

 In-Transit Lights

 (Cont’d)

 

 

 

 

 

 

 

 4) Fuel Dump Nozzle

     Valve Lights

 

 

 

 

 

 

 

     a) 727-100/JT8D-1

C

2

0

(O) Both may be inoperative provided:

a)       Takeoff gross weight does not exceed 105% of the authorized maximum landing weight, and

b)       Performance is not dependent upon fuel dumping for en route engine(s) out procedures.    

 

 

 

    

C

2

0

(M) Both may be inoperative provided operation of the nozzle valve and fuel transfer capability through the fuel dump system is verified once each flight day.

 

 

 

     b) All Other 727

         Models

 

 

 

 

 

 

 

 

C

2

0

(O) Both may be inoperative provided:

a)       Takeoff weight does not exceed maximum landing weight climb limit plus 1,850 lbs. (839 kg) for the 727-100 and 100QF, or 2,200 lbs. (998 kg) for the 727-200,and

b)       Performance is not dependent upon fuel dumping for en route engine(s) out procedures.

 

 

 

C

2

0

(M) Both may be inoperative provided

operation of the nozzle valve and fuel

transfer capability through the fuel dump

system is verified once each flight day.

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

28-5

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

28 FUEL

 

 

 

 

 

 

 

 

 

 

 

28-09

 Fuel Dump System

 

 

 

 

 

 

 

 1) 727-100/JT8D-1

C

1

0

May be inoperative provided:

a)       Takeoff gross weight does not exceed 105% of the authorized maximum landing weight,

b)       All jettison valves remain closed, and

c)       Performance is not dependent upon fuel dumping for en route engine(s) out procedures.

 

 

 

 2) All Other

     727 Models

     

C

1

0

May be inoperative provided:

a)       Takeoff gross weight does not exceed maximum landing weight climb limit plus 1,850 lbs. (839 kg) for the 727-100 and 100QF, or 2,200 lbs. (998 kg) for the 727-200,

b)       All jettison valves remain closed, and

c)       Performance is not dependent upon fuel dumping for en route engine(s) out procedures.

 

 

28-10

 ***

 Fuel Quantity

 Totalizer

 

D

1

0

 

 

28-11

 Flight Deck Fuel 

 Quantity Gauges

 

 

 

 

 

 

 

 1) Main Tanks (With

     associated

     Refueling Control

     quantity gauge

     operative)

 

 

 

 

 

 

 

C

3

2

(O) One may be inoperative provided:

a)       Fuel dump system (including all boost pumps) operates normally,

b)       Procedures are established to assure that fuel in the tank with the inoperative indicator will not be emptied below the non-dumpable level if fuel dump is required, and

c)       Associated fuel flow meter operates normally.

 

 

 

(Continued)

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

28-6

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

28 FUEL

 

 

 

 

 

 

 

 

 

 

 

28-11

 Flight Deck Fuel 

 Quantity Gauges

 (Cont’d)

 

 

 

 

 

 

 

 1) Main Tanks (With

      associated

      Refueling Control

      quantity gauge

      operative)

      (Cont’d)

 

C

3

2

(O) One may be inoperative provided:

a)       Associated fuel flow meter operates normally,

b)       Takeoff gross weight does not exceed the following:

1)       (727-100/JT8D-1) 105% of the authorized maximum landing weight,

2)       (727-100 and -100QF) Maximum landing climb limit weight plus 1,850 lbs. (839 kg),

3)       (727-200) Maximum landing climb limit weight plus 2,200 lbs. (998 kg), and

c)       (727-100/JT8D-1) Performance is
not dependent upon fuel dumping for
enroute engine(s) out procedures.

 

 

 

 

 

 

 

 

 

 

 

 

 

(Continued)

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

28-7

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

28 FUEL

 

 

 

 

 

 

 

 

 

 

 

28-11

 Flight Deck Fuel 

 Quantity Gauges

 (Cont’d)

 

 

 

 

 

 

 

 2) Main Tanks

      (With any or all

     associated

     Refueling Control

     quantity gauges

     inoperative)

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

C

3

2

(M)(O) One may be inoperative provided:

a)       Fuel tank is emptied and serviced with a known quantity of fuel,

b)       Associated fuel flow meter operates normally,

c)       Takeoff gross weight does not   exceed the following:

1)       (727-100/JT8D-1) 105% of the authorized maximum landing weight,

2)       (727-100 and -100QF) Maximum landing climb limit weight plus 1,850 lbs. (839 kg),

3)       (727-200) Maximum landing climb limit weight plus 2,200 lbs. (998 kg), and

d)       (727-100/JT8D-1) Performance is
not dependent upon fuel dumping for
enroute engine(s) out procedures.

 

 

 

 

 

 

 

 

 

 

 

 

 

(Continued)

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

28-8

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

28 FUEL

 

 

 

 

 

 

 

 

 

 

 

28-11

 Flight Deck Fuel 

 Quantity Gauges

 (Cont’d)

 

 

 

 

 

 

 

 2) Main Tanks (With

     any or all

     associated

     Refueling Control

     quantity gauges

     inoperative)

     (Cont’d)

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

C

3

2

(M)(O) One may be inoperative provided:

a)       Fuel tank is measured by the use of dripsticks,

b)       Associated fuel flow meter operates normally,

c)       Takeoff gross weight does not exceed the following:

1)       (727-100/JT8D-1) 105% of the authorized maximum landing weight,

2)       (727-100 and -100QF) Maximum landing climb limit weight plus 1,850 lbs. (839 kg),

3)       (727-200) Maximum landing climb limit weight plus 2,200 lbs. (998 kg), and

d)       (727-100/JT8D-1) Performance is
not dependent upon fuel dumping for
enroute engine(s) out procedures.

 

NOTE: When measuring wing tanks through use

            of dripsticks, wings must be within 1/16

            degree of level in the lateral axis if pitch

            attitude is lower then 1 degree down, or

            within 1/8 degree of level at all other

            pitch attitudes, unless SB 28-48, or

            production equivalent, is incorporated.

 

 

 

 

 

 

 

 

 

(Continued)

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

28-9

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

28 FUEL

 

 

 

 

 

 

 

 

 

 

 

28-11

 Flight Deck Fuel 

 Quantity Gauges

 (Cont’d)

 

 

 

 

 

 

 

 2) Main Tanks (With

     any or all

     associated

     Refueling Control

     quantity gauges

     inoperative)

     (Cont’d)

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

A

3

2

(M)(O) One may be inoperative provided:

a)       Fuel tank is serviced with fuel as determined from a continuous fuel log. This method is limited to:

(1)     A maximum of 5 consecutive flight legs not to exceed 10 hours total after determining original fuel quantity by measurement,

(2)     Flights on which all other lights, gauges and switches associated with that system operate normally, and

(3)     If associated tank is No.1 or No. 3, both wing tanks are serviced equally,

b)       Associated fuel flow meter operates normally,

c)       Takeoff gross weight does not exceed the following:

1)         (727-100/JT8D-1) 105% of the authorized maximum landing weight,

2)         (727-100 and -100QF) Maximum landing climb limit weight plus 1,850 lbs. (839 kg), and,

3)         (727-200) Maximum landing climb limit weight plus 2,200 lbs. (998 kg), and

d)       (727-100/JT8D-1) Performance is not dependent upon fuel dumping for

      enroute engine(s) out procedures.

 

 

 

 

(Continued)

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

28-10

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

28 FUEL

 

 

 

 

 

 

 

 

 

 

 

28-11

 Flight Deck Fuel 

 Quantity Gauges

 (Cont’d)

 

 

 

 

 

 

 

 2) Main Tanks (With

     any or all

     associated

     Refueling Control

     quantity gauges

     inoperative)

     (Cont’d)

 

 

 

 

 

 

 

C

3

2

 (M)(O) One may be inoperative provided:

a)       Fuel tank is emptied and serviced with a known quantity of fuel,

b)       Associated fuel flow meter operates normally,

c)       Fuel dump system (including all boost pumps) operates normally, and

d)       Procedures are established to assure that fuel in the tank with the inoperative indicator will not be emptied below the non-dumpable level if fuel dump is required.

 

 

 

 

C

3

2

 (M)(O) One may be inoperative  provided:

a)       Fuel tank is measured by the use of dripsticks,

b)       Associated fuel flow meter operates normally,

c)       Fuel dump system (including all boost pumps) operates normally, and

d)       Procedures are established to assure that fuel in the tank with the inoperative indicator will not be emptied below the non-dumpable level if fuel dump is required.

 

 NOTE: When measuring wing tanks through use

             of dripsticks, wings must be within 1/16

             degree of level in the lateral axis if pitch

             attitude is lower then 1 degree down,

             or within 1/8 degree of level at all other

             pitch attitudes, unless SB 28-48, or

             production equivalent, is incorporated

 

 

(Continued)

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

28-11

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

28 FUEL

 

 

 

 

 

 

 

 

 

 

 

28-11

 Flight Deck Fuel 

 Quantity Gauges

 (Cont’d)

 

 

 

 

 

 

 

 2) Main Tanks (With

     any or all

     associated

     Refueling Control

     quantity gauges

     inoperative)

     (Cont’d)

 

 

 

 

 

 

 

A

3

2

 (M)(O) One may be inoperative provided:

a)       Fuel tank is serviced with fuel as determined from a continuous fuel log. This method is limited to:

1)       A maximum of 5 consecutive flight legs not to exceed 10 hours total after determining original fuel quantity by measurement,

2)       Flights on which all other lights, gauges and switches associated with that system operate normally, and

3)       If associated tank is No. 1 or No. 3, both wing tanks are serviced equally,

b)       Associated fuel flow meter operates normally,

c)       Fuel dump system (including all boost pumps) operates normally, and

d)       Procedures are established to ensure that fuel in the tank with the inoperative indicator will not be emptied below the non-dumpable level if fuel dump is required.

 

 

 

 

 

 

 

 

 

 

 

 

(Continued)

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

28-12

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

28 FUEL

 

 

 

 

 

 

 

 

 

 

 

28-11

 Flight Deck Fuel 

 Quantity Gauges

 (Cont’d)

 

 

 

 

 

 

***

 3) Auxiliary Tanks

C

-

-

(O) Gauges for one aux tank may be inoperative and the tank may be used provided:

a)       SB 727-28 A62, or production equivalent, has been incorporated, and

b)       Fuel quantity in associated tank is verified by an acceptable alternate procedure.

 

 

 

 

C

-

0

(M) All may be inoperative and the tanks not used provided:

a)       SB 727-28 A62, or production equivalent, has been incorporated, and

b)       Fuel quantity in associated tank is verified by an acceptable alternate procedure, and is considered as part of the zero fuel weight.

 

 

 

 

C

-

0

(M) All may be inoperative and the tanks not used provided associated tanks are verified empty after each refueling.

 

 

 

 

C

-

0

(M) All may be inoperative and the tanks not used provided associated tanks are verified empty and fill valve deactivated.

 

 

28-12

 Fuel Temperature

 Gauge

C

1

0

(O) May be inoperative provided Total Air

Temperature or Ram Air Temperature is

substituted as an indication of fuel temperature.

 

 

28-13

***

 Fenwall Fuel Surge

 Tank Suppression

 System

 

 

 

 

 

 

D

1

0

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

28-13

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

28 FUEL

 

 

 

 

 

 

 

 

 

 

 

28-14

 Fuel Dripsticks

C

-

0

(M) One or more may be inoperative provided fuel quantity is verified by an alternate

acceptable procedure.

 

 

28-15

 Fuel Sump Drain 

 Valves

 

C

-

-

One may be inoperative.

 

 

28-16

***

 Auxiliary Fuel Tank

 Boost Pumps

 

 

 

 

 

 

 

 1) Specified Models

C

-

-

One pump in each tank may be inoperative provided tank remains empty.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

C

-

-

(O) One pump in each tank may be inoperative provided:

a)       Fuel quantity remains in other tanks is adequate to reach an alternate destination if the remaining pump fails at any time.

b)       Fuel in the associated tank(s) is included as payload, and

c)       The effect on airplane balance in the event auxiliary tank fuel cannot be used is accounted for by limiting cargo compartment payload as follows:

 

 

 

 

 

 

SEAT SPACING LESS THEN 32

 INCHES:

 

 

 

 i) All Models

    (All Passenger

    Configuration)

 

 

 

 

 

 

 

 

 

C

 

 

FWD TANK ANY PUMP INOP.--

Forward cargo compartments remains empty.

AFT TANK ANY PUMP INOP.--

Aft cargo compartment remains empty.

 

 

 

 

 

 

(Continued)

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

28-14

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

28 FUEL

 

 

 

 

 

 

 

 

 

 

 

28-16

 ***

 Auxiliary Fuel Tank

 Boost Pumps

 (Cont’d)

 

 

 

 

 

 

 

 i) All Models (All

    Passenger

    Configuration)

    (Cont’d)

 

 

 

 

 

 

 

 

 SEAT SPACING 32 INCHES OR MORE:

 

FWD TANK ANY PUMP INOP.- -

No restrictions.

AFT TANK ANY PUMP INOP.- -

Aft cargo compartment load maximum 2,000 lbs. (907 kg)

 

 

 ii) 727-100C, -100

    Conversions (In All

    Cargo or Combi

    Configuration)

 

 

C

 

 

FWD TANK ANY PUMP INOP.- -

Forward cargo compartment remain empty.

AFT TANK ANY PUMP INOP.- -

Aft cargo compartment remains empty.

 

 

 iii) 727-200F

     (All Cargo

     Configurations)

 

 

 

 

 

FWD TANK ANY PUMP INOP.- -

Forward cargo compartment remain empty.

AFT TANK ANY PUMP INOP.- -

Aft cargo compartment load

maximum

2000 lbs (907Kgs)

 

 

 

 

  2) All Models

 

 

C

-

-

 Both pumps in any aux tank may be

 inoperative provided tank remains empty.

 

 

 

 

 

 

 

 

 

 

 

C

-

-

 Both pump in any aux tank may be

 inoperative provided:

a)       Fuel in the associated tank is included

      as part of the zero fuel weight, and

b)       Cargo compartment payload limitations for Specified Models, noted above, are observed.

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

28-15

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

28 FUEL

 

 

 

 

 

 

 

 

 

 

 

28-17

 Fueling Bay

 Fuel Cap

 

 

 

 

C

2

0

(M) One or both may be missing provided:

a)       Refueling receptacle is visually checked for contamination before each refueling, and

b)       No leakage is detected.

 

28-18

 ***

 Page/PATS Auxiliary

 Tank Fuel System

 

 

 

 

 

C

1

0

(M) May be inoperative provided:

a)       Both auxiliary tank fuel valve and vent valve are verified closed,

b)       Auxiliary tank circuit breakers are pulled and collared, and

c)       Auxiliary tank is drained of fuel.

 

28-19

***

 Page/PARTS 

 Auxiliary

 Tank Fuel Valve

 Open

 Light (Fueling Panel)

 

C

1

0

(M) May be inoperative provided

a)       Auxiliary tank valve open light on F/E panel operates normally, and

b)       All other functions of the system operate normally.

 

28-20

***

 ATS (Aircraft Tank

 Service) Auxiliary

 Tank Fuel System

 (STC SA 3810 WE)

 

 

 

 

 

 

 

 1) Sub-systems

     Forward, Mid

     and Aft

 

 

 

 

 

 

 

 

 

 

 

 

 

 

C

3

0

(M) May be inoperative provided:

a)       Flight operations are not predicated on the use of the inoperative sub-system(s) fuel,

b)       Associated aux fuel tanks are verified empty,

c)       Associated appropriate electrical circuits are deactivated and secured,

d)       Associated auxiliary tank vent valves are verified open, and

e)       Aircraft Center of Gravity (C/G) limitations are observed and maintained through-out the flight profile.

 

 

 

(Continued)

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

28-16

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

28 FUEL

 

 

 

 

 

 

 

 

 

 

 

28-20

***

 ATS (Aircraft Tank

 Service) Auxiliary

 Tank Fuel System

 (STC SA 3810 WE)

 (Cont’d)

 

 

 

 

 

 

 

 2) Air Pressure

     Indicator

 

C

1

0

 

 

 

 3) Vent Valves

 

C

2

1

(M)(O) One may be inoperative open provided:

a)       Remaining vent valve operates normally,

b)       Fuel quantity in other tanks is adequate to reach an alternate destination, if the remaining valve fails at any time during flight, and

c)       Fuel in associated aux tank is considered undumpable and that fuel weight is included in all take off alternate landing performance considerations including center of Gravity (Weight and Balance) envelope.

 

 

 

 4) Vent Valve

     Intransit Lights

C

2

1

(M) One may be inoperative provided it

is verified that both vent valves operate

normally before each departure when

ATS aux fuel is required.

 

 

 

 

C

2

1

(M) One may be inoperative provided

associated valve is either inoperative

or considered inoperative.

 

 

 

 

 

 

 

 

 

 

 

(Continued)

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

28-17

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

28 FUEL

 

 

 

 

 

 

 

 

 

 

 

28-20

***

 ATS (Aircraft Tank

 Service) Auxiliary

 Tank Fuel System

 (STC SA 3810 WE)

 (Cont’d)

 

 

 

 

 

 

 

 5) System Bleed Air

     Pressure Valves

C

2

1

(O) One may be inoperative provided:

a)       Remaining pressure valve operates normally,

b)       Fuel quantity in other tanks is adequate to reach an alternate destination, if the remaining valve fails at any time during flight, and

c)       Fuel in associated aux tank is considered undumpable and that fuel weight is included in all take off alternate landing performance considerations including center of gravity (Weight and balance) envelope.

 

 

 

 6) Transfer Valve

     Intransit Lights

C

3

2

(O) One may be inoperative provided

associated transfer valve is verified to operate normally before each departure, when ATS aux fuel is required.

 

 

 

 7) ATS System

     Quantity Indicator

C

1

0

(M) May be inoperative provided fuel quantity in ATS Aux Tank System is verified by an alternate acceptable procedure.

 

 

 

 

C

1

0

(M) May be inoperative provided tanks are verified to be empty before each departure.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

28-18

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

28 FUEL

 

 

 

 

 

 

 

 

 

 

 

28-21

***

 ATS (Aircraft Tanks

 Service) Auxiliary

 Tank Refuel Valve

 Intransit Lights

 (STC SA 3810WE)

 

C

3

0

(M) May be inoperative provided:

a)       An alternate means of determining that the fueling valves operate is utilized, and

b)       Quantity of fuel in the associated tank is known after each refueling.

 

28-22

***

 Auxiliary Fuel Tank

 System

 (STC SA 3564WE)

 

 

 

 

 

 

 

 1) Forward System

C

1

0

(O) May be inoperative provided:

a)       Any fuel in the Forward Aux Tanks is considered unusable, and

b)       AFM Limitations are applied.

 

 

 

 2) Aft System

C

1

0

(O) May be inoperative provided:

a)       Any fuel in the AFT Aux Tanks is considered unusable, and

b)       AFM Limitations are applied.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

29-1

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

29 HYDRAULIC POWER

 

 

 

 

 

 

 

 

 

 

 

29-01

 System “A” Pumps

 

 

 

 

 

 

 

 1) Depressurization

     Function

C

2

0

(O) May be inoperative on one or both pumps.

 

NOTE: Starting # 1 or # 2 engines will pressurize

            nose wheel steering system, unless

            alternate procedures are established

            and used.

 

 

29-02

 DELETED

 

 

 

 

Deleted prior to Rev. 33

 

29-03

***

 System “A” Heat

 Exchange Bleed Air

 Control Valves

 

C

2

1

(M) One may be inoperative closed provided the associated overheat light operates normally.

 

29-04

 Ground Interconnect

 Valve

 (A and B Systems)

 

C

1

0

(M) May be inoperative provided valve remains closed.

 

 

29-05

 Brake Interconnect

 System

C

1

0

(M)(O) May be inoperative closed provided approved procedures are defined in the operator’s manual for “B” System malfunctions.

 

NOTE: Both brake pressure and brake

            pressure indication(s) are absent

            during a battery start.

 

 

29-06

 DELETED

 

 

 

Deleted prior to Rev.33.

 

 

29-07

 DELETED

 

 

 

Deleted prior to Rev.33.

 

 

29-08

 System Pressure

 Indication System

 (“A” or “B”)

 (Flight Deck)

 

 

C

2

1

(O) One may be inoperative provided:

a)       Associated low pressure warning lights operate normally, and

b)       Associated system pressure is checked before each departure.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

29-2

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

29 HYDRAULIC POWER

 

 

 

 

 

 

 

 

 

 

 

29-09

 Pump Low Pressure

 Lights (“A” systems)

 

 

 

 

C

2

1

(O) One may be inoperative provided:

a)       The output of the associated pump is checked before each departure, and

b)       Both pumps remain ON continuously during flight.

 

29-10

 Pump Low Pressure

 Lights (“B” System)

 

 

 

 

C

2

1

(O) One may be inoperative provided:

a)       The output of the associated pump is checked before each departure, and

b)       Both pumps remain ON continuously during flight.

 

29-11

 Accumulator  

 Pressure

 Indication Systems

 

C

-

0

(O) May be inoperative provided associated

flight deck gauge operates normally.

 

29-12

 DELETED

 

 

 

 

Deleted prior to Rev.33

 

29-13

 “A”, “B” and

 Standby System

 Overheat Lights

 

C

3

0

 

 

29-14

 System “A” Quantity

 Indication System

 (F/E Panel)

 

 

 

 

 

C

1

0

(M) May be inoperative provided:

a)       Quantity is checked before each departure,

b)       “A” system pressure gauge operates normally, and

c)       “B” system and Standby system quantity gauges operate normally.

 

29-15

 System “B” Quantity

 Indication System

 (F/E Panel)

 

 

C

1

0

(M) May be inoperative provided:

a)       Quantity is verified adequate, and

b)       Ground interconnect is verified closed before each departure.

 

29-16

 Standby System

 Quantity Indication

 System

 (F/E Panel)

 

C

1

0

 May be inoperative provided adequate  quantity is verified before each  departure.

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

29-3

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

29 HYDRAULIC POWER

 

 

 

 

 

 

 

 

 

 

 

29-17

 Reservoir and Fill

 Station Quantity

 Indication System

 

C

1

0

 

 

29-18

***

 

 Low Level Lights

 (“A” and “B”)

 Systems

 

D

2

0

 

 

29-19

***

 Reservoir Air

 Pressure

 Gauge

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

D

1

0

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

30-1

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

30 ICE AND RAIN PROTECTION

 

 

 

 

 

 

 

 

 

 

 

30-01

 Wing Anti-Icing Duct

 Temperature

 Indicating System

 

C

1

0

May be inoperative provided valve position lights operate normally when the system is in use.

 

30-02

 Wing Anti-Icing

 System

 

 

 

C

1

0

(M) May be inoperative provided:

a)       The airplane is not operated in known

       or forecast icing conditions, and

b)       Inoperative valve remains closed.

 

 

 

C

1

0

(M) May be inoperative provided damaged ducting is removed, and a suitable blocking

plate is installed.

 

 

30-03

***

 Wing Anti-Icing

 Interconnect Valve

 

 

 

 

D

1

0

(M) May be inoperative provided:

a)       The interconnect valve remains closed, and

b)       Engine anti-icing AFM limitations are observed.

 

 

 

 

 

 

 

 

 

C

1

0

May be inoperative open provided:

a)       No. 2 engine thermal anti-icing is not operated on the ground or during

      takeoff, and

b)       Icing conditions do not exist on the ground at departure airport.

 

30-04

 Wing Anti-Ice Valve

 Position Lights

 

 

C

2

0

One or both may be inoperative provided

wing anti-icing duct temperature indicating system operates normally.

 

30-05

***

 

 Wing Anti-Ice

 Auto Trip

 System

 

 

 

 

 

 

 

 

 

D

1

0

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

30-2

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

30 ICE AND RAIN PROTECTION

 

 

 

 

 

 

 

 

 

 

 

30-06

 Wing Anti-Ice

 Isolation

 Valves (B-727-100

 And 100QF APU

 Equipped Airplanes)

 

C

2

0

(M) One or both may be inoperative

provided both valves are secured open

by an accepted maintenance procedure.

 

 

 

C

2

0

One or both may be inoperative provided

flight is not operated in known or

forecast icing conditions.

 

 

30-07       ***

 Tail Anti-Icing System

C

1

0

May be inoperative provided AFM limitations are observed.

 

 

30-08        ***

 Tail Anti-Icing Duct

 Temperature

 Indicating System

C

1

0

May be inoperative provided the valve position light operates normally when the system is in use.

 

 

30-09

***

 Tail Anti-Icing Valve

 Position Light

 C

1

0

May be inoperative provided temperature indicator operates normally.

 

 

30-10

 DELETED

 

 

 

Deleted prior to Rev. 27 A.

 

 

30-11

 Engine and Cowl

 Anti-Ice Valves

 All Models

 (Except 727-100QF)

 

C

10

9

(M) One may be inoperative closed provided:

a)       Airplane is not operated in known or forecast icing conditions, and

b)       All other anti-ice valves operate normally.

 

 

 All Models

 (Except 727-100QF)

 

 

 

 

 

 

 

 

 

 

 

C

1

0

(M) No. 2 engine 13th stage valve may be inoperative open provided:

a)       No. 2 engine automated sixth stage bleed valve is not installed or is deactivated closed, and

b)       All other anti-ice valves operate normally.

 

 

 

 

 

 

 

(Continued)

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

30-3

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

30 ICE AND RAIN PROTECTION

 

 

 

 

 

 

 

 

 

 

 

30-11

 Engine and Cowl

 Anti- Ice Valves

 (Cont’d)

 

 

 

 

 

 

 

 All Models

 (Excluding Valsan

 727-100,  -200RE

 and 727-100QF)

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

C

9

8

(M) (O) One pod engine cowl valve or one inlet guide vane valve, or the No. 2 engine mixed air valve may be inoperative open provided:

a)       All thrust rating limits on the affected engine, except takeoff and go-around are reduced by .03 EPR, or .05 EPR for No. 2 engine mixed air valve,

b)       En route climb limited weight is reduced by 4,900 lb. (2,223 kg) or by 8,100 lb. (3,674 kg) for No. 2 engine mixed air valve,

c)       At temperature greater than 50 degrees F (10 degrees C),

1)       Takeoff and go-around thrust limits on the affected engine are reduced by .03 EPR, or by .05 EPR for No. 2 engine mixed air valve,

2)       Takeoff and landing performance limited weight is reduced by 2,900 lb. (1,315 kg), or by 4,600 lb. (2,087 kg) for No. 2 engine mixed air valve,

d)       All other anti-ice valves operate

      normally, and

      e)   Operating temperature with one

   pod engine cowl valve

   inoperative open is limited to

   50 degrees F (10 degrees C)

   maximum (ambient or Total Air

   Temperature) unless S/B 30-31

   “Nose Cowl TAI Spray Ring

   Modification” has been

      incorporated.

 

 

 

 

(Continued)

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

30-4

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

30 ICE AND RAIN PROTECTION

 

 

 

 

 

 

 

 

 

 

 

30-11

 Engine and Cowl

 Anti- Ice Valves

 (Cont’d)

 

 

 

 

 

 

 

 All Models

 (Excluding Valsan

 727-100, -200RE

 and 727-100QF)

 (Cont’d)

 

 

 

 

ADDITIONAL REQUIREMENTS FOR JT8D-15-15A AND JT8D-17/17A ENGINES

 

 

The adjustments listed below must be applied

when dispatching with anti-ice OFF, and the

following conditions exist:

 

Takeoff—

JT8D-15/15A  Pressure altitude

                        between

                           3,000 feet and 10,000

                           feet, ambient

                           temperature

                           below 0 degrees F

                           (-18 degrees C).

JT8D-17/17A  Pressure altitude

                        between

                           3,000 feet and 10,000

                           feet, ambient

                           temperature

                           below 15 degrees F

                           (-10 degrees C).

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

(Continued)

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

30-5

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

30 ICE AND RAIN PROTECTION

 

 

 

 

30-11

 Engine and Cowl

 Anti- Ice Valves

 (Cont’d)

 

 

 

 

 

 

 

All Models

 (Excluding Valsan

 727-100, -200RE

 and 727-100QF)

 (Cont’d)

 

C

 

 

Go Around –

JT8D-15/15A   Pressure altitude

                        between

                           3,000 feet and 10,000

                           feet, total air

                           temperature

                           below 0 degrees F (-18

                           degrees C).

JT8D-17/17A   Pressure altitude

                        between

                           3,000 feet and 10,000

                           feet, total air

                           temperature 

                           below 15 degrees F

                           (-10 degrees C).

1)       Takeoff and go-around thrust limits on the affected engine are reduced by .03 EPR, and

2)       Takeoff and landing performance weight is reduced by 2,900 lb. (1,315 kg), or by 2,600 lb. (1,179 kg) for No. 2 engine mixed air valve,

            OR

 

 

 

C

 

 

3)       AFM Appendix 28 for JT8D-15/15A or AFM Appendix 61 for JT8D-17/17A weight reductions are observed.

 

NOTE: Valve position light operation not

               required for the specific inoperative

               valve.

 

 

 

 

 

 

 

(Continued)

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

30-6

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

30 ICE AND RAIN PROTECTION

 

 

 

 

 

 

 

 

 

 

 

30-11

 Engine and Cowl

 Anti- Ice Valves

 (Cont’d)

 

 

 

 

 

 

 

Valsan B-727-100/200RE Only

C

9

8

(M)(O) One inlet guide vane valve, or the No. 2 engine mixed air valve (cowl shutoff valve) may be inoperative open provided:

a)   All other anti-ice valves operate

     normally,

b)   All thrust rating limits on the

     affected engine, except takeoff

     and go-around, are reduced by:

     Pod Engine, inlet guide vane

     valve, .05 EPR. No. 2 Engine,

     inlet guide vane valve, .03 EPR,

     or mixed air valve, .05 EPR.

c)   En route climb limited weight is

     reduced by: Pod Engine, inlet

     guide vane valve 6900 lbs.

     (3130 kg.). No. 2 Engine, inlet

     guide vane valve 4900 lbs.

     (2223 kg.). No. 2 Engine, inlet

     guide vane valve, 4900 lbs.

     (2223 kg.) or by 8100 lbs.

     (3674 kg.) for mixed air valve,

     and

d)   At temperatures greater than

     50 Deg. F (10 Deg. C),

1)   Takeoff and go-around

      thrust limits on the

      affected engine are

      reduced by: Pod Engine,

      inlet guide vane valve,

      .05 EPR. No. 2 Engine,

       inlet guide vane valve,

      .03 EPR, or mixed air

       valve .05 EPR.

 

 

 

 

(Continued)

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

30-7

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

30 ICE AND RAIN PROTECTION

 

 

 

 

 

 

 

 

 

 

 

30-11

 Engine and Cowl

 Anti- Ice Valves

 (Cont’d)

 

 

 

 

 

 

 

Valsan B-727-100/200RE Only

(Cont’d)

 

C

 

 

2)       Takeoff and landing performance weight is reduced by: Pod Engine, inlet guide vane valve, 5100 lbs. (2312 kg.) No. 2 Engine, inlet guide vane valve, 2900 lbs. (1315 kg.) or mixed air valve 4600 lbs. (2087 kg.).

 

NOTE: No relief is given for Pod Engine

               cowl valves in the open position

               on the Valsan B-727- 100/200RE.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

ADDITIONAL REQUIREMENTS FOR

JT8D- 15/15A AND JT8D-17/17A ENGINES

 

In addition, the adjustments listed below must be applied to the No. 2 engine, when dispatching with anti-ice OFF, a valve open, and the following conditions exist:

 

Takeoff:

JT8D-15/15A - Pressure altitude 

                        between

                          3000 ft. and 10000 ft.,

                          ambient temperature

                          below 0 Deg. F

                          (-18 Deg. C.                          

JT8D-17/17A - Pressure altitude

                        between

                          3000 ft. and 10000 ft.,

                          ambient temperature

                          below 15 Deg. F

                          (-10 Deg. C).

 

            

   

 

(Continued)

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

30-8

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

30 ICE AND RAIN PROTECTION

 

 

 

 

30-11

 Engine and Cowl

 Anti- Ice Valves

 (Cont’d)

 

 

 

 

 

 

 

Valsan B-727-100/200RE Only

(Cont’d)

 

 

 

 

 Go-Around:

 JT8D-15/15A - Pressure altitude between

                          3000 ft. and 10000 ft.,

                          total air temperature

                          below 0 Deg. F

                          (-18 Deg. C)

 JT8D-17/17A - Pressure altitude between

                          3000 ft. and 10000 ft.,

                           total air temperature

                           below 15 Deg. F

                           (-10 Deg. C).

(1)     Takeoff and go-around thrust limits on the affected engine are reduced by .03 EPR, and

(2)     Takeoff and landing performance weight is reduced by: No. 2 Engine-inlet guide vane valve, 2900 lbs. (1315 kg.) or mixed air valve 2600 lbs. (1179 kg.),

 

 

 

 

 

 

               OR

 

 

 

 

 

 

(3)     AFM Appendix 28 for JT8D-15/15A or AFM Appendix 61 for JT8D-17/17A weight reductions are observed.

 

NOTE: Valve position light operation not

               required for the specific

               inoperative valve.

 

 

 

 

 

 

 

 

 

 

(Continued)

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

30-9

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

30 ICE AND RAIN PROTECTION

 

 

 

 

 

 

 

 

 

 

 

30-11

 Engine and Cowl

 Anti- Ice Valves

 (Cont’d)

 

 

 

 

 

 

 

B-727-100QF Only

C

3

2

(M)(O) One valve may be inoperative secured open provided:

a)   Engine start procedures for anti-

     ice valve secured open is used,

b)   AFM engine EPR reductions for

     inlet anti-ice ON for effected

     engine are used,

c)   Aircraft performance is

     determined using AFM engine

     inlet anti-ice ON correction chart,

d)   Outside Air Temperature (OAT)

     does not exceed 55 degrees F

     (12 degrees C) with valve

     secured open on engines 1 or 3

     and OAT does not exceed 80

     degrees F (26 degrees C) with

     valve secured open on No. 2

     engine, and

e)   All other engine anti-ice valves 

     operate normally.

 

 

 

 

 

 

 

 

 

 

C

3

2

(M) One may be inoperative secured closed provided:

a)   Airplane is not operated in

     known or forecast icing

     conditions, and

b)   All other engine anti-ice valves

     operate normally.

 

 

 

 1) Indicator Lights

     (B-727-100QF

     Only)

 

 

 

 

 

 

 

C

3

0

(M)(O) May be inoperative provided normal valve operation is verified prior to operations in known or forecast icing conditions.

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

30-10

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

30 ICE AND RAIN PROTECTION

 

 

 

 

30-12

 Pitot Heat Systems

B

2

1

(O) Pilot’s or Copilot’s may be inoperative provided the airplane is not operated in known

or forecast icing conditions.

 

 

 

 

 

 

 

 

 

 

B

1

0

(O) Auxiliary pitot heat system may be inoperative provided:

a)   Dispatch deviations for affected

     equipment for are observed, and

b)   All affected equipment must be

     identified and the crew advised.

 

NOTE: Light not required for an

               inoperative heater.

 

 

30-13

 Static Port Heater

 System

C

-

-

One may be inoperative provided the airplane

is not operated in known or forecast icing conditions.

 

 

 

 1) B-727-100/QC

     and 727-100QF

C

-

0

All may be inoperative provided static port system has been modified per AD-76-17-07 or production equivalent.

 

 

 

 2) B-727-200

C

-

0

(O) May be inoperative provided AFM Limitations, Takeoff at 35 Deg. F.

(2 Deg. C) or below are observed.

 

 

30-14

 Elevator Feel

 Pitot Heater

C

2

1

One may be inoperative provided airplane is not operated in known or forecast icing conditions.

 

 

30-15

 Flight Deck Window

 Heat System

 

C

8

-

 

 

NOTE: See AFM for window heat

            requirements.

 

 

30-16

 Windshield Wipers

C

2

0

May be inoperative provided airplane is not operated in precipitation within 5 nautical miles

of the airport of takeoff or intended landing.

 

 

 

 1) Windshield Wiper

     Speeds

C

-

1

May be inoperative provided one speed

operates normally at both pilot stations.

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

30-11

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

30 ICE AND RAIN PROTECTION

 

 

 

 

 

 

 

 

 

 

 

30-17

 ***

 Rain Repellent   

 System

 

D

1

0

 

 

30-18

***

 

 Ice Detection System

 

D

1

0

 

 

30-19

 Pitot/Static,

 Temperature Probe 

 Heater Indicating

 System

 

 

 

 

 

 

***

 1) Ammeter System

 

 

 

 

 

 

 

      a) AC Ammeters

B

2

0

(M) May be inoperative provided associated heaters are verified to operate normally.

 

 

 

b) Heater Off

    Light

 

 

 

 

 

B

1

0

(O) May be inoperative provided:

a)   All other components of the pitot heat

     system are verified to perate normally,

     and

b)   Airplane is not operated in known or

     forecast icing conditions.

 

***

 2) 8 Light System

 

 

 

 

 

 

 

      a) PITOT L & R

          Lights

 

 

 

 

 

B

2

1

(O) One may be inoperative provided:

a)   All other components of the pitot heat

     system are verified to operate normally,

     and

b)   The airplane is not operated in known

      or forecast icing conditions.

 

 

 

       b) ELEV PITOT

           L & R, STATIC   

           L & R, AUX

           PITOT, and

           TEMP PROBE

           Lights

 

B

6

0

(M) May be inoperative provided associated heaters are verified to operate normally.

 

NOTE: Light not required for an

            inoperative heater.

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

30-12

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

30 ICE AND RAIN PROTECTION

 

 

 

 

 

 

 

 

 

 

 

30-20

 Total Air

 Temperature

 Probe Heater

C

-

0

(O) May be inoperative provided an approved alternate system is installed and operates normally.

 

 

 

 

C

-

0

(O) May be inoperative provided airplane is not operated in known or forecast icing conditions.

 

NOTE: Light not required for an

            inoperative heater.

 

 

30-21

 Windshield Heat

 Power

 On/Overheat Test

 

C

1

0

 

 

30-22

 De-Fog System

 

C

1

0

 

 

30-23

 Anti-Ice Duct

 Overheat Light

 System

 

 

 

C

1

0

(M) May be inoperative provided:

a)   Associated anti-ice valves remain

      closed, and

b)   Airplane is not operated in known or

      forecast icing conditions.

 

30-24

Drain Mast Heaters

 

 

 

 

 

C

-

0

(M) May be inoperative provided:

a)       Associated TOILET FLUSH PORT(S) is capped at toilet service panel, and

b)       Associated galley is used without water service.

 

 

 

 

 

 

 

 

C

-

0

(M) May be inoperative provided:

a)       Associated lavatory entrance door is secured to prevent use of lavatory, and

b)       Associated galley is used without water service.

 

 

 

C

-

0

(M) May be inoperative provided:

a)       Water supply to associated galley, lavatory sink, and drinking fountain is secured OFF, and

b)       Associated galley drains, lavatory sinks, and drinking fountain drains are not used.

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

30-13

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

30 ICE AND RAIN PROTECTION

 

 

 

 

 

 

 

 

 

 

 

30-25

***

 Windshear Perimeter

 Heater

 

D

1

0

 

 

30-26

 Pitot Heat Indicating

 System

 (Heater OFF Monitor)

 

 

 

 

Delete, Rev. 38. (Combined with Item 30-19.)

 

30-27

 Wing Anti-Ice

 Pressure Regulating

 Valve

 (727-100QF)

 

 

 

 

 

 

C

1

0

(M) (O) May be inoperative provided:

a)       Valve is secured open by an acceptable maintenance procedure, and

b)       EPR settings and performance data for wing anti-ice ON, as appropriate, are used.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

31-1

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

31 INDICATING/RECORDING

   SYSTEMS

 

 

 

 

 

 

 

 

 

 

 

31-01

Clocks

C

-

1

May be inoperative provided one clock at either the pilot’s or copilot’s position operates normally.

 

 

31-02

Flight Data Recorder (FDR) System

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

A

-

0

May be inoperative provided:

a)       Cockpit Voice Recorder (CVR) operates normally,

b)       Airplane is not dispatched from a designated airport as listed in the operator’s Mel unless:

1)       The FDR failure occurs after pushback but prior to takeoff, or

2)       The FDR repair was attempted but was not successful.

c)       In those cases where repair is attempted but not successful, the aircraft may be dispatched on a flight or series of flights until the next designated airport where repair must be accomplished prior to dispatch, and

d)       Repairs are made within three flight days.

 

 

 

C

-

1

Any in excess of those required by FAR may be inoperative.

 

 

 

 1) FDR Recording

     Parameters

     required by FAR

 

   

A

-

-

Up to three (3) recording parameters may be inoperative provided:

a)       Cockpit Voice Recorder (CVR) operates normally, and

b)       Repairs are made within 20 calendar days.

 

|
|

 

 2) FDR Recording

     Parameters not

     required by FAR

A

-

-

May be inoperative provided repairs are made prior to the completion of the next heavy maintenance visit.

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

31-2

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

31 INDICATING/RECORDING

   SYSTEMS

 

 

 

 

31-03

***

AIDS Maintenance Recorder

 

D

1

0

May be inoperative provided alternate procedures are used.

 

 

 

D

1

0

May be inoperative provided maintenance procedures are not dependent upon its use.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

32-1

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

32 LANDING GEAR

 

 

 

 

 

 

 

 

 

 

 

32-01

Landing Gear Door Warning System

 

C

1

0

 

 

32-02

Landing Gear Warning Horn Function

 

 

 

 

Deleted, Rev. 29.

 

32-03

Landing Gear Indication

B

-

2

May be inoperative provided center panel indicators, and one other indicating system operates normally.

 

 

32-04

***

Ground Lock Pin Annunciator System

 

D

1

0

 

 

32-05

Antiskid System

C

1

0

(O) May be inoperative provided AFM

Limitations are observed.

 

 

 

 1) Test Feature

 

C

1

0

 

 

 

 2) Touchdown

     Feature

 

C

1

0

 

 

 

 

 3) Annunciators

C

-

0

May be inoperative for an inoperative system.

 

 

32-06

***

Nose Wheel Brake/ Anti-skid System

D

1

0

(O) May be inoperative provided:

a)       Nose wheel brake/anti-skid switch remains OFF, and

b)       AFM Limitations are observed.

 

 

32-07

Parking Brake

 

 

 

Deleted, Rev. 29.

 

 

32-08

Parking Brake Light

 

 

 

 

 

 

 

 1) Solenoid Operated

     Parking Brake

     Valve

C

1

0

(O) Light may be inoperative provided anti-ski system is turned OFF when parking brake is in use.

 

 

 

 2) Motor Operates

     Parking Brake

     Valve (Mark III

     Anti-Skid System)

 

 

C

1

0

(M) Light may be inoperative provided the parking brake shutoff valve operates normally.

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

32-2

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

32 LANDING GEAR

 

 

 

 

 

 

 

 

 

 

 

32-09

Pneumatic Brake System

 

 

 

 

Deleted, Rev. 29.

 

32-10

Flight Deck Pneumatic Brake Pressure Indicator

 

 

 

 

 

A

1

0

May be inoperative provided:

a)       Pneumatic brake pressure indicator in the nose wheel well operates normally.

b)       Pneumatic brake pressure is verified before each departure, and

c)       Operations are limited to not more than three flight days before repair is made.

 

32-11

Pneumatic Brake Pressure Indicator (Nose Wheel Well)

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

C

1

0

May be inoperative provided indicator on the flight deck operates normally.

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

32-3

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

32 LANDING GEAR

 

 

 

 

 

 

 

 

 

 

 

32-12

Tail Skid

C

1

0

(M)(O) May be inoperative provided:

a)       Tail skid is secured extended,

b)       Aft lavatory drain mast is deactivated, and

c)       The following performance penalties are applied:

 

2,000 lb (907 kg) gross weight reduction to 2nd segment climb limits.

 

6,000 lb. (2, 722 kg) gross weight reduction to one engine inoperative en route climb limits.

 

6,800 lb. (3,084 kg) gross weight reduction to two engine inoperative en route climb limits.

 

1,400 lb. (635 kg) gross weight reduction to approach climb and landing climb limits.

 

 

 

 

 

 

            OR

 

 

 

 

 

 

 

 

 

 

 

 

 

 

C

 

 

d)       Tail skid is secured extended,

e)       Water supply to aft galleys, lavatory sinks, and drinking fountain is secured OFF,

f)         Aft galley drains, lavatory sinks, and drinking fountain drains are not used, and

g)       Performance penalties in c) above are applied.

 

 

 

 

 

 

 

 

 

 

 

(Continued)

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

32-4

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

32 LANDING GEAR

 

 

 

 

 

 

 

 

 

 

 

32-12

Tail Skid

(Cont’d)

 

 

 

 

 

 

 

 1) 727-200 Only

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

C

1

0

May fail to lock when retracted provided:

a)       Tail skid extends and retracts normally,

b)       Tail skid warning light illuminates only when gear handle is placed OFF following retraction, and operates normally during routine operations,

c)       After gear retraction, the gear handle is placed OFF momentarily and door warning lights remain extinguished (indicating proper locking of gear and doors), and

d)       Following (c), the gear handle is returned to UP and the tail skid annunciator extinguishes.

 

NOTE: Handle should remain UP until

            necessary to lower gear.

 

32-13

Tail Skid Position Light

 

C

1

0

(M) May be inoperative provided tail skid is functionally checked once each flight day.

 

32-14

Rudder Pedal Nose Wheel Steering System

 

 

 

C

1

0

(O) May be inoperative provided:

a)       Operation of other systems is not impaired, and

b)       All takeoffs and landings are made by the pilot occupying the left seat.

 

32-15

***

Autobrake System

C

1

0

(M) May be inoperative provided that if the autobrake disarm light illuminates with the autobrake ARM switch OFF, the inlet pressure line to the autobrake valve module must be capped.

 

NOTE: AFM takeoff and landing distances are

           not based on use of autobrakes.

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

32-5

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

32 LANDING GEAR

 

 

 

 

 

 

 

 

 

 

 

32-16

***

Brake Low

Pressure Light

 

C

1

0

 

 

32-17

***

 

Brake Temperature Monitoring System

 

C

1

0

 

 

32-18

***

Nose Gear Steering Lockout System

 

 

 

 

C

1

0

(M)(O) May be inoperative provided:

a)       System is deactivated, pressurized, and

b)       Alternate procedures for push-back and towing are utilized.

 

32-19

***

Direct reading Tire Pressure indicator(s)

 

D

-

0

 

 

32-20

Nose Gear

Snubber Pads

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

C

2

0

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

33-1

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

33 LIGHTS

 

 

 

 

 

 

 

 

 

 

 

33-01

Cockpit/ Flight Deck/Flight Compartment and Instrument Lighting Systems

 

 

 

 

 

 

 

 

C

-

-

Individual lights may be inoperative provided remaining lights are:

a)     Not on the Essential or Standby bus,

b)     Sufficient to clearly illuminate all required instruments, controls, and other devices for which they are provided,

c)     Positioned so that direct rays are shielded from flight crewmembers’ eyes, and

d)     Lighting configuration and intensity is acceptable to the flight crew.

 

NOTE: Individual button/switch lights and/or annunciations/indications are excluded from this relief.

 

 

 

|

 

 

 

 

 

 

 

 

|
|
|

 

33-02

Cabin Interior

Illumination System

 

 

 

 

 

 

 

 1) Passenger And 

     Combi Config-

     urations Without

     Photoluminescent

     Escape Path

     Marking Systems

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

C

-

-

Individual lights may be inoperative provided remaining lighting is sufficient for cabin attendants to perform their duties.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

(Continued)

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

33-2

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

33 LIGHTS

 

 

 

 

 

 

 

 

 

 

 

33-02

Cabin Interior

Illumination System

(Cont’d)

 

 

 

 

 

 

 

 2) Passenger And 

     Combi Config-

     urations With

     Photoluminescent

     Escape Path

     Marking Systems

 

C

-

-

Individual lights may be inoperative provided:

      a)  Remaining lighting is sufficient

            for cabin attendants to perform

            their duties, and

       b)  FAA approved minimum

            acceptable lighting levels

            specified in one of the following

            documents are complied with:

1)        FAA engineering

       approval letter,

2)        FAA approved report of

 the Type Design holder,

  3)    Limitations and

         Conditions section of

         the applicable

         Supplemental Type

         Certificate (STC).

         OR

4)    An FAA approved    

 report incorporated in

 the Master Drawing

 List for the applicable  

 STC.

       

 

 

 3) Cargo 

     Configurations

     (Including AEI

     STC SA1798SO)

 

 

 

 

 

 

 

a) Cargo Door

          Floodlights

C

2

0

(M) May be inoperative for night operations provided alternate procedures are established and used.

 

 

 

 

C

2

0

May be inoperative for day operations.

 

 

 

b) Cabin Interior

          Lights    

C

-

0

Individual lights may be inoperative provided sufficient lighting remains for cargo handlers to perform their duties.

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

33-3

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

33 LIGHTS

 

 

 

 

 

 

 

 

 

 

 

33-03

Passenger Lighted Information Signs  (No Smoking/Fasten Seat Belt/Return to Seat)

 

C

-

-

(M) May be inoperative provided:

      a)  Associated passenger seat, cabin

           attendant seat or lavatory is not

           occupied from which a lighted

           information sign is not readily legible, and

      b)  Associated seat or lavatory is blocked

           and placarded- “DO NOT OCCUPY”.

 

NOTE: These conditions are not intended to

            prohibit lavatory use or inspections by

            crewmembers.

 

|
|
|
|
|
|
|

 

|
|
|

 

 

 

 

 

 

 

 

 

C

-

-

(O) May be inoperative and associated passenger seat, cabin attendant seat or lavatory may be occupied provided:

a)       PA system operates normally, and

b)       PA system is used to notify passengers and cabin crew when associated sign(s)

       are placed on or off.

|
|
|
|
|
|
|

 

 !) Aural Tone

    Feature

 

C

1

0

 

 

 

2)  All-Cargo,

    Supernumerary/

    Courier Area

     Lighted

     Information Sign  

 

C

-

0

(O) May be inoperative provided alternate procedures are established and used to notify couriers/supernumeraries when associated sign(s) are placed off.

|

|

|

|

33-04

AFT AIRSTAIR Compartment

Service Light System

 

C

1

0

 

 

33-05

Cargo Compartment Lights

 

 

 

 

 

 

 

 

C

-

0

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

33-4

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

33 LIGHTS

 

 

 

 

 

 

 

 

 

 

 

33-06

Wheel Well Lights

 

 

 

 

 

 

 

 1) Main Wheel Lights

 

C

-

0

 

 

 

 2) Nose Wheel Well

     Light(s)

 

C

-

1

May be inoperative provided the Nose Gear Down Lock Light (Aft Light), focused on the

nose gear down lock, operates normally.

 

 

33-07

***

High Intensity Oscillating or Strobe Navigation Lights

 

D

-

0

 

 

33-08

Anti-Collision Beacon

C

2

1

One unit may be inoperative for night operations provided strobe anti-collision (wing/tail mounted lights) are installed and operate normally.

 

 

 

 

C

2

0

Both may be inoperative for night operations provided Minneapolis Honeywell airplanes recognition light system or approved equivalent

is installed and operates normally.

 

 

 

 

C

2

0

All may be inoperative for day operations.

 

 

33-09

Wing Illumination Lights

C

2

0

(O) May be inoperative provided ground deicing procedures do not require their use.

 

 

33-10

Landing Lights

C

4

2

One on each side may be inoperative for night operations.

 

 

 

 

C

4

0

All may be inoperative for day operation.

 

 

33-11

***

Taxi Light

C

-

0

 

 

33-12

Runway Turnoff Lights

 

 

 

 

 

 

 

 

C

2

0

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

33-5

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

33 LIGHTS

 

 

 

 

 

 

 

 

 

 

 

33-13

Position Lights

(Wing Tips & Tail)

 

 

 

 

 

 

 

 1) Bulbs

 

 

 

 

 

 

 

 

 

 

C

-

4

One or two bulbs may be inoperative for night operations provided the following minimum lights operate normally:

a)       One stationary red wing tip

bulb,

b)       One stationary green wing tip

bulb, and

c)       One stationary white tail light

at each wing tip position.

 

 

 

 

C

-

0

All may be inoperative for day operations.

 

 

33-14

DELETED

 

 

 

 

 

 

33-15

Interior Emergency Lighting System

 

 

 

 

 

 

 

 1) Combi (Mixed) or

     All Cargo 

     Configurations

     only

C

-

-

Individual lights may be inoperative in cargo areas provided:

a)       No one occupies those areas  during flight, and

b)       Flight deck and forward entrance door exit lights operate normally.

 

 

33-16

Exterior Emergency Lighting System

 

 

 

 

 

 

 

 1) Passenger Combi,

     and All Cargo

     Configuration

 

 

 

 

 

 

 

 

 

B

1

0

May be inoperative for day operations.

 

 

 

 

 

 

 

 

 

 

(Continued)

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

33-6

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

33 LIGHTS

 

 

 

 

33-16

Exterior Emergency Lighting System

(Cont’d)

 

 

 

 

 

 

 

 2) All Cargo 

     Operations

B

1

0

May be inoperative for all-cargo night operations provided the forward entry door escape slide lights operate normally.

 

 

 

a) Forward Entry

          Door Escape

          Slide lights

 

B

-

0

May be inoperative for day operations.

 

 

 

B

-

0

May be inoperative for night operations provided the interior emergency exit system lights over

the cockpit entry door or the left forward entry door of the aircraft are removable

(for emergency use) type lights.

 

 

33-17

Floor Proximity Emergency Escape Path Marking System

 

 

 

 

 

 

 

 1) Incandescent

     Lighting System

C

1

1

Individual lights may be inoperative provided

FAA approved minimum acceptable lighting levels specified in one of the following

documents are complied with:

a)       FAA engineering approval letter,

b)       FAA approved report of the Type Design holder,

c)       Limitations and Conditions section of the applicable Supplemental Type Certificate (STC), or

d)       An FAA approved report incorporated in the Master Drawing List for the applicable STC.

 

NOTE: Not required for all cargo operations.

 

 

 

 

 

(Continued)

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

33-7

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

33 LIGHTS

 

 

 

 

33-17

Floor Proximity Emergency Escape Path Marking System (Cont’d)

 

 

 

 

 

 

 

 2) Photoluminescent

     Lighting System

C

1

1

Components may be inoperative provided FAA approved minimum acceptable lighting levels specified in one of the following documents are complied with:

a)       FAA engineering approval letter,

b)       FAA approved report of the Type Design holder,

c)       Limitations and Conditions section of the applicable Supplemental Type Certificate (STC), or

d)       An FAA approved report incorporated in the Master Drawing List for the applicable STC.

 

NOTE: Not required for all cargo operations.

 

 

33-18

***

Master Caution System Annunciator Lights, Left and Right (Pilot’s Glareshield)

 

C

-

-

(O) One may be inoperative for normally operating systems.

 

33-19

***

Logo Lights

D

-

0

 

 

33-20

***

Sterile Cockpit Light System

(Add On System)

 

C

1

0

(O) May be inoperative provided alternate procedures are established and used.

 

33-21

Aft Airstair

Tread Lights

 

 

 

 

 

 

 

 

C

-

0

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

33-8

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

33 LIGHTS

 

 

 

 

 

 

 

 

 

 

 

33-22

Master Dim and

Test System

 

 

 

 

 

 

 

 1) Test Function

C

1

0

(M) May be inoperative provided the intended function of the associated light (s) is verified.

 

 

 

 2) Dim Function

C

1

0

May be inoperative provided:

a)       Bright function operates normally, and

b)       Light intensity is acceptable to the crew.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

    

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

34-1

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

34 NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

34-01

***

True or Calibrated Airspeed indicator (Both Analogue and EFIS)

 

C

1

0

 

 

34-02

Airspeed Indicators (IAS)

 

 

 

 

 

 

***

 1) Basic Indications

     (Pointers and

     Manual Mode

     Flag)

 

 

 

 

 

 

 

 

 

C

2

2

(M)(O) Mode Selector indicator at copilot’s station ONLY may be inoperative, and a standard airspeed indicator substituted provided:

a)       Both Mach/Airspeed warning systems operate normally,

b)       Red Line is marked on glass at 350 KIAS, and

c)       A placard is placed next to instruments starting “Red Line is the limit for Mode B operation except when existing limit speed pointer (Barber Pole) is lower.

 

***

 2) Integral Airspeed

     Reference Bug

A

2

1

One may be inoperative provided repair or replacement is made within three flight days.

 

 

***

 3) External Airspeed

     Bugs

C

-

1

May be inoperative provided alternate procedures are established and used.

 

 

***

 4) Digital Airspeed

     Readout

 

C

-

0

 

 

34-03

Mach Indicators

 

 

 

 

 

 

 

 1) Basic Mach

     Indications

C

-

1

All but one may be inoperative provided one Mach/Airspeed warning system operates normally.

 

 

 

 

C

-

0

All may be inoperative provided operating

altitude is limited to FL 330 or below.

 

 

 

(Continued)

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

34-2

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

34 NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

34-03

Mach Indicators

(Cont’d)

 

 

 

 

 

 

 

 2) Mach OFF Flag

C

-

0

May be inoperative provided all basic indicators are considered inoperative.

 

 

34-04

Mach/Airspeed Warning Systems

 

 

 

 

 

 

 

 1) B-727-100/200

     and 727-100QF

 

B

2

1

One may be inoperative provided speed is

limited to less than M .88.

 

 

 2) Valsan B-727-

     100/200RE and

     airplanes with

     STC’s ST00488SE

     or ST00507SE

B

2

1

One may be inoperative provided speed is

limited to less than M .85.

 

  

     

 

 

 

 3) B-727-100/200

     and 727-100QF

 

 

 

 

B

2

0

Both systems may be inoperative provided:

a)       Both Machmeters operate normally, and

b)       The following speed limits are observed:

Vmo - 320 KIAS below FL 260.

Mmo - .78 above FL 260.

 

 

 

B

2

0

Both systems may be inoperative, if the overspeed warning system malfunctioned

during flight by sounding earlier than scheduled, operations are limited to speeds below the warning horn setting.

 

 

 

 

B

2

0

(M) Both systems may be inoperative

 if the warning system sounded below M .86, provided the system is deactivated by pulling the associated circuit breaker, then observing the Vmo/Mmo speed limits shown below:

Vmo- 320 KIAS below FL 260.

Mmo- .78 above FL 260.

 

NOTE 1: If the operating warning system is dual

               (A/B) mode, only the selected mode is

         required to operate normally.

 

(Continued)

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

34-3

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

34 NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

34-04

Mach/Airspeed Warning Systems

(Cont’d)

 

 

 

 

 

 

 

 4) Valsan B-727-100/

     200RE Only

 

 

 

 

B

2

0

(O) Both systems may be inoperative provided:

a)       Both Machmeters operate normally, and

b)       The following speed limits are observed:

Vmo- 320 KIAS below FL 260.

Mmo- .78 above FL 260.

 

 

 

B

2

0

(O) Both systems may be inoperative, if the overspeed warning system malfunctioned during flight by sounding earlier than scheduled, operations are limited to speeds below the warning horn setting.

 

 

 

 

B

2

0

(M) Both systems may be inoperative if the warning system sounded below M .85, provided the system is deactivated by pulling the associated circuit breaker, then observing the Vmo/Mmo speed limits shown below:

Vmo- 320 KIAS below FL 260.

Mmo- .78 above FL 260.

 

NOTE: If the operating warning system is dual

            (A/B) mode, only the selected mode is

      required to operate normally

 

 

34-05

Altimeters

 

 

 

 

 

 

 

 1) Basic Altimeters

 

C

-

2

May be inoperative provided:

a)       One altimeter operates normally at each pilot station, and

b)       At least one of the above is a pneumatic, or servo pneumatic altimeter.

 

 

 ***

 2) Servo Pneumatic

     Altimeter Mode

C

-

0

(M) May be inoperative provided Altimeter remains in the pneumatic mode.

 

 

 

 

(Continued)

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

34-4

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

34 NAVIGATION

 

 

 

 

34-05

Altimeters

(Cont’d)

 

 

 

 

 

 

 

 3) Standby

     Pneumatic

     Altimeter

C

-

0

May be inoperative provided at least one of the pilot’s altimeters is a pneumatic or servo-pneumatic (switchable) altimeter.

 

 

 

 4) Air Data Display

    Unit (ADDU)

     Static Source Error

     Correction (SSEC)

     Mode

     (STC ST01011SE)

 

C

1

0

(O) May be inoperative provided operations or procedures do not require its use.

 

34-06

Altimeter Vibrators

 

 

 

 

 

 

 

 1) Servo-Pneumatic

C

2

1

One may be inoperative provided associated

air data computer function is installed and operating normally.

 

 

 

 2) Pneumatic

C

2

1

One may be inoperative provided VMC exists

at departure and arrival airports.

 

 

 

 3) Pneumatic (With 2

     Electric Altimeters)

C

1

0

May be inoperative provided VMC exists at departure and arrival airports.

 

 

 

     a) Analogue

         Instrument

         System

 

C

1

0

May be inoperative provided VMC exists at departure and arrival airports.

 

 

 

     b) EFIS Instrument

         System

C

1

0

May be inoperative provided VMC exists at departure and arrival airports.

 

 

 

 4) One Pneumatic

     and One Servo-

     Pneumatic

C

2

1

Servo-pneumatic may be inoperative provided associated air data computer function is

installed and operating normally.

 

 

 

 

C

2

1

Pneumatic may be inoperative provided VMC exists at departure and arrival airports.

 

 

34-07

DELETED

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

34-5

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

34 NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

34-08

***

Static Air Temperature Gauge (Both Analogue and EFIS)

 

D

1

0

May be inoperative provided Total Air Temperature or Ram Air Temperature gauge operates normally.

 

34-09

***

Ram Air Temperature Gauge

D

1

0

May be inoperative provided Total Air Temperature or Static Air Temperature gauge operates normally.

 

 

34-10

Total Air Temperature Gauge (Both Analogue and EFIS)

C

1

0

May be inoperative provided Ram Air Temperature or Static Air Temperature gauge operates normally.

 

 

34-11

DELETED

 

 

 

 

 

 

34-12

Standby Attitude Indicator

 

C

-

0

May be inoperative provided not required by FAR.

 

 

 

 

 

 

 

 

B

1

0

May be inoperative provided:

a)       Operations are conducted in Day VMC only, and

b)       Operations are not conducted into known or forecast VFR-on-Top conditions.

 

34-13

***

Angle of Attack Indicators

 

D

-

0

 

 

34-14

Turn and Bank Indicators

 

 

 

 

 

 

 

 1) Rate of Turn

     Indicators

C

2

1

Turn function of one instrument may be inoperative for VMC flight.

 

 

 

 

C

2

0

May be inoperative provided the Standby Horizon indicator operates normally.

 

 

34-15

DELETED

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

34-6

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

34 NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

34-16

Non-Stabilized Magnetic Compass

B

1

0

(O) May be inoperative provided any combination of three gyro or INS (IRU) stabilized Compass Systems are operative.

 

 

 

 

B

1

0

(O) May be inoperative provided:

a)       Any combination of two gyro or INS (IRU) stabilized Compass Systems operate normally, and

b)       Airplane is operated with Dual Independent Navigation Capability and under Positive Radar Control by ATC on the enroute portion of the flight.

 

 

 

 

B

1

0

(O) May be inoperative for flights that are entirely within areas of magnetic unreliability provided at least two Stabilized Directional Gyro Systems

are installed, operate normally, and used in conjunction with approved Free Gyro Navigation Techniques.

 

 

34-17

Flight Director Systems

C

-

0

May be inoperative provided approach procedures do not require its use.

 

NOTE: Any mode which operates normally

            may be used.

 

 

 ***

 1) Go-Around

     Switches

C

-

0

May be inoperative provided approach procedures do not require their use.

 

 

 ***

     a) Go Around

         Annunciation

 

 

 

C

-

0

May be inoperative provided:

a)       G/A function is not used, and

b)       Approach minimums do not require its use.

 

 ***

 2) Altitude Hold

     Mode

    (ALT/ALT HOLD)

 

C

-

0

 

 

 ***

 3) Go-Around Mode

     (G/A)

 

 

 

 

C

-

0

 

 

 

 

(Continued)

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

34-7

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

34 NAVIGATION

 

 

 

 

34-17

Flight Director Systems

(Cont’d)

 

 

 

 

 

 

 ***

 4) Nav Back Course

    Mode (NAV BACK)

 

C

-

0

May be inoperative provided approach minimums do not require its use.

 

 

 ***

 5)  VOR/LOC Mode

      (NAV/LOC)

 

C

-

0

May be inoperative provided approach minimums do not require its use.

 

 ***

 6) NAV Mode  (NAV)

 

C

-

0

 

 

34-18

Distance Measuring Equipment (DME) Systems

 

D

-

-

Any in excess of those required by FAR may be inoperative.

 

34-19

Marker Beacon Systems

 

C

-

-

May be inoperative provided approach procedures do not require its use.

 

 ***

 1) Excess Items

 

D

-

0

 

 

34-20

Doppler Navigation System

 

C

-

-

As required by FAR.

 

 ***

 1) Excess Items

 

D

-

0

 

 

34-21

Weather Radar

 

C

-

-

As required by FAR.

 

 

 1) Map

 

C

-

0

 

 

 

 2) Test

C

-

0

(O) May be inoperative provided an alternate means is developed and used to verify system operates normally.

 

 

 

 

 

 

 

 

 

(Continued)

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

34-8

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

34 NAVIGATION

 

 

 

 

34-21

Weather Radar

(Cont’d)

 

 

 

 

 

 

***

 3) Windshear

     Detection and

     Avoidance System

 

 

C

-

0

(O) May be inoperative provided:

a)       Alternate procedure are established and used, and

b)       Windshear Warning and Guidance System operates normally.

 

 

 

 

 

 

 

 

 

 

C

-

0

(O) May be inoperative provided:

a)       Alternate procedures are established and used, and

b)       Takeoffs and landings are not conducted in known or forecast windshear conditions.

 

 

 4) Display(s)

 

C

-

1

 

 

***

 5) Excess Items

 

D

-

0

 

 

34-22

Radio Compass  (ADF) Systems

 

C

-

-

As required by FAR.

 

***

 1) Excess Items

 

D

-

0

 

 

34-23

VHF Navigation Systems (VOR/ILS)

D

-

-

Any in excess of those required by FAR, and not powered by a Standby Bus, may be inoperative.

 

 

***

 1) Self Test

 

D

-

0

 

 

***

 2) Frequency

     Transfer Light

 

C

-

0

 

 

***

 3) Frequency

     Transfer Switch

 

C

-

0

 

 

 

 4) Frequency

     Selectors

C

-

-

One per each VHF Nav required by FAR must operate normally.

 

 

 

 5) Frequency

     Indicators

C

-

-

One per each VHF Nav required by FAR must operate normally.

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

34-9

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

34 NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

34-24

ATC Transponders and Automatic Altitude Reporting Systems

 

 

 

B

-

0

May be inoperative provided:

a)       Operations do not require its use, and

b)       Prior to flight, approval is obtained from ATC facilities having jurisdiction over the planned route of flight.

 

|

 

 

D

-

1

Any in excess of those required by FAR may be inoperative.

 

 

.

 1) Elementary and

     Enhanced

     Downlink

     Aircraft Reportable

     Parameters not

     Required by FAR

 

A

-

0

May be inoperative provided:

a)       Operations do not require its use, and

b)       Repairs are made prior to completion of the next heavy maintenance visit. 

 

 

|

***

 2) ADS-B Squitter

     Transmissions

 

 

A

-

0

May be inoperative provided:

a)       Operations do not require its use, and

b)       Repairs are made prior to completion

      of the next heavy maintenance visit.

 

|
|
|

|

34-25

Instrument Comparator Warning Systems

 

C

-

0

May be inoperative provided approach minimums do not require its use.

 

 

34-26

Air Data Systems (KIFIS or CADC)

 

 

 

 

C

-

-

May be inoperative provided:

a)       Dispatch deviation for affected equipment are observed, and

b)       All affected equipment is listed in this column of the individual operator’s MEL.

 

***

 1) Flight Deck Self

     Test Switches

 

 

 

 

 

 

 

 

C

-

0

(M) May be inoperative provided an alternate

test procedure is established and used.

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

34-10

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

34 NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

34-27

Altitude Alerting System

 

 

 

 

A

-

0

(O) May be inoperative provided:

a)       Autopilot with altitude hold and altitude

      capture operates normally,

b)       Enroute operations, ie RVSM, do not require its use,

c)       Airplane does not depart from a designated airport (as listed in the operator’s MEL) where repair or replacement can be made, and

d)       Repairs are made within three flight days.

 

 

|

|

|

 

|
|
|
|

 

 

 

C

-

0

May be inoperative provided it is not required by FAR.

 

 

 

 

 1) Dimming Feature

 

 

 

A

-

0

May be inoperative (failed) in the Bright Mode for day operations provided operations are limited to three flight days before repair is made.

 

 

 

 

 

 

A

-

0

May be inoperative (failed) in the Dim Mode for night operations provided operations are limited to three flight days before repair is made.

 

 

 2) Aural Alert

 

 

 

C

-

0

May be inoperative provided:

a)       Visual alert operates normally, and

b)       Auto-pilot with altitude hold and altitude 

      capture operates normally.

  

|
|
|
|

 

 3) Visual Alert

 

 

 

 

 

 

 

 

 

 

 

 

 

 

C

-

0

May be inoperative provided:

a)  Aural alert operates normally, and

b)  Auto-pilot with altitude hold and altitude 

     capture operates normally.

  

|
|
|
|

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

34-11

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

34 NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

34-28

Radio Altimeter Systems

 

 

 

 

 

 

 

 1) Indications  

     (Analogue and

     EFIS)

 

C

-

0

May be inoperative provided approach minimums or operating procedures do not require use of the indicator(s).

 

 

     a) Decision Height

         (DH)

         Annunciation,

         Set Indication,

         Set Control

 

C

-

0

May be inoperative provided approach minimums or operating procedures do not require its use.

 

 

 

 

 

 2) Receiver/

     Transmitter (R/T)

     Units    

 

 

 

 

 

 

 

    a) Dual R/T Units

 

 

 

 

 

 

C

2

1

May be inoperative provided:

a)       Failed R/T Unit by design, does not provided inputs to the GPWS, and

b)   Approach minimums or operating

      procedures do not require use of failed

      indicator.

 

 

 

A

2

0

May be inoperative provided:

a)       Dispatch deviation for GPWS inoperative, is observed,

b)       Approach minimums or operating procedures do not require use of failed indicators, and

c)       Operations are limited to not more than two flight days before repair is made.

 

 

 

     b) Single R/T

          Units

 

 

 

 

 

 

 

 

A

1

0

May be inoperative provided:

a)       Dispatch deviation for GPWS inoperative, is observed,

b)       Approach minimums or operating procedures do not require use of failed indicators, and

c)       Operations are limited to not more than two flight days before repair is made.

 

(Continued)

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

34-12

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

34 NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

34-28

Radio Altimeter Systems

(Cont’d)

 

 

 

 

 

 

 

 3) Radio Altimeter

     Indications on

     EADI

     (EFIS Instrument

     System)

 

 

 

 

A

2

0

May be inoperative provided:

a)       Dispatch deviation for GPWS inoperative, is observed,

b)       Approach minimums or operating procedures do not require its use, and

c)       Operations are limited to not more than three flight days before repair is made.

 

 

 4) R/A Test   

     Switch(es)

 

C

-

0

(M) May be inoperative provided an alternate

test procedure is established and used.

 

 

34-29

Ground Proximity Warning System (GPWS)

 

 

A

1

0

(O) May be inoperative provided:

a)       Alternate Procedures are established and used, and

b)       Repairs are made within two flight days.

 

 

 

 

|

 

 1)  (Modes 1-4)

A

4

0

(O) May be inoperative provided:

a)       Alternate procedures are established

      and used, and

b)       Repairs are made within two flight days.

 

 

 

 

 

|

 

 2) Test Mode

A

1

0

May be inoperative provided:

a)       GPWS is considered inoperative, and

b)       Repairs are made within two flight days.

 

 

 

 

|

 

 3) Glideslope

     Deviation

     (Mode 5)

 

C

-

1

 

|

 

 

B

-

0

 

 

 

 

 

 

 

    (Continued)

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

34-13

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

34 NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

34-29

Ground Proximity Warning System (GPWS)

(Cont’d)

 

 

 

 

 

 

***

 4) Advisory Callouts

B

-

0

(O) May be inoperative provided alternate procedures are established and used.

 

|

|

 

 

C

-

0

(O) May be inoperative provided:

       a)  Advisory callout not required by FAR,  

            and

       b)  Alternate procedures are established and 

            used.

 

|
|
|
|
|

***

 5) Windshear  

     Warning and

     Flight Guidance

     System

B

1

0

(O) May be inoperative provided:

a)  Alternate procedures are established

     and   used, and

b)  Windshear Detection and Avoidance

     System operates normally.

 

 

 

 

C

1

0

(O) May be inoperative provided:

a)       Alternate procedures are established and used, and

b)       Takeoffs and landings are not conducted in known or forecast windshear conditions.

 

|

***

 6) Terrain Awareness

      And Warning

      System (TAWS)

 

 

 

 

 

 

***

     a) Forward

         Looking Terrain

         Avoidance

         (FLTA) and

         Premature

         Descent Alert

         (PDA) Functions

 

 

 

 

 

B

1

0

(O) May be inoperative provided alternate procedures are established and used.

 

 

 

 

 

 

 

 

   (Continued)

|
|
|
|
|
|
|
|

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

34-14

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

34 NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

34-29

Ground Proximity Warning System (GPWS)

(Cont’d)

 

 

 

 

 

 

***

 6) Terrain Awareness

      And Warning

      System (TAWS)

(Cont’d)

 

 

 

 

 

 

***

     b) Terrain Display

          Functions

 

C

-

1

 

|
|

 

 

 

B

-

0

 

  

|

 

 

7)  Runway

     Awareness &

     Advisory System

    (RAAS)

 

C

1

0

 

|
|
|
|

34-30

***

Speed Command System

D

1

0

May be inoperative provided approach minimums or operating procedures are not dependent upon its use.

 

 

 

34-31

Long Range Navigation Systems (Other than INS i.e. Loran, Omega)

 

C

-

-

As required by FAR.

 

***

 1) Excess Items

 

D

-

0

 

 

 

34-32

***

Performance Data Computer System

 

D

-

0

 

 

***

 1) PDCS INOP Flag

     In Airspeed

     Indicator

 

D

-

0

May be inoperative provided Airspeed Bug Selector remains in manual mode.

 

 

***

 2) PDCS Command

     EPR System

D

1

0

May be inoperative provided EPR Setting Controls remain in manual mode.

 

  (Continued)

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

34-15

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

34 NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

34-32

***

Performance Data Computer System

(Cont’d)

 

 

 

 

 

 

***

 3) PDCS EPR Bugs

 

 

D

3

0

May be inoperative provided associated EPR Setting Control remains in manual mode.

 

 

34-33

***

Inertial Navigation System (INS)

 

C

-

-

As required by FAR.

 

***

 1) Excess Items

 

D

-

-

 

 

***

 2) Auxiliary Drift

     Angle/Ground

     Speed Indicator

     (Separate from

     INS CDU)

     (Add On Indicator)

 

C

-

0

 

 

34-34

***

Flight Director

Go-Around Switches

 

D

-

-

Moved to Item 34-17, Rev. 35.

 

34-35

Microwave Landing System (MLS)

 

C

-

-

As required by FAR.

 

***

 1) Excess Items

 

D

-

0

 

 

 

34-36

***

Head-Up Display System (HUD)

 

D

-

-

May be inoperative provided approach procedures do not require its use.

 

NOTE: Any mode which operates normally

            may be used.

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

34-16

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

34 NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

34-37

RMI Systems (Both Analogue and EFIS)

 

 

 

 

 

 

 

 1) Compass Cards

C

-

1

One may be inoperative provided:

a)       Associated HSI operates normally, and

b)       Remaining RMI operates normally.

 

NOTE: FOEB Policy requires both pilot’s HSI’s

            to operate normally.

 

 

 

 2) VOR/ADF

     Pointer Indication

C

-

1

May be inoperative provided other VOR/ADF system(s) operate normally and meet FAR requirements.

 

 

34-38

***

Metric Altimeter

D

-

0

 

 

 

 

34-39

True or Calibrated Airspeed Indicator

 

 

 

 

Deleted Rev. 33c, Combined with Item 34-1.

 

34-40

 

Airspeed Vibrator

 

C

2

0

 

 

34-41

Traffic Alert and Collision Avoidance System

(TCAS I & II)

B

-

0

(M) (O) May be inoperative provided:

a)       System is deactivated and secured, and

b)       Enroute and approach procedures do

      not require its use.

 

 

 

 

|

 

 

 

 

 

 

 

C

-

0

(M)(O) May be inoperative provided:

a)       Not required by FAR,

b)       System is deactivated and secured, and

c)       Enroute or approach procedures do not require its use.

 

 

 

 1) Combined Traffic

     Alert (TA) and

     Resolution

     Advisory (RA)

     Dual Display

     System(s)

C

2

1

May be inoperative on the non-flying pilot side provided:

a)       TA and RA visual display is operative on flying pilot side, and

b)       TA and RA audio function is operative on flying pilot side.

 

 

 

(Continued)

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

34-17

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

34 NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

34-41

Traffic Alert and Collision Avoidance System

(TCAS I & II)

(Cont’d)

 

 

 

 

 

 

 

 2) Resolution   

     Advisory

     (RA) Display

     System(s)

 

C

2

1

May be inoperative on non-flying pilot side.

 

 

 

 

C

-

0

(O) May be inoperative provided:

a)       Traffic Alert (TA) visual display elements and audio functions are operative,

b)       TA only mode is selected by the crew, and

c)       Enroute or approach procedures do not require its use.

 

 

 

 3) Traffic Alert (TA)

      Display System(s)

C

-

0

(O) May be inoperative provided:

a)       RA visual display and audio functions are operative, and

b)       Enroute or approach procedures do not require its use.

 

 

 

 4) Audio Functions

B

1

0

May be inoperative provided enroute or

approach procedures do not require its use.

 

|
|

***

 5) Airspace Selection

     Function

 

C

-

0

 

|
|

34-42

***

Windshear Detection and Guidance Systems

 

C

-

0

(O) May be inoperative provided alternate procedures are established and used.

 

 

34-43

Attitude Reference Systems: Vertical Gyro, INS, IRU

C

-

2

May be inoperative provided:

a)       An independent attitude reference source is available to each ADI, and

b)       Attitude reference switching and selection capability is normal.

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

34-18

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

34 NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

34-44

***

Auxiliary Vertical Gyro

D

-

0

 

 

34-45

Instrumental Source Select Switches (EFIS) (STC)

C

-

-

May be inoperative provided:

a)       Associated instruments operate from isolated sources, and

b)       Inoperative switches are not moved in flight.

 

 

34-46

***

Flight Profile Advisory System (FTA-80)

 

C

1

0

 

 

34-47

EFIS Cooling Fans (STC SA 7942SW)

 

 

 

 

 

 

 

 1) Captain’s Front

     Instrument Panel

     EFIS Fans

A

2

1

(M) One fan may be inoperative provided:

a)       Operation of the remaining fan is verified before each departure,

b)       Unpressurized flight is not contemplated, and

c)       Operations are limited to not more than three flight days before repair is made.

 

 

 

 2) First Officer’s

     Front Instrument

     Panel EFIS Fans

A

2

1

(M) One fan may be inoperative provided:

a)       Operation of the remaining fan is verified before each departure,

b)       Unpressurized flight is not contemplated, and

c)       Operations are limited to not more than three flight days before repair is made.

 

 

34-48

Comparator Reset Switch

(STC SA 7942SW)

 

C

2

0

Either pilot’s switch may be inoperative provided the associated comparator is considered inoperative.

 

 

34-49

***

Global Positioning System

D

-

0

May be inoperative provided procedures do not require its use.

 

 

34-50

***

Flight Director Approach Progress Display Panel

C

2

0

May be inoperative provided associated flight director mode is considered inoperative and not used.

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

34-19

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

34 NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

34-51

***

Radio Altimeter Altitude Display

(Rising RWY in ADI)

 

C

2

0

May be inoperative provided approach minimums do not require its use.

 

 

34-52

Horizontal Situation Indicators (HSI)

 

 

 

 

 

 

 

 1) Glide Slope

C

2

0

May be inoperative provided approach procedures do not require it use, i.e., ILS procedures are not required.

 

 

 

 2) TO-FROM

     Indicator

C

2

0

May be inoperative provide RMI VOR needle on the respective pilot’s instrument panel operates normally.

 

 

 

 3) INS Indication

 

 

 

 

 

 

***

    a) Waypoint

        ALERT Light

 

C

2

1

 

 

 ***

    b) TRUE/MAG

        Heading

        Annunciator

 

C

2

1

One may be inoperative provided INS Annunciator operates normally.

 

 

***

    c) Miles-To-Go/

        Ground Speed

 

C

2

1

 

 

***

    d) INS Annunciator

 

 

C

2

1

One may be inoperative provided TRUE/MAG Heading Annunciator operates normally.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

34-20

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

34 NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

34-53

Attitude Director Indicator (ADI)

 

 

 

 

 

 

 

***

 

 1) Course Deviation

     Indicator

A

2

1

One may be inoperative provided:

a)       Course deviation indicator in associated HSI operates normally, and

b)       Operations are limited to not more than three flight days before repair is made.

 

 

 

 

C

2

0

May be inoperative provided approach procedures do not require its use, i.e., ILS procedures are not required.

 

 

  ***

 2) Glide Slope

     Deviation Indicator

A

2

1

One may be inoperative provided:

a)       Glide slope indicator in associated HSI operates normally, and

b)       Operations are limited to not more than three flight days before repair is made.

 

 

 

 

C

2

0

May be inoperative provided approach procedures do not require its use, i.e., ILS procedures are not required.

 

 

34-54

***

 EFIS Course  

 Heading Panel

 (CHP)

 (STC SA 7942SW)

 

 

 

 

 

 

 

 1) Course Control

     (CRS CTL)

     Functions

C

2

0

May be inoperative provided associated primary course needle operates normally and can be controlled by the course knob.

 

 

 

 2) Course Direct

     Control (PUSH

     CRS DIRECT)

     Functions

 

C

2

0

 

 

 

 3) Elapsed Time (ET)

     Functions

 

 

 

 

C

2

0

 

 

 

 

  (Continued)

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

34-21

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

34 NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

34-54

***

 EFIS Course  

 Heading Panel

 (CHP)

 (STC SA 7942SW)

 (Cont’d)

 

 

 

 

 

 

 

 4) Heading Sync

     (PUSH HDG

     SYNC) Functions

 

C

2

0

 

 

 

 5) Nav. Data (NAV

     DATA) Functions

 

C

2

0

 

 

34-55

***

EFIS Display Control Panel (DCP)

(STC SA 7942SW)

 

 

 

 

 

 

 

 1) Course Preselect

     (CRS PRE)

     Functions

 

C

2

0

 

 

 

 2) Course Active

     (CRS ACT)

     Functions

C

2

1

(O) One may be inoperative provided:

a)       Associated active course is displayed on the EHSI, and

b)       Associated preselect and course transfer functions operate normally.

 

 

 

 3) Bearing (BRG)

     Functions

C

2

0

May be inoperative provided associated RMI bearing pointer operates normally.

 

 

 

 

C

2

0

May be inoperative provided approach minimums do not require its use.

 

 

 

 4) Course Transfer

     (CRS XFR)

     Functions

 

 

 

 

 

 

 

C

2

0

 

 

 

 

 

 

 

 

   (Continued)

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

34-22

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

34 NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

34-55

***

EFIS Display Control Panel (DCP)

(STC SA 7942SW)

 (Cont’d)

 

 

 

 

 

 

 

 5) Radar (RDR)

     Switches

C

2

1

One may be inoperative provided radar information can be displayed on the operative system.

 

 

 

 

C

2

0

May be inoperative provided weather radar is considered inoperative.

 

 

 

 6) DIM Functions

C

4

2

One may be inoperative on each DCP provided display brightness is acceptable to the flight crew.

 

 

 

 

 7) Select/ Range

     (SEL/ RNG)

     Controls

 

 

 

 

 

 

 

     a) Select

         Functions

C

2

0

(O) May be inoperative provided:

a)       Appropriate navigation sensor is selected in the active mode, and

b)       Associated RMI bearing pointers operate normally.

 

 

 

     b) Range

         Functions

 

C

2

0

 

 

 

 8)  EHSI Mode

      Selectors

      (ARC, MAP, HSI)

C

2

0

May be inoperative provided one EHSI operates normally in ARC or MAP mode allowing display of weather radar.

 

 

 

 

C

2

0

May be inoperative provided weather radar is considered inoperative.

 

 

34-56

***

EFIS Self Test Switches

(STC SA 7942SW)

 

 

 

 

A

2

0

(M) (O) May be inoperative provided:

a)       An alternate procedure is used to test the system prior to flight, and

b)       Operations are limited to not more than one flight day before repair is made.

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

34-23

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

34 NAVIGATION

 

 

 

 

34-57

***

Liquid Crystal Displays (LCD) (ADI & HSI) (STC ST01115AT)

 

 

 

 

A

4

3

(M) (O) First Officer’s lower LCD may be inoperative provided:

a)       First Officer’s RMI operates normally,

b)       Integrate mode is selected on First Officer’s upper LCD,

c)       Approach minimums do not require its use, and

d)       Operations are limited to not more than one flight day before repair is made.

 

 

 

34-58

***

Automatic Dependent Surveillance Broadcast

(ADS-B) System

 

D

-

0

May be inoperative provided it is not required by 14 CFR.

 

NOTE: If ADS-B is installed in lieu of or as a

            replacement for 14 CFR required

            equipment, the repair category in the

            operator’s MEL will be the same as that

            of the 14 CFR required equipment.

 

 

 

 1) Cockpit Display

     and Traffic

     Information (CDTI)

D

-

0

NOTE: Cockpit Display Traffic Information

            (CDTI) display of data from other

            Aircraft systems may be used.

 

|
|
|

 

 2) CDTI Control

     Panel

 

D

-

0

May be inoperative provided:

a)       Flight ID can be set, and

b)       Screen display is acceptable to the

       flight crew.

.

 

 

 3) Data Link

     Transmitter(s)

 

D

-

0

NOTE: In some Aircraft the Data Link

            Transmission is an integral part of the

            transponder and relief is provided in

            that section.

 

|
|
|
|

 

 4) Data Link

     Receivers

 

D

-

0

 



 

 5) ADS-B

     Applications

 

 

 

 

 

D

-

0

 

|
|

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

34-24

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

34 NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

34-59

Navigation Management System

 

 

 

 

 

 

 

 1) Navigation

     Databases

C

-

-

(O) May be out of currency provided:

a)       Current Aeronautical Charts are used to verify Navigation Fixes prior to dispatch,

b)       Procedures are established and used to verify status and suitability of Navigation Facilities used to define route of flight, and

c)       Approach Navigation Radios are manually tuned and identified..

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

35-1

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

35 OXYGEN

 

 

 

 

 

 

 

 

 

 

 

35-01

Crew Oxygen System

 

 

 

 

Deleted prior to Rev. 29.

 

35-02

Passenger / Persons Service Units

C

-

-

(M) May be inoperative for unrestricted flight operations provided:

a)       No person(s) occupies the associated seat(s), and

b)       Seat(s) are blocked from occupancy.

 

 

 

 1) Automatic

     Opening

     Feature of Door

     Latch(es)

B

-

-

(M)(O) May be inoperative unlatched, and taped closed provided:

a)       PSU oxygen system operates normally,

b)       Flight operated at FL 250 or below, and

c)       Passenger(s) / persons occupying the seat(s) with the inoperative door latch(es) are briefed on oxygen mask access.

 

 

35-03

Flight Deck Oxygen Pressure Indicators

 

 

 

 

 

 

 

 1) Crew Indicator

     (Single Indicator

      on Flight

      Engineer’s

      Panel)

 

 

 

 

 

 

 

A

1

0

(M)(O) May be inoperative provided:

a)       Before each departure, alternate procedure is used to verify oxygen supply is above minimum required for dispatch,

b)       Each regulator’s oxygen emergency lever is verified to be in the NORMAL or OFF position prior to each flight, and

c)       Operations are limited to not more than three flight days before repair is made.

 

 

 2) Passenger

     Indicator

 

 

 

 

 

 

 

 

 

C

1

0

(M) May be inoperative provided an alternate procedure is used to verify oxygen supply is above minimum required before each departure.

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

35-2

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

35 OXYGEN

 

 

 

 

 

 

 

 

 

 

 

35-04

Portable Oxygen Dispensing Units (Bottle and Mask)

 

 

 

 

 

 

D

-

-

(M) Any in excess of those required by FAR may be unserviceable or missing provided:

a)       Required distribution of serviceable bottles is maintained throughout the aircraft, and

b)       Bottles not properly serviced are replaced, serviced, or removed at the next available maintenance facility.

 

35-05

Passenger Oxygen System

 

 

 

 

 

 

 

 1) Passenger and

     Combi Operations

 

 

 

 

 

 

 

 

 

 

 

 

 

 

B

1

0

(M)(O) May be inoperative provided:

a)       Flight is not conducted where the minimum altitude enroute is above 14,000 feet MSL,

b)       Both air conditioning packs, and all other components of the pressurization system operate normally,

c)       Maximum altitude does not exceed FL 250,

d)       Portable oxygen units for at least 10% of the passengers are provided, with each unit capable of delivering a minimum of 2 liters per minute for 30 minutes, and

e)       Passenger briefing procedures are modified to accommodate this operation.

 

 

 2) Cargo Operations

 

 

 

 

B

1

0

May be inoperative provided a portable oxygen supply sufficient for planned operations, meeting the requirements of the operating rule, is available for each occupant.

 

 

 

 

 

 

 

 

 

 

 

D

1

0

May be inoperative provided:

a)       Associated seats are not occupied, and

b)       Any person(s) on that flight or series of flights in any compartment is verbally informed about the status of those affected seats.

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

35-3

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

35 OXYGEN

 

 

 

 

 

 

 

 

 

 

 

35-06

Protective Breathing Equipment (PBE)

 

D

-

-

Any is excess of those required by 14 CFR may be inoperative or removed provided location placarding is removed or obscured.

 

|
|
|

35-07

***

Servicing Panel Pressure Indicator

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

C

1

0

(M) May be inoperative provided Crew Oxygen Pressure is checked as required per applicable servicing procedures after each service.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

36-1

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

36 PNEUMATIC

 

 

 

 

 

 

 

 

 

 

 

36-01

Manifold Isolation Shutoff Valves

 

 

 

 

 

 

 

 1) 727-100C Class

     “E” Cargo

     Configuration

     (Excluding

     727-100QF)

 

C

2

1

(M) Left valve may be inoperative closed.

 

 

 

C

2

1

(M)(O) Right valve may be inoperative open provided No. 2 bleed air shutoff valve is installed and operating normally.

 

 

 

 2) All Others

     (Excluding

     727-100QF)

 

C

2

1

(M) One may be inoperative closed.

 

 

 

 

 

 

C

2

1

(M)(O) One may be inoperative open provided No. 2 bleed air shutoff valve is installed and operating normally.

 

36-02

Ground Pneumatic Connector Check Valve

 

C

1

0

May be inoperative closed.

 

 

 1) All Models Except

     727-100C and

     727-100QF

     Class “E” Cargo

     Configuration

 

 

 

C

1

0

(O) May be inoperative open provided:

a)       The right isolation shutoff valve and Engine No. 3 bleed air shutoff valve remains closed except for engine start,

b)       Right air conditioning pack remains OFF, and

c)       Altitude is limited to FL 250 or below.

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

36-2

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

36 PNEUMATIC

 

 

 

 

 

 

 

 

 

 

 

36-03

Precooler Temperature Control Systems

 

 

 

 

 

 

 

 1) All Models Except

     727-100QF

 

C

2

0

(M) May be inoperative provided cooling air modulating valve remains full open.

 

 

 

 

 

 

 

 

 

C

2

0

(M)(O) May be inoperative provided:

a)       Associated engine bleed remains OFF except for engine start, and

b)       AFM Configuration Limitations regarding use of No. 2 engine bleed for pack operation are observed.

 

 

 2) 727-100QF

 

 

 

 

 

 

 

 

C

3

2

(M)(O) One may be inoperative provided:

a)       Airplane is not operated in known or forecast icing conditions,

b)       Associated engine bleed valve remains closed after engine start, and

c)       AFM Configuration Limitations regarding use of No. 2 engine for pack operation is observed.

 

36-04

Precooler Systems

 

 

 

 

 

 

 

 1) All Models Except

     727-100QF

 

 

 

 

 

C

2

0

(O) May be inoperative provided:

a)       Associated pod engine bleed remains closed after start, and

b)       AFM Configuration Limitations regarding use of No. 2 engine bleed for pack operation are observed.

 

 

 2) 727-100QF

 

 

 

 

 

 

 

 

 

 

C

3

2

(O) One may be inoperative provided:

a)       Airplane is not operated in known or forecast icing conditions,

b)       Associated engine bleed valve remains closed after engine start, and

c)       AFM Configuration Limitation regarding use of No. 2 engine for pack operation is observed.

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

36-3

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

36 PNEUMATIC

 

 

 

 

 

 

 

 

 

 

 

36-05

Pneumatic Duct Pressure Indicating Systems

 

 

 

C

2

1

(O) One may be inoperative provided, that in the case of a single pack operation, the duct pressure indicator associated with the working pack operates normally.

 

36-06

Engine Bleed Air Shutoff Valves

 

 

 

 

 

 

 

 1) 727-100C and  

    100QF Class “E”

    Cargo

    Configuration

 

C

-

-

(M) Engine No. 1 valve ONLY may be inoperative closed.

 

 

 2) All Others

 

C

-

-

(M) One may be inoperative closed.

 

36-07

Engine Bleed Air Trip-Off Lights

C

2

0

(O) One or both may be inoperative provided

the associated engine bleed is not used except for engine start.

 

 

 

 1) 727-100C Cargo

     Configuration

C

2

1

(O) Left light may be inoperative provided the associated engine bleed is not used except for engine start.

 

 

 

 2) 727-100QF

C

3

2

(O) Left light only may be inoperative provided the aircraft is not operated in known or forecast icing conditions.

 

 

36-08

(Moved to 21-38)

 

 

 

 

 

 

36-09

(Moved to 21-39)

 

 

 

 

 

 

36-10

Engine No. 2 High Temperature Warning System (All except –100C and –100QF Class “E” Cargo Configuration)

 

 

 

 

 

C

1

0

(O) May be inoperative provided engine bleed is not used except for engine start.

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

36-4

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

36 PNEUMATIC

 

 

 

 

 

 

 

 

 

 

 

36-11

13th Stage Bleed Air Modulating and Shutoff Valves (Engine 1 and 3)

 

 

 

 

 

 

 

 1) All Except

     727-200F and

     727-100QF

 

C

2

0

(O) One or both may be inoperative closed.

 

 

 

C

2

1

(O) One may be inoperative open provided the associated engine bleed air shutoff valve is closed after engine start, and not opened in flight.

 

 

 

 2) 727-200F

C

2

1

(M) One valve may be inoperative closed.

 

NOTE: One pack may be inoperative provided

            it is associated with the inoperative valve.

 

 

36-12

Manifold Isolation Shutoff Valves 727-100QF with TAY 651 Engines

 

 

 

 

 

 

 

 1) No. 1 Engine

     Isolation Valve

 

C

1

0

(M) May be inoperative closed.

 

 

 2) No. 2 Engine

     Isolation Valves

C

2

1

(M) Left isolation valve only may be inoperative closed provided airplane is operated at FL250

or below.

 

 

 

 

 

 

 

 

 

 

 

 

A

2

1

(M) Left isolation valve only may be inoperative closed provided:

a)       Airplane is not operated in known or forecast icing condition, and

b)       Operations are limited to not more than three flight days before repair is made.

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

36-5

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

36 PNEUMATIC

 

 

 

 

 

 

 

 

 

 

 

36-13

***

12th Stage Shutoff Valve Open Lights

(12 SOV OPEN)

 727-100QF

 

C

3

0

 

 

36-14

***

Engine Bleed Valve Open Lights

727-100QF

 

D

3

0

 

 

36-15

12th Stage Bleed System 727-100QF with TAY 651 Engines

 

 

 

 

C

3

0

(M)(O) One may inoperative closed provided:

a)       Airplane is not operated in known or forecast icing conditions, and

b)       All other bleed components operate normally.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

38-1

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

38 WATER/WASTE

 

 

 

 

 

 

 

 

 

 

 

38-01

Potable Water Systems

 

 

 

 

 

C

-

-

(M) Individual components may be inoperative provided:

a)       Associated components are deactivated or isolated, and

b)       Associated system components are verified not to have leaks.

 

 

 

 

 

 

 

 

NOTE: Any portion of system which operates

            normally may be used.

 

 

 

 

 

 

 

 

C

-

-

(M) May be inoperative provided:

a)       System is drained, and

b)       Procedures are established to ensure that system is not serviced.

 

38-02

Lavatory Waste Systems

 

 

C

-

-

(M) Individual components may be inoperative provided:

a)       Associated components are deactivated or isolated, and

b)       Associated system components are verified not to have leaks.

 

NOTE: Any portion of system which operates

            normally may be used.

 

 

 

 1) Lavatory Waste

     Systems (Including

     Wheelchair

     Accessible

     Lavatories Not

     Required by

     14 CFR)

 

 

 

 

C

-

-

(M) Associated lavatory system(s) may be inoperative provided:

a)       Associated components are deactivated or isolated to prevent leaks, and

b)       Associated lavatory door(s) is secured closed and placarded, “INOPERATIVE- DO NOT ENTER” (unless AFM door limitation require the door to be secured in the open position).

 

NOTE: These provisions are not intended to

            prohibit inspections by crewmembers.

 

 

 

 

 

 

(Continued)

 

 

 

|
|

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B-727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

38-2

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

38 WATER/WASTE

 

 

 

 

 

 

 

 

 

 

 

38-02

Lavatory Waste Systems

(Cont’d)

 

 

 

 

 

 

 

 2) Wheelchair

     Accessible

     Lavatories 

     Required by

     14 CFR

 

 

 

 

 

B

-

-

(M) Associated lavatory system(s) may be inoperative provided:

a)       Associated components are deactivated or isolated to prevent leaks,and

b)       Associated lavatory door(s) is secured closed and placarded INOPERATIVE – DO NOT ENTER.

 

NOTE: These provisions are not intended to prohibit inspections by crewmembers.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

|
|
|
|
|
|
|

 

|
|

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION                             

AIRCRAFT:

B 727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

46-1

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

46 INFORMATION SYSTEMS

 

 

 

 

 

 

 

 

 

 

 

46-01

***

 

Electronic Flight Bag  Systems

(EFBs)

 

 

 

 

 

|
|
|

***

 1) Class 3 EFB

 

C

-

-

(O) May be inoperative provided alternate procedures are established and used.

 

NOTE: Any function, program or document  which operates normally may be used.

 

|
|

|
|

 

 

D

-

0

May be inoperative provided procedures do not require its use.

 

|
|

***

 2) Class 2 EFB

 

 

 

 

 

 

 

     a) Data

          Connectivity

C

-

-

(O) May be inoperative provided alternate procedures are established and used.

 

|
|

 

 

D

-

0

May be inoperative provided procedures do not require its use.

 

|
|

 

     b) Power

         Connections

C

-

-

(O) May be inoperative provided alternate procedures are established and used.

 

|
|

 

 

D

-

0

May be inoperative provided procedures do not require its use.

 

|
|

 

     c) Mounting

   Device

C

-

-

(M)(O) May be inoperative provided:

      a)   Associated EFB and hardware is

            secured by an alternate means or

            removed from the aircraft, and

      b)   Alternate procedures are established

            and used.

 

|
|
|
|
|
|

 

 

D

-

0

(M)(O) May be inoperative provided:

      a)   Associated EFB and hardware is

            secured by an alternate means or

            removed from the aircraft, and

b)  Procedures do not require its use.   

 

 

 

        

|
|
|
|
|

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION                             

AIRCRAFT:

B 727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

46-2

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

46 INFORMATION SYSTEMS

 

 

 

 

 

 

 

 

 

 

 

***

 3) Class 1 EFB

 

 

 

 

 

 

 

    a) Power

        Connections

C

-

-

(O) May be inoperative provided alternate procedures are established and used.

 

|
|

 

 

D

-

0

May be inoperative provided procedures do

not require its use.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

|
|

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B 727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

47-1

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

47 INERT GAS SYSTEM

 

 

 

 

 

 

 

 

 

 

 

47-01

***

Nitrogen Generation System (NGS)

 

A

1

0

(M) May be inoperative provided:

a)       NGS shutoff valve is deactivated closed, and

b)       Repairs are made within ten flight days.

 

|
|
|
|

 

  1) Nitrogen

      Generation

      Performance

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

C

1

0

 

|
|
|

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B 727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

49-1

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

49 AIRBORNE AUXILIARY POWER

 

 

 

 

 

 

 

 

 

 

 

49-01

Auxiliary Power Unit

C

1

0

May be inoperative provided procedures are not dependent upon its use.

 

 

 

 1) APU Pneumatic

     System

C

1

0

(M)O) May be inoperative and the generator used, provided the APU bleed valve remains closed.

 

 

 

 2) APU Generator

C

1

0

(O) May be inoperative and the pneumatic source used, provided the generator field relay remains open.

 

 

49-02

***

APU Exhaust Door System

 

 

 

 

 

 

 

C

1

0

(O) May be inoperative provided:

a)       APU door annunciator light operates normally,

b)       Speed is restricted to 250 KIAS if APU door annunciator light illuminates, and

c)       APU exhaust door is removed from the takeoff warning horn circuit by SB 49-25 or production equivalent.

 

49-03

APU Annunciator Lights

 

 

 

 

 

 

***

 1) APU Exhaust Door

    Annunciator light

    (APU)

 

 

 

 

C

1

0

(M) May be inoperative provided that before each departure the following is accomplished:

a)       Visually verify that the exhaust door is closed flush with the wing surface,

b)       Visually verify in wheel well that door locking cams are locked, and

c)       Deactivate door actuator by pulling and collaring the actuator circuit breaker.

 

 

 ***

 2) Louvered Exhaust

     System

     APU Light

 

C

1

0

(M) May be inoperative provided the APU fuel shutoff valve located on the left wing rear spar

is verified closed before each departure.

 

 

 3) APU Crank Light

 

 

 

C

1

0

(O) May be inoperative provided alternate procedures for verifying APU starter operation are established and used.

 

 

 4) APU Bleed Light

     (727-200)

 

 

C

1

0

May be inoperative provided the aircraft is restricted to a single pack during ground operation.

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B 727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

49-2

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

49 AIRBORNE AUXILIARY POWER

 

 

 

 

 

 

 

 

 

 

 

49-04

APU EGT Indicator

 

 

C

1

0

May be inoperative provided APU is considered inoperative.

 

49-05

APU Cockpit Hourmeter

 

C

1

0

 

 

49-06

APU Start Counter Meter

 

C

1

0

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B 727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

52-1

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

52 DOORS

 

 

 

 

52-01

Aft Entry Door

C

1

0

May be inoperative closed in the all-cargo configuration.

 

 

52-02

***

 

Forward Airstair

 

D

1

0

 

 

52-03

Aft Airstair

 

 

 

 

 

 

 

 1) Passenger Or

     Combi

     Configurations

     (Applies Only to

     727-100, and -100

     with 119 or Less

     Passengers, and

     727-200)

 

 

 

C

1

0

(M) or (O) May be hydraulically inoperative provided:

a)       Stairs can be operated manually (including free fall extension),

b)       Stairs are manually stowed and locked after preflight inspection, and

c)       When main deck cargo is being loaded or unloaded while in the mixed configuration, airstair side struts are fully extended (locked) before enplaning or deplaning passengers.

 

 

 

 2) Cargo

     Configurations

     (727-100C, 200F,

     and Other Cargo

     Conversations,

     STC’s)

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

C

1

0

(M) or (O) May be hydraulically inoperative provided:

a)       Stairs can be operated manually,

b)       No persons are seated aft of cargo unless stairs will extend by free-fall,

c)       Stairs are manually stowed and locked after preflight inspections, and

d)       When main deck cargo is being loaded or unloaded, one of the following occurs:

                                 i.            air stair side struts are fully extended (locked), using an alternate means, or

                               ii.            a tail stand is installed, or

                              iii.            an acceptable fueling and loading schedule, designed to prevent aircraft tipping, is utilized.

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B 727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

52-2

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

52 DOORS

 

 

 

 

 

 

 

 

 

 

 

52-04

Door Warning Light System (Including Main Deck Cargo Door)

 

C

-

0

(M) May be inoperative provided door(s) are verified closed and locked.

 

52-05

Center Engine Duct Access Door Warning Light

 

C

1

0

(M) May be inoperative provided door is verified closed and locked.

 

52-06

AFT AIRSTAIR Warning Light

System

C

1

0

One or both control station red lights may be inoperative when the airstair is in the DOWN

and LOCKED position.

 

 

 

 

C

1

0

One or both control station red lights may be inoperative with the airstair UP and locked provided the F/E panel amber AFT AIRSTAIR light operates normally.

 

 

 

 

 

 

 

 

 

 

 

C

1

0

F/E panel amber AFT AIRSTAIR light may be inoperative provided:

a)       Control station red light operates normally during airstair operation, and

b)       Control station red light extinguishes when locked UP.

 

 

 

 

 

C

1

0

(O) F/E panel green AFT AIRSTAIR light may

be inoperative.

 

 

 1) 727-100C, 200F,

     and 727-100,

     727-200 Cargo

     Conversions

     (STC’s) In

     Class “E”

     Configuration

 

 

 

 

 

 

 

 

C

1

0

(M) May be inoperative provided:

a)       Door is deactivated closed,

b)       No persons, cargo handlers or passengers are carried behind the cargo, and either:

1)       A tail stand is used for cargo loading and unloading, or

2)       An acceptable fueling and loading schedule, designed to prevent aircraft tipping, is utilized.

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B 727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

52-3

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

52 DOORS

 

 

 

 

52-07

***

 

Aft Airstair Pneumatic Emergency Extension System

 

 

 

 

 

C

1

0

May be inoperative provided:

a)       Boeing SB 52-60 or production equivalent has been incorporated,

b)       Passengers are limited to 119 person, and

c)       Mixed passenger/cargo operations are prohibited.

 

NOTE: Not required for all-cargo operations.

 

 

52-08

FWD Cabin Door Pressure Stop

Fittings

 

 

 

 

   

 

 

 

C

18

17

(M)(O) Either the upper aft fitting, or the fifth-from-top forward fitting may be broken or

missing provided:

a)       No visible defects on other fittings for the associated doors can be found,

b)       Auto pressurization controller operates normally and is used, and

c)       Pressure differential does not

exceed 6.8 psi.

 

NOTE: Not required for all-cargo operations.

 

 

52-09

Aft Airstair In-Flight Security Mechanism

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

A

1

0

(M) May be inoperative unlocked, or missing provided operations are limited to three flight days before repair is made.

 

NOTE: Not required for all-cargo operations.

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B 727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

52-4

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

52 DOORS

 

 

 

 

 

 

 

 

 

 

 

52-10

Lower Cargo Door Pressure Stop

Fittings

 

 

 

 

 

 

 

 

 

A

-

-

(M) One may be broken or missing on each cargo door or frame provided:

a)       There are no visible defects on the other fittings for the associated door,

b)       Auto pressurization controller operates normally and is used,

c)       Not more than 50 landings are made before completion of repairs or replacements, and

d)       Adjacent stop fittings are inspected within 25 landings.

 

 

 

 

 

C

-

-

Two may be broken or missing on any cargo door or frame provided the airplane is operated

in an approved unpressurized configuration only.

 

 

52-11

Entry/Service Door Hold Open Latch Assembly

 

C

-

0

May be inoperative for all-cargo operations.

 

 

 1) Latch Release

     Lever

C

-

0

May be inoperative for passenger or cargo operations.

 

 

52-12

Main Deck Cargo Door Electric Hydraulic Pump

(Including AEI STC

SA1368SO and

SA1797SO)

 

 

 

 

A

1

0

May be inoperative provided:

a)       Manual hand pump is designed to perform the exact same function as the electric pump, i.e. provide cargo door system hydraulic pressure only,

b)       Manual and hand pump operates normally and is used in accordance with accepted procedures, and

c)       Repairs are made within 120 days.

 

 

 1) Main Deck Cargo

     Door Electrical

     Control

     (OPEN/CLOSE)

 

C

1

0

(M) May be inoperative provided alternate procedures for opening and closing cargo door are established and used.

 

52-13

***

Cockpit Door Hinge Pin Emergency Release Cables (STC)

 

C

-

0

(O) May be broken or missing provided alternate procedures for abnormal access and egress are established.

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B 727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

52-5

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

52 DOORS

 

 

 

 

 

 

 

 

 

 

 

52-14

***

Flight Deck Door Lock System (Not FAR 25.795 Compliant)

 

A

1

0

May be inoperative provided:

a)       Flight is conducted in an all cargo

      configuration, and

b)       Repairs are made prior to the completion

      of the next heavy maintenance visit.

 

 

 

 

|
|

 

 1) Manual Lock

 

 

 

C

1

0

May be inoperative provided supplemental

flight deck door security device is installed

and operates normally.

 

NOTE: This relief applies only to SFAR 92

            compliant doors.

 

 

 

 2) Electric Lock

 

 

 

C

1

0

May be inoperative provided flight deck door

can be locked and unlocked manually by

flight crewmember.

 

52-15

 ***

Main Cabin Cargo Door Warning Light System

(STC ST01270CH, STC ST01438CH and

STC ST02128CH)

 

 

 

 

 

 

 

 1) Cargo Door

     Warning Lights

     (A and B)

 

 

 

 

 

C

2

1

(O) One (A or B) may be inoperative provided:

a)       Cargo Door and Vent Door are verified closed and locked,

b)       Vent door actuator flag is properly positioned, and

c)       Cargo Door In-Transit light operates normally.

 

NOTE: Vent Door Warning light may

            be illuminated.

 

 

 

 

 

 

 

 

(Continued)

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B 727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

52-6

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

52 DOORS

 

 

 

 

52-15

 ***

Main Cabin Cargo Door Warning Light System

(STC ST01270CH, STC ST01438CH and

STC ST02128CH)

(Cont’d)

 

 

 

 

 

 

 

 2) Cargo Door

     In-Transit Light

 

 

 

 

 

 

C

1

0

(O) May be inoperative provided:

a)       Cargo Door and Vent Door are verified closed and locked,

b)       Vent Door actuator flag is properly positioned, and

c)       Cargo Door A and B Warning light systems operate normally.

 

 

 

 3) Vent Door

      Warning Light

 

 

 

 

 

 

 

 

C

1

0

(O) May be inoperative provided:

a)       Cargo Door and Vent Door are verified closed and locked,

b)       Vent Door actuator flag is properly positioned,

c)       Cargo Door A and B Warning light systems operate normally, and

d)       Cargo Door In-Transit light operates normally.

 

 

52-16

Main Cabin Exits/ Slides (All Cargo Configuration)

 

B

-

1

L1 may be inoperative provided R1 operates normally.

 

 

 

 

 

B

-

1

R1 may be inoperative provided L1 operates normally.

 

 

 

 

 

 

 

 

 

B

-

0

May be inoperative provided:

a)       Only essential crew members including official observer in the observers seat

      are allowed on the flight, and

b)       An alternate means of egress is available.

 

 

 

 

C

-

0

All slides in the cargo area except L1/R1 may be inoperative without restriction.

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B 727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

52-7

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

52 DOORS

 

 

 

 

52-17

***

Main Cargo Door Sequence Valves

(STC SA1767SO)

 

 

 

 

 

 

B

3

0

(M)(O) May be inoperative provided:

a)       Valve(s) failed in the closed position,

b)       Associated door warning system operates normally,

c)       Door is operated using manual procedures, and

d)       Door is verified closed and locked

      prior to each flight.

 

52-18

***

Boeing/C&D Aerospace Enhanced Flight Deck Security Door

(FAR 25.795 Compliant)

 

 

 

 

 

 

 

 1) Automatic

     Locking System

 

 

 

 

 

B

1

0

(M)(O) May be inoperative provided:

a)       Automatic locking system is deactivated,

b)       Door dead bolt operates normally and is used to lock the door, and

c)       Alternate procedures are established

      and used for locking and unlocking the

      door using the dead bolt.

 

 

 

a) LED Crew

          Indicator

 

C

1

0

(O) May be inoperative provided alternate procedures are established and used.

 

 

b) Flight Deck

          Door LOCK

          Fail Light

 

C

1

0

(M) May be inoperative provided automatic lock controls are verified to operate normally.

 

 

 

 

 2) Flight Deck Door

     Panel Pressure

     Relief Latches

 

A

2

0

May be inoperative in the latched position provided repairs are made within two flight days.

 

 

3) Dead Bolt

 

 

B

1

0

May be inoperative provided automatic lock controls operate normally.

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B 727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

52-8

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

52 DOORS

 

 

 

 

 

 

 

 

 

 

 

52-19

***

Dugan Air Enhanced Flight Deck Door

(STC ST01444LA) (FAR 25.795 Compliant)

 

 

 

 

 

 

 

 1) Dead Bolt Locks

C

2

1

One may be inoperative provided remaining deadbolt operates normally.

 

 

 

 2) Flight Deck Door

     Panel Pressure

     Relief Latches

 

A

2

0

May be inoperative in the latched position provided repairs are made within two flight days.

 

 

52-20

***

Main Deck Side

Cargo Door

(STC SA1368SO

and SA1797SO)

 

 

 

 

 

 

 

 1) Latch Pin,

     Latch Base,

     Latch Hook and

     Lower Jamb Fitting

 

 

 

 

 

 

 

 

 

 

 

 

 

 

A

7

6

(M)(O) One may be broken or missing

provided:

a)       A visual check is made before

each departure that remaining

latch pins, bases, hooks and

lower jamb fittings are not

damaged,

b)       The broken / missing latch pin,

base, hook or lower jamb

fitting does not interfere with

operation of the remaining

latches, pins, hooks or lower

jamb fittings,

c)       Flight is operated in an

unpressurized configuration,

d)       Main deck cargo compartment

     remains empty, and

e)       Repairs are made within two

flights.

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B 727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

56-1

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

56 WINDOWS

 

 

 

 

 

 

 

 

 

 

 

11-01

***

 1) Pilot’s Left Sliding

     Window External

     Emergency

     Opening System

 

 

 

 

 

 

 

1) Passenger

        Configuration

 

C

1

0

 

 

 

2) Cargo

         Configuration

C

1

0

May be inoperative provided an approved rigid bulkhead, or equivalent, is properly installed.

 

 

 

 

C

1

0

May be inoperative provided main cargo compartment remains empty.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B 727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

73-1

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

73 ENGINE FUEL & CONTROL

 

 

 

 

 

 

 

 

 

 

 

73-01

DELETED

 

 

 

 

 

 

73-02

Fuel Filter Heater System

 

 

 

 

C

3

0

(M)(O) May be inoperative provided:

a)       Fuel temperature is maintained at or above 0 degrees C (32 degrees F), and

b)       Associated fuel deicing air valve is deactivated closed.

 

73-03

Fuel Heat Valve Lights

 

 

 

 

C

3

2

(O) One may be inoperative provided:

a)       The associated valve operates normally prior to each flight, and

b)       Oil temperature gauge is monitored during flight.

 

73-04

Fuel Filter Differential Pressure Warning Systems

 

C

3

2

(O) One may be inoperative provided heater system operates normally.

 

73-05

***

APR System

 

 

 

 

D

1

0

(O) May be inoperative provided:

a)       System is deactivated, and

b)       Operations are conducted in

      accordance with AFM.

 

73-06

***

Engine Fuel Shutoff Valve Start Lever Switches

 

D

3

0

(M) May be inoperative provided F/E fuel shutoff switches are installed and operating normally.

 

73-07

Fuel Flow Meters

 

 

 

 

 

C

3

2

One may be inoperative provided:

a)       N1, N2 and EPR gauges for the associated engine operate normally, and

b)       The associated fuel quantity gauges operate normally.

 

73-08

***

Fuel Used Gauges

 

D

3

0

 

 

73-09

Dual Datum Idle Control System

727-100QF with TAY 651 Engines

 

 

 

 

C

3

0

May be inoperative failed in Flight Idle provided:

a)       Anti Skid System operates normally, and

b)       For operating weights of 110,000 lbs. and below, use V Speeds and Field Length required for 110,000 lbs.

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B 727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

73-2

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

73 ENGINE FUEL & CONTROL

 

 

 

 

 

 

 

 

 

 

 

73-10

Fuel Low Pressure Lights

(TAY 651 Engines)

 

 

 

C

3

2

(M) One may be inoperative provided:

a)       Associated Engine (tank) fuel boost pumps operate normally, and

b)       Associated engine fuel filter differential pressure warning lights operate normally.

 

73-11

Approach Idle Functions (Valsan B-727-100/ 200RE Only)

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

C

2

1

(M)(O) May be inoperative on one engine provided any appropriate AFM Performance Limitations are observed.

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B 727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

74-1

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

74 IGNITION

 

 

 

 

 

 

 

 

 

 

 

74-01

High Energy Ignition Systems

(Three Twin 20-Joule Systems or Three Dual 18-Joule Systems)

 

C

6

3

One system on each engine may be inoperative.

 

74-02

Low Energy Ignition Systems

 

 

 

C

3

0

(O) Any or all may be inoperative provided switching is available to select FLIGHT for high energy continuous ignition.

 

74-03

High Energy Ignition Systems

(Three Twin 10-Joule Systems 727-100QF)

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

C

6

5

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B 727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

77-1

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

77 ENGINE INDICATING

 

 

 

 

 

 

 

 

 

 

 

77-01

Engine Pressure Ratio Systems

 

 

 

 

 

 

 

 1) All models

     without STC’s

     ST00555SE,

     ST00399SE, or

     ST00448SE

 

 

 

 

 

 

 

 

A

3

2

(O) One may be inoperative provided:

a)       Before the loss of the EPR gauge, all associated engine indications were normal,

b)       N1, N2 and fuel flow meter on the associated engine operate normally,

c)       Appropriate N1 thrust setting curves are available,

d)       Assumed temperature reduced thrust is not permitted,

e)       727-100QF apply appropriate AFM performance corrections, and

f)         Operations are limited to not more than three flight days before repair is made.

 

 

 

 2) All models with

     STC’s

     ST00555SE,

     ST00399SE, or

     ST00448SE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

A

3

2

(M)(O) One may be inoperative provided:

a)       Before the loss of the EPR gauge, all associated engine indications were normal,

b)       N1, N2 and fuel flow meter on the associated engine operate normally,

c)       Appropriate N1 thrust setting curves are available,

d)       Assumed temperature reduced thrust is not permitted,

e)       727-100QF apply appropriate AFM performance corrections,

f)         Associated EPR indicator circuit breaker is pulled if engine No. 1 or No. 3 indicator is inoperative (only allowed if there is a separate circuit breaker for the EPR indicator),

g)       Takeoff is not made with flaps in the 25 degree position if engine No. 1 or No. 3 indicator is inoperative, and

h)       Operations are limited to not more than three flight days before repair is made.

 

  

(Continued)

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B 727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

77-2

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

77 ENGINE INDICATING

 

 

 

 

77-01

Engine Pressure Ratio Systems

(Cont’d)

 

 

 

 

 

 

 

 3) Digital Indicator

     (All models)

 

C

3

0

 

 

 

 4) EPR Bug

     (Alll models)

A

3

2

One may be inoperative provided operations are limited to not more than three flight days before repair is made.

 

 

77-02

N1 Tachometers

 

 

 

 

 

B

3

2

(M)(O) One may be inoperative provided:

a)       EPR, N2 and fuel flow meters on the associated engine operate normally, and

b)       APR System is not required for takeoff performance.

 

***

 1) Digital Indicators

 

 

C

3

0

 

 

77-03

N2 Tachometers

 

 

 

 

B

3

2

(O) One may be inoperative provided:

a)       EPR, N1 and fuel flow indicators for the associated engine operate normally, and

b)       An alternate starting procedure is used.

 

***

 1) Digital Indicators

 

 

C

3

0

 

 

77-04

MOVED TO 73-7

 

 

 

 

 

 

77-05

EGT Gauges

 

 

 

 

 

 

***

 1) Over temperature

     Warning Lights

     (Amber)

 

 

 

 

 

 

 

D

3

0

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B 727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

77-3

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

77 ENGINE INDICATING

 

 

 

 

 

 

 

 

 

 

 

77-06

***

Vibration Indicating System

 

C

1

0

May be inoperative unless required by maintenance procedures.

 

 

77-07

Engine Failure Detection Lights

 

 

 

C

2

0

(O) May be inoperative provided:

a)       APR System is not used, and

b)       AFM performance data and procedures are observed.

 

77-08

MOVED to 73-5

 

 

 

 

 

 

77-09

MOVED to 73-8

 

 

 

 

 

 

77-10

Turbine Gas Temperature Gauges (TGT)

(TAY 651 Engines)

 

 

 

 

 

 

 

 1) Digital Indicators

 

C

3

0

 

 

77-11

Engine Overheat Warning Light Bright/Dim Switch

727-100QF

 

C

1

0

Switch select function may be inoperative.

 

77-12

Engine Idle Lights

727-100QF

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

C

3

2

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B 727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

78-1

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

78 ENGINE EXHAUST

 

 

 

 

 

 

 

 

 

 

 

78-01

Thrust Reversers

 

 

 

 

 

 

 

 1) B-727-100/200

     Only

 

 

 

 

 

 

C

3

2

(M) One may be inoperative provided:

a)       There is no damage to the thrust reverser system that would adversely affect operation of the airplane, and

b)       A procedure is established to determine the related thrust reverser is locked in the closed (forward thrust) position.

 

 

 2) Valsan

     B-727–100/200RE

     Only

 

 

 

 

 

 

 

 

 

 

 

 

C

2

1

(M) One may be inoperative provided:

a)       There is no damage to the thrust reverser system that would adversely affect operation of the airplane,

b)       No external leakage exists,

c)       The respective THRUST REV. ACCUM. LOW PRESS light is deactivated, and

d)       A procedure is established to determine the related thrust reverser is locked in the closed (forward thrust) position.

 

NOTE: On airplanes with Auto Spoiler RTO

            feature, if No. 1 Reverser System is

            inoperative, the Auto Spoiler RTO

            feature will also be inoperative.

 

 

 

 3) B-727-100QF

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

C

2

1

(M) One may be inoperative provided:

a)       There is no damage to the thrust reverser system that would adversely affect operation of the airplane,

b)       No external leakage exists, and

c)       A procedure is established to determine that the related thrust reverser is locked in the closed (forward thrust) position.

 

 

 

 

 

 

 

 

(Continued)

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B 727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

78-2

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

78 ENGINE EXHAUST

 

 

 

 

78-01

Thrust Reversers (Cont’d)

 

 

 

 

 

 

 

 4) B-727-100/200

     With Quiet Wing

     System

     STC’s ST00488SE

     or ST00507SE

 

 

 

 

C

2

1

(M) One may be inoperative provided:

a)       There is no damage to the thrust reverser system that would adversely affect operation of the airplane, and

b)       A procedure is established to determine that the related thrust reverser is locked in the closed (forward thrust) position.

 

78-02

Thrust Reversers Operating Lights

 

 

 

 

 

 

 

 1) B-727-100/200

     Only

 

 

 

 

 

 

C

3

0

(M) May be inoperative provided:

a)       There is no damage to the thrust reverser system that would adversely affect operation of the airplane, and

b)       A procedure is established to determine the related thrust reverser is locked in the closed (forward thrust) position.

 

 

 2) Valsan

     B-727-100/200RE,

     B727-100QF and

     airplanes with

     STC’s ST00488SE

     or ST000507SE

 

 

C

2

0

(M) May be inoperative provided:

a)       There is no damage to the thrust reverser system that would adversely affect operation of the airplane, and

b)       A procedure is established to determine the related thrust reverser is locked in the closed (forward thrust) position.

 

 

78-03

Thrust Reverser In Transit Lights

 

 

 

 

 

 

 

 1) B-727-100/200

     Only (Excluding

     B-727-100QF)

 

C

3

0

 

 

 

 2) Valsan

     B-727-100/200RE

     Only

 

 

C

2

0

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B 727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

78-3

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

78 ENGINE EXHAUST

 

 

 

 

 

 

 

 

 

 

 

78-04

Thrust Reverser Accumulator

Pressure Indicator (Valsan B-727-100/200RE Only)

 

C

2

0

(M) One or both may be inoperative provided:

a)       No external leakage exists, and

b)       Respective THRUST REV. ACCUM. LOW PRESS light(s) operate normally.

 

78-05

Thrust Reverser Accumulator Lights (Valsan B-727-100/200RE Only)

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

C

2

0

(M) One or both may be inoperative provided:

a)       No external leakage exists, and

b)       Respective thrust reverser accumulator pressure indicator(s) operate(s) normally and are checked before each departure.

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B 727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

79-1

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

79 ENGINE OIL

 

 

 

 

 

 

 

 

 

 

 

79-01

Oil Quantity Indicators

 

 

 

 

 

 

 

 1) All Models Except

     727-100QF

 

 

 

 

 

 

 

 

B

3

2

(M) One may be inoperative provided:

a)       Associated oil tank is filled to maximum recommended capacity before each refueling,

b)       There is no evidence of above normal

       oil consumption or leakage, and

c)       Associated low oil pressure warning

      light, and oil temperature and oil

      pressure indicators operate normally.

 

 

 2) 727-100QF

 

 

 

 

 

 

 

 

 

 

C

3

0

(M) May be inoperative provided:

a)       It is verified that the associated oil tank level is adequate for the flight being planned including alternate planning considerations, and

b)       It is verified that the oil tank level is not more than two quarts low before each refueling.

 

NOTE: The oil quantity indicators on the

            TAY 651 engines are not operative

            in flight.

 

 

 

 3) Oil Quantity

     Indicator Test

     Feature

     (All Models)

 

 

 

 

 

 

 

 

 

C

1

0

(M) May be inoperative provided:

a)       Oil quantities are checked once each flight day for correct service,

b)       There is no evidence of above normal

       oil consumption or leakage, and

c)       Engine low oil pressure warning lights, and oil temperature and oil pressure indicators operate normally.

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B 727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

79-2

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

79 ENGINE OIL

 

 

 

 

 

 

 

 

 

 

 

79-02

Oil Filter Bypass

Warning Lights

 

 

 

 

 

C

3

2

(M) One may be inoperative provided:

a)       Malfunction is in the warning system,

      and

b)       Associated main oil screen is inspected

      for presence of contaminants at least

      every 12 hours.

 

79-03

DELETED

 

 

 

 

 

 

79-04

Oil Low Pressure Warning Lights

 

 

B

3

2

(O) One may be inoperative provided the associated engine oil pressure, oil temperature and oil quantity indicators operate normally.

 

79-05

DELETED

 

 

 

 

 

 

79-06

***

Engine Oiler System (STC SA 1327SO)

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

C

1

0

(M) May be inoperative provided alternate (normal) procedures are established and used.

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                                                                                MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

B 727-100/200

REVISION NO:      49

 

DATE:   06/06/2012

PAGE:

 

80-1

SYSTEM &

SEQUENCE

NUMBERS

ITEM

 

1.

2.

NUMBER INSTALLED

 

 

3.

NUMBER REQUIRED FOR DISPATCH

 

 

 

4.

REMARKS OR EXCEPTIONS

80 STARTING

 

 

 

 

 

 

 

 

 

 

 

80-01

***

 

Starter Valve Open Lights

 

 

 

 

 

 

 

 1) All Models Except

     727-100QF

 

 

C

3

0

(O) May be inoperative provided the Start Valve Arming System is installed and operating normally.

 

 

 2) 727-100QF

 

 

 

 

 

A

3

0

(O) May be inoperative provided:

a)       Associated start valve is verified closed after engine start, and

b)       Operations are limited to not more than three flight days before repair is made.

 

80-02

***

Engine Starter Auto Cutout System

 

 

 

 

 

 

 

 1) All Models Except

     727-100QF

 

 

C

3

0

(O) May be inoperative provided associated

start switch is manually selected OFF at 40 per cent N2 RPM.

 

 

 2) 727-100QF

 

 

 

C

3

0

(O) May be inoperative provided associated

start switch is manually selected OFF at 42 per cent N2 RPM.

 

80-03

Starter Valves

 

 

 

C

3

0

(M)(O) May be inoperative provided alternate starting procedures are established and used.

 

80-04

***

Start Valve Arming

System

 

 

 

 

 

 

 

 

 

 

 

 

C

1

0

(O) May be inoperative provided Starter Valve Open Lights are installed and operating normally.