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TRANSPORT CANADA MMEL SUPPLEMENT TO BOEING 737-8 MASTER MINIMUM EQUIPMENT LIST Chief, Flight Test National Aircraft Certification for Minister of Transport September 24, 2020 Revision: 08

TRANSPORT CANADA MMEL SUPPLEMENT TO BOEING 737-8 … · 2020. 9. 28. · Supplement BOEING 737-8 Page: VI Revision: 08 24 SEP 2020 Introduction This Transport Canada MMEL Supplement

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Page 1: TRANSPORT CANADA MMEL SUPPLEMENT TO BOEING 737-8 … · 2020. 9. 28. · Supplement BOEING 737-8 Page: VI Revision: 08 24 SEP 2020 Introduction This Transport Canada MMEL Supplement

TRANSPORT CANADA

MMEL SUPPLEMENT

TO

BOEING 737-8

MASTER MINIMUM EQUIPMENT LIST

Chief, Flight Test

National Aircraft Certification

for Minister of Transport

September 24, 2020

Revision: 08

Page 2: TRANSPORT CANADA MMEL SUPPLEMENT TO BOEING 737-8 … · 2020. 9. 28. · Supplement BOEING 737-8 Page: VI Revision: 08 24 SEP 2020 Introduction This Transport Canada MMEL Supplement

INTENTIONALLY LEFT BLANK

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TRANSPORT CANADA Master Minimum Equipment List

Supplement BOEING 737-8

Page: I Revision: 08 24 SEP 2020

List of Effective Pages

Title Page

List of Effective Pages I Rev 08 24 SEP 2020

II Rev 08 24 SEP 2020

III Rev 08 24 SEP 2020

Log of Revisions IV Rev 08 24 SEP 2020

Reasons for Changes V Rev 08 24 SEP 2020

Introduction VI Rev 08 24 SEP 2020

Pages 21-1 Original 07 JUN 2017

21-2 Original 07 JUN 2017

21-3 Rev 01 24 AUG 2017

21-4 Original 07 JUN 2017

21-5 Rev 01 24 AUG 2017

21-6 Rev 01 24 AUG 2017

21-7 Original 07 JUN 2017

21-8 Original 07 JUN 2017

21-9 Original 07 JUN 2017

22-1 Rev 08 24 SEP 2020

22-2 Rev 08 24 SEP 2020

23-1 Original 07 JUN 2017

23-2 Original 07 JUN 2017

23-3 Original 07 JUN 2017

23-4 Original 07 JUN 2017

23-5 Original 07 JUN 2017

23-6 Rev 08 24 SEP 2020

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TRANSPORT CANADA Master Minimum Equipment List

Supplement BOEING 737-8

Page: II Revision: 08 24 SEP 2020

List of Effective Pages (cont’d)

Pages 23-7 Original 07 JUN 2017

25-1 Original 07 JUN 2017

25-2 Original 07 JUN 2017

25-3 Rev 02 23 MAR 2018

25-4 Rev 08 24 SEP 2020

25-5 Rev 08 24 SEP 2020

25-6 Rev 08 24 SEP 2020

25-7 Rev 08 24 SEP 2020

25-8 Rev 08 24 SEP 2020

25-9 Rev 08 24 SEP 2020

26-1 Original 07 JUN 2017

26-2 Original 07 JUN 2017

26-3 Rev 02 23 MAR 2018

26-4 Original 07 JUN 2017

26-5 Original 07 JUN 2017

26-6 Original 07 JUN 2017

27-1 Rev 07 19 JUN 2019

27-2 Rev 07 19 JUN 2019

30-1 Original 07 JUN 2017

31-1 Original 07 JUN 2017

31-2 Original 07 JUN 2017

32-1 Original 07 JUN 2017

32-2 Original 07 JUN 2017

33-1 Original 07 JUN 2017

33-2 Original 07 JUN 2017

Page 5: TRANSPORT CANADA MMEL SUPPLEMENT TO BOEING 737-8 … · 2020. 9. 28. · Supplement BOEING 737-8 Page: VI Revision: 08 24 SEP 2020 Introduction This Transport Canada MMEL Supplement

TRANSPORT CANADA Master Minimum Equipment List

Supplement BOEING 737-8

Page: III Revision: 08 24 SEP 2020

List of Effective Pages (cont’d)

Pages 33-3 Original 07 JUN 2017

34-1 Rev 02 23 MAR 2018

34-2 Rev 08 24 SEP 2020

34-3 Rev 08 24 SEP 2020

34-4 Rev 02 23 MAR 2018

34-5 Original 07 JUN 2017

35-1 Original 07 JUN 2017

35-2 Original 07 JUN 2017

35-3 Original 07 JUN 2017

35-4 Original 07 JUN 2017

38-1 Original 07 JUN 2017

38-2 Original 07 JUN 2017

49-1 Rev 05 15 JUN 2018

50-1 Original 07 JUN 2017

52-1 Original 07 JUN 2017

52-2 Original 07 JUN 2017

73-1 Original 07 JUN 2017

75-1 Rev 02 23 MAR 2018

77-1 Rev 04 11 MAY 2018

Page 6: TRANSPORT CANADA MMEL SUPPLEMENT TO BOEING 737-8 … · 2020. 9. 28. · Supplement BOEING 737-8 Page: VI Revision: 08 24 SEP 2020 Introduction This Transport Canada MMEL Supplement

TRANSPORT CANADA Master Minimum Equipment List

Supplement BOEING 737-8

Page: IV Revision: 08 24 SEP 2020

Log of Revisions

Revision No. Date Page Number Initials

Original 07 JUN 2017 All

01 24 AUG 2017 I, II, III, IV, V, VI, 21-3, 21-5, 21-6, 25-6 to 25-10

02 23 MAR 2018 I, II, III, IV, V, VI, 25-3, 25-6, 26-3, 27-1, 34-1, 34-4, 75-1

03 06 APR 2018 I, II, III, IV, V, VI, 77-1

04 11 MAY 2018 I, II, III, IV, V, VI, 77-1

05 18 JUN 2018 I, II, III, IV, V, VI, 49-1

06 01 APR 2019 I, II, III, IV, V, VI, 22-1

07 19 JUN 2019 I, II, III, IV, V, VI, 27-1, 27-2

08 24 SEP 2020 I, II, III, IV, V, VI, 22-1, 22-2, 23-6, 25-4 to 25-9, 34-2, 34-3

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TRANSPORT CANADA Master Minimum Equipment List

Supplement BOEING 737-8

Page: V Revision: 08 24 SEP 2020

Reasons for Changes

22-10-02 Deleted.

22-11-10 Added (O) and proviso (a) to item A. Item B deleted.

23-42-03 Item 23-42-03-02 is harmonized with FAA MMEL.

25-22-01 Added relief for STC SA19-27.

25-40-01 Removed from TCS. Harmonized with FAA MMEL.

34-36-01 Add relief for STC ST02522SE.

34-49-01 Removed (O) from 34-49-01-01-05.

Page 8: TRANSPORT CANADA MMEL SUPPLEMENT TO BOEING 737-8 … · 2020. 9. 28. · Supplement BOEING 737-8 Page: VI Revision: 08 24 SEP 2020 Introduction This Transport Canada MMEL Supplement

TRANSPORT CANADA Master Minimum Equipment List

Supplement BOEING 737-8

Page: VI Revision: 08 24 SEP 2020

Introduction

This Transport Canada MMEL Supplement constitutes a mandatory change to the FAA Approved MMEL for the BOEING 737-8 aircraft. The B737-9 MMEL has not been validated in Canada.

This MMEL Supplement must be used in conjunction with the FAA Approved MMEL (Revision No. 2, dated 10 April 2020, or later applicable revision).

The information contained herein supersedes the existing FAA MMEL only for those items listed herein. For items not contained in this Supplement, consult the FAA approved MMEL.

Operating and/or maintenance procedures referred to in this Supplement are the same as those supporting the FAA MMEL unless otherwise indicated. Procedures required by the Transport Canada MMEL Supplement and not indicated in the FAA Approved MMEL must be provided by the operator.

The FAA MMEL has entries where the “Remarks or Exceptions” column makes reference to applicable FARs. Unless such an entry is superseded by an item in this Supplement, all references should be made to the applicable Canadian regulation.

This MMEL Supplement uses the standard four column format as referenced in the Transport Canada MMEL/MEL Policy and Procedures Manual (TP 9155E). The same definitions and symbols as the FAA MMEL are also used. Items which have no MMEL relief (i.e. relief withdrawn) are not categorized.

Comments and inquiries should be directed to:

Transport Canada Chief, Flight Test - AARDC National Aircraft Certification

Page 9: TRANSPORT CANADA MMEL SUPPLEMENT TO BOEING 737-8 … · 2020. 9. 28. · Supplement BOEING 737-8 Page: VI Revision: 08 24 SEP 2020 Introduction This Transport Canada MMEL Supplement

TRANSPORT CANADA Master Minimum Equipment List

Supplement

Aircraft:

BOEING 737-8

Revision No. Original Page:

Date: 07 JUN 2017 21-1

System & 1. 2. Number Installed

Sequence 3. Number Required for Dispatch

Numbers 4. Remarks or Exceptions

21 AIR CONDITIONING

21-01 Ground Conditioned Air Connector Check Valve

21-01A C 1 0 No change from FAA MMEL.

21-01B C 1 0 (M)(O) May be inoperative provided:

a) Flight is conducted in an unpressurized configuration at or below 10,000 ft MSL,

b) No change from FAA MMEL,

c) No change from FAA MMEL, and

d) No change from FAA MMEL.

NOTE: Unit Load Devices (ULDs) may be carried provided no cargo is carried on or in these devices. For ballast purposes, use of bags (made of glass fibre or Kevlar) of sand or ingots of non-magnetic metals (such as lead) is acceptable.

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TRANSPORT CANADA Master Minimum Equipment List

Supplement

Aircraft:

BOEING 737-8

Revision No. Original Page:

Date: 07 JUN 2017 21-2

System & 1. 2. Number Installed

Sequence 3. Number Required for Dispatch

Numbers 4. Remarks or Exceptions

21 AIR CONDITIONING

27-02 Overboard Exhaust Valve

27-02A C 1 0 (M) No change from FAA MMEL.

27-02B C 1 0 (M)(O) May be inoperative in open position provided:

a) Flight is conducted in an unpressurized configuration at or below 10,000 ft MSL,

b) No change from FAA MMEL,

c) No change from FAA MMEL, and

d) No change from FAA MMEL.

NOTE: Unit Load Devices (ULDs) may be carried provided no cargo is carried on or in these devices. For ballast purposes, use of bags (made of glass fibre or Kevlar) of sand or ingots of non-magnetic metals (such as lead) is acceptable.

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TRANSPORT CANADA Master Minimum Equipment List

Supplement

Aircraft:

BOEING 737-8

Revision No. 01 Page:

Date: 24 AUG 2017 21-3

System & 1. 2. Number Installed

Sequence 3. Number Required for Dispatch

Numbers 4. Remarks or Exceptions

21 AIR CONDITIONING

31-01 Cabin Pressure Control Systems

31-01-01A Automatic Mode C 2 1 (M)(O) No change from FAA MMEL.

31-01-01B Automatic Mode C 2 0 (M)(O) Both automatic modes may be inoperative provided:

a) Flight is conducted in an unpressurized configuration at or below 10,000 ft MSL,

b) No change from FAA MMEL,

c) No change from FAA MMEL, and

d) No change from FAA MMEL.

NOTE: Unit Load Devices (ULDs) may be carried provided no cargo is carried on or in these devices. For ballast purposes, use of bags (made of glass fibre or kevlar) of sand or ingots of non-magnetic metals (such as lead) is acceptable.

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TRANSPORT CANADA Master Minimum Equipment List

Supplement

Aircraft:

BOEING 737-8

Revision No. Original Page:

Date: 07 JUN 2017 21-4

System & 1. 2. Number Installed

Sequence 3. Number Required for Dispatch

Numbers 4. Remarks or Exceptions

21 AIR CONDITIONING

31-01 Cabin Pressure Control Systems (cont’d)

31-01-02 Manual Mode C 1 0 (M)(O) May be inoperative provided:

a) Flight is conducted in an unpressurized configuration at or below 10,000 ft MSL,

b) No change from FAA MMEL,

c) No change from FAA MMEL,

d) No change from FAA MMEL, and

e) No change from FAA MMEL.

NOTE: Unit Load Devices (ULDs) may be carried provided no cargo is carried on or in these devices. For ballast purposes, use of bags (made of glass fibre or Kevlar) of sand or ingots of non-magnetic metals (such as lead) is acceptable.

31-02 Main Outflow Valve C 1 0 (M)(O) May be inoperative provided:

a) Flight is conducted in an unpressurized configuration at or below 10,000 ft MSL,

b) No change from FAA MMEL,

c) No change from FAA MMEL,

d) No change from FAA MMEL, and

e) No change from FAA MMEL.

NOTE: Unit Load Devices (ULDs) may be carried provided no cargo is carried on or in these devices. For ballast purposes, use of bags (made of glass fibre or Kevlar) of sand or ingots of non-magnetic metals (such as lead) is acceptable.

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TRANSPORT CANADA Master Minimum Equipment List

Supplement

Aircraft:

BOEING 737-8

Revision No. 01 Page:

Date: 24 AUG 2017 21-5

System & 1. 2. Number Installed

Sequence 3. Number Required for Dispatch

Numbers 4. Remarks or Exceptions

21 AIR CONDITIONING

32-01 Positive Pressure Relief Valves

32-01A C 2 1 (M) No change from FAA MMEL.

32-01B C 2 0 (M)(O) May be inoperative provided:

a) Flight is conducted in an unpressurized configuration at or below 10,000 ft MSL,

b) No change from FAA MMEL,

c) No change from FAA MMEL, and

d) No change from FAA MMEL.

NOTE: Unit Load Devices (ULDs) may be carried provided no cargo is carried on or in these devices. For ballast purposes, use of bags (made of glass fibre or Kevlar) of sand or ingots of non-magnetic metals (such as lead) is acceptable.

Page 14: TRANSPORT CANADA MMEL SUPPLEMENT TO BOEING 737-8 … · 2020. 9. 28. · Supplement BOEING 737-8 Page: VI Revision: 08 24 SEP 2020 Introduction This Transport Canada MMEL Supplement

TRANSPORT CANADA Master Minimum Equipment List

Supplement

Aircraft:

BOEING 737-8

Revision No. 01 Page:

Date: 24 AUG 2017 21-6

System & 1. 2. Number Installed

Sequence 3. Number Required for Dispatch

Numbers 4. Remarks or Exceptions

21 AIR CONDITIONING

33-01 Cabin Rate of Climb Indicator

33-01-01 Pressurized Flight C 1 0 No change from FAA MMEL.

33-01-02 Unpressurized Flight C 1 0 (M)(O) May be inoperative provided:

a) Flight is conducted in an unpressurized configuration at or below 10,000 ft MSL,

b) No change from FAA MMEL,

c) No change from FAA MMEL, and

d) No change from FAA MMEL.

NOTE: Unit Load Devices (ULDs) may be carried provided no cargo is carried on or in these devices. For ballast purposes, use of bags (made of glass fibre or Kevlar) of sand or ingots of non-magnetic metals (such as lead) is acceptable.

Page 15: TRANSPORT CANADA MMEL SUPPLEMENT TO BOEING 737-8 … · 2020. 9. 28. · Supplement BOEING 737-8 Page: VI Revision: 08 24 SEP 2020 Introduction This Transport Canada MMEL Supplement

TRANSPORT CANADA Master Minimum Equipment List

Supplement

Aircraft:

BOEING 737-8

Revision No. Original Page:

Date: 07 JUN 2017 21-7

System & 1. 2. Number Installed

Sequence 3. Number Required for Dispatch

Numbers 4. Remarks or Exceptions

21 AIR CONDITIONING

33-02 Cabin Differential Pressure Indication

33-02-01 Cabin Altitude Indication Operative

C 1 0 No change from FAA MMEL.

33-02-02 Unpressurized Flight C 1 0 (M)(O) May be inoperative provided:

a) Flight is conducted in an unpressurized configuration at or below 10,000 ft MSL,

b) No change from FAA MMEL,

c) No change from FAA MMEL, and

d) No change from FAA MMEL.

NOTE: Unit Load Devices (ULDs) may be carried provided no cargo is carried on or in these devices. For ballast purposes, use of bags (made of glass fibre or Kevlar) of sand or ingots of non-magnetic metals (such as lead) is acceptable.

Page 16: TRANSPORT CANADA MMEL SUPPLEMENT TO BOEING 737-8 … · 2020. 9. 28. · Supplement BOEING 737-8 Page: VI Revision: 08 24 SEP 2020 Introduction This Transport Canada MMEL Supplement

TRANSPORT CANADA Master Minimum Equipment List

Supplement

Aircraft:

BOEING 737-8

Revision No. Original Page:

Date: 07 JUN 2017 21-8

System & 1. 2. Number Installed

Sequence 3. Number Required for Dispatch

Numbers 4. Remarks or Exceptions

21 AIR CONDITIONING

33-03 Cabin Altitude Indication

33-03-01 Cabin Differential Pressure Indication Operative

C 1 0 No change from FAA MMEL.

33-03-02 Unpressurized Flight C 1 0 (M)(O) May be inoperative:

a) Flight is conducted in an unpressurized configuration at or below 10,000 ft MSL,

b) No change from FAA MMEL,

c) No change from FAA MMEL, and

d) No change from FAA MMEL.

NOTE: Unit Load Devices (ULDs) may be carried provided no cargo is carried on or in these devices. For ballast purposes, use of bags (made of glass fibre or Kevlar) of sand or ingots of non-magnetic metals (such as lead) is acceptable.

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TRANSPORT CANADA Master Minimum Equipment List

Supplement

Aircraft:

BOEING 737-8

Revision No. Original Page:

Date: 07 JUN 2017 21-9

System & 1. 2. Number Installed

Sequence 3. Number Required for Dispatch

Numbers 4. Remarks or Exceptions

21 AIR CONDITIONING

51-01 Air Conditioning Packs

51-01A C 2 1 (O) No change from FAA MMEL.

51-01B C 2 0 (M)(O) Except for ER operations, both may be inoperative provided:

a) Flight is conducted in an unpressurized configuration at or below 10,000 ft MSL,

b) No change from FAA MMEL,

c) No change from FAA MMEL, and

d) No change from FAA MMEL.

NOTE: Unit Load Devices (ULDs) may be carried provided no cargo is carried on or in these devices. For ballast purposes, use of bags (made of glass fibre or Kevlar) of sand or ingots of non-magnetic metals (such as lead) is acceptable.

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TRANSPORT CANADA Master Minimum Equipment List

Supplement

Aircraft:

BOEING 737-8

Revision No. 08 Page:

Date: 24 SEP 2020 22-1

System & 1. 2. Number Installed

Sequence 3. Number Required for Dispatch

Numbers 4. Remarks or Exceptions

22 AUTOFLIGHT

10-02 Autopilot Disengage Aural Warning System

Deleted in FAA MMEL Rev 2.

11-01 Speed Trim Function - 2 2 Must be operative.

11-02 SPEED TRIM FAIL Light - 1 1 Must be operative.

11-10 Control Wheel Autopilot

Disengage Switches

11-10A C 2 1 (O) One may be inoperative provided:

a) Mode Control Panel autopilot DISENGAGE bar is verified to operate normally by conducting the following prior to each flight:

1) Engage either autopilot.

2) Disengage the autopilot using the autopilot DISENGAGE bar.

3) Verify that the autopilot (A/P) disengage lights flash red and that the A/P disengage warning tone sounds.

b) Autopilot is not used below 1,500 feet AGL,

c) Approach minimums do not require the use of the autopilot, and

d) The pilot flying has the operative disconnect.

11-10B Deleted in FAA MMEL Rev 2.

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TRANSPORT CANADA Master Minimum Equipment List

Supplement

Aircraft:

BOEING 737-8

Revision No. 08 Page:

Date: 24 SEP 2020 22-2

System & 1. 2. Number Installed

Sequence 3. Number Required for Dispatch

Numbers 4. Remarks or Exceptions

22 AUTOFLIGHT

21-01 Mach Trim Systems

21-01A C 2 1 (M) No change from FAA MMEL.

21-01B C 2 0 (M)(O) May be inoperative provided:

a) Mach trim actuator is verified to be in null/uncommanded elevator position,

b) Appropriate performance adjustments are applied, and

c) Do not exceed 280 KIAS/ .82M.

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TRANSPORT CANADA Master Minimum Equipment List

Supplement

Aircraft:

BOEING 737-8

Revision No. Original Page:

Date: 07 JUN 2017 23-1

System & 1. 2. Number Installed

Sequence 3. Number Required for Dispatch

Numbers 4. Remarks or Exceptions

23 COMMUNICATIONS

11-01 High Frequency (HF) *** Communication System

11-01A D - 0 Any in excess of those required by regulations may be inoperative.

11-01B C 2 1 (O) No change from FAA MMEL.

NOTE: SATCOM is to be used only as a backup to normal HF communications unless otherwise authorized by the appropriate ATS authorities.

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TRANSPORT CANADA Master Minimum Equipment List

Supplement

Aircraft:

BOEING 737-8

Revision No. Original Page:

Date: 07 JUN 2017 23-2

System & 1. 2. Number Installed

Sequence 3. Number Required for Dispatch

Numbers 4. Remarks or Exceptions

23 COMMUNICATIONS

24-01 Fixed Emergency Locator Transmitter (ELT)

24-01A A - - (M) As required by regulations.

24-01B D - - Any in excess of those required by regulations may be inoperative or missing.

24-01C Not applicable.

24-01D Not applicable.

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TRANSPORT CANADA Master Minimum Equipment List

Supplement

Aircraft:

BOEING 737-8

Revision No. Original Page:

Date: 07 JUN 2017 23-3

System & 1. 2. Number Installed

Sequence 3. Number Required for Dispatch

Numbers 4. Remarks or Exceptions

23 COMMUNICATIONS

31-01 Passenger Address (PA) System

31-01A B 1 0 (O) May be inoperative provided:

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

b) Flight deck/cabin interphone system (two way) with associated calls (e.g. chimes) is verified operative prior to each flight, and

c) Megaphone(s) is/are readily available and operative.

NOTE: Any station function(s) that operates normally may be used.

31-01B C 1 0 (O) May be inoperative provided:

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

b) It is not required by regulations.

NOTE: Any station function(s) that operates normally may be used.

31-01C A 1 0 (O) May be inoperative for non-passenger carrying operations for one flight day provided:

a) Crew members are the only occupants of the aircraft, and

b) Alternate procedures are established and used.

31-01-01 Lavatory Speakers C - 0 (O) No change from FAA MMEL.

31-01-02 Cabin Speakers C - - No change from FAA MMEL.

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TRANSPORT CANADA Master Minimum Equipment List

Supplement

Aircraft:

BOEING 737-8

Revision No. Original Page:

Date: 07 JUN 2017 23-4

System & 1. 2. Number Installed

Sequence 3. Number Required for Dispatch

Numbers 4. Remarks or Exceptions

23 COMMUNICATIONS

31-02 Prerecorded Passenger *** Announcement System

31-02A C 1 0 (O) No change from FAA MMEL.

31-02B Not applicable.

42-01 Service (Cabin) Interphone

System

42-01-01 Flight Deck to Cabin, Cabin to Flight Deck Functions

42-01-01A B - 1 (O) May be inoperative provided:

a) An operative flight deck/cabin interphone system (two way) is at an operative flight attendant seat,

b) The passenger address system is verified operative prior to each flight, and

c) Alternate communications procedures are established and used.

NOTE: No change from FAA MMEL.

42-01-01B A 1 0 (O) May be inoperative for non-passenger carrying operations for one flight day provided:

a) Crew members are the only occupants of the aircraft, and

b) Alternate procedures are established and used.

NOTE: No change from FAA MMEL.

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TRANSPORT CANADA Master Minimum Equipment List

Supplement

Aircraft:

BOEING 737-8

Revision No. Original Page:

Date: 07 JUN 2017 23-5

System & 1. 2. Number Installed

Sequence 3. Number Required for Dispatch

Numbers 4. Remarks or Exceptions

23 COMMUNICATIONS

42-01 Service (Cabin) Interphone System (cont’d)

42-01-02 Cabin to Cabin Functions

42-01-02A B - 1 (O) May be inoperative provided:

a) An operative flight deck/cabin interphone system (two way) is at an operative flight attendant seat,

b) The passenger address system is verified operative prior to each flight, and

c) Alternate communications procedures are established and used.

NOTE: Any station function(s) that operates normally may be used.

42-01-02B A - 0 (O) May be inoperative for non-passenger carrying operations for one flight day provided:

a) Crew members are the only occupants of the aircraft, and

b) Alternate procedures are established and used.

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TRANSPORT CANADA Master Minimum Equipment List

Supplement

Aircraft:

BOEING 737-8

Revision No. 08 Page:

Date: 24 SEP 2020 23-6

System & 1. 2. Number Installed

Sequence 3. Number Required for Dispatch

Numbers 4. Remarks or Exceptions

23 COMMUNICATIONS

42-02 Interphone Handset System

42-02-01 Flight Deck ***

No change from FAA MMEL.

42-02-02 Cabin B - - (O) May be inoperative provided:

a) Fifty percent of cabin handsets operate normally,

b) Operative handset(s) is located at an operative flight attendant seat, and

c) Alternate communication procedures between the affected flight attendant station(s) are established and used.

NOTES: No change from FAA MMEL.

42-02-03 ePhone Cordless *** Handset System

D 1 0 (M)(O) May be inoperative provided:

a) System is deactivated,

b) Alternate procedures are established and used, and

c) ePhone Cordless Handset and associated circuit breakers are placarded “INOPERATIVE”.

42-03 Call System (Audio / Visual Alerting)

42-03-01 Flight Deck Call Visual Alerting System

B 1 0 No change from FAA MMEL.

42-03-02 Flight Deck Call Audio Alerting System

B 1 0 No change from FAA MMEL.

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TRANSPORT CANADA Master Minimum Equipment List

Supplement

Aircraft:

BOEING 737-8

Revision No. Original Page:

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Numbers 4. Remarks or Exceptions

23 COMMUNICATIONS

42-03 Call System (Audio / Visual Alerting) (cont’d)

42-03-03 Flight Attendant Visual Alerting System

B 1 0 (O) No change from FAA MMEL.

42-03-04 Flight Attendant Audio Alerting System

B 1 0 (O) No change from FAA MMEL.

51-02 Audio Control Panels (ACPs)

51-02-01 First Officer A 2 1 (O) First officer’s audio control panel may be inoperative provided:

a) Observer’s audio control panel operates normally,

b) OBS AUDIO selector operates normally,

c) Observer’s seat is not required to be occupied by a person in an official capacity, and

d) Repairs are made within two flight days.

NOTE: Any function that operates normally may be used.

51-02-02 Observer B 1 0 May be inoperative except when required by a person in an official capacity.

51-02-03 Switch Lights C - 0

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25 EQUIPMENT/

FURNISHINGS

00-01 Passenger Convenience / *** Non-Essential Equipment

and Furnishings (NEF)

NOTE 1: Operators are to select either Passenger Convenience Items or NEF (Non-Essential Equipment and Furnishings) in their MELs.

NOTE 2: For operators with NEF defect rectification and control procedures, refer to sub-item 00-01-02 (NEF) only.

00-01-01 Passenger Convenience Items

- 0 Passenger convenience items as expressed in this MMEL are those related to passenger convenience, comfort or entertainment, such as, but not limited to – galley equipment, movie equipment, ashtrays, stereo equipment, and overhead reading lamps. Items addressed elsewhere in this document shall not be included.

(M) and (O) procedures may be required and included in the MEL.

NOTE 1: Exterior lavatory door ashtrays are not considered convenience items.

NOTE 2: Galley equipment restraining devices such as latches, etc. must be serviceable or the compartment must not be used for storage and placarded “INOPERATIVE - DO NOT USE”.

NOTE 3: Movie equipment individual screens, if applicable, must be capable of being stowed.

NOTE 4: Audio or audio-visual entertainment equipment which is used as the sole means of providing safety briefings and demonstrations is not considered a passenger convenience item.

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00-01-02 Non-Essential Equipment & Furnishings (NEF)

- 0 May be inoperative, damaged or missing provided that the item(s) is deferred in accordance with the operator's defect rectification and control procedures. The NEF policies are outlined in the operator's Maintenance Control 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 ashtrays are not considered NEF items.

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11-02 Observer Seats

11-02-01 First Observer Seat (Including Associated Equipment)

11-02-01A B 1 0 (M) May be inoperative except when required by a person in an official capacity provided the seat is removed, stowed or secured in the retracted position.

11-02-01B D 1 0 (M) May be inoperative provided:

a) The seat is not required to be occupied in an official capacity for extended periods of time, and

b) The seat is removed, stowed or secured in the retracted position.

11-02-01C Not Applicable.

11-02-02 Second Observer Seat *** (Including Associated

Equipment)

D 1 0 May be inoperative provided procedures do not require its use.

NOTE: No change from FAA MMEL.

11-02-03 Crotch Straps

Deleted.

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22-01 Passenger Seats (Includes STC SA19-27)

D - - No change from MMEL.

NOTE 1: No change from FAA MMEL.

NOTE 2: Deleted.

NOTE 3: No change from FAA MMEL.

22-01-01 Recline Mechanism No change from FAA MMEL.

22-01-02 Underseat Baggage Restraining Bars

C - - (O) No change from FAA MMEL.

22-01-03 Armrests No change from FAA MMEL.

22-01-04 Seat Belt Air Bag *** Restraint Systems

No change from FAA MMEL.

22-01-05 Headrests *** (STC SA19-27)

D - - (M) May be inoperative and seat occupied provided affected headrest(s) is/are secured in the normal position.

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25-01 Flight Attendant Seat Assembly (Single or Dual Position)

25-01-01 Required Flight Attendant Seats

25-01-01A B - 1 (M)(O) No change from FAA MMEL.

NOTE 1: An automatic folding seat (which does not have a secondary stowing / locking mechanism) that will not stow automatically is considered inoperative.

NOTE 2: A seat position with a missing or inoperative required component, such as safety belt (including shoulder harness) or headrest renders the seat position inoperative.

25-01-01B Not applicable.

25-01-02 Excess Flight Attendant Seats

D - - (M) Seats / assemblies in excess of requirements and not assigned to a flight attendant may be inoperative provided they are not occupied, are placarded and are:

a) Properly stowed,

b) Secured in the retracted position, or

c) Removed.

40-01 Exterior Lavatory Door

Ashtrays Deleted. Refer to FAA MMEL.

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64-01 Megaphones

64-01A D - - (M)(O) Any in excess of those required by regulations may be inoperative or missing provided:

a) Inoperative megaphone is removed from the passenger cabin and its location is placarded INOPERATIVE, or it is removed from the installed location, secured out of sight and the megaphone and its installed location are placarded INOPERATIVE,

b) Required distribution is maintained, and

c) Procedures are established and used to alert crew members of inoperative or missing megaphones.

64-01B D - 0 May be inoperative provided all crew members are on the flight deck.

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64-03 Emergency Medical Equipment

64-03-01 First Aid Kit (FAK) and/or Associated Equipment

D - - (O) Any kit or items contained in the kit in excess of those required by regulations may be incomplete or missing provided:

a) Required distribution is maintained,

b) Procedures are established and used to alert crew members of missing or incomplete kits.

64-03-01-01 First Aid Kit Seal (Required First Aid Kits)

A - - (O) The seal affixed on the exterior of any required first aid kit may be missing or broken for three flight days provided:

a) First aid kit is fully equipped or the kit has a maximum of one missing item,

b) Kit includes a list of its contents,

c) An inventory is taken on the contents of the kit prior to departure, and

d) Procedures are established and used to alert crew members of:

1) The missing or broken seal,

2) The need to perform an inventory under proviso c).

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64-03 Emergency Medical Equipment (cont’d)

64-03-02 Emergency Medical Kit (EMK) and/or Associated Equipment

64-03-02A A - 0 (O) May be incomplete or missing provided:

a) The kit is sealed in a manner that will identify it as a unit that cannot be mistaken for a fully serviceable unit, and

b) Replacements are made within one flight.

64-03-02B D - - (O) Any kit or items contained in the kit in excess of those required by regulations may be incomplete or missing provided procedures are established and used to alert crew members of missing or incomplete kits.

64-03-02-01 Emergency Medical Kit Seal

B - - (O) The seal affixed on the exterior of the emergency medical kit may be missing or broken provided:

a) The emergency medical kit is fully equipped,

b) The kit includes a list of its contents,

c) An inventory is taken on the contents of the kit prior to departure,

d) Procedures are established and used to alert crew members of:

1) The missing or broken seal, and

2) The need to perform an inventory under proviso c).

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64-03 Emergency Medical Equipment (cont’d)

64-03-03 Automatic External Defibrillators (AED) and/or Associated Equipment

D - 0

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26 FIRE PROTECTION NOTE: The following NOTE replaces the

NOTE found in MMEL items that contain a proviso requiring associated cargo compartment to remain empty:

“NOTE: Unit Load Devices (ULDs) may be carried provided no cargo is carried on or in these devices. For ballast purposes, use of bags (made of glass fibre or kevlar) of sand or ingots of non-magnetic metals (such as lead) is acceptable.”

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26 FIRE PROTECTION

14-01 Lavatory Smoke Detection Systems

14-01A C - 0 (M)(O) For each lavatory, the lavatory smoke detection system may be inoperative provided:

a) Lavatory is not used by passengers for any purpose,

b) Lavatory waste receptacle is empty,

c) Lavatory door is locked closed and placarded ”INOPERATIVE - DO NOT ENTER”,

d) Access to waste receptacle from outside the lavatory must be secured closed and placarded “INOPERATIVE - DO NOT USE”,

e) Lavatory is used only by crew members, and

f) In-flight service waste bags are not stored in the lavatory.

NOTE: The above-mentioned provisos are not intended to preclude crew member lavatory inspections, which must be detailed in the (O) procedures.

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26 FIRE PROTECTION

14-01 Lavatory Smoke Detection Systems (cont’d)

14-01B B - 0 (O) For each lavatory, the lavatory smoke detection system may be inoperative for non-passenger carrying operations provided:

a) Crew members are the only occupants of the aircraft, and

b) Occupants have been briefed as to which lavatory fire extinguisher system(s) is inoperative, and

c) In-flight service waste bags are not stored in the lavatory.

NOTE: The above-mentioned provisos are not intended to preclude crew member lavatory inspections, which must be detailed in the (O) procedures.

14-01-01 Lavatory Smoke Detector SELF TEST Switch

C - 0 (M) No change from FAA MMEL.

14-01-02 Flight Deck LAVATORY *** SMOKE Light

14-01-02A C 1 0 (O) No change from FAA MMEL.

14-01-02B D 1 0 No change from FAA MMEL.

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26 FIRE PROTECTION

18-01 Wheel Well Fire Detection System

18-01A Not applicable.

18-01B B 1 0 (M)(O) May be inoperative provided:

a) Brakes are inspected before each flight and are cool to the touch,

b) Landing gear is left extended for a minimum of ten minutes after takeoff,

c) Takeoff performance is in accordance with AFM, and

d) Takeoff is not conducted in icing conditions.

NOTE 1: In case of engine failure after V1, performance is the prime consideration and the landing gear should be retracted normally until performance penalty with gear down is not a problem.

NOTE 2: Pilots must consider the effects associated with delayed raising of landing gear or lowering landing gear during operation from contaminated runways in icing conditions.

18-01-01 Detection Loops C 2 1 (M) No change from FAA MMEL.

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26 FIRE PROTECTION

24-01 Lavatory Fire Extinguisher Systems

24-01A C - 0 No change from FAA MMEL.

24-01B C - 0 (M)(O) For each lavatory, the lavatory fire extinguisher system may be inoperative provided:

a) Lavatory is not used by passengers for any purpose,

b) Lavatory waste receptacle is empty,

c) Lavatory door is locked closed and placarded ”INOPERATIVE - DO NOT ENTER”,

d) (where applicable) Access to waste receptacle must be secured closed and placarded “INOPERATIVE - DO NOT USE”, and

e) Lavatory is used only by crew members.

24-01C B - 0 (O) May be inoperative for non-passenger carrying operations provided:

a) Crew members are the only occupants of the aircraft, and

b) Occupants have been briefed as to which lavatory fire extinguisher system(s) is inoperative.

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26 FIRE PROTECTION

26-01 Portable Fire Extinguishers D - - (M)(O) Any in excess of those required by regulations may be inoperative or missing provided:

a) Inoperative fire extinguisher(s) is removed from the passenger cabin or flight deck and its location is placarded INOPERATIVE, or it is removed from the installed location, secured out of sight and the fire extinguisher and its installed location are placarded INOPERATIVE,

b) Required distribution is maintained in the passenger compartment and the flight deck, and

c) Procedures are established and used to alert crew members of missing portable fire extinguishers.

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27 FLIGHT CONTROLS

08-01 Control Surface Position *** Indication System

C 1 0 (M)(O) May be inoperative provided:

a) Affected control surface(s) is visually checked for full, free and correct movement before each flight, and

b) A placard identifying the inoperative indicator must be affixed to the instrument panel adjacent to the applicable display.

41-01 Control Wheel Trim Switch

Systems - 2 2 Must be operative.

51-01 Flap Load Relief Function C 1 0 (O) May be inoperative provided:

a) Appropriate performance adjustments are applied,

b) For takeoff when using Flaps 25, gross weight may not exceed 177,300 lb (80,422 kg),

c) For takeoff when using Flaps 15, gross weight may not exceed 176,300 lb (79,968 kg),

d) For takeoff when using Flaps 10, gross weight may not exceed 173,900 lb (78,879 kg),

e) For landing when using Flaps 40, gross weight may not exceed 100,000 lb (45,359 kg),

f) For landing when using Flaps 30, gross weight may not exceed 104,000 lb (47,174 kg), and

g) For landing when using Flaps 15, gross weight may not exceed 136,700 lb (62,006 kg).

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27 FLIGHT CONTROLS

61-02 Maneuver Load Alleviation (MLA) Function

C 1 0 (O) May be inoperative provided maximum takeoff weight limitation is 105,000 lb (47,627 kg).

62-01 Auto Speedbrake System C 1 0 (M)(O) May be inoperative provided:

a) Auto speedbrake system is deactivated,

b) Appropriate performance adjustments are applied, and

c) Placard “AUTO BRAKE INOP” adjacent to the AUTO BRAKE switch.

62-02 SPEEDBRAKES EXTENDED

Light B 1 0 (M) No change from FAA MMEL.

90-01 Rudder Pedal Adjustment C 1 0 (M) May be inoperative provided:

a) Rudder pedals can be secured in a position which meets individual pilot requirements, and

b) Full and unrestricted movement of the rudder and brake pedal deflection is possible at both pilot stations.

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30 ICE AND RAIN

PROTECTION

21-02 Engine Anti-Ice COWL VALVE Position Lights and TAI Indications

21-02A Not applicable.

21-02B C 4 2 No change from FAA MMEL.

21-02C C 4 2 No change from FAA MMEL.

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31 INDICATING/RECORDING

SYSTEMS

25-01 Clock Switches C 2 0 Aircraft clocks may be inoperative provided a reliable and functioning timepiece is readily available to all flight deck crew members.

31-01 Flight Data Recorder System

(FDR)

31-01A Not applicable.

31-01B A - 0 May be inoperative provided:

a) At least one Cockpit Voice Recorder (CVR) function is operative, and

b) Repairs are made within three flight days.

31-01-01 FDR Recording Parameters required by regulations

A - - Up to three recording parameters may be inoperative provided:

a) At least one Cockpit Voice Recorder (CVR) function is operative, and

b) Repairs are made within 20 calendar days.

31-01-02 FDR Recording Parameters not required by regulations

A - - No change from FAA MMEL.

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31 INDICATING/RECORDING

SYSTEMS

62-01 MAX Display System (MDS)

62-01-01 Display Units (DU)

62-01-01-01 Outboard DU 2 2 Must be operative.

62-01-01-02 Inboard DU A 2 1 (M)(O) May be inoperative provided:

a) Associated PFD/MFD display selector switch remains in the OUTBD position.

b) Opposite PFD/MFD display selector switch is verified to operate normally.

c) Captain’s and First Officer’s engine display control selectors operate normally.

d) Engine display is available and selected on opposite inboard display.

e) ISFD operates normally.

f) EFIS Control Panels operate normally.

g) Outboard display units operate normally.

h) Repairs are made within one flight day.

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32 LANDING GEAR

30-01 Landing Gear Actuation System

B 1 0 (M)(O) May be inoperative provided:

a) Landing gear is secured in down position,

b) Airplane is dispatched in accordance with AFM Landing Gear Extended appendix, and

c) Airplane remains at or below FL380.

31-02 Landing Gear Control

Systems

31-02A C 2 1

31-02B B 2 0 (M)(O) May be inoperative provided:

a) Landing gear is secured in down position,

b) Airplane is dispatched in accordance with AFM Landing Gear Extended appendix, and

c) Airplane remains at or below FL380.

35-01 Landing Gear Manual

Extension System B 1 0 (M)(O) May be inoperative provided:

a) Landing gear is secured in down position,

b) Airplane is dispatched in accordance with AFM Landing Gear Extended appendix, and

c) Airplane remains at or below FL380.

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32 LANDING GEAR

42-01 Antiskid System C 1 0 (M)(O) May be inoperative provided:

a) Inoperative antiskid channels are deactivated,

b) Autobrake system is not used,

c) Appropriate performance adjustments for antiskid inoperative are applied, and

d) Crew members are the only occupants of the aircraft.

44-01 Parking Brake Valve C 1 0 (M)(O) May be inoperative provided:

a) Parking brake valve is deactivated in closed position,

b) Antiskid system is considered inoperative,

c) Autobrake system is not used,

d) Appropriate performance adjustments for antiskid inoperative are applied, and

e) Crew members are the only occupants of the aircraft.

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33 LIGHTS

11-01 Flight Compartment and Instrument Lighting System

11-01A C - - No change from FAA MMEL.

11-01B D - 0 May be inoperative for day operations.

24-01 Passenger Lighted

Information Signs and Notice System

24-01-01 Individual Passenger Lighted Information Signs

24-01-01A C - - (M) Passenger seats, cabin attendant seats or lavatories from which a light is not readily legible, may not be occupied and must be blocked and placarded “DO NOT OCCUPY”.

24-01-01B C - - (O) Affected seats or lavatories may be occupied provided:

a) PA system and crew call/cabin interphone system including associated chimes operate normally, and

b) Procedures are established and used to alert cabin attendants and notify passengers when seat belts should be fastened, return to seat is requested and smoking prohibited.

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Aircraft:

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Revision No. Original Page:

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System & 1. 2. Number Installed

Sequence 3. Number Required for Dispatch

Numbers 4. Remarks or Exceptions

33 LIGHTS

24-01 Passenger Lighted Information Signs and Notice System (cont’d)

24-01-01 Individual Passenger Lighted Information Signs (cont’d)

24-01-01C A - 0 (O) May be inoperative for non-passenger carrying operations provided:

a) Crew members are the only occupants of the aircraft,

b) Alternate procedures are established and used, and

c) Repairs are made within one flight day.

24-01-02 Aural Tone System C 1 0 (O) May be inoperative provided alternate procedures are established and used.

24-01-03 Flight Deck Automatic Function

C 1 0 (O) No change from FAA MMEL.

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Aircraft:

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Revision No. Original Page:

Date: 07 JUN 2017 33-3

System & 1. 2. Number Installed

Sequence 3. Number Required for Dispatch

Numbers 4. Remarks or Exceptions

33 LIGHTS

41-01 Wing Illumination Lights

41-01A C 2 0 (O) No change from FAA MMEL.

41-01B C 2 0 One or both may be inoperative for day operations.

51-02 Exterior Emergency Lighting

System

51-02A C 1 0 May be inoperative for day operations.

51-02B A 1 0 (O) May be inoperative for one flight day provided:

a) Aircraft crew members are the only occupants of the aircraft, and

b) Alternate procedures are established and used.

NOTE 1: For the purposes of this item, “aircraft crew” means the operating crew members including flight crew members, flight attendants, aircraft maintenance personnel and supervisory crew members.

NOTE 2: The operator’s MEL must state the maximum number of aircraft crew permitted.

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Aircraft:

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Revision No. 02 Page:

Date: 23 MAR 2018 34-1

System & 1. 2. Number Installed

Sequence 3. Number Required for Dispatch

Numbers 4. Remarks or Exceptions

34 NAVIGATION

23-01 Standby Magnetic Compass B 1 0 May be inoperative provided:

a) Integrated standby flight display (ISFD) heading display operates normally, and

b) Airplane is operated:

1) With Dual Independent Navigation Capability, and

2) Under Positive Radar Control by ATC during the en-route flight phase, or one of the navigation systems is a TSO’d GPS which provides track information.

24-01 Integrated Standby Flight

Display (ISFD)

24-01-01 Attitude Indication B 1 0 May be inoperative provided:

a) Operations are conducted in Day VMC only,

b) Operations are not conducted into known or forecast over-the-top conditions, and

c) It is clearly identified to the flight crew as inoperative.

24-01-02 to 24-01-05 No change from FAA MMEL.

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Revision No. 08 Page:

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System & 1. 2. Number Installed

Sequence 3. Number Required for Dispatch

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34 NAVIGATION

36-01 Head-Up Display (HUD) *** System (Includes STC ST02522SE)

- 0 No change from FAA MMEL.

49-01 Ground Proximity Warning

System (GPWS)

49-01-01 GPWS Function A 1 0 (O) May be inoperative provided:

a) Alternate procedures are established and used.

b) Repairs are made within three flight days.

49-01-01-01 Modes 1 - 4 A 4 0 (O) May be inoperative provided:

a) Alternate procedures are established and used.

b) Repairs are made within three flight days.

49-01-01-02 Excessive Deviation Below Glide Slope (Mode 5)

B 1 0

49-01-01-03 Advisory Altitude/Bank Angle Callout (Mode 6)

C 1 0 (O) May be inoperative provided alternate procedures are established and used.

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Aircraft:

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Revision No. 08 Page:

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34 NAVIGATION

49-01 Ground Proximity Warning System (GPWS) (cont’d)

49-01-01 GPWS Function (cont’d)

49-01-01-04 Reactive Windshear (RWS) Detection (Mode 7)

49-01-01-04A B 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.

49-01-01-04B C 1 0 (O) May be inoperative provided:

a) Alternate procedures are established and used, and

b) Windshear Detection and Avoidance System (Predictive) operates normally.

49-01-01-05 Test Mode A 1 0 May be inoperative provided:

a) GPWS is considered inoperative.

b) Repairs are made within three flight days.

49-01-02 Terrain Awareness Function

B 1 0 (O) No change from FAA MMEL.

49-01-03 Terrain Displays No change from FAA MMEL.

49-01-04 Runway Awareness and *** Advisory System (RAAS)

C 1 0

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Aircraft:

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Revision No. 02 Page:

Date: 23 MAR 2018 34-4

System & 1. 2. Number Installed

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34 NAVIGATION

51-01 VOR Systems Deleted from TCS. Refer to FAA MMEL.

53-01 ATC Transponder/Automatic

Altitude Reporting Systems

53-01A D 2 1 No change from FAA MMEL.

53-01B B 2 0 No change from FAA MMEL.

53-01-01 Elementary and Enhanced Downlink Aircraft Reportable Parameters Not Required by Regulations

A - 0 No change from FAA MMEL.

53-01-02 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.

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Revision No. Original Page:

Date: 07 JUN 2017 34-5

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34 NAVIGATION

61-01 Flight Management Computer System (FMCS)

61-01-01 Computer C - 0 (M) No change from FAA MMEL.

61-01-02 Navigation Databases C - 0 (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,

c) Approach navigation radios are manually tuned and identified, and

d) Approaches are not conducted using associated system.

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Aircraft:

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Revision No. Original Page:

Date: 07 JUN 2017 35-1

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Sequence 3. Number Required for Dispatch

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35 OXYGEN

21-01 Passenger Oxygen System

21-01A B 1 0 (O) May be inoperative provided:

a) Both air conditioning packs operate normally,

b) Pressurization system operates normally,

c) Flight is not conducted where minimum enroute altitude is above 13,000 ft MSL,

d) Airplane remains at or below FL 250,

e) Portable oxygen units are provided for all crew members and 10% of the passengers for half an hour (supplemental oxygen), and

f) Passengers are appropriately briefed.

21-01B B 1 0 May be inoperative provided flight is conducted at or below 10,000 feet MSL.

21-01C C 1 0 May be inoperative for non-passenger carrying operations provided portable oxygen bottles are available for all crew members required to be off the flight deck.

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Revision No. Original Page:

Date: 07 JUN 2017 35-2

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35 OXYGEN

21-02 Oxygen Service Units (Passenger, Attendant, Lavatory)

B - - (M) May be inoperative provided:

a) Associated seats are blocked and placarded to prevent occupancy,

b) Associated flight attendant seat is considered inoperative,

c) Associated lavatory door is locked closed and placarded INOPERATIVE – DO NOT ENTER, and

d) No more than two consecutive banks of seats and their adjacent banks of seats have missing or inoperative Oxygen Service Units.

21-02-01 Automatic Presentation System

B 1 0 (M)(O) No change from FAA MMEL.

21-02-02 Door Latches B - - (M)(O) May be inoperative provided:

a) Associated oxygen service unit operates normally,

b) Flight remains at or below FL 300,

c) Alternate deployment system is operative, and

d) No more than two consecutive banks of seats and their adjacent banks of seats have an inoperative automatic opening feature.

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Revision No. Original Page:

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35 OXYGEN

31-01 Portable Oxygen Dispensing Units (Bottle and Mask)

D - - (M)(O) Any in excess of those required by regulations may be inoperative or missing provided:

a) Required distribution of operative units is maintained throughout the aircraft,

b) Inoperative portable oxygen dispensing unit is removed from the passenger cabin and its location is placarded INOPERATIVE, or it is removed from the installed location, secured out of sight and the portable oxygen dispensing unit and its installed location are placarded INOPERATIVE, and

c) Procedures are established and used to alert crew members of inoperative or missing equipment.

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Revision No. Original Page:

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35 OXYGEN

31-02 Protective Breathing Equipment (PBE)

D - - (M)(O) Any in excess of those required by regulations may be inoperative or missing provided:

a) Required distribution of operative units is maintained throughout the aircraft,

b) Inoperative protective breathing equipment unit is removed from the passenger cabin and its location is placarded INOPERATIVE, or it is removed from the installed location, secured out of sight and the protective breathing equipment unit and its installed location are placarded INOPERATIVE, and

c) Procedures are established and used to alert crew members of inoperative or missing equipment.

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Aircraft:

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Revision No. Original Page:

Date: 07 JUN 2017 38-1

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38 WATER/WASTE

10-01 Potable Water System

10-01A C - - (M) No change from FAA MMEL.

10-01B C 1 0 (M)(O) System may be inoperative provided:

a) Tank is drained and inspected to ensure no leakage, and

b) Procedures are established to deactivate applicable system components to prevent its use or servicing.

NOTE 1: The (O) procedure addresses other means for water provision for crew members as well as the need to advise of system status during crew changes.

NOTE 2: Aviation Occupational Health & Safety (AOH&S) requirements should be addressed.

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Revision No. Original Page:

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38 WATER/WASTE

30-01 Lavatory Waste System

30-01A C - - (M) No change from FAA MMEL.

30-01B C - 1 (M) May be inoperative provided:

a) Waste is drained and system is inspected for leakage,

b) Procedures are established to deactivate system components,

c) Lavatory door is locked closed and placarded “INOPERATIVE - DO NOT ENTER”, and

d) There is at least one serviceable lavatory on the aircraft.

NOTE: Aviation Occupational Health & Safety (AOH&S) requirements should be addressed.

30-01-01 Vacuum Blower C 1 0 (M)(O) No change from FAA MMEL.

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Aircraft:

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Revision No. 05 Page:

Date: 15 JUN 2018 49-1

System & 1. 2. Number Installed

Sequence 3. Number Required for Dispatch

Numbers 4. Remarks or Exceptions

49 AIRBORNE AUXILIARY

POWER

11-01 Auxiliary Power Unit C 1 0 (M) Except for ER operations, may be inoperative provided:

a) Both engine driven generator systems operate normally,

b) At least one engine bleed air shutoff valve (PRSOV) operates normally, and

c) FSOV is verified to be closed.

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Aircraft:

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Revision No. Original Page:

Date: 07 JUN 2017 50-1

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50 CARGO AND ACCESSORY

COMPARTMENTS

10-01 Lower Cargo Compartment Lining Panels and Floor Panels

C - - (O) No change from FAA MMEL.

NOTE: Unit Load Devices (ULDs) may be carried provided no cargo is carried on or in these devices. For ballast purposes, use of bags (made of glass fibre or Kevlar) of sand or ingots of non-magnetic metals (such as lead) is acceptable.

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Revision No. Original Page:

Date: 07 JUN 2017 52-1

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52 DOORS

31-01 Lower Cargo Doors Pressure Stop Fittings

31-01-01 Pressurized Flight A 24 22 (M) No change from FAA MMEL.

31-01-02 Unpressurized Flight C 24 20 (M)(O) May be inoperative:

a) Flight is conducted in an unpressurized configuration at or below 10,000 ft MSL,

b) No change from FAA MMEL, and

c) No change from FAA MMEL.

NOTE: Unit Load Devices (ULDs) may be carried provided no cargo is carried on or in these devices. For ballast purposes, use of bags (made of glass fibre or Kevlar) of sand or ingots of non-magnetic metals (such as lead) is acceptable.

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Revision No. Original Page:

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52 DOORS

90-01 Main Cabin Exit / Slide A - - (M)(O) One cabin door/slide or one emergency exit/slide may be inoperative provided:

a) Only aircraft crew are carried,

b) Affected emergency exit is verified closed, latched and locked before each flight,

c) Aircraft crew are advised of the nature (emergency exit and slide availability) and extend of the unserviceability and that evacuation procedures do not include affected exit, though opposite exit may be used,

d) Conspicuous sign or placard, indicating that exit is inoperative, is attached to exit,

e) Emergency exit signs and lights associated only with inoperative exit are obscured (NOTE 3), and

f) Repairs are made within three flight days.

NOTE 1: For the purpose of this item only, “aircraft crew” means operating crew members including flight crew members, flight attendants, aircraft maintenance personnel and supervisory crew members.

NOTE 2: Operator’s MEL must state the maximum number of aircraft crew permitted.

NOTE 3: Exit locator signs and emergency aisle path markings which are shared between two exits must not be obscured.

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Revision No. Original Page:

Date: 07 JUN 2017 73-1

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73 ENGINE AND FUEL

CONTROL

31-01 Fuel Flow Indications C 2 1 Except for ER operations, may be inoperative provided flight deck fuel quantity indicating systems operate normally.

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Revision No. 02 Page:

Date: 23 MAR 2018 75-1

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Numbers 4. Remarks or Exceptions

75 BLEED AIR

23-01 EEC Cooling Systems C 2 1 (M)(O) May be inoperative provided:

a) Associated fans are deactivated off, and

b) OAT is below 50 degrees C for takeoff and landing.

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Revision No. 04 Page:

Date: 11 MAY 2018 77-1

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Numbers 4. Remarks or Exceptions

77 ENGINE INDICATING

31-01 Engine Vibration Indications

31-01A Non-ETOPS C 2 1 (M) May be inoperative provided an approved maintenance reliability program (which included engine vibration monitoring) is in place.

31-01B ETOPS A 2 1 (M) May be inoperative for one flight day provided an approved maintenance reliability program (which includes engine vibration monitoring) is in place.