BOMBARDIER BUSINESS JET

M A S T E R M I N I M U M E Q U I P M E N T L I S T

BD-100-1A10

TRANSMITTAL LETTER

This letter presents Revision 6 of the Challenger 300 Master Minimum Equipment List, dated 5-May-2022.

This revision introduces the fourth issue of the Challenger 300 Master Minimum Equipment List.

The associated Challenger 300 Dispatch Deviation Guide (DDG) will be issued to support this MMEL. The DDG is

to be issued within 30 days after approval.

TRANSPORT CANADA

MASTER MINIMUM EQUIPMENT LIST

Bombardier Business Jet

BD-100-1A10

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

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de révision:

Original Page

BD-100-1A10 Date: Sep 30/03 TOC-1

TABLE OF CONTENTS

Subject Chapter/Page

TITLE PAGE

TABLE OF CONTENTS TOC-1

MANUAL APPROVAL PAGE

RECORD OF REVISIONS REV-1

RECORD OF TEMPORARY REVISIONS TPR-1

USER COMMENTS

LIST OF EFFECTIVE PAGES LEP-1

HIGHLIGHTS OF CHANGE HOC-1

DEFINITIONS DEF-1

ABBREVIATIONS and ACRONYMS ABB-1

PREAMBLE PRE-1

EQUIPMENT LIST

Air Conditioning 21-1

Auto Flight 22-1

Communications 23-1

Electrical Power 24-1

Equipment/Furnishings 25-1

Fire Protection 26-1

Flight Controls

27-1

Fuel 28-1

Hydraulic Power 29-1

Ice and Rain Protection 30-1

Indicating/Recording Systems 31-1

Landing Gear 32-1

Lights 33-1

Navigation 34-1

Oxygen

35-1

Pneumatics 36-1

(cont’d)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

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de révision:

3 Page

BD-100-1A10 Date: Jun 21/11 TOC-2

TABLE OF CONTENTS (cont’d)

Subject Chapter/Page

EQUIPMENT LIST (cont’d)

Central Maintenance System 45-1

Information Systems 46-1

Auxiliary Power Unit 49-1

Doors 52-1

Engine Fuel and Control 73-1

Ignition 74-1

Engine Controls 76-1

Engine Indicating 77-1

Exhaust 78-1

Oil 79-1

Starting 80-1

May 5, 2022

4DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

2 Page

BD-100-1A10 Date: Oct 28/08 REV-1

RECORD OF REVISIONS

Retain this index in the front of the manual. When Revisions are received and inserted, enter the relevant

information in the columns below.

Revision # Pages Affected By

Original All

Rev. 1 Manual Approval, REV-1, LEP-1, LEP-2, LEP-3, HOC-1,

HOC-2, HOC-3, HOC-4, HOC-6

21-1, 21-2, 21-3, 21-4, 21-5, 21-6, 21-7, 21-8, 21-9, 21-10, 21-

11

22-1, 22-2

23-1, 23-2, 23-3

24-1,24-2, 24-3

25,1, 25-2, 25-3, 25-4, 25-5, 25-6, 25-7, 25-8

27-1, 27-2

29-1

30-4, 30-5, 30-6, 30-7

31-1, 31-2, 31-3, 31-4

33-1, 33-2, 33-3, 33-4, 33-5

34-1, 34-2, 34-3, 34-4, 34-5

36-1, 36-2, 36-3, 36-4, 36-5,36-6, 36-7, 36-8, 36-9, 36-10,

36-11, 36-12

38-1, 38-2

49-1

52-1, 52-2

Rev. 2 Manual Approval, REV-1, TPR-1, LEP-1, LEP-2, LEP-3, LEP-

4, HOC-1, HOC-2, HOC-3, HOC-4

21-1 THRU 21-18

23-1 THRU 23-6

24-4

25-1 THRU 25-10

29-1

30-3, 30-4, 30-5, 30-6

31-1THRU 31-8

33-3, 33-4, 33-6

34-3, 34-4, 34-5, 34-6

36-1 THRU 36-26

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

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de révision:

4 Page

BD-100-1A10 Date: May 02/18 REV-2

Revision # Pages Affected By

Rev 3 Manual Approval, TOC-2, REV-2, TPR-2, LEP-1, LEP-2, LEP-

3, LEP-4, HOC-1, HOC-2, PRE-2, TITLE-1, TITLE-2

SECTION 1

21-8, 21-14

22-1, 22-2

23-1, 23-2, 23-3, 23-4

26-1

28-1, 28-2, 28-3, 28-4

29-1, 29-2,

32-1

34-2, 34-4, 34-5, 34-6,

46-1, 46-2

49-1

SECTION 2

TITLE-1, TITLE-2, INT-1, INT-2, TOC-1,TOC-2

2-1, 2-2, 2-3

Rev 4

Manual Approval, Rev-3, User Comments, LEP-1, LEP-2,

LEP-3, HOC-1

SECTION 1

21-1, 21-2,

22-2,

23-1, 23-2, 23-3, 23-4, 23-5,

29-1,

30-3, 30-4, 30-5, 30-6, 30-7, 30-8,

31-8,

32-1,

33-4, 33-5, 33-6,

34-1, 34-2, 34-3, 34-4, 34-5, 34-6, 34-7,34-8,

36-5, 36-6, 36-7, 36-8, 36-13, 36-14, 36-15, 36-16, 36-17, 36-

21, 36-22, 36-23, 36-24,

46-1,

49-1,

73-1,

78-1.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

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de révision:

6 Page

BD-100-1A10 Date: May 05/22 REV-3

Rev 5

Manual Approval, Rev-3, TPR-2, TPR-3, User Comments,

LEP-1, LEP-2, LEP-3, HOC-1.

Section 1

24-1,

25-9,

26-1, 26-2

29-1,

32-1,

33-4,

46-1, 46-2

Rev 6

Manual Approval, Rev-3, TPR-4, LEP-1 thru LEP-4, HOC-1,

HOC-2, DEF-2.

Section One

21-4 thru 21-8, 21-10 thru 21-17, 22-2 thru 22-3, 24-1, 25-4

thru 25-7, 25-10, 26-1 thru 26-2, 27-1, 28-1, 28-3, 29-1, 30-1

thru 30-2, 31-2, 31-4 thru 31-5, 31-7 thru 31-8, 32-1 thru 32-2,

34-1, 34-6, 35-1 thru 35-3, 36-1 thru 36-8, 38-1 thru 38-2, 49-

1, 73-1, 74-1, 76-1, 78-1, 79-1, 80-1.

Section Two

TOC-1, 2-1, 2-3.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

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de révision:

2 Page

BD-100-1A10 Date: Oct 28/08 TPR-1

RECORD OF TEMPORARY REVISIONS

Retain this index in the front of the manual. When Temporary Revisions are issued or cancelled, enter the date you

insert each revision in your manual.

Temp

Rev #

Pages

Affected

TC approval Description of Revision Date Incorporated

Signatu

r

e

1

33-3

33-4

TRS No 01 was approved

by Leo Galvin, Acting Chief,

Flight Test for Minister of

Transport, 14 September

2005.

This MMEL TR is based on TCCA

approved TRS No. 01.

TR 1 replaces the terms "Aircraft

without Modsum 100T010143"

and "Aircraft with Modsum

100T010143 with "Aircraft

without Wing Tip Strobe Lights"

and "Aircraft with Wing Tip

Strobe Lights" respectively

Superseded by Rev. 2

Dated 10/28/08

2

29-1

31-2

31-3

TRS No 03 was approved

by B. Jupp, Chief, Flight

Test for Minister of

Transport,13 November

2007 TRS 07, 08 and. 09

were approved by R.

Walker, A/Chief, Flight Test

for Minister of Transport,

21 November 2007.

This MMEL TR is based on TCCA

approved TRS No. 3, No. 07, No.

8, and No. 9. TRS. No. 3 revises

MMEL item 29-12-01.TRS. No. 7

revises MMEL item 31-41-01.

TRS. No. 8 introduces MMEL

item 31-41-02. TRS. No. 9

introduces MMEL item 23-20-

02.

Superseded by Rev. 2

Dated 10/28/08

3

23-1

31-2

31-3

TRS 10 rev – was approved

by R. Walker, A/Chief,

Flight Test for Minister of

Transport, 6 May 2008.

This MMEL TR is based on TCCA

approved TRS No. 10 rev --.

TRS. No. 10 rev. – revises MMEL

items 23-20-02 and 31-41-02.

Superseded by Rev. 2

Dated 10/28/08

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 TPR-2

Temp

Rev #

Pages

Affected

TC approval Description of Revision Date Incorporated

Signat

u

re

4

TPR-1

34-5

34-6

TRS 13 was approved

by R. Walker, A/Chief,

Flight Test for Minister of

Transport,

24 November 2008 and

TRS 16 was approved

by R. Walker, A/Chief,

Flight Test for Minister of

Transport,

09 December 2008.

This MMEL TR is based on

TCCA approved TRS No. 13

and TRS No 16.

TRS. No. 13 revises MMEL

item 34-55-01 and TRS No

16 revises MMEL item 34-61-

01.

Superseded by Rev. 3

Dated 06/21/11

5

TPR-1

28-1

TRS 14 rev. 1 and

TRS 15 were approved

by R. Walker, A/Chief,

Flight Test for Minister of

Transport

18 March 2009.

This MMEL TR is based on

TCCA approved TRS No. 14

rev. 1 and TRS No. 15.

TRS. No. 14 rev. 1 revises

MMEL items 28-21-02.

TRS. No. 15 revises MMEL

items 28-21-03.

Superseded by Rev. 3

Dated 06/21/11

6

33-5

TRS No 17 was

approved by

Walter Istchenko,

Chief, Flight Test for

Minister of Transport,

30 July 2010

This MMEL TR is based on

TCCA approved TRS No. 17.

TRS. No. 17 revises MMEL

item 33-50-02.

Superseded by Rev. 3

Dated 06/21/11

7

TPR-1

34-5

34-6

TRS 18 was approved

by Kevin Horton,

Acting Chief, Flight Test

for Minister of Transport,

14 October 2010.

This MMEL TR is based on

TCCA approved TRS No. 18.

TRS. No. 18 revises MMEL

items 34-55-01 and 34-61-01.

Superseded by Rev. 3

Dated 06/21/11

8

TPR-2

36-17

TRS No. 20,

Walter Istchenko,

Chief Flight Test for

Minister of Transport,

26 April 2013.

This MMEL is based on

TCCA approved TRS No.20

TRS No.20 deletes MMEL

item 36-10-03 XBLEED Valve

(CBV) as it is required to

perform AFM Emergency

Procedures.

Superseded by Rev 4

Dated

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

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de révision:

4 Page

BD-100-1A10 Date: May 02/18 TPR-3

Temp

Re

v #

Pages

Affected

TC approval Description of Revision Date Incorporated

Signature

9

TPR-2

23-1

34-2

34-3

34-5

TRS No. 21,

John Wiseman,

Acting Chief, Flight Test

for Minister of Transport,

07 June 2013.

This MMEL is based on

TCCA approved TRS No.21

that covers CL300 Avionics

Update, that includes (23-20-

01, 34-42-01, 34-43-01, 34-

54-01)

Superseded by Rev 4

10

TPR-2.

34-2.

TRS No 22R1,Walter

Istchenko, Chief Flight

Test for Minister of

Transport, 17 June

2014.

This MMEL is based on the

TCCA approved TRS No.22

that covers a new item 34-34-

01 Synthetic Vision System

(SVS) (including Database) is

introduced.

Superseded by Rev 4

11

TPR-2

30-3

TRS No. 23, Walter

Istchenko, Chief Flight

Test for Minister of

Transport, 17 June

2014.

This MMEL is based on the

TRS No.23 that covers the

introduction of SB 100-34-38

to improve Pitot-Static Probe

reliability (30-31-01).

Superseded by Rev 4

12

TPR-3

73-1

TRS No. 24, Walter

Istchenko, Chief Flight

Test for Minister of

Transport, 16 July 2014.

This MMEL is based on the

TRS No.24 that introduces

Limitation changed to

address CL300 and CL350

different engines time limited

dispatch (TLD).

Superseded by Rev 4

13

TPR-2

34-6

TRS No. 25,

W.Istchenko Chief Flight

Test for Minister of

Transport, 23 October

2017.

This MMEL is based on the

TRS No.25 introduces the

following changes:

Relief for 34-61-01 Flight

Management Computer, SB

100-34-10 reference is

removed from Note.

Operating procedure for LPV

Approach and RNP-AR

approach is incorporated.

New item 34-61-02 Flight

Management System

Performance Database

introduced.

New item 34-61-03 Flight

Management System Vspeed

Database introduced.

Superseded by Rev 4

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

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de révision:

6 Page

BD-100-1A10 Date: May 05/22 TPR-4

Temp

Rev #

Pages

Affected

TC approval Description of Revision Date Incorporated

Signature

14 TPR-3

TRS No. 14,

Jason Randall

Chief Flight Test for

Minister of Transport,

March 1st, 2022

New item Life Jackets

introduced

New item Life Rafts

introduced

Deletion Pitch Trim System

New item Hydraulic Shut off

Valve (HYD SOV) EICAS

Synoptic Page Indications

introduced

Revision Engine Anti-Ice

Valves OAT operations

limitation

New item Quick Access

Recorder (QAR) introduced

New item Nose Wheel

Steering - Oversteer Switch

introduced

NWS LIMIT EXCEEDED (C)

– New CAS message

oriented MMEL relief

introduced

Superseded by Rev 6

BD-100-1A10 BOMBARDIER Business Jet

MMEL USER COMMENTS

ON ERRORS, OMISSIONS, PROCEDURES (IF APPLICABLE), ETC.

FAX to: (514) 855-8648

Bombardier Aerospace

RMS Section Chief, Reliability, Maintainability, and Safety

Department 15T, Systems Engineering

OR

Email to: martin.zeppete[email protected]dier.com

OR

Mail to: address on back of this page

From: Telephone No.:

Company: Email address:

Date:

The MMEL requires the following correction or clarification:

ATA Chapter/MMEL Item No.:

Page No.: Page Date:

OUR RESPONSE

Thank you for your comment;

 We will issue Temporary Revision No.____

 We will include in Revision ___ scheduled for:

Comment:

Date:

--------------------------------------------------------------------------------------------------------------------------------------------------------

Bombardier Aerospace

500 Cote-Vertu Road West

Dorval, Quebec H4S 1Y9

Canada

Attention: Martin Zeppetelli

RM&S - Reliability, Maintainability and Safety

Dept. 15T

--------------------------------------------------------------------------------------------------------------------------------------------------------

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

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de révision:

6 Page

BD-100-1A10 Date: May 05/22 LEP-1

LIST OF EFFECTIVE PAGES

CHAPTER

PAGE DATE

CHAPTER

PAGE DATE

Title Page Jun 21/11

Table of Contents

TOC-1 Sep 30/03

TOC-2 Jun 21/11

Manual Appr. May 05/22 |

Page

Record of Revisions

REV-1 Oct 28/08

REV-2 May 02/18

REV-3 May 05/22 |

Record of Temporary Revisions

TPR-1 Oct 28/08

TPR-2 May 02/18

TPR-3 May 02/18

TPR-4 May 05/22 |

User Comments Apr 28/19

List of Effective Pages

LEP-1 May 05/22 |

LEP-2 May 05/22 |

LEP-3 May 05/22 |

LEP-4 May 05/22 |

Highlights Of Changes

HOC-1 May 05/22 |

HOC-2 May 05/22 |

Definitions

DEF-1 Sep 30/03

DEF-2 May 05/22 |

DEF-3 Sep 30/03

DEF-4 Sep 30/03

Abbreviations and Acronyms

ABB-1 May 02/18

Preamble

PRE-1 Sep 30/03

PRE-2 Jun 21/11

Section 1

TITLE-1 Jun 21/11

21 Air Conditioning

21-1 May 02/18

21-2 May 02/18

21-3 Oct 28/08

21-4 May 05/22 |

21-5 May 05/22 |

21-6 May 05/22 |

21-7 May 05/22 |

21-8 May 05/22 |

21-9 Oct 28/08

21-10 May 05/22 |

21-11 May 05/22 |

21-12 May 05/22 |

21-13 May 05/22 |

21-14 May 05/22 |

21-15 May 05/22 |

21-16 May 05/22 |

21-17 May 05/22 |

21-18 Oct 28/08

22 Auto Flight

22-1 Jun 21/11

22-2 May 05/22 |

22-3 May 05/22 |

23 Communications

23-1 May 02/18

23-2 May 02/18

23-3 May 02/18

23-4 May 02/18

23-5 May 02/18

24 Electrical Power

24-1 May 05/22 |

24-2 Mar 24/05

24-3 Mar 24/05

24-4 Oct 28/08

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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BD-100-1A10 Date: May 05/22 LEP-2

LIST OF EFFECTIVE PAGES (cont’d)

CHAPTER

PAGE DATE

CHAPTER

PAGE DATE

25 Equipment/Furnishings

25-1 Oct 28/08

25-2 Oct 28/08

25-3 Oct 28/08

25-4 May 05/22 |

25-5 May 05/22 |

25-6 May 05/22 |

25-7 May 05/22 |

25-8 Oct 28/08

25-9 Apr 28/19

25-10 May 05/22 |

26 Fire Protection

26-1 May 05/22 |

26-2 May 05/22 |

27 Flight Controls

27-1 May 05/22 |

27-2 Mar 24/05

28 Fuel

28-1 May 05/22 |

28-2 Jun 21/11

28-3 May 05/22 |

28-4 Jun 21/11

29 Hydraulic Power

29-1 May 05/22 |

29-2 Jun 21/11

29-3 Sep 30/03

29-4 Sep 30/03

30 Ice & Rain Protection

30-1 May 05/22 |

30-2 May 05/22 |

30-3 May 02/18

30-4 May 02/18

30-5 May 02/18

30-6 May 02/18

30-7 May 02/18

30-8 May 02/18

31 Instruments

31-1 Oct 28/08

31-2 May 05/22 |

31-3 Oct 28/08

31-4 May 05/22 |

31-5 May 05/22 |

31-6 Oct 28/08

31-7 May 05/22 |

31-8 May 05/22 |

31-9 May 02/18

32 Landing Gear

32-1 May 05/22 |

32-2 May 05/22 |

33 Lights

33-1 Mar 24/05

33-2 Mar 24/05

33-3 Oct 28/08

33-4 Apr 28/19

33-5 May 02/18

33-6 May 02/18

34 Navigation

34-1 May 05/22 |

34-2 May 02/18

34-3 May 02/18

34-4 May 02/18

34-5 May 02/18

34-6 May 05/22 |

34-7 May 02/18

34-8 May 02/18

35 Oxygen

35-1 May 05/22 |

35-2 May 05/22 |

35-3 May 05/22 |

35-4 Sep 30/03

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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BD-100-1A10 Date: May 05/22 LEP-3

LIST OF EFFECTIVE PAGES (cont’d)

CHAPTER

PAGE DATE

CHAPTER

PAGE DATE

36 Pneumatics

36-1 May 05/22 |

36-2 May 05/22 |

36-3 May 05/22 |

36-4 May 05/22 |

36-5 May 05/22 |

36-6 May 05/22 |

36-7 May 05/22 |

36-8 May 05/22 |

36-9 Oct 28/08

36-10 Oct 28/08

36-11 Oct 28/08

36-12 Oct 28/08

36-13 May 02/18

36-14 May 02/18

36-15 May 02/18

36-16 May 02/18

36-17 May 02/18

36-18 May 02/18

36-19 Oct 28/08

36-20 Oct 28/08

36-21 May 02/18

36-22 May 02/18

36-23 May 02/18

36-24 May 02/18

36-25 Oct 28/08

36-26 Oct 28/08

38 Water/Waste

38-1 May 05/22 |

38-2 May 05/22 |

45 Central Maintenance Systems

45-1 Sep 30/03

45-2 Sep 30/03

46 Information Systems

46-1 Apr 28/19

46-2 Apr 28/19

49 Auxiliary Power Unit

49-1 May 05/22 |

49-2 Sep 30/03

52 Doors

52-1 Mar 24/05

52-2 Mar 24/05

73 Engine Fuel and Control

73-1 May 05/22 |

73-2 Sep 30/03

74 Ignition

74-1 May 05/22 |

74-2 Sep 30/03

76 Engine Control

76-1 May 05/22 |

76-2 Sep 30/03

77 Engine Indicating

77-1 Sep 30/03

77-2 Sep 30/03

78 Exhaust

78-1 May 05/22 |

78-2 Sep 30/03

79 Oil

79-1 May 05/22 |

79-2 Sep 30/03

80 Starting

80-1 May 05/22 |

80-2 Sep 30/03

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

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3 Page

BD-100-1A10 Date: Jun 21/11 LEP-4

LIST OF EFFECTIVE PAGES (cont’d)

CHAPTER

PAGE DATE

CHAPTER

PAGE DATE

Section 2

TITLE-1 Jun 21/11

TITLE-2 Jun 21/11

INT-1 Jun 21/11

INT-2 Jun 21/11

TOC-1 May 05/22 |

TOC-2 Jun 21/11

2-1 May 05/22 |

2-2 Jun 21/11

2-3 May 05/22 |

2-4 Jun 21/11

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

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6 Page

BD-100-1A10 Date: May 05/22 HOC-1

HIGHLIGHTS OF CHANGE

Revision 6 introduces following changes.

Page No

Type of

change

Summary of changes

DEF-2 Editorial Definition M# removed.

All Editorial “M#” relaced with “M”.

22-2 Technical

22-30-01: New introduced.

22-30-02: New introduced.

22-3 Technical 22-30-03: New introduced.

25-4 Technical

25-14-09: New introduced.

25-14-10: New introduced.

25-10 Technical 25-70-02: New introduced.

27-1 Technical 27-41-01: Deleted.

28-1 Technical 28-11-01: New introduced.

29-1 Technical 29-11-02: New introduced.

30-2 Technical 30-10-06: Proviso c) added.

31-2 Technical 31-31-02: New introduced.

31-4 Editorial 31-41-02 1): Edit change of proviso c) and d).

31-5

Editorial

31-41-02 4): Edit change.

31-41-02 5): Edit change of proviso a) and b).

31-41-02 6): Edit change of proviso a) and b).

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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BD-100-1A10 Date: May 05/22 HOC-2

HIGHLIGHTS OF CHANGE (cont’d)

Page No

Type of

change

Summary of changes

31-7 Editorial 31-41-02 25): Edit change of proviso c) and d).

31-8 Editorial 31-41-02 27): Edit change.

34-1 Technical 34-10-01 3): New introduced.

34-6

Technical 34-44-01: Deleted.

35-2 Technical 35-20-02 2): New introduced.

35-3 Technical 35-20-02 2): New introduced.

74-1 Editorial 74-21-01: NOTE removed.

2-1 Technical AT RETARD INHIBIT (Caution) added.

2-3 Technical NWS LIMIT EXCEEDED (Caution) added.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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DEFINITIONS

COLUMN 1

1. "System & Sequence Numbers" are based on Air Transport Association (ATA) Specification No. 100 and

items are numbered sequentially.

2. "Item" means the equipment, system, component, or function listed in the "Item" column.

3. Repair Intervals: All users of an MEL must effect repairs of inoperative systems or components, deferred in

accordance with the MEL at or prior to the repair times established by the following letter designators:

Category "A": Items in this category shall be repaired within the time interval specified in the

remarks column of the operator's approved MEL, excluding the day the malfunction was recorded in

the Aircraft Maintenance Record/Logbook.

Category "B": Items in this category shall be repaired within three (3) consecutive calendar days (72

hours), excluding the day the malfunction was recorded in the Aircraft Maintenance Record/Logbook.

For example, if it were recorded at 10 a.m. on January 26th, the three-day interval would begin at

midnight the 26th and end at midnight the 29th.

Category "C": Items in this category shall be repaired within ten (10) consecutive calendar days

(240 hours), excluding the day the malfunction was recorded in the Aircraft Maintenance

Record/Logbook. For example, if it were recorded at 10 a.m. on January 26th, the 10-day interval

would end at midnight February 5th.

Category "D": Items in this category shall be repaired within one hundred and twenty (120)

consecutive calendar days (2880 hours), excluding the day the malfunction was recorded in the

Aircraft Maintenance Record/Logbook.

The letter designators are inserted adjacent to Column 2.

4. "***" symbol indicates an item which is not required by Regulations but which may have been installed on

some models of aircraft covered by this MMEL. This item may be included on the operator's MEL after the

approving office has determined that the item has been installed on one or more of the operator's aircraft. The

symbol, however, shall not be carried forward into the operator's MEL. It should be noted that neither this

policy nor the use of this symbol provide authority to install or remove an item from an aircraft. The "***"

symbol may be considered equivalent to the term "if installed".

COLUMN 2

1. "Number Installed" is the number (quantity) of items installed in the aircraft. This number represents the

aircraft configuration considered in developing this MMEL. Should the number be a variable (e.g., passenger

cabin items) a number is not required.

2. "-" symbol indicates a variable number (quantity) of the item installed.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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BD-100-1A10 Date: May 05/22 DEF-2

NOTE: Where the MMEL shows a variable number installed, the MEL must reflect the actual number

installed or an alternate means of configuration control approved by Transport Canada.

COLUMN 3

1. "Number Required For Dispatch" is the minimum number (quantity) of items required for operation provided

the conditions specified in Column 4 are met.

2. "-" symbol indicates a variable number (quantity) of the item required for dispatch.

NOTE: Where the MMEL shows a variable number required for dispatch, the MEL must reflect the actual

number required for dispatch or an alternate means of configuration control approved by

Transport Canada.

COLUMN 4

1. "Remarks or Exceptions" in this column includes a statement either prohibiting or permitting operation with a

specific number of items inoperative, provisos (conditions and limitations) for such operation, and appropriate

notes.

2. "(M)" symbol indicates a requirement for a specific maintenance procedure which must be accomplished prior

to operation with the listed item inoperative. If there is a requirement to perform the procedures more

frequently, for example, before each flight, then this is clearly stated in the provisos. Normally these

procedures are accomplished by maintenance personnel; however, other personnel may be qualified and

authorized to perform certain functions. Procedures requiring specialized knowledge or skill, or requiring the

use of tools or test equipment should be accomplished by maintenance personnel. The satisfactory

accomplishment of all maintenance procedures, regardless of who performs them, is the responsibility of the

operator.

Appropriate procedures, including the identification of qualified personnel authorized to accomplish them are

required to be published as part of the operator's manual or MEL.

3. "(O)" symbol indicates a requirement for a specific operations procedure which must be accomplished in

planning for and/or operating with the listed item inoperative. Normally these procedures are accomplished by

the flight crew; however, other personnel may be qualified and authorized to perform certain functions. The

satisfactory accomplishment of all procedures, regardless of who performs them, is the responsibility of the

operator.

Appropriate procedures are required to be published as part of the operator's manual or MEL.

These procedures are outlined in the Challenger 300 Operations and Maintenance Procedures. If a procedure

is not covered in the Challenger 300 Operations and Maintenance Procedures, the procedural requirements

can be found in the provisos of the MMEL or in the relevant Airplane Flight Manual (AFM).

NOTE: The (M) and (O) symbols are required in the operator's MEL unless otherwise authorized by

Transport Canada.

4. Alphabetical symbol indicates a proviso (condition or limitation) that must be complied with for operation with

the listed item inoperative.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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5. NOTES provide additional information for crewmember or maintenance consideration. Notes are used to

identify applicable material which is intended to assist with compliance, but do not relieve the operator of the

responsibility for compliance with all applicable requirements. Notes are not a part of the provisos.

6. Deleted in the remarks column after a sequence item indicates that the item was previously listed but is now

required to be operative if installed in the aircraft.

ADDITIONAL DEFINITIONS

1. "Administrative Control Item" means an item listed by the operator in the MEL for tracking and information

purposes. It may be added to an operator's MEL provided no relief is granted, or provided conditions and

limitations are contained in an approved document (i.e., Structural Repair Manual, Airworthiness Directive,

etc.). If relief other than that granted by an approved document is sought for an administrative control item, a

request must be submitted to Transport Canada. If the request results in review and approval, the item

becomes an MMEL item rather than an administrative control item.

2. "Airplane Flight Manual" (AFM) is the document required for type approval and approved by Transport

Canada. The approved AFM for the specific aircraft is listed on the applicable Type Approval Data Sheet.

3. "As required by Regulations" and other similar statements mean that the listed item is subject to certain

provisions (restrictive or permissive) expressed in the Federal Aviation Regulations (FARs), Airworthiness

Manual (AWM) or Canadian Aviation Regulations (CARs). The number of items specified by these

requirements must be operative. When the listed item is not required by the requirements, it may be

inoperative for the time specified by repair category.

4. "Change bar": A vertical bar in the margin indicates a change, addition or deletion in the adjacent text for the

current revision of that page only. The change bar is dropped at the next revision of that page.

5. Day of Discovery is the calendar day an equipment/instrument malfunction was recorded in the Aircraft

Maintenance Logbook and/or Record. This day is excluded from the calendar days or flight days specified in

the MMEL for the repair of an inoperative item of equipment, and is applicable to all MMEL items in categories

A,B,C, and D.

6. "Deactivated" and "Secured" means that the specified component must be put into an acceptable condition

for safe flight. An acceptable method of securing or deactivating will be established by the operator.

7. Engine Indicating Crew Alerting System (EICAS) that provides electronic messages refers to a system

capable of providing different priority levels of system information messages (e.g., WARNING, CAUTION,

ADVISORY and STATUS). Any airplane discrepancy message that affects dispatchability will be at the

WARNING, CAUTION or STATUS level.

8. "ER" refers to extended range operations of a two-engine airplane which has a type design approval for ER

operations and complies with the provisions of TP 6327 (ETOPS).

9. "Excess Items" means those items that have been installed but are redundant to the requirements.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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10. "Extended Overwater Operations" means operations over water at a horizontal distance of more than 50

nautical miles from the nearest shoreline.

11. ."Federal Aviation Regulations" (FARs) means the applicable portions of the Federal Aviation Act and

Federal Aviation Regulations.

12. "Flight Day" means a 24-hour period (from midnight to midnight) either Universal Coordinated Time (UCT) or

local time, as established by the operator, during which at least one flight is initiated for the affected aircraft.

13. "Icing Conditions" means an atmospheric environment that may cause ice to form on the aircraft or in the

engine(s).

14. "Inoperative" means a system and/or a component malfunction to the extent that it does not accomplish its

intended purpose and/or is not consistently functioning normally within its approved operating limit(s) or

tolerance(s).

15. Inoperative components of an inoperative system: Inoperative items which are components of a system

which is inoperative are usually considered components directly associated with and having no other function

than to support that system. (Warning/caution systems associated with the inoperative system must be

operative unless relief is specifically authorized per the MMEL).

16. "Passenger Convenience Items" means those items related to passenger convenience, comfort or

entertainment such as , but not limited to, galley equipment, movie equipment, ash trays, stereo equipment,

overhead reading lamps, etc.

17. Placarding: Each inoperative item must be placarded to inform and remind the crewmembers and

maintenance personnel of the equipment condition.

NOTE: To the extent practical, placards should be located adjacent to the control or indicator for the item

affected; however, unless otherwise specified, placard wording and location will be determined

by the operator.

18. "Visual Flight Rules" (VFR) is as defined in the CARs. This precludes a pilot from filing an Instrument Flight

Rules (IFR) flight plan.

19. "Visual Meteorological Conditions" (VMC) means the atmospheric environment is such that would allow a

flight to proceed under the visual flight rules applicable to the flight. This does not preclude operating under

Instrument Flight Rules.

20. "Visible Moisture" means an atmospheric environment containing water in any form that can be seen in

natural or artificial light; for example, clouds, fog, rain, sleet, hail, or snow.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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BD-100-1A10 Date: May 02/18 ABB-1

ABBREVIATIONS and ACRONYMS

ADC Air Data Computer

AFM Aircraft Flight Manual

AOA Angle of Attack

APR Automatic Performance

Reserve

APU Auxiliary Power Unit

ARINC Aeronautical Radio

Incorporated

ATC Air Traffic Control

AUX Auxiliary

BOOM Headset microphone

BRT Brightness

DCMP Direct Current Motor Pump/

Engine Secondary

Hydraulic Pump

DFDR Digital Flight Data

Recorder

DIM Dimming

EDP Engine Driven Pump/

Engine Primary

Hydraulic Pump

FDR Flight Data Recorder

(Digital)

FL Flight Level

HF High Frequency

ILS Instrument Landing

System

L/H Left Hand

LCD Liquid Crystal Display

LED Light Emitting Diode

MFD Multifunction Display

MMEL Master Minimum

Equipment List

MSL Mean Sea Level

NAV Navigation

PFD Primary Flight Display

R/H Right Hand

RVSM Reduced Vertical Separation

SAT Static Air

Temperature

SAL Steep Approach Landing

SYNC Synchronous

SOV Shutoff Valve

TT2 Engine Inlet

Temperature

V

1

Takeoff Decision

Speed (formerly

Denoted as Critical

Engine Failure Speed)

VFR Visual Flight Rules

VMC Visual Meteorological

Conditions

VOR VHF Omnidirectional

Range Station

VHF Very High Frequency

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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BD-100-1A10 Date: Sep 30/03 PRE-1

PREAMBLE

All equipment installed on an aircraft in compliance with the Airworthiness Standards and Operating Rules must be

operative. However, Canadian Aviation Regulations (605.07, 704.07 and 705.07) permit the publication of a

Minimum Equipment List (MEL) where compliance with certain equipment requirements is not necessary in the

interests of safety under all operating conditions. Experience has shown that with the various levels of redundancy

designed into aircraft, operation of every system or installed component may not be necessary when the remaining

operative component can provide the required level of safety.

A Master Minimum Equipment List (MMEL) is developed by Transport Canada, with participation by the aviation

industry, to improve aircraft utilization and thereby provide more convenient and economic air transportation for the

public. The approved MMEL includes those items of equipment related to airworthiness and operating regulations

and other items of equipment Transport Canada finds may be inoperative and yet maintain the required level of

safety by appropriate conditions and limitations; it does not contain obviously required items such as wings, flaps,

and rudders.

The MMEL is the basis for development of individual operator MELs which take into consideration the operator's

particular aircraft equipment configuration and operational conditions. Operator MELs, for administrative control,

may include items not contained in the MMEL; however, relief for administrative control items must be approved. An

operator's MEL may differ in format from the MMEL, but cannot be less restrictive than the MMEL. The individual

operator's MEL, when approved and authorized, permits operation of the aircraft with inoperative equipment.

Equipment not required by the operation being conducted and equipment in excess of the requirements are

included in the MEL with appropriate conditions and limitations. The MEL must not deviate from the Aircraft Flight

Manual Limitations, Emergency Procedures or with Airworthiness Directives. It is important to remember that all

equipment related to the airworthiness and the operating regulations of the aircraft not listed on the MMEL must be

operative.

Suitable conditions and limitations in the form of placards, maintenance procedures, crew operating procedures and

other restrictions as necessary are specified in the MEL to ensure that the required level of safety is maintained.

The MEL is intended to permit operation with inoperative items of equipment for a period of time until repairs can be

accomplished. It is important that repairs be accomplished at the earliest opportunity. In order to maintain the

required level of safety and reliability, the MMEL establishes limitations on the duration of and conditions for

operation with inoperative equipment. The MEL provides for release of the aircraft for flight with inoperative

equipment. When an item of equipment is discovered to be inoperative, it is reported by making an entry in the

Aircraft Maintenance Record/Logbook. The item is then either repaired or may be deferred per the MEL or other

approved means acceptable to Transport Canada prior to further operation. MEL conditions and limitations do not

relieve the operator from determining that the aircraft is in condition for safe operation with items of equipment

inoperative.

Operators are responsible for exercising the necessary operational control to ensure that the required level of safety

is maintained. When operating with multiple inoperative items, the interrelationships between those items and the

effect on aircraft Operation and crew workload must be considered.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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BD-100-1A10 Date: June 21/11 PRE-2

Operators are to establish a controlled and sound repair program including the parts, personnel, facilities,

procedures, and schedules to ensure timely repair.

WHEN USING THE MEL, COMPLIANCE WITH THE STATED INTENT OF THE PREAMBLE, DEFINITIONS, AND

THE CONDITIONS AND LIMITATIONS SPECIFIED IN THE MEL IS REQUIRED.

A new section has been authorized as an alternative to the standard method of MMEL dispatch relief, as is

normally achieved through fault isolation procedures, and subsequent reference to the dispatch

LRU/Component MMEL relief. Standard references to MMEL dispatch relief are in Section 1. Following the

standard MMEL herein, Section 2 has been developed with the objective of minimizing the requirement for

maintenance personnel to be available, largely allowing flight crews to dispatch from the displayed CAS

(Crew Alerting System) message, without specifically identifying failed LRUs or components.

As Section 2 is intended as an alternative dispatch relief methodology, the LRU/Component (Section 1)

relief will be retained in order to provide maximum flexibility for relief. Flight crews / operators may

dispatch failures with reference to either Section 1 or Section 2 of this MMEL to the advantage that either

may provide.

It will be recognized in many cases that when comparing dispatch relief provisos for posted CAS messages

in Section 2, to those of the related LRU / Component dispatch relief in Section 1, the provisos associated

with dispatching the CAS message will generally be more restrictive in content and relief interval. Without

the opportunity for fault isolation through maintenance, it must be assumed that worst-case failure

conditions always underlie the posted message - commensurately, dispatch must be more restrictive.

However, where maintenance personnel are available and fault isolation conducted, relief provisos in

Section 1 may be found to provide fewer or less stringent restrictions upon operations and offer a longer

relief interval.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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BD-100-1A10 Date: Jun 21/11 1 TITLE-1

SECTION ONE

LRU /

COMPONENT

ORIENTED

MMEL RELIEF

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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BD-100-1A10 Date: Jun 21/11 1 TITLE-2

THIS PAGE INTENTIONALLY LEFT BLANK

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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BD-100-1A10 Date: May 02/18 21-1

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série

article

3. Number Required For Dispatch

Nombre d'articles à expédier

21 – AIR CONDITIONING

4.

Remarks or Exceptions

Remarques ou exceptions

00-01 Integrated Air System

Controller (IASC)

1) Aircraft without

SB 100-21-05

a) IASC 1

Channel B

B

1 0 (O) May be inoperative provided:

a) IASC 2 Channel B is operative,

b) Left Bleed Loop is considered inoperative

(36-20-01),

c) Left High Pressure Valve is considered

inoperative (30-10-01), and

d) Operational status of Pre-cooler Cross Over

Valve is verified once each flight day.

b) IASC 2

Channel B

B

1 0 (O) May be inoperative provided:

a) IASC 1 Channel B is operative,

b) Trim Air System is considered inoperative

(21-61-03),

c) Right Bleed Loop is considered inoperative

(36-20-01),

d) Right High Pressure Valve is considered

inoperative (30-10-01), and

e) Operational status of Pre-cooler Cross Over

Valve is verified once each flight day.

2) Aircraft with

SB 100-21-05,

Aircraft 20101

and Subs.

a) IASC 1

Channel B

C

1 0 (O) May be inoperative provided:

a) IASC 2 Channel B is operative,

b) Left Bleed Loop is considered inoperative

(36-20-01),

c) Left High Pressure Valve is considered

inoperative (30-10-01), and

d) Operational status of Pre-cooler Cross Over

Valve is verified once each flight day.

(cont’d)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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BD-100-1A10 Date: May 02/18 21-2

1.

2.

Number In

stalled

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série

article

3. Number Required For Dispatch

Nombre d'articles à e

xpédier

21 – AIR CONDITIONING

4.

Remarks or Exceptions

Remarques ou exceptions

00-01 Integrated Air System

Controller (IASC)

(Cont’d)

2) Aircraft with

SB 100-21-05,

Aircraft 20101

and Subs.

(Cont’d)

b) IASC 2

Channel B

C

1 0 (O) May be inoperative provided:

a) IASC 1 Channel B is operative,

b) Trim Air System is considered inoperative

(21-61-03),

c) Right Bleed Loop is considered inoperative

(36-20-01),

d) Right High Pressure Valve is considered

inoperative (30-10-01), and

e) Operational status of Pre-cooler Cross Over

Valve is verified once each flight day.

23-03 Avionics Ventilated

Temperature Sensors

1) L/H Avionics

Ventilated

Temperature

Sensor Elements

C

2 1

C

2 0 (M) Any or all may be inoperative provided:

a) One R/H Avionics Ventilated Temperature

Sensor Element is verified operative once each

flight day,

b) Avionics cooling valve is verified operative

before each flight, and

c) Avionics cooling fan is verified operative before

each flight.

(

cont'd

)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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BD-100-1A10 Date: Oct 28/08 21-3

1.

2.

Number Installe

d

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série

article

3. Number Required For Dispatch

Nombre d'articles

à expédier

21 – AIR CONDITIONING

4.

Remarks or Ex

c

eptions

Remarques ou exceptions

23-03 Avionics Ventilated

Temperature Sensors

(Cont'd)

2) R/H Avionics

Ventilated

Temperature

Sensor Elements

C

2 1

C

2 0 (M) Any or all may be inoperative provided:

a) One L/H Avionics Ventilated Temperature

Sensor Element is verified operative once each

flight day,

b) Avionics cooling valve is verified operative

before each flight, and

c) Avionics cooling fan is verified operative before

each flight.

31-02 Safety Valves

C

2 0 (O) Any or all may be inoperative provided:

a) PRESSURIZATION EMER DEPRESS switch is

selected ON, and

b) Operations are conducted unpressurized at or

below 9000 ft. MSL.

31-03 PRESSURIZATION

MANUAL “ON”

Switch Light

(light function only)

C

1 0

31-04 PRESSURIZATION

EMER DEPRESS

“ON” Switch Light

(light function only)

C

1 0

31-05 PRESSURIZATION

DITCHING “ON”

Switch Light

(light function only)

C

1 0

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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BD-100-1A10 Date: May 05/22 21-4

1.

2.

Num

ber Ins

talled

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série

article

3. Number Required For Dispatch

Nombre d'articles à ex

p

édier

21 – AIR CONDITIONING

4.

Remar

ks or Excepti

ons

Remarques ou exceptions

51-01 Flow Control Valves

(FCV)

1) Aircraft without

SB 100-21-05

B

2 1 (M)(O) Left may be inoperative provided:

a) Valve is secured CLOSED,

b) Trim Air System is operative,

c) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to NORM,

d) Trim Air Inlet Temperature Sensor is operative,

e) Right Bleed Loop is operative,

f) Operational status of L/H Environmental

Control Bleed Pressure Indication System is

verified before each flight,

g) Ram Air Valve is verified operative,

h) Operations are conducted at or below FL 250,

and

i) Operations are conducted within one hour from

a suitable airport.

|

B

2 1 (M)(O) Right may be inoperative provided:

a) Valve is secured CLOSED,

b) Pack Inlet Temperature Sensor is operative,

c) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to NORM,

d) Left Bleed Loop is operative,

e) Operational status of R/H Environmental

Control Bleed Pressure Indication System is

verified before each flight,

f) Ram Air Valve is verified operative,

g) Operations are conducted at or below FL 250,

and

h) Operations are conducted within one hour from

a suitable airport.

|

(cont’d)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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BD-100-1A10 Date: May 05/22 21-5

1

.

2.

Number Installed

System

& Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/

s

érie

article

3. Number Required For Dispatch

No

mbre

d'articles à expédier

21 – AIR CONDITIONING

4.

Remarks or Exceptions

Remarques ou exceptions

51-01 Flow Control Valves

(FCV)

(Cont’d)

1) Aircraft without

SB 100-21-05

(Cont’d)

C

2 0 (M)(O) Any or all may be inoperative provided:

a) Affected valve is secured CLOSED,

b) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to OFF,

c) Ram Air Valve is selected OPEN,

d) PRESSURIZATION EMER DEPRESS switch

is selected ON, and

e) Operations are conducted unpressurized at or

below 9000 ft. MSL.

|

2) Aircraft with

SB 100-21-05

C

2 1 (M)(O) Left may be inoperative provided:

a) Valve is secured CLOSED,

b) Trim Air System is operative,

c) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to NORM,

d) Trim Air Inlet Temperature Sensor is operative,

e) Right Bleed Loop is operative,

f) Operational status of L/H Environmental

Control Bleed Pressure Indication System is

verified before each flight,

g) Ram Air Valve is verified operative,

h) Operations are conducted at or below FL 250,

and

i) Operations are conducted within one hour from

a suitable airport.

|

(cont’d)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

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- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 21-6

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série

arti

cle

3. Number Required For Dispatch

Nombre d'ar

ticles à ex

pédier

21 – AIR CONDITIONING

4.

Remark

s or Exceptions

Remarques ou exceptions

51-01 Flow Control Valves

(FCV)

(Cont’d)

2) Aircraft with

SB 100-21-05

(Cont’d)

C

2 1 (M)(O) Right may be inoperative provided:

a) Valve is secured CLOSED,

b) Pack Inlet Temperature Sensor is operative,

c) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to NORM,

d) Left Bleed Loop is operative,

e) Operational status of R/H Environmental

Control Bleed Pressure Indication System is

verified before each flight,

f) Ram Air Valve is verified operative,

g) Operations are conducted at or below FL 250,

and

h) Operations are conducted within one hour

from a suitable airport.

|

C

2 0 (M)(O) Any or all may be inoperative provided:

a) Affected valve is secured CLOSED,

b) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to OFF,

c) Ram Air Valve is selected OPEN,

d) PRESSURIZATION EMER DEPRESS switch

is selected ON, and

e) Operations are conducted unpressurized at or

below 9000 ft. MSL.

|

52-01 Compressor

Discharge

Temperature Sensor

(CDTS)

C

1 0 May be inoperative provided left and right Flow Control

Valves are considered inoperative (21-51-01).

1) Compressor

Discharge

Temperature

Sensor Elements

C

2 1 (O) May be inoperative provided operational status of

Pre-cooler Cross Over Valve is verified once each flight

day.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 21-7

1

.

2.

Number Installed

System

& Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série

article

3. Number Required For Dispatch

Nombre d'articles à

expédier

21 – AIR CONDITIONING

4.

Rem

arks or Exceptions

Remarques ou exceptions

52-02 Pack Temperature

Sensor (PTS)

C

1 0 (O) May be inoperative provided operational status of

Pre-cooler Cross Over Valve is verified once each flight

day.

52-03 Pack Discharge

Temperature Sensor

(PDTS)

C

1 0 May be inoperative provided left and right Flow Control

Valves are considered inoperative (21-51-01).

1) Pack Discharge

Temperature

Sensor

Elements

C

2 1 (O) May be inoperative provided operational status of

Pre-cooler Cross Over Valve is verified once each flight

day.

52-04 Air Conditioning

Pack

C

1 0 (O) May be inoperative provided:

a) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to OFF,

b) Ram Air Valve is selected OPEN,

c) PRESSURIZATION EMER DEPRESS switch

is selected ON, and

d) Operations are conducted unpressurized at or

below 9000 ft. MSL.

53-01 Ram Air Valve

(RAV)

C

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

a) Valve is secured OPEN,

b) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to OFF,

c) PRESSURIZATION EMER DEPRESS switch is

selected ON, and

d) Operations are conducted unpressurized at or

below 9000 ft. MSL.

|

(cont’d)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Révision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 21-8

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/sé

rie article

3. Number Required For Dispatch

No

m

bre d

'articles à expédier

21 – AIR CONDITIONING

4.

Rem

arks or Exceptions

Remarques ou exceptions

53-02 Ram Air Regulating

Valve

(RARV)

Aircraft 20006 to

20033 without

SB 100-21-01

C

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

a) Valve is secured CLOSED,

b) Ram Air Valve is verified operative,

c) Operations are conducted at or below FL 250,

and

d) Operations are conducted within one hour from

a suitable airport.

|

C

1 0 (O) May be inoperative provided:

a) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to OFF,

b) Ram Air Valve is selected OPEN,

c) PRESSURIZATION EMER DEPRESS switch

is selected ON, and

d) Operations are conducted unpressurized at or

below 9000 ft. MSL.

Aircraft

20006 to 20033 with

SB 100-21-01,

20001 to 20005,

20034 and

subsequent.

C

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

a) Valve is secured in DISPATCH position,

b) Ram Air Valve is verified operative,

c) Operations are conducted at or below FL 250,

and

d) Operations are conducted within one hour from

a suitable airport.

|

C

1 0 (O) May be inoperative provided:

a) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to OFF,

b) Ram Air Valve is selected OPEN,

c) PRESSURIZATION EMER DEPRESS switch

is selected ON, and

d) Operations are conducted unpressurized at or

below 9000 ft. MSL.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

2 Page

BD-100-1A10 Date: Oct 28/08 21-9

1.

2.

N

umber Installed

System

& S

equence N

o

Item

Nombre d’articles installés

N

o

de

système/série article

3. Number Required For Dispatch

Nombre d'articles à expédier

21 – AIR CONDITIONING

4.

Remarks or Exceptions

Remarques ou exceptions

60-01 AIR COND/BLEED

RAM AIR “ON” Switch

Light

(light function only)

C

1 0

60-02 AIR COND/BLEED

MAN TEMP “ON”

Switch Light

(light function only)

C

1 0

61-01 Cockpit/Cabin

Ventilated

Temperature Sensors

C

2 0 (O) Any or all may be inoperative provided cockpit and

cabin temperatures are controlled manually.

1) Cockpit/ Cabin

Ventilated

Temperature

Sensor

Elements

C

4 2 (O) One sensor element per sensor may be inoperative

provided operational status of Pre-cooler Cross Over

Valve is verified once each flight day.

61-02 Duct Temperature

Sensors (DTS)

1) Aircraft without

SB 100-21-05

B

2 0 Any or all may be inoperative provided Trim Air System

is considered inoperative (21-61-03).

a) Duct

Temperature

Sensor

Elements

B

4 2 (O) One sensor element per sensor may be inoperative

provided operational status of Pre-cooler Cross Over

Valve is verified once each flight day.

2) Aircraft with

SB 100-21-05

C

2 0 Any or all may be inoperative provided Trim Air System

is considered inoperative (21-61-03).

a) Duct

Temperature

Sensor

Elements

C

4 2 (O) One sensor element per sensor may be inoperative

provided operational status of Pre-cooler Cross Over

Valve is verified once each flight day.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 21-10

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série

article

3. Number Required For Dispatch

Nombre d'articles

à expé

dier

21 – AIR CONDITIONING

4.

Remarks or Exceptio

ns

Remarques ou exceptions

61-03 Trim Air System

(HARSOVs)

1) Aircraft without

SB 100-21-05

B

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

a) Right Flow Control Valve is secured CLOSED,

b) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to PACK ONLY,

c) R BLEED is selected OFF,

d) Pre-cooler Cross Over Valve is operative,

e) Left Flow Control Valve is operative,

f) Pack Inlet Temperature Sensor is operative,

g) Left Bleed Loop is operative,

h) Ram Air Valve is verified operative,

i) Operations are conducted at or below FL 250,

and

j) Operations are conducted within one hour from

a suitable airport.

|

C

1 0 (O) May be inoperative provided:

a) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to OFF,

b) Ram Air Valve is selected OPEN,

c) PRESSURIZATION EMER DEPRESS switch is

selected ON, and

d) Operations are conducted unpressurized at or

below 9000 ft. MSL.

(cont’d)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 21-11

1.

2.

Number Installed

S

ystem

& Sequence N

o

Ite

m

Nombre d’articles installés

N

o

de

sy

stème/série article

3. Number Required For Dispatch

Nombre d'articles à expédier

21 – AIR CONDITIONING

4.

Remarks or Exceptions

Remarques ou exceptions

61-03 Trim Air System

(HARSOVs)

(Cont’d)

2) Aircraft with

SB 100-21-05

C

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

a) Right Flow Control Valve is secured CLOSED,

b) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to PACK ONLY,

c) R BLEED is selected OFF,

d) Pre-cooler Cross Over Valve is operative,

e) Left Flow Control Valve is operative,

f) Pack Inlet Temperature Sensor is operative,

g) Left Bleed Loop is operative,

h) Ram Air Valve is verified operative,

i) Operations are conducted at or below FL 250,

and

j) Operations are conducted within one hour from

a suitable airport.

|

C

1 0 (O) May be inoperative provided:

a) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to OFF,

b) Ram Air Valve is selected OPEN,

c) PRESSURIZATION EMER DEPRESS switch

is selected ON, and

d) Operations are conducted unpressurized at or

below 9000 ft. MSL.

61-04 Pre-cooler Cross

Over Valve (PCV)

C

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

a) Valve is secured OPEN,

b) Trim Air System is operative,

c) Ram Air Valve is verified operative,

d) Operations are conducted at or below FL 250,

and

e) Operations are conducted within one hour from

a suitable airport.

|

(cont'd)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 21-12

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série article

3. Number Required For Dispatch

Nombre

d'articles à expédier

21 – AIR CONDITIONING

4.

Rem

a

rks or Exceptions

Remarques ou exceptions

61-04 Pre-cooler Cross

Over Valve (PCV)

(Cont'd)

C

1 0 (O) May be inoperative provided:

a) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to OFF,

b) Ram Air Valve is selected OPEN,

c) PRESSURIZATION EMER DEPRESS switch is

selected ON, and

d) Operations are conducted unpressurized at or

below 9000 ft. MSL.

61-05 Pack Inlet

Temperature Sensor

(PITS)

1) Aircraft without

SB 100-21-05

B

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

a) L/H Bleed Valve is secured CLOSED,

b) XBLEED Valve is selected CLOSED,

c) R/H Bleed Valve is operative,

d) R/H Environmental Control Bleed Pressure

Indication System is operative,

e) Right Bleed Loop is operative,

f) Right Flow Control Valve is operative,

g) Trim Air System is operative,

h) Trim Air Inlet Temperature Sensor is operative,

i) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to NORM,

j) Ram Air Valve is verified operative,

k) Operations are conducted at or below FL 250,

and

l) Operations are conducted within one hour from

a suitable airport.

|

(cont'd)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 21-13

1.

2.

N

umber Installed

System & Se

quence N

o

Item

Nombre d’articles installés

N

o

de

système

/série article

3. Number Required For Dispatch

Nombre d'articles à expédier

21 – AIR CONDITIONING

4.

Remarks or Except

ions

Remarques ou exceptions

61-05 Pack Inlet

Temperature Sensor

(PITS)

(Cont'd)

1) Aircraft without

SB 100-21-05

(Cont’d)

B

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

a) L/H Bleed Valve is secured CLOSED,

b) XBLEED Valve is selected CLOSED,

c) APU is operative and used throughout flight,

d) APU Load Control Valve is operative,

e) Right Bleed Loop is operative,

f) Right Flow Control Valve is operative,

g) Trim Air System is operative,

h) Trim Air Inlet Temperature Sensor is operative,

i) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to NORM,

j) Ram Air Valve is verified operative,

k) Operations are conducted at or below FL 190,

and

l) Operations are conducted within one hour from

a suitable airport.

|

C

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

a) L/H Bleed Valve is secured CLOSED,

b) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to OFF,

c) Ram Air SOV is selected OPEN,

d) PRESSURIZATION EMER DEPRESS switch is

selected ON, and

e) Operations are conducted unpressurized at or

below 9000 ft. MSL.

|

a) Pack Inlet

Temperature

Sensor

Elements

B

2 1 (O) May be inoperative provided operational status of

Pre-cooler Cross Over Valve is verified once each flight

day.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 21-14

1.

2.

Numbe

r Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série article

3. Number Required For Dispatch

Nombre d'articles à ex

p

édier

21 – AIR CONDITIONING

4.

Remar

ks or Exceptions

Remarques ou exceptions

61-05 Pack Inlet

Temperature Sensor

(PITS)(Cont'd)

2) Aircraft with

SB 100-21-05

C

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

a) L/H Bleed Valve is secured CLOSED,

b) XBLEED Valve is selected CLOSED,

c) R/H Bleed Valve is operative,

d) R/H Environmental Control Bleed Pressure

Indication System is operative,

e) Right Bleed Loop is operative,

f) Right Flow Control Valve is operative,

g) Trim Air System is operative,

h) Trim Air Inlet Temperature Sensor is operative,

i) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to NORM,

j) Ram Air Valve is verified operative,

k) Operations are conducted at or below FL 250,

and

l) Operations are conducted within one hour from

a suitable airport.

|

C

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

a) L/H Bleed Valve is secured CLOSED,

b) XBLEED Valve is selected CLOSED,

c) APU is operative and used throughout flight,

d) APU Load Control Valve is operative,

e) Right Bleed Loop is operative,

f) Right Flow Control Valve is operative,

g) Trim Air System is operative,

h) Trim Air Inlet Temperature Sensor is operative,

i) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to NORM,

j) Ram Air Valve is verified operative,

k) Operations are conducted at or below FL 190,

and

l) Operations are conducted within one hour

from a suitable airport.

(cont’d)

|

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 21-15

1.

2.

Number Installed

System &

Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série article

3. Number Required For Dispatch

Nombre

d’articles

à e

xpédier

21 – AIR CONDITIONING

4.

Remarks or Exceptions

Remarques ou exceptions

61-05 Pack Inlet

Temperature Sensor

(PITS)

(Cont'd)

2) Aircraft with

SB 100-21-05

(Cont’d)

C

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

a) L/H Bleed Valve is secured CLOSED,

b) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to OFF,

c) Ram Air SOV is selected OPEN,

d) PRESSURIZATION EMER DEPRESS switch

is selected ON, and

e) Operations are conducted unpressurized at or

below 9000 ft. MSL.

|

a) Pack Inlet

Temperature

Sensor

Elements

C

2 1 (O) May be inoperative provided operational status of

Pre-cooler Cross Over Valve is verified once each flight

day.

61-06 Trim Air Inlet

Temperature Sensor

(HATS)

1) Aircraft without

100-21-05

B

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

a) R/H Bleed Valve is secured CLOSED,

b) XBLEED Valve is selected CLOSED,

c) L/H Bleed Valve is operative,

d) L/H Environmental Control Bleed Pressure

Indication System is operative,

e) Left Bleed Loop is operative,

f) Left Flow Control Valve is operative,

g) Pack Inlet Temperature Sensor is operative,

h) APU bleed is used for engines start only,

i) Ram Air Valve is verified operative,

j) Operations are conducted at or below FL 250,

and

k) Operations are conducted within one hour from

a suitable airport.

(cont’d)

|

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 21-16

1.

2

.

Number Inst

alled

Sy

stem & Sequence N

o

I

t

em

Nombre d’articles installés

N

o

de

système/série article

3. Number Required For Dispatch

Nombre d'articles à e

xpédier

21 – AIR CONDITIONING

4.

Remarks or Exceptions

Remarques ou exceptions

61-06 Trim Air Inlet

Temperature Sensor

(HATS)

(Cont’d)

1) Aircraft without

100-21-05

(Cont’d)

C

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

a) R/H Bleed Valve is secured CLOSED,

b) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to OFF,

c) Ram Air Valve is selected OPEN,

d) PRESSURIZATION EMER DEPRESS switch is

selected ON, and

e) Operations are conducted unpressurized at or

below 9000 ft. MSL.

|

a) Trim Air Inlet

Temperature

Sensor

Elements

B

2 1

2) Aircraft with

100-21-05

C

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

a) R/H Bleed Valve is secured CLOSED,

b) XBLEED Valve is selected CLOSED,

c) L/H Bleed Valve is operative,

d) L/H Environmental Control Bleed Pressure

Indication System is operative,

e) Left Bleed Loop is operative,

f) Left Flow Control Valve is operative,

g) Pack Inlet Temperature Sensor is operative,

h) APU bleed is used for engines start only,

i) Ram Air Valve is verified operative,

j) Operations are conducted at or below FL 250,

and

k) Operations are conducted within one hour from

a suitable airport.

(cont’d)

|

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 21-17

1.

2.

Number Installed

System & Sequence N

o

Ite

m

Nombre d’articles installés

N

o

de

système/série

a

rticle

3. Number Required For Dispatch

Nombre d'articles à expédier

21 – AIR CONDITIONING

4.

Remarks or Exceptions

Remarques ou exceptions

61-06 Trim Air Inlet

Temperature Sensor

(HATS)

(Cont’d)

2) Aircraft with

100-21-05

(Cont’d)

C

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

a) R/H Bleed Valve is secured CLOSED,

b) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to OFF,

c) Ram Air Valve is selected OPEN,

d) PRESSURIZATION EMER DEPRESS switch

is selected ON, and

e) Operations are conducted unpressurized at or

below 9000 ft. MSL.

|

a) Trim Air Inlet

Temperature

Sensor

Elements

C

2 1

61-07 Temperature

Control Valve (TCV)

C

1 0 May be inoperative provided L/H and R/H Flow Control

Valves are considered inoperative (21-51-01).

61-08 Baggage

Compartment

Heaters

C

2 0 (M)(O) Any or all may be inoperative provided affected

heater is deactivated.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

2 Page

BD-100-1A10 Date: Oct 28/08 21-18

1.

2.

Number

Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

systèm

e/série article

3. Number Required For Dispatch

N

ombre d'articles à expé

d

i

er

21 – AIR CONDITIONING

4.

Remarks

or Exceptions

Remarques ou exceptions

THIS PAGE INTENTIONALLY LEFT BLANK

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

3 Page

BD-100-1A10 Date: Jun 21/11 22-1

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

s

ystème/

série articl

e

3. Number Required For Dispatch

Nombre d'articles à expé

dier

22 – AUTO FLIGHT

4.

Remarks or Exceptions

Remarques ou exceptions

10-01 Autopilot System B

1 0 Except where enroute operations or approach

procedures require its use, may be inoperative

provided Altitude Alerting System is operative.

NOTE1: Autopilot is required for RVSM Operations.

NOTE2: Relief for inoperative individual flight

guidance operational modes is provided by

MMEL Item 22-10-02 Flight Directors.

10-02 Flight Directors B

2 1 (O) Except where enroute operations or approach

procedures require its use, may be inoperative

provided Autopilot System is considered inoperative

(22-10-01).

B

2 0 Except where enroute operations or approach

procedures require its use, may be inoperative

provided:

a) Autopilot System is considered inoperative

(22-10-01),

b) TO/GA Switches are considered inoperative

(22-11-02), and

c) Operations are conducted in accordance with

AFM Supplement, Supplement 2 -

Supplemental information for the MMEL.

1) Flight Director

Modes

C

- - Except where enroute operations or approach

procedures require its use, individual flight director

modes may be inoperative provided Altitude Alerting

System is operative.

NOTE1: Flight director altitude hold mode is required

for RVSM Operations.

NOTE2: Any flight director mode which operates

normally may be used.

11-01 Autopilot/Flight

Director Sync

Switches

C

2 0 Any or all may be inoperative in Non-SYNC mode.

(cont'd)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 22-2

1.

2.

Number Installed

System & Se

quence

N

o

Item

Nombre d’articles installés

N

o

de

sy

s

t

ème/série article

3. Number Required For Dispatch

Nombre d'articles à expédier

22 – AUTO FLIGHT

4.

Remarks or Exceptions

Remarques ou exceptions

11-01 Autopilot/Flight

Director Sync

Switches

(Cont'd)

B

2 0 Any or all may be inoperative in SYNC mode provided:

a) Autopilot is disengaged and considered inoperative

(22-10-01),

b) Flight Directors are selected off and considered

inoperative (22-10-02), and

c) TO/GA Switches are considered inoperative (22-

11-02).

11-02 Take-Off/Go-Around

(TO/GA) Switches

C

2 1 (O) May be inoperative provided alternate procedures

are established and used.

C

2 0

Any or all may be inoperative provided:

a) Operations are conducted in accordance with AFM

Supplement, Supplement 2 - Supplemental

information for the MMEL, and

b) Operations with Steep Approach are not

conducted.

30-01 Auto Throttle

System (Auto

throttle System is

installed either via

SB 350−22−002 or

on Aircraft 20937

and subsequent)

C

1 0

(O) May be inoperative provided:

a) Auto Throttle is confirmed disengaged, and.

b) LH and RH Thrust levers are verified to move freely

and maintain adequate friction, prior to each flight.

|

30-02 AT Disengage

Buttons/Function-

(loss of

disengagement

capability)

(Auto Throttle

System is installed

either via SB

350−22−002 or on

Aircraft 20937 and

subsequent)

C

2 1 (O) One may be inoperative in the inactive state (loss

of disengagement capability) provided:

a) Remaining AT Disengage Button is verified

operative before each flight, and

b) Alternate procedures are established and used to

disengage using the remaining AT Disengage

Button.

|

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 22-3

1

.

2.

Number Installed

System & Se

quence N

o

Ite

m

Nombre d’articles installés

N

o

de

système/série article

3. Number Required For Dispatch

Nombre d'artic

les à expédier

22 – AUTO FLIGHT

4.

Remarks or Exceptions

Remarques ou exceptions

30-03

Auto Throttle

Engagement

Switches (Auto

Throttle System is

installed either via

SB 350−22−002 or

on Aircraft 20937

and subsequent)

C

2 1 One may be inoperative in inactive state (loss of

engagement capability) provided the remaining Auto

Throttle Engagement Switch is used.

|

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 23-1

1.

2.

Number Installed

Syst

em & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série article

3. Number Required For Dispatch

Nombre d'articles à expédier

23 – COMMUNICATIONS

4.

Remarks or Exceptions

Remarques ou exceptions

11-01 VHF Communication

Systems

D

- 2 VHF 3 may be inoperative.

11-02 HF Communication

Systems

***

D

- - (M) Any in excess of those required by Regulations

may be inoperative.

13-01 Satellite

Communication

(SATCOM) System

***

C

1 0 (O) May be inoperative provided alternate procedures

are established and used.

D

1 0 May be inoperative provided routine procedures do not

require its use.

20-01 Datalink System

(Includes CPDLC and

ADS-C functions***)

C

1 0 (O) May be inoperative where routine procedures

require its use provided alternate procedures are

established and used.

D

1 0 May be inoperative provided operating regulations do

not require its use.

1) Controller Pilot

Data Link

Communications

(CPDLC) (Aircraft

20003 to 20407

with SB 100-23-

22) (Aircraft

20408 and up)

C

2 0 (O) May be inoperative where routine procedures

require its use provided alternate procedures are

established and used.

D

2 0 May be inoperative provided operating regulations do

not require its use.

a) CPDLC In-

Coming

Message

Visual

Alerting (CDU

and EICAS)

C

2 0 May be inoperative where routine procedures require

its use provided In-Coming Message Aural Alerting

(chime) is operative.

D

2 0 May be inoperative provided operating regulations and

routine operations do not require the use of CPDLC.

(Cont’d)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 23-2

1.

2.

N

umbe

r Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série a

rt

icle

3. Number Required For Dispatch

Nombre d'articles à expédier

23 – COMMUNICATIONS

4.

Remarks or Exceptions

Remarques ou exceptions

20-01 Datalink System

(Includes CPDLC and

ADS-C functions***)

(Cont’d)

2)

Automatic

Dependent

Surveillance

Contract (ADS-C)

***

C

1 0

(O) May be inoperative where routine procedures

require its use provided alternate procedures are

established and used.

D

1 0 May be inoperative provided operating regulations do

not require its use.

22-01 Selective Call System

(SELCAL)

***

C

1 0 (O) May be inoperative provided alternate procedures

are established and used.

D

1 0 May be inoperative provided routine procedures do not

require its use.

41-01 Passenger Address

(PA) System

B

1 0 (O) May be inoperative provided:

a) Alternate procedures are established and used,

and

b) Required standard safety briefings are given to

passengers using a means that will ensure the

briefings are audible to each passenger.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 23-3

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série

article

3. Number Required For Dispatch

Nombre d'articles à expédier

23 – COMMUNICATIONS

4.

Remark

s or Exce

ptions

Remarques ou exceptions

41-02 Alerting System

1) Cabin Chimes

C

- 0 May be inoperative provided Passenger Address

System is operative.

NOTE: Passenger to Flight Crew Call System

(Cabin/Lavatory Call) is considered a

Passenger Convenience Item (25-70-01).

B

- 0 (O) May be inoperative provided alternate procedures

are established and used.

NOTE: Passenger to Flight Crew Call System

(Cabin/Lavatory Call) is considered the

Passenger Convenience Item (25-70-01).

51-01 Hand Held

Microphones

C

2 1

May be inoperative provided associated Boom

Microphone is operative and used.

C

2 0 Any or all may be inoperative provided:

a) Boom Microphones are operative and used,

and

b) Spare Boom Microphone is available in flight

compartment.

51-02 Flight Compartment

Speakers

C

2 0 Any or all may be inoperative provided:

a) All flight crew members on flight deck duty

utilize headsets, and

b) Spare headset is readily available.

51-03 Boom Microphones

A

- 0 May be inoperative provided:

a) Associated Hand Held Microphone is operative

and used, and

b) Repairs are made within three flight days.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 23-4

1.

2.

Number Installed

Sy

st

em & Sequence

N

o

Item

Nombre d’articles installés

N

o

de

système/série

article

3. Number Required For Dispatch

Nombre d'article

s à expéd

ier

23 – COMMUNICATIONS

4.

Remarks or Exceptions

Remarques ou exceptions

51-04 Headsets D

- - Any in excess of those required for each flight crew

member on flight deck duty may be inoperative.

51-06 Cabin/Lavatory

Speakers

B

- 0 Any or all may be inoperative provided:

a) Passenger Address System is considered

inoperative (23-41-01),

b) Alerting System is considered inoperative

(23-41-02), and

c) Pre-recorded Announcement System is

considered inoperative (23-70-01).

1) Lavatory

Speaker

B

1 0 (O) May be inoperative provided alternate procedures

are established and used.

51-07 Control Wheel

TX/INPH Switches

A

2 1 (O) May be inoperative in non-transmit mode provided:

a) Boom Microphone on affected side is

considered inoperative (23-51-03),

b) Crew interphone using O2 mask and hot mike

is verified operative before each flight, and

c) Repairs are made within three flight days.

NOTE: Pilot with inoperative TX/INTPH Switch will

not be able to transmit when wearing the O2

mask.

70-01 Pre-recorded

Announcement

System (Airshow

Custom Passenger

Briefings)

***

C

1 0 (O) May be inoperative provided alternate procedures

are established and used.

D

1 0 May be inoperative provided routine procedures do not

require its use.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 23-5

1.

2.

Number Installed

Syst

em & Sequ

ence N

o

Item

Nombre d’articles installés

N

o

de

système/série

article

3. Number Required For Dispatch

Nomb

re

d'articles à

expédier

23 – COMMUNICATIONS

4.

Remarks or Exceptions

Remarques ou exceptions

71-01 Cockpit Voice

Recorder

(CVR) System

Including the Recorder

Independent Power

Supply (RIPS)

1) If CVR and FDR

required by

regulations

A

1 0 May be inoperative provided:

a) FDR is operative, and

b) Repairs are made within three flight days.

a) Recorder

Independent

Power Supply

(RIPS)

(20292 and

Subs Post

SB 100-23-20)

***

C

1 0 (M)

2) If only CVR

required by

regulations

A

1 0 May be inoperative provided repairs are made within

three flight days.

a) Recorder

Independent

Power Supply

(RIPS)

(20292 and

Subs Post

SB 100-23-20)

***

C

1 0 (M)

3) If CVR not required

by regulations

D

- 0

a) Recorder

Independent

Power Supply

(RIPS)

(20292 and

Subs Post

SB 100-23-20)

***

D

1 0 (M)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 24-1

1.

2.

Nu

mber Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série article

3. Number Required For Dispatch

Nombre d

'art

icles à expédier

24 – ELECTRICAL POWER

4.

Remarks or Exceptions

Remarques ou exceptions

20-01 APU Generator

Channel

C

1 0 (M) May be inoperative provided:

a) APU generator is disabled, and

b) Engine Driven Generator Channels are

operative.

20-02 ELECTRICAL APU

GEN “ON” Switch

Light

(light function only)

C

1 0 (O)

30-01 ELECTRICAL L/R

BATT “OFF” Switch

Light

(light function only)

C

2 0

30-02 ELECTRICAL STBY

INST “OFF” Switch

Light

(light function only)

C

1 0

31-01 Engine Driven

Generator Channels

B

2 1 (M)(O) May be inoperative provided:

a) Affected generator is disabled,

b) APU is operative,

c) APU Generator Channel is operative and used

throughout flight,

d) Flight planning must consider additional fuel

burn for the APU, and

e) Operations are conducted at or below FL 300.

31-02 ELECTRICAL L/R

GEN “OFF” Switch

Light

(light function only)

C

2 0

31-03 Hydraulic Motor

Driven Generator

(HMDG) System

***

D

1 0 (M) May be inoperative provided system is deactivated. |

41-01 External Power

System

C

1 0

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

1 Page

BD-100-1A10 Date: Mar 24/05 24-2

1.

2.

Number Install

ed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de système/série article

3. Number Required For Dispatch

Nombre d'articles à expédier

24 – ELECTRICAL POWER

4.

Remarks or Exceptions

Remarques ou exceptions

41-02 ELECTRICAL EXT

PWR "AVAIL/ON"

Switch Light

(Pedestal)

(light function only)

C

1 0 (O)

41-03 EXTERNAL

POWER "AVAIL/IN

USE" Indicator

(Service Panel)

C

1 0

41-04 Ground Service

Power System

C

1 0 (O) May be inoperative provided ground service

contactor is verified open.

41-05 GND SERVICE

“ON” Switch Light

(light function only)

(Service Panel)

C

1 0

50-01 Bus Tie Contactors B

2 1 May be inoperative CLOSED.

50-02

ELECTRICAL BUS

TIE “-

” Switch Light

(light function only)

C

1 0 (O)

64-01 Auxiliary Buses

1) Left Auxiliary

Bus

C

1 0 (O)

(cont'd)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

1 Page

BD-100-1A10 Date: Mar 24/05 24-3

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série article

3. Number Required For Dispatch

Nombre d'articles à expédier

24 – ELECTRICAL POWER

4.

Remarks

or E

xceptions

Remarques ou exceptions

64-01 Auxiliary Buses

(Cont'd)

2) Right Auxiliary

Bus

B

1 0 (O) May be inoperative provided:

a) Passenger Address System is considered

inoperative (23-41-01),

b) Alerting System is considered inoperative

(23-41-02),

c) Pre-recorded Announcement System (if

installed) is considered inoperative (23-70-01),

d) Windshield & Side Window Heating System

right Side Window Heating Channel is

considered inoperative (30-41-01),

e) Cabin Lighting System is considered

inoperative (33-20-01),

f) Water System is considered inoperative

(38-00-01), and

g) Lavatory Waste System is considered

inoperative (38-30-01).

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

2 Page

BD-100-1A10 Date: Oct 28/08 24-4

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série article

3. Number Required For Dispatch

Nombr

e d'

articles à expédier

24 – ELECTRICAL POWER

4.

Remarks or Exceptions

Remarques ou exceptions

THIS PAGE INTENTIONALLY LEFT BLANK

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

2 Page

BD-100-1A10 Date: Oct 28/08 25-1

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série

ar

ticle

3. Number Required For Dispatch

Nombre d'articles à expédier

25 – EQUIPMENT/

4.

Remarks or Exceptions

FURNISHINGS Remarques ou exceptions

11-01 Pilot seats

1) Lumbar

supports

C

2 0 Any or all may be inoperative in the lowest position

provided seat is acceptable to the affected

crewmember.

2) Arm rests C

4 0 (M) Any or all may be inoperative or missing provided:

a) Affected armrest is secured in upright

position,

b) Egress is not impaired, and

c) Seat is acceptable to the affected crewmember.

3) Seat

adjustments

C

- - Vertical, recline, and fore/aft adjustment may be

inoperative provided seat is secured in a position to

meet individual pilot requirements.

11-02 Belted Toilet Seat

***

D

1 0 (O) May be inoperative provided it is not occupied.

NOTE: An inoperative seat belt renders the seat

inoperative for taxi, take-off, during

turbulence and landing.

11-03 Forward Pull Out In

Flight Seat

***

D

1 0 (M)(O) May be inoperative provided It is removed or

secured in the STOWED position.

NOTE: An inoperative seat belt renders the seat

inoperative for taxi, take-off, during

turbulence and landing.

13-01 Pilots Heated Mats

***

C

2 0 (M) Any or all may be inoperative provided affected mat

is deactivated.

14-01 Cockpit Sunvisors

1) Sunvisors

(Headliner)

C

2 0 Any or all may be inoperative (missing) provided

affected sunvisor does not obstruct either pilot’s field of

view for take-off and landing.

C

2 0 (O) Any or all may be inoperative provided affected

sunvisor is removed.

2) Glareshield

Retractable

Visors

C

2 0 (M) Any or all may be inoperative or missing provided

affected visor is secured in the retracted position or

removed.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

2 Page

BD-100-1A10 Date: Oct 28/08 25-2

1.

2.

N

umber Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série article

3. Number Required For Dispatch

Nombre d'

arti

cles à expédier

25 – EQUIPMENT/

4.

Remarks or Exceptions

FURNISHINGS Remarques ou exceptions

14-02 Control Wheel Chart

Holders

C

2 0 Any or all may be inoperative provided affected holder

does not impede associated crew member to perform

his duties.

14-03 Cockpit Writing

Tables

***

D

2 0 Any or all may be inoperative provided affected table

does not impede associated crew member to perform

his duties.

14-04 Lavatory Entry Area

Ashtray

B

1 0

14-05

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.

14-06 Cabin and Galley

Storage

Compartments/

Closets

C

- - (M) May be inoperative provided:

a) Procedures are established to secure

Compartment/Closets CLOSED,

b) Associated Compartment/Closets is

prominently placarded DO NOT USE,

c) Any emergency equipment located in affected

Compartment/Closets is considered

inoperative, and

d) Affected Compartment/Closets is not used for

storage of any item(s) except for those

permanently affixed.

(cont’d)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

2 Page

BD-100-1A10 Date: Oct 28/08 25-3

1

.

2.

Number

Installed

System

& S

equence N

o

Item

Nombre d’articles installés

N

o

de

système/série article

3. Number Required For Dispatch

Nombre d'articles à expédier

25 – EQUIPMENT/

4.

Remarks or Exceptions

FURNISHINGS Remarques ou exceptions

14-06 Cabin and Galley

Storage

Compartments/

Closets

(Cont’d)

C

- - (M)(O) May be inoperative provided:

a) Affected door(s) is removed,

b) Associated Compartment/Closets is not used

for storage of any items, except those

permanently affixed,

c) Associated Compartment/Closets is

prominently placarded DO NOT USE, and

d) Passengers are briefed that associated

compartment is not used.

NOTE : Any emergency equipment located in the

associated Compartment/Closets

(permanently affixed) is available for use.

1) Storage

Compartment

Key Locks

D

- 0 (M) May be inoperative in the unlocked position

provided doors can be secured by other means.

14-07 Passenger Seat Life

Vest Storage

Compartment

Panels

C

- - (O) May be inoperative (missing) provided:

a) Associated life vest is relocated and accessible

for affected passenger, while seated

b) Affected passenger is briefed about life vest

location.

C

- - May be inoperative (missing) provided:

a) Associated life vest is removed, and

b) Affected Passenger Seat is considered

inoperative (25-21-01).

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 25-4

1.

2.

Number Installed

Sys

tem & Sequence N

o

Item

Nombre d’articles installés

N

o

de système/série article

3. Number Required For Dispatch

Nombre d'articles à expédier

25 – EQUIPMENT/

4.

Remarks or Exceptions

FURNISHINGS Remarques ou exceptions

14-08 Lavatory Door

C

1 0 (M) May be inoperative provided:

a) Door is secured OPEN or CLOSED, and

b) Baggage compartment remains empty.

NOTE: Does not preclude the carriage of ballast.

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.

14-09 Life Jackets D

- - (O)(M) Any in excess of those required may be

inoperative or missing, provided:

a) Required distribution is maintained,

b) Inoperative lifejacket and its installed

location are placarded inoperative,

c) Inoperative life jacket is secured out of

sight, and

d) Procedures are established and used to

alert crew members of inoperative or

missing equipment.

|

14-10

Life Rafts

C

- - (O)(M) Any in excess of those required for the

intended flight may be inoperative or missing

for extended overwater flights provided:

a) Required distribution is maintained,

b) Inoperative life raft and its installed

location are placarded inoperative,

c) When practical, the inoperative life raft is

secured out of sight, and

d) Procedures are established and used to

alert crew members of inoperative or

missing equipment.

|

D

- - (O) May be inoperative or missing provided:

a) Extended overwater flights are not conducted,

and

b) Procedures are established and used to alert

crew members of inoperative or missing

equipment.

|

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 25-5

1.

2.

Num

ber

Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de système/série article

3. Number Required For Dispatch

Nombre d'articles à expéd

ier

25 – EQUIPMENT/

4.

Remarks or Exceptions

FURNISHINGS Remarques ou exceptions

21-01 Passenger Seats D

- - (M) May be inoperative provided:

a) Seat(s) does not block or restrict access to an

emergency exit,

b) Seat(s) does not restrict any passenger from

access to the main aisle, and

c) Affected seat(s) is not used and is blocked and

placarded "DO NOT OCCUPY".

NOTE1: A seat(s) with an inoperative seat belt is

considered inoperative.

NOTE2: Affected seat(s) may include the seat(s)

behind and/or adjacent outboard seats.

NOTE3: Seat(s) facing aft with an inoperative

(missing) headrest is considered

inoperative.

NOTE4: Seat provided with 3-rd Audio System is

covered by the MMEL Item 25-21-02

Passenger/ Observer Seat (including 3-rd

Audio System) ***

1) Recline

Mechanism

D

- - (M) May be inoperative and seat(s) occupied provided

seat(s) is secured in the up-right position.

|

2) Lazyboy Legrest

Mechanism

***

D

- - (M) May be inoperative and seat(s) occupied provided

legrest(s) is secured in stowed position.

|

(cont'd)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 25-6

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de système/série article

3. Number Required For Dispatch

Nombre d'articles à expé

dier

25 – EQUIPMENT/

4.

Remark

s or Exceptions

FURNISHINGS Remarques ou exceptions

21-01 Passenger Seats

(Cont'd)

3) Track/Swivel

Mechanism

***

D

- - (M) May be inoperative and seat(s) occupied provided:

a) Affected forward facing seat is secured in fully

aft, fully outboard, forward facing position, and

b) Affected aft facing seat is secured in fully

forward, fully outboard, aft facing position.

|

21-02 Observer Seat

***

1) Jump Seat

(Crew closet)

(including

associated

equipment)

***

B

1 0 (M) May be inoperative provided the seat is removed,

stowed, or secured in the retracted position.

NOTE: An inoperative seat belt renders seat

inoperative.

D

1 0 (M) May be inoperative provided:

a) Seat is removed, stowed, or secured in the

retracted position, and

b) Seat is not required to be occupied in an

official capacity for extended periods of time.

NOTE: An inoperative seat belt renders seat

inoperative.

2) Passenger/

Observer Seat

(including 3-rd

Audio System)

***

B

1 0 (M) May be inoperative provided the seat is not used

and is blocked and placarded "DO NOT OCCUPY".

NOTE: An inoperative seat belt renders seat

inoperative.

D

1 0 (M) May be inoperative provided:

a) Seat is not used and is blocked and placarded

"DO NOT OCCUPY", and

b) Seat is not required to be occupied in an

official capacity for extended periods of time.

NOTE: An inoperative seat belt renders seat

inoperative.

(cont’d)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 25-7

1.

2.

Number Installed

System

& S

equence N

o

Item

Nombre d’articles installés

N

o

de systè

me/série article

3. Number Required For Dispatch

Nombre d'articl

es à expédier

25 – EQUIPMENT/

4.

Remarks or Exce

ptions

FURNISHINGS Remarques ou exceptions

21-02 Observer Seat

***

(Cont’d)

2) Passenger/

Observer Seat

(including 3-rd

Audio System)

***

(Cont’d)

a) Recline

Mechanism

C

1 0 (M) May be inoperative and seat occupied provided

seat(s) is secured in the up-right position.

|

b) Lazyboy

Legrest

Mechanism

***

D

1 0 (M) May be inoperative and seat occupied provided

legrest is secured in stowed position.

|

c) Track/Swivel

Mechanism

***

D

1 0 (M) May be inoperative and seat occupied provided:

a) Affected forward facing seat is secured in fully

aft, fully outboard, forward facing position, and

b) Affected aft facing seat is secured in fully

forward, fully outboard, aft facing position.

|

3) Observer Seat

not required by

regulations

(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).

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

2 Page

BD-100-1A10 Date: Oct 28/08 25-8

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

sys

tème/série ar

ticle

3. Number Required For Dispatch

Nombre d'articles à expédier

25 – EQUIPMENT/

4.

Remarks or Exceptions

FURNISHINGS Remarques ou exceptions

50-01 Cargo Restraint

System

C

1 0 May be inoperative provided cargo compartment

remains empty.

1) Cabin Interior

Door Baggage

Net

C

1 0 May be inoperative or missing provided no baggage is

carried on the baggage compartment floor.

2) Baggage Shelf *** D

1 0 May be inoperative or missing provided shelf is not

used.

NOTE: An inoperative baggage shelf restraining net

renders shelf inoperative.

61-01 Emergency Locator

Transmitter

(ELT)

***

D

- - As required by Regulations.

62-01 Emergency Medical

Equipment

1) First Aid Kits 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, and

b) Procedures are established to alert crew

members of missing or incomplete kits.

2) First Aid Kit Seal

B

- - (O) The seal affixed on the exterior of the first aid kit

may be missing or inoperative provided:

a) First Aid Kit is fully equipped or the kit has a

maximum of one missing item that was used

after the flight left a base where the item could

be replaced,

b) First Aid Kit includes a list of its contents,

c) Inventory is taken on the content of the kit prior

to departure, and

d) Procedures are established to alert crew

members of the missing or broken seal.

(cont’d)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

2 Page

BD-100-1A10 Date: Oct 28/08 25-9

1.

2.

Number Insta

lled

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de système/série

a

rticle

3. Number Required For Dispatch

Nombre d'articles à expédier

25 – EQUIPMENT/

4.

Remarks or Exceptions

FURNISHINGS Remarques ou exceptions

62-01 Emergency Medical

Equipment

(Cont’d)

3) Automatic

External

Defibrillator

(AED) and/or

Associated

Equipment

B

- 0 (O) May be incomplete, missing or inoperative provided

AED is resealed in a manner that will identify it as a

unit that cannot be mistaken for a fully serviceable

unit.

D

- - Any in excess of those required by Regulations may be

incomplete, missing, or inoperative.

62-02 Flotation Equipment

(Crew and

Passengers)

D

- - As required by Regulations.

62-03 Flashlights/

Flashlight Holders

1) Flashlights C

- 0 (O) Any or all may be inoperative or missing provided

affected crew member has a flashlight of equivalent

characteristics readily available.

2) Holders C

- 0 (O) Any or all may be inoperative or missing provided

alternate stowage provisions are provided.

(cont'd)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 25-10

1.

2.

Number Inst

alled

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de système/série article

3. Number Required For Dispatch

No

mbre d'articles à expédier

25 – EQUIPMENT/

4.

Remarks

or Excepti

ons

FURNISHINGS Remarques ou exceptions

70-01 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. Items addressed elsewhere in this

document shall not be included.

(M) and (O) procedures may be required and included

in the air carrier's appropriate document.

NOTE1: Exterior lavatory door ash trays are not

considered convenience items.

NOTE2: 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”.

NOTE3: Movie equipment individual screens must be

capable of being stowed.

NOTE4: 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.

70-02 Lavatory Waste Bin C

- 0 (M) May be inoperative provided:

a) Associated Lavatory Waste Bin is empty, and

b) Associated Lavatory Waste Bin is secured

closed, and placarded DO NOT USE.

|

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

2 Page

BD-100-1A10 Date: Oct 28/08 25-11

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de système/série article

3. Number Required For Dispatch

Nombre d'articles à expédier

25 – EQUIPMENT/

4.

Remarks or Exceptions

FURNISHINGS Remarques ou exceptions

THIS PAGE INTENTIONALLY LEFT BLANK

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 26-1

1.

2.

Number Installed

System & Sequence

N

o

Item

Nombre d’articles installés

N

o

de système/série articl

e

3. Number Required For Dispatch

Nom

bre d'articles

à expédier

26 – FIRE PROTECTION

4.

Remarks or Exceptions

Remarques ou exceptions

11-01 FIREX System C

1 1 System redundancy may be degraded as indicated by

“FIRE SYS FAULT” advisory message.

NOTE: All FIREX System failures causing “FIRE

SYS FAULT” advisory message must be

repaired within 10 days after appearance of

this message on EICAS.

11-02 FIREX Control Unit

ARINC

Communication

B

1 0 (O) May be inoperative provided FIRE DET test is

performed before each flight.

13-01 APU Fire Detection

Subsystem

C

1 0 May be inoperative provided APU is considered

inoperative (49-11-01).

C

1 0 (M) May be inoperative for ground operations only

provided:

a) APU access panel is opened,

b) APU is continuously visually monitored, and

c) APU is shut down before taxi.

|

14-01 Main Landing Gear

Bay Overheat

Detection

Subsystem

B

1 0 May be inoperative provided:

a) Landing gear is left extended for a minimum of

5 minutes after takeoff,

b) Takeoff performance is in accordance with the

AFM Supplement, Supplement 2 -

Supplemental information for the MMEL (Flight

with Landing Gear Down).

c) Takeoff is not conducted in icing conditions,

and

d) Short Field Operations (Supplement 11) are not

conducted.

NOTE: 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.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 26-2

1.

2.

Number Installed

System & Se

quence N

o

Item

Nombre d’articles installés

N

o

de système/série article

3. Number Required For Dispatch

Nombr

e d'

articles à ex

pédier

26 – FIRE PROTECTION

4.

Remarks or Exceptions

Remarques ou exceptions

15-01 Baggage

Compartment

Smoke Detection

Subsystem

C

1 0 May be inoperative provided baggage compartment

remains empty.

NOTE: Does not preclude the carriage of ballast.

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.

21-01 APU Fire

Extinguishing

Subsystem

C

1 0 May be inoperative provided APU is considered

inoperative (49-11-01).

C

1 0 (M) May be inoperative for ground operations only

provided:

a) APU access panel is opened,

b) APU is continuously visually monitored, and

c) APU is shut down before taxi.

|

23-01 Portable Fire

Extinguishers

D

- - (M)(O) Any in excess of those required by Regulations

may be inoperative or missing provided:

a) Inoperative fire extinguisher is removed from

the passenger cabin or flight compartment 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, and

c) Procedures are established to alert crew

members of missing or inoperative fire

extinguishers.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 27-1

1.

2.

Number

Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de système/série

article

3. Number Required For Dispatch

Nombre d

'ar

ticles à expédier

27 – FLIGHT CONTROLS

4

.

Remarks or Exceptions

Remarques ou exceptions

10-01 EICAS Aileron

Control Surface

Position Indications

C

2 0 (O) Any or all may be inoperative provided the affected

control surface is visually checked for full, free and

correct movement before each flight.

20-01 EICAS Rudder

Control Surface

Position Indication

C

1 0 (O) May be inoperative provided:

a) Rudder Pedal Adjustment Systems are

operative, and

b) Control surface is visually checked for full, free

and correct movement before each flight.

20-02 Rudder Pedal

Adjustment Systems

C

2 0 (M)(O) Any or all may be inoperative provided:

a) Actuators are deactivated,

b) EICAS Rudder Control Surface Position

Indication is operative,

c) Pedals position is acceptable to the affected

crewmember, and

d) Rudder and brake pedals are checked for full

and unrestricted movement at both pilot

stations.

32-02 STALL PUSHER

“OFF” Switch Light

(light function only)

C

1 0

41-01 Pitch Trim System

Deleted, Revision 6. |

60-01 Spoiler System

1) Ground Lift

Dumping AUTO

Function

C

1 0 (O) May be inoperative provided:

a) GND SPOILERS rotary selector switch is

selected to MANUAL ARM before each take off

and landing, and

b) GND SPOILERS rotary selector switch is

selected to OFF after each landing.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

1 Page

BD-100-1A10 Date: Mar 24/05 27-2

1.

2.

Numbe

r I

nstalled

System & Sequence N

o

Ite

m

Nombre d’articles installés

N

o

de système/série

article

3. Number Required For Dispatch

Nombre d'articles à expédier

27 – FLIGHT CONTROLS

4.

Remarks or Exceptions

Remarques ou exceptions

61-01 ROLL SPOILERS

“OFF” Switch Light

(light function only)

C

1 0

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 28-1

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

d

e

système/série

article

3. Number Required For Dispatch

Nomb

re d'articles à expédier

28 – FUEL

4.

Remarks or Exceptions

Remarques ou exceptions

11-01 Gravity Filler Caps C

2 0 (M)(O) May be inoperative CLOSED provided:

a) There is no fuel leakage from affected Gravity

Filler Cap, and

b) Pressure Refueling System is operative.

|

21-01 APU Fuel SOV C

1 0 (M) May be inoperative provided:

a) Valve is deactivated CLOSED, and

b) APU is considered inoperative (49-11-01).

|

21-02 L & R Fuel Boost

Pumps

A 2 1 (M)(O) May be inoperative provided:

a) Inoperative Boost Pump is selected to OFF,

b) Inoperative Boost Pump is deactivated,

c) Both primary feed ejectors are verified

operative,

d) Transfer (XFER) Valve is verified operative,

e) Gravity cross-flow (XFLOW) valve is verified

operative,

f) Operations are conducted at or below

18500 ft,

g) Bulk Fuel Temperature before takeoff is below

or equal to 25

o

C (77

o

F),

h) Aircraft has fuel of types Jet A or Jet A1,

i) A minimum fuel quantity of 2000 lbs per wing

(4000 lbs total) is required for landing and any

fuel quantity below this value is considered

unusable.

j) Cross-side Fuel Boost Pump AUTO function is

verified operative,

k) Operations are conducted within one hour from

a suitable airport, and

l) Repairs are made within one flight day.

21-03 L & R Fuel Boost

Pumps Auto

Function

1) L Fuel Boost

Pump AUTO

Function

C 1 0

May be inoperative provided FUEL L PUMP rotary

selector switch is selected to ON before left engine

start and selected to OFF after engine started.

(cont’d)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

3 Page

BD-100-1A10 Date: Jun 21/11 28-2

1.

2.

Number Instal

led

Syste

m & Sequence N

o

Item

Nombre d’articles installés

N

o

d

e

système/série

article

3. Number Required For Dispatch

Nombre d'articles à expédi

er

28 – FUEL

4.

Remarks o

r Exceptions

Remarques ou exceptions

21-03 L & R Fuel Boost

Pumps Auto

Function

(Cont’d)

2) R Fuel Boost

Pump AUTO

Function

C 1 0 May be inoperative provided:

a) FUEL R PUMP rotary selector switch is

selected to ON before right engine start and

selected to OFF after engine started, and

b) FUEL R PUMP rotary selector switch is

selected to ON before APU start and selected

to OFF after right engine started or APU shut

down.

22-01 XFER Valve

C

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

a) Valve is deactivated CLOSED,

b) Gravity XFLOW Valve is verified operative, and

c) Operations are conducted within one hour from

a suitable airport.

22-02 FUEL XFER “-”

Switch Light

(light function only)

C

1 0

22-03 FUEL GRAVITY

XFLOW “-” Switch

Light

(light function only)

C

1 0

22-04 Gravity XFLOW Valve

C

1 0 (M) May be inoperative provided:

a) Valve is deactivated CLOSED,

b) XFER Valve is verified operative, and

c) Operations are conducted within one hour from

a suitable airport.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 28-3

1.

2.

Number Installed

Sys

tem

& Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série article

3. Number Required For Dispatch

Nombre d'articles à expédier

28 – FUEL

4

.

Re

ma

r

ks or Exceptions

Remarques ou exceptions

23-01 Pressure Refueling

System

(Refuel/Defuel

Control Panel)

C

1 0 (O) May be inoperative provided gravity refueling

procedure is used.

1) Automatic

Mode

C

1 0 (O) May be inoperative provided Manual Mode is

operative.

2) Manual Mode C

1 0 (O) May be inoperative provided Automatic Mode is

operative.

3) Fuel Quantity

Display

Indications (Left

and Right)

C

2 0 (O) Any or all may be inoperative provided Manual

Mode is operative and used.

23-02 Refuel/Defuel

Valves

C

2 0 (M) Any or all may be inoperative provided:

a) Valves are deactivated,

b) Affected valve is verified CLOSED, and

c) Gravity refueling procedure is used.

23-03 Pressure Relief

Valves

C

2 0 (M) Any or all may be inoperative provided:

a) Affected valve is verified CLOSED, and

b) Pressure Refueling System Manual Mode is

operative and used.

|

C

2 0 (M) Any or all may be inoperative provided:

a) Affected valve is verified CLOSED, and

b) Gravity refueling procedure is used for the

affected tank.

|

23-04 Refuel/Defuel

Adapter Cap

C

1 0 (M) May be inoperative (missing) provided:

a) Refuel/defuel adapter is visually checked for

contamination before each pressure refueling,

b) Check valve is verified CLOSED after each

pressure refueling, and

c) Refuel/Defuel SOVs are verified CLOSED after

each pressure refueling.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

3 Page

BD-100-1A10 Date: Jun 21/11 28-4

1.

2.

N

umber Inst

alled

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série

article

3. Number Required For Dispatch

Nombre d'articles à expédier

28 – FUEL

4.

Remarks or Exceptions

Remarques ou exceptions

40-01 EICAS Bulk Fuel

Temperature

Indication System

C

1 0 (M) May be inoperative provided fuel temperature is

verified to be within limits before each flight.

41-01

High Level Sensors

C

2 0 (O) Any or all may be inoperative provided:

a) Pressure Refueling System Manual Mode is

operative and used, and

b) Maximum allowed fuel quantity in each tank is

limited to 5500 lbs (2500 kg).

C

2 0 (O) Any or all may be inoperative provided gravity

refueling procedure is used for the affected tank.

NOTE: Refer to AFM fuel limitations for the maximum

usable fuel load when using gravity refueling.

41-02 Fuel Quantity

Gauging Computer

Channels

C

2 1 May be inoperative provided Fuel Used Readout is

operative.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 29-1

1.

2.

Number Installed

System & Sequence N

o

It

em

Nombre d’articles installés

N

o

de

système/série article

3. Number Required For Dispatch

Nombre d'article

s à expédier

29 – HYDRAULIC POWER

4.

Remarks or Exceptions

Remarques ou exceptions

11-01 HYDRAULIC L/R

SOV “CLOSED”

Switch Light

(light function only)

C

2 0

11-02 Hydraulic Shut off

Valve (SOV) EICAS

Synoptic Page

Indications

C

2 0

(O)(M) One or both EICAS Synoptic HYD SOV icons

(SOV circular outline) may be amber or

magenta coloured, provided that prior to each

dispatch:

a) Associated valve is visually verified to

operate fully OPEN and fully CLOSED

positions,

b) Confirm associated hydraulic pressure

shows correct pressure, with the engine

operating and DCMP selected OFF,

c) Associated valve confirmed in the OPEN

position for takeoff, and

d) Associated hydraulic quantity, pressure and

temperature on the Synoptic Page, is

checked periodically during flight.

NOTE 1: Amber coloured HYD SOV circular outline will

be accompanied by respective HYD SOV

FAIL Caution message.

|

12-01 L & R DC Motor

Pumps

(DCMP)

1) AUTO Function

(Aircraft 20003 to

20190 without

SB 100-29-11)

C

2 0

2) AUTO Function

(Aircraft 20003 to

20190 with

SB 100-29-11)

Aircraft 20191

and subs.

C

2 0

(O) Any or all may be inoperative provided affected

pump HYDRAULIC L/R PUMP rotary selector switch is

selected to ON before each take-off and approach.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

5 Page

BD-100-1A10 Date: Apr 28/19 29-2

1.

2.

Numb

er

Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série article

3. Number Required For Dispatch

Nombre d'articles à expédi

er

29 – HYDRAULIC POWER

4.

Remarks or E

xceptions

Remarques ou exceptions

12-01 L & R DC Motor

Pumps

(DCMP)

3) AUTO Function

(Aircraft 20003 to

20190 without

SB 100-29-11)

C

2 0

4) AUTO Function

(Aircraft 20003 to

20190 with

SB 100-29-11)

Aircraft 20191

and subs.

C

2 0

(O) Any or all may be inoperative provided affected

pump HYDRAULIC L/R PUMP rotary selector switch is

selected to ON before each take-off and approach.

12-02 Power Transfer

System

C

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

a) Power transfer unit selector valve is

deactivated CLOSED,

b) Takeoff performance is in accordance with the

AFM Supplement 2 – Supplemental

information for the MMEL (Flight with Landing

Gear Down), and

c) Steep approach (Supplement 10) or Short

Field Operations (Supplement 11) are not

conducted.

NOTE: Only take-off and climb performance penalties

for Landing Gear Down apply.

1) AUTO Function C

1 0 May be inoperative provided:

a) HYDRAULIC PTU rotary selector switch is

selected to ON before each take off and

selected to OFF during each climb, and

b) HYDRAULIC PTU rotary selector switch is

selected to ON before each approach and

selected to OFF after each landing.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

3 Page

BD-100-1A10 Date: Jun 21/11 29-3

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série article

3. Number Required For Dispatch

Nombre d'articles à ex

pédier

29 – HYDRAULIC POWER

4.

Remarks or Excepti

ons

Remarques ou exceptions

31-01 EICAS L & R

Hydraulic Pressure

Readouts

C

2 0 (O) Any or all may be inoperative provided DCMP Low

Pressure Switch and EDP Low Pressure Switch on the

affected side are verified operative.

31-02 L & R Hydraulic

Pump Low Pressure

Switches

1) DCMP Low

Pressure

Switches

C

2 0 (O) Any or all may be inoperative provided:

a) EDP Low Pressure Switch on the affected side

is operative,

b) Affected hydraulic pump is verified operative

before each flight, and

c) EICAS Hydraulic Pressure Readout and

Hydraulic Reservoir Quantity Readout in the

affected system are operative and monitored

during flight.

2) EDP Low

Pressure

Switches

C

2 0 (O) Any or all may be inoperative provided:

a) DCMP Low Pressure Switch on the affected

side is operative,

b) Affected hydraulic pump is verified operative

before each flight, and

c) EICAS Hydraulic Pressure Readout and

Hydraulic Reservoir Quantity Readout in the

affected system are operative and monitored

during flight.

NOTE: When aircraft is dispatched with right EDP

Low Pressure Switch inoperative, flaps will

operate at low rate.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

Original Page

BD-100-1A10 Date: Sep 30/03 29-4

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de syst

ème

/sér

ie

article

3. Number Required For Dispatch

Nombre d'articles à expédier

29 – HYDRAULIC POWER

4.

Remarks or Exceptions

Remarques ou exceptions

32-01 EICAS Hydraulic

Reservoir Quantity

Readouts

1) L & R C

2 0 (O) Any or all may be inoperative provided:

a) Hydraulic Reservoir Quantity Gauge in the

affected system is operative,

b) Quantity in associated reservoir is verified

adequate on respective Hydraulic Reservoir

Quantity Gauge before each flight, and

c) Hydraulic Pump Low Pressure Switches

(DCMP and EDP) on the affected side are

operative.

2) AUX

C

1 0 (O) May be inoperative provided:

a) AUX Hydraulic Reservoir Quantity Gauge is

operative, and

b) Quantity in auxiliary system reservoir is verified

adequate on AUX Hydraulic Reservoir Quantity

Gauge before each flight.

32-02 Hydraulic Reservoir

Quantity Gauges

1) L & R C

2 0 Any or all may be inoperative provided EICAS

Hydraulic Reservoir Quantity Readout in the affected

system is operative.

2) AUX

C

1 0 May be inoperative provided AUX EICAS Hydraulic

Reservoir Quantity Readout is operative.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

Original Page

BD-100-1A10 Date: Sep 30/03 29-5

1.

2.

Numb

er Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de systèm

e/série article

3. Number Required For Dispatch

Nombre d'articles à expédier

29 – HYDRAULIC POWER

4

.

Remarks or

Exc

epti

on

s

Remarques ou exceptions

THIS PAGE INTENTIONALLY LEFT BLANK

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 30-1

1.

2.

Number Instal

led

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série article

3. Number Required For Dispatch

Nomb

re d

'a

r

ticles à expédi

er

30 – ICE AND RAIN

4.

Remarks or Exceptions

PROTECTION Remarques ou exceptions

10-01 High Pressure

Valves (HPV)

C

2 0 (M) Any or all may be inoperative provided:

a) Affected valve is secured CLOSED,

b) ANTI-ICE WING switch is selected OFF,

c) Operations are not conducted in known or

forecast icing conditions, and

d) One Ice Detection System is operative.

|

10-02 Anti-Ice Bleed

Pressure Indication

Systems

C

2 0 Any or all may be inoperative provided:

a) ANTI-ICE WING switch is selected OFF,

b) Operations are not conducted in known or

forecast icing conditions, and

c) One Ice Detection System is operative.

10-03 Wing Anti-Ice

Valves (WAIV)

C

2 0 (M) Any or all may be inoperative provided:

a) Affected valve is secured CLOSED,

b) ANTI-ICE WING switch is selected OFF,

c) Operations are not conducted in known or

forecast icing conditions, and

d) One Ice Detection System is operative.

|

10-04 Wing Isolation Valve

(CBW)

C

1 0 May be inoperative provided:

a) ANTI-ICE WING switch is selected OFF,

b) Operations are not conducted in known or

forecast icing conditions, and

c) One Ice Detection System is operative.

10-05

ANTI-ICE WING

“ON” Switch Light

(light function only)

C

1 0

10-06

Engine Anti-Ice

Valves

C

2 1 (O) May be inoperative CLOSED provided:

a) Operations are not conducted in known or

forecast icing conditions, and

b) One Ice Detection System is operative.

(Cont’d)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 30-2

1.

2.

Numbe

r I

ns

talled

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de syst

ème/série article

3. Number Required For Dispatch

Nombre d'articles à e

xpédie

r

30 – ICE AND RAIN

4.

Remarks or Exceptions

PROTECTION Remarques ou exceptions

10-06 Engine Anti-Ice

Valves

(Cont’d)

C

2 1 (O) May be inoperative OPEN provided:

a) Affected engine ITT margin is checked before

each take-off,

b) Operations are conducted in accordance with

AFM Performance data for engine anti-ice ON,

and

c) Operations are prohibited with Outside Air

Temperature (OAT) above 10°C.

|

10-07 Engine Anti-Ice TT2

Probe Heaters

C

2 1 (O) May be inoperative provided:

a) Operations are not conducted in known or

forecast icing conditions, and

b) One Ice Detection System is operative.

10-08 Engine Anti-Ice Low

Pressure Switches

C

2 1 (O) May be inoperative provided:

a) Operations are conducted in accordance with

AFM Performance data for engine anti-ice ON,

b) Operations are not conducted in known or

forecast icing conditions, and

c) One Ice Detection System is operative.

10-09 ANTI-ICE ENG

L & R “ON” Switch

Lights

(light function only)

C

2 0

11-01 Wing Anti-Ice

Temperature

Sensors

C

4 0 Any or all may be inoperative provided:

a) ANTI-ICE WING switch is selected OFF,

b) Operations are not conducted in known or

forecast icing conditions, and

c) One Ice Detection System is operative.

1) Outboard Wing

Anti-Ice

Temperature

Sensor

Elements

C

4 2 (M) One sensor element per sensor may be inoperative

provided Anti-Ice Bleed Pressure Indication

Systems operational status is verified before each

flight.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 30-3

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de système/série article

3. Number Required For Dispatch

N

ombre d'articles à expédier

30 – ICE AND RAIN

4.

Remarks

or Exceptions

PROTECTION Remarques ou exceptions

31-01 Air Data Probe

Heating System

1) Pitot/Static

Probe & Base

Heaters

a) Aircraft

20003 to

20500 with

SB 100-34-

38 and

aircraft

20501 and

Subs

B

4 2 (M) Except where enroute operations require its use,

same side Probe and/or Base Heaters may be

inoperative provided:

a) Affected heater is deactivated,

b) Standby Pitot Probe Heater is operative,

c) Operations are not conducted in visible

moisture (including standing water and slush) in

any form,

d) Operations are not conducted in known or

forecast icing conditions,

e) One Ice Detection System is operative, and

f) Operations are conducted in day VMC

conditions only.

b) Aircraft

20003 to

20500

without SB

100-34-38

A

4 2 (M) Except where enroute operations require its use

same side Probe and/or Base Heaters may be

inoperative provided:

a) Affected heater is deactivated,

b) Standby Pitot Probe Heater is operative,

c) Operations are not conducted in visible

moisture (including standing water and slush) in

any form,

d) Operations are not conducted in known or

forecast icing conditions,

e) One Ice Detection System is operative,

f) Operations are conducted in day VMC

conditions only, and

g) Repairs are made within one flight day.

(Cont’d)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 30-4

1.

2

.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

sy

stè

me/

série

article

3. Number Required For Dispatch

Nombre d'ar

ticles à expédier

30 – ICE AND RAIN

4.

Remarks or Exceptions

PROTECTION Remarques ou exceptions

31-01 Air Data Probe

Heating System

(Cont’d)

2) Standby Pitot

Probe Heater

a) Aircraft

20003 to

20500 with

SB 100-34-

38 and

aircraft

20501 and

Subs

B

1 0 (M) Except where enroute operations require its use

may be inoperative provided:

a) Heater is deactivated,

b) Pitot/Static Probe & Base Heaters are

operative,

c) Operations are not conducted in visible

moisture (including standing water and slush)

in any form,

d) Operations are not conducted in known or

forecast icing conditions,

e) One Ice Detection System is operative, and

f) Operations are conducted in day VMC

conditions only.

b) Aircraft

2003 to

20500

without SB

100-34-38

A

1 0 (M) Except where enroute operations require its use

may be inoperative provided:

a) Heater is deactivated,

b) Pitot/Static Probe & Base Heaters are

operative,

c) Operations are not conducted in visible

moisture (including standing water and slush)in

any form,

d) Operations are not conducted in known or

forecast icing conditions,

e) One Ice Detection System is operative,

f) Operations are conducted in day VMC

conditions only, and

g) Repairs are made within one flight day.

(Cont’d)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 30-5

1.

2.

Number Installed

Sys

tem

&

Sequenc

e N

o

Item

Nombre d’articles installés

N

o

de système/sér

ie article

3. Number Required For Dispatch

Nombre d'articles à expédier

30 – ICE AND RAIN

4.

Remarks or Exceptions

PROTECTION Remarques ou exceptions

31-01 Air Data Probe

Heating System

(Cont’d)

3) Static Port

Heaters

a) Aircraft

20003 to

20500 with

SB 100-34-

38 and

aircraft

20501 and

Subs

B

2 1 (M) Except where enroute operations require its use,

may be inoperative provided:

a) Affected heater is deactivated,

b) Operations are not conducted in visible

moisture (including standing water and slush)

in any form,

c) Operations are not conducted in known or

forecast icing conditions,

d) One Ice Detection System is operative, and

e) Operations are conducted in day VMC

conditions only.

b) Aircraft

20003 to

205000

without SB

100-34-38

A

2 1 (M) Except where enroute operations require its use,

may be inoperative provided:

a) Affected heater is deactivated,

b) Operations are not conducted in visible

moisture (including standing water and slush)

in any form,

c) Operations are not conducted in known or

forecast icing conditions,

d) One Ice Detection System is operative,

e) Operations are conducted in day VMC

conditions only, and

f) Repairs are made within one flight day.

(Cont’d)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 30-6

1.

2.

Nu

mber Installed

System &

Se

que

nce N

o

Item

Nombre d’articles installés

N

o

de système/série

article

3. Number Required For Dispatch

Nombre d'articles à expédier

30 – ICE AND RAIN

4

.

Re

ma

r

ks or Exceptions

PROTECTION Remarques ou exceptions

31-01 Air Data Probe

Heating System

(Cont’d)

4) AOA Sensor

Vane & Case

Heaters

B

4 2 (M) Same side Vane and/or Case Heaters may be

inoperative provided:

a) Affected heater is deactivated,

b) Operations are not conducted in visible

moisture (including standing water and slush)

in any form,

c) Operations are not conducted in known or

forecast icing conditions,

d) One Ice Detection System is operative, and

e) Operations are conducted in day VMC

conditions only.

5) TAT Sensor

Heater

B

1 0 (M) May be inoperative provided:

a) Heater is deactivated,

b) Operations are not conducted in visible

moisture (including standing water and slush)

in any form,

c) Operations are not conducted in known or

forecast icing conditions,

d) One Ice Detection System is operative, and

e) Operations are conducted in day VMC

conditions only.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 30-7

1.

2.

Num

ber Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de système/série art

icle

3. Number Required For Dispatch

Nombre d'artic

les à expé

dier

30 – ICE AND RAIN

4

.

R

emarks

or Exceptions

PROTECTION Remarques ou exceptions

31-02 ANTI-ICE L/R

PROBES “OFF

Switch Light

(light function only)

C

2 0

40-01 Drain Mast Heaters C

2 0 (M) Any or all may be inoperative provided:

a) Heaters are deactivated,

b) Water System is considered inoperative

(38-00-01),

c) Galley ice drawers remain empty, and

d) Lavatory sink and galley drip tray (sink) are

placarded “INOPERATIVE – DO NOT USE”.

41-01 Windshield & Side

Window Heating

System

1) Windshield

Heating

Channels

C

2 1 (M) May be inoperative provided:

a) Affected channel is deactivated,

b) Operations are not conducted in known or

forecast icing conditions, and

c) One Ice Detection System is operative.

C

2 0 (M) Any or all may be inoperative provided:

a) Affected channel is deactivated,

b) Side Window Heating Channels are operative,

c) Operations are not conducted in known or

forecast icing conditions, and

d) One Ice Detection System is operative.

2) Side Window

Heating

Channels

C

2 1 (M) Right may be inoperative provided:

a) Channel is deactivated, and

b) One Windshield Heating Channel is operative.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 30-8

1.

2.

Number Installed

System & Sequence

N

o

Item

Nombre d’articles installés

N

o

de système/série article

3. Number Required For Dispatch

Nombre d'articles à expédier

30 – ICE AND RAIN

4.

Rem

arks or Exceptions

PROTECTION Remarques ou exceptions

80-01 Ice Detection

Systems

C

2 1 (M) May be inoperative provided:

a) Affected detector is deactivated,

b) Anti-ice systems are turned ON when icing

conditions exist as defined in AFM.

C

2 0 (M) Any or all may be inoperative for day operations

provided:

a) Affected detector is deactivated,

b) Anti-ice systems are turned ON when icing

conditions exist as defined in AFM.

C

2 0 (M) Any or all may be inoperative for night operations

provided:

a) Affected detector is deactivated,

b) Anti-ice systems are turned ON when SAT is

between +10 C and –40 C.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

2 Page

BD-100-1A10 Date: Oct 28/08 31-1

1

.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de système/sér

ie

a

r

ticle

3. Number Required For Dispatch

Nombre

d'article

s à expédier

31 – INDICATING/

4.

R

emarks or Exceptions

RECORDING SYSTEMS Remarques ou exceptions

21-01 Clock

C

1 0 May be inoperative provided a reliable and functioning

timepiece is readily available to all flight compartment

crew members.

1) Universal Time

Co-ordination

Display (UTC)

C

1 0

2) Flight Time (FT)

C

1 0

3) Chronometer

(CHR)

C

1 0 (O) May be inoperative provided alternate procedures

are established and used to determine elapsed time.

4) LCD Display

Segments / Mode

(Annuns.)

C

- - Individual segments or annunciations may be

inoperative provided flight crews can readily determine

mode of operation.

31-01 Flight Data Recorder

(FDR)

***

1) If CVR and FDR

are required by

regulations

A

1 0 (O) May be inoperative provided:

a) Cockpit voice recorder is verified operative,

and

b) Repairs are made within three flight days.

2) If only FDR

required by

regulations

A

1 0 May be inoperative provide repairs are made within

three flight days.

3) DFDR Recording

Parameters

required by

Regulations

A

- - May be inoperative provided:

a) Cockpit voice recorder is operative, and

b) Repairs are made within twenty calendar days.

4) DFDR Recording

Parameters not

required by

Regulations

A

- - May be inoperative provided repairs are made before

the completion of the next heavy maintenance visit

5) If not required by

regulations

D

1 0

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 31-2

1.

2.

Number Installed

System & Seq

uence N

o

Item

Nombre d’articles installés

N

o

de système/série article

3. Number Required For Dispatch

N

o

mbre d'articles à expédier

31 – INDICATING/

4.

R

emarks or Exceptions

RECORDING SYSTEMS Remarques ou exceptions

31-02

Quick Access

Recorder (QAR)

***

C

1 0

(O) (M) May be inoperative for Flight Data Monitoring

(FDM) purposes, provided approved alternate

procedures, if appropriate to the FDM program, are

established and used.

|

D

1 0 May be inoperative provided procedures do not require

its use.

|

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

2 Page

BD-100-1A10 Date: Oct 28/08 31-3

1.

2.

Number Installed

System & Sequence N

o

I

tem

Nombre d’articles installés

N

o

de systè

me/série

article

3. Number Required For Dispatch

Nombre d'articles à expédier

31 – INDICATING/

4.

Remarks or Exceptions

RECORDING SYSTEMS Remarques ou exceptions

41-01 Cursor Control Panel

(CCP)

(Aircraft with Single

CCP)

(Aircraft 20000 to

20124)

1) L/R Toggle

Switch

C

1 0 May be inoperative with CCP control active for right

MFD provided right MFD is operative.

C

1 0 May be inoperative with CCP control active for left

MFD.

2) Joystick C

1 0 May be inoperative provided:

a) Electronic Checklist is considered inoperative

(31-60-01), and

b) Maintenance Diagnostic Computer is

considered inoperative (45-45-01).

3) CKLST

Pushbutton

C

1 0 May be inoperative provided Electronic Checklist is

considered inoperative

(31-60-01).

4) SKIP

Pushbutton

C

1 0

5) FRMT

Pushbutton

C

1 0 May be inoperative provided Maintenance Diagnostic

Computer is considered inoperative (45-45-01).

NOTE: Plan Map will not be available unless PLAN

pushbutton is installed and operative.

6) TFC

Pushbutton

C

1 0 May be inoperative provided Maintenance Diagnostic

Computer is considered inoperative (45-45-01).

7) TR/WX

Pushbutton

C

1 0 May be inoperative provided Maintenance Diagnostic

Computer is considered inoperative (45-45-01).

8) ENTER

Pushbutton

C

1 0 May be inoperative provided:

a) Electronic Checklist is considered inoperative

(31-60-01), and

b) Maintenance Diagnostic Computer is

considered inoperative (45-45-01).

(cont'd)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 31-4

1.

2.

Number Installed

System & Sequence N

o

It

em

Nombre d’articles installés

N

o

de sys

tème/série article

3. Number Required For Dispatch

Nombre d'articles à expédier

31 – INDICATING/

4.

Remarks or Exceptions

RECORDING SYSTEMS Remarques ou exceptions

41-01 Cursor Control Panel

(CCP)

(Aircraft with Single

CCP)

(Aircraft 20000 to

20124)

(Cont’d)

9) AUTO

Pushbutton

D

1 0

10) PLAN

Pushbutton

D

1 0

11) SHLDR

Pushbutton

D

1 0

12) SIDE

Pushbutton

D

1 0

41-02 Cursor Control Panel

(CCP)

(Aircraft with dual

Cursor Control

Panel)

(Aircraft 20125 and

up)

C

2 1 (O) Right side may be inoperative.

1) Joystick C

2 1

C

2 0 May be inoperative provided:

a) Maintenance Diagnostic Computer

(45-45-01) is considered inoperative,

b) Electronic Checklist (31-60-01) is considered

inoperative,

c) If installed, XM Graphical Weather function

(46-10-01) is considered inoperative, and

d) If installed, Electronic Charts (46-10-01) are

considered inoperative.

|

(cont'd)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 31-5

1.

2.

Number

Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de système/série article

3. Number Required For Dispatch

Nombre

d'a

rticles à expédier

31 – INDICATING/

4.

Remarks or Exceptions

RECORDING SYSTEMS Remarques ou exceptions

41-02 Cursor Control Panel

(CCP)

(Aircraft with dual

Cursor Control

Panel)

(Aircraft 20125 and

up)

(Cont’d)

2) JSTK

Pushbuttons

C

2 0

3) MEM

Pushbuttons

D

6 0

4) CHART

Pushbuttons

C

2 1

C

2 0 May be inoperative provided Electronic Charts

(46-10-01) if installed, are considered inoperative.

|

5) ZOOM

Pushbuttons

C

2 1

C

2 0 May be inoperative provided:

a) If installed, XM Graphical Weather function

(46-10-01) is considered inoperative, and

b) If installed, Electronic Charts (46-10-01) are

considered inoperative.

|

6) Orient

Pushbuttons

(located

under the

CHART

pushbutton)

C

2 1

C

2 0 May be inoperative provided:

a) If installed, XM Graphical Weather function (46-

10-01) is considered inoperative, and

b) If installed, Electronic Charts

(46-10-01) are considered inoperative.

|

7) LWR FRMT

Pushbuttons

C

2 0 (O)

(cont’d)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

2 Page

BD-100-1A10 Date: Oct 28/08 31-6

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série article

3. Number Required For Dispatch

Nombre d'articles à expédier

31 – INDICATING/

4.

Re

marks or E

xceptions

RECORDING SYSTEMS Remarques ou exceptions

41-02 Cursor Control Panel

(CCP)

(Aircraft with dual

Cursor Control Panel)

(Aircraft 20125 and

up)

(Cont’d)

8) UPR MENU

Pushbuttons

C

2 1

9) LWR MENU

Pushbuttons

C

2 1

10) ESC

Pushbuttons

C

2 0

11) PUSH

SELECT

Pushbuttons

(Menu)

C

2 1

12) MENU ADV

knobs

C

2 1

13) DATA knobs

(Menu)

C

2 1

14) TFC

Pushbuttons

C

2 0 (O)

15) TR/WX

Pushbuttons

C

2 0

16) ELEC

Pushbuttons

C

2 0

17) FLT

Pushbuttons

C

2 0

NOTE: The Flight Control System (FCS) diagnostics

page may not be accessible.

18) HYD

Pushbutton

C

2 0

(cont’d)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 31-7

1.

2.

Nu

mber Installed

System & Seque

nce

N

o

Item

Nombre d’articles installés

N

o

de système/série article

3. Number Required For Dispatch

Nombre

d'arti

cles à

exp

édier

31 – INDICATING/

4.

Re

mark

s

o

r Exceptions

RECORDING SYSTEMS Remarques ou exceptions

41-02 Cursor Control Panel

(CCP)

(Aircraft with dual

Cursor Control Panel)

(Aircraft 20125 and

up)(Cont’d)

19) A/ICE

Pushbutton

C

2 0 May be inoperative provided Maintenance Diagnostic

Computer (45-45-01) is considered inoperative.

NOTE: The Flight Control System (FCS)

diagnostics page will not be accessible.

20) ECS

Pushbutton

C

2 0 May be inoperative provided Maintenance Diagnostic

Computer (45-45-01) is considered inoperative.

NOTE: The Flight Control System (FCS)

diagnostics page will not be accessible.

21) FUEL

Pushbutton

C

2 0 May be inoperative provided Maintenance Diagnostic

Computer (45-45-01) is considered inoperative.

22) CAS

Pushbutton

C

2 1 Right side may be inoperative.

23) CKLST

Pushbutton

C

2 0 May be inoperative provided Electronic Checklist

(31-60-01) is considered inoperative.

24) SKIP

Pushbutton

C

2 0

25) ENTER

Pushbutton

C

2 1

C

2 0 May be inoperative provided:

a) Maintenance Diagnostic Computer

(45-45-01) is considered inoperative.

b) Electronic Checklist (31-60-01) is considered

inoperative,

c) If installed, XM Graphical Weather function

(46-10-01) is considered inoperative, and

d) If installed, Electronic Charts (46-10-01) are

considered inoperative.

NOTE: Flight crew will lose the ability to select

waypoint with joysticks.

(cont'd)

|

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 31-8

1.

2.

Nu

mber Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de système/série article

3. Number Required For Dispatch

Nombre d'arti

cles à exp

édier

31 – INDICATING/

4.

Rema

rks or Exceptions

RECORDING SYSTEMS Remarques ou exceptions

41-02 Cursor Control

Panel (CCP)

(Aircraft with dual

Cursor Control

Panel)

((Aircraft 20125 and

up)

(Cont'd)

26) SUMRY

Pushbutton

D

2 1

C

2 0 May be inoperative provided the Right MFD is

operative.

27) STAT

Pushbutton

C

2 1

C

2 0

May be inoperative provided both FSU (46-10-01) are

considered inoperative.

|

52-01 BRT/DIM System

C

1 0 May be inoperative provided lighting brightness is

acceptable to flight crew for intended flight (day/night)

conditions.

60-01 Electronic Checklist C

1 0 (O) May be inoperative provided alternate procedures

are established and used.

D

1 0 May be inoperative provided normal procedures do not

require its use.

60-02 Digital Voice

Checklist

***

C

1 0 (O) May be inoperative provided alternate procedures

are established and used.

D

1 0 May be inoperative provided normal procedures do not

require its use.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 31-9

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de système

/série arti

cle

3. Number Required For Dispatch

Nombre d'a

rticles à expédier

31 – INDICATING/

4.

Remarks or Exceptions

RECORDING SYSTEMS Remarques ou exceptions

61-01 Adaptive Flight

Displays (AFD)

1) Aircraft with

Single Cursor

Control Panel

A

4 3 (O) Right MFD may be inoperative provided:

a) Cursor Control Panel L/R Toggle Switch is

operative to select CCP control to left MFD,

b) Two Control Display Units are installed and

operative,

c) Unaffected displays reversion capabilities are

verified operative before each flight,

d) Radio tuning reversion capabilities are verified

operative before each flight, and

e) Repairs are made within one flight day.

NOTE: If right side radio tuning is required, the RIGHT

DISPLAYS reversion switch must be selected to PFD

REV or the TUNE reversion switch must be selected to

CDU ONLY.

2) Aircraft with Dual

Cursor Control

Panel (Aircraft

20125 and subs)

A

4 3 (O) Right MFD may be inoperative provided:

a) Left Cursor Control Panel is operative to

control left MFD,

b) Two Control Display Units are installed and

operative,

c) Unaffected displays reversion capabilities are

verified operative before each flight,

d) Radio tuning reversion capabilities are verified

operative before each flight, and

e) Repairs are made within one flight day.

NOTE: If right side radio tuning is required, the RIGHT

DISPLAYS reversion switch must be selected

to PFD REV or the TUNE reversion switch

must be selected to CDU ONLY.

(Cont’d)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 32-1

1.

2.

Number Installed

Syste

m & Sequence

N

o

Item

Nombre d’articles installés

N

o

de système

/série article

3. Number Required For Dispatch

Nombre d'art

icl

es à expédier

32 – LANDING GEAR

4.

Remarks or Exceptions

Remarques ou exceptions

30-01 Landing Gear

Retraction System

B

1 0 (M) May be inoperative provided:

a) Ground lock pins are installed,

b) Operations are not conducted in known or

forecast icing conditions,

c) Extended overwater operations are prohibited,

d) Operations are conducted in accordance with

AFM Supplement, Supplement 2 -

Supplemental information for the MMEL (Flight

with Landing Gear Down), and

e) Operations with steep approach are not

conducted.

43-01 Brake Accumulator

Pressure Gauges

C

2 0 (M) Any or all may be inoperative provided accumulator

pre-charge pressure is checked using a suitable

pressure gauge.

|

50-01 Nosewheel Steering

System

C

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

a) Nosewheel steering limits are not exceeded,

b) LANDING GEAR NWS switch is selected OFF,

c) Solenoid selector valve is verified CLOSED,

d) Operations are not conducted on contaminated

runways,

e) Operations are conducted in accordance with

AFM Supplement, Supplement 2 -

Supplemental information for the MMEL, and

f) Operation with steep approach are not

conducted.

60-01 Nose Landing Gear

Doors System

A 1 1 (M) May be inoperative as indicated by

NOSE GEAR DOOR caution message provided:

a) Nose Landing Gear Door mechanism is

visually inspected and does not have any

disconnected part, wear, excessive corrosion

or cracks,

b) Airspeed is limited to 250 KIAS,

c) Operations are conducted at or below FL180,

and

d) Repairs are made within three flight days.

NOTE: For missing Nose Gear Door Seal,

refer to the Configuration Deviation List

(CDL).

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 32-2

1.

2.

Number Installed

Syste

m & Sequen

ce

N

o

Item

Nombre d’articles installés

N

o

de système/série article

3. Number Required For Dispatch

Nombre

d'articles à expédier

32 – LANDING GEAR

4.

Remarks or Exceptions

Remarques ou exceptions

60-02 Nose Wheel

Steering -Oversteer

Switch

B

1 0

(O) May be inoperative or tripped provided Oversteer

switch frangible pin (mechanical indicator) is intact

before and after every towing operation and before

every flight.

NOTE: NWS LIMIT EXCEEDED (C) Caution message

may be present (32-01), See Section 2 CAS

Message MMEL relief.

|

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

1 Page

BD-100-1A10 Date: Mar 24/05 33-1

1.

2.

Number Installed

Sy

stem & Sequence N

o

Item

Nombre d’articles installés

N

o

de

sy

stème/série

article

3. Number Required For Dispatch

Nombre d'articl

es

à expédier

33 – LIGHTS

4.

R

emarks or Exceptions

Remarques ou exceptions

10-01 Cockpit and

Instrument Lighting

Systems

1) Reading,

Stowage Lights,

and Panels'

Backlighting

C

- - Individual lights may be inoperative for night operations

provided remaining lights are:

a) Sufficient to clearly illuminate all instruments,

controls, and other devices for which it is

provided,

b) Positioned so that direct rays are shielded from

flight crew members’ eyes, and

c) Lighting configuration and intensity is

acceptable to flight crew.

D

- 0 May be inoperative for day operations.

2) Dome Light

LEDs

C

- - May be inoperative provided lighting from remaining

LEDs is acceptable to flight crew for night operations.

D

- 0 May be inoperative for day operations.

20-01 Cabin Lighting

System (Overhead

& Sidewall)

C

- - Individual lighting sources may be inoperative provided

cabin lighting is sufficient for crew members to perform

their duties.

20-02 Floor Accent

Lighting System

***

D

- 0

21-01 Airstair Lights

D

- 0

23-01 Passenger Notice

System (No

Smoking / Fasten

Seat Belt)

C

1 0 (O) May be inoperative provided procedures are

established and used to notify passengers when seat

belts should be fastened and smoking prohibited.

1) Aural tone

Function

C

1 0 (O) May be inoperative provided alternative procedures

are established and used.

(cont'd)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

1 Page

BD-100-1A10 Date: Mar 24/05 33-2

1.

2.

Number Installed

System & Sequence N

o

Ite

m

Nombre d’articles installés

N

o

de

sy

stèm

e

/

s

érie

article

3. Number Required For Dispatch

Nombre d'articles à expédier

33 – LIGHTS

4.

Remarks or Exceptions

Remarques ou exceptions

23-01 Passenger Notice

System (No

Smoking / Fasten

Seat Belt)

(Cont'd)

2) Passenger

Notice Signs

“No Smoking/

Fasten Seat

Belt”

C

- - (M) May be inoperative provided passenger seats or

lavatory from which a sign is not readily legible shall

not be occupied and must be blocked and placarded

“DO NOT OCCUPY”.

C

- - (O) May be inoperative provided procedures are

established and used to notify passengers for whom a

sign is not readily legible when seat belts should be

fastened and smoking prohibited.

31-01 Service Lighting

1) Aft

Compartment

Lights

D

2 0

2) Cargo Loading

Light

D

1 0

3) Service Panel

Lights

***

D

4 0

41-01

Landing Lights

1) Belly Fairing

Lights

C

2 1 May be inoperative for night operations provided Nose

Light is operative.

C

2 1 May be inoperative for night operations provided Taxi

Light is operative.

C

2 0 Any or all may be inoperative for night operations

provided:

a) Nose Light is operative, and

b) Taxi Light is operative.

(cont'd)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

2 Page

BD-100-1A10 Date: Oct 28/08 33-3

1.

2.

Number Insta

lled

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série artic

le

3. Number Required For Dispatch

Nomb

r

e

d'art

icles à ex

pédier

33 – LIGHTS

4.

Remarks or Exceptions

Remarques ou exceptions

41-01 Landing Lights

(Cont'd)

1) Belly Fairing

Lights

(Cont'd)

C

2 0 Any or all may be inoperative for day operations.

a) Belly Fairing

Lights Pulse

Function

***

D

2 0

2) Nose Light C

1 0 May be inoperative for night operations provided:

a) One Belly Fairing Light is operative, and

b) Taxi Light is operative.

C

1 0 May be inoperative for night operations provided Belly

Fairing Lights are operative.

C

1 0 May be inoperative for day operations.

41-02 Taxi Light C

1 0 May be inoperative for night operations provided:

a) Nose Landing Light is operative, and

b) One Belly Fairing Landing Light is operative.

C

1 0 May be inoperative for night operations provided Belly

Fairing Landing Lights are operative.

C

1 0 May be inoperative for day operations.

42-01 Navigation Lights

(Halogen or LED

types)

1) Wing Tip

Navigation Lights

C - 2 (M) One on each side must be operative and enabled

for night operations.

C - 0 Any or all may be inoperative for day operations.

(cont’d)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

5 Page

BD-100-1A10 Date: Apr 28/19 33-4

1.

2.

Number Installed

Sys

te

m & Sequence N

o

Item

Nombre d’articles installés

N

o

de système/série article

3. Number Required For Dispatch

No

mbre d'articles à

expédier

33 – LIGHTS

4.

R

e

marks

or Except

ions

Remarques ou exceptions

42-01 Navigation Lights

(Halogen or LED

types)

(Cont’d)

2) Tail Navigation

Lights

C

- 1 (M) One must be operative and enabled for night

operations.

C

- 0 Any or all may be inoperative for day operations.

43-01 Dual Function Anti -

Collision Lights

1) White Strobes

(Upper / Lower)

C

2 0 (O) Any or all may be inoperative for day operations.

2) Red Beacons

(Upper / Lower)

C

2 0 (M)(O) Any or all may be inoperative provided

adequate precautions are taken to clear danger areas

before engine start and while engines are running.

43-02 Wing Tip Strobe

Lights

***

D

2 0

45-01 Logo Lights

***

D

2 0

45-02 Wing Inspection

Lights

1) Aircraft 20001 to

20143 without

SB 100-30-04

C

2 0

May be inoperative provided:

a) Aircraft is not operated in known or forecast icing

conditions at night, and

b) Ground deicing procedures do not require their

use.

2) Aircraft 20001 to

20143 with SB

100-30-04,

Aircraft 20144

and

subsequent.

C

2 0

(O) May be inoperative provided:

a) Both Ice Detectors are operative,

b) Wing ANTI-ICE is turned ON below 210 Knots

when icing conditions as defined in the AFM

exist or anticipated, and

c) Ground deicing procedures do not require their

use.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 33-5

1.

2.

Number Insta

lled

System & Sequence N

o

It

em

Nombre d’articles installés

N

o

de

systèm

e/série article

3. Number Required For Dispatch

Nombre d'articles

à

expédier

33 – LIGHTS

4.

Rem

arks or Exceptions

Remarques ou exceptions

50-01 Exterior Emergency

Lights

C

3 0 Any or all may be inoperative for day operations.

A

3 0 (O) Any or all may be inoperative for night operations

provided:

a) Aircraft crew are the only occupants of the

aircraft,

b) Alternate procedures are established and used,

and

c) Repairs are made within one flight day.

NOTE: For the purpose of this item “aircraft crew” is

considered to be flight attendants, aircraft

maintenance engineers and supervisory

crew members.

50-02 Exit Identifiers and

Emergency Escape

Path Marking System

(Seat Mounted

Lighting System)

1 1 System must be operative

1) Path Marking

Light Fixtures

(Bruce Industries

Lights STC

ST01569LA)

C - - A minimum of one out of two bulbs in each fixture must

be operative.

2) Exit Identifiers

a) Bruce

Industries

Light Model

BR9661-

series

STC

ST01569LA

C 2 2 A minimum of two out of five bulbs within each fixture

must be operative.

(cont’d)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 33-6

1.

2.

Number Installed

System & Sequence N

o

It

em

Nombre d’articles installés

N

o

de

système/série article

3. Number Required For Dispatch

Nombre d

'articles à expédier

33 – LIGHTS

4.

Remarks or Ex

cept

i

o

n

s

Remarques ou exceptions

50-02 Exit Identifiers and

Emergency Escape

Path Marking System

(Seat Mounted

Lighting System)

(Cont’d)

2) Exit Identifiers

(Cont’d)

b) EMTEQ LED

type (P/N

C300-ELES-

001 and

C300-ELES-

002 only)

Aircraft,

20139,20143,

20146, 20148

and up.

C 3 3 A minimum of three full LED rows out of four within

each fixture must be operative.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 34-1

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de sy

stème/série articl

e

3. Number Required For Dispatch

Nombre

d'articles à expédier

34 – NAVIGATION

4.

Remarks or Exceptions

Remarques ou exceptions

10-01 Integrated Standby

Instrument System

(ISIS)

1) ILS Function C

1 0

2) Attitude

Function

B

1 0 (M) May be inoperative provided:

a) Operations conducted in day VMC,

b) Operations are not conducted into known or

forecast VFR-On-Top conditions, and

c) Instrument attitude display is covered.

3) STD (Standard)

Button

C

1 0 May be inoperative provided BARO Rotary Knob is

operative.

|

10-02 Non-stabilized

Magnetic Compass

(Standby Compass)

B

1 0 (O) May be inoperative provided operations are

conducted under positive radar control by ATC during

the enroute flight phase.

C

1 0 (O) May be inoperative for flights that are entirely within

areas of magnetic unreliability provided operations are

conducted in conjunction with approved Free Gyro

Navigation Techniques.

11-01 Altitude Alerting

Systems

A

2 0 (O) Except where enroute operations require its use,

any or all may be inoperative provided:

a) Autopilot with altitude hold is operative, and

b) Repairs are made within three flight days.

NOTE: Altitude Alerting System is required for

RVSM Operations.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 34-2

1.

2.

Num

ber Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de sy

stème/série article

3. Number Required For Dispatch

N

om

br

e

d

'arti

cles à expédier

34 – NAVIGATION

4.

Remarks or Exceptions

Remarques ou exceptions

Attitude Heading

Reference System

(AHRS)

(Aircraft 20003 to

20407 without SB

100-34-32)

B

2 1

(M)(O) AHRS 2 may be inoperative provided:

a) Integrated Standby Instrument System is

operative,

b) Flight Director 2 is considered inoperative

22-10-02),

c) Autopilot System is considered inoperative

(22-10-01),

d) Reversion Switch Panel ATT/HDG rotary

switch is selected to 1,

e) Operations are conducted in day VMC only,

f) Operations are not conducted into known or

forecast VFR-On-Top conditions,

g) Operations are conducted within one hour from

a suitable airport, and

h) Operations are conducted in accordance with

AFM Supplement, Supplement 2-Supplemental

information for the MMEL.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 34-3

1.

2.

N

umber Installed

System & S

equence

N

o

I

t

e

m

Nombre d’articles installés

N

o

de

système/série article

3. Number Required For Dispatch

Nombre d'a

rticles à expédier

34 – NAVIGATION

4.

Remarks or Exceptions

Remarques ou exceptions

30-01 Steep Approach

Landing Push

Button Annunciator

***

1) “ARM” or “ON”

Light Function

B

1 0 May be inoperative provided:

1) Operations with steep approach are not conducted,

and

2) Steep approach PBA is verified OFF.

2) Switch failed in

“OFF”

B

1 0 May be inoperative provided steep approach

operations are not conducted.

34-01 Synthetic Vision

System (SVS)

(including Database)

***

D

1 0 O) May be inoperative provided SVS is deactivated.

NOTE: SVS is considered inoperative if associated

database is out of date.

41-01 Weather Radar

System

D

1 - Any in excess of those required by Regulations may be

inoperative.

42-01 Terrain Awareness

Warning System

(TAWS) Class A

A

1 0

1) GPWS/TAWS A

1 0 (O) May be inoperative provided:

a) Alternate procedures are established and

used, and

b) Repairs are made within three flight days.

a) Modes 1 - 4 A

4 0 (O) May be inoperative provided:

a) Alternate procedures are established and used,

and

b) Repairs are made within three flight days.

b) Test Mode A

1 0 May be inoperative provided:

a) GPWS/TAWS is considered inoperative, and

b) Repairs are made within three flight days.

c) Glideslope

Deviation

(Mode 5)

B

1 0

d) Advisory

Callouts

C

1 0 (O) May be inoperative provided alternate procedures

are established and used.

(Cont’d)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 34-4

1.

2.

Number Installed

System & Sequence

N

o

Item

Nombre d’articles installés

N

o

d

e

s

ystème/série article

3. Number Required For Dispatch

Nombre d'articles à expé

di

er

34 – NAVIGATION

4.

Remarks or Exceptions

Remarques ou exceptions

42-01 Terrain Awareness

Warning System

(TAWS) Class A

(Cont’d)

1) GPWS/TAWS

(Cont’d)

e) Windshear

Reactive

Mode

(Mode 7)

***

C

1 0 (O) May be inoperative provided:

a) Alternate procedures are established and used,

and

b) Take-offs and landings are not conducted in

known or forecast windshear conditions.

2) Terrain System

- Forward

Looking Terrain

Avoidance

(FLTA) and

Premature

Descent Alert

(PDA)

Functions

***

C

1 0

3) Terrain

Displays

C

1 0

4) Runway

Awareness and

Advisory

System (RAAS)

(Includes Smart

Landing and

Smart Takeoff

functions)

***

C

1 0 (O) May be inoperative provided the RAAS system is

selected OFF.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 34-5

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série a

rticle

3. Number Required For Dispatch

Nombre d'articles à expédier

34 – NAVIGATION

4.

Remarks or

Exceptions

Remarques ou exceptions

43-01 Traffic Alert Collision

Avoidance System

(TCAS)

TCAS II (Including

TCAS function of

the Traffic

Surveillance System

(TSS) Aircraft 20408

and up)

B

1 0 (M) May be inoperative provided system is deactivated.

1) Combined

Traffic Alert (TA)

and Resolution

Advisory (RA)

Dual Display

Systems

C

2 1 (O) May be inoperative on non-flying pilot side

provided TA and RA elements and audio functions are

operative on flying pilot side.

2) Resolution

Advisory (RA)

Display

System(s)

C

2 1 (O) May be inoperative on non-flying pilot side.

C

2 0 (O) Any or all may be inoperative provided:

a) All Traffic Alert (TA) display elements and voice

command audio functions are operative, and

b) TA only mode is selected by the crew.

3) Traffic Alert (TA)

Display

System(s)

C

2 0

(O) Any or all may be inoperative provided all installed

RA display and audio functions are operative.

4) Audio

Functions

C

1 0

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 34-6

1.

2.

Number Installed

System & Sequ

ence N

o

Item

Nombre d’articles installés

N

o

de

s

y

s

t

ème/série article

3. Number Required For Dispatch

Nombre d'articles à expédier

34 – NAVIGATION

4.

Remarks or Exceptions

Remarques ou exceptions

44-01 Radio Altimeter

Deleted, Revision 6.

|

46-01 Lightning Detection

System

***

D

1 0

51-01 VHF Navigation

System (VOR/ILS)

C

2 1 NAV 2 may be inoperative.

51-02 Automatic Direction

Finding (ADF)

System

D

- - Any in excess of those required by Regulations may be

inoperative.

51-03 Marker Beacon

System

C

2 0 Any or all may be inoperative provided alternate

procedures are established and used.

D

2 0 Any or all may be inoperative provided routine

procedures do not require its use.

53-01 Distance Measuring

Equipment Systems

(DME)

D

- - Any in excess of those required by Regulations may be

inoperative.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 34-7

1.

2.

N

u

m

ber

Installed

System & Sequen

ce N

o

Item

Nombre d’articles installés

N

o

de

systèm

e

/s

érie article

3. Number Required For Dispatch

Nombre d'articles à expédier

34 – NAVIGATION

4.

Remarks or Exceptions

Remarques ou exceptions

54-01 ATC Transponders

and Automatic

Altitude Reporting

Systems

(Includes

transponder function

of Traffic

Surveillance System

(TSS) Aircraft 20408

and up)

C

2 - As required by Regulations.

D

2 - Any in excess of those required by Regulations may be

inoperative.

NOTE: Transponder and Flight Director/Autopilot

must use same side ADC data for RVSM

operations.

1) Elementary and

Enhanced

Downlink

Aircraft

Parameters not

Required by

regulations

A

2 0 May be inoperative provided:

a) Operations do not require its use,

b) Repairs are made prior to completion of the

next heavy maintenance visit.

2) ADS-B Squitter

Transmissions

A

2 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.

55-01 Global Positioning

System

(GPS)

C - 0 (O) Except where enroute operations or approach

procedures require its use, may be inoperative

provided:

a) Terrain/Obstacle Awareness functions of

Terrain Awareness Warning System are

considered inoperative (34-42-01), and

b) Alternate procedures are established and

used.

NOTE: At least one GPS system is required for

ADS-B operations.

D

- 1 Except where enroute operations or approach

procedures require dual GPS.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 34-8

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

s

y

s

tèm

e/série

article

3. Number Required For Dispatch

Nombre d'articles à expéd

i

er

34 – NAVIGATION

4.

Remarks o

r Exceptions

Remarques ou exceptions

61-01 Flight Management

Systems

1) Flight

Management

Computers

C

- 1 (O) Right Flight Management Computer (FMC) may be

inoperative provided operations do not require dual

FMS.

NOTE: When operating with one FMS inoperative,

FMS-computed take off and approach

performance must be verified using

applicable AFM data.

C

- 0 (O) May be inoperative provided:

a) Fuel Used Readout is considered inoperative,

b) Operations do not require its use, and

c) Alternate procedures are established and

used.

2) Control Display

Units

C

- 1 Right may be inoperative provided Adaptive Flight

Displays are operative.

3) 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,

c) Approach Navigation Radios are manually

tuned and identified, and

d) Approaches are not conducted using Flight

Management Systems.

62-01 Data Base Unit

***

D

1 0

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 34-9

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

syst

ème/

séri

e

article

3. Number Required For Dispatch

Nombre d'articles à expédier

34 – NAVIGATION

4.

Remarks or Exceptio

ns

Remarques ou exceptions

61-02 Flight Management

System (FMS)

Performance

Database (Aircraft

20001 to 20500),

(Aircraft 20501 to

20577 with SB 350-

34-013), (Aircraft

20578 and up)

C

- 0 (O) May be inoperative (not installed) provided

alternate procedures are established and used.

61-03 Flight Management

System (FMS)

Vspeed Database

(Aircraft 20001 to

20407 with SB 100-

34-10 or SB 100-34-

32 or SB 100-34-

36),

(Aircraft 20408 to

20500), (Aircraft

20501 to 20577 with

SB 350-34-013),

(Aircraft 20578 and

up)

C

- 0 (O) May be inoperative (not installed) provided

alternate procedures are established and used.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 35-1

1.

2.

Number Installed

System & Sequen

c

e

N

o

Item

Nombre d’articles installés

N

o

de

système/série article

3. Number Required For Dispatch

Nombre d'articles à expéd

ier

35 – OXYGEN

4.

Rem

arks

or E

xcep

t

i

ons

Remarques ou exceptions

12-01 EICAS Oxygen

Quantity Readout

C

1 0 (O) May be inoperative provided:

a) Ground Service Panel Pressure Gauge is

operative and checked before each flight, and

b) Operations are conducted within one hour from

a suitable airport.

12-02 Oxygen

Overpressure Relief

Indicator

C

1 0 (O) May be inoperative (missing) provided alternate

procedure is used to ensure that oxygen supply is at or

above minimum requirements for flight.

13-01 Ground Service

Panel Pressure

Gauge

C

1 0 May be inoperative provided EICAS Oxygen Quantity

Readout is operative.

13-02 Bottle(s) Pressure

Gauge

C

- 0

13-03 Filler Valve

(Service Panel)

C

1 0 (M) May be inoperative provided replenished bottle(s)

is installed with adequate oxygen for flight.

|

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 35-2

1.

2.

Num

be

r In

stal

l

e

d

System & Sequ

ence N

o

Item

Nombre d’articles installés

N

o

de

système/série ar

t

ic

le

3. Number Required For Dispatch

Nombre d'articles à expédier

35 – OXYGEN

4.

Remarks or Exceptions

Remarques ou exceptions

20-02 Passenger Oxygen

Circuit

B

1 0 (O) May be inoperative provided:

a) PAX OXYGEN Control Panel rotary selector

switch is selected to OFF,

b) Operations are conducted so that minimum

enroute altitude (MEA) is at or below 13 000 ft.

MSL,

c) Operations are conducted at or below FL 250,

d) Portable oxygen units are provided for all crew

members and for 10 percent of passengers for

half an hour (supplemental oxygen), and

e) Procedures are established to ensure that

passengers are appropriately briefed.

C

1 0 May be inoperative provided:

a) PAX OXYGEN Control Panel rotary selector

switch is selected to OFF, and

b) Passengers are not carried.

1) Automatic

Presentation

System

B

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

a) Manual deployment is verified operative, and

b) Operations are conducted at or below FL 300.

NOTE: Flight planning has to take into account

higher oxygen consumption in manual

Deploy Mode.

2) Passenger

Oxygen Mask

Containers

(including Door,

Masks, and

Latch

Mechanism)

B

- 0 May be inoperative provided Passenger Oxygen Circuit

(35-20-02) is considered inoperative and associated

(O) procedures are followed.

|

(Cont’d)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 35-3

1.

2.

Number Install

ed

Sy

s

te

m & Sequen

ce N

o

Item

Nombre d’articles installés

N

o

de

système/série article

3. Number Required For Dispatch

Nombre d'articles à exp

édier

35 – OXYGEN

4.

Rem

a

r

ks or Exceptions

Remarques ou exceptions

20-02 Passenger Oxygen

Circuit

|

2) Passenger

Oxygen Mask

Containers

(including Door,

Masks, and

Latch

Mechanism)

(Cont’d)

D

- - (M) May be inoperative with no flight altitude restriction

provided:

a) Affected seats or divans are blocked and

placarded “INOPERATIVE” to prevent

occupancy, and

b) Passenger Oxygen Mask Containers at

assigned flight attendant locations are

operative.

|

20-03 Therapeutic Oxygen

Circuit

C

1 0 May be inoperative provided PAX OXYGEN

THERAPEUTIC switch is selected OFF.

30-01 Protective Breathing

Equipment

D

- - (M)(O) Any in excess of those required by Regulations

may be missing or inoperative provided:

a) Required distribution of operative units is

maintained throughout the aircraft,

b) Inoperative PBE unit is removed from

passenger cabin and its location is placarded

INOPERATIVE, or it is removed from the

installed location, secured out of sight and the

PBE unit and its installed location are

placarded INOPERATIVE, and

c) Procedures are established to alert crew

members of inoperative or missing equipment.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

Original Page

BD-100-1A10 Date: Sep 30/03 35-4

1.

2.

Number Instal

led

S

y

st

em & Seque

nce N

o

Item

Nombre d’articles installés

N

o

de système/série article

3. Number Required For Dispatch

Nombre d'articles à ex

pédier

35 – OXYGEN

4

.

Re

m

a

rks or Exceptions

Remarques ou exceptions

THIS PAGE INTENTIONALLY LEFT BLANK

\

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 36-1

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série article

3. Number Required For Dispatch

Nombre d'articles à expédier

36 – PNEUMATICS

4.

Remarks or Exception

s

Remarques ou exceptions

10-01 Bleed Valves

(IPV)

1) Aircraft without

SB 100-21-05

B

2 0 (M)(O) Any or all may be inoperative provided:

a) Valves are secured CLOSED,

b) XBLEED Valve is operative and selected

OPEN,

c) APU is operative and used throughout flight,

d) APU Load Control Valve is operative,

e) Trim Air Inlet Temperature Sensor is verified

operative once each flight day,

f) Pack Inlet Temperature Sensor is verified

operative once each flight day,

g) Bleed Loops are verified operative before each

flight,

h) Ram Air Valve is verified operative,

i) Operations are conducted at or below FL 190,

and

j) Operations are conducted within one hour from

a suitable airport.

|

B

2 0 (M)(O) Any or all may be inoperative provided:

a) Valves are secured CLOSED,

b) XBLEED Valve is selected CLOSED,

c) APU is operative and used throughout flight,

d) APU Load Control Valve is operative,

e) Trim Air Inlet Temperature Sensor is verified

operative once each flight day,

f) Right Bleed Loop is verified operative before

each flight,

g) Right Flow Control Valve is operative,

h) Trim Air System is operative,

i) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to NORM,

j) Ram Air Valve is verified operative,

k) Operations are conducted at or below FL 190,

and

l) Operations are conducted within one hour from

a suitable airport.

(cont’d)

|

\

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 36-2

1.

2.

Nu

m

be

r Installe

d

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série article

3. Number Required For Dispatch

Nombr

e d'articles à expé

dier

36 – PNEUMATICS

4.

Remarks or Exceptions

Remarques ou exceptions

10-01 Bleed Valves

(IPV)

(Cont’d)

1) Aircraft without

SB 100-21-05

(Cont’d)

C

2 0 (M)(O) Any or all may be inoperative provided:

a) Valves are secured CLOSED,

b) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to OFF,

c) Ram Air Valve is selected OPEN,

d) PRESSURIZATION EMER DEPRESS switch is

selected ON, and

e) Operations are conducted unpressurized at or

below 9000 ft. MSL.

|

a) L/H Bleed

Valve

B

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

a) Valve is secured CLOSED,

b) XBLEED Valve is operative and selected

OPEN,

c) R/H Bleed Valve is operative,

d) R/H Environmental Control Bleed Pressure

Indication System is operative,

e) Bleed Loops are verified operative before each

flight,

f) Trim Air Inlet Temperature Sensor is operative,

g) Pack Inlet Temperature Sensor is verified

operative once each flight day,

h) Ram Air Valve is verified operative,

i) Operations are conducted at or below FL 250,

and

j) Operations are conducted within one hour from

a suitable airport.

(cont’d)

|

\

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 36-3

1.

2.

N

u

mber Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

systè

m

e/

s

érie ar

ticle

3. Number Required For Dispatch

Nombre d'articles à expédier

36 – PNEUMATICS

4.

Remarks or Exceptions

Remarques ou exceptions

10-01 Bleed Valves

(IPV)

(cont’d)

a) L/H Bleed

Valve

(Cont’d)

B

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

a) Valve is secured CLOSED,

b) XBLEED Valve is selected CLOSED,

c) R/H Bleed Valve is operative,

d) R/H Environmental Control Bleed Pressure

Indication System is operative,

e) Right Bleed Loop is operative,

f) Right Flow Control Valve is operative,

g) Trim Air System is operative,

h) Trim Air Inlet Temperature Sensor is operative,

i) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to NORM,

j) Ram Air Valve is verified operative,

k) Operations are conducted at or below FL 250,

and

l) Operations are conducted within one hour from

a suitable airport.

(cont’d)

|

\

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 36-4

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de système/série art

icle

3. Number Required For Dispatch

Nombre d'articles à expédier

36 – PNEUMATICS

4.

Remarks or E

x

ceptio

n

s

Remarques ou exceptions

10-01 Bleed Valves

(IPV)

(cont’d)

b) R/H Bleed

Valve

B

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

a) Valve is secured CLOSED,

b) XBLEED Valve is operative and selected

OPEN,

c) L/H Bleed Valve is operative,

d) L/H Environmental Control Bleed Pressure

Indication System is operative,

e) Bleed Loops are verified operative before each

flight,

f) Trim Air Inlet Temperature Sensor is verified

operative once each flight day,

g) Pack Inlet temperature Sensor is operative,

h) Ram Air Valve is verified operative,

i) Operations are conducted at or below FL 250,

and

j) Operations are conducted within one hour from

a suitable airport.

|

B

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

a) Valve is secured CLOSED,

b) XBLEED Valve is selected CLOSED,

c) L/H Bleed Valve is operative,

d) L/H Environmental Control Bleed Pressure

Indication System is operative,

e) Left Bleed Loop is operative,

f) Left Flow Control Valve is operative,

g) Pack Inlet temperature Sensor is operative,

h) APU bleed is used for engines start only,

i) Ram Air Valve is verified operative,

j) Operations are conducted at or below FL 250,

and

k) Operations are conducted within one hour from

a suitable airport,

|

\

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 36-5

1.

2.

Number Installe

d

System & Sequenc

e N

o

Ite

m

Nombre d’articles installés

N

o

de

sys

tème/série

article

3. Number Required For Dispatch

N

ombre d'articles à expédier

36 – PNEUMATICS

4.

Remarks or Exceptions

Remarques ou exceptions

10-01 Bleed Valves

(IPV)(Cont’d)

2) Aircraft with

SB 100-21-05,

Aircraft 20101

and Subs.

C

2 0 (M)(O) Any or all may be inoperative provided:

a) Valves are secured CLOSED,

b) XBLEED Valve is operative and selected

OPEN,

c) APU is operative and used throughout flight,

d) APU Load Control Valve is operative,

e) Trim Air Inlet Temperature Sensor is verified

operative once each flight day,

f) Pack Inlet Temperature Sensor is verified

operative once each flight day,

g) Bleed Loops are verified operative before each

flight,

h) Ram Air Valve is verified operative,

i) Operations are conducted at or below FL 190,

and

j) Operations are conducted within one hour

from a suitable airport.

|

C

2 0 (M)(O) Any or all may be inoperative provided:

a) Valves are secured CLOSED,

b) XBLEED Valve is selected CLOSED,

c) APU is operative and used throughout flight,

d) APU Load Control Valve is operative,

e) Trim Air Inlet Temperature Sensor is verified

operative once each flight day,

f) Right Bleed Loop is verified operative before

each flight,

g) Right Flow Control Valve is operative,

h) Trim Air System is operative,

i) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to NORM,

j) Ram Air Valve is verified operative,

k) Operations are conducted at or below FL 190,

and

l) Operations are conducted within one hour from

a suitable airport.

(cont’d)

|

\

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 36-6

1.

2

.

Number Installed

Sys

tem

&

Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série

article

3. Number Required For Dispatch

Nombre d'articles à expédier

36 – PNEUMATICS

4.

Remarks or Exceptions

Remarques ou exceptions

10-01 Bleed Valves (IPV)

(cont’d)

2) Aircraft with

SB 100-21-05,

Aircraft 20101

and Subs.

(Cont’d)

C

2 0 (M)(O) Any or all may be inoperative provided:

a) Valves are secured CLOSED,

b) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to OFF,

c) Ram Air Valve is selected OPEN,

d) PRESSURIZATION EMER DEPRESS switch

is selected ON, and

d) Operations are conducted unpressurized at or

below 9000 ft. MSL.

|

a) L/H Bleed

Valve

C

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

a) Valve is secured CLOSED,

b) XBLEED Valve is operative and selected

OPEN,

c) R/H Bleed Valve is operative,

d) R/H Environmental Control Bleed Pressure

Indication System is operative,

e) Bleed Loops are verified operative before each

flight,

f) Trim Air Inlet Temperature Sensor is operative,

g) Pack Inlet Temperature Sensor is verified

operative once each flight day,

h) Ram Air Valve is verified operative,

i) Operations are conducted at or below FL 250,

and

j) Operations are conducted within one hour from

a suitable airport.

(cont’d)

|

\

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 36-7

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de système/sé

rie

article

3. Number Required For Dispatch

Nombre d'arti

cles à

ex

pédier

36 – PNEUMATICS

4.

Remarks or Exceptions

Remarques ou exceptions

10-01 Bleed Valves

(IPV)

(cont’d)

2) Aircraft with

SB 100-21-05,

Aircraft 20101

and Subs.

(Cont’d)

a) L/H Bleed

Valve

(Cont’d)

C

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

a) Valve is secured CLOSED,

b) XBLEED Valve is selected CLOSED,

c) R/H Bleed Valve is operative,

d) R/H Environmental Control Bleed Pressure

Indication System is operative,

e) Right Bleed Loop is operative,

f) Right Flow Control Valve is operative,

g) Trim Air System is operative,

h) Trim Air Inlet Temperature Sensor is operative,

i) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to NORM,

j) Ram Air Valve is verified operative,

k) Operations are conducted at or below FL 250,

and

l) Operations are conducted within one hour from

a suitable airport.

(cont’d)

|

\

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 36-8

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de système/série

article

3. Number Required For Dispatch

N

ombre d'articles à expédi

er

36 – PNEUMATICS

4.

Remarks or Exceptions

Remarques ou exceptions

10-01 Bleed Valves

(IPV) (cont’d)

2) Aircraft with

SB 100-21-05,

Aircraft 20101

and Subs.

(Cont’d)

b) R/H Bleed

Valve

C

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

a) Valve is secured CLOSED,

b) XBLEED Valve is operative and selected

OPEN,

c) L/H Bleed Valve is operative,

d) L/H Environmental Control Bleed Pressure

Indication System is operative,

e) Bleed Loops are verified operative before each

flight,

f) Trim Air Inlet Temperature Sensor is verified

operative once each flight day,

g) Pack Inlet temperature Sensor is operative,

h) Ram Air Valve is verified operative,

i) Operations are conducted at or below FL 250,

and

j) Operations are conducted within one hour from

a suitable airport.

|

C

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

a) Valve is secured CLOSED,

b) XBLEED Valve is selected CLOSED,

c) L/H Bleed Valve is operative,

d) L/H Environmental Control Bleed Pressure

Indication System is operative,

e) Left Bleed Loop is operative,

f) Left Flow Control Valve is operative,

g) Pack Inlet temperature Sensor is operative,

h) APU bleed is used for engines start only,

i) Ram Air Valve is verified operative,

j) Operations are conducted at or below FL 250,

and

k) Operations are conducted within one hour from

a suitable airport.

|

\

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

2 Page

BD-100-1A10 Date: Oct 28/08 36-9

1.

2.

Numb

er I

n

s

ta

lled

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système

/série

ar

ticle

3. Number Required For Dispatch

Nombre d'articles à expédier

36 – PNEUMATICS

4.

Remarks or Exceptions

Remarques ou exceptions

10-02 Environmental Control

Bleed Pressure

Indication Systems

1) Aircraft without

SB 100-21-05

B

2 0 (O) Any or all may be inoperative provided:

a) Bleed Valves are selected CLOSED,

b) XBLEED Valve is selected CLOSED,

c) APU is operative and used throughout flight,

d) APU Load Control Valve is operative,

e) Right Bleed Loop is operative,

f) Right Flow Control Valve is operative,

g) Trim Air System is operative,

h) Trim Air Inlet Temperature Sensor is operative,

i) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to NORM,

j) Ram Air Valve is verified operative,

k) Operations are conducted at or below FL 190,

and

l) Operations are conducted within one hour from

a suitable airport.

B

2 0 (O) Any or all may be inoperative provided:

a) Bleed Valves are selected CLOSED,

b) XBLEED Valve is operative and selected

OPEN,

c) APU is operative and used throughout flight,

d) APU Load Control Valve is operative,

e) Trim Air Inlet Temperature Sensor is operative,

f) Pack Inlet Temperature Sensor is operative,

g) Bleed Loops are operative,

h) Ram Air Valve is verified operative,

i) Operations are conducted at or below FL 190,

and

j) Operations are conducted within one hour from

a suitable airport.

(cont’d)

\

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

2 Page

BD-100-1A10 Date: Oct 28/08 36-10

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série

arti

cle

3. Number Required For Dispatch

Nombre d'articles à expédier

36 – PNEUMATICS

4.

R

e

ma

rks or Exc

eptions

Remarques ou exceptions

10-02 Environmental

Control Bleed

Pressure Indication

Systems

(cont’d)

1) Aircraft without

SB 100-21-05

(Cont’d)

C

2 0 (O) Any or all may be inoperative provided:

a) Bleed Valves are selected CLOSED,

b) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to OFF,

c) Ram Air Valve is selected OPEN,

d) PRESSURIZATION EMER DEPRESS switch is

selected ON, and

e) Operations are conducted unpressurized at or

below 9000 ft. MSL.

a) L/H Bleed

Pressure

Indication

System

B

1 0 (O) May be inoperative provided:

a) L/H Bleed Valve is selected CLOSED,

b) XBLEED Valve is operative and selected

OPEN,

c) R/H Bleed Valve is operative,

d) R/H Environmental Control Bleed Pressure

Indication System is operative,

e) Bleed Loops are operative,

f) Trim Air Inlet Temperature Sensor is operative,

g) Pack Inlet Temperature Sensor is operative,

h) Ram Air Valve is verified operative,

i) Operations are conducted at or below FL 250,

and

j) Operations are conducted within one hour from

a suitable airport.

(cont’d)

\

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

2 Page

BD-100-1A10 Date: Oct 28/08 36-11

1.

2.

Number

Insta

l

le

d

System

& Sequence N

o

Item

Nombre d’articles installés

N

o

de système/série

article

3. Number Required For Dispatch

Nombre d'articles

à expédier

36 – PNEUMATICS

4.

Remarks or Exceptions

Remarques ou exceptions

10-02 Environmental

Control Bleed

Pressure Indication

Systems

(cont’d)

1) Aircraft without

SB 100-21-05

(Cont’d)

a) L/H Bleed

Pressure

Indication

System

(cont’d)

B

1 0 (O) May be inoperative provided:

a) L/H Bleed Valve is selected CLOSED,

b) XBLEED Valve is selected CLOSED,

c) R/H Bleed Valve is operative,

d) R/H Environmental Control Bleed Pressure

Indication System is operative,

e) Right Bleed Loop is operative,

f) Right Flow Control Valve is operative,

g) Trim Air System is operative,

h) Trim Air Inlet temperature Sensor is operative,

i) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to NORM,

j) Ram Air Valve is verified operative,

k) Operations are conducted at or below FL 250,

and

l) Operations are conducted within one hour from

a suitable airport.

(cont’d)

\

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

2 Page

BD-100-1A10 Date: Oct 28/08 36-12

1.

2.

Number Installed

System & Sequ

ence N

o

I

tem

Nombre d’articles installés

N

o

de système/s

érie

article

3. Number Required For Dispatch

Nombre d'articles à expédier

36 – PNEUMATICS

4.

Remarks or

Exc

epti

o

n

s

Remarques ou exceptions

10-02 Environmental

Control Bleed

Pressure Indication

Systems

(cont’d)

1) Aircraft without

SB 100-21-05

(Cont’d)

b) R/H Bleed

Pressure

Indication

System

B

1 0 (O) May be inoperative provided:

a) R/H Bleed Valve is selected CLOSED,

b) XBLEED Valve is operative and selected

OPEN,

c) L/H Bleed Valve is operative,

d) L/H Environmental Control Bleed Pressure

Indication System is operative,

e) Bleed Loops are operative,

f) Trim Air Inlet Temperature Sensor is operative,

g) Pack Inlet Temperature Sensor is operative,

h) Ram Air Valve is verified operative,

i) Operations are conducted at or below FL 250,

and

j) Operations are conducted within one hour from

a suitable airport.

B

1 0 (O) May be inoperative provided:

a) R/H Bleed Valve is selected CLOSED,

b) XBLEED Valve is selected CLOSED,

c) L/H Bleed Valve is operative,

d) L/H Environmental Control Bleed Pressure

Indication System is operative,

e) Left Bleed Loop is operative,

f) Left Flow Control Valve is operative,

g) Pack Inlet Temperature Sensor is operative,

h) Ram Air Valve is verified operative,

i) Operations are conducted at or below FL 250,

and

j) Operations are conducted within one hour from

a suitable airport.

\

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 36-13

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de système

/série

article

3. Number Required For Dispatch

Nomb

re d'articles à expédier

36 – PNEUMATICS

4.

Rem

arks o

r

E

xceptions

Remarques ou exceptions

10-02 Environmental Control

Bleed Pressure

Indication Systems

2) Aircraft with

SB 100-21-05,

Aircraft 20101

and Subs.

C

2 0 (O) Any or all may be inoperative provided:

a) Bleed Valves are selected CLOSED,

b) XBLEED Valve is selected CLOSED,

c) APU is operative and used throughout flight,

d) APU Load Control Valve is operative,

e) Right Bleed Loop is operative,

f) Right Flow Control Valve is operative,

g) Trim Air System is operative,

h) Trim Air Inlet Temperature Sensor is operative,

i) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to NORM,

j) Ram Air Valve is verified operative,

k) Operations are conducted at or below FL 190,

and

l) Operations are conducted within one hour from

a suitable airport.

C

2 0 (O) Any or all may be inoperative provided:

a) Bleed Valves are selected CLOSED,

b) XBLEED Valve is operative and selected

OPEN,

c) APU is operative and used throughout flight,

d) APU Load Control Valve is operative,

e) Trim Air Inlet Temperature Sensor is operative,

f) Pack Inlet Temperature Sensor is operative,

g) Bleed Loops are operative,

h) Ram Air Valve is verified operative,

i) Operations are conducted at or below FL 190,

and

j) Operations are conducted within one hour from

a suitable airport.

(cont’d)

\

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 36-14

1.

2.

Number Inst

alled

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série

article

3. Number Required For Dispatch

Nombre d'articles à expédier

36 – PNEUMATICS

4.

Remarks or Exceptions

Remarques ou exceptions

10-02 Environmental

Control Bleed

Pressure Indication

Systems

(cont’d)

2) Aircraft with

SB 100-21-05,

Aircraft 20101

and Subs.

C

2 0 (O) Any or all may be inoperative provided:

a) Bleed Valves are selected CLOSED,

b) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to OFF,

c) Ram Air Valve is selected OPEN,

d) PRESSURIZATION EMER DEPRESS switch is

selected ON, and

e) Operations are conducted unpressurized at or

below 9000 ft. MSL.

a) L/H Bleed

Pressure

Indication

System

C

1 0 (O) May be inoperative provided:

a) L/H Bleed Valve is selected CLOSED,

b) XBLEED Valve is operative and selected

OPEN,

c) R/H Bleed Valve is operative,

d) R/H Environmental Control Bleed Pressure

Indication System is operative,

e) Bleed Loops are operative,

f) Trim Air Inlet Temperature Sensor is operative,

g) Pack Inlet Temperature Sensor is operative,

h) Ram Air Valve is verified operative,

i) Operations are conducted at or below FL 250,

and

j) Operations are conducted within one hour from

a suitable airport.

(cont’d)

\

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 36-15

1.

2.

Number Installed

Sys

tem & Sequence N

o

I

tem

Nombre d’articles installés

N

o

de système/série

article

3. Number Required For Dispatch

Nombre

d'articles à expédier

36 – PNEUMATICS

4.

Remarks or Exceptions

Remarques ou exceptions

10-02 Environmental

Control Bleed

Pressure Indication

Systems

(cont’d)

2) Aircraft with

SB 100-21-05,

Aircraft 20101

and Subs.

a) L/H Bleed

Pressure

Indication

System

(cont’d)

C

1 0 (O) May be inoperative provided:

a) L/H Bleed Valve is selected CLOSED,

b) XBLEED Valve is selected CLOSED,

c) R/H Bleed Valve is operative,

d) R/H Environmental Control Bleed Pressure

Indication System is operative,

e) Right Bleed Loop is operative,

f) Right Flow Control Valve is operative,

g) Trim Air System is operative,

h) Trim Air Inlet temperature Sensor is operative,

i) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to NORM,

j) Ram Air Valve is verified operative,

k) Operations are conducted at or below FL 250,

and

l) Operations are conducted within one hour from

a suitable airport.

(cont’d)

\

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 36-16

1.

2.

Number Installed

System & Seque

nce N

o

Item

Nombre d’articles installés

N

o

de système/

série

article

3. Number Required For Dispatch

Nombr

e

d

'articles

à expédier

36 – PNEUMATICS

4.

Remarks or Exceptions

Remarques ou exceptions

10-02 Environmental

Control Bleed

Pressure Indication

Systems

(cont’d)

2) Aircraft with

SB 100-21-05,

Aircraft 20101

and Subs.

b) R/H Bleed

Pressure

Indication

System

C

1 0 (O) May be inoperative provided:

a) R/H Bleed Valve is selected CLOSED,

b) XBLEED Valve is operative and selected

OPEN,

c) L/H Bleed Valve is operative,

d) L/H Environmental Control Bleed Pressure

Indication System is operative,

e) Bleed Loops are operative,

f) Trim Air Inlet Temperature Sensor is operative,

g) Pack Inlet Temperature Sensor is operative,

h) Ram Air Valve is verified operative,

i) Operations are conducted at or below FL 250,

and

j) Operations are conducted within one hour from

a suitable airport.

C

1 0 (O) May be inoperative provided:

a) R/H Bleed Valve is selected CLOSED,

b) XBLEED Valve is selected CLOSED,

c) L/H Bleed Valve is operative,

d) L/H Environmental Control Bleed Pressure

Indication System is operative,

e) Left Bleed Loop is operative,

f) Left Flow Control Valve is operative,

g) Pack Inlet Temperature Sensor is operative,

h) Ram Air Valve is verified operative,

i) Operations are conducted at or below FL 250,

and

j) Operations are conducted within one hour from

a suitable airport.

\

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 36-17

1.

2.

Number Installed

System & Sequen

ce N

o

I

te

m

Nombre d’articles installés

N

o

de

système/série

article

3. Number Required For Dispatch

Nombre d'articles à expédier

36 – PNEUMATICS

4.

Remarks or E

xcep

tion

s

Remarques ou exceptions

10-04 AIR COND/BLEED

L/R BLEED “OFF”

Switch Light

(light function only)

C

2 0 (O)

10-05 AIR COND/BLEED

XBLEED “-”

Switch Light

(light function only)

C

1 0

20-01 Leak Detection

Loops

1) Environmental

Control System

C

7 0 (O) Any or all may be inoperative provided:

a) Bleed Valves are selected CLOSED,

b) Anti-Ice System Wing/Pylon Leak Detection

Loops are operative,

c) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to OFF,

d) Ram Air Valve is selected OPEN,

e) PRESSURIZATION EMER DEPRESS switch is

selected ON,

f) APU bleed is used for engines start only,

g) Cross bleed start procedure is not used for

engine start, and

h) Operations are conducted unpressurized at or

below 9000 ft. MSL.

(cont’d)

\

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

2 Page

BD-100-1A10 Date: Oct 28/08 36-18

1.

2.

Number Installe

d

S

yste

m

&

Sequence N

o

Item

Nombre d’articles installés

N

o

de système/série

article

3. Number Required For Dispatch

Nombre d'articles à expédier

36 – PNEUMATICS

4.

Remarks or Exceptions

Remarques ou exceptions

20-01 Leak Detection

Loops

(Cont’d)

a) Pylon Loops

B

2 0 Any or all may be inoperative provided Anti-Ice System

Wing/Pylon Leak Detection Loop on the affected side is

operative.

NOTE: Pylon loops include powerplant interface to the

right Bleed Valve (IPV).

b) Bleed Loops

Aircraft without

SB 100-21-05

B

2 1 (O) Right may be inoperative provided:

a) R/H Bleed Valve is selected CLOSED,

b) XBLEED Valve is selected CLOSED,

c) L/H Bleed Valve is operative,

d) L/H Environmental Control Bleed Pressure

Indication System is operative,

e) Left Flow Control Valve is operative,

f) Pack Inlet Temperature Sensor is operative,

g) APU bleed is used for engines start only,

h) Cross bleed start procedure is not used for

engine start,

i) Ram Air Valve is verified operative,

j) Operations are conducted at or below FL 250,

and

k) Operations are conducted within one hour from

a suitable airport.

NOTE: The right bleed ducting loop includes all the

ducting downstream of the right Bleed Valve

down to the Flow Control Valve (FCV), the

ATS duct. The right bleed loop also includes

the APU and high pressure ground connection

ducting.

(cont’d)

\

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

2 Page

BD-100-1A10 Date: Oct 28/08 36-19

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de système/série

article

3. Number Required For Dispatch

Nombre d'articles à expédier

36 – PNEUMATICS

4.

Remarks or

Exceptions

Remarques ou exceptions

20-01 Leak Detection

Loops

(Cont’d)

b) Bleed Loops

Aircraft without

SB 100-21-05

(Cont’d)

B

2 1 (O) Left may be inoperative provided:

a) L/H Bleed Valve is selected CLOSED,

b) XBLEED Valve is selected CLOSED,

c) R/H Bleed Valve is operative,

d) R/H Environmental Control Bleed Pressure

Indication System is operative,

e) Right Flow Control Valve is operative,

f) Trim Air System is operative,

g) Trim Air Inlet Temperature Sensor is operative,

h) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to NORM,

i) Cross bleed start procedure is not used for

engine start,

j) Ram Air Valve is verified operative,

k) Operations are conducted at or below FL 250,

and

l) Operations are conducted within one hour from

a suitable airport.

NOTE: The left bleed ducting loop includes all the

ducting downstream of the left Intermediate

Pressure Valve (IPV) down to the Flow Control

Valve (FCV) and the Air Turbine Starter (ATS)

duct.

(cont’d)

\

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

2 Page

BD-100-1A10 Date: Oct 28/08 36-20

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série

artic

le

3. Number Required For Dispatch

Nombre d'articles à expédier

36 – PNEUMATICS

4.

Re

m

ar

ks or Exce

ptions

Remarques ou exceptions

20-01 Leak Detection

Loops

(Cont’d)

b) Bleed Loops

Aircraft without SB

100-21-05

(Cont’d)

B

2 1 (O) Left may be inoperative provided:

a) L/H Bleed Valve is selected CLOSED,

b) XBLEED Valve is selected CLOSED,

c) APU is operative and used throughout flight,

d) APU Load Control Valve is operative,

e) R/H Environmental Control Bleed Pressure

Indication System is operative,

f) Right Flow Control Valve is operative,

g) Trim Air System is operative,

h) Trim Air Inlet Temperature Sensor is operative,

i) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to NORM,

j) Cross bleed start procedure is not used for

engine start,

k) Ram Air Valve is verified operative,

l) Operations are conducted at or below FL 190,

and

m) Operations are conducted within one hour from

a suitable airport.

NOTE: The left bleed ducting loop includes all the

ducting downstream of the left Intermediate

Pressure Valve (IPV) down to the Flow

Control Valve (FCV) and the Air Turbine

Starter (ATS) duct.

\

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 36-21

1.

2.

Number Installed

Syste

m

&

Sequence

N

o

Item

Nombre d’articles installés

N

o

de système/série

article

3. Number Required For Dispatch

Nombre d'articles à expédier

36 – PNEUMATICS

4.

Rema

r

k

s

or Exceptions

Remarques ou exceptions

20-01 Leak Detection

Loops

(Cont’d)

c) Bleed Loops

Aircraft with

SB 100-21-05,

Aircraft 20101

and Subs.

C

2 1 (O) Right may be inoperative provided:

a) R/H Bleed Valve is selected CLOSED,

b) XBLEED Valve is selected CLOSED,

c) L/H Bleed Valve is operative,

d) L/H Environmental Control Bleed Pressure

Indication System is operative,

e) Left Flow Control Valve is operative,

f) Pack Inlet Temperature Sensor is operative,

g) APU bleed is used for engines start only,

h) Cross bleed start procedure is not used for

engine start,

i) Ram Air Valve is verified operative,

j) Operations are conducted at or below FL 250,

and

k) Operations are conducted within one hour from

a suitable airport.

NOTE: The right bleed ducting loop includes all the

ducting downstream of the right Bleed Valve

down to the Flow Control Valve (FCV), the

ATS duct. The right bleed loop also includes

the APU and high pressure ground connection

ducting.

(cont’d)

\

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 36-22

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

d

e

s

ystème/série

article

3. Number Required For Dispatch

Nombre d'articles

à exp

é

di

er

36 – PNEUMATICS

4.

Remarks or Exceptions

Remarques ou exceptions

20-01 Leak Detection

Loops

(Cont’d)

c) Bleed Loops

Aircraft with

SB 100-21-05,

Aircraft 20101

and Subs.

(Cont’d)

C

2 1 (O) Left may be inoperative provided:

a) L/H Bleed Valve is selected CLOSED,

b) XBLEED Valve is selected CLOSED,

c) R/H Bleed Valve is operative,

d) R/H Environmental Control Bleed Pressure

Indication System is operative,

e) Right Flow Control Valve is operative,

f) Trim Air System is operative,

g) Trim Air Inlet Temperature Sensor is operative,

h) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to NORM,

i) Cross bleed start procedure is not used for

engine start,

j) Ram Air Valve is verified operative,

k) Operations are conducted at or below FL 250,

and

l) Operations are conducted within one hour from

a suitable airport.

NOTE: The left bleed ducting loop includes all the

ducting downstream of the left Intermediate

Pressure Valve (IPV) down to the Flow

Control Valve (FCV) and the Air Turbine

Starter (ATS) duct.

(cont’d)

\

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 36-23

1.

2.

Number Instal

led

S

y

st

em & Seque

nce N

o

Item

Nombre d’articles installés

N

o

de

système/série

article

3. Number Required For Dispatch

Nombre d'articles à expé

dier

36 – PNEUMATICS

4.

R

e

ma

rks or Exceptions

Remarques ou exceptions

20-01 Leak Detection

Loops

(Cont’d)

c) Bleed Loops

Aircraft with

SB 100-21-05,

Aircraft 20101 and

Subs.

(Cont’d)

C

2 1 (O) Left may be inoperative provided:

a) L/H Bleed Valve is selected CLOSED,

b) XBLEED Valve is selected CLOSED,

c) APU is operative and used throughout flight,

d) APU Load Control Valve is operative,

e) R/H Environmental Control Bleed Pressure

Indication System is operative,

f) Right Flow Control Valve is operative,

g) Trim Air System is operative,

h) Trim Air Inlet Temperature Sensor is operative,

i) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to NORM,

j) Cross bleed start procedure is not used for

engine start,

k) Ram Air Valve is verified operative,

l) Operations are conducted at or below FL 190,

and

m) Operations are conducted within one hour from

a suitable airport.

NOTE: The left bleed ducting loop includes all the

ducting downstream of the left Intermediate

Pressure Valve (IPV) down to the Flow

Control Valve (FCV) and the Air Turbine

Starter (ATS) duct.

d) Pack Loops B

2 1

B

2 0 All may be inoperative provided left and right Flow

Control Valves are considered inoperative

(21-51-01).

NOTE: The Air Conditioning System (ACS) pack

ducting loop includes all the ducting

downstream of the FCV to the ACS pack and

Pre-cooler Cross-over Valve.

(cont’d)

\

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

4 Page

BD-100-1A10 Date: May 02/18 36-24

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de système/série

article

3. Number Required For Dispatch

Nombre d'articles à expédier

36 – PNEUMATICS

4

.

Remarks or Except

ions

Remarques ou exceptions

20-01 Leak Detection

Loops

(Cont’d)

e) Trim Loop B

1 0 May be inoperative provided Trim Air System is

considered inoperative (21-61-03).

NOTE: The trim air ducting loop includes all the

ducting downstream of the right FCV to the

mixing manifold.

2) Anti-Ice System

a) Wing/Pylon

Loops

C

2 0 Any or all may be inoperative provided:

a) Environmental Control System Leak Detection

Pylon Loop on affected side is operative, and

b) Anti-Ice System Leak Detection Fuselage/Wing

Loop on affected side is operative.

NOTE: The Wing/Pylon loops include the powerplant

interface to the IPV (part of ACS system) and

HPV.

C

2 0 Any or all may be inoperative provided:

a) Environmental Control System Leak Detection

Pylon Loop on the affected side is operative,

b) ANTI-ICE WING switch is selected OFF,

c) Operations are not conducted in known or

forecast icing conditions, and

d) One Ice Detection System is operative.

NOTE: The Wing/Pylon loops include the powerplant

interface to the IPV (part of ACS system) and

HPV.

(cont’d)

\

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

2 Page

BD-100-1A10 Date: Oct 28/08 36-25

1.

2

.

Nu

mber Installed

System &

Sequence N

o

Item

Nombre d’articles installés

N

o

de

sys

t

èm

e/série

ar

ticle

3. Number Required For Dispatch

Nombre d'articles à expédier

36 – PNEUMATICS

4.

Remarks or Exceptions

Remarques ou exceptions

20-01 Leak Detection

Loops

(Cont’d)

b) Fuselage / Wing

Loops

C

2 0 Any or all may be inoperative provided Anti-Ice System

Leak Detection Wing/Pylon Loop on affected side is

operative.

NOTE: The Fuselage / Wing loops include the ducting

downstream of the HPV down to the end of

the piccolo (including the Wing Isolation

Valve).

C

2 0 Any or all may be inoperative provided:

a) ANTI-ICE WING switch is selected OFF,

b) Operations are not conducted in known or

forecast icing conditions, and

c) One Ice Detection System is operative.

NOTE: The Fuselage / Wing loops include the ducting

downstream of the HPV down to the end of

the piccolo (including the Wing Isolation

Valve).

\

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

2 Page

BD-100-1A10 Date: Oct 28/08 36-26

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

sys

tème/série

article

3. Number Required For Dispatch

Nombre d'articles à expédier

36 – PNEUMATICS

4.

Remar

k

s

or Excepti

ons

Remarques ou exceptions

THIS PAGE INTENTIONALLY LEFT BLANK

\

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 38-1

1.

2.

Number Installed

System & Sequence

N

o

Item

Nombre d’articles installés

N

o

de

s

ystème/série article

3. Number Required For Dispatch

Nombre

d'

articles à

expédier

38 – WATER/WASTE

4.

Remarks or Exceptions

Remarques ou exceptions

00-01 Water System

1) Lavatory Water

System

C

1 0 (M) Individual components may be inoperative

provided:

a) Affected components are deactivated or

isolated, and

b) Affected components are verified not to have

leaks.

NOTE: Any portion of system which operates

normally may be used.

|

C

1 0 (M) May be inoperative provided:

a) System is drained, and

b) Procedures are established to ensure that

system is not serviced.

|

2) Galley Water

System

C

1 0 (M) Individual components may be inoperative

provided:

a) Affected components are deactivated or

isolated, and

b) Affected components are verified not to have

leaks.

NOTE: Any portion of system which operates

normally may be used.

|

C

1 0 (M) May be inoperative provided:

a) System is drained, and

b) Procedures are established to ensure that

system is not serviced.

|

30-01 Lavatory Waste

System

C

1 0 (M) Individual components may be inoperative

provided:

a) Affected components are deactivated or

isolated, and

b) Affected components are verified not to have

leaks.

NOTE: Any portion of system which operates

normally may be used.

(cont’d)

|

\

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 38-2

1.

2.

Nu

mber

Ins

t

a

ll

ed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/s

érie

ar

ticle

3. Number Required For Dispatch

Nombre d'articles à expédier

38 – WATER/WASTE

4.

Remarks or Exceptions

Remarques ou exceptions

30-01 Lavatory Waste

System

(Cont'd)

C

1 0 (M) May be inoperative provided:

a) System is drained,

b) Pilot-in-Command will determine if flight

duration is acceptable, and

c) Toilet lid is secured CLOSED and placarded,

“INOPERATIVE – DO NOT USE”.

|

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

Original Page

BD-100-1A10 Date: Sep 30/03 45-1

1.

2.

Number Ins

talle

d

System & Se

quen

ce N

o

I

tem

Nombre d’articles installés

N

o

de

système/série article

3. Number Required For Dispatch

Nombre d'articles à expédier

45 – CENTRAL

4.

Remarks or Exceptions

MAINTENANCE SYSTEMS Remarques ou exceptions

45-01 Maintenance

Diagnostic

Computer (MDC)

C

1 0 May be inoperative provided alternate procedures are

established and used.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

Original Page

BD-100-1A10 Date: Sep 30/03 45-2

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de

système/série article

3. Number Required For Dispatch

N

o

mbre d'articles à expédier

45 – CENTRAL

4.

Remarks or Exceptions

MAINTENANCE SYSTEMS Remarques ou exceptions

THIS PAGE INTENTIONALLY LEFT BLANK

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

5 Page

BD-100-1A10 Date: Apr 28/19 46-1

1.

2.

Number Installed

System & Sequ

ence

N

o

Item

Nombre d’articles installés

N

o

de

système/série article

3. Number Required For Dispatch

No

m

br

e d'articl

es à expédier

46 – INFORMATION SYSTEMS

4.

Remarks or Exceptions

Remarques ou exceptions

10-01 Integrated Flight

Information System

(IFIS)

1) File Server Unit

(FSU)

(Aircraft 20125 to

20181 with SB

100-46-02)

(Aircraft 20182

and up)

(Aircraft 20182

and up with SB

100

-

46

-

01)

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.

NOTE: Any function which operates normally, may

be used.

2) Electronic Charts

(Including

Electronic CHART

Database)

(Aircraft 20125 to

20181 with SB

100-46-02)

(Aircraft 20182

and up)

(Aircraft 20182

and up with SB

100-46-01)

C

2 0 (O) May be inoperative provided alternate procedures

are established and used.

D

2 0 May be inoperative provided procedures do not require

its use.

3) XM Graphical

Weather Function

(Including

Graphical Weather

Database)

(Aircraft 20125 and

up with SB

100-46-03)

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.

(cont’d)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

5 Page

BD-100-1A10 Date: Apr 28/19 46-2

1.

2.

Numb

e

r

Installed

System & Sequence No Item

Nombre

d’articles

installés

No de sys

tème/s

é

ri

e

ar

ticle

3.

Number Required For Dispatch

Nombre d'articles à expédier

46 – INFORMATION SYSTEMS

4.

Remarks or Exceptions

Remarques ou exceptions

10-01 Integrated Flight

Information System

(IFIS)

(Cont’d)

4) Enhanced Map

Overlay Function

(Including

Enhanced Map

Overlay Database)

(Aircraft 20125 to

20181 with SB

100-46-02)

(Aircraft 20182 and

up with SB

100-46-01)

C

1 0 (O) May be inoperative on either or both MFDs

provided alternate procedures are established and

used.

D

1 0 May be inoperative on either or both MFDs provided

procedures do not require its use.

20-1 XM Satellite System C

1 0 (O) May be inoperative provided alternate procedures

are established and used.

D

1 0 May be inoperative provided routine procedures do not

require its use.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 49-1

1.

2

.

N

umber Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de système/série

article

3. Number Required For Dispatch

Nom

bre d'articles à ex

p

édi

er

49 – APU

4.

Remarks or Exceptions

Remarques ou exceptions

11-01 Auxiliary Power Unit

(APU)

C

1 0 (M) May be inoperative provided:

a) Auxiliary Power Unit is deactivated,

b) Engine Driven Generator Channels are

operative, and

c) Operations with steep approach are not

conducted.

NOTE: Appropriate bleed source performance data

must be used.

11-02 APU Hour Meter C

1 0 (M) May be inoperative provided alternate method for

checking APU hour is used.

51-01 APU Load Control

Valve

C

1 0 (M) May be inoperative provided it is deactivated

CLOSED.

NOTE1: The APU is still available as source of

electrical power, if required.

NOTE2: Appropriate bleed source performance data

must be used.

|

51-02 AIR COND/BLEED

APU “ON”

Switch Light

(light function only)

C

1 0 (O)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

Original Page

BD-100-1A10 Date: Sep 30/03 49-2

1.

2.

Numb

er I

n

s

talled

System & Sequence N

o

Item

Nombre d’articles installés

N

o

de système

/série

article

3. Number Required For Dispatch

Nombre d'articles à expédier

49 – APU

4.

Remarks or Exceptions

Remarques ou exceptions

THIS PAGE INTENTIONALLY LEFT BLANK

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

1 Page

BD-100-1A10 Date: Mar 24/05 52-1

1.

2.

Number Installed

System & Sequen

ce N

o

I

te

m

Nombre d’articles installés

N

o

de système/série article

3. Number Required For Dispatch

Nombre d'articles à expédier

52 – DOORS

4.

Remarks or Exce

ptio

ns

Remarques ou exceptions

00-01 Exterior Door

Keyable Locks

***

D

- 0 May be inoperative provided affected lock does not

affect associated door normal operation.

10-01 Passenger Door

Power Assist

System

C

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

a) Door is verified manually operative, and

b) Opening damping feature is verified operative.

30-01 Baggage Door

Counterbalance

Systems

C

2 0 (M) Any or all may be inoperative provided:

a) Baggage door is verified closed, latched and

not used, and

b) Baggage door is placarded "BAGGAGE DOOR

INOPERATIVE - DO NOT OPEN".

NOTE: Baggage compartment is accessible through

the door located in cabin.

70-01 Door Indication

Systems

1) Passenger Door

Indication

System

C

1 0 (O) May be inoperative provided:

a) Door is CLOSED and LOCKED before each

departure,

b) External handle is verified STOWED before

each departure,

c) External pressure vent flap is verified CLOSED

before each departure, and

d) Internal mechanism indicator flag is verified

green before each flight.

2) Emergency Exit

Indication

System

C

1 0 (O) May be inoperative provided:

a) Door is CLOSED and LOCKED before each

departure, and

b) External pressure vent flap is verified CLOSED

before each departure.

(cont'd)

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

1 Page

BD-100-1A10 Date: Mar 24/05 52-2

1.

2.

Number Installed

System & Sequence N

o

Item

Nombre d’articles installés

N

o

d

e

système/série article

3. Number Required For Dispatch

Nombre d'article

s à ex

p

éd

ier

52 – DOORS

4.

Remarks or Exceptions

Remarques ou exceptions

70-01 Door Indication

Systems

(cont’d)

3) Cargo Door

Indication

System

C

1 0 (O) May be inoperative provided:

a) Door is CLOSED and LOCKED before each

departure,

b) External handle is verified STOWED before

each departure, and

c) External pressure vent flap is verified CLOSED

before each departure.

4) Aft Equipment

Bay Door

Indication

System

C

1 0 (O) May be inoperative provided door is CLOSED and

LOCKED before each departure.

5) Battery Bay

Door Indication

System

C

1 0 (O) May be inoperative provided door is CLOSED and

LOCKED before each departure.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

6 Page

BD-100-1A10 Date: May 05/22 73-1

1.

2.

Number Installed

System

& Sequence N

o

It

em

Nombre d’articles installés

N

o

de système/série article

3. Number Required For Dispatch

Nombre

d'art

i

cl

es à expédier

73 – ENGINE FUEL &

4.

Remarks or Exceptions

CONTROL Remarques ou exceptions

00-01 Engine Control

Systems

A

2 2

May be dispatched with “L and/or R ENGINE MINOR

FAULT” advisory message(s) provided repairs are

made in accordance with times established in the

Airworthiness Limitations Section of the Engine

Maintenance Manual.

NOTE: Repair Interval extensions are not permitted.

30-01 Fuel Flow Readouts B

2 1 (O) May be inoperative provided Fuel Used Readout is

considered inoperative (73-30-02).

30-02 Fuel Used Readout C

1 0 May be inoperative provided Fuel Quantity Gauging

Computer Channels are operative.

40-02 Fuel Filter

Impending Bypass

Indication Systems

C

2 1 (M) May be inoperative provided fuel filter element on

the affected engine is replaced before the first flight

after failure occurred and every 20 flight hours

thereafter.

|

40-03 Fuel Low

Temperature

Indication Systems

C

2 1 May be inoperative provided icing inhibitor is added to

the fuel.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

o

- N

o

de révision:

Original Page

BD-100-1A10 Date: Sep 30/03 73-2

1.

2.

Number Installed

System & Se

quence

N

o

Item

Nombre d’articles installés

N

o

de système/série article

3. Number Required For Dispatch

Nombre d'articles à e

xpédier

73 – ENGINE FUEL &

4.

Rem

arks

or

E

x

ceptions

CONTROL Remarques ou exceptions

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DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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System & Sequence N

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N

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de

système/séri

e arti

cle

3. Number Required For Dispatch

Nombre d'articles à expédier

74 – IGNITION

4.

Remarks

or Exceptions

Remarques ou exceptions

21-01 Engine Ignition

Systems

B

2 2 System(s) redundancy may be degraded as indicated

by “L/R ENG IGN FAULT” advisory message.

|

31-01 ENGINE IGNITION

“ON” Switch Light

(light function only)

C

1 0

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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System & Sequence N

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N

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de systè

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3. Number Required For Dispatch

Nombre d'articles à expédier

74 – IGNITION

4

.

Remarks or Exceptions

Remarques ou exceptions

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DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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Item

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système/série article

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Nom

bre d'articles à

expédier

76 – ENGINE CONTROL

4.

Remarks o

r Except

io

ns

Remarques ou exceptions

11-01 FADECs Automatic

Engine Control

Functions

1) SYNC Function

C

1 0

2) MACH HOLD

Function

(Not Applicable

To Aircraft With

AT System

Installed)

C

1 0

|

20-01 ENGINE AUTO

APR “OFF” Switch

Light

(light function only)

C

1 0

20-02 ENGINE MACH

HOLD “ON” Switch

Light

(light function only)

(Not Applicable

To Aircraft With

AT System

Installed)

C

1 0

|

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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1.

2.

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ed

Syst

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S

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o

It

e

m

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N

o

de

système/série article

3. Number Required For Dispatch

Nombre d'articles à exp

édier

76 – ENGINE CONTROL

4.

Remarks or Exceptions

Remarques ou exceptions

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DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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o

de système/séri

e article

3. Number Required For Dispatch

Nombre d'articles à expédier

77 – ENGINE INDICATING

4.

Rem

arks

or

Ex

ceptions

Remarques ou exceptions

31-01 Engine Vibration

Indications

B

2 1 May be inoperative provided:

a) Operations are not conducted in known or

forecast icing conditions, and

b) One Ice Detection System is operative.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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1.

2

.

Nu

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Ins

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System

&

Sequence N

o

Ite

m

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N

o

de

système/

série

ar

ticle

3. Number Required For Dispatch

Nombre

d'articles à exp

édier

77 – ENGINE INDICATING

4.

Remarks or Exceptions

Remarques ou exceptions

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DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

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Aircraft – Aéronef

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o

Item

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N

o

de

système/série

article

3. Number Required For Dispatch

Nombre d'articles à expédier

78 – EXHAUST

4.

R

emar

ks o

r

Exc

eptions

Remarques ou exceptions

30-01 Thrust Reverser

Systems

C

2 1 (M) May be inoperative provided:

a) Affected Thrust Reverser is stowed and locked,

b) Operations are conducted in accordance with

AFM performance data, and

c) Operations with steep approach are not

conducted.

|

C

2 0 (M) Any or all may be inoperative provided:

a) Affected Thrust Reverser is stowed and locked,

b) Operations are not conducted on wet or

contaminated runways, and

c) Operations with steep approach are not

conducted.

|

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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N

o

de

sy

stème/série article

3. Number Required For Dispatch

Nombre

d'articles à expédier

78 – EXHAUST

4.

Remarks or Exceptions

Remarques ou exceptions

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DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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de sys

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3. Number Required For Dispatch

Nombre d'articles à expédier

79 – OIL

4.

Rem

arks

o

r Excep

ti

ons

Remarques ou exceptions

30-01 Remote Oil Level

Indications

(Refuel/Defuel

Panel)

C

2 0 Any or all may be inoperative provided associated oil

tank sight gauge is used to determine oil level.

30-02 Oil Filter Impending

Bypass Indication

Systems

A

2 1 (M) May be inoperative provided:

a) Affected oil filter element is replaced, and

b) Repairs are made within three flight days.

|

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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Item

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N

o

de

syst

ème

/sér

ie

art

ic

le

3. Number Required For Dispatch

Nombre d'articles à expédier

79 – OIL

4.

Re

marks or Exceptions

Remarques ou exceptions

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DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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It

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N

o

de système/série article

3. Number Required For Dispatch

Nombre d'articles à expédier

80 – STARTING

4.

Remarks or Exceptions

Remarques ou exceptions

11-01 Air Turbine Starter

Valve

C

2 1 (M)(O) May be inoperative provided:

a) Valve is deactivated, and

b) Alternate starting procedures are established

and used to start the affected engine.

|

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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a

rtic

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3. Number Required For Dispatch

Nombre d'articles à expédier

80 – STARTING

4.

R

em

arks or Exceptions

Remarques ou exceptions

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DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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3 Section Page

BD-100-1A10 Date: Jun 21/11 2 TITLE-1

SECTION TWO

CAS

MESSAGE

ORIENTED

MMEL RELIEF

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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BD-100-1A10 Date: Jun 21/11 2 INT-1

INTRODUCTION

The following new section has been authorized in accordance with the provisions of TCCA MMEL GB Item 00-00-0,

Rev 1, or later, regarding dispatching directly from displayed CAS (Crew Alerting System) messages. “CAS

message” relief is an alternative to the standard method of MMEL dispatch relief, as is normally achieved through

fault isolation procedures, and the subsequent dispatch under the traditional LRU oriented MMEL relief. This

Section 2, has been developed with the objective of allowing flight crews to dispatch from the displayed CAS

message, without specifically identifying associated failed LRUs or components.

As Section 2 is intended as an alternative dispatch relief methodology, the LRU-oriented relief (Section 1) will be

retained in order to provide maximum flexibility for dispatch relief. Flight crews / operators may dispatch failures

with reference to either Section 1 or Section 2 of this MMEL to the advantage that either associated relief may

provide. Upon comparison, it will be recognized in some cases that dispatch relief provisos for posted CAS

messages to those of the related LRU dispatch relief, the provisos associated with the CAS message can appear

more restrictive in content and/or relief interval. Without the opportunity for fault isolation through maintenance, it

must be assumed that worst-case failure conditions always underlie the posted message - commensurately,

dispatch should be more restrictive. However, where maintenance personnel are available and fault isolation

conducted, relief provisos in Section 1 may be found to provide fewer or less stringent restrictions upon operations

and offer a longer relief interval.

Section 2 has been arranged in alphabetical order of the indicated CAS message, without association to ATA

Chapter. However, to avoid any possible mis-identification, each message is identified beneath as to its alert level.

Repair intervals (A, B, C & D) associated with CAS message reliefs herein, remain consistent with those of Section

1, and as described in the Definitions section in the front matter of this MMEL.

In conjunction with Section 2, a new separate dispatch procedures section has also been developed, also arranged

in alphabetical order of the indicated CAS message. Where deemed necessary, the familiar “(O)” indicates the

need for such supporting tasks, the scope of which shall be at the discretion of the approval authority. Acceptable

tasks include, but are not necessarily limited to the following duties:

a) Procedures described which exercise cockpit (or cabin) system controls utilized in normal flight operations;

b) Deactivation of affected systems, as achieved by pulling system breaker or use of remote electronic system

isolation;

c) Visual inspection behind panels (internal or external) which are accessible without tools via quick-release

latches and which clearly indicate their unlocked or unsafe state;(red/green safe window; flush fit latches).

d) Visual confirmation of remote gauge indications, or valve positions as provided by integral external

indicators.

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

Revision N

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BD-100-1A10 Date: Jun 21/11 2 INT-2

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DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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BD-100-1A10 Date: May 05/22 2 TOC-1

SECTION 2 Cover…………………………………………………………………………………………………….. TITLE-1

INTRODUCTION……………………………………………………………………………………………………………INT1

TABLE of CONTENTS……………………………………………………………………………………………………TOC1

MESSAGES…………………………………………………………………………………………………………………..2-1

CAS MESSAGES

PAGE

AIR COND FAULT (Advisory)

2-1

AT RETARD INHIBIT (Caution)

2-1

AUTO PRESS FAIL (Caution)

2-1

AUX HYD PUMP FAIL ON (Advisory)

2-1

CABIN PRESS FAULT (Caution)

2-2

ELECTRICAL FAULT (Advisory)

2-2

ICE DETECTOR FAIL (Caution)

2-2

ICE DETECTOR FAULT (Advisory)

2-2

L AUX BUS FAIL (Advisory)

2-2

L WSHLD HEAT FAIL (Caution)

2-3

MANUAL PRESS FAIL (Advisory)

2-3

NOSE GEAR DOOR (Caution)

2-3

NWS LIMIT EXCEEDED (Caution)

2-3

R WINDOW HEAT FAIL (Caution)

2-4

R WSHLD HEAT FAIL (Caution)

2-4

STBY INST BATT FAULT (Advisory)

2-4

TRIM AIR FAIL (Caution)

2-4

TABLE OF CONTENTS

DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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BD-100-1A10 Date: May 05/22 2 2-1

1.

CAS Indication

2.

Dispatch Consideration

AT RETARD INHIBIT (Caution)

(Auto Throttle System is installed

either via SB 350−22−002 or on

Aircraft 20937 and subsequent)

C (O) May be displayed provided:

a) Auto Throttle is confirmed disengaged and not used

throughout the flight, and.

b) LH and RH Thrust levers are verified to move freely

and maintain adequate friction, prior to each flight.

|

AIR COND FAULT

(Advisory)

C (O) May be inoperative provided:

a) AIR COND/BLEED AIR SOURCE rotary selector

switch is selected to OFF,

b) Ram Air Valve is selected OPEN,

c) PRESSURIZATION EMER DEPRESS switch is

selected ON, and

d) Operations are conducted unpressurized at or below

9000 ft. MSL.

AUTO PRESS FAIL

(Caution)

C (O) Aircraft may be dispatched provided:

a) AIR COND/BLEED AIR SOURCE rotary selector

switch is selected to OFF,

b) Ram Air Valve is selected OPEN,

c) PRESSURIZATION EMER DEPRESS switch is

selected ON, and

d) Operations are conducted unpressurized at or below

9000 ft. MSL.

AUX HYD PUMP FAIL ON

(Advisory)

B (O) Aircraft may be dispatched provided:

a) The AUX pump is verified to stop when selected to

OFF, and

b) The AUX pump is selected OFF after takeoff,

selected to AUTO before approach and OFF after

landing.

DEPARTMENT OF TRANSPORT

MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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1.

CAS Indication

2.

Dispatch Consideration

CABIN PRESS FAULT

(Caution)

B

(O) Aircraft may be dispatched provided:

a) Manual pressurization is verified operative

before flight,

b) No other CAS messages related to air

conditioning or pressurization is posted,

c) Ram Air Valve is verified operative, and

d) Operations are conducted at or below FL 250.

C (O) Aircraft may be dispatched provided:

a) AIR COND/BLEED AIR SOURCE rotary

selector switch is selected to OFF,

b) Ram Air Valve is selected OPEN,

c) PRESSURIZATION EMER DEPRESS switch is

selected ON, and

d) Operations are conducted unpressurized at or

below 9000 ft. MSL.

ELECTRICAL FAULT

(Advisory)

B (O) Aircraft may be dispatched provided Battery

temperature indications are verified operative before

each flight.

ICE DETECTOR FAIL

(Caution)

C (O) Aircraft may be dispatched for day operations

provided:

a) Affected detector is deactivated,

b) Anti-ice systems are turned ON when icing

conditions exist as defined in AFM.

C (O) Aircraft may be dispatched for night operations

provided:

a) Affected detector is deactivated,

b) Anti-ice systems are turned ON when SAT is

between +10 C and –40 C.

ICE DETECTOR FAULT

(Advisory)

C (O) Aircraft may be dispatched provided:

a) Affected detector is deactivated, and

b) Anti-ice systems are turned ON when icing

conditions exist as defined in AFM.

L AUX BUS FAIL

(Advisory)

C (O)

DEPARTMENT OF TRANSPORT

MINISTÈRE DES TRANSPORTS

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Aircraft – Aéronef

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1.

CAS Indication

2.

Dispatch Consideration

L WSHLD HEAT FAIL

(Caution)

C (O) Aircraft may be dispatched provided:

a) None of following messages are displayed:

L or R WINDOW HEAT FAIL

R WSHLD HEAT FAIL

ICE DETECTOR FAIL

b) Left windshield channel is deactivated, and

c) Operations are not conducted in known or forecast

icing conditions.

MANUAL PRESS FAIL

(Advisory)

C (O) Aircraft may be dispatched provided:

a) AIR COND/BLEED AIR SOURCE rotary selector

switch is selected to OFF,

b) Manual Pressurization switch is selected OFF,

c) Ram Air Valve is selected OPEN,

d) Pressurization EMER DEPRESS switch is selected

ON, and

e) Operations are conducted unpressurized at or below

9000 ft. MSL.

NOSE GEAR DOOR

(Caution)

A (O) Aircraft may be dispatched provided:

a) Flight is conducted with Landing Gear Down and

Landing Gear Retraction System is considered

inoperative (Section1 Item 32-30-01), and

b) Repairs are made within three flight days.

NOTE: Fuel Planning Data is contained in Flight Planning

and Cruise Control Manual– Special Operation

Data – Gear Down Operation.

NWS LIMIT EXCEEDED

(Caution)

B (O) Aircraft may be dispatched provided Nose wheel

Steering - Oversteer switch frangible pin (serves as

mechanical indicator) is intact before and after every towing

operation and before every flight.

NOTE: See MMEL 32-60-02.

|

DEPARTMENT OF TRANSPORT

MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef

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BD-100-1A10 Date: Jun 21/11 2 2-4

1.

CAS Indication

2.

Dispatch Consideration

R WINDOW HEAT FAIL

(Caution)

C (O) Aircraft may be dispatched provided:

a) Right Side Window Heating Channel is deactivated,

and

b) No more than one of the following messages is

displayed:

L WSHLD HEAT FAIL

R WSHLD HEAT FAIL, and

c) Operations are not conducted in known or forecast

icing conditions.

R WSHLD HEAT FAIL

(Caution)

C (O) Aircraft may be dispatched provided:

a) None of following messages are displayed:

L or R WINDOW HEAT FAIL

L WSHLD HEAT FAIL

ICE DETECTOR FAIL

b) Right windshield channel is deactivated, and

c) Operations are not conducted in known or forecast

icing conditions.

STBY INST BATT FAULT

(Advisory)

B Aircraft may be dispatched provided operations are not

conducted more than one hour from a suitable airport.

TRIM AIR FAIL

(Caution)

C O) Aircraft may be dispatched provided:

a) AIR COND/BLEED AIR SOURCE rotary selector

switch is selected to OFF,

b) Ram Air Valve is selected OPEN,

c) PRESSURIZATION EMER DEPRESS switch is

selected ON, and

d) Operations are conducted unpressurized at or below

9000 ft. MSL.