Dash 8 Series 400, DOT, Master Minimum Equipment List, PSM 1

E

To:

Date:

Subject:

Distribution

09 September, 2015

Dash 8 Series 400, DOT, Master Minimum Equipment List, PSM 1−84−16A.

This is Revision 7 of the Dash 8 Series 400, DOT, Master Minimum Equipment List (MMEL), PSM 1−84−16A, dated 09 September, 2015.

Any revision bars appear in this revision are only against the changes affected on this revision with Revision 7 date.

Remove all pages and replace with the attached DOT MMEL package at Revision 7.

We are providing you with the changes to DOT MMEL manual at Revision 7. Record the insertion of Revision

7 in the appropriate columns of the Log of Revisions page.

Revision 7 to the Dash 8 Series 400, DOT MMEL incorporates previously approved Temporary Revisions 140 to 156. Remove these TRs and record in the TR index.

The following is a breakdown of the changes followed by a description of the change:

Notes & Definitions page revised to add “Extended Overwater Operation” and also some minor editorial changes.

Item 21−30−1 − “CABIN PRESS Warning Light” (TR141) incorporated.

Item 21−30−2 − Cabin ALT Indicator (TR142) incorporated.

Item 21−30−3 − Cabin DIFF Pressure Indicator (TR143) incorporated.

Item 21−30−4 − Cabin RATE Indicator (TR144) incorporated.

Item 21−30−5 − Cabin Pressure Control System (TR145) incorporated.

Item 21−60−1 − Cabin Temp Control, updated current MMEL relief with editorial change to wording of provisos for the AUTO and MAN Modes case. Due to software issue revision bar appears on the entire item.

Item 23−30−1 − Alerting System (CHIME/LIGHT), revised to further clarified to include all the PACIS lights relief and to update CALL lights number installed.

Item 25−20−1 − Passenger Convenience Items/Non Essential Equipment and Furnishings NEF items, revised to update to reflect requirements to have NEF listed in tandem to it as this is the updated category listing according to TCCA MMEL Guidance Manual Rev. 7.

ITEM 25−20−8 − Revised the number required for dispatch is changed, 1 to 0 for case 2.

Item 25−30−1 − Galley Waste Compartment, update the MMEL to include relief for the Galley Waste

Compartment.

Item 25−40−1 − Exterior Lavatory Door Ashtrays, revised to add relief for aircraft with more than one exterior

PAGE 1

Rev 7 Sep 09/2015

E lavatory door ashtray as relief is currently only for aircraft with one lavatory door ashtray.

Item 25−50−3 − “Compartment Liners”. Relief is for both forward and aft cargo compartment liners.

Item 25−60−1 − Emergency Locator Transmitter, update to provide clarification to the procedures as well clarify current provisos to fall in line with CAR 605.38 and 605.39.

Item 25−60−6 − To update MMEL relief with a note defining “over water” to clarify proviso.

Item 25−60−9 − New MMEL relief is being proposed for life vests installed on the Q400 series aircraft.

Item 25−62−1 − To provide relief for inoperative Cabin Video Monitoring and Surveillance System partial failure.

Item 26−10−1 − Revision bar is for minor editorial change only. No changes to the item.

Item 26−10−2 − Minor editorial change.

Item 26−10−3 − Revised for 86 passenger configuration, TR 147.

Item 26−20−4− Revised for 86 passenger configuration, TR 148.

Item 28−20−1 − To update relief to include the partial failure of the Pressure Refueling System.

Item 28−20−2− New proposal to allow for relief for MASTER VALVE CLOSED indication on Q400 aircraft.

Item 28−40−8 − Revision bar due to software issue, no changes.

Item 29−10−2 − To create a new MMEL item for inoperative Hydraulic Firewall Shutoff Valve (HYD FSOV)

OPEN Indicator Light.

Item 30−20−2 − To update relief to include the option of an operational procedure to verify operation of heaters during flight.

Item 30−20−3 − To update MMEL provisos to change M# procedure to a M and O procedure.

Item 30−40−2 − Windshield heaters, revised. (TR 140)

Item 30−80−1 − Provisos updated to include night operation with the spigot light failed.

Item 31−60−5 − MMEL relief updated for the multifunctional Purpose Display (MFD2) on co−pilot side to meet new requirements imposed by the aircraft certification approval for Required Navigation Performance

Authorization Required (RNP AR) approach.

Item 32−50−1 − To extend the relief period to allow operators the ability to get to a maintenance base.

Item 33−10−2 − Revise MMEL to add relief for the Caution/Warning/Advisory Light System Brighten and

Dimming Function whose “BRT” function is inoperative.

Item 33−30−2 − Revised for 86 passenger configuration, (TR 149).

Item 33−40−8 − Revision bar due to software issue, no changes.

Item 33−50−2 − Revised the existing MMEL relief for Emergency Marker and Emergency Locator Signs in the classic Interior.

Item 34−20−6 − To update relief for Integrated Standby Instrument (ISI) to include relief for the STD Button.

Item 34−20−7 − New relief for the Inertial Reference System (IRS) optional installation, required only for

Required Navigation Performance Authorization Required (AR).

Item 34−50−1 − ATC Transponder / Altitude Reporting System, revised (TR 153).

Item 34−50−6 − Update the Global Positioning System (GPS) MMEL relief to meet new requirements (TR

154).

Item 34−60−1 − Update the MMEL relief for the Flight Directors (FD) to meet new requirements.

Item 34−60−2 − MMEL proviso updates to consider the RNP AR 0.3/0.3 approach, the TAWS Enhanced

PAGE 2

Rev 7 Sep 09/2015

E mode and to correct the existing relief for the FMS database (TR 155).

Item 35−30−3 − Revised for 86 passenger configuration (TR 150).

Item 38−10−2 − Item name revised.

Item 52−10−2 − Editorial change to proviso was made to change the applicable AFM reference. (TR 146).

Item 52−10−3 − Revised for 86 passenger configuration, (TR 151).

Item 52−10−4 − Updated MMEL wording with editorial change to proviso.

Item 52−10−5 − FUSELAGE DOORS warning system revised, (TR 152).

Item 52−50−1 − Fortified Flight Deck Door, revised (TR 156).

Item 52−50−2 − This item referred to Item 52−50−1.










We recommend that this letter of transmittal be retained and placed in the front of the manual for record purposes.

PAGE 3

Rev 7 Sep 09/2015

THIS PAGE INTENTIONALLY LEFT BLANK

E

DEPARTMENT OF TRANSPORT

MASTER MINIMUM EQUIPMENT LIST

MANUAL

PSM 1−84−16A

M.M.E.L. (DOT) REVISION 7 (SEP 09, 2015)

BOMBARDIER INC.

BOMBARDIER AEROSPACE COMMERCIAL AIRCRAFT

CUSTOMER SUPPORT

123 GARRATT BLVD., TORONTO, ONTARIO

CANADA M3K 1Y5

Copyright © 1999 − 2015 by Bombardier Inc.

All rights reserved. No part of this work may be reproduced or copied in any form or by any means without written permission of Bombardier Inc.

The Bombardier logo and de Havilland are registered trademarks of Bombardier Inc.

B

Initial Issue: Dec 24/1999

Revision 7: Sep 09/2015

"The information, technical data and the designs disclosed herein are the exclusive property of Bombardier Inc. or contain proprietary rights of others and are not to be used or disclosed to others without the written consent of

Bombardier Inc. The recipient of this document, by its retention and use, agrees to hold in confidence the technical data and designs contained herein. The foregoing shall not apply to persons having proprietary rights to such information, technical data or such designs to the extent that such rights exist."

Technical Publications

Manual Change Request

TO: MCR FOCAL, TECHNICAL PUBLICATIONS

BOMBARDIER AEROSPACE

123 GARRATT BLVD.

TORONTO, ONTARIO, CANADA, M3K 1Y5

MAIL STOP: N42−25 FAX: (416) 375−4538

E−MAIL ADDRESS: [email protected]

ALL fields marked with an asterisk * are required

Contact Information

*Name: *Corporation Name:

Address: City:

B

Name of Airline:

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Date:

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NOTE: Electronic submissions of MCRs are available on www.iflybombardier.com

Oct 04/2013

DEPARTMENT OF TRANSPORT

Approval Page

MASTER MINIMUM EQUIPMENT LIST

DHC−8 SERIES 400

MANUAL APPROVAL

This is to certify that the PSM 1−84−16A Dash 8 Series 400 Master Minimum Equipment List has been revised and incorporates Revision 7 and is D.O.T. Approved.

Approved:

Chief Flight Test

National Aircraft Certification for Minister of Transport

Date: 09 September, 2015

BOMBARDIER INC.

BOMBARDIER AEROSPACE REGIONAL AIRCRAFT

CUSTOMER SUPPORT

123 GARRATT BLVD.,

TORONTO, ONTARIO

CANADA M3K 1Y5




Bombardier Inc. DHC−8

Series 400

List of Effective Pages

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5

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7




Series 400

LOG OF REVISIONS

Log of Revisions

Page 1

Rev 7 Sep 09/2015

When revisions are received and inserted, record the relevant information in the appropriate columns of the

LOG OF REVISIONS below.

REV.

NO.

1

2

ISSUE

DATE

DATE

INSERTED

24 December,

1999

26 December,

1999

24 May 2002 24 May 2002

INSERTED

BY

DHI

DHI

REV.

NO.

ISSUE

DATE

DATE

INSERTED

INSERTED

BY

16 July 2004 16 July 2004

24 January

2008

28 November,

2011

26 March,

2014

09 September,

2015

24 January

2008

28 November

2011

26 March,

2014

DHI

DHI

DHI

DHI

BCSG: Bombardier Customer Service Group




Series 400

LOG OF REVISIONS

Log of Revisions

Page 2

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REV.

NO.

ISSUE

DATE

DATE

INSERTED

INSERTED

BY

REV.

NO.

ISSUE

DATE

DATE

INSERTED

INSERTED

BY


BOMBARDIER

MASTER MINIMUM EQUIPMENT LIST MANUAL (DOT)

EFFECTIVE TEMPORARY REVISIONS

The following Temporary Revisions are effective in your Manual at Revision 7 dated Sep 09, 2015.

TR

No.

Chapter/Section/

Subject/Pg. No.

ISSUE

DATE

TR

No.

Chapter/Section/

Subject/Pg. No.

ISSUE

DATE

EFFECTIVITY: ALL

Effective Temporary Revisions

PAGE 1 OF 1




Series 400

TEMPORARY REVISION INDEX

T.R. Index

Page 1

Rev 5 NOV 28/2011

Retain this index in the front of the manual. When Temporary Revisions are issued or cancelled, enter the relevant information in the columns below.

TEMPORARY

REVISION NO.

MMEL−1

SECTION /

PAGE NO.

31−2

ISSUE

DATE

18 Feb/00

DATE

INSERTED

21 Feb/00

INSERTED

BY

BCSG

DATE

REMOVED

24 May /02

REMOVED

BY

BCSG

REVISION

INCORP. IN /

REPLACED

WITH

Rev. 2

25−1

52−1

33−2

32−1

27−1

35−2

52−1

34−2

77−1

52−1

33−2

32−1

31−1

34−2

24−2

24−3

52−1

27−1

27−1

27−1

MMEL−10

MMEL−11

MMEL−12

MMEL−13

MMEL−14

MMEL−15

MMEL−16

MMEL−17

MMEL−2

MMEL−3

MMEL−4

MMEL−5

MMEL−6

MMEL−7

MMEL−8

MMEL−9

MMEL−18

MMEL−19

MMEL−20

MMEL−21

MMEL−22 27−2 02 Mar/01 02 Mar/01


09 May/00

09 May/00

09 May/00

12 May/00

29 May/00

29 May/00

16 Jun/00

28 Jun/00

18 Feb/00

23 Mar/00

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05 Aprr/00

09 May/00

09 May/00

09 May/00

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12 Sep/00

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16 Jun/00

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05 Apr/00

09 May/00

09 May/00

09 May/00

09 May/00

08 Aug/00

12 Sep/00

23 Oct/00

02 Mar/01

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

24 May /02

24 May /02

31 Oct/01

24 May /02

24 May /02

17 Oct/01

24 May /02

24 May /02

09 May /00

24 May /02

24 May /02

24 May /02

24 May /02

24 May /02

24 May /02

24 May /02

24 May /02

24 May /02

24 May /02

24 May /02

24 May /02

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

Rev. 2

Rev. 2

TR 32

Rev. 2

Rev. 2

TR 30

Rev. 2

Rev. 2

Rev. 2

Rev. 2

Rev. 2

Rev. 2

Rev. 2

TR 12

Rev. 2

Rev. 2

Rev. 2

Rev. 2

Rev. 2

Rev. 2

Rev. 2




Series 400


T.R. Index

Page 2

Rev 5 NOV 28/2011

TEMPORARY

REVISION NO.

SECTION /

PAGE NO.

ISSUE

DATE

22−1

27−1

30−2

28−1

30−2

52−1

33−3

21−1

26−2

26−3

73−1

61−1

32−1

32−1

33−2

33−2

52−1

PAGE 1

33−4

23−3

52−1

MMEL−31

MMEL−32

MMEL−33

MMEL−34

MMEL−35

MMEL−36

MMEL−37

MMEL−38

MMEL−23

MMEL−24

MMEL−25

MMEL−26

MMEL−27

MMEL−28

MMEL−29

MMEL−30

MMEL−39

MMEL−40

MMEL−41

MMEL−42

MMEL−43

MMEL−44 29−1 05 Dec/02 05 dec/02


31 Oct/01

31 Oct/01

06 Nov/01

07 Nov/01

13 Nov/01

13 Nov/01

23 Nov/01

18 Jan/02

04 May/01

10 Jul/01

28 Aug/01

14 Aug 01

18 Jun/01

23 Jul/01

19 Sep/01

17 Oct/01

28 Mar/02

28 Mar/02

04 Jul/02

04 Jul/02

23 Aug/02

31 Oct/01

31 Oct/01

06 Nov/01

07 Nov/01

13 Nov/01

13 Nov/01

23 Nov/01

18 Jan/02

04 May/01

10 Jul/001

28 Aug/01

14 Aug 01

18 Jun/01

23 Jul/01

19 Sep/01

17 Oct/01

28 Mar/02

28 Mar/02

04 Jul/02

04 Jul/02

23 Aug/02

DATE

INSERTED

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

INSERTED

BY

DATE

REMOVED

24 May /02

24 May /02

24 May /02

24 May /02

24 May /02

24 May /02

24 May /02

24 May /02

24 May /02

24 May /02

24 May /02

24 May /02

24 May /02

24 May /02

24 May /02

24 May /02

24 May /02

24 May /02

16 Jul/04

16 Jul/04

16 Jul/04

16 Jul/04

REMOVED

BY

Rev. 2

Rev. 2

Rev. 2

Rev. 2

Rev. 2

Rev. 2

Rev. 2

Rev. 2

REVISION

INCORP. IN /

REPLACED

WITH

Rev. 2

Rev. 2

Rev. 2

Rev. 2

Rev. 2

Rev. 2

Rev. 2

Rev. 2

Rev. 2

Rev. 2

Rev. 3

Rev. 3

Rev. 3

Rev. 3

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG




Series 400


T.R. Index

Page 3

Rev 5 NOV 28/2011

TEMPORARY

REVISION NO.

SECTION /

PAGE NO.

ISSUE

DATE

33−40−9

52−30−2

21−60−2

25−20−8

23−30−4

27−30−3

25−10−2

25−20−9

21−3

25−1

31−1

52−2

22−1

23−3

52−2

26−10−4

25−60−7

25−60−8

34−40−4

34−50−3

35−30−4

MMEL−53

MMEL−54

MMEL−55

MMEL−56

MMEL−57

MMEL−58

MMEL−59

MMEL−60

MMEL−45

MMEL−46

MMEL−47

MMEL−48

MMEL−49

MMEL−50

MMEL−51

MMEL−52

MMEL−61

MMEL−62

MMEL−63

MMEL−64

MMEL−65

MMEL−66 23−30−3 24 May/05 24 May/05


12 Nov/04

04 Oct/04

06 Dec/04

07 Dec/04

12 Jan/05

18 Jan/05

28 Apr/05

28 Apr/05

15 Nov/02

03 Dec/02

14 Aug/03

08 Apr/03

29 Aug 03

11 Sep/03

24 Jun/04

25 Oct/04

28 Apr/05

28 Apr/05

28 Apr/05

28 Apr/05

28 Apr/05

12 Nov 04

04 Oct/04

06 Dec/04

07 Dec/04

12 Jan/05

18 Jan/05

28 Apr/05

28 Apr/05

15 Nov/02

03 Dec/02

14 Aug/03

08 Apr/03

29 Aug 03

11 Sep/03

24 Jun/04

25 Oct/04

28 Apr/05

28 Apr/05

28 Apr/05

28 Apr/05

28 Apr/05

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

DATE

INSERTED

INSERTED

BY

DATE

REMOVED

24 Jan/08

24 Jan/08

29 Dec/05

24 Jan/08

24 Jan/08

24 Jan/08

24 Jan/08

24 Jan/08

16 Jul/04

16 Jul/04

16 Jul/04

16 Jul/04

16 Jul/04

16 Jul/04

16 Jul/04

24 Jan/08

24 Jan/08

24 Jan/08

24 Jan/08

24 Jan/08

24 Jan/08

24 Jan/08

REMOVED

BY

Rev. 4

Rev. 4

Rev. 4

TR 74

Rev. 4

Rev. 4

Rev. 4

Rev. 4

REVISION

INCORP. IN /

REPLACED

WITH

Rev. 3

Rev. 3

Rev. 3

Rev. 3

Rev. 3

Rev. 3

Rev. 3

Rev. 4

Rev. 4

Rev. 4

Rev. 4

Rev. 4

Rev. 4

Rev. 4

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG




Series 400


T.R. Index

Page 4

Rev 5 NOV 28/2011

TEMPORARY

REVISION NO.

SECTION /

PAGE NO.

ISSUE

DATE

34−40−6

52−50−12

21−20−5

21−20−6

21−20−7

73−20−2

61−20−2

76−10−1

22−10−6

23−40−1

73−20−3

73−20−4

25−20−10

21−20−8

26−10−2

21−60−2

21−50−3

32−30−1

23−80−1

23−30−4

30−80−2

MMEL−75

MMEL−76

MMEL−77

MMEL−78

MMEL−79

MMEL−80

MMEL−81

MMEL−82

MMEL−67

MMEL−68

MMEL−69

MMEL−70

MMEL−71

MMEL−72

MMEL−73

MMEL−74

MMEL−83

MMEL−84

MMEL−85

MMEL−86

MMEL−87

MMEL−88 28−40−11 11 Apr 08 11 Apr 08


27 Jan/06

05 Sep/06

31 May/05

31 May/05

31 May/05

08 Nov/06

08 Nov/06

08 Nov/06

24 May/05

24 May/05

23 Jun/05

23 Jun/05

27 Jul/05

14 Sep/05

14 Sep/05

29 Dec/05

06 Dec/06

02 Apr/07

29 Mar/07

28 Mar/08

04 Apr 08

27 Jan/06

05 Sep/06

31 May/05

31 May/05

31 May/05

08 Nov/06

08 Nov/06

08 Nov/06

24 May/05

24 May/05

23 Jun/05

23 Jun/05

27 Jul/05

14 Sep/05

14 Sep/05

29 Dec/05

06 Dec/06

02 Apr/07

29 Mar/07

28 Mar/08

04 Apr 08

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

DATE

INSERTED

INSERTED

BY

DATE

REMOVED

24 Jan/08

24 Jan/08

24 Jan/08

24 Jan/08

24 Jan/08

24 Jan/08

24 Jan/08

24 Jan/08

24 Jan/08

24 Jan/08

24 Jan/08

24 Jan/08

24 Jan/08

24 Jan/08

24 Jan/08

24 Jan/08

24 Jan/08

24 Jan/08

24 Jan/08

28 Nov/11

28 Nov/11

28 Nov/11

REMOVED

BY

Rev. 4

Rev. 4

Rev. 4

Rev. 4

Rev. 4

Rev. 4

Rev. 4

Rev. 4

REVISION

INCORP. IN /

REPLACED

WITH

Rev. 4

Rev. 4

Rev. 4

Rev. 4

Rev. 4

Rev. 4

Rev. 4

Rev. 4

Rev. 4

Rev. 4

Rev. 4

Rev. 5

Rev. 5

Rev. 5

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG




Series 400


T.R. Index

Page 5

Rev 5 NOV 28/2011

TEMPORARY

REVISION NO.

SECTION /

PAGE NO.

ISSUE

DATE

25−50−1

32−30−1

25−40−1

38−10−1

25−20−5

25−60−1

35−10−1

35−10−2

52−50−1

26−10−1

28−40−4

25−62−1

24−30−6

33−25−1

33−20−3

52−50−13

25−20−7

26−10−1

34−20−1

25−20−4

36−10−1

MMEL−97

MMEL−98

MMEL−99

MMEL−100

MMEL−101

MMEL−102

MMEL−103

MMEL−104

MMEL−89

MMEL−90

MMEL−91

MMEL−92

MMEL−93

MMEL−94

MMEL−95

MMEL−96

MMEL−105

MMEL−106

MMEL−107

MMEL−108

MMEL−109

MMEL−110 34−40−2 04 Aug 10 04 Aug 10


01 Sep 09

07 Oct 09

26 Oct 09

12 Nov 09

26 May 10

26 May 10

26 May 10

26 May 10

15 May 08

−

12 Jan 09

28 Jan 09

15 May 08

−

12 Jan 09

28 Jan 09

24 Mar 09 24 Mar 09

22 June 09 22 June 09

24 June 09 24 June 09

26 June 09 26 June 09

05 July 10

05 July 10

05 July 10

05 July 10

15 July 10

05 July 10

05 July 10

05 July 10

05 July 10

15 July 10

01 Sep 09

07 Oct 09

26 Oct 09

12 Nov 09

26 May 10

26 May 10

26 May 10

26 May 10

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

DATE

INSERTED

INSERTED

BY

DATE

REMOVED

04 Aug 10

28 Nov/11

28 Nov/11

28 Nov/11

28 Nov/11

28 Nov/11

28 Nov/11

28 Nov/11

28 Nov/11

−

28 Nov/11

28 Nov/11

28 Nov/11

11 Jan 11

24 Jan 11

07 Jan 11

28 Nov/11

28 Nov/11

28 Nov/11

28 Nov/11

28 Nov/11

28 Nov/11

REMOVED

BY

TR115

TR111

Rev. 5

Rev. 5

Rev. 5

Rev. 5

Rev. 5

Rev. 5

REVISION

INCORP. IN /

REPLACED

WITH

Rev. 5

TR106

Rev. 5

Rev. 5

Rev. 5

TR117

TR116

Rev. 5

Rev. 5

Rev. 5

Rev. 5

Rev. 5

Rev. 5

Rev. 5

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG




Series 400


T.R. Index

Page 6

Rev 6 Mar 26/2014

TEMPORARY

REVISION NO.

SECTION /

PAGE NO.

ISSUE

DATE

MMEL−119

MMEL−120

MMEL−121

MMEL− 122

MMEL− 123

MMEL− 124

MMEL− 125

MMEL− 126

MMEL−111

MMEL−112

MMEL−113

MMEL−114

MMEL−115

MMEL−116

MMEL−117

MMEL−118

MMEL− 127 28−40−11

MMEL− 128 25−20−2

MMEL− 129 52−10−4

MMEL− 130 28−40−10

MMEL− 131 31−60−3

25−50−1

25−10−2

34−40−6

34−60−2

52−50−13

33−20−3

33−25−1

38−30−1

22−10−6

33−20−2

33−50−2

29−30−4

33−20−2

23 −50−7

31−30−1

26−20−2

MMEL− 132 29−30−8 24 Jul 12 24 Jul 12


21 Nov 11

13 Jan 12

13 Jan 12

23 Mar 12

02 May 12

16 May 12

05 Jun 12

05 Jun 12

04 Aug 10

13 Aug 10

04 Aug 10

20 Dec 10

07 Jan 11

10 Jan 11

11 Jan 11

11 Jan 11

05 Jun 12

05 Jun 12

05 Jun 12

20 Jun 12

20 Jul 12

21 Nov 11

13 Jan 12

13 Jan 12

23 Mar 12

02 May 12

16 May 12

05 Jun 12

05 Jun 12

04 Aug 10

13 aug 10

04 Aug 10

20 Dec 10

07 Jan 11

10 Jan 11

11 Jan 11

11 Jan 11

05 Jun 12

05 Jun 12

05 Jun 12

20 Jun 12

20 Jul 12

DATE

INSERTED

INSERTED

BY

26 Mar 14

26 Mar 14

02 May 12

26 Mar 14

26 Mar 14

26 Mar 14

26 Mar 14

26 Mar 14

DATE

REMOVED

15

June/2011

15

June/2011

26 Mar 14

26 Mar 14

26 Mar 14

26 Mar 14

26 Mar 14

26 Mar 14

26 Mar 14

26 Mar 14

26 Mar 14

26 Mar 14

26 Mar 14

26 Mar 14

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

REMOVED

BY

Rev 6

Rev 6

Rev 6

Rev 6

Rev 6

Rev 6

TR123

Rev 6

REVISION

INCORP. IN /

REPLACED

WITH

Rev. 5

Rev. 5

Rev 6

Rev 6

Rev 6

Rev 6

Rev 6

Rev 6

Rev 6

Rev 6

Rev 6

Rev 6

Rev 6

Rev 6

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG




Series 400


T.R. Index

Page 7

Rev 7 Sep 09/2015

TEMPORARY

REVISION NO.

SECTION /

PAGE NO.

ISSUE

DATE

21−30−1

21−30−2

21−30−3

21−30−4

21−30−5

52−10−2

26−10−3

26−20−4

31−60−5

31−51−1

25−50−2

34−50−1

52−10−5

35−20−1

31−60−5

30−40−2

33−30−2

35−30−3

52−10−3

52−10−5

34−50−1

MMEL− 141

MMEL− 142

MMEL− 143

MMEL− 144

MMEL− 145

MMEL− 146

MMEL− 147

MMEL− 148

MMEL− 133

MMEL−134

MMEL−135

MMEL− 136

MMEL− 137

MMEL− 138

MMEL− 139

MMEL−140

MMEL− 149

MMEL− 150

MMEL− 151

MMEL− 152

MMEL− 153

MMEL− 154 34−50−6 24 Apr 15 05 May 15


24 Jul 12

22Aug 12

10 Sep 12

15 Oct 12

15 Oct 12

07 Jul 12

13 May 13

10 Apr 14

14 May 14

14 May 14

14 May 14

14 May 14

14 May 14

14 May 14

14 May 14

14 May 14

14 May 14

14 May 14

14 May 14

14 May 14

24 Apr 15 24 Apr 15

24 Apr 15 05−May−15

24 Apr 15

24 Apr 15

24 Apr 15

24 Apr 15

24 Apr 15

24 Jul 12

22 Aug 12

10 Sep 12

15 Oct 12

15 Oct 12

07 Jul 12

13 May 13

10 Apr 14

05 May 15

05 May 15

05 May 15

05 May 15

05 May 15

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

DATE

INSERTED

INSERTED

BY

DATE

REMOVED

09 Sep 15

09 Sep 15

09 Sep 15

09 Sep 15

09 Sep 15

09 Sep 15

09 Sep 15

09 Sep 15

13 May 13

26 Mar 14

26 Mar 14

26 Mar 14

26 Mar 14

26 Mar 14

26 Mar 14

09 Sep 15

09 Sep 15

09 Sep 15

09 Sep 15

09 Sep 15

09 Sep 15

09 Sep 15

REMOVED

BY

Rev 7

Rev 7

Rev 7

Rev 7

Rev 7

Rev 7

Rev 7

Rev 7

REVISION

INCORP. IN /

REPLACED

WITH

TR 139

Rev 6

Rev 6

Rev 6

Rev 6

Rev 6

Rev 6

Rev 7

Rev 7

Rev 7

Rev 7

Rev 7

Rev 7

Rev 7

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG

BCSG




Series 400


T.R. Index

Page 8

Rev 7 Sep 09/2015

TEMPORARY

REVISION NO.

SECTION /

PAGE NO.

MMEL− 155

MMEL− 156

34−60−2

52−50−1

ISSUE

DATE

24 Apr 15

24 Apr 15

DATE

INSERTED

INSERTED

BY

DATE

REMOVED

05 May 15

05 May 15

BCSG

BCSG

09 Sep 15

09 Sep 15

REMOVED

BY

BCSG

BCSG

REVISION

INCORP. IN /

REPLACED

WITH

Rev 7

Rev 7





Series 400


T.R. Index

Page 9

Rev 7 Sep 09/2015

TEMPORARY

REVISION NO.

SECTION /

PAGE NO.

ISSUE

DATE

DATE

INSERTED

INSERTED

BY

DATE

REMOVED

REMOVED

BY

REVISION

INCORP. IN /

REPLACED

WITH





Series 400

TABLE OF CONTENTS

Page 1

Rev 5 NOV 28/2011

System No.

33

34

35

36

29

30

31

32

25

26

27

28

21

22

23

24

61

71

73

76

38

45

49

52

77

79

Preamble

Notes & Definitions

System

Air Condtioning

Automatic Flight Control

Communication

Electrical Power

Equipment and Furnishings

Fire Protection

Flight Controls

Fuel

Hydraulic Power

Ice and Rain Protection

Indicating and Recording Systems

Landing Gear

Lights

Navigation

Oxygen

Pneumatics

Water/Waste

Central Maintenance System

Auxiliary Power Unit

Doors

Propellers

Power Plant

Engine Fuel and Control

Engines

Engine Indicating

Engine Oil

Page

29−1

30−1

31−1

32−1

33−1

34−1

35−1

36−1

21−1

22−1

23−1

24−1

25−1

26−1

27−1

28−1

38−1

45−1

49−1

52−1

61−1

71−1

73−1

76−1

77−1

79−1





Series 400

Page 1

Rev 5 NOV 28/2011

PREAMBLE

All equipment installed on an aircraft in compliance with the Airworthiness Standards and the Operating Rules must be operative. However, CARs 605.07 permits the publication of a Master Minimum Equipment List (MMEL) where compliance with certain equipment requirements is not necessary 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 equipment 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 applying 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, 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 (M) and (M#) procedures identified in the MMEL are required to be performed once prior to dispatching with MEL relief. If there is a requirement to perform the procedures more frequently, for example, prior to each flight, then this is clearly stated in the provisos. The same principle applies to the (O) procedures, although in some cases it is required that certain equipment be confirmed operative and this equipment is checked regularly in accordance with the normal Flight Manual procedures. When an item of equipment is discovered to be inoperative, it is reported by making an entry in the Aircraft Maintenance

Record/Journey Logbook. The item is then either repaired or deferred per the MEL. Alternatively, the aircraft must be in compliance with CAR sections 605.08 (2) or 605.09 (2) which specify the requirements for operating an aircraft subject to the conditions of flight permit and the subordinate position of a MEL with regard to an

Airworthiness Directive (AD) for the same Item. MEL conditions and limitations do not relieve the operator from determining that the aircraft is in condition for operation with items of equipment inoperative. (See CAR

605.08(1)).

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.

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

Page 2

Rev 5 NOV 28/2011




Series 400

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.




Series 400

Page 1

Rev 5 NOV 28/2011

Notes and Definitions

1. System Definitions

System numbers are based on the Air Transport Association (ATA) Specification Number 100 and items are numbered sequentially.

a) “Items” (Column 1) means the equipment, system, component, or function listed in the “Item” column.

b) “Number Installed” (Column 2) is the number (quantity) of items normally 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.

“***”symbol in Column 1 indicates an item which is not required by regulation 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 item “if installed”.

c) “Number Required for Dispatch” (Column 3) is the minimum number (quantity) of items required for operation provided the conditions specified in Column 4 are met.

"−" symbol in Column 2 and/or Column 3 indicates a variable number (quantity) of the item installed.

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.

d) “Remarks or Exceptions” (Column 4) in this column includes a statement either prohibiting or permitting operation with a specified number of items inoperative, provisos (conditions and limitations) for such operation, and appropriate notes.

e) A “vertical bar” (change 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.

f) “Approved” means approved by the Minister (appropriate civil aviation authority).

g) “Master Minimum Equipment List” means a document approved by the Minister that establishes the aircraft equipment allowed to be inoperative under the conditions specified therein for a specific type of aircraft.

h) “Minimum Equipment List” means a document approved by the Minister that authorizes an operator to dispatch an aircraft with aircraft equipment inoperative under the conditions specified therein.

i) “Minister” means the Minister of Transport.

2. “Administrative control items”means an item listed by the operator in the MEL for tracking and informational 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 such as the Structural Repair Manual. 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.

3. “Aircraft Crew” is considered to be flight crew members, flight attendants, aircraft maintenance crew engineers and supervisory crew members.

4. “Airplane Flight Manual” (AFM) is the document required for type certification and approved by Transport

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

Page 2

Rev 7 Sep 09/2015




Series 400

5. “Alphabetical symbol” in Column 4 indicates a proviso (condition or limitation) that must be complied with for operation with the listed item inoperative.

6. "Alternate Procedures" includes alternate normal, abnormal and emergency procedures.

7. “As required by regulations”, “As required by FAR” and other similar statements mean that the listed item is subject to certain provisions (restrictive or permissive) expressed in such regulations as the

Canadian Aviation Regulations, Federal Aviation Regulations, or the Airworthiness Manual, etc. Unless the

MMEL provides otherwise, the items specified by these requirements must be operative.

8. “Class 1 failures” are failures that prevent continued operation of a specific LRU or channel and are annunciated via advisory messages, cautions, warnings or advisory lights in the flight compartment.

Dispatch with such posted failures are to be in accordance with the MMEL. “Class 2 failures” are failures which do not prevent continued system function. These faults will not be annunciated to the flight crews and the absence of the higher level alert (warning, caution, advisory) indicates that the system/component is operating within its approved operating limits or tolerances. Such faults would be evident during maintenance interrogation performed on opportunity basis. Class 2 faults do not affect dispatch and will be listed in the Fault Isolation Manual (FIM). Class 2 faults will be left to the discretion of the operators when these faults are to be rectified.

9. “Considered Inoperative” as used in the provisos, remarks or exceptions means that item must be treated for dispatch, taxi and flight purposes as though it were inoperative. The item shall not be used or operated until the original deferred item is repaired. Additional actions include: documenting the item on the dispatch release (if applicable), placarding, and complying with all remarks, exceptions, and related MMEL provisions, including any (M) and (O) procedures and observing the repair category.

10. “Crew Members” (from CARS) means a person assigned to duty in an aircraft during flight time.

11. “Day of Discovery” is the calendar day an equipment/instrument malfunction was discovered. 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

12. “Deactivated” and “Secured” means that the specified component must be put into an acceptable condition for safe flight. An acceptable method of deactivating and securing will be established by the operator for inclusion in his/her MEL.

13. “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.

14. “ETOPS” refers to extended range (ER) operations of a two−engine airplane which has a type design approval for ER operations and complies with the provisions of TP 6327 (ETOPS).

15. “Excess Items” means those items installed that are excess to the requirements.

16. “Extended Overwater Operation” means operations over water at a horizontal distance of more than 50 nautical miles from the nearest shore.

17. “Federal Aviation Regulation (FAR)” means the applicable portions of the Federal Aviation Act and

Federal Aviation Regulations.

18. “Flight Crew Member” (from CARS) means a crew member assigned to act as pilot or flight engineer of an aircraft during flight time.




Series 400

Page 3

Rev 7 Sep 09/2015

19. “Flight Day” means a 24 hour period (e.g. 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.

20. “Icing Conditions” means an atmospheric environment that may cause ice to form on the aircraft or in the engine(s)

21. “Indication” is where a number of parameters are reported on a line replaceable unit. To allow relief for individual parameters being inoperative rather than the entire unit, the word indication is used as opposed to indicator.

22. “Indicator” is a line replaceable unit. The parameters displayed can be analogue or digital. To allow relief for the line replaceable unit rather than individual parameters we use the word indicator.

23. “Inoperative” means a system and/or 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).

NOTE: A caution or warning light is considered inoperative if either it fails to illuminate (ie. during lamp test) or if it fails to extinguish (ie. is illuminated continuously).

24. “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).

25. “Is not used” in the provisos, remarks or exceptions for an MMEL item may specify that another item relieved in the MMEL “is not used.” In such cases, crew members should not activate, actuate, or otherwise utilize that component or system under normal operations. It is not necessary for the operators to accomplish the (M) procedures associated with the item. However operational requirements must be complied with, and an additional placard must be affixed, to the extent practical, adjacent to the control or indicator for the item that is not used to inform crew members that a component or system is not to be used under normal operations.

26. “(M)” symbol indicates a requirement for a specified maintenance procedure which must be accomplished prior to operation with the listed item inoperative. 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 must be accomplished by maintenance personnel (see “(M#)” below). The satisfactory accomplishment of all maintenance procedures, regardless of who perform them, is the responsibility of the operator.

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

NOTE: The (M) symbol is required in the operator’s MEL unless otherwise authorized by

Transport Canada.

27. “(M#)” symbol indicates a requirement for maintenance personnel to accomplish an “(M)” procedure.

28. “Maintenance Instruction” indicates maintenance instructions that must be accomplished prior to operation with the listed item inoperative, as per “(M)”procedure above.

Page 4

Rev 7 Sep 09/2015




Series 400

29. “Notes” in Column 4 provides additional information for crew member 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.

30. “(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 a crew member; 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 a part of the operator’s manual or

MEL. Recording of the accomplishment of required specific operations procedures in the log book will be accomplished by adding the following statement to the “Instructions for Journey Log Book Use” found in the

Operators Journey Log Book to cover those items requiring Operating Procedures.

NOTE: The (O) symbol is required in the operator’s MEL unless otherwise authorized by

Transport Canada.

31. “Operating Instruction” indicates operating instructions that must be accomplished prior to operation with the listed item inoperative as per “(O)”procedure above.

32. “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.

33. “Placarding” Each inoperative item must be placarded to inform and remind the crew members 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.




Series 400

Page 5

Rev 7 Sep 09/2015

34. Repair Intervals: All users of an MEL must effect repairs to inoperative systems or components, deferred in accordance with the MEL, at or prior to the repair time intervals established by the following letter designators:

“Category A”

Items in this category shall be repaired within the time interval specified in the “Remarks or

Exceptions” column of the operator’s approved MEL. Whenever the proviso in the “Remarks or

Exceptions” column of the MMEL states cycles or flight time, the time interval begins with the next flight. Whenever the time interval is listed as flight days, the time interval begins on the flight day following the day of discovery.

“Category B”

Items in this category shall be repaired within three (3) consecutive calendar days, excluding the day of discovery. For example, if it were discovered at 10 am 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, excluding the day of discovery. For example, if it were discovered at 10 am on January 26th, the 10 day interval would begin at midnight the 26th and end at midnight February 5th.

“Category D”

Items in this category shall be repaired within one hundred and twenty (120) consecutive calendar days, excluding the day of discovery.

The letter designators are inserted in Column 1 adjacent to Column 2.

No specified repair interval: Items in this category do not have a limiting repair interval and is left to the operator”s discretion when this item is to be repaired. An example of an MMEL item with no specified repair interval is passenger convenience items. Passenger convenience items that require a specific repair interval limitation will be addressed as a separate MMEL item.

35. “Time Limited Dispatch” relief that is subject to time limited dispatch expressed as a specific number of engine hours or cycles, and will start in accordance with the times established by the engine manufacturer or as indicated in the remarks column of the MMEL. Time limited relief cannot be extended.

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

Flight Rules (IFR) flight plan.

37. “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.

38. “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.




Aircraft − Aeronef

Bombardier Inc. DHC−8 Series 400

MINISTERE DES TRANSPORTS

LIST PRINCIPALE D

Revision No./Date − No de révision/Date

Rev 6 Mar 26/2014

Page

21−1

Systems & Nos de

Sequence système

Numbers de série

1.

Item − Article

2. Number installed − Nombre d’articles installés

3. Number required for dispatch − Nombre requis pour le départ

4. Remarks or Exceptions − Remarques ou exceptions

21 AIR CONDITIONING

−20−1 Distribution Damper

−20−2 Recirculation Fan

1) Pre−Mod 4−126236 and Pre−Mod 4−126211 or Pre−Mod 4−126212

C 1

B 1

C 1

0

0

0

May be inoperative.

May be inoperative provided: a) The Fan is switched OFF, and b) The Standby Magnetic Compass is considered inoperative.

May be inoperative provided Fan is switched OFF.

2) Pre−Mod 4−126236 and Mod 4−126211 or

Mod 4−126212

−20−3 Flow (Pack) Control and

Shutoff Valve

C 1 0

C 3 2

(M#) May be inoperative provided: a) The Valve is secured in the open position, b) The Nacelle Shutoff Valves are verified operative, and c) Both digital (AUTO) channels of the ECU are verified operative.

May be inoperative.

−20−4 Display Cooling Fans

−20−5 SIDE WINDOW DEMIST

Vent Controls

−20−6 Low Level Vent Controls

A 2

C 2

A 2

C 2

1

0

1

0

One may be inoperative provided: a) Aircraft is dispatched for one flight day.

b) Airflow from the side window vent on the inoperative side is confirmed by the pilot.

(M#) May be inoperative provided the affected side(s) is failed in the open position.

One may be inoperative provided: a) Aircraft is dispatched for one flight day.

b) Airflow from the side window vent, on the side with the inoperative low level vent, is confirmed by the pilot.

(M) May be inoperative provided the Low Level Vent position is confirmed and lever moved to closed position.

Page

21−2




Rev 7 Sep 09/2015


LIST PRINCIPALE D






1.



21 AIR CONDITIONING (CONT’D)



−20−7 FLT COMPT GASPERS

(Small and Large)

−20−8 Aft Baggage Compartment

Vent Valves

1) Inlet and outlet vent valves

C 4

C 2

0 May be inoperative provided comfort level is acceptable to the pilot.

−30−1 CABIN PRESS Warning

Light

−30−2 Cabin ALT Indicator

C 2

2) VENT VALVE INLT and

VENT VALVE OUTLT

CLOSED advisory lights

C 2

C 1

C 1

D 1

0

0

0

0

0

0

(M) May be inoperative in closed position provided: a) Inlet and outlet valves (shut off valves) are deactivated, b) VENT VALVE INLT and VENT VALVE OUTLT

CLOSED advisory lights are verified illuminated prior to each flight, and c) Live animals are not carried.

May be inoperative in open position provided: a) The baggage compartment is empty or, for ballast purpose, use of bags (made of glass fiber or Kevlar) of sand or ingots of non−magnetic metals (such as lead) is acceptable.

May be inoperative in open position provided: a) The baggage compartment is empty or, for ballast purpose, use of bags (made of glass fiber or Kevlar) of sand or ingots of non−magnetic metals (such as lead) is acceptable.

May be inoperative provided flight is conducted at or below 10,000 feet MSL, per AFM Supplement 113,

UNPRESSURIZED FLIGHT − BLEED ON.

(O) May be inoperative provided: a) The Cabin DIFF Pressure Indicator is verified operative, and b) A chart is provided to convert cabin differential pressure to cabin altitude.

(O) May be inoperative provided flight is conducted in an unpressurized configuration, at or below 10,000 feet MSL, in accordance with AFM Supplement 113,







LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

21−3




1.






−30−3 Cabin DIFF Pressure

Indicator

C 1

−30−4 Cabin RATE Indicator

D 1

C 1

D 1

0

0

0

0

(O) May be inoperative provided: a) The Cabin ALT Indicator is verified operative, and b) A chart is provided to convert cabin altitude to cabin differential pressure.



May be inoperative provided all other instruments and functions of the Pressurization System are operative.



−30−5 Cabin Pressure Control

System

1) AUTO and MAN Modes A 2

2) AUTO Mode A 1

0

0

(M)(O) May be inoperative provided: a) The FWD OUTFLOW valve and DUMP functions are verified operative, b) The AFT OUTFLOW valve is verified open, c) The flight is conducted in an unpressurized configuration, at or below 10,000 feet MSL, in accordance with AFM Supplement 113,

UNPRESSURIZED FLIGHT − BLEED ON, and d) Repairs are made within three flight days.

(M) May be inoperative provided: a) MAN control is verified operative, b) The FWD OUTFLOW control and the DUMP function are verified operative, c) Cabin RATE Indicator, Cabin ALT Indicator, and

Cabin DIFF Pressure Indicator are verified operative, and d) Repairs are made within three flight days.

Page

21−4




Rev 6 Mar 26/2014


LIST PRINCIPALE D






1.






3) MAN Mode C 1 0 (M) May be inoperative provided: a) AUTO control is verified operative, b) The FWD OUTFLOW control and the DUMP function are verified operative, c) Cabin RATE Indicator, Cabin ALT Indicator, and

Cabin DIFF Pressure Indicator are verified operative.

−30−6 Aft Valves

1) Aft Outflow Valve C 1

2) Aft Safety Valve

−50−1 Air Cycle Machines (ACM) C 2

−50−2 Turbine Shut−Off Valves C 2

−50−3 Pack Bypass Valve


Vent Valves

C 1

C 2

0

0

1

1

1

(M)(O) May be inoperative provided: a) The AFT OUTFLOW valve is verified open, and b) Flight is conducted in an unpressurized configuration, at or below 10,000 feet MSL, in accordance with AFM, Section 4, Paragraph

4.16.7.

(M)(O) May be inoperative provided: a) The AFT OUTFLOW valve is verified open, and b) Flight is conducted in an unpressurized configuration, at or below 10,000 feet MSL, in accordance with AFM, Section 4, Paragraph

4.16.7.

May be inoperative provided the associated PACKS switch is selected and remains OFF.

(M#) May be inoperative provided: a) Turbine Shut−Off Valve is secured in the closed position, and b) Associated PACKS switch is selected and remains OFF.

(M#) May be inoperative provided: a) Pack Bypass Valve is locked in the closed, position, and b) Associated PACKS switch is selected and remains OFF.

Deleted. Refer to item 21−20−8.






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

21−5




1.






−60−1 CABIN TEMP CONTROL

1) AUTO and MAN Modes C 1

2) AUTO Mode

3) MAN Mode

−60−2 DUCT TEMP GAUGE

C 1

C 1

C 1

1) CABIN Temperature C 1

2) CAB DUCT

Temperature

C 1

3) FC DUCT Temperature C 1

0

0

0

0

0

0

0

(M) May be inoperative provided: a) The associated CABIN PACK is considered inoperative and is selected and remains OFF, and b) FLT COMP TEMP CONTROL is verified operative.

(M) May be inoperative provided: a) MAN control is verified operative, and b) DUCT TEMP indicator is verified operative.

(M) May be inoperative provided AUTO control is verified operative.

May be inoperative provided Flight Attendant

Temperature Control is operative and flights are conducted in accordance with AFM supplement 85,

Operation with inoperative CAB DUCT/CABIN/FC

Duct Gauge.

May be inoperative provided Flight Attendant

Temperature Control is operative.

May be inoperative provided flights are conducted in accordance with AFM supplement 85, Operation with

Inoperative CAB DUCT/CABIN/FC Duct Gauge.

May be inoperative provided flights are conducted in accordance with AFM supplement 85, Operation with

Inoperative CAB DUCT/CABIN/FC Duct Gauge.

−60−3 FLT COMP TEMP

CONTROL

1) AUTO and MAN Modes C 2 0 (M) Both may be inoperative provided: a) The associated FLT COMP PACK is considered inoperative and is selected and remains OFF, and b) CABIN TEMP CONTROL (AUTO & MANUAL) is verified operative.

Page

21−6




Rev 6 Mar 26/2014


LIST PRINCIPALE D






1.






2) AUTO Mode C 1

3) MAN Mode C 1

−60−4 Flight Attendant Control

Panel − Cabin Temperature

Control and CABIN TEMP indication

C −

0

0

0

(M) May be inoperative provided: a) MAN control is verified operative, and b) DUCT TEMP indicator is verified operative.

(M) May be inoperative provided AUTO control is operative.

One or all functions/indications may be inoperative provided cabin temperature control is available from the flight deck.

NOTE:

Flight Attendant control of cabin temperature is not available if MANUAL cabin temperature control is selected in the cockpit.






LIST PRINCIPALE D


Rev 6 Mar 26/2014

Page

22−1




1.





22 AUTOMATIC FLIGHT CONTROL

−10−1 A/P DISENG Annunciators

(Glareshield)

C 2 1 May be inoperative.

C 2 0 May be inoperative provided autopilot is not used.

−10−2 Autopilot

1) Autopilot

2) Autopilot Pitch Trim

System (AP PITCH TRIM

FAIL)

−10−3 Tactile Control Steering

(TCS) Switches

B 1

B 1

C 2

0

0

0

Any mode functioning normally may be used.

May be inoperative provided: a) Manual pitch trim is operative, b) Autopilot is considered inoperative and not used, and c) Flap Auto Pitch Trim (AUTO TRIM FAIL) is considered inoperative and not used.

May be inoperative.

−10−4 Flight Guidance Control

Panel (FGCP)

D 2

C 1

C 4

1

1

0

May be inoperative on the pilot not flying side.

Individual modes of operation may be inoperative provided that heading bugs, nav source selectors and course selection functions are operative.

May be inoperative.

Flight Guidance Control

Panel Indicators (AP, HSI

SEL only)

−10−5 Yaw Damper System B 1 0

−10−6 A/P DIS Switches B 2

C 2

0

1

(M) May be inoperative.

NOTE:

Autopilot will not be available.

May be inoperative provided the Autopilot is considered inoperative and not used.

One may be inoperative provided: a) The Autopilot is not used below 1,000 ft. AGL, b) Approach minimums do not require the use of the autopilot, and c) The pilot flying has the operative disconnect.







LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

23−1




23 COMMUNICATION

−10−1 Communication Systems

Transmitters and Receivers

(VHF, HF and UHF)

−10−2

***

−20−1

***

“Flitefone (or equivalent)”

System

SELCAL System

D −

D 1

C 1

D 1

−20−2

***

1.





Aircraft Communications

Addressing and Reporting

System (ACARS)

C 1

2

0

0

0

0

Any in excess of those required by regulations and not powered by an essential bus may be inoperative.


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

May be inoperative provided procedures do not require its use.


ACARS Printer

D 1

C 1

D 1

0

0

0

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

(M)(O) May be inoperative provided the printer is deactivated and secured, and alternate procedures are established and used.


−30−1 Alerting System

(CHIME/LIGHT)

1) Passenger

Configuration a) Flight Deck Call Light B 2 0 b) Flight Deck EMER Light B 2 c) Flight Deck PA Light B 2

0

0

May be inoperative provided the flight deck chime is operative.



Page

23−2




Rev 7 Sep 09/2015


LIST PRINCIPALE D






1.



23 COMMUNICATION (CONT’D)



d) Flight Attendant Call

Light e) Flight Attendant EMER

Light f) Flight Attendant PA

Light

B

B

B

2

2

2 g) Flight Attendant Chime B −

0

0

0

0

May be inoperative provided: a) The PA system is operative, and b) Affected alert is not used for lavatory smoke detector alerting.




2) Cargo Configuration

Flight Deck Call Light B 2

−30−2 Pre−Recorded

Announcement (Passenger

Briefing) System

All Cargo Operations

C 1

D 1

0

0

0



May be inoperative provided all crew members are in the flight compartment.






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

23−3




1.






−30−3 PACIS (Passenger Address and Cabin Interphone

System)

Passenger Address

System

1) Passenger

Configuration

B 1 0 (O) May be inoperative provided: a) Alternate procedures are established and used, b) Flight deck/cabin interphone (two way) with associated calls (e.g. chimes) is operative, and c) Megaphone(s) is/are readily available and operative.

NOTE:

Any station that operates normally may be used.

Page

23−4




Rev 7 Sep 09/2015


LIST PRINCIPALE D






1.






2) Non−Passenger

Configuration

A 1 0

0

(O) May be inoperative for non−passenger carrying operations for one flight day provided: a) Crew members are the only occupants of the aircraft, and b) Alternate procedures are established and used.

(O) May be inoperative provided all crew members are on the flight deck.


Cabin Interphone System

1) Passenger

Configuration

Flight Deck / Cabin and

Cabin / Cabin

D 1

B 1

A 1

1

0

(O) May be inoperative provided: a) An operative flight deck/cabin interphone (two way) is at an operative flight attendant seat, and b) Alternate communications procedures between the affected flight attendant station(s) are established and used.

(O) May be inoperative for non− passenger carrying operations for one flight day provided: a) Crew members are the only occupants of the aircraft, and b) Alternate procedures are established and used.






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

23−5




1.







Flight Deck / Cabin and

Cabin / Cabin

−30−4 Active Noise and Vibration

Suppression System

D

D

1

1

−40−1 Service Interphone System

(Flight Compartment to

Ground Crew)

C 1

−50−1 Boom Microphone Push−

To−Talk (PTT) Switches

−50−2 Headsets

−50−3 Flight Compartment

Speakers

−50−4

−50−5

Boom Microphones (incl.

Headset mics)

Cockpit Handheld

Microphones

D 1

C 4

D −

C 2

A −

C 2

0

0

0

May be inoperative provided all crew members are on the flight deck.


NOTE:

Aircraft may be dispatched with system operative in the DEGRADED mode with ANVS SYS

DEGRADED lamp illuminated on the Maintenance

Panel.

May be inoperative provided alternate procedures are established and used.

0

2

2

0

−

0

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

(M) May be inoperative provided one switch at each pilot’s position is verified operative.

One required at each pilot’s station.

May be inoperative provided: a) Procedures are not dependent on their use, b) Headsets are installed and used by each person on flight deck duty, c) All aural alerts, messages and other communication which are normally routed through the flight deck speakers must be audible through headsets, and d) A spare headset must be readily available for crew use.

May be inoperative provided: a) The Flight Data Recorder (FDR) operates normally, and b) Repairs are made within three flight days.

May be inoperative provided associated boom microphones are operative.

Page

23−6




Rev 7 Sep 09/2015


LIST PRINCIPALE D






1.






−50−6 Cabin Handsets

−50−7 Observer’s Audio Control

Panel

−60−1 Static Dischargers

−70−1 Cockpit Voice Recorder

−80−1 ARCDU Radio Tuning

Function (Aircraft with at least one FMS installed)

B 2 1

B

D

1

1

0

0

May be inoperative except when required by a person in an official capacity.

May be inoperative provided the seat is not required to be available in an official capacity for extended periods of time.

D 25 19 May be missing provided no more than one is missing from each control surface cluster.

A 1 0

(O) May be inoperative provided : a) One cabin handset operates normally, b) Operative handset is located at an operative flight attendant seat, and c) Alternate communication procedures between the affected flight attendant station(s) are established and used.

NOTE:

Any station that operates normally may be used.

C 2 1

May be inoperative provided: a) The Flight Data Recorder is operative, and b) Repairs are made within three flight days.

(O) May be inoperative provided: a) FMS Radio Tuning Function of the inoperative

ARCDU in “FMS” mode is verified operative.

b) The operative ARCDU Radio Tuning Function is verified operative in “BOTH” or “FMS” mode.






LIST PRINCIPALE D


Rev 6 Mar 26/2014

Page

24−1




1.





24 ELECTRICAL POWER

−20−1 AC GEN 1 and AC GEN 2

VOLT Indications (on ESID)

C 6 0

−20−2 AC GEN 1 and AC GEN 2

LOAD Indications (on ESID)

C 6

−20−3 #1 AC GEN and #2 AC

GEN Caution Lights

−30−1 Transformer Rectifier Units

(TRUs)

B 2

−30−2 DC Generator Control Unit

− Start / Termination

Function

−30−3 BATT °C Temperature

Indications

−30−4

***

APU Generation System

C 2

B 2

C 3

D 1

D 1

0

1

1

0

0

0

0

May be inoperative provided: a) Associated electrical cautions are operative, b) Associated AC GEN LOAD Indication(s) are operative, and c) Both DC Generators are operative.

May be inoperative provided: a) Associated electrical cautions and/or warnings are operative, b) Associated AC GEN VOLT Indications are operative, and c) Both DC Generators are operative.

May be inoperative provided: a) Associated AC GEN VOLT and AC GEN LOAD

Indications are operative and are periodically monitored during flight, and b) Both AC Generators are verified operative prior to each flight.

(M) May be inoperative provided: a) Both DC Starter/Generators are operative, and b) Associated TRU is deactivated.

(O) May be inoperative provided the start is manually terminated at 50% NH.

(O) May be inoperative provided: a) The associated BAT HOT Warning Light(s) are verified operative, and b) The associated DC BATT LOAD Indication(s) are verified operative.

(M#) May be inoperative provided: a) The cause of the malfunction is determined, and b) Appropriate action is taken to ensure that no hazard exists.

May be inoperative provided the APU is considered inoperative and is not used.

Page

24−2




Rev 6 Mar 26/2014


LIST PRINCIPALE D






1.



24 ELECTRICAL POWER (CONT’D)



−30−5 DC GEN LOAD Indications C 2

−30−6 DC Starter/Generation

Systems

C 2

B 2

−40−1 AC External Power System D 1

−40−2 DC External Power System D 1

1

1

1

0

0

(O) May be inoperative provided both DC Generators are operative.

(O) May be inoperative provided the inoperative

Indication is associated with a failed DC Generator.

(M#)(O) One GCU and/or Generator may be inoperative in the generation mode only (i.e. DC GEN caution light illuminated) provided: a) The cause of the malfunctions is determined and appropriate action is taken to ensure that no hazard exists, b) The failed DC Generator is switched OFF, and c) Both Transformer Rectifier Units (TRUs) are verified operative, and d) Operations are conducted in compliance with

AFM Supplement 92, OPERATION WITH ONE

DC GENERATOR INOPERATIVE.

May be inoperative.

May be inoperative.






LIST PRINCIPALE D


Rev 6 Mar 26/2014

Page

25−1




1.





25 EQUIPMENT AND FURNISHINGS

−10−1 Forward Observer Seat

(including associated equipment)

B 1

D 1

0

0

(M) May be inoperative provided the seat is removed, stowed, or secured in the retracted position.

(M) May be inoperative provided: a) The seat is not required to be occupied in an official capacity for extended periods of time, and b) The seat is removed, stowed, or secured in the retracted position.

−10−2 Pilot’s Seat Adjustments

1) Vertical Mode

Adjustment

C 2 0

−10−3

***

2) Fore/Aft Mode

3) Crew Armrests

4) Lumber Support

5) Lumbar Support

Padding

6) Recline Mechanism

Pilot’s Seat Heaters

B 2

C 4

C 2

D −

B −

D 2

D 2

0

0

0

−

0

1

0

(M#) Vertical adjustment may be inoperative provided the seat is secured in a position, which meets individual pilot requirements.

(M#) Fore/aft adjustment may be inoperative provided the seat is secured in a position, which meets individual pilot requirements.

(M#) May be inoperative provided the armrest(s) is

(are) removed from the seat.

May be inoperative in the lowest position provided the seat is acceptable to the affected crew member.

May be worn or damaged if acceptable to the affected crew member.

(M#) May be inoperative provided backrest is secured in a position acceptable to the affected crew member.

(M#) May be inoperative provided the affected Heater is deactivated.

(M) May be inoperative provided the Heaters are deactivated.

Page

25−2




Rev 7 Sep 09/2015


LIST PRINCIPALE D






1.






(CONT’D)

−20−1

***

Passenger Convenience

Items / Non−Essential

Equipment and Furnishings

(NEF)

1) 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, ash trays, stereo equipment, overhead reading lamps, etc. Items addressed elsewhere in this document shall not be included.

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

NOTE:

1.

Exterior lavatory door ash tray is not considered a convenience item.

2.

Galley equipment restraining devices such as latches, etc. must be serviceable or the compartment must not be used for storage and placarded

“INOPERATIVE − DO NOT USE”.

3.

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

4.

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






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

25−3




1.






(CONT’D)

2) Non−Essential

Equipment and

Furnishings (NEF)

− 0 May be inoperative, damaged or missing provided that the item(s) is (are) deferred in accordance with the operator’s NEF deferral program. The NEF program, procedures and processes are outlined in the operator’s Maintenance Control Manual.

(M) and/ or (O) procedures, if required, must be available to the flight crew and included in the operator’s appropriate document.

NOTE:

1.

Exterior lavatory door ash trays are not considered NEF items.

2.

Items addressed elsewhere in the

MMEL document cannot be considered for NEF relief.

Page

25−4




Rev 7 Sep 09/2015


LIST PRINCIPALE D






1.






(CONT’D)

−20−2 Overhead Storage Bin(s) /

Cabin and Galley Storage

Compartment / Closets

C − − (M) May be inoperative provided: a) Procedures are established to secure bins/compartments/closets CLOSED, b) Associated bin/compartment/closet is prominently placarded “INOPERATIVE − DO

NOT USE”, c) Any emergency equipment located in affected bin/compartment/closet is considered inoperative, and d) Affected bin/compartment/closet is not used for storage of any item(s) except for those permanently affixed.

NOTE:

1.

If no partitions are installed, the entire overhead storage compartment is considered to be one bin or compartment.

2.

An inoperative door/lid latch renders the door/lid inoperative.

3.

Required quantity of emergency equipment must be observed.






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

25−5




1.






(CONT’D)

C − −

−20−3 Megaphones


D −

D −

−

0

(M)(O) May be inoperative provided: a) Affected bin/compartment/closet door(s) is (are) removed, b) Associated bin/compartment/closet is not used for storage of any item(s), except for those permanently affixed, c) Associated bin/compartment/ closet is prominently placarded “INOPERATIVE − DO

NOT USE”, d) Procedures are established and used to alert crew members and passengers of inoperative bins/compartments/closets, and e) Passengers are briefed that associated bin/compartment/closet is not used.

NOTE:

1.

If no partitions are installed, the entire overhead storage compartment is considered to be one bin or compartment.

2.

Any emergency equipment located in the associated compartment

(permanently affixed) is available for use.

3.

An inoperative door/lid latch renders the door/lid inoperative.

(M)(O) Any in excess of those required by regulations may be inoperative or missing provided: a) Inoperative Megaphone(s) is/are removed from the passenger cabin and its location is placarded

"INOPERATIVE", or it is removed from the installed location, secured out of sight and the megaphone and its installed location are placarded "INOPERATIVE".

b) Required distribution is maintained, and c) Procedures are established to alert crew members of inoperative or missing Megaphones.


Page

25−6




Rev 7 Sep 09/2015


LIST PRINCIPALE D






1.






(CONT’D)

−20−4 Flight Attendant Seat

1) Required Flight

Attendant Seats

B − 1 (M)(O) One seat may be inoperative provided: a) Affected seat is not occupied, b) Affected flight attendant displaced by inoperative seat occupies the passenger seat which is most accessible to the inoperative seat, so as to most effectively perform assigned duties, c) Alternate procedures are established and used as published in the crew member manuals, d) Folding type seat stows automatically or is removed, stowed, or secured in the retracted position, and e) Passenger seat assigned to the flight attendant is placarded “FOR FLIGHT ATTENDANT USE

ONLY”.

NOTE:

1.

If automatic stow feature of a folding seat is inoperative, the seat is considered inoperative and must be secured in the stowed position.

2.

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






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

25−7




1.






(CONT’D)

2) Excess Equipment

***

D − −

−20−5 Passenger Seats

1) Recline Mechanism

***

D −

D −

−

−

(M) Seats in excess of requirements and not assigned to a flight attendant may be inoperative provided they are placarded, not occupied, and are: a) Properly stowed, or b) Secured in the retracted position, or c) Removed.

NOTE:

1.

If automatic stow feature of a folding seat is inoperative, the seat is considered inoperative and must be secured in the stowed position.

2.

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

(M) May be inoperative provided: a) Seat does not block or restrict access to an emergency exit, b) It does not restrict any passenger from access to the main aircraft aisle, and c) The affected seat(s) is/are not used and blocked and placarded "DO NOT OCCUPY".

NOTE:

1.

A seat with an inoperative safety belt is considered to be inoperative.

2.

The affected seat(s) may include the seat behind and/or the adjacent outboard seat(s).

(M) May be inoperative and seat occupied provided the seat is secured in the full upright position.

Page

25−8




Rev 7 Sep 09/2015


LIST PRINCIPALE D






1.






(CONT’D)

2) Armrest with Recline

Mechanism

***

D −

3) Armrest without Recline

Mechanism

***

4) Tray table in the unstowed position

***

−20−6 “Fasten Seat Belt While

Seated” and “No Smoking”

Signs or Placards

−20−7 Lavatory “NO SMOKING”

Placard

−20−8

***

Flight Attendant’s Seat

Heaters

−20−9 Flight Attendant Reading

Light

D −

D −

C −

B −

D 2

D 2

C −

−

−

−

−

−

1

0

0

(M) May be inoperative and seat occupied provided: a) The affected armrest does not block an emergency exit, b) The affected armrest does not restrict any passenger from access to the main aircraft aisle, and c) If armrest is missing, seat back is secured in the full upright position.

(M) May be inoperative and seat occupied provided: a) The affected armrest does not block an emergency exit, and b) The affected armrest does not restrict any passenger from access to the main aircraft aisle.

(M) May be inoperative provided: a) The affected tray table does not block an emergency exit, b) The affected tray table does not restrict any passenger from access to the main aircraft aisle, and c) The affected seat(s) is blocked and placarded

“DO NOT OCCUPY”.

NOTE:

An inoperative tray table in the stowed position is a Passenger Convenience/Non−Essential

Equipment and Furnishings item.

One or more signs or placards may be illegible or missing provided a legible sign or placard is readable from each occupied passenger seat.

May be missing provided the lavatory smoke detection system is operative.

(M#) May be inoperative provided the affected heater is deactivated.

(M) May be inoperative provided Heaters are deactivated.

(O) May be inoperative provided a suitable alternate light source is available.






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

25−9




1.






(CONT’D)

−20−10 Passenger Service Unit

(PSU)

C − −

C − −

(M) Passenger seats from which “No Smoking/Fasten

Seat Belt” light is not readily legible shall not be occupied and must be blocked and placarded “DO

NOT OCCUPY”.

(O) The affected seat(s) may be occupied provided: a) The Crew Cabin Interphone System, Cabin

Chime System and Passenger Address System are operative, and b) Procedures are established and used to alert flight attendants and notify affected passengers when seat belts should be fastened and smoking prohibited.

−30−1 Galley Waste Compartment

1) Door C − −

2) Flap 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 waste containers are available to accommodate all waste that may be generated on a flight.

(M)(O) May be inoperative provided: a) The container is empty and the access is secured to prevent waste introduction into the receptacle, and b) Procedures are established to ensure that sufficient waste containers are available to accommodate all waste that may be generated on a flight.

Page

25−10




Rev 7 Sep 09/2015


LIST PRINCIPALE D






1.






(CONT’D)

−40−1 Exterior Lavatory Door

Ashtrays

Aircraft with more than one exterior lavatory door or entry area ashtray installed

C 2 1 One may be missing on the entire aircraft.

NOTE:

1.

Repair interval extensions are not permitted.

2.

Interior lavatory ashtrays are considered under passenger convenience items/NEF and are not required by regulations.






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

25−11





(CONT’D)

Aircraft with only one exterior lavatory door or entry area ashtray installed

B 1

−50−1

***

1.





Aft Baggage Divider Nets D −

0

−

May be missing.

NOTE:

1.

Repair interval extensions are not permitted.

2.

Interior lavatory ashtrays are considered under passenger convenience items/NEF and are not required by regulations.

(M) May be inoperative or missing provided: a) Inoperative aft baggage divider net installation is completely removed including associated mounting hardware.

b) Ground crew is notified of missing aft baggage divider nets.

Page

25−12




Rev 7 Sep 09/2015


LIST PRINCIPALE D






1.






(CONT’D)

−50−2 Aft Baggage Door

Threshold Net

D 1 1

C 1

−50−3 Cargo Compartment Liners and Floor Panels

(Applicable to Forward and/or Aft Baggage

Compartments)

C −

0

−

(M) May be damaged provided: a) The number of detached stitching locations does not exceed six, b) The number of detached stitching locations per nylon strap (horizontal or vertical) does not exceed two, c) Detached stitching locations are separated by a minimum of two horizontal or vertical nylon strap intersection locations, d) No more than 25% of a nylon strap width is found to be defective, e) No more than one detached stitching location exists on main horizontal securing straps, f) There is no detached stitching on the two outermost vertical straps, g) Of the four installed, no more than one attachment clip is missing/inoperative, and h) Net is inspected weekly to ensure no further damage exists.

(M) May be missing provided: a) Inoperative aft baggage door threshold net assembly is completely removed, b) Baggage threshold protector remains installed, and c) Ground crew is notified of missing aft baggage door threshold net prior to unloading aircraft.

(O) Liner panels may be damaged or missing provided cargo is not carried in the associated compartment.

NOTE:

Unit Load Devices (ULDs) may be carried in the associated compartment provided no cargo is carried on or in these devices. For ballast purposes, use of bags (made of glass fibre or

Kevlar) of sand or ingots of non−magnetic metals

(such as lead) is acceptable.






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

25−13




1.






(CONT’D)

−60−1 Emergency Locator

Transmitter (ELT)

Fixed ELT A − −

Survival Type ELTs

***

−60−2 First Aid Kit

A −

D −

D −

D −

−

−

−

−

(M) May be inoperative provided: a) System is deactivated, b) Placard is displayed in the flight deck indicating the date the ELT has been deactivated, c) Repair or replacement of the ELT is done at the first aerodrome where repair or replacement can be accomplished, and d) Repair or replacement is made within the time interval prescribed by regulations as of the date of deactivation of the ELT.

(M) May be inoperative provided: a) System is deactivated, b) Placard is displayed in the flight deck indicating the date the ELT has been deactivated, c) Removal of the ELT is done at the first aerodrome where removal can be accomplished, d) When the ELT is removed, placard is displayed in the flight deck indicating the ELT has been removed in conjunction with date of when the

ELT has been deactivated, and e) Repair or replacement is made within the time interval prescribed by regulations as of the date of deactivation of the ELT.

(M) Any in excess of those required by regulations may be inoperative provided the system is deactivated and or removed.

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

(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.

Page

25−14




Rev 7 Sep 09/2015


LIST PRINCIPALE D






1.






(CONT’D)

First Aid Kit Seal B − −

−60−3

***

Emergency Medical Kit

Emergency Medical Kit

Seal

***

D −

A −

B −

−

0

−

The seal affixed on the exterior of the first aid kit may be missing or inoperative provided: a) The first aid kit is fully equipped or the kit has a maximum of one missing item, b) The kit includes a list of its contents, c) An inventory is taken on the content of the kit prior to departure, and d) Procedures are established to alert crew members of: i) Missing or broken seal, and ii) Need to perform an inventory under proviso c).

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

(O) May be incomplete or missing provided: a) The kit is sealed in a manner that will identify it as a unit that cannot be mistaken for a fully serviceable unit, and b) Replacements are made in one flight.

(O) The seal affixed on the exterior of the emergency medical kit may be missing or broken provided: a) The emergency medical kit is fully equipped, b) The kit includes a list of its contents, c) An inventory is taken on the content of the kit prior to departure, and d) Procedures are established and used to alert crew members of:

1.

The missing or broken seal, and

2.

The need to perform an inventory under proviso c).

−60−4 Flight Attendant Flashlights

1) Flashlights C − 0 (O) May be inoperative or missing provided the flight attendant assigned to the associated seat has a flashlight of equivalent characteristics readily available.






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

25−15




1.






(CONT’D)

2) Flashlight Holders C − 0

−60−6 Airstair Door Ditching Dam C 1

−60−7

***

Flight Deck Sun Visors C −

C −

0

−

−

(M)(O) May be inoperative or missing provided alternate stowage provisions are provided.

(M) May be inoperative provided: a) The ditching dam is secured in the stowed position, b) Extended overwater operations are prohibited, and c) Takeoffs and landings are not conducted on runways that may lead to imminent ditching.

May be inoperative provided affected sun visor does not obstruct either pilot’s field of view for take−off and landing.

(M#) May be inoperative provided affected Sun Visor is removed.

−60−8 Flight Deck

Flashlights/Flashlight

Holders

1) Flashlights C 2 0

2) Flashlight Holders C 2 0

(O) May be inoperative or missing provided that a flashlight of equivalent characteristics is readily available.

(M)(O) May be inoperative or missing provided alternate stowage provisions are provided.

−60−9 Life Vests

1) Flight Crew and Flight

Attendant Life Vests

C − − (O) Any in excess of those required by regulations may be inoperative or missing, provided that: a) Required distribution is maintained, b) Inoperative life vest is removed or secured out of sight, c) Inoperative life vest and its installed location are placarded “INOPERATIVE”, and d) Procedures are established and used to alert crew members of inoperative or missing life vests.

Page

25−16




Rev 7 Sep 09/2015


LIST PRINCIPALE D






1.






(CONT’D)

2) Passenger Life Vests

***

C − −

−62−1

***

Cabin Video Monitoring and

Surveillance System

C 1

Video Converter

C −

D 1

D 2

−

0

0

1

(O) As per regulations, for flights greater than 50 nautical miles from shore, may be inoperative provided: a) Inoperative life vest is removed or secured out of sight, b) The affected seat with the inoperative and/or missing life vest is not used and blocked and placarded, “DO NOT OCCUPY”, and c) Procedures are established and used to alert crew members of inoperative or missing life vest.

(O) As per regulations, for flights less than 50 nautical miles from shore, may be inoperative provided: a) Inoperative life vest is removed or secured out of sight, b) If the affected seat has a missing or inoperative floatation cushion, seat is not used and blocked and placarded, “DO NOT OCCUPY”, and c) Procedures are established and used to alert crew members of inoperative or missing life vest.

(O) May be inoperative provided: a) Alternate procedures are established and used for monitoring the area outside the flight crew compartment, b) Communication between the flight crew and flight attendant is available via intercom, and c) Spy hole view on the cockpit door is available.


One may be inoperative provided operative video converter is connected to an operative FMS.






LIST PRINCIPALE D


Rev 6 Mar 26/2014

Page

26−1




1.





26 FIRE PROTECTION

−10−1 Lavatory Smoke Detection

System

C − 0

C − 0

(M)(O) For each lavatory, where the Smoke Detector fails to test, the lavatory smoke detection system may be inoperative provided: a) Lavatory is not used by passengers for any purpose, b) Lavatory waste receptacle is empty, c) Lavatory door is locked closed and placarded

INOPERATIVE − DO NOT ENTER, d) Lavatory is used only by crew members, and e) In−flight service waste bags are not stored in the lavatory.

NOTE:

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

(M#)(O) For each lavatory, where the Smoke Detector indicates a failed condition intermittently or continuously, the lavatory smoke detection system may be inoperative provided: a) Smoke detector is deactivated, b) Lavatory is not used by passengers for any purpose, c) Lavatory waste receptacle is empty, d) Lavatory door is locked closed and placarded

INOPERATIVE − DO NOT ENTER, e) Lavatory is used only by crew members. and f) In−flight service waste bags are not stored in the lavatory.

NOTE:


Page

26−2




Rev 7 Sep 09/2015


LIST PRINCIPALE D






1.



26 FIRE PROTECTION (CONT’D)



1) Non−passenger

Carrying Operations

B −

B −

0

0

(O) For each lavatory, where the Smoke Detector fails to test, the Lavatory Smoke Detection System may be inoperative for non−passenger carrying operations provided: a) Crew members are the only occupants of the aircraft, b) Occupants are briefed as to which smoke detection system(s) is/are inoperative, and c) In−flight service waste bags are not stored in the lavatory.

NOTE:


(M#)(O) For each lavatory, where the Smoke Detector indicates a failed condition intermittently or continuously, the Lavatory Smoke Detection System may be inoperative for non−passenger carrying operations provided: a) Smoke Detector is deactivated, b) Crew members are the only occupants of the aircraft, c) Occupants are briefed as to which smoke detection system(s) is/are inoperative, and d) In−flight service waste bags are not stored in the lavatory.

NOTE:







LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

26−3




1.






2) All Cargo Operations C 1

C 1

0

0

(O) For each lavatory, where the Smoke Detector fails to test, the lavatory smoke detection system may be inoperative provided: a) The crew members have been briefed as to which lavatory smoke detection system(s) is/are inoperative, and b) In−flight service waste bags are not stored in the lavatory.

NOTE:


(M#)(O) For each lavatory, where the Smoke Detector indicates a failed condition intermittently or continuously, the lavatory smoke detection system may be inoperative for non−passenger carrying operations provided: a) Smoke Detector is deactivated, and b) Crew members have been briefed as to which lavatory smoke detection system(s) is/are inoperative, and c) In−flight service waste bags are not stored in the lavatory.

NOTE:


Page

26−4




Rev 7 Sep 09/2015


LIST PRINCIPALE D






1.






D 1

D 1

0

0

(O) For each lavatory, where the Smoke Detector fails to test, the lavatory smoke detection system may be inoperative provided: a) Crew members have been briefed as to which lavatory smoke detection system(s) is/are inoperative, b) The lavatory is placarded INOPERATIVE − DO

NOT ENTER, and c) In−flight service waste bags are not stored in the lavatory.

NOTE:


(M#)(O) For each lavatory, where the Smoke Detector indicates a failed condition intermittently or continuously, the Lavatory Smoke Detection system may be inoperative provided: a) Smoke Detector is deactivated, b) Crew members have been briefed as to which lavatory smoke detection system(s) is/are inoperative.

c) The lavatory is placarded INOPERATIVE − DO

NOT ENTER, and d) In−flight service waste bags are not stored in the lavatory.

NOTE:







LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

26−5




1.







Smoke Detectors

C 2

−10−3 Forward Baggage

Compartment Smoke

Detector

−10−4

***

−20−1

***

APU Fire Extinguishing

System

C 2

C 1

APU Fire Detection System D 1

D 1

1

0

0

0

0

(M#) May be inoperative provided: a) Affected smoke detector is deactivated, b) Inlet and outlet valve are deactivated in closed position, c) VENT VALVE INLT and VENT VALVE OUTLT

CLOSED advisory lights are verified illuminated prior to each flight, and d) Live animals are not carried.

(M#) May be inoperative provided: a) The baggage compartment is empty, or for ballast purpose, use of bags (made of glass fiber or Kevlar) of sand or ingots of non−magnetic metals (such as lead) is acceptable, and b) Affected smoke detectors are deactivated.

(M) May be inoperative provided the baggage compartment is empty, or for ballast purpose, use of bags (made of glassfiber or kevlar) of sand or ingots of non−magnetic metals (such as lead) is acceptable.

NOTE:

Only applicable if Forward Baggage Compartment is installed.

(M#) May be inoperative provided: a) The APU fuel shut−off valve is verified closed, and b) The APU is considered inoperative and is not used.

(M#) May be inoperative provided the APU is considered inoperative and is not used.

Page

26−6




Rev 7 Sep 09/2015


LIST PRINCIPALE D






1.






−20−2 Lavatory Fire Extinguishing

System

Non−passenger Carrying

Operations


C

C

−

−

B −

C

D

1

1

0

0

0

0

0

(M)(O) For each lavatory the lavatory fire extinguishing system may be inoperative provided the lavatory smoke detection system is operative.

(M)(O) For each lavatory the lavatory fire extinguishing system may be inoperative provided: a) Lavatory is not used by passengers for any purpose, b) Lavatory waste receptacle is empty, c) Lavatory door is locked closed and placarded

“INOPERATIVE − DO NOT ENTER”, and d) Lavatory is used only by crew members.

For each lavatory the lavatory fire extinguishing system may be inoperative for non−passenger carrying operations provided: a) Crew members are the only occupants of the aircraft, and b) Occupants have been briefed as to which lavatory fire extinguishing system(s) is/are inoperative.

(O) May be inoperative provided crew members have been briefed that the Lavatory Fire Extinguishing

System is inoperative.

(M)(O) The lavatory fire extinguishing system may be inoperative provided: a) Crew members have been briefed that the

Lavatory Fire Extinguishing System is inoperative, and b) Waste receptacle is emptied, secured closed, and placarded “INOPERATIVE − DO NOT USE”.

NOTE:







LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

26−7




1.






−20−3 Portable Fire Extinguishers D − − (M)(O) Any in excess of those required by regulations may be inoperative or missing provided: a) The inoperative fire extinguisher(s) is/are removed from the passenger cabin, flight deck, and its location is placarded "INOPERATIVE", or it is removed from the installed location, secured out of sight and the fire extinguisher and its installed location are placarded

"INOPERATIVE".

b) Required distribution is maintained in the passenger compartment and flight deck, and c) Procedures are established to alert crew of missing portable fire extinguishers.

−20−4 Baggage Compartment Fire

Extinguishers

1) Low Rate Discharge

Bottle (LRD)

C 1

2) High Rate Discharge

Bottle (HRD)

C −

0

0

(M#) May be inoperative provided the forward baggage compartment (if installed) and aft baggage compartment are empty.

NOTE:

For ballast purpose, use of bags (made of glass fiber or kevlar) of sand or ingots of non−magnetic metals (such as lead) is acceptable.

(M#) May be inoperative provided the associated baggage compartment is empty.

NOTE:

For ballast purpose, use of bags (made of glass fiber or kevlar) of sand or ingots of non−magnetic metals (such as lead) is acceptable.







LIST PRINCIPALE D


Rev 6 Mar 26/2014

Page

27−1




27 FLIGHT CONTROLS

−10−1 AIL TRIM Indicator

1.





C 1 0

−20−1 RUDDER TRIM Indicator

−20−2 Rudder Pedal Adjustment

−30−1 Flap Auto Pitch Trim (AUTO

TRIM FAIL)

C 1

−30−2 Stick Shaker

C 1

C 2

A 2

0

0

0

1

(M) May be inoperative provided, prior to each flight, the aileron trim is: a) Visually checked for full, free and correct movement, and b) Confirmed neutral.

(O) May be inoperative provided, prior to each take− off, the rudder trim is: a) Visually checked for full, free and correct movement as indicated on the PFCS indicator, and b) Selected to neutral.

(M#)(O) May be inoperative provided: a) The rudder pedal adjustment mechanism is not free to move, and b) The mechanism has failed such that the rudder pedals are in a position which meets individual pilot requirements.

(O) May be inoperative provided: a) Flap angles are limited to 15 degrees or less, and b) Manual pitch trim is operative.

(M) May be inoperative provided: a) The affected stick shaker is deactivated, b) The unaffected stick shaker is tested before each flight, c) Flight is not conducted into known or forecast icing conditions, and d) Repairs are made within two flight days.

Page

27−2




Rev 7 Sep 09/2015


LIST PRINCIPALE D






1.



27 FLIGHT CONTROLS (CONT’D)



−30−3 #1 STALL SYSTEM FAIL,

#2 STALL SYSTEM FAIL,

Caution Light(s)

A 2 0 (M) One or both caution lights may be illuminated for two flight days provided: a) It is confirmed that the illumination of the #

STALL SYST FAIL and accompanying PUSHER

SYST FAIL caution lights occur only on ground, b) Prior to each flight the reason for illumination is confirmed to be a result of the listed eligible failures, c) The Centralized Diagnostic System must be interrogated for the affected SPM to ensure that the PROPELLER DE−ICE failure is not indicated, and d) The aircraft is dispatched in accordance with the applicable proviso(s) below:

Eligible failure annunciations as determined through

Centralized Diagnostic system interrogation:

1) “FLAP DISCREPANCY”

2) “ADU 1 or ADU 2”

3) “AHRS 1 or AHRS 2”

4) “NO DATA FROM

FADEC 1" or “NO DATA

FROM FADEC 2”

(O) a) Use of flaps limited to maximum 15° or less, and b) Aircraft is not dispatched into known or forecast icing conditions.

May be inoperative.

NOTE:

Dual ADU failure will cause immediate illumination of the PUSHER SYST FAIL caution light in air or ground modes − refer to Item 27−30−5.

May be inoperative.

NOTE:

Dual AHRS failure will cause immediate illumination of the PUSHER SYST FAIL caution light in air or ground modes − refer to Item 27−30−

5.

May be inoperative.






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

27−3




1.






5) “STICK SHAKER”

−30−4 Stall Warning System

−30−5 Stick Pusher System

A 2

A 1

1

0

Dispatch is also to consider provisos of MMEL Item

27−30−2.

(M)(O) May be inoperative for two days provided: a) Affected system and stick pusher are deactivated, b) The unaffected system is tested before each departure, c) CG restrictions are observed, d) Flight is not conducted into known or forecast icing conditions, and e) Flights are conducted in accordance with the

AFM Supplement 11 OPERATION WITH ONE

INOPERATIVE STALL WARNING AND/OR

STICK PUSHER SYSTEM.

(M)(O) May be inoperative for two days provided: a) Stick pusher is deactivated, b) CG restrictions are observed, c) Flight is not conducted into known or forecast icing conditions, and d) Flights are conducted in accordance with the

AFM Supplement 11 OPERATION WITH ONE

INOPERATIVE STALL WARNING AND/OR

STICK PUSHER SYSTEM.

−60−1 Roll Spoiler Caution Lights

1) ROLL SPLR INBD GND C 1 0 (M#)(O) May be inoperative provided: a) Associated Roll Spoiler (ground mode) is deactivated, and b) Appropriate AFM performance decrements are applied per Supplement 17 OPERATION WITH

INOPERATIVE FLIGHT SPOILERS IN

GROUND MODE.

Page

27−4




Rev 6 Mar 26/2014


LIST PRINCIPALE D






1.






2) ROLL SPLR OUTBD

GND

C 1

−60−2 FLIGHT/TAXI Switch TAXI

Position Latch

C 1

0

0

(M#)(O) May be inoperative provided: a) Associated Roll Spoiler (ground mode) is deactivated, and b) Appropriate AFM performance decrements are applied per Supplement 17 OPERATION WITH


GROUND MODE.

(O) May be inoperative provided: a) The FLIGHT/TAXI Switch operates in both the

FLIGHT and TAXI positions, b) The ROLL INBD and ROLL OUTBD Spoiler

Advisory Lights are verified operative, and c) Retraction of the spoilers is verified when the

Switch is held in the TAXI position prior to each flight.

−60−3 Spoiler Advisory Lights

1) ROLL INBD C 1

2) ROLL OUTBD C 1

−60−4 Roll Spoilers (Ground Mode

System)

C 2

0

0

0

(O) May be inoperative provided all PFCS SPOILER indications on the MFD are operative and are periodically monitored.

(O) May be inoperative provided all PFCS SPOILER indications on the MFD are operative and are periodically monitored.

(M#)(O) May be inoperative provided: a) Associated Roll Spoiler (ground mode) is deactivated, and b) Appropriate AFM performance decrements are applied per supplement 17 OPERATION WITH


GROUND MODE.






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

28−1




1.





28 FUEL

−20−1 Pressure Refueling System

1) REFUEL C 1 0

2) PRESELECT REFUEL

3) REFUEL AND

PRESELECT REFUEL

−20−2 MASTER VALVE CLOSED

Light (Refuel/Defuel Panel)

C 1

−40−1 Height Measuring Unit

(Magnetic Dipsticks)

−40−2 Fuel TANK °C Temperature

Indication (on ESID)

C 2

C 1

−40−4 TANK 1 AUX PUMP and

TANK 2 AUX PUMP

Advisory Lights

C 1

C 1

−40−3 FUELING ON Caution Light C 1

C 2

0

0

0

0

0

0

1

(M) May be inoperative provided the fuel transfer system is verified operative.

(M) May be inoperative provided the fuel transfer system is verified operative.

(M) May be inoperative provided: a) Fuel transfer system is verified operative, and b) Procedures are established and used for gravity refueling.

(M) May be inoperative provided the

REFUEL/DEFUEL SHUT−OFF VALVE is verified closed following refueling.

May be inoperative provided the fuel quantity is determined by other approved means.

May be inoperative.

NOTE:

If using JET B / JP−4 fuel, the maximum operating altitude should not exceed 20,000 feet.

(O) May be inoperative provided prior to each flight: a) The REFUEL/OFF/DEFUEL switch is confirmed

OFF, and b) The Refuel/Defuel access panel is verified closed.

(O) May be inoperative provided: a) The associated ENG FUEL PRESS caution light and Aux Fuel Pump are verified operative, and b) Both flight compartment FUEL QTY Indications are verified operative, and c) Operations are conducted in compliance with

AFM Supplement 95, OPERATION WITH AN

INOPERATIVE AUX PUMP ADVISORY LIGHT.

Page

28−2




Rev 7 Sep 09/2015


LIST PRINCIPALE D






28 FUEL (CONT’D)

1.





−40−5 #1 TANK FUEL LOW and

#2 TANK FUEL LOW

Caution Lights

C 2

−40−6 Refuel/Defuel/Transfer

VALVE (OPEN/CLOSED)

Advisory Lights

−40−7 External Refuel/Defuel

Panel FUEL QTY Indicators

C 2

C 2

−40−8 REFUEL SHUTOFF TANK

1 and REFUEL SHUTOFF

TANK 2 Advisory Lights

−40−9

***

APU FUEL VALVE

Advisory Light

1) (OPEN)

C 2

C 1

1

1

0

0

(O) May be inoperative provided: a) The associated flight compartment FUEL QTY

Indication is verified operative and is periodically monitored during flight, and b) The associated engine FF (Fuel Flow) Indication is verified operative.

(M) May be inoperative provided the fuel transfer system and flight compartment FUEL QTY Indications are verified operative.

(M) May be inoperative provided the fuel quantity is determined by other approved means prior to each flight.

(M) May be inoperative provided the flight compartment FUEL QTY Indications are verified operative.

2) (CLOSED)

−40−10 Flight Compartment Fuel

QTY Indications (on ESID)

C 2

−40−11 Fuel Inlet Temperature

Indications (on Engine

Display)

D 1

A 2

0

0

1

1

(M) May be inoperative provided: a) The OPEN light is extinguished, and b) The CLOSED light is illuminated when the APU is selected OFF.

(M) May be inoperative provided: a) APU is not operated, and b) The APU fuel shut off valve is verified closed.

(M) May be inoperative provided: a) The fuel quantity is determined by other approved means prior to each flight, b) The Fuel Flow Indications are operative, are monitored during flight, and fuel consumption is recorded, c) TANK FUEL LOW caution light is operative, and d) Aircraft is dispatched with wing tanks balanced.

(O) May be inoperative for one flight provided the

TANK AUX PUMP Advisory Lights are operative.






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

29−1




−30−2 HYD PRESS STBY

Indication

1.





29 HYDRAULIC POWER

−10−1 Parking/Emergency Brake

Accumulator Hand Pump

−10−2 HYD FSOV OPEN Indicator

Light

C 1

C 2

−30−1 HYD PRESS 1 and HYD

PRESS 2 Indications

−30−3 System #1 and #2 Nacelle

Reservoir Quantity

Indicators

−30−4 #1 STBY HYD PUMP HOT

Caution Light

A 1

−30−5 HYD QTY 3 Indication

C 2

C 1

C 2

C 1

−30−6 System #3 Aft Fuselage

Hydraulic Quantity Indicator

C 1

0

1

1

0

0

0

0

0

May be inoperative provided accumulator pressure is verified prior to engine start.

(M) One may be inoperative provided: a) The associated HYD FSOV is verified open, and b) The associated HYD FSOV CLOSED indicator light is verified operative.

(M) May be inoperative provided: a) The associated ENG HYD PUMP Caution Light is verified operative, and b) The associated HYD QTY Indication is verified operative.

(O) May be inoperative provided: a) Normal operation of the Standby Hydraulic

Pump is verified before each flight, and b) HYD PRESS 1 and HYD PRESS 2 Indications are verified operative.

(M)(O) May be inoperative provided: a) HYD QTY 1 and HYD QTY 2 Indications are verified operative, and b) ENG HYD PUMP Caution Lights are verified operative.

May be inoperative provided: a) STBY HYD PRESS Indication is operative, and b) Repairs are made within one flight day.

(M) May be inoperative provided: a) The System #3 Aft Fuselage Hydraulic Quantity

Indicator is verified operative, and b) Adequate fluid quantity is verified before each flight.

May be inoperative provided HYD QTY 3 Indication is operative.

Page

29−2




Rev 7 Sep 09/2015


LIST PRINCIPALE D






1.



29 HYDRAULIC POWER (CONT’D)



−30−7 HYD PRESS 3 Indication C 1 0 (M#) May be inoperative provided: a) The #3 HYD PUMP Caution Light is verified operative, and b) The HYD QTY 3 Indication is verified operative.

−30−8 PTU CNTRL ON Advisory

Light

1) Pre Modsum 4−126354 or 4−126425 a) PTU CNTRL ON

Advisory Light

C 1 0 (O) May be inoperative provided: a) The HYD PRESS 2 indication is verified operative, b) The #2 ENG HYD PUMP caution light is verified operative, and c) The hydraulic Power Transfer Unit is verified operative prior to each flight.

2) Post Modsum 4−

126354 or 4−126425 a) PTU CNTRL ON

Advisory Light (White) b) PTU CNTRL FAIL

Advisory Light (Amber) c) PTU CNTRL pressure

Green Cross Hatch

Advisory Light (Green)

C 1

C 1

C 1

−30−9 #1 ENG HYD PUMP and #2

ENG HYD PUMP Caution

Lights

C 2

0

0

0

1

May be inoperative provided Pressure Green Cross

Hatch Advisory Light is operative.

May be inoperative provided Pressure Green Cross

Hatch Advisory Light is operative.

(O) May be inoperative provided: a) The HYD PRESS 2 indication is verified operative, b) The #2 ENG HYD PUMP caution light is verified operative, and c) The hydraulic Power Transfer Unit is verified operative prior to each flight.

(M) May be inoperative provided: a) The associated flight compartment HYD PRESS

Indication is verified operative, b) The associated ISOLATION VALVE is verified operative, and c) The associated hydraulic pressure is periodically monitored.






LIST PRINCIPALE D


Rev 6 Mar 26/2014

Page

29−3




1.



29 HYDRAULIC POWER (CONT’D)



−30−10 HYD QTY 1 and HYD QTY

2 Indications

C 2

−30−11 STBY HYD PRESS ON

Advisory Light

−30−12 #1 HYD FLUID HOT and #2

HYD FLUID HOT Caution

Lights

C 1

B 2

−30−13 HYD #3 ISOL VLV OPEN

Advisory Light

C 1

1

0

1

0

(M) May be inoperative provided: a) The quantity is verified adequate prior to each flight, b) The associated ENG HYD PUMP Caution Light and HYD PRESS Indication are verified operative, c) The associated HYD ISO VLV Caution Light is verified operative, and d) The associated Nacelle Hydraulic Quantity

Indicator is verified operative.

(O) May be inoperative provided the HYD PRESS

STBY indication is verified operative.

(M#)(O) May be inoperative provided: a) The associated HYD PRESS Indication is verified operative and is periodically monitored during flight, b) Adequate steps are taken each flight day to ensure that an overheat condition has not occurred, and c) The associated HYD QTY Indication is verified operative.

(O) May be inoperative provided: a) The HYD PRESS 3 indication is operative, and b) The ELEVATOR PRESS caution light is operative.







LIST PRINCIPALE D


Rev 6 Mar 26/2014

Page

30−1




1.





30 ICE AND RAIN PROTECTION

−10−1 TAIL De−Ice Boots

Advisory Lights

−10−2 DEICE PRESS Caution

Light

−10−3 DEICE PRESS Indicators

−10−4 Low Pressure Warning

Switches (LPWS)

−10−5 WING De−Ice Boots

Advisory Lights

C 4

C 1

C 1

C 2

C 2

C 2

C 2

C 8

0

0

0

0

0

1

0

2

May be inoperative provided the flight is not conducted in known or forecast icing conditions.


(M) May be inoperative provided: a) All De−Ice Boot Advisory Lights are verified operative, and b) The DEICE PRESS Indicators are verified operative.


(M) May be inoperative provided: a) All De−Ice Boot Advisory Lights are verified operative, and b) The DEICE PRESS Caution Light is verified operative.

(M#) May be inoperative provided: a) DEICE PRESS Caution Light is verified operative, b) DEICE PRESS Indicator is verified operative, c) All De−ice Advisory Lights are verified operative, and d) Faulty LPWS is disconnected.

May be inoperative provided flight is not conducted in known or forecast icing conditions.

(O) May be inoperative provided: a) The left wing root de−icer boot advisory light and right wing root de−icer boot advisory light are verified operative, b) The associated boot operation is visually monitored when in use, and c) The appropriate wing inspection light(s) operate normally for night operation.

Page

30−2




Rev 7 Sep 09/2015


LIST PRINCIPALE D






1.






(CONT’D)

−10−6 Timer Monitor Unit (TMU,

Timer Function)

C 1 0

−10−7 Airframe De−Icing System C 1

−20−1 Engine Intake Bypass Door

OPN and CLOSED

Advisory Lights

C 2

−20−2 ENGINE INTAKE HTR

Advisory Lights

−20−3 ENG ADPT HEAT 1 and

ENG ADPT HEAT 2

Caution Lights

C 2

C 2

C 2

C 2

0

0

0

0

1

1

(M#) May be inoperative provided: a) Flight is not conducted in known or forecast icing conditions, b) PITOT HEAT 1, PITOT HEAT 2 and PITOT

HEAT STBY are verified operative, c) L AOA VANE HEAT and R AOA VANE HEAT are verified operative, and d) ENGINE INTAKE HEATER 1 and 2 are verified operative.

NOTE:

AUTO mode of De−icer boots cycle will be inoperative.


(M) May be inoperative provided: a) Bypass Door operation is verified prior to each flight, and b) The related engine intake heater indicator is verified operative.

May be inoperative provided: a) Associated bypass door(s) remains closed, and b) Flight is not conducted in known or forecast icing conditions.

(M)(O) May be inoperative provided: a) The associated Heater(s) is verified operative prior to dispatch, and b) Associated ENG ADPT HEAT Caution Light(s) is verified operative.


(M)(O) May be inoperative provided: a) The associated heater is verified operative prior to dispatch, and b) The associated ENGINE INTAKE HTR advisory light is verified operative and is periodically monitored.






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

30−3




−40−1 Windshield Wipers

1.






(CONT’D)

−20−4 Engine Intake Adapter

Heater Assemblies

−30−1 Pitot/Static Heaters

−30−2 PITOT HEAT 1, PITOT

HEAT 2 and PITOT HEAT

STBY Caution Lights

−40−2 Windshield Heaters

Co−Pilot Heated

Windshield (Right Hand

Windshield)

−60−2 PROPS Heat Advisory

Lights

C 2

B 3

B 3

C 2

A 3

A 1

−60−1 Propeller De−icing System C 1

B 2

C 2

1

2

0

0

1

0

0

0

0


May be inoperative for DAY VMC provided: a) There is no visible moisture, and b) The flight is not conducted into known or forecast icing conditions.

(M) May be inoperative provided: a) The flight is not conducted into known or forecast icing conditions, and b) All other elements of the pitot heat systems are verified operative prior to each flight.

May be inoperative provided the flight is not conducted in precipitation within five nautical miles of the airport of take−off or intended landing.

May be inoperative provided: a) The flight is not conducted in known or forecast icing conditions, and b) Repairs are made within three flight days.

(M#)(O) May be inoperative for one day provided: a) The Pilot’s Side Window heating is operative, b) The Pilot Windshield (Left Hand Windshield) heating is verified operative prior to dispatch, and c) The flight is conducted in accordance with AFM

Supplement 114, “OPERATION WITH ONE

WINDSHIELD HEATING SYSTEM

INOPERATIVE”.


(O) May be inoperative provided: a) AC LOAD indication is operating and periodically monitored, and b) the PROP DEICE caution light is operative.


Page

30−4




Rev 7 Sep 09/2015


LIST PRINCIPALE D






1.






(CONT’D)

−80−1 Ice Detector Spigot

Illumination Lights

C 2 1

−80−2 Ice Detector Probes

(Electronic)

C 2

A 2

A 2

0

0

1

One may be inoperative at either the pilot’s or co− pilot’s position.

May be inoperative for day operations.

(M) May be inoperative for night operations for one flight day provided: a) Both Ice Detector Probes are operative, b) The flight is not conducted in known or forecast icing conditions, and c) A flashlight of adequate capacity is available and confirmed operable prior to each flight.

(M)(O) May be inoperative for thirty days.

B 2 0 (M)(O) Both may be inoperative provided: a) Windshield wipers are stored in the normal horizontal position, and b) Both Ice Detector Spigot illumination lights are confirmed operative prior to night operations.

c) Flight will be conducted in accordance with AFM

Supplement Number 98, Operation with Both Ice

Detector Probes (Electronic) inoperative (ICE

DETECT FAIL caution Light Illuminated).

d) The flight is not conducted at night into known or forecast icing conditions.






LIST PRINCIPALE D


Rev 6 Mar 26/2014

Page

31−1




1.





31 INDICATING AND RECORDING

SYSTEMS

−20−1 Clocks

1) Pilot Clock A 1 0

2) Co−pilot Clock C 1 0

May be inoperative provided: a) Reliable and functioning timepiece is readily available to all Flight Compartment crew members, and b) Repairs are made within three flight days.

May be inoperative.

−30−1 Flight Data Recorder A 1

1) DFDR Recording

Parameters required by

Regulation

A −

0

−

−

0

(M) May be inoperative provided: a) The Cockpit Voice Recorder is operative, and b) Repairs are made within three flight days.

(M#) Up to three (3) digital recording parameters may be inoperative provided: a) The Cockpit Voice Recorder is operative, and b) Repairs are made within twenty calendar days.

(M#) May be inoperative provided repairs are made before completion of the next heavy maintenance check.


2) DFDR Recording

Parameters not required by Regulation

−30−2

***

Extended Quick Access

Recorder

−51−1 Caution and Warning Lights

System

1) Dual Master Caution switchlight (Glareshield, light function only)

(CR833CH00034)

2) Dual Master Warning

Switchlight (Glareshield, light function only)

(CR833CH00034)

A −

D −

C 2

C 2

1 One may be inoperative.

1 One may be inoperative.

Page

31−2




Rev 7 Sep 09/2015


LIST PRINCIPALE D






1.






SYSTEMS (CONT’D)

−60−1 ESID Control Panel

1) System Page Push

Button Switches

C 4 0 (O) The ELEC SYS, ENG SYS, FUEL SYS, and

DOORS SYS Switches may be inoperative provided the ALL Switch is operative.






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

31−3




1.






SYSTEMS (CONT’D)

2) ALL Switch C 1 0

0

(O) The ALL Switch may be inoperative provided the

ELEC SYS, FUEL SYS, ENG SYS and DOORS SYS

Switches are operative.

Dimming may be inoperative provided the display intensity is adequate.

3) Engine Display

Dimming Function

−60−2 MFD and PFD Engine

Display Messages

1) PFD 1 / 2 LINK FAIL

Engine Display message

2) MFD 1 / 2 LINK FAIL

Engine Display message

−60−3 Electronic Flight Instrument

System Control Panels

C 1

C 2

C 2

C 2

1

1

1

Message may be displayed.

Message may be displayed.

Bright/Dim Controls C 6 0

1

One panel may be inoperative provided: a) The pilot flying panel is fully operative, and b) Affected side must meet navigational requirements for route being flown.

Dimming may be inoperative provided the display intensity is adequate.

Message may be annunciated for three flight days.

−60−4 FADEC 1 / DU or FADEC 2

/ DU Engine Display

Message

−60−5 EFIS/ESID Display Units

A 2

A 5 4 (M)(O) RH MFD (MFD2) may be inoperative provided: a) RNP AR approach is not being conducted, b) The left hand Electronic Flight Instrument

System Control panel (EFCP) and the Engine and System Integrated Display Control Panel

(ESCP) are fully functional, c) The MFD1 rotary selector and ELEC SYS, ENG

SYS, FUEL SYS, DOOR SYS and ALL push button switches are operative, and d) Repairs are made within one flight day.

NOTE:

The pilot occupying the left seat must conduct all departures and arrivals in Instrument

Meteorological Conditions.







LIST PRINCIPALE D


Rev 6 Mar 26/2014

Page

32−1




32 LANDING GEAR

−20−1

***

NOSE GEAR LOCK

Advisory Light

1.





D 1 0

−30−1 Landing Gear Retraction

System

A 1 0

May be inoperative provided Nose Gear Lock is verified disengaged prior to each departure.

(O) Landing gear retraction system may be inoperative for one flight provided operations are conducted in compliance with AFM Supplement 94,

OPERATION WITH LANDING GEAR EXTENDED.

−40−1 Parking Brake Pressure

Indications

1) HYD PRESS PK BRK

Indication

C 1 0

−40−2 Anti−Skid System

−40−3

***

2) Aft Wing Root Fairing

Indicator

Fill Valve Gauge

(CR411000−001)

C 1

C 1

D 6

0

0

0

(M) May be inoperative provided: a) The Aft Wing Root Fairing Indicator is verified operative, and b) Brake pressure is confirmed adequate prior to engine start.

(M) May be inoperative provided: a) The HYD PRESS PK BRAKE Indication is verified operative, and b) Brake pressure is confirmed adequate prior to engine start.

(O) May be inoperative provided operations are conducted in compliance with AFM Supplement 7

OPERATION WITH INOPERATIVE ANTI−SKID

BRAKE CONTROL SYSTEM.

Gauge may be inoperative.

Page

32−2




Rev 7 Sep 09/2015


LIST PRINCIPALE D






1.



32 LANDING GEAR (CONT’D)



−50−1 Nosewheel Steering A 1

−60−1 Touched Runway Indicating

System

C 1

0

0

(M)(O) May be inoperative for one flight day provided: a) NOSE STEERING caution light is extinguished when the nosewheel STEERING switch is in the

OFF position, b) Nosewheel STEERING switch is selected and remains OFF, c) Nosewheel steering system is deactivated, and d) Operations are conducted in compliance with

AFM Supplement 8 OPERATION WITH

INOPERATIVE NOSEWHEEL STEERING

SYSTEM.

(M) May be inoperative provided prior to each flight, it is confirmed that the frangible switch has not been contacted.






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

33−1




1.





33 LIGHTS

−10−1 Cockpit and Instrument

Panel Lighting System

C 1 1

D 1 0

Individual lights may be inoperative for night flight provided the 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 member’s eyes, and c) Lighting configuration and intensity is acceptable to the flight crew.

May be inoperative for daylight operations.

−10−2 Caution/Warning/Advisory

Lights System DIM/BRT

Function

Dimming Function

Brighten Function

C 1

C 1

0

0

(M) May be inoperative for day operations.

(M)(O) May be inoperative for day operations provided: a) Dimming function is considered inoperative, b) DIM/BRT switch is not operated, and c) DIM/BRT switch is placarded, “INOPERATIVE −

DO NOT USE”

NOTE:

Operation of the DIM/BRT switch to Dimming mode during dispatch will exclude the ability to

Brighten the lights again until the aircraft is power cycled during ground operations.

−10−3 Caution/Warning/Advisory

Lights System

1) Caution/Warning Panel

LEDs

2) Advisory Lights

C −

C −

−

−

May be inoperative provided one half of each light is operative.

(O) Individual bulb(s) /LED(s) may be inoperative for advisory lights with multiple light elements provided: a) Advisory lights are tested before each flight, and b) Luminescence and legibility of affected advisory light(s) is acceptable to the flight crew.

Page

33−2




Rev 6 Mar 26/2014


LIST PRINCIPALE D






33 LIGHTS (CONT’D)

1.





−20−1 No Smoking / Fasten Seat

Belt Lights

C −

Aural Tone Function

Automatic Function


−20−2 Cabin Lighting System

1) Sidewall Lighting

Classic Interior

C −

A −

C

C

D −

C

−

−

−

−

−

−

−

−

−

(M)(O) Passenger Seats, Flight Attendant Seats, or

Lavatory from which a light is not readily legible shall not be occupied and must be blocked and placarded

“DO NOT OCCUPY”.

(O) The affected Seats or Lavatory may be occupied provided: a) The crew Cabin Interphone System, Cabin

Chime System, and Passenger Address System are operative, and b) Procedures are established and used to alert flight attendants and notify passengers when seat belts should be fastened and smoking prohibited.

(O) May be inoperative for one flight day for non− passenger carrying operations provided: a) Crew members are the only occupants of the aircraft, and b) Alternate procedures are established and used.


(O) May be inoperative provided: a) Manual control function is operative, and b) Alternate procedures are established and used.


− May be inoperative.






LIST PRINCIPALE D


Rev 6 Mar 26/2014

Page

33−3





1.





Classic Interior 3−Abreast

Layout

NextGen Interior

(CR825CH02598)

NextGen Interior 3−

Abreast Layout

C −

C −

C −

−

−

−

(M) Up to 25% of total length of sidewall downwash lights may be inoperative provided: a) No two adjacent LED strips are inoperative, or no opposite LED strip and lighting tube are inoperative, b) No three adjacent or two opposite lighting tubes are inoperative, c) Cabin lighting is sufficient for flight attendants to perform required duties, and d) Sidewall lighting forward of class dividers is operational.

(M) Up to 25% of total length of sidewall downwash lights may be inoperative provided: a) No two adjacent or opposite LED strips are inoperative, and b) Cabin lighting is sufficient for flight attendants to perform required duties.

(M) Up to 25% of total length of sidewall downwash lights may be inoperative provided: a) No two adjacent or opposite LED strips are inoperative, b) Cabin lighting is sufficient for flight attendants to perform required duties. and c) Sidewall lighting forward of class dividers is operational.

2) Ceiling Lighting

Classic Interior C − − (M) Individual lighting sources may be inoperative provided: a) No three adjacent or two opposite lighting tubes are inoperative, and b) Cabin lighting is sufficient for flight attendants to perform required duties.

Page

33−4




Rev 6 Mar 26/2014


LIST PRINCIPALE D







1.





Classic Interior 3−Abreast

Layout

NextGen Interior

(CR825CH02598)

NextGen Interior 3−

Abreast Layout

3) All Cargo Operations

C −

C −

C −

D −

−

−

−

−

(M) Up to 25% of total length of Ceiling upwash lights may be inoperative provided: a) No two adjacent LED strips are inoperative, or no opposite LED strip and lighting tube are inoperative, b) No three adjacent or two opposite lighting tubes are inoperative, c) Cabin lighting is sufficient for flight attendants to perform required duties, and d) Ceiling lighting forward of class dividers is operational.

(M) Up to 25% of total length of Ceiling upwash lights may be inoperative provided: a) No two adjacent or opposite LED strips are inoperative, and b) Cabin lighting is sufficient for flight attendants to perform required duties.

(M) Up to 25% of total length of Ceiling upwash lights may be inoperative provided: a) No two adjacent or opposite LED strips are inoperative, b) Cabin lighting is sufficient for flight attendants to perform required duties, and c) Ceiling lighting forward of class dividers is operational.

NOTE:

For Classic and NextGen 3−Abreast Interiors, referring to the placard on the Flight Attendant

Panel. “BEFORE FIRST FLIGHT OF THE DAY:

WITH OVERHEAD BIN DOORS CLOSED KEEP ALL

CEILING AND SIDEWALL LIGHTS ON/FULL

BRIGHT FOR MINIMUM OF 15 MINUTES”. The intent of this placard is that all available lighting

(excludes inoperative lighting under MMEL relief) should be ON/FULL bright for at least 15 minutes.

May be inoperative provided cabin lighting is sufficient to inspect cargo and to perform fire−fighting duties.






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

33−5





1.





−20−3 Lavatory Compartment

(RETURN TO SEAT and

Lavatory OCCUPIED Light)

1) RETURN TO SEAT

Light

C

C

−

−

2) Toilet OCCUPIED Light C −

−20−4 Accent Lights (Spotlights)

NextGen Interior D 30

0

0

0

(O) The lavatory may be occupied provided: a) Passenger Address System is operating normally and can be clearly heard in the lavatory compartment during flight, and b) Alternate procedures are established and used to notify passengers when return to seat is required.

(M) Lavatory compartment shall not be occupied and must be blocked and placarded − “DO NOT OCCUPY”

May be inoperative.

−25−1 Lavatory Light


Ceiling Lights

C

C

C

D

−

−

2

2

0

0

0

0

0

May be inoperative.

NOTE:

This relief is not intended for Emergency Flood

Lights within the Accent Light Assemblies.

Full illumination mode may be inoperative provided the dimmed mode is functional at all times.

(M) May be inoperative provided lavatory door is locked closed and placarded, “INOPERATIVE − DO

NOT ENTER”.

May be inoperative provided alternate lighting is available.


Page

33−6




Rev 7 Sep 09/2015


LIST PRINCIPALE D







−30−2 Forward Baggage

Compartment Light

1.





−30−3

***

Aft Service Light

−40−1 Position Lights

−40−2 A/COL WHITE Lights

−40−3

***

Logo Lights

−40−4 A/COL RED Light (Red

Recognition Light)

C

D

D 1

C 6

C 6

C −

C 2

D

C

1

1

2

1

0

0

0

3

0

−

0

0

May be inoperative provided alternate lighting is available.

NOTE:



NOTE:


(M) May be inoperative provided the light is deactivated.

One bulb at each position (wing tip and aft) may be inoperative.


As required by regulations.


NOTE:

The A/COL switch must be operated as if the lights were operating normally.

May be inoperative.

0 (O) May be inoperative provided adequate precautions are taken to clear the area prior to engine start and while engines are running.

NOTE:

The A/COL Light switch must be operated as if the light was operative.






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

33−7





−40−5 Boarding Lights

1) Passenger

Configuration

1.






C 2

C 2

C 2

D 2

0

0

0

0

May be inoperative provided Cabin Overhead Lighting or alternate means is used.


May be inoperative provided “aircraft crew” are the only occupants of the aircraft.

May be inoperative provided the “crew member” are the only occupants of the aircraft.

NOTE:

For the purpose of this item, “aircraft crew” is considered to be crew members including the flight crew, flight attendants, aircraft maintenance engineers and supervisory crew members. “Crew member” means a person assigned to duty in an aircraft during flight time.

−40−6 Passenger Airstair Door

Lights

1) Passenger

Configuration


C 4

C 4

C 4

C 4

D 4

2 May be inoperative provided they are not adjacent.

0

0

0

0

May be inoperative provided acceptable alternate lighting is used to board and deplane passengers.


May be inoperative provided the “aircraft crew” are the only occupants of the aircraft.

May be inoperative provided the “crew member” are the only occupants of the aircraft.

NOTE:

For the purpose of this item, “aircraft crew” is considered to be crew members including the flight crew, flight attendants, aircraft maintenance engineers and supervisory crew members. “Crew member” means a person assigned to duty in an aircraft during flight time.

Page

33−8




Rev 7 Sep 09/2015


LIST PRINCIPALE D







−40−7 Landing Lights

1.





C 4

−40−8 Taxi Light

−40−9 WING INSP Lights

−50−1 Exterior Emergency

Lighting System

D 4

C 1

D 1

A 4

C 4

C 4

A 1

C 1

−50−2 Interior Electrical

Emergency Lighting System

Relief limited to installation defined by Bombardier

AEROC 84.6.E.1 Sect. 5

1) Ceiling Lights C 1

2

0

0

0

2

0

0

0

0

One inboard and/or one outboard light may be inoperative for night operations provided steep approach landings are not conducted.


May be inoperative provided Landing Lights are operative.


One or more may be inoperative for three flight days provided: a) At least one wing inspection light is operative, and b) A portable lamp/light of adequate capacity for wing inspection is available for night operations in icing conditions.

One or more may be inoperative provided the flight is not conducted in known or forecast icing conditions at night.


(O) May be inoperative for one flight day provided: a) Aircraft crew are the only occupants of the aircraft, and b) Alternate procedures are established and used.

NOTE:

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


1 Individual light bulbs, etc. may be inoperative provided no two adjacent overhead emergency lights are inoperative.






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

33−9





1.





2) EXIT Identifiers C 4

3) Emerg. Markers,

Emerg. Locators

C 7

NextGen Interior

(CR825CH02598)


AEROC 84.6.E.1, Sect.

15.24

1) Ceiling Emergency

Flood Lights

C 7

2) Exit Identifiers

4

7

Two bulbs from five may be inoperative on each identifier.

Two bulbs from five may be inoperative on each marker/locator given that inoperative bulbs are not adjacent.

C 4

−

4

Individual light units may be inoperative provided: a) No two adjacent ceiling emergency flood lights are inoperative, and b) Floodlight at aircraft fuselage station X=335.31 is operative.

Each exit identifier may have 40% of its internal lights inoperative.

NextGen Interior (Dual

Class)


AEROC 84.6.E.1, Sect.

13.8 and AEROC

84.6.E.1, Sect. 15.24

Page

33−10




Rev 7 Sep 09/2015


LIST PRINCIPALE D







1.





1) Ceiling Emergency

Flood Lights

2) Exit Identifiers C 4

−50−3 Photoluminescent Floor

Proximity Emergency

Escape Path Lighting

Photoluminescent Tape

System − Relief limited to installation defined by

Bombardier design

AEROC 84.8.AC.10, Sect.

11

C 1


C 7 −

4

Individual light units may be inoperative provided: a) No two adjacent ceiling emergency flood lights are inoperative, and b) Floodlight at aircraft fuselage station X=239.56

and X=335.31 are operative.

Each exit identifier may have 40% of the internal lights inoperative.

D 1

1

0

Four meters of lighting strip may be unserviceable provided: a) Any unserviceable section does not exceed 0.2

meters (8 in.) of continuous length, b) The distance between two adjacent unserviceable sections must be not less than 1.5

meters (60 in.) on the same strip.

(O) May be inoperative.






LIST PRINCIPALE D


Rev 6 Mar 26/2014

Page

34−1




1.





34 NAVIGATION

−10−1 Altitude Alerting System A 1 0

−20−1 Standby Magnetic

Compass

−20−2 Standby Attitude Indicator

B 1

B 1

C 1

B 1

−20−3 IVSI Indications (on PFDs) C 2

−20−4 AHRS Control Panel

Indicators

1) DG Indicators

2) ALIGN Indicators

3) SLAVE Indicators

4) BASIC Indicators

C

C

C

C

2

2

2

2

0

0

0

0

1

1

1

1

1

(O) May be inoperative provided: a) Autopilot with ALT hold is verified operative, and b) Repairs are made within three flight days.

May be inoperative provided any combination of three gyro (or INS (IRU)) stabilized compass systems are operative.

May be inoperative provided: a) Any combination of two gyro (or INS (IRU)) stabilized compass systems are operative, and b) Aircraft is operated: i) With dual independent navigation capability, and ii) Under positive radar control by ATC during the enroute flight phase, or one of the navigation systems is a TSO’d GPS which provides track information.

(O) May be inoperative for flights that are entirely within areas of magnetic unreliability provided at least two stabilized directional gyro systems are installed, are operative, and if necessary, used in conjunction with approved free gyro navigation techniques.

May be inoperative for day VMC provided: a) The instrument face is covered, and b) Operation is not conducted into known or forecast VFR OTT (Over the Top) conditions.

May be inoperative for day VMC.

May be inoperative provided switching function is operative for each Indicator.

May be inoperative.

May be inoperative.

May be inoperative.

May be inoperative.

Page

34−2




Rev 7 Sep 09/2015


LIST PRINCIPALE D






34 NAVIGATION (CONT’D)

1.





−20−5 Flux Valves B 2 1 May be inoperative provided: a) The opposite Attitude Heading Reference Unit is operative, b) The Standby Magnetic Compass is operative, c) The AHRS on the affected side is operated in

DG mode, d) Flight is restricted to DAY VMC, and e) DG Slew Mode is confirmed operative.

−20−6 Integrated Standby

Instrument

(CR839CH00013)

1) Attitude / Slip Skid

Function

2) STD (Standard) Button

−20−7

***

Inertial Reference System

(IRS)

B 1

C 1

C 1

D 1

−30−1

***

Microwave Landing

Systems (MLS)

If used routinely C −

If not used routinely D −

−40−1 Weather Radar System

−40−2 Traffic Alert and Collision

Avoidance System (TCAS)

1) Traffic Alert and

Collision Avoidance

System (TCAS)

D 1

B 1

0 May be inoperative for day VMC.

0

0

0

May be inoperative.

Except where required by operations, may be inoperative provided alternate procedures are established and used.


0

0

0

May be inoperative provided alternate procedures are established and used.


As required by regulations.

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






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

34−3





1.





2) Combined Traffic Alert

(TA) and Resolution

Advisory (RA) Dual

Displays

3) RA Display System(s)

C

C

C

2

2

4) TA Display System(s)

−40−3 RA Height Indications (on

PFDs)

C −

B 2

C

2

2

1 (O) May be inoperative on the non−flying pilot side provided TA and RA elements and audio functions are operative on flying pilot side.

1

0

0

0

1

(O) May be inoperative on the non−flying pilot side.

(O) 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.

May be inoperative provided all installed RA display and audio functions are operative.

(O) May be inoperative provided: a) A minimum of one RAD ALT is operative, and b) Approach minimums and operating procedures are not dependent on their use.

(O) May be inoperative provided approach minimums and operating procedures are not dependent on its use.

−40−4 Ground Proximity Warning

System (GPWS) /

Enhanced Ground

Proximity Warning System

(EGPWS)

(CR831CH00064)

If Required by Regulation A 1 a) Modes 1 to 4 A 1

0

0

(O) May be inoperative provided: a) Alternate procedures are established and used, and b) Repairs are made within three flight days.

(O) May be inoperative provided: a) Alternate procedures are established and used, and b) Repairs are made within three flight days.

Page

34−4




Rev 7 Sep 09/2015


LIST PRINCIPALE D







1.





b) Test Mode A 1 c) Flap Over−ride Function A 1 d) Glideslope Deviation

(Mode 5) e) Minimums Alert (Mode

6)

*** f) TAWS Enhanced Mode

(CR831CH00064)

If Not Required by

Regulation

−40−5 GPWS I/F FAIL Engine

Display Message

B 2

C 1

C 1

D 1

B 1

0

0

0

May be inoperative provided: a) The GPWS/EGPWS is considered inoperative, and b) Repairs are made within three flight days.

May be inoperative provided: a) The GPWS/EGPWS flap aural warning is operative, and b) Repairs are made within three flight days.

May be inoperative.

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

0 May be inoperative.


0 (M) Message may be displayed provided GPWS is considered inoperative.






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

34−5





1.





−40−6 Radio Altimeters A 2 0

1

(M)(O) May be inoperative for two flight days provided: a) GPWS/EGPWS is considered inoperative, b) TCAS is considered inoperative, c) Weather minimums or operating procedures are not dependent on use of both, and d) Operations are conducted in compliance with

AFM SUPPLEMENT 11, OPERATION WITH

ONE INOPERATIVE STALL WARNING

AND/OR STICK PUSHER SYSTEM, e) Operations are conducted in compliance with

AFM SUPPLEMENT 37, SUPPLEMENTARY

PERFORMANCE INFORMATION FOR

OPERATION ON CONTAMINATED RUNWAYS, and f) Operations are conducted in compliance with

AFM SUPPLEMENT 39, NOISE ABATEMENT

PROCEDURES AND PERFORMANCE

(LANDING WITH 850 PROPELLER RPM), if applicable.

NOTE:

In the absence of both Radio Altimeters, use the Barometric Altimeters for all height indications.

(M) One may be inoperative.

C 2

−50−1 ATC Transponder / Altitude

Reporting System

1) ATC Transponders

2) ATC Identifier Switch

(on hand −wheels)

C 2

D 2

C 2

C 2

−

0

1

(O) As required by regulations.

May be inoperative, if not required by regulations.

May be inoperative.

0 May be inoperative provided one ATC ID button (on

ARCDU1 or ARCDU2) is operative.

Page

34−6




Rev 7 Sep 09/2015


LIST PRINCIPALE D







1.





−50−2

3) ATC ID Button (on

ARCDU1 or ARCDU2)

4) ADS−B Squitter

Transmissions

VHF Navigation Systems

C

C

A

C

2

2

2

2

C −


0

0

0

−

May be inoperative provided one ATC Identifier Switch

(on hand−wheels) is operative.

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.


NOTE:

Any ADS−B Out function that operates normally may be used.

Any in excess of those required by regulations and not powered by an essential electrical bus may be inoperative provided alternate procedures are established and used.

−50−3 Distance Measuring

Equipment (DME)

1) DME HOLD function A 2

C 2

2) DME System D −

−50−4 Automatic Direction Finding

(ADF) Systems

−50−5 Marker Beacon

If used routinely

D −

C 2

0

1

−

−

(O) May be inoperative provided: a) Associated DME is operative b) Alternate means are established and used to provide position and distance, and c) Repairs are made within three flight days.

May be inoperative provided associated DME is operative.

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

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

0 May be inoperative provided alternate procedures are established and used.






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

34−7





1.





If not used routinely D 2

−50−6

***

Global Positioning System

(GPS)


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

C −

0

1

(O) Except where required by operations, may be inoperative provided alternate procedures are established and used.

NOTE:

1.

TAWS enhanced mode is considered inoperative (if installed), and

2.

ATC ADS−B function is considered inoperative (if installed).

Where required by operations, one GPS must be operative.

NOTE:

This relief is applicable for aircraft with:

1.

TAWS Enhanced Mode

(CR831CH00064) installed and required by regulation, and/or

2.

ATC ADS−B function installed and required by regulation.

Page

34−8




Rev 7 Sep 09/2015


LIST PRINCIPALE D







1.





If not used routinely

−60−1 Flight Directors

D −

D −

C 2

0

1

−

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

NOTE:

1.


2.



NOTE:


1.



2.


Except where enroute operations require their use, may be inoperative provided: a) Approach procedures are not dependent on their use, and b) Autopilot is considered inoperative.






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

34−9





1.





−60−2

***

Flight Management System

(FMS)


C −

0

1

(O) Except where required by operations, may be inoperative provided alternate procedures are established and used.

NOTE:

1.


2.


Where required by operations, one FMS must be operative.

NOTE:


1.



2.


Page

34−10




Rev 7 Sep 09/2015


LIST PRINCIPALE D







1.





If not used routinely D −

D −

0

1


NOTE:

1.


2.



NOTE:


1.



2.







LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

34−11





1.





FMS Database C −

C −

0

1

(O) May be out of currency (outdated) 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 system(s) with out of currency (outdated) database.

En−route/approach navigation is conducted using a current (up to date) FMS database.

SBAS (Satelight Based

Augmentation System )

Level of Service (LOS)

Annunciator

1) LPV LOS Light

2) LNAV LOS Light

3) LAV/VNAV LOS Light

C −

C −

C −

C −

1

0

0

0

May be inoperative provided that the LPV approach must be conducted from the side with the functioning

LPV Light.

May be inoperative provided LPV approaches are not conducted.

May be inoperative.

May be inoperative.







LIST PRINCIPALE D


Rev 6 Mar 26/2014

Page

35−1




35 OXYGEN

−10−1 Flight Deck Fixed Oxygen

System OXYGEN Pressure

Gauges

C 2

−10−2 Flight Deck Fixed Oxygen

System Overboard

Discharge Indicator

−20−1

***

1.





PASSENGER OXYGEN

SYSTEM

1) Entire Automatic

Presentation Passenger

Oxygen System (APPOS)

C 1

B 1

1

0

0

(M) Either the Flight Compartment Gauge or Cylinder

Mounted Gauge may be inoperative provided there is another method to confirm that adequate oxygen is available for the intended flight.

(O) May be missing provided an approved procedure is used to ensure that the oxygen supply is at or above minimum requirements for the flight.

2) Automatic Deployment

3) Passenger Service

Units (PSUs)

4) Lavatory Passenger

Service Unit (PSU)

B 1

D −

C 1

0

−

0

(O) May be inoperative provided: a) Minimum en−route altitude does not exceed

13,000 ft. above MSL.

b) Portable oxygen units are provided for all crew members and 10% of the passengers for half an hour (supplemental oxygen), and c) Passengers are appropriately briefed.

(M) May be inoperative provided the manual deployment system is operative.

(M)(O) Individual PSUs may be inoperative with no flight altitude restriction provided: a) Affected seats are blocked and placarded

INOPERATIVE to prevent occupancy, b) No more than two consecutive banks of seats and their adjacent banks of seats have an inoperative PSU (forward and aft, left and right), and c) Units at assigned flight attendant locations are operative.

(O) May be inoperative provided lavatory is inspected by FA in case of depressurization.

Page

35−2




Rev 6 Mar 26/2014


LIST PRINCIPALE D






35 OXYGEN (CONT’D)

1.





5) Automatic Opening

Feature of Door Latches

−30−1 Protective Breathing

Equipment (PBE)

−30−2 First Aid Oxygen System

B −

D −

D 2

−

−

−

(M)(O) May be inoperative provided: a) The PSU oxygen system is operative, b) The manual deployment system is operative, c) No more than two consecutive banks of seats and their adjacent banks of seats have an inoperative automatic opening feature, and d) Occupants are briefed on oxygen mask access.

(M)(O) Any in excess of those required by regulation may be inoperative or missing provided: a) Required distribution of operative units is maintained throughout the aircraft, b) The inoperative unit is removed from the flight compartment / passenger cabin and its normally installed location is placarded “INOPERATIVE”, or removed from the installed location, secured out of sight and the unit and its normally installed location are placarded “INOPERATIVE”, and c) Procedures are established to alert crew members of inoperative or missing equipment.

(M)(O) Any in excess of those required by regulation may be unserviceable or missing provided: a) Required distribution of operative units is maintained throughout the aircraft, b) The inoperative unit is removed from the passenger cabin and its normally installed location is placarded “INOPERATIVE”, or removed from the installed location secured out of sight and the unit and its normally installed location are placarded “INOPERATIVE”, and c) Procedures are established and used to alert crew members of inoperative or missing equipment.






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

35−3




35 OXYGEN (CONT’D)

1.





−30−3 Portable Oxygen

Dispensing Units

−30−4

***

Dual−Purpose Oxygen

System Units

C −

C −

−

−

(M)(O) Any in excess of those required by regulation may be inoperative or missing provided: a) Required distribution of operative units is maintained throughout the aircraft, b) The inoperative unit is removed from passenger cabin and its normally installed location is placarded "INOPERATIVE", or removed from the installed location, secured out of sight and the unit and its normally installed location are placarded "INOPERATIVE", and c) Procedures are established to alert crew members of inoperative or missing units.

(M#)(O) Any in excess of those required by regulation may be inoperative or missing provided: a) Required distribution of operative units are maintained throughout the aircraft, b) The inoperative unit is removed from passenger cabin and its normally installed location is placarded "INOPERATIVE", or removed from the installed location, secured out of sight and the unit and its normally installed locations are placarded "INOPERATIVE", and c) Procedures are established to alert crew members of inoperative or missing units.







LIST PRINCIPALE D


Rev 6 Mar 26/2014

Page

36−1




36 PNEUMATICS

−10−1 BLEED SYSTEMS

1.





B 2 1

B 2 1

(O) One may be inoperative provided: a) Associated BLEED Switch is selected OFF, b) Flight is not conducted in known or forecast icing condition, c) Flight is conducted at or below 10,000 feet, and d) Flights are conducted in accordance with AFM supplement 100, Operation with ONE BLEED

SYSTEM inoperative.

(O) One may be inoperative provided: a) Associated BLEED Switch is selected OFF, b) Associated Nacelle Shut−Off Valve (NSOV) operates normally, c) LP/HP Switching through relay logic, and

AIRFRAME MODE SELECT de−ice rotary switch operates normally, d) Flight is conducted at or below 10,000 feet, and e) Flights are conducted in accordance with AFM

Supplement 100, Operation with ONE BLEED

SYSTEM inoperative.







LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

38−1




1.





38 WATER/WASTE

−10−1

***

Potable Water Systems C − 0

−10−2

***

C −

Warm Water Wash System

(Not applicable to systems

Deactivated as per

Bombardier Modsum)

C −

C −

0

0

0

(M)(O) May be inoperative provided: a) System is drained and inspected to ensure no leakage, and b) Procedures are established and used to deactivate applicable system components to prevent its use of servicing.

(M)(O) Individual components may be inoperative provided: a) Associated components are deactivated or isolated, and b) Associated system components are verified not to have leaks.

NOTE:

Any portion of the system which operates normally may be used.

(M) May be inoperative provided: a) System is drained and inspected to ensure no leakage, and b) Procedures are established and used to deactivate applicable system components to prevent its use or servicing.

(M)(O) Individual components may be inoperative provided: a) Associated components are deactivated or isolated, and b) Associated system components are verified not to have leaks.

NOTE:

Any portion of the system which operates normally may be used.

Page

38−2




Rev 6 Mar 26/2014


LIST PRINCIPALE D






1.



38 WATER/WASTE (CONT’D)



Drain Mast Heater

−30−1 Lavatory Waste System

C 1

C −

C −

0

−

−

(M)(O) May be inoperative provided: a) Flight and overnight storage is not carried out in freezing conditions, b) Procedures are established and used to verify drain mast and external fill ports’ temperatures are acceptable prior to refilling or draining wash water system, and c) “DRAIN MAST HEATERS INOPERATIVE” is placarded on ground service door 134BR.

(M) Individual components may be inoperative provided: a) Associated components are deactivated or isolated, and b) Associated system components are verified not to have leaks.

NOTE:

Any portion of system which operates normally may be used.

(M)(O) May be inoperative provided: a) Waste is drained and system is inspected for leakage, b) Procedures are established to deactivate system components, and c) Associated lavatory door is locked closed and placarded, “INOPERATIVE − DO NOT ENTER.”

NOTE:

Aviation Occupational Health and Safety

(AOH&S) requirements should be addressed.






LIST PRINCIPALE D


Rev 6 Mar 26/2014

Page

45−1




1.





45 CENTRAL MAINTENANCE SYSTEM

−45−1 Centralized Diagnostic

System (CDS) (incl.

Maintenance Interlock

Switch in Wardrobe)

C 1 0 May be inoperative.







LIST PRINCIPALE D


Rev 6 Mar 26/2014

Page

49−1




49 AUXILIARY POWER UNIT

1.





−00−1

***

−50−1

***

Auxiliary Power Unit (APU) D 1

APU Bleed Air System D 1

0

0

(M) May be inoperative provided APU Airframe Fuel

Shutoff Valve is verified closed.

(M#) May be inoperative provided APU Bleed Valve is verified closed.







LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

52−1




1.





52 DOORS

−10−1 Door Seal System Charging

Valve

−10−2 Door Seal Drain Valve

C 1

C 1

C 1

0

0

0

(M#) May be inoperative provided the valve is secured in the closed position.

May be failed in the closed position.

(O) May be failed in the open position provided flight is conducted in an unpressurized configuration, at or below 10,000 feet MSL in accordance with AFM

Supplement 113, UNPRESSURIZED FLIGHT −

BLEED ON.

−10−3 Internal Baggage Door

1) “INTERNAL BAGG

DOOR” Caution Light

C 1 0 (M) May be inoperative provided: a) Access to the forward baggage compartment through the internal baggage door is considered inoperative, b) Internal Baggage Door is secured closed by an acceptable means or method, and c) Internal Baggage Door is placarded “INTERNAL

BAGGAGE DOOR INOPERATIVE − DO NOT

OPEN”.

NOTE:

Only applicable for aircraft without Flight

Deck Door Remote Access System installed, and with Forward Baggage Compartment installed.

Page

52−2




Rev 7 Sep 09/2015


LIST PRINCIPALE D






52 DOORS (CONT’D)

2) Door Handle

1.





C 1

2) Door Handle (Cont’d) C 1

0

0

(M) If door cannot be unlatched, may be inoperative provided: a) Access to the forward baggage compartment through the internal baggage door is considered inoperative, b) Internal Baggage Door is secured closed by an acceptable means or method, and c) Internal Baggage Door is placarded “INTERNAL


OPEN”.

NOTE:

Only applicable if Forward Baggage

Compartment installed.

(M#) If door cannot be latched, may be inoperative provided: a) Access to the forward baggage compartment through the internal baggage door is considered inoperative, b) Internal Baggage Door is secured closed by an acceptable means or method, and c) Internal Baggage Door is placarded “INTERNAL


OPEN”.

NOTE:

Only applicable if Forward Baggage

Compartment installed.






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

52−3




52 DOORS (CONT’D)

1.





−10−4

***

Aft Entry Stair System A 1 0 (M#) May be inoperative provided: a) Stair System is secured by an acceptable procedure, b) Placarded “INOPERATIVE − DO NOT USE”, and c) Repairs are made prior to completion of the next heavy maintenance visit.

NOTE:

For the purposes of this item, a heavy maintenance visit (HMV) means an airworthiness maintenance program inspection where the aircraft is scheduled to be out of service for 4 or more days.

−10−5 FUSELAGE DOORS

Warning System

1) Airstair Door, Forward

Baggage Door, Aft

Passenger Door and Aft

Service Door Proximity

Sensors a) Pre−Mod 4−126420 or

4−126432

A 8 7 (M)(O) May be inoperative for one door provided: a) The affected door is physically verified closed and locked prior to each flight, b) The warning light is verified to re−trigger flashing upon subsequent door opening, and c) Repairs are made within one flight day.

NOTE:

An inoperative door warning system sensor will render AUTO Mode of the Cabin Pressure Control

System inoperative.

Page

52−4




Rev 7 Sep 09/2015


LIST PRINCIPALE D






52 DOORS (CONT’D)

1.





b) Post −Mod 4−126420 or

4−126432

A 8

2) Airstair Door, Aft

Passenger Door and Aft

Service Door Proximity

Sensors (Forward baggage compartment not installed)

A 6

−30−1 Aft Baggage Door Counter

Balance System

C 2

−30−2 Aft Baggage Door

Telescopic Strut

Lock Release Collar

C 1

C 1

C 1

7

5

0

0

0

0

(M)(O) May be inoperative for one door provided: a) The affected door is physically verified closed and locked prior to each flight, b) The warning light is verified to re−trigger flashing upon subsequent door opening, and c) Repairs are made within one flight day.

NOTE:

An inoperative Passenger Airstair door warning system sensor will render AUTO Mode of the

Cabin Pressure Control System inoperative.

(M)(O) May be inoperative for one door provided: a) The affected door is physically verified closed and locked prior to each flight, b) The warning light is verified to re−trigger flashing upon subsequent door opening, and c) Repairs are made within one flight day.

NOTE:

An inoperative Passenger Airstair door warning system sensor will render AUTO

MODE of the Cabin Pressure Control System inoperative.

(M) 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”.

(M) May be inoperative provided: a) Baggage door is verified closed, locked, and not used, and b) Baggage door is placarded “BAGGAGE DOOR

INOPERATIVE − DO NOT OPEN”.

(M) May be inoperative provided an alternate approved means to support the baggage door in the open position is established and used.

May be inoperative provided the strut is only used in the non−extended position.






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

52−5




52 DOORS (CONT’D)

1.





−50−1

***

Fortified Flight Deck Door

(With Remote Access

System)

1) Automatic Locking

System (Primary System)

Forward baggage compartment installed

A 1

Forward baggage compartment not installed

A 1

0

0

(M)(O) May be inoperative for a maximum of two flight days provided: a) Automatic locking (Remote Access) system is deactivated, b) Secondary locking system (Deadbolt) is verified operative and used to lock the door, c) Alternate procedures are established and used for using the mechanical (Deadbolt) system and for accessing the flight compartment, d) Access to the Forward baggage compartment through the Internal baggage door is considered inoperative, e) Internal baggage door to the Forward baggage compartment is secured closed by an acceptable means or method, and f) Internal baggage door is placarded, “INTERNAL


OPEN”.

(M)(O) May be inoperative for a maximum of two flight days provided: a) Automatic locking (Remote Access) system is deactivated, b) Secondary locking system (Deadbolt) is verified operative and used to lock the door, and c) Alternate procedures are established and used for using the mechanical (Deadbolt) system and for accessing the flight compartment.

Page

52−6




Rev 7 Sep 09/2015


LIST PRINCIPALE D






52 DOORS (CONT’D)

1.





2) Flight Deck Emergency

Access Function


A 1


A 1

0

0

(M)(O) May be inoperative for a maximum of flight days provided: a) Automatic locking (Remote Access) system is deactivated, b) Secondary locking system (Deadbolt) is verified operative and used to lock the door, c) Alternate procedures are established and used for using the mechanical (Deadbolt) system and for accessing the flight compartment, d) Access to the Forward baggage compartment through the Internal baggage door is considered inoperative, e) Internal baggage door to the Forward baggage compartment is secured closed by an acceptable means or method, and f) Internal baggage door is placarded, “INTERNAL


OPEN”.

(M)(O) May be inoperative for a maximum of two flight days provided: a) Automatic locking (Remote Access) system is deactivated, b) Secondary locking system (Deadbolt) is verified operative and used to lock the door, c) Alternate procedures are established and used for using the mechanical (Deadbolt) system and for accessing the flight compartment.






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

52−7




52 DOORS (CONT’D)

1.





3) DENY Function


A 1


A 1

0

0

(M)(O) May be inoperative for a maximum of flight days provided: a) Automatic locking (Remote Access) system is deactivated, b) Secondary locking system (Deadbolt) is verified operative and used to lock the door, c) Alternate procedures are established and used for using the mechanical (Deadbolt) system and for accessing the flight compartment, d) Access to the Forward baggage compartment through the Internal baggage door is considered inoperative, e) Internal baggage door to the Forward baggage compartment is secured closed by an acceptable means or method, and f) Internal baggage door is placarded, “INTERNAL


OPEN”.

(M)(O) May be inoperative for a maximum of two flight days provided: a) Automatic locking (Remote Access) system is deactivated, b) Secondary locking system (Deadbolt) is verified operative and used to lock the door, c) Alternate procedures are established and used for using the mechanical (Deadbolt) system and for accessing the flight compartment.

Page

52−8




Rev 7 Sep 09/2015


LIST PRINCIPALE D






52 DOORS (CONT’D)

4) UNLK Function

1.





C 1 0

0

(O) May be inoperative provided: a) Automatic locking system is verified operative, b) Emergency access function is verified operative, and c) Alternate procedures are established and used for using the mechanical (Deadbolt) system, and for accessing the flight compartment.

(O) May be inoperative provided Emergency access function is verified operative.

5) Emergency Access

Push Button Switch Panel

White/Amber Indication

Lights

6) “FAIL” − COCKPIT

DOOR Advisory Light


C 4

C 1


C 1

0

0

(M)(O) May be inoperative provided: a) Door Unlock and Auto Lock functions are verified operative, b) “INTERNAL DOORS” caution light is verified operative, and c) “BAGG DOOR”, “CKPT DOOR” and “AUTO

UNLK” advisory lights are verified operative.

(M)(O) May be inoperative provided: a) Door Unlock and Auto Lock functions are verified operative, b) “COCKPIT DOOR” caution light is verified operative, and c) “CKPT DOOR” and “AUTO UNLK” advisory lights are verified operative.






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

52−9




52 DOORS (CONT’D)

1.





7) “CKPT DOOR” − OPEN

Advisory Light


C 1


C 1

0

0

(M)(O) May be inoperative provided: a) Automatic door lock function is verified operative, b) “INTERNAL DOORS” caution light is verified operative in the event door is left open more than three (3) minutes, and c) “BAGG DOOR”, “FAIL”, and “AUTO UNLK” advisory lights are verified operative.

(M)(O) May be inoperative provided: a) Automatic door lock function is verified operative, b) “COCKPIT DOORS” caution light is verified operative in the event door is left open more than three (3) minutes, and c) “FAIL”, and “AUTO UNLK” advisory lights are verified operative.

8) “AUTO UNLK” −

COCKPIT DOOR Advisory

Light


C 1


C 1

0

0

(M)(O) May be inoperative provided: a) Emergency access function is verified operative, b) “INTERNAL DOORS” caution light is verified operative, and c) “BAGG DOOR”, ”CKPT DOOR” and “FAIL” advisory lights are verified operative.

(M)(O) May be inoperative provided: a) Emergency access function is verified operative, b) “COCKPIT DOORS” caution light is verified operative, and c) “CKPT DOOR”, and “FAIL” advisory lights are verified operative.

Page

52−10




Rev 7 Sep 09/2015


LIST PRINCIPALE D






52 DOORS (CONT’D)

1.





9) “BAGG DOOR” −

OPEN Advisory Light

(Forward Baggage

Compartment Installed)

C 1

10) Deadbolt (Secondary locking system)

11) “INTERNAL DOORS”

Caution Light (Forward baggage compartment installed)

C 1

A 1

0

0

0

(M)(O) May be inoperative provided: a) Forward baggage door lock is operative, b) “INTERNAL DOORS” caution light is verified operative, and c) “CKPT DOOR”, ”FAIL” and “AUTO UNLK” advisory lights are verified operative.

(O) May be inoperative provided Automatic locking

(Remote Access) system is operative.

(M)(O) May be inoperative for a maximum of two flight days provided: a) Automatic locking (Remote Access) system is deactivated, b) Secondary locking system (Deadbolt) is verified operative and used to lock the door, c) Alternate procedures are established and used for using the mechanical (Deadbolt) system, and for accessing the flight compartment, d) Access to the Forward baggage compartment through the Internal baggage door is considered inoperative, e) Internal baggage door is secured closed by an acceptable means or method, and f) Internal baggage door is placarded, “INTERNAL


OPEN”.






LIST PRINCIPALE D


Rev 7 Sep 09/2015

Page

52−11




52 DOORS (CONT’D)

−50−2

***

−50−3

***

−50−4

***

−50−5

***

−50−6

***

−50−7

***

−50−8

***

−50−9

***

−50−10

***

−50−11

***

UNLK Function

1.





12) “COCKPIT DOOR”

Caution Light (Forward baggage compartment not installed)

A 1

Flight Deck Emergency

Access Function

DENY Function

Emergency Access Push

Button Switch − White /

Amber Indication Lights

COCKPIT DOOR − ’FAIL’

Advisory Light

CKPT DOOR Open

Advisory Light

CKPT DOOR ’AUTO UNLK’

Advisory Light

BAGG DOOR Advisory

Light

Deadbolt

INTERNAL DOORS

Caution Light

0 (M)(O) May be inoperative for a maximum of two flight days provided: a) Automatic locking (Remote Access) system is deactivated, b) Secondary locking system (Deadbolt) is verified operative and used to lock the door, and c) Alternate procedures are established and used for using the mechanical (Deadbolt) system, and for accessing the flight compartment.

Incorporated into Item 52−50−1, 2).



Incorporated in Item 52−50−1, 5).







Page

52−12




Rev 7 Sep 09/2015


LIST PRINCIPALE D






52 DOORS (CONT’D)

1.





−50−12 Fortified Flight Deck Door

(Without Remote Access

System)

1) Deadbolt Lock

−50−13 Lavatory Door Lock/Door

Latch

1) Door Lock

C 1

C −

2) Door Latch

0 (O) May be inoperative provided primary locking mechanism, slide latch, is operative.

C −

0

0

(O) May be inoperative provided: a) Lavatory door latch operates normally, and b) Procedures are established and used to inform occupants of inoperative door lock.

(M) May be inoperative provided:

Lavatory door is locked closed and placarded,

“INOPERATIVE − DO NOT ENTER”.






LIST PRINCIPALE D


Rev 6 Mar 26/2014

Page

61−1




61 PROPELLERS

−20−1 Propeller Maintenance

Unfeather Function

−20−2

***

RDC NP Switch

1.





D 2 0 (M#) May be inoperative provided an alternate feather check is performed.

Moved to 76−10−01 ENGINE CONTROL Panel

Switches







LIST PRINCIPALE D


Rev 6 Mar 26/2014

Page

71−1




71 POWER PLANT

−60−1 Engine Intake Bypass

Doors

1.





C 2 0

C 2 0

May be inoperative in closed position provided the flight is not conducted in known or forecast icing conditions.

(M#)(O) May be inoperative in the open position provided: a) The OAT along the route flown is less than ISA

+25 degrees C., b) The related engine oil temperature indicator operates normally and is monitored, and c) The associated intake heater(s) is confirmed operative prior to each flight into known or forecast icing conditions.







LIST PRINCIPALE D


Rev 6 Mar 26/2014

Page

73−1




1.





73 ENGINE FUEL AND CONTROL

−20−1 Engine FADEC System

FADEC faults A − −

−20−2

***

MTOP Switch

−20−3 Power Rating Switches

1) MCR Switch

May be dispatched with FADEC faults provided repairs are made in accordance with times established in the

Time Limited Dispatch section of Pratt & Whitney

Canada Airworthiness Limitations Manual Part No.

3043520.

NOTE:

1.

MEL extensions are not permitted.

2.

Time Limited Dispatch reporting system is maintained as per Pratt &

Whitney Canada Airworthiness

Limitations Manual Part No. 3043520.


Switches


Switches.

2) MCL Switch

−20−4 Reduce Power Switches

1) RDC TOP TRQ DEC

Switch

2) RDC TOP TRQ RESET

Switch

−30−1 FF (Fuel Flow) Indications B 2 1


Switches.

May be inoperative provided Fuel QTY indications are operative.







LIST PRINCIPALE D


Rev 6 Mar 26/2014

Page

76−1




1.





76 ENGINES

−10−1 ENGINE CONTROL Panel

Switches

1) RDC Np LDG Switch

***

2) MTOP Switch

***

C 1

C 1

0

0

3) MCR Switch

4) MCL Switch

5) RDC TOP TRQ DEC

Switch

6) RDC TOP TRQ RESET

Switch

C 1

D 1

D 1

D 1

D 1

0

0

0

0

0

May be inoperative provided the RDC Np LDG function is not used.

(O) May be inoperative in the ON (selected) position provided: a) #1 and #2 ENG FADEC caution lights are extinguished, b) MTOP is annunciated on ED when condition levers are at MAX/1020, and c) Flight is conducted in accordance with the AFM

Supplement 46, TAKE−OFF WITH MAXIMUM

POWER AND UPTRIM DISABLED.

NOTE:

1.

Do not press (select) MTOP switch during Pre−Take−off Checks.

2.

Do not press (deselect) MTOP switch during In−flight procedures after

Take−off. NTOP will not appear on ED.

May be failed in the OFF (deselected) position provided: a) #1 and #2 ENG FADEC caution lights are extinguished, b) NTOP is annunciated on ED when condition levers are at MAX/1020, and c) MTOP is not used.

May be inoperative provided condition levers are used to set power rating.

May be inoperative provided condition levers are used to set power rating.

May be inoperative provided RDC TOP TRQ DEC is not used.

May be inoperative provided RDC TOP TRQ DEC is not used.







LIST PRINCIPALE D


Rev 6 Mar 26/2014

Page

77−1




1.





77 ENGINE INDICATING

−30−1 Engine Monitoring Unit

(EMU)

D 1 0 May be inoperative provided alternate procedures are established and used to record engine data.







LIST PRINCIPALE D


Rev 6 Mar 26/2014

Page

79−1




1.





79 ENGINE OIL

−30−1

***

OIL LEVEL Indication in

Cockpit

D 2 0 (M) May be inoperative provided engine oil level is confirmed by alternate means.


Dash 8 Series 400, DOT, Master Minimum Equipment List, PSM 1

DEPARTMENT OF TRANSPORT

MASTER MINIMUM EQUIPMENT LIST

MANUAL

Technical Publications

Manual Change Request

MASTER MINIMUM EQUIPMENT LIST

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