Dash 8 Series 400, DOT, Master Minimum Equipment List, PSM A.

Transcription

1 E To: Distribution Date: 09 September, 2015 Subject: Dash 8 Series 400, DOT, Master Minimum Equipment List, PSM A. This is Revision 7 of the Dash 8 Series 400, DOT, Master Minimum Equipment List (MMEL), PSM A, dated 09 September, 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 CABIN PRESS Warning Light (TR141) incorporated. Item Cabin ALT Indicator (TR142) incorporated. Item Cabin DIFF Pressure Indicator (TR143) incorporated. Item Cabin RATE Indicator (TR144) incorporated. Item Cabin Pressure Control System (TR145) incorporated. Item 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 Alerting System (CHIME/LIGHT), revised to further clarified to include all the PACIS lights relief and to update CALL lights number installed. Item 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 Revised the number required for dispatch is changed, 1 to 0 for case 2. Item Galley Waste Compartment, update the MMEL to include relief for the Galley Waste Compartment. Item Exterior Lavatory Door Ashtrays, revised to add relief for aircraft with more than one exterior PAGE 1

2 E lavatory door ashtray as relief is currently only for aircraft with one lavatory door ashtray. Item Compartment Liners. Relief is for both forward and aft cargo compartment liners. Item Emergency Locator Transmitter, update to provide clarification to the procedures as well clarify current provisos to fall in line with CAR and Item To update MMEL relief with a note defining over water to clarify proviso. Item New MMEL relief is being proposed for life vests installed on the Q400 series aircraft. Item To provide relief for inoperative Cabin Video Monitoring and Surveillance System partial failure. Item Revision bar is for minor editorial change only. No changes to the item. Item Minor editorial change. Item Revised for 86 passenger configuration, TR 147. Item Revised for 86 passenger configuration, TR 148. Item To update relief to include the partial failure of the Pressure Refueling System. Item New proposal to allow for relief for MASTER VALVE CLOSED indication on Q400 aircraft. Item Revision bar due to software issue, no changes. Item To create a new MMEL item for inoperative Hydraulic Firewall Shutoff Valve (HYD FSOV) OPEN Indicator Light. Item To update relief to include the option of an operational procedure to verify operation of heaters during flight. Item To update MMEL provisos to change M# procedure to a M and O procedure. Item Windshield heaters, revised. (TR 140) Item Provisos updated to include night operation with the spigot light failed. Item 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 To extend the relief period to allow operators the ability to get to a maintenance base. Item Revise MMEL to add relief for the Caution/Warning/Advisory Light System Brighten and Dimming Function whose BRT function is inoperative. Item Revised for 86 passenger configuration, (TR 149). Item Revision bar due to software issue, no changes. Item Revised the existing MMEL relief for Emergency Marker and Emergency Locator Signs in the classic Interior. Item To update relief for Integrated Standby Instrument (ISI) to include relief for the STD Button. Item New relief for the Inertial Reference System (IRS) optional installation, required only for Required Navigation Performance Authorization Required (AR). Item ATC Transponder / Altitude Reporting System, revised (TR 153). Item Update the Global Positioning System (GPS) MMEL relief to meet new requirements (TR 154). Item Update the MMEL relief for the Flight Directors (FD) to meet new requirements. Item MMEL proviso updates to consider the RNP AR 0.3/0.3 approach, the TAWS Enhanced PAGE 2

3 E mode and to correct the existing relief for the FMS database (TR 155). Item Revised for 86 passenger configuration (TR 150). Item Item name revised. Item Editorial change to proviso was made to change the applicable AFM reference. (TR 146). Item Revised for 86 passenger configuration, (TR 151). Item Updated MMEL wording with editorial change to proviso. Item FUSELAGE DOORS warning system revised, (TR 152). Item Fortified Flight Deck Door, revised (TR 156). Item This item referred to Item Item This item referred to Item Item This item referred to Item Item This item referred to Item Item This item referred to Item Item This item referred to Item Item This item referred to Item Item This item referred to Item Item This item referred to Item Item This item referred to Item We recommend that this letter of transmittal be retained and placed in the front of the manual for record purposes. PAGE 3

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5 E DEPARTMENT OF TRANSPORT MANUAL PSM A 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 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

6 "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."

7 Technical Publications Manual Change Request B TO: MCR FOCAL, TECHNICAL PUBLICATIONS BOMBARDIER AEROSPACE 123 GARRATT BLVD. TORONTO, ONTARIO, CANADA, M3K 1Y5 MAIL STOP: N42 25 FAX: (416) E MAIL ADDRESS: [email protected] ALL fields marked with an asterisk * are required Contact Information Name of Airline: Bombardier Reference #: Date: *Name: *Corporation Name: *Dept Name/Code: Address: City: State/Province: Postal Code / Zip: Country: *Telephone: Mobile/Cell Phone: Fax Number: *E Mail: I would like to receive notification of actions on this request. NOTE: Responses will only be sent by electronic mail. Publication Information *Aircraft Type: *Aircraft Model: *PSM/CSP: *Publication Name/Revision: Originator s reference number: *Media Type: Paper CD ROM DVD ifly *Chapter/Section/Subject/Task (or) Block/ Number: Impact on other programs: *Description of Change Request: Reason for change: Reference data provided: Yes No Description: NOTE: Electronic submissions of MCRs are available on Oct 04/2013

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9 Approval DHC 8 SERIES 400 MANUAL APPROVAL This is to certify that the PSM A 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

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11 Bombardier Inc. DHC 8 Series 400 List of Effective s Transmittal Rev 5 NOV 28/2011NOV 28/ / /2014 * 21 5 Sep 21 6 Rev 6 Mar 26/2014Mar Approval * Sep 09/ Rev 6 Mar 26/2014Mar 26/2014 List of Effective s * 1 Sep 09/2015 * 2 Sep 09/2015 * 3 Sep 09/2015 Log of Revisions 09/ /2014 * 1 Sep 2 Rev 6 Mar 26/2014Mar 28/ / / / / /2014 Temporary Revision Index 1 Rev 5 NOV 28/2011NOV 2 Rev 5 NOV 28/2011NOV 3 Rev 5 NOV 28/2011NOV 4 Rev 5 NOV 28/2011NOV 5 Rev 5 NOV 28/2011NOV 6 Rev 6 Mar 26/2014Mar * 7 Sep 09/2015 * 8 Sep 09/2015 * 9 Sep 09/2015 Table of Contents 1 Rev 5 NOV 28/2011NOV 28/ / /2011 Preamble 1 Rev 5 NOV 28/2011NOV 2 Rev 5 NOV 28/2011NOV Notes & Definitions 1 Rev 5 NOV 28/2011NOV 28/2011 * 2 Sep 09/2015 * 23 1 Sep 09/2015 * 23 2 Sep 09/2015 * 23 3 Sep 09/2015 * 23 4 Sep 09/2015 * 23 5 Sep 09/2015 * 23 6 Sep 09/ / / Rev 6 Mar 26/2014Mar 24 2 Rev 6 Mar 26/2014Mar 25 1 Rev 6 Mar 26/2014Mar 26/2014 * 25 2 Sep 09/2015 * 25 3 Sep 09/2015 * 25 4 Sep 09/2015 * 25 5 Sep 09/2015 * 25 6 Sep 09/2015 * 25 7 Sep 09/2015 * 25 8 Sep 09/2015 * 25 9 Sep 09/2015 * Sep 09/2015 * Sep 09/2015 * Sep 09/2015 * Sep 09/2015 * Sep 09/2015 * Sep 09/2015 * Sep 09/2015 * 3 Sep 09/2015 * 4 Sep 09/2015 * 5 Sep 09/ Rev 6 Mar 26/2014Mar 26/2014 * 26 2 Sep 09/ Rev 6 Mar 26/2014Mar 26/2014 * 26 4 Sep 09/2015 * 26 3 Sep 09/2015 * 21 2 Sep 09/ / /2014 * 21 3 Sep 21 4 Rev 6 Mar 26/2014Mar * 26 5 Sep 09/2015 * 26 6 Sep 09/2015 * 26 7 Sep 09/2015 The asterisk (*) indicates pages revised, added or deleted by current revision. L 1

12 Bombardier Inc. DHC 8 Series 400 List of Effective s (Cont d) 27 1 Rev 6 Mar 26/2014Mar 26/2014 * 27 2 Sep 09/ / /2014 * 27 3 Sep 27 4 Rev 6 Mar 26/2014Mar 26/ / / / Rev 6 Mar 26/2014Mar * 34 2 Sep * 34 3 Sep * 34 4 Sep * 34 5 Sep 09/2015 * 34 6 Sep 09/2015 * 28 1 Sep 09/2015 * 28 2 Sep 09/2015 * 34 7 Sep 09/2015 * 34 8 Sep 09/2015 * 34 9 Sep 09/2015 * 29 1 Sep 09/ / /2014 * 29 2 Sep 29 3 Rev 6 Mar 26/2014Mar * Sep 09/2015 * Sep 09/ Rev 6 Mar 26/2014Mar 26/2014 * 30 2 Sep 09/ / / Rev 6 Mar 26/2014Mar 35 2 Rev 6 Mar 26/2014Mar * 35 3 Sep 09/2015 * 30 3 Sep 09/2015 * 30 4 Sep 09/ Rev 6 Mar 26/2014Mar 26/ Rev 6 Mar 26/2014Mar 26/2014 * 31 2 Sep 09/ / /2014 * 38 1 Sep 38 2 Rev 6 Mar 26/2014Mar * 31 3 Sep 09/ Rev 6 Mar 26/2014Mar 26/ Rev 6 Mar 26/2014Mar 26/2014 * 32 2 Sep 09/ Rev 6 Mar 26/2014Mar 26/ / / / /2014 * 33 1 Sep 33 2 Rev 6 Mar 26/2014Mar 33 3 Rev 6 Mar 26/2014Mar 33 4 Rev 6 Mar 26/2014Mar * 33 5 Sep 09/2015 * 33 6 Sep 09/2015 * 33 7 Sep 09/2015 * 33 8 Sep 09/2015 * 33 9 Sep 09/2015 * Sep 09/ / / / / / / / / /2015 * 52 1 Sep * 52 2 Sep * 52 3 Sep * 52 4 Sep * 52 5 Sep * 52 6 Sep * 52 7 Sep * 52 8 Sep * 52 9 Sep 09/ / /2015 * Sep * Sep * Sep The asterisk (*) indicated pages revised, added or deleted by current revision L 2

13 Bombardier Inc. DHC 8 Series 400 List of Effective s (Cont d) 61 1 Rev 6 Mar 26/2014Mar 26/ Rev 6 Mar 26/2014Mar 26/ Rev 6 Mar 26/2014Mar 26/ Rev 6 Mar 26/2014Mar 26/ Rev 6 Mar 26/2014Mar 26/ Rev 6 Mar 26/2014Mar 26/2014 The asterisk (*) indicated pages revised, added or deleted by current revision L 3

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15 Bombardier Inc. DHC 8 Series 400 LOG OF REVISIONS Log of Revisions 1 When revisions are received and inserted, record the relevant information in the appropriate columns of the LOG OF REVISIONS below. REV. NO. ISSUE DATE DATE INSERTED INSERTED BY REV. NO. ISSUE DATE DATE INSERTED INSERTED BY 1 24 December, December, 1999 DHI 2 24 May May 2002 DHI 3 16 July July 2004 DHI January November, March, September, January November March, 2014 DHI DHI DHI BCSG: Bombardier Customer Service Group

16 Bombardier Inc. DHC 8 Series 400 LOG OF REVISIONS Log of Revisions 2 Rev 6 Mar 26/2014 REV. NO. ISSUE DATE DATE INSERTED INSERTED BY REV. NO. ISSUE DATE DATE INSERTED INSERTED BY BCSG: Bombardier Customer Service Group

17 BOMBARDIER MANUAL (DOT) EFFECTIVE TEMPORARY REVISIONS The following Temporary Revisions are effective in your Manual at Revision 7 dated Sep 09, 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

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19 Bombardier Inc. DHC 8 Series 400 TEMPORARY REVISION INDEX T.R. Index 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. REVISION TEMPORARY REVISION NO. SECTION / PAGE NO. ISSUE DATE DATE INSERTED INSERTED BY DATE REMOVED REMOVED BY INCORP. IN / REPLACED WITH MMEL Feb/00 21 Feb/00 BCSG 24 May /02 BCSG Rev. 2 MMEL Feb/00 21 Feb/00 BCSG 09 May /00 BCSG TR 12 MMEL Mar/00 23 Mar/00 BCSG 24 May /02 BCSG Rev. 2 MMEL Mar/00 23 Mar/00 BCSG 24 May /02 BCSG Rev. 2 MMEL Aprr/00 05 Apr/00 BCSG 24 May /02 BCSG Rev. 2 MMEL May/00 09 May/00 BCSG 24 May /02 BCSG Rev. 2 MMEL May/00 09 May/00 BCSG 24 May /02 BCSG Rev. 2 MMEL May/00 09 May/00 BCSG 24 May /02 BCSG Rev. 2 MMEL May/00 09 May/00 BCSG 24 May /02 BCSG Rev. 2 MMEL May/00 09 May/00 BCSG 24 May /02 BCSG Rev. 2 MMEL May/00 09 May/00 BCSG 24 May /02 BCSG Rev. 2 MMEL May/00 09 May/00 BCSG 31 Oct/01 BCSG TR 32 MMEL May/00 12 May/00 BCSG 24 May /02 BCSG Rev. 2 MMEL May/00 29 May/00 BCSG 24 May /02 BCSG Rev. 2 MMEL May/00 29 May/00 BCSG 17 Oct/01 BCSG TR 30 MMEL Jun/00 16 Jun/00 BCSG 24 May /02 BCSG Rev. 2 MMEL Jun/00 28 Jun/00 BCSG 24 May /02 BCSG Rev. 2 MMEL Aug/00 08 Aug/00 BCSG 24 May /02 BCSG Rev. 2 MMEL Sep/00 12 Sep/00 BCSG 24 May /02 BCSG Rev. 2 MMEL Oct/00 23 Oct/00 BCSG 24 May /02 BCSG Rev. 2 MMEL Mar/01 02 Mar/01 BCSG 24 May /02 BCSG Rev. 2 MMEL Mar/01 02 Mar/01 BCSG 24 May /02 BCSG Rev. 2 BCSG: Bombardier Customer Service Group

20 Bombardier Inc. DHC 8 Series 400 TEMPORARY REVISION INDEX T.R. Index 2 Rev 5 NOV 28/2011 REVISION TEMPORARY REVISION NO. SECTION / PAGE NO. ISSUE DATE DATE INSERTED INSERTED BY DATE REMOVED REMOVED BY INCORP. IN / REPLACED WITH MMEL May/01 04 May/01 BCSG 24 May /02 BCSG Rev. 2 MMEL Jul/01 10 Jul/001 BCSG 24 May /02 BCSG Rev. 2 MMEL Aug/01 28 Aug/01 BCSG 24 May /02 BCSG Rev. 2 MMEL Aug Aug 01 BCSG 24 May /02 BCSG Rev. 2 MMEL 27 PAGE 1 18 Jun/01 18 Jun/01 BCSG 24 May /02 BCSG Rev. 2 MMEL Jul/01 23 Jul/01 BCSG 24 May /02 BCSG Rev. 2 MMEL Sep/01 19 Sep/01 BCSG 24 May /02 BCSG Rev. 2 MMEL Oct/01 17 Oct/01 BCSG 24 May /02 BCSG Rev. 2 MMEL Oct/01 31 Oct/01 BCSG 24 May /02 BCSG Rev. 2 MMEL Oct/01 31 Oct/01 BCSG 24 May /02 BCSG Rev. 2 MMEL Nov/01 06 Nov/01 BCSG 24 May /02 BCSG Rev. 2 MMEL Nov/01 07 Nov/01 BCSG 24 May /02 BCSG Rev. 2 MMEL Nov/01 13 Nov/01 BCSG 24 May /02 BCSG Rev. 2 MMEL Nov/01 13 Nov/01 BCSG 24 May /02 BCSG Rev. 2 MMEL Nov/01 23 Nov/01 BCSG 24 May /02 BCSG Rev. 2 MMEL Jan/02 18 Jan/02 BCSG 24 May /02 BCSG Rev. 2 MMEL Mar/02 28 Mar/02 BCSG 24 May /02 BCSG Rev. 2 MMEL Mar/02 28 Mar/02 BCSG 24 May /02 BCSG Rev. 2 MMEL Jul/02 04 Jul/02 BCSG 16 Jul/04 BCSG Rev. 3 MMEL Jul/02 04 Jul/02 BCSG 16 Jul/04 BCSG Rev. 3 MMEL Aug/02 23 Aug/02 BCSG 16 Jul/04 BCSG Rev. 3 MMEL Dec/02 05 dec/02 BCSG 16 Jul/04 BCSG Rev. 3 BCSG: Bombardier Customer Service Group

21 Bombardier Inc. DHC 8 Series 400 TEMPORARY REVISION INDEX T.R. Index 3 Rev 5 NOV 28/2011 REVISION TEMPORARY REVISION NO. SECTION / PAGE NO. ISSUE DATE DATE INSERTED INSERTED BY DATE REMOVED REMOVED BY INCORP. IN / REPLACED WITH MMEL Nov/02 15 Nov/02 BCSG 16 Jul/04 BCSG Rev. 3 MMEL Dec/02 03 Dec/02 BCSG 16 Jul/04 BCSG Rev. 3 MMEL Aug/03 14 Aug/03 BCSG 16 Jul/04 BCSG Rev. 3 MMEL Apr/03 08 Apr/03 BCSG 16 Jul/04 BCSG Rev. 3 MMEL Aug Aug 03 BCSG 16 Jul/04 BCSG Rev. 3 MMEL Sep/03 11 Sep/03 BCSG 16 Jul/04 BCSG Rev. 3 MMEL Jun/04 24 Jun/04 BCSG 16 Jul/04 BCSG Rev. 3 MMEL Oct/04 25 Oct/04 BCSG 24 Jan/08 BCSG Rev. 4 MMEL Nov/04 12 Nov 04 BCSG 24 Jan/08 BCSG Rev. 4 MMEL Oct/04 04 Oct/04 BCSG 24 Jan/08 BCSG Rev. 4 MMEL Dec/04 06 Dec/04 BCSG 29 Dec/05 BCSG TR 74 MMEL Dec/04 07 Dec/04 BCSG 24 Jan/08 BCSG Rev. 4 MMEL Jan/05 12 Jan/05 BCSG 24 Jan/08 BCSG Rev. 4 MMEL Jan/05 18 Jan/05 BCSG 24 Jan/08 BCSG Rev. 4 MMEL Apr/05 28 Apr/05 BCSG 24 Jan/08 BCSG Rev. 4 MMEL Apr/05 28 Apr/05 BCSG 24 Jan/08 BCSG Rev. 4 MMEL Apr/05 28 Apr/05 BCSG 24 Jan/08 BCSG Rev. 4 MMEL Apr/05 28 Apr/05 BCSG 24 Jan/08 BCSG Rev. 4 MMEL Apr/05 28 Apr/05 BCSG 24 Jan/08 BCSG Rev. 4 MMEL Apr/05 28 Apr/05 BCSG 24 Jan/08 BCSG Rev. 4 MMEL Apr/05 28 Apr/05 BCSG 24 Jan/08 BCSG Rev. 4 MMEL May/05 24 May/05 BCSG 24 Jan/08 BCSG Rev. 4 BCSG: Bombardier Customer Service Group

22 Bombardier Inc. DHC 8 Series 400 TEMPORARY REVISION INDEX T.R. Index 4 Rev 5 NOV 28/2011 REVISION TEMPORARY REVISION NO. SECTION / PAGE NO. ISSUE DATE DATE INSERTED INSERTED BY DATE REMOVED REMOVED BY INCORP. IN / REPLACED WITH MMEL May/05 24 May/05 BCSG 24 Jan/08 BCSG Rev. 4 MMEL May/05 24 May/05 BCSG 24 Jan/08 BCSG Rev. 4 MMEL Jun/05 23 Jun/05 BCSG 24 Jan/08 BCSG Rev. 4 MMEL Jun/05 23 Jun/05 BCSG 24 Jan/08 BCSG Rev. 4 MMEL Jul/05 27 Jul/05 BCSG 24 Jan/08 BCSG Rev. 4 MMEL Sep/05 14 Sep/05 BCSG 24 Jan/08 BCSG Rev. 4 MMEL Sep/05 14 Sep/05 BCSG 24 Jan/08 BCSG Rev. 4 MMEL Dec/05 29 Dec/05 BCSG 24 Jan/08 BCSG Rev. 4 MMEL Jan/06 27 Jan/06 BCSG 24 Jan/08 BCSG Rev. 4 MMEL Sep/06 05 Sep/06 BCSG 24 Jan/08 BCSG Rev. 4 MMEL May/05 31 May/05 BCSG 24 Jan/08 BCSG Rev. 4 MMEL May/05 31 May/05 BCSG 24 Jan/08 BCSG Rev. 4 MMEL May/05 31 May/05 BCSG 24 Jan/08 BCSG Rev. 4 MMEL Nov/06 08 Nov/06 BCSG 24 Jan/08 BCSG Rev. 4 MMEL Nov/06 08 Nov/06 BCSG 24 Jan/08 BCSG Rev. 4 MMEL Nov/06 08 Nov/06 BCSG 24 Jan/08 BCSG Rev. 4 MMEL Dec/06 06 Dec/06 BCSG 24 Jan/08 BCSG Rev. 4 MMEL Apr/07 02 Apr/07 BCSG 24 Jan/08 BCSG Rev. 4 MMEL Mar/07 29 Mar/07 BCSG 24 Jan/08 BCSG Rev. 4 MMEL Mar/08 28 Mar/08 BCSG 28 Nov/11 BCSG Rev. 5 MMEL Apr Apr 08 BCSG 28 Nov/11 BCSG Rev. 5 MMEL Apr Apr 08 BCSG 28 Nov/11 BCSG Rev. 5 BCSG: Bombardier Customer Service Group

23 Bombardier Inc. DHC 8 Series 400 TEMPORARY REVISION INDEX T.R. Index 5 Rev 5 NOV 28/2011 REVISION TEMPORARY REVISION NO. SECTION / PAGE NO. ISSUE DATE DATE INSERTED INSERTED BY DATE REMOVED REMOVED BY INCORP. IN / REPLACED WITH MMEL May May 08 BCSG 28 Nov/11 BCSG Rev. 5 MMEL BCSG BCSG TR106 MMEL Jan Jan 09 BCSG 28 Nov/11 BCSG Rev. 5 MMEL Jan Jan 09 BCSG 28 Nov/11 BCSG Rev. 5 MMEL Mar Mar 09 BCSG 28 Nov/11 BCSG Rev. 5 MMEL June June 09 BCSG 11 Jan 11 BCSG TR117 MMEL June June 09 BCSG 24 Jan 11 BCSG TR116 MMEL June June 09 BCSG 07 Jan 11 BCSG TR115 MMEL Sep Sep 09 BCSG 04 Aug 10 BCSG TR111 MMEL Oct Oct 09 BCSG 28 Nov/11 BCSG Rev. 5 MMEL Oct Oct 09 BCSG 28 Nov/11 BCSG Rev. 5 MMEL Nov Nov 09 BCSG 28 Nov/11 BCSG Rev. 5 MMEL May May 10 BCSG 28 Nov/11 BCSG Rev. 5 MMEL May May 10 BCSG 28 Nov/11 BCSG Rev. 5 MMEL May May 10 BCSG 28 Nov/11 BCSG Rev. 5 MMEL May May 10 BCSG 28 Nov/11 BCSG Rev. 5 MMEL July July 10 BCSG 28 Nov/11 BCSG Rev. 5 MMEL July July 10 BCSG 28 Nov/11 BCSG Rev. 5 MMEL July July 10 BCSG 28 Nov/11 BCSG Rev. 5 MMEL July July 10 BCSG 28 Nov/11 BCSG Rev. 5 MMEL July July 10 BCSG 28 Nov/11 BCSG Rev. 5 MMEL Aug Aug 10 BCSG 28 Nov/11 BCSG Rev. 5 BCSG: Bombardier Customer Service Group

24 Bombardier Inc. DHC 8 Series 400 TEMPORARY REVISION INDEX T.R. Index 6 Rev 6 Mar 26/2014 TEMPORARY SECTION / ISSUE DATE INSERTED REVISION NO. PAGE NO. DATE INSERTED BY MMEL Aug Aug 10 BCSG MMEL Aug aug 10 BCSG DATE REMOVED 15 June/ June/2011 REVISION REMOVED INCORP. IN / BY REPLACED WITH BCSG Rev. 5 BCSG Rev. 5 MMEL Aug Aug 10 BCSG 26 Mar 14 BCSG Rev 6 MMEL Dec Dec 10 BCSG 26 Mar 14 BCSG Rev 6 MMEL Jan Jan 11 BCSG 26 Mar 14 BCSG Rev 6 MMEL Jan Jan 11 BCSG 26 Mar 14 BCSG Rev 6 MMEL Jan Jan 11 BCSG 26 Mar 14 BCSG Rev 6 MMEL Jan Jan 11 BCSG 26 Mar 14 BCSG Rev 6 MMEL Nov Nov 11 BCSG 26 Mar 14 BCSG Rev 6 MMEL Jan Jan 12 BCSG 02 May 12 BCSG TR123 MMEL Jan Jan 12 BCSG 26 Mar 14 BCSG Rev 6 MMEL Mar Mar 12 BCSG 26 Mar 14 BCSG Rev 6 MMEL May May 12 BCSG 26 Mar 14 BCSG Rev 6 MMEL May May 12 BCSG 26 Mar 14 BCSG Rev 6 MMEL Jun Jun 12 BCSG 26 Mar 14 BCSG Rev 6 MMEL Jun Jun 12 BCSG 26 Mar 14 BCSG Rev 6 MMEL Jun Jun 12 BCSG 26 Mar 14 BCSG Rev 6 MMEL Jun Jun 12 BCSG 26 Mar 14 BCSG Rev 6 MMEL Jun Jun 12 BCSG 26 Mar 14 BCSG Rev 6 MMEL Jun Jun 12 BCSG 26 Mar 14 BCSG Rev 6 MMEL Jul Jul 12 BCSG 26 Mar 14 BCSG Rev 6 MMEL Jul Jul 12 BCSG 26 Mar 14 BCSG Rev 6 BCSG: Bombardier Customer Service Group

25 Bombardier Inc. DHC 8 Series 400 TEMPORARY REVISION INDEX T.R. Index 7 REVISION TEMPORARY REVISION NO. SECTION / PAGE NO. ISSUE DATE DATE INSERTED INSERTED BY DATE REMOVED REMOVED BY INCORP. IN / REPLACED WITH MMEL Jul Jul 12 BCSG 13 May 13 BCSG TR 139 MMEL Aug Aug 12 BCSG 26 Mar 14 BCSG Rev 6 MMEL Sep Sep 12 BCSG 26 Mar 14 BCSG Rev 6 MMEL Oct Oct 12 BCSG 26 Mar 14 BCSG Rev 6 MMEL Oct Oct 12 BCSG 26 Mar 14 BCSG Rev 6 MMEL Jul Jul 12 BCSG 26 Mar 14 BCSG Rev 6 MMEL May May 13 BCSG 26 Mar 14 BCSG Rev 6 MMEL Apr Apr 14 BCSG 09 Sep 15 BCSG Rev 7 MMEL May May 14 BCSG 09 Sep 15 BCSG Rev 7 MMEL May May 14 BCSG 09 Sep 15 BCSG Rev 7 MMEL May May 14 BCSG 09 Sep 15 BCSG Rev 7 MMEL May May 14 BCSG 09 Sep 15 BCSG Rev 7 MMEL May May 14 BCSG 09 Sep 15 BCSG Rev 7 MMEL May May 14 BCSG 09 Sep 15 BCSG Rev 7 MMEL Apr Apr 15 BCSG 09 Sep 15 BCSG Rev 7 MMEL Apr May 15 BCSG 09 Sep 15 BCSG Rev 7 MMEL Apr May 15 BCSG 09 Sep 15 BCSG Rev 7 MMEL Apr May 15 BCSG 09 Sep 15 BCSG Rev 7 MMEL Apr May 15 BCSG 09 Sep 15 BCSG Rev 7 MMEL Apr May 15 BCSG 09 Sep 15 BCSG Rev 7 MMEL Apr May 15 BCSG 09 Sep 15 BCSG Rev 7 MMEL Apr May 15 BCSG 09 Sep 15 BCSG Rev 7 BCSG: Bombardier Customer Service Group

26 Bombardier Inc. DHC 8 Series 400 TEMPORARY REVISION INDEX T.R. Index 8 REVISION TEMPORARY REVISION NO. SECTION / PAGE NO. ISSUE DATE DATE INSERTED INSERTED BY DATE REMOVED REMOVED BY INCORP. IN / REPLACED WITH MMEL Apr May 15 BCSG 09 Sep 15 BCSG Rev 7 MMEL Apr May 15 BCSG 09 Sep 15 BCSG Rev 7 BCSG: Bombardier Customer Service Group

27 Bombardier Inc. DHC 8 Series 400 TEMPORARY REVISION INDEX T.R. Index 9 REVISION TEMPORARY REVISION NO. SECTION / PAGE NO. ISSUE DATE DATE INSERTED INSERTED BY DATE REMOVED REMOVED BY INCORP. IN / REPLACED WITH BCSG: Bombardier Customer Service Group

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29 Bombardier Inc. DHC 8 Series 400 TABLE OF CONTENTS 1 Rev 5 NOV 28/2011 Preamble Notes & Definitions System No. 21 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 79 1

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31 Bombardier Inc. DHC 8 Series 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 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 (2) or (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 (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,

32 2 Rev 5 NOV 28/2011 DEPARTMENT OF TRANSPORT Bombardier Inc. DHC 8 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.

33 Bombardier Inc. DHC 8 Series Rev 5 NOV 28/2011 Notes and Definitions 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.

34 2 DEPARTMENT OF TRANSPORT Bombardier Inc. DHC 8 Series 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. 1 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.

35 Bombardier Inc. DHC 8 Series 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) 2 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.

36 4 DEPARTMENT OF TRANSPORT Bombardier Inc. DHC 8 Series 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. 3 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.

37 Bombardier Inc. DHC 8 Series 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.

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39 Rev 6 Mar 26/ AIR CONDITIONING 20 1 Distribution Damper C 1 0 May be inoperative Recirculation Fan ) Pre Mod and Pre Mod or Pre Mod ) Pre Mod and Mod or Mod Flow (Pack) Control and Shutoff Valve B 1 0 May be inoperative provided: a) The Fan is switched OFF, and b) The Standby Magnetic Compass is considered inoperative. C 1 0 May be inoperative provided Fan is switched OFF. C 1 0 (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 Display Cooling Fans C 3 2 May be inoperative SIDE WINDOW DEMIST Vent Controls A 2 1 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. C 2 0 (M#) May be inoperative provided the affected side(s) is failed in the open position Low Level Vent Controls A 2 1 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. C 2 0 (M) May be inoperative provided the Low Level Vent position is confirmed and lever moved to closed position.

40 AIR CONDITIONING (CONT D) FLT COMPT GASPERS (Small and Large) Aft Baggage Compartment Vent Valves 1) Inlet and outlet vent valves 2) VENT VALVE INLT and VENT VALVE OUTLT CLOSED advisory lights CABIN PRESS Warning Light C 4 0 May be inoperative provided comfort level is acceptable to the pilot. C 2 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. C 2 0 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. C 2 0 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. C 1 0 May be inoperative provided flight is conducted at or below 10,000 feet MSL, per AFM Supplement 113, UNPRESSURIZED FLIGHT BLEED ON Cabin ALT Indicator C 1 0 (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. D 1 0 (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, UNPRESSURIZED FLIGHT BLEED ON.

41 AIR CONDITIONING (CONT D) 30 3 Cabin DIFF Pressure Indicator C 1 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. D 1 0 (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, UNPRESSURIZED FLIGHT BLEED ON Cabin RATE Indicator C 1 0 May be inoperative provided all other instruments and functions of the Pressurization System are operative. D 1 0 (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, UNPRESSURIZED FLIGHT BLEED ON Cabin Pressure Control System 1) AUTO and MAN Modes A 2 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. 2) AUTO Mode A 1 0 (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.

42 21 4 Rev 6 Mar 26/ AIR CONDITIONING (CONT D) 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 Aft Valves 1) Aft Outflow Valve C 1 0 (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 ) Aft Safety Valve C 1 0 (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 Air Cycle Machines (ACM) C 2 1 May be inoperative provided the associated PACKS switch is selected and remains OFF Turbine Shut Off Valves C 2 1 (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 Pack Bypass Valve C 2 1 (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 Aft Baggage Compartment Vent Valves Deleted. Refer to item

43 AIR CONDITIONING (CONT D) 60 1 CABIN TEMP CONTROL 1) AUTO and MAN Modes C 1 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. 2) AUTO Mode C 1 0 (M) May be inoperative provided: a) MAN control is verified operative, and b) DUCT TEMP indicator is verified operative. 3) MAN Mode C 1 0 (M) May be inoperative provided AUTO control is verified operative DUCT TEMP GAUGE C 1 0 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. 1) CABIN Temperature C 1 0 May be inoperative provided Flight Attendant Temperature Control is operative. 2) CAB DUCT Temperature C 1 0 May be inoperative provided flights are conducted in accordance with AFM supplement 85, Operation with Inoperative CAB DUCT/CABIN/FC Duct Gauge. 3) FC DUCT Temperature C 1 0 May be inoperative provided flights are conducted in accordance with AFM supplement 85, Operation with Inoperative CAB DUCT/CABIN/FC Duct Gauge 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.

44 21 6 Rev 6 Mar 26/ AIR CONDITIONING (CONT D) 2) AUTO Mode C 1 0 (M) May be inoperative provided: a) MAN control is verified operative, and b) DUCT TEMP indicator is verified operative. 3) MAN Mode C 1 0 (M) May be inoperative provided AUTO control is operative Flight Attendant Control Panel Cabin Temperature Control and CABIN TEMP indication C 0 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.

45 Rev 6 Mar 26/ AUTOMATIC FLIGHT CONTROL A/P DISENG Annunciators (Glareshield) Autopilot C 2 1 May be inoperative. C 2 0 May be inoperative provided autopilot is not used. 1) Autopilot B 1 0 Any mode functioning normally may be used ) Autopilot Pitch Trim System (AP PITCH TRIM FAIL) Tactile Control Steering (TCS) Switches Flight Guidance Control Panel (FGCP) Flight Guidance Control Panel Indicators (AP, HSI SEL only) B 1 0 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. C 2 0 May be inoperative. D 2 1 May be inoperative on the pilot not flying side. C 1 1 Individual modes of operation may be inoperative provided that heading bugs, nav source selectors and course selection functions are operative. C 4 0 May be inoperative Yaw Damper System B 1 0 (M) May be inoperative. NOTE: Autopilot will not be available A/P DIS Switches B 2 0 May be inoperative provided the Autopilot is considered inoperative and not used. C 2 1 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.

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47 COMMUNICATION *** Communication Systems Transmitters and Receivers (VHF, HF and UHF) Flitefone (or equivalent) System D 2 Any in excess of those required by regulations and not powered by an essential bus may be inoperative. D 1 0 (M) May be inoperative *** SELCAL System C 1 0 (O) May be inoperative provided alternate procedures are established and used *** Aircraft Communications Addressing and Reporting System (ACARS) D 1 0 May be inoperative provided procedures do not require its use. C 1 0 (O) May be inoperative provided alternate procedures are established and used. D 1 0 May be inoperative provided routine procedures do not require its use. ACARS Printer C 1 0 (M)(O) May be inoperative provided the printer is deactivated and secured, and alternate procedures are established and used. D 1 0 May be inoperative provided routine procedures do not require its use Alerting System (CHIME/LIGHT) 1) Passenger Configuration a) Flight Deck Call Light B 2 0 May be inoperative provided the flight deck chime is operative. b) Flight Deck EMER Light B 2 0 May be inoperative provided the flight deck chime is operative. c) Flight Deck PA Light B 2 0 May be inoperative provided the flight deck chime is operative.

48 COMMUNICATION (CONT D) d) Flight Attendant Call Light e) Flight Attendant EMER Light f) Flight Attendant PA Light B 2 0 May be inoperative provided: a) The PA system is operative, and b) Affected alert is not used for lavatory smoke detector alerting. B 2 0 May be inoperative provided: a) The PA system is operative, and b) Affected alert is not used for lavatory smoke detector alerting. B 2 0 May be inoperative provided: a) The PA system is operative, and b) Affected alert is not used for lavatory smoke detector alerting. g) Flight Attendant Chime B 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 0 May be inoperative provided the flight deck chime is operative Pre Recorded Announcement (Passenger Briefing) System C 1 0 (O) May be inoperative provided alternate procedures are established and used. All Cargo Operations D 1 0 May be inoperative provided all crew members are in the flight compartment.

49 COMMUNICATION (CONT D) 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.

50 COMMUNICATION (CONT D) 2) Non Passenger Configuration A 1 0 (O) May be inoperative for non passenger carrying operations for one flight day provided: a) Crew members are the only occupants of the aircraft, and b) Alternate procedures are established and used. 3) Cargo Configuration D 1 0 (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 B 1 1 (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. A 1 0 (O) May be inoperative for non passenger carrying operations for one flight day provided: a) Crew members are the only occupants of the aircraft, and b) Alternate procedures are established and used.

51 COMMUNICATION (CONT D) 2) Cargo Configuration Flight Deck / Cabin and Cabin / Cabin Active Noise and Vibration Suppression System Service Interphone System (Flight Compartment to Ground Crew) Boom Microphone Push To Talk (PTT) Switches D 1 0 May be inoperative provided all crew members are on the flight deck. D 1 0 (M) May be inoperative. NOTE: Aircraft may be dispatched with system operative in the DEGRADED mode with ANVS SYS DEGRADED lamp illuminated on the Maintenance Panel. C 1 0 May be inoperative provided alternate procedures are established and used. D 1 0 May be inoperative provided procedures are not dependent on its use. C 4 2 (M) May be inoperative provided one switch at each pilot s position is verified operative Headsets D 2 One required at each pilot s station Flight Compartment Speakers Boom Microphones (incl. Headset mics) Cockpit Handheld Microphones C 2 0 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. A May be inoperative provided: a) The Flight Data Recorder (FDR) operates normally, and b) Repairs are made within three flight days. C 2 0 May be inoperative provided associated boom microphones are operative.

52 COMMUNICATION (CONT D) 50 6 Cabin Handsets B 2 1 (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 Observer s Audio Control Panel B 1 0 May be inoperative except when required by a person in an official capacity. D 1 0 May be inoperative provided the seat is not required to be available in an official capacity for extended periods of time Static Dischargers D May be missing provided no more than one is missing from each control surface cluster Cockpit Voice Recorder A 1 0 May be inoperative provided: a) The Flight Data Recorder is operative, and b) Repairs are made within three flight days ARCDU Radio Tuning Function (Aircraft with at least one FMS installed) C 2 1 (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.

53 Rev 6 Mar 26/ ELECTRICAL POWER 20 1 AC GEN 1 and AC GEN 2 VOLT Indications (on ESID) 20 2 AC GEN 1 and AC GEN 2 LOAD Indications (on ESID) C 6 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. C 6 0 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 #1 AC GEN and #2 AC GEN Caution Lights Transformer Rectifier Units (TRUs) DC Generator Control Unit Start / Termination Function BATT C Temperature Indications C 2 1 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. B 2 1 (M) May be inoperative provided: a) Both DC Starter/Generators are operative, and b) Associated TRU is deactivated. B 2 0 (O) May be inoperative provided the start is manually terminated at 50% NH. C 3 0 (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 *** APU Generation System D 1 0 (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. D 1 0 May be inoperative provided the APU is considered inoperative and is not used.

54 24 2 Rev 6 Mar 26/ ELECTRICAL POWER (CONT D) 30 5 DC GEN LOAD Indications C 2 1 (O) May be inoperative provided both DC Generators are operative. C 2 1 (O) May be inoperative provided the inoperative Indication is associated with a failed DC Generator DC Starter/Generation Systems B 2 1 (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 AC External Power System D 1 0 May be inoperative DC External Power System D 1 0 May be inoperative.

55 Rev 6 Mar 26/ EQUIPMENT AND FURNISHINGS Forward Observer Seat (including associated equipment) Pilot s Seat Adjustments 1) Vertical Mode Adjustment B 1 0 (M) May be inoperative provided the seat is removed, stowed, or secured in the retracted position. D 1 0 (M) May be inoperative provided: a) The seat is not required to be occupied in an official capacity for extended periods of time, and b) The seat is removed, stowed, or secured in the retracted position. C 2 0 (M#) Vertical adjustment may be inoperative provided the seat is secured in a position, which meets individual pilot requirements. 2) Fore/Aft Mode B 2 0 (M#) Fore/aft adjustment may be inoperative provided the seat is secured in a position, which meets individual pilot requirements. 3) Crew Armrests C 4 0 (M#) May be inoperative provided the armrest(s) is (are) removed from the seat. 4) Lumber Support C 2 0 May be inoperative in the lowest position provided the seat is acceptable to the affected crew member. 5) Lumbar Support Padding D May be worn or damaged if acceptable to the affected crew member. 6) Recline Mechanism B 0 (M#) May be inoperative provided backrest is secured in a position acceptable to the affected crew member *** Pilot s Seat Heaters D 2 1 (M#) May be inoperative provided the affected Heater is deactivated. D 2 0 (M) May be inoperative provided the Heaters are deactivated.

56 EQUIPMENT AND FURNISHINGS (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: 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.

57 25 3 2) Non Essential Equipment and Furnishings (NEF) 25 EQUIPMENT AND FURNISHINGS (CONT D) 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: Exterior lavatory door ash trays are not considered NEF items. 2. Items addressed elsewhere in the MMEL document cannot be considered for NEF relief.

58 EQUIPMENT AND FURNISHINGS (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: 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.

59 EQUIPMENT AND FURNISHINGS (CONT D) C (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: 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 Megaphones D (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. All Cargo Operations D 0 May be inoperative provided all crew members are in the flight compartment.

60 EQUIPMENT AND FURNISHINGS (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: 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.

61 EQUIPMENT AND FURNISHINGS (CONT D) 2) Excess Equipment *** 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: 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 Passenger Seats D (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: 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). 1) Recline Mechanism *** D (M) May be inoperative and seat occupied provided the seat is secured in the full upright position.

62 EQUIPMENT AND FURNISHINGS (CONT D) *** ) Armrest with Recline Mechanism *** 3) Armrest without Recline Mechanism *** 4) Tray table in the unstowed position *** Fasten Seat Belt While Seated and No Smoking Signs or Placards Lavatory NO SMOKING Placard Flight Attendant s Seat Heaters Flight Attendant Reading Light D (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. D (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. D (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. C One or more signs or placards may be illegible or missing provided a legible sign or placard is readable from each occupied passenger seat. B May be missing provided the lavatory smoke detection system is operative. D 2 1 (M#) May be inoperative provided the affected heater is deactivated. D 2 0 (M) May be inoperative provided Heaters are deactivated. C 0 (O) May be inoperative provided a suitable alternate light source is available.

63 EQUIPMENT AND FURNISHINGS (CONT D) Passenger Service Unit (PSU) Galley Waste Compartment 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. C (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. 1) Door 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. 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 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.

64 EQUIPMENT AND FURNISHINGS (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: Repair interval extensions are not permitted. 2. Interior lavatory ashtrays are considered under passenger convenience items/nef and are not required by regulations.

65 EQUIPMENT AND FURNISHINGS (CONT D) Aircraft with only one exterior lavatory door or entry area ashtray installed B 1 0 May be missing. NOTE: Repair interval extensions are not permitted. 2. Interior lavatory ashtrays are considered under passenger convenience items/nef and are not required by regulations *** Aft Baggage Divider Nets D (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.

66 EQUIPMENT AND FURNISHINGS (CONT D) Aft Baggage Door Threshold Net Cargo Compartment Liners and Floor Panels (Applicable to Forward and/or Aft Baggage Compartments) D 1 1 (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. C 1 0 (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. C (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.

67 EQUIPMENT AND FURNISHINGS (CONT D) 60 1 Emergency Locator Transmitter (ELT) Fixed ELT A (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. A (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. D (M) Any in excess of those required by regulations may be inoperative provided the system is deactivated and or removed. Survival Type ELTs *** D Any in excess of those required by regulations may be inoperative or missing First Aid Kit D (O) Any kit or items contained in the kit in excess of those required by regulations may be incomplete or missing provided: a) Required distribution is maintained, and b) Procedures are established to alert crew members of missing or incomplete Kits.

68 EQUIPMENT AND FURNISHINGS (CONT D) First Aid Kit Seal B 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) *** Emergency Medical Kit D (O) Any kit or items contained in the kit in excess of those required by regulations may be incomplete or missing provided procedures are established and used to alert crew members of missing or incomplete kits. A 0 (O) May be incomplete or missing provided: a) The kit is sealed in a manner that will identify it as a unit that cannot be mistaken for a fully serviceable unit, and b) Replacements are made in one flight. Emergency Medical Kit Seal *** B (O) The seal affixed on the exterior of the emergency medical kit may be missing or broken provided: a) The emergency medical kit is fully equipped, b) The kit includes a list of its contents, c) An inventory is taken on the content of the kit prior to departure, and d) Procedures are established and used to alert crew members of: The missing or broken seal, and 2. The need to perform an inventory under proviso c) 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.

69 EQUIPMENT AND FURNISHINGS (CONT D) 2) Flashlight Holders C 0 (M)(O) May be inoperative or missing provided alternate stowage provisions are provided Airstair Door Ditching Dam C 1 0 (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 *** Flight Deck Sun Visors C May be inoperative provided affected sun visor does not obstruct either pilot s field of view for take off and landing. C (M#) May be inoperative provided affected Sun Visor is removed Flight Deck Flashlights/Flashlight Holders 1) Flashlights C 2 0 (O) May be inoperative or missing provided that a flashlight of equivalent characteristics is readily available. 2) Flashlight Holders C 2 0 (M)(O) May be inoperative or missing provided alternate stowage provisions are provided 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.

70 EQUIPMENT AND FURNISHINGS (CONT D) 2) Passenger Life Vests *** C (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 *** Cabin Video Monitoring and Surveillance System C (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. C 1 0 (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. D 1 0 May be inoperative provided procedures do not require its use. Video Converter D 2 1 One may be inoperative provided operative video converter is connected to an operative FMS.

71 Rev 6 Mar 26/ FIRE PROTECTION 10 1 Lavatory Smoke Detection System 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. C 0 (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: The above mentioned provisos are not intended to preclude crew member lavatory inspections which must be detailed in the (O) procedures.

72 FIRE PROTECTION (CONT D) 1) Non passenger Carrying Operations B 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: The above mentioned provisos are not intended to preclude crew member lavatory inspections which must be detailed in the (O) procedures. B 0 (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: The above mentioned provisos are not intended to preclude crew member lavatory inspections which must be detailed in the (O) procedures.

73 FIRE PROTECTION (CONT D) 2) All Cargo Operations C 1 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: The above mentioned provisos are not intended to preclude crew member lavatory inspections which must be detailed in the (O) procedures. C 1 0 (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: The above mentioned provisos are not intended to preclude crew member lavatory inspections which must be detailed in the (O) procedures.

74 FIRE PROTECTION (CONT D) D 1 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: The above mentioned provisos are not intended to preclude crew member lavatory inspections which must be detailed in the (O) procedures. D 1 0 (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: The above mentioned provisos are not intended to preclude crew member lavatory inspections which must be detailed in the (O) procedures.

75 FIRE PROTECTION (CONT D) Aft Baggage Compartment Smoke Detectors Forward Baggage Compartment Smoke Detector C 2 1 (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. C 2 0 (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. C 1 0 (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 *** APU Fire Detection System D 1 0 (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 *** APU Fire Extinguishing System D 1 0 (M#) May be inoperative provided the APU is considered inoperative and is not used.

76 FIRE PROTECTION (CONT D) 20 2 Lavatory Fire Extinguishing System Non passenger Carrying Operations C 0 (M)(O) For each lavatory the lavatory fire extinguishing system may be inoperative provided the lavatory smoke detection system is operative. C 0 (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. B 0 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. All Cargo Operations C 1 0 (O) May be inoperative provided crew members have been briefed that the Lavatory Fire Extinguishing System is inoperative. D 1 0 (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: The above mentioned provisos are not intended to preclude crew member lavatory inspections which must be detailed in the (O) procedures.

77 FIRE PROTECTION (CONT D) 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 Baggage Compartment Fire Extinguishers 1) Low Rate Discharge Bottle (LRD) 2) High Rate Discharge Bottle (HRD) C 1 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. C 0 (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.

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79 Rev 6 Mar 26/ FLIGHT CONTROLS 10 1 AIL TRIM Indicator C 1 0 (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 RUDDER TRIM Indicator C 1 0 (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 Rudder Pedal Adjustment C 2 0 (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 Flap Auto Pitch Trim (AUTO TRIM FAIL) C 1 0 (O) May be inoperative provided: a) Flap angles are limited to 15 degrees or less, and b) Manual pitch trim is operative Stick Shaker A 2 1 (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.

80 FLIGHT CONTROLS (CONT D) 30 3 #1 STALL SYSTEM FAIL, #2 STALL SYSTEM FAIL, Caution Light(s) Eligible failure annunciations as determined through Centralized Diagnostic system interrogation: 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: 1) FLAP DISCREPANCY (O) a) Use of flaps limited to maximum 15 or less, and b) Aircraft is not dispatched into known or forecast icing conditions. 2) ADU 1 or ADU 2 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 ) AHRS 1 or AHRS 2 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 ) NO DATA FROM FADEC 1" or NO DATA FROM FADEC 2 May be inoperative.

81 FLIGHT CONTROLS (CONT D) 5) STICK SHAKER Dispatch is also to consider provisos of MMEL Item Stall Warning System A 2 1 (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 Stick Pusher System A 1 0 (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 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.

82 27 4 Rev 6 Mar 26/ FLIGHT CONTROLS (CONT D) ) ROLL SPLR OUTBD GND FLIGHT/TAXI Switch TAXI Position Latch Spoiler Advisory Lights 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. C 1 0 (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. 1) ROLL INBD C 1 0 (O) May be inoperative provided all PFCS SPOILER indications on the MFD are operative and are periodically monitored. 2) ROLL OUTBD C 1 0 (O) May be inoperative provided all PFCS SPOILER indications on the MFD are operative and are periodically monitored Roll Spoilers (Ground Mode System) C 2 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.

83 FUEL 20 1 Pressure Refueling System 1) REFUEL C 1 0 (M) May be inoperative provided the fuel transfer system is verified operative. 2) PRESELECT REFUEL C 1 0 (M) May be inoperative provided the fuel transfer system is verified operative ) REFUEL AND PRESELECT REFUEL MASTER VALVE CLOSED Light (Refuel/Defuel Panel) Height Measuring Unit (Magnetic Dipsticks) Fuel TANK C Temperature Indication (on ESID) C 1 0 (M) May be inoperative provided: a) Fuel transfer system is verified operative, and b) Procedures are established and used for gravity refueling. C 1 0 (M) May be inoperative provided the REFUEL/DEFUEL SHUT OFF VALVE is verified closed following refueling. C 2 0 May be inoperative provided the fuel quantity is determined by other approved means. C 1 0 May be inoperative. NOTE: If using JET B / JP 4 fuel, the maximum operating altitude should not exceed 20,000 feet FUELING ON Caution Light C 1 0 (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 TANK 1 AUX PUMP and TANK 2 AUX PUMP Advisory Lights C 2 1 (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.

84 FUEL (CONT D) *** #1 TANK FUEL LOW and #2 TANK FUEL LOW Caution Lights Refuel/Defuel/Transfer VALVE (OPEN/CLOSED) Advisory Lights External Refuel/Defuel Panel FUEL QTY Indicators REFUEL SHUTOFF TANK 1 and REFUEL SHUTOFF TANK 2 Advisory Lights APU FUEL VALVE Advisory Light C 2 1 (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. C 2 1 (M) May be inoperative provided the fuel transfer system and flight compartment FUEL QTY Indications are verified operative. C 2 0 (M) May be inoperative provided the fuel quantity is determined by other approved means prior to each flight. C 2 0 (M) May be inoperative provided the flight compartment FUEL QTY Indications are verified operative. 1) (OPEN) C 1 0 (M) May be inoperative provided: a) The OPEN light is extinguished, and b) The CLOSED light is illuminated when the APU is selected OFF. 2) (CLOSED) D 1 0 (M) May be inoperative provided: a) APU is not operated, and b) The APU fuel shut off valve is verified closed Flight Compartment Fuel QTY Indications (on ESID) Fuel Inlet Temperature Indications (on Engine Display) C 2 1 (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. A 2 1 (O) May be inoperative for one flight provided the TANK AUX PUMP Advisory Lights are operative.

85 HYDRAULIC POWER Parking/Emergency Brake Accumulator Hand Pump HYD FSOV OPEN Indicator Light HYD PRESS 1 and HYD PRESS 2 Indications HYD PRESS STBY Indication System #1 and #2 Nacelle Reservoir Quantity Indicators #1 STBY HYD PUMP HOT Caution Light C 1 0 May be inoperative provided accumulator pressure is verified prior to engine start. C 2 1 (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. C 2 1 (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. C 1 0 (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. C 2 0 (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. A 1 0 May be inoperative provided: a) STBY HYD PRESS Indication is operative, and b) Repairs are made within one flight day HYD QTY 3 Indication C 1 0 (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 System #3 Aft Fuselage Hydraulic Quantity Indicator C 1 0 May be inoperative provided HYD QTY 3 Indication is operative.

86 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 PTU CNTRL ON Advisory Light 1) Pre Modsum or 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 or a) PTU CNTRL ON Advisory Light (White) b) PTU CNTRL FAIL Advisory Light (Amber) c) PTU CNTRL pressure Green Cross Hatch Advisory Light (Green) 30 9 #1 ENG HYD PUMP and #2 ENG HYD PUMP Caution Lights C 1 0 May be inoperative provided Pressure Green Cross Hatch Advisory Light is operative. C 1 0 May be inoperative provided Pressure Green Cross Hatch Advisory Light is operative. 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. C 2 1 (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.

87 Rev 6 Mar 26/ HYDRAULIC POWER (CONT D) HYD QTY 1 and HYD QTY 2 Indications STBY HYD PRESS ON Advisory Light C 2 1 (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. C 1 0 (O) May be inoperative provided the HYD PRESS STBY indication is verified operative #1 HYD FLUID HOT and #2 HYD FLUID HOT Caution Lights B 2 1 (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 HYD #3 ISOL VLV OPEN Advisory Light C 1 0 (O) May be inoperative provided: a) The HYD PRESS 3 indication is operative, and b) The ELEVATOR PRESS caution light is operative.

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89 Rev 6 Mar 26/ ICE AND RAIN PROTECTION TAIL De Ice Boots Advisory Lights DEICE PRESS Caution Light C 4 0 May be inoperative provided the flight is not conducted in known or forecast icing conditions. C 1 0 May be inoperative provided the flight is not conducted in known or forecast icing conditions. C 1 0 (M) May be inoperative provided: a) All De Ice Boot Advisory Lights are verified operative, and b) The DEICE PRESS Indicators are verified operative DEICE PRESS Indicators C 2 0 May be inoperative provided the flight is not conducted in known or forecast icing conditions. C 2 0 (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 Low Pressure Warning Switches (LPWS) WING De Ice Boots Advisory Lights C 2 1 (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. C 2 0 May be inoperative provided flight is not conducted in known or forecast icing conditions. C 8 2 (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.

90 ICE AND RAIN PROTECTION (CONT D) 10 6 Timer Monitor Unit (TMU, Timer Function) C 1 0 (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 Airframe De Icing System C 1 0 May be inoperative provided the flight is not conducted in known or forecast icing conditions Engine Intake Bypass Door OPN and CLOSED Advisory Lights ENGINE INTAKE HTR Advisory Lights ENG ADPT HEAT 1 and ENG ADPT HEAT 2 Caution Lights C 2 0 (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. C 2 0 May be inoperative provided: a) Associated bypass door(s) remains closed, and b) Flight is not conducted in known or forecast icing conditions. C 2 0 (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. C 2 1 May be inoperative provided the flight is not conducted in known or forecast icing conditions. C 2 1 (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.

91 ICE AND RAIN PROTECTION (CONT D) 20 4 Engine Intake Adapter Heater Assemblies C 2 1 May be inoperative provided the flight is not conducted in known or forecast icing conditions Pitot/Static Heaters B 3 2 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 PITOT HEAT 1, PITOT HEAT 2 and PITOT HEAT STBY Caution Lights B 3 0 (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 Windshield Wipers C 2 0 May be inoperative provided the flight is not conducted in precipitation within five nautical miles of the airport of take off or intended landing Windshield Heaters A 3 1 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. Co Pilot Heated Windshield (Right Hand Windshield) A 1 0 (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 Propeller De icing System C 1 0 May be inoperative provided flight is not conducted in known or forecast icing conditions PROPS Heat Advisory Lights B 2 0 (O) May be inoperative provided: a) AC LOAD indication is operating and periodically monitored, and b) the PROP DEICE caution light is operative. C 2 0 May be inoperative provided flight is not conducted in known or forecast icing conditions.

92 ICE AND RAIN PROTECTION (CONT D) Ice Detector Spigot Illumination Lights Ice Detector Probes (Electronic) C 2 1 One may be inoperative at either the pilot s or co pilot s position. C 2 0 May be inoperative for day operations. A 2 0 (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. A 2 1 (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.

93 Rev 6 Mar 26/ INDICATING AND RECORDING SYSTEMS 20 1 Clocks 1) Pilot Clock A 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. 2) Co pilot Clock C 1 0 May be inoperative Flight Data Recorder A 1 0 (M) May be inoperative provided: a) The Cockpit Voice Recorder is operative, and b) Repairs are made within three flight days *** ) DFDR Recording Parameters required by Regulation 2) DFDR Recording Parameters not required by Regulation Extended Quick Access Recorder 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 (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. A (M#) May be inoperative provided repairs are made before completion of the next heavy maintenance check. D 0 (M) May be inoperative. C 2 1 One may be inoperative. C 2 1 One may be inoperative.

94 INDICATING AND RECORDING SYSTEMS (CONT D) 60 1 ESID Control Panel 1) System 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.

95 INDICATING AND RECORDING SYSTEMS (CONT D) 2) ALL Switch C 1 0 (O) The ALL Switch may be inoperative provided the ELEC SYS, FUEL SYS, ENG SYS and DOORS SYS Switches are operative. 3) Engine Display Dimming Function C 1 0 Dimming may be inoperative provided the display intensity is adequate MFD and PFD Engine Display Messages ) PFD 1 / 2 LINK FAIL Engine Display message 2) MFD 1 / 2 LINK FAIL Engine Display message Electronic Flight Instrument System Control Panels C 2 1 Message may be displayed. C 2 1 Message may be displayed. C 2 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. Bright/Dim Controls C 6 0 Dimming may be inoperative provided the display intensity is adequate FADEC 1 / DU or FADEC 2 / DU Engine Display Message A 2 1 Message may be annunciated for three flight days EFIS/ESID Display Units 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.

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97 Rev 6 Mar 26/ LANDING GEAR 20 1 *** NOSE GEAR LOCK Advisory Light D 1 0 May be inoperative provided Nose Gear Lock is verified disengaged prior to each departure Landing Gear Retraction System Parking Brake Pressure Indications 1) HYD PRESS PK BRK Indication 2) Aft Wing Root Fairing Indicator A 1 0 (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. C 1 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. C 1 0 (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 Anti Skid System C 1 0 (O) May be inoperative provided operations are conducted in compliance with AFM Supplement 7 OPERATION WITH INOPERATIVE ANTI SKID BRAKE CONTROL SYSTEM *** Fill Valve Gauge (CR ) D 6 0 Gauge may be inoperative.

98 LANDING GEAR (CONT D) 50 1 Nosewheel Steering A 1 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 Touched Runway Indicating System C 1 0 (M) May be inoperative provided prior to each flight, it is confirmed that the frangible switch has not been contacted.

99 LIGHTS Cockpit and Instrument Panel Lighting System Caution/Warning/Advisory Lights System DIM/BRT Function C 1 1 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. D 1 0 May be inoperative for daylight operations. Dimming Function C 1 0 (M) May be inoperative for day operations. Brighten Function C 1 0 (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 Caution/Warning/Advisory Lights System 1) Caution/Warning Panel LEDs C May be inoperative provided one half of each light is operative. 2) Advisory Lights C (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.

100 33 2 Rev 6 Mar 26/ LIGHTS (CONT D) 20 1 No Smoking / Fasten Seat Belt Lights 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. C (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. A (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. Aural Tone Function C (O) May be inoperative provided alternate procedures are established and used. Automatic Function C (O) May be inoperative provided: a) Manual control function is operative, and b) Alternate procedures are established and used. All Cargo Operations D May be inoperative provided all crew members are in the flight compartment Cabin Lighting System 1) Sidewall Lighting Classic Interior C May be inoperative.

101 Rev 6 Mar 26/ LIGHTS (CONT D) Classic Interior 3 Abreast Layout NextGen Interior (CR825CH02598) NextGen Interior 3 Abreast Layout 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. C (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. C (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.

102 33 4 Rev 6 Mar 26/ LIGHTS (CONT D) Classic Interior 3 Abreast Layout NextGen Interior (CR825CH02598) NextGen Interior 3 Abreast Layout C (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. C (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. C (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. 3) All Cargo Operations D May be inoperative provided cabin lighting is sufficient to inspect cargo and to perform fire fighting duties.

103 LIGHTS (CONT D) 20 3 Lavatory Compartment (RETURN TO SEAT and Lavatory OCCUPIED Light) 1) RETURN TO SEAT Light C 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. C 0 (M) Lavatory compartment shall not be occupied and must be blocked and placarded DO NOT OCCUPY 2) Toilet OCCUPIED Light C 0 May be inoperative Accent Lights (Spotlights) NextGen Interior D 30 0 May be inoperative. NOTE: This relief is not intended for Emergency Flood Lights within the Accent Light Assemblies Lavatory Light C 0 Full illumination mode may be inoperative provided the dimmed mode is functional at all times. C 0 (M) May be inoperative provided lavatory door is locked closed and placarded, INOPERATIVE DO NOT ENTER Aft Baggage Compartment Ceiling Lights C 2 0 May be inoperative provided alternate lighting is available. D 2 0 May be inoperative for day operations.

104 LIGHTS (CONT D) 30 2 Forward Baggage Compartment Light C 1 0 May be inoperative provided alternate lighting is available. NOTE: Only applicable if Forward Baggage Compartment is installed. D 1 0 May be inoperative for day operations. NOTE: Only applicable if Forward Baggage Compartment is installed *** Aft Service Light D 1 0 (M) May be inoperative provided the light is deactivated Position Lights C 6 3 One bulb at each position (wing tip and aft) may be inoperative. C 6 0 May be inoperative for daylight operations A/COL WHITE Lights C As required by regulations. C 2 0 May be inoperative for daylight operations. NOTE: The A/COL switch must be operated as if the lights were operating normally *** Logo Lights D 2 0 May be inoperative A/COL RED Light (Red Recognition Light) C 1 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.

105 LIGHTS (CONT D) 40 5 Boarding Lights 1) Passenger Configuration C 2 0 May be inoperative provided Cabin Overhead Lighting or alternate means is used. C 2 0 May be inoperative for day operations. C 2 0 May be inoperative provided aircraft crew are the only occupants of the aircraft. 2) All Cargo Operations D 2 0 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 Passenger Airstair Door Lights 1) Passenger Configuration C 4 2 May be inoperative provided they are not adjacent. C 4 0 May be inoperative provided acceptable alternate lighting is used to board and deplane passengers. C 4 0 May be inoperative for day operations. C 4 0 May be inoperative provided the aircraft crew are the only occupants of the aircraft. 2) All Cargo Operations D 4 0 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.

106 LIGHTS (CONT D) 40 7 Landing Lights C 4 2 One inboard and/or one outboard light may be inoperative for night operations provided steep approach landings are not conducted. D 4 0 May be inoperative for day operations Taxi Light C 1 0 May be inoperative provided Landing Lights are operative. D 1 0 May be inoperative for day operations WING INSP Lights A 4 2 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. C 4 0 One or more may be inoperative provided the flight is not conducted in known or forecast icing conditions at night. C 4 0 May be inoperative for day operations Exterior Emergency Lighting System Interior Electrical Emergency Lighting System Relief limited to installation defined by Bombardier AEROC 84.6.E.1 Sect. 5 A 1 0 (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. C 1 0 May be inoperative for daylight operations. 1) Ceiling Lights C 1 1 Individual light bulbs, etc. may be inoperative provided no two adjacent overhead emergency lights are inoperative.

107 LIGHTS (CONT D) 2) EXIT Identifiers C 4 4 Two bulbs from five may be inoperative on each identifier. 3) Emerg. Markers, Emerg. Locators C 7 7 Two bulbs from five may be inoperative on each marker/locator given that inoperative bulbs are not adjacent. NextGen Interior (CR825CH02598) Relief limited to installation defined by Bombardier AEROC 84.6.E.1, Sect ) Ceiling Emergency Flood Lights C 7 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= is operative. 2) Exit Identifiers C 4 4 Each exit identifier may have 40% of its internal lights inoperative. NextGen Interior (Dual Class) Relief limited to installation defined by Bombardier AEROC 84.6.E.1, Sect and AEROC 84.6.E.1, Sect

108 LIGHTS (CONT D) 1) Ceiling Emergency Flood Lights C 7 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= and X= are operative. 2) Exit Identifiers C 4 4 Each exit identifier may have 40% of the internal lights inoperative 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 1 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 5 meters (60 in.) on the same strip. All Cargo Operations D 1 0 (O) May be inoperative.

109 Rev 6 Mar 26/ NAVIGATION 10 1 Altitude Alerting System A 1 0 (O) May be inoperative provided: a) Autopilot with ALT hold is verified operative, and b) Repairs are made within three flight days Standby Magnetic Compass B 1 0 May be inoperative provided any combination of three gyro (or INS (IRU)) stabilized compass systems are operative. B 1 0 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. C 1 0 (O) May be inoperative for flights that are entirely within areas of magnetic unreliability provided at least two stabilized directional gyro systems are installed, are operative, and if necessary, used in conjunction with approved free gyro navigation techniques Standby Attitude Indicator B 1 0 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 IVSI Indications (on PFDs) C 2 1 May be inoperative for day VMC AHRS Control Panel Indicators May be inoperative provided switching function is operative for each Indicator. 1) DG Indicators C 2 1 May be inoperative. 2) ALIGN Indicators C 2 1 May be inoperative. 3) SLAVE Indicators C 2 1 May be inoperative. 4) BASIC Indicators C 2 1 May be inoperative.

110 NAVIGATION (CONT D) 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 Integrated Standby Instrument (CR839CH00013) 1) Attitude / Slip Skid Function B 1 0 May be inoperative for day VMC. 2) STD (Standard) Button C 1 0 May be inoperative *** 30 1 *** Inertial Reference System (IRS) Microwave Landing Systems (MLS) C 1 0 Except where required by operations, may be inoperative provided alternate procedures are established and used. D 1 0 May be inoperative provided procedures do not require its use. If used routinely C 0 May be inoperative provided alternate procedures are established and used. If not used routinely D 0 May be inoperative provided routine procedures do not require its use Weather Radar System D 1 0 As required by regulations Traffic Alert and Collision Avoidance System (TCAS) 1) Traffic Alert and Collision Avoidance System (TCAS) B 1 0 (M) May be inoperative provided the system is deactivated and secured.

111 NAVIGATION (CONT D) 2) Combined Traffic Alert (TA) and Resolution Advisory (RA) Dual Displays C 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. 3) RA Display System(s) C 2 1 (O) May be inoperative on the non flying pilot side. C 2 0 (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. 4) TA Display System(s) C 0 May be inoperative provided all installed RA display and audio functions are operative RA Height Indications (on PFDs) Ground Proximity Warning System (GPWS) / Enhanced Ground Proximity Warning System (EGPWS) (CR831CH00064) B 2 0 (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. C 2 1 (O) May be inoperative provided approach minimums and operating procedures are not dependent on its use. If Required by Regulation A 1 0 (O) May be inoperative provided: a) Alternate procedures are established and used, and b) Repairs are made within three flight days. a) Modes 1 to 4 A 1 0 (O) May be inoperative provided: a) Alternate procedures are established and used, and b) Repairs are made within three flight days.

112 NAVIGATION (CONT D) b) Test Mode A 1 0 May be inoperative provided: a) The GPWS/EGPWS is considered inoperative, and b) Repairs are made within three flight days. c) Flap Over ride Function A 1 0 May be inoperative provided: a) The GPWS/EGPWS flap aural warning is operative, and b) Repairs are made within three flight days d) Glideslope Deviation (Mode 5) e) Minimums Alert (Mode 6) *** f) TAWS Enhanced Mode (CR831CH00064) If Not Required by Regulation GPWS I/F FAIL Engine Display Message B 2 0 May be inoperative. C 1 0 (O) May be inoperative provided alternate procedures are established and used. C 1 0 May be inoperative. D 1 0 May be inoperative. B 1 0 (M) Message may be displayed provided GPWS is considered inoperative.

113 NAVIGATION (CONT D) 40 6 Radio Altimeters A 2 0 (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. C 2 1 (M) One may be inoperative ATC Transponder / Altitude Reporting System 1) ATC Transponders C 2 (O) As required by regulations. D 2 0 May be inoperative, if not required by regulations. 2) ATC Identifier Switch (on hand wheels) C 2 1 May be inoperative. C 2 0 May be inoperative provided one ATC ID button (on ARCDU1 or ARCDU2) is operative.

114 NAVIGATION (CONT D) 3) ATC ID Button (on ARCDU1 or ARCDU2) C 2 1 May be inoperative. C 2 0 May be inoperative provided one ATC Identifier Switch (on hand wheels) is operative. 4) ADS B Squitter Transmissions A 2 0 May be inoperative provided: a) Operations do not require its use, and b) Repairs are made prior to completion of the next heavy maintenance visit. C 2 0 (O) May be inoperative provided alternate procedures are established and used. NOTE: Any ADS B Out function that operates normally may be used VHF Navigation Systems C 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 Distance Measuring Equipment (DME) 1) DME HOLD function A 2 0 (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. C 2 1 May be inoperative provided associated DME is operative. 2) DME System D Any in excess of those required by regulation may be inoperative Automatic Direction Finding (ADF) Systems Marker Beacon D Any in excess of those required by regulations may be inoperative. If used routinely C 2 0 May be inoperative provided alternate procedures are established and used.

115 NAVIGATION (CONT D) If not used routinely D 2 0 May be inoperative provided routine procedures do not require its use *** Global Positioning System (GPS) If used routinely C 0 (O) Except where required by operations, may be inoperative provided alternate procedures are established and used. NOTE: TAWS enhanced mode is considered inoperative (if installed), and 2. ATC ADS B function is considered inoperative (if installed). C 1 Where required by operations, one GPS must be operative. NOTE: This relief is applicable for aircraft with: TAWS Enhanced Mode (CR831CH00064) installed and required by regulation, and/or 2. ATC ADS B function installed and required by regulation.

116 NAVIGATION (CONT D) If not used routinely D 0 May be inoperative provided procedures and operations do not require its use. NOTE: TAWS enhanced mode is considered inoperative (if installed), and 2. ATC ADS B function is considered inoperative (if installed). D 1 May be inoperative provided procedures and operations do not require its use. NOTE: This relief is applicable for aircraft with: TAWS Enhanced Mode (CR831CH00064) installed and required by regulation, and/or 2. ATC ADS B function installed and required by regulation Flight Directors C 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.

117 NAVIGATION (CONT D) 60 2 *** Flight Management System (FMS) If used routinely C 0 (O) Except where required by operations, may be inoperative provided alternate procedures are established and used. NOTE: TAWS enhanced mode is considered inoperative (if installed), and 2. ATC ADS B function is considered inoperative (if installed). C 1 Where required by operations, one FMS must be operative. NOTE: This relief is applicable for aircraft with: TAWS Enhanced Mode (CR831CH00064) installed and required by regulation, and/or 2. ATC ADS B function installed and required by regulation.

118 NAVIGATION (CONT D) If not used routinely D 0 May be inoperative provided procedures and operations do not require its use. NOTE: TAWS enhanced mode is considered inoperative (if installed), and 2. ATC ADS B function is considered inoperative (if installed). D 1 May be inoperative provided procedures and operations do not require its use. NOTE: This relief is applicable for aircraft with: TAWS Enhanced Mode (CR831CH00064) installed and required by regulation, and/or 2. ATC ADS B function installed and required by regulation.

119 NAVIGATION (CONT D) FMS Database C 0 (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. SBAS (Satelight Based Augmentation System ) Level of Service (LOS) Annunciator C 1 En route/approach navigation is conducted using a current (up to date) FMS database. 1) LPV LOS Light C 1 May be inoperative provided that the LPV approach must be conducted from the side with the functioning LPV Light. C 0 May be inoperative provided LPV approaches are not conducted. 2) LNAV LOS Light C 0 May be inoperative. 3) LAV/VNAV LOS Light C 0 May be inoperative.

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121 Rev 6 Mar 26/ OXYGEN *** Flight Deck Fixed Oxygen System OXYGEN Pressure Gauges Flight Deck Fixed Oxygen System Overboard Discharge Indicator PASSENGER OXYGEN SYSTEM 1) Entire Automatic Presentation Passenger Oxygen System (APPOS) C 2 1 (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. C 1 0 (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. B 1 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. 2) Automatic Deployment B 1 0 (M) May be inoperative provided the manual deployment system is operative. 3) Passenger Service Units (PSUs) 4) Lavatory Passenger Service Unit (PSU) D (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. C 1 0 (O) May be inoperative provided lavatory is inspected by FA in case of depressurization.

122 35 2 Rev 6 Mar 26/ OXYGEN (CONT D) ) Automatic Opening Feature of Door Latches Protective Breathing Equipment (PBE) B (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. D (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 First Aid Oxygen System D 2 (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.

123 OXYGEN (CONT D) *** Portable Oxygen Dispensing Units Dual Purpose Oxygen System Units 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. C (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.

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125 Rev 6 Mar 26/ PNEUMATICS 10 1 BLEED SYSTEMS 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. B 2 1 (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.

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127 WATER/WASTE 10 1 *** Potable Water Systems C 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 *** Warm Water Wash System (Not applicable to systems Deactivated as per Bombardier Modsum) C 0 (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. C 0 (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. C 0 (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.

128 38 2 Rev 6 Mar 26/ WATER/WASTE (CONT D) Drain Mast Heater C 1 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 Lavatory Waste System C (M) Individual components may be inoperative provided: a) Associated components are deactivated or isolated, and b) Associated system components are verified not to have leaks. NOTE: Any portion of system which operates normally may be used. C (M)(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.

129 Rev 6 Mar 26/ CENTRAL MAINTENANCE SYSTEM 45 1 Centralized Diagnostic System (CDS) (incl. Maintenance Interlock Switch in Wardrobe) C 1 0 May be inoperative.

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131 Rev 6 Mar 26/ AUXILIARY POWER UNIT 00 1 *** 50 1 *** Auxiliary Power Unit (APU) D 1 0 (M) May be inoperative provided APU Airframe Fuel Shutoff Valve is verified closed. APU Bleed Air System D 1 0 (M#) May be inoperative provided APU Bleed Valve is verified closed.

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133 DOORS 10 1 Door Seal System Charging Valve C 1 0 (M#) May be inoperative provided the valve is secured in the closed position Door Seal Drain Valve C 1 0 May be failed in the closed position. C 1 0 (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 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.

134 DOORS (CONT D) 2) Door Handle C 1 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 BAGGAGE DOOR INOPERATIVE DO NOT OPEN. NOTE: Only applicable if Forward Baggage Compartment installed. 2) Door Handle (Cont d) C 1 0 (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 BAGGAGE DOOR INOPERATIVE DO NOT OPEN. NOTE: Only applicable if Forward Baggage Compartment installed.

135 DOORS (CONT D) 10 4 *** 10 5 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. FUSELAGE DOORS Warning System 1) Airstair Door, Forward Baggage Door, Aft Passenger Door and Aft Service Door Proximity Sensors a) Pre Mod or 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.

136 DOORS (CONT D) b) Post Mod or ) Airstair Door, Aft Passenger Door and Aft Service Door Proximity Sensors (Forward baggage compartment not installed) Aft Baggage Door Counter Balance System Aft Baggage Door Telescopic Strut 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 Passenger Airstair door warning system sensor will render AUTO Mode of the Cabin Pressure Control System inoperative. A 6 5 (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. C 2 0 (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. C 1 0 (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. C 1 0 (M) May be inoperative provided an alternate approved means to support the baggage door in the open position is established and used. Lock Release Collar C 1 0 May be inoperative provided the strut is only used in the non extended position.

137 DOORS (CONT D) 50 1 *** Fortified Flight Deck Door (With Remote Access System) 1) Automatic Locking System (Primary System) Forward baggage compartment installed Forward baggage compartment not installed A 1 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 BAGGAGE DOOR INOPERATIVE DO NOT OPEN. A 1 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.

138 DOORS (CONT D) 2) Flight Deck Emergency Access Function Forward baggage compartment installed Forward baggage compartment not installed A 1 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 BAGGAGE DOOR INOPERATIVE DO NOT OPEN. A 1 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.

139 DOORS (CONT D) 3) DENY Function Forward baggage compartment installed Forward baggage compartment not installed A 1 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 BAGGAGE DOOR INOPERATIVE DO NOT OPEN. A 1 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.

140 DOORS (CONT D) 4) UNLK Function C 1 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. 5) Emergency Access Push Button Switch Panel White/Amber Indication Lights C 4 0 (O) May be inoperative provided Emergency access function is verified operative. 6) FAIL COCKPIT DOOR Advisory Light Forward baggage compartment installed Forward baggage compartment not installed C 1 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. C 1 0 (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.

141 DOORS (CONT D) 7) CKPT DOOR OPEN Advisory Light Forward baggage compartment installed Forward baggage compartment not installed C 1 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. C 1 0 (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 Forward baggage compartment installed Forward baggage compartment not installed C 1 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. C 1 0 (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.

142 DOORS (CONT D) 9) BAGG DOOR OPEN Advisory Light (Forward Baggage Compartment Installed) 10) Deadbolt (Secondary locking system) 11) INTERNAL DOORS Caution Light (Forward baggage compartment installed) C 1 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. C 1 0 (O) May be inoperative provided Automatic locking (Remote Access) system is operative. A 1 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 is secured closed by an acceptable means or method, and f) Internal baggage door is placarded, INTERNAL BAGGAGE DOOR INOPERATIVE DO NOT OPEN.

143 DOORS (CONT D) 50 2 *** 12) COCKPIT DOOR Caution Light (Forward baggage compartment not installed) Flight Deck Emergency Access Function A 1 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 , 2) *** 50 4 *** DENY Function Incorporated into Item , 3). UNLK Function Incorporated into Item , 4) *** 50 6 *** 50 7 *** 50 8 *** 50 9 *** 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 Incorporated in Item , 5). Incorporated into Item , 6). Incorporated into Item , 7). Incorporated into Item , 8). Incorporated into Item , 9) *** Deadbolt Incorporated into Item , 10) *** INTERNAL DOORS Caution Light Incorporated into Item , 11).

144 DOORS (CONT D) Fortified Flight Deck Door (Without Remote Access System) 1) Deadbolt Lock C 1 0 (O) May be inoperative provided primary locking mechanism, slide latch, is operative Lavatory Door Lock/Door Latch 1) Door Lock C 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. 2) Door Latch C 0 (M) May be inoperative provided: Lavatory door is locked closed and placarded, INOPERATIVE DO NOT ENTER.

145 Rev 6 Mar 26/ PROPELLERS *** Propeller Maintenance Unfeather Function RDC NP Switch D 2 0 (M#) May be inoperative provided an alternate feather check is performed. Moved to ENGINE CONTROL Panel Switches

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147 Rev 6 Mar 26/ POWER PLANT 60 1 Engine Intake Bypass Doors C 2 0 May be inoperative in closed position provided the flight is not conducted in known or forecast icing conditions. C 2 0 (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.

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149 Rev 6 Mar 26/ ENGINE FUEL AND CONTROL 20 1 Engine FADEC System FADEC faults A 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 NOTE: MEL extensions are not permitted. 2. Time Limited Dispatch reporting system is maintained as per Pratt & Whitney Canada Airworthiness Limitations Manual Part No *** 20 3 MTOP Switch Power Rating Switches Moved to ENGINE CONTROL Panel Switches 1) MCR Switch Moved to ENGINE CONTROL Panel Switches. 2) MCL Switch 20 4 Reduce Power Switches 1) RDC TOP TRQ DEC Switch Moved to ENGINE CONTROL Panel Switches. 2) RDC TOP TRQ RESET Switch 30 1 FF (Fuel Flow) Indications B 2 1 May be inoperative provided Fuel QTY indications are operative.

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151 Rev 6 Mar 26/ ENGINES 10 1 ENGINE CONTROL Panel Switches 1) RDC Np LDG Switch *** 2) MTOP Switch *** C 1 0 May be inoperative provided the RDC Np LDG function is not used. C 1 0 (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: 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. C 1 0 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. 3) MCR Switch D 1 0 May be inoperative provided condition levers are used to set power rating. 4) MCL Switch D 1 0 May be inoperative provided condition levers are used to set power rating. 5) RDC TOP TRQ DEC Switch 6) RDC TOP TRQ RESET Switch D 1 0 May be inoperative provided RDC TOP TRQ DEC is not used. D 1 0 May be inoperative provided RDC TOP TRQ DEC is not used.

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153 Rev 6 Mar 26/ 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.

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155 Rev 6 Mar 26/ 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.

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