# F Model CL−600−2D24 (Series 900) Model CL−600−2D15

(Series 705) <2705> 

# AIRPLANE FLIGHT MANUAL Volume 1 CSP C−012 

# MASTER Information copy only. This material is not customized to a specific airplane configuration. The user must ascertain that this material is applicable for the intended use. 

### BOMBARDIER INC. BOMBARDIER AEROSPACE COMMERCIAL AIRCRAFT CUSTOMER SUPPORT 123 GARRATT BLVD., TORONTO, ONTARIO CANADA M3K 1Y5 Copyright © 2002 − 2015 by Bombardier Inc. All rights reserved. No part of this work may be reproduced or copied in any form or by any means without written permission of Bombardier Inc. The Bombardier logo is a registered trademark of Bombardier Inc. **Initial Issue: Revision 11A:**  **Sep 09/2002 May 25/2015**  

## B"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."

### This is revision **11A** to the **MASTER Airplane Flight Manual , CSP C−012** . To bring this manual up to date, remove old pages and insert revised pages as follows: **REMOVE: INSERT:**  **Chapter Section**  **Subject Page**  **Chapter Section**  **Subject Page**  

### Title Page / Disclaimer All Title Page / Disclaimer All 00−02 00−02−55 to 00−02−58 00−02 00−02−55 to 00−02−60 00−04 00−04−1 to 00−04−14 Limitations 02−00−4 to 02−00−5 Limitations 02−00−4 to 02−00−5 02−08−8 02−08−8 Normal Procedures 04−02−10 Normal Procedures 04−02−10 04−02−13 04−02−13 Abnormal Procedures 05−00−7 to 05−00−8 Abnormal Procedures 05−00−7 to 05−00−8 05−15−12 05−15−12 to 05−15−14 

# F **TRANSMITTAL LETTER** Transmit−1 Rev. 11A, May 25/2015

DOT Approved 

### Airplane Flight Manual **CSP C−012** NOTE Re. pages04-02 - 10 and 04-02-13 . Th esepageswerereissued with revision bars due to changes i nthepublishing software attributes, however the text remains unchanged.

# F **TRANSMITTAL LETTER** Transmit−2 Rev. 11A, May 25/2015

DOT Approved 

### Airplane Flight Manual **CSP C−012** THIS PAGE INTENTIONALLY LEFT BLANKTitle Page / Disclaimer All* May 25/2015 00 − 01 <TC> − 1 May 02/2011 −2 Feb 16/2010 00 − 01 <FAA> − 1 May 02/2011 −2 Feb 16/2010 00 − 01 <JAA> − 1 May 02/2011 −2 Feb 16/2010 00 − 01 <DNA> − 1 May 02/2011 −2 Feb 16/2010 00 − 01 <TC> and <2705> − 1 May 02/2011

−2 Feb 16/2010 00 − 01 <FAA> and <2705> − 1 May 02/2011

−2 Feb 16/2010 00 − 01 <JAA> and <2705> − 1 Feb 14/2013

−2 Feb 14/2013 00 − 01 <DNA> and <2705> − 1 May 02/2011

−2 Feb 16/2010 00 − 01 <ECAA> − 1 May 02/2011 −2 May 02/2011 00 − 01 <CAAC> − 1 Jun 08/2012 −2 Jun 08/2012 00 − 02 − 1 Mar 25/2011 −2 Mar 25/2011 − 3 Mar 25/2011 −4 Mar 25/2011 − 5 Mar 25/2011 − 6 Mar 25/2011 − 7 Mar 25/2011 − 8 Mar 25/2011 − 9 Mar 25/2011 − 10 Mar 25/2011 − 11 Mar 25/2011 − 12 Mar 25/2011 − 13 Mar 25/2011 − 14 Mar 25/2011 − 15 Mar 25/2011 − 16 Mar 25/2011 − 17 Mar 25/2011 − 18 Mar 25/2011 − 19 Mar 25/2011 −20 Mar 25/2011 −21 Mar 25/2011 −22 Mar 25/2011 −23 Mar 25/2011 −24 Mar 25/2011 −25 Jun 08/2012 −26 Jun 08/2012 −27 Jun 07/2013 −28 Jun 07/2013 −29 Jun 07/2013 − 30 Sep 27/2013 − 31 Sep 27/2013 − 32 Sep 27/2013 − 33 Sep 27/2013 − 34 Sep 27/2013 − 35 Sep 27/2013 − 36 Dec 22/2014 − 37 Dec 22/2014 − 38 Dec 22/2014 − 39 Sep 27/2013 −40 Sep 27/2013 −41 Sep 27/2013 −42 Sep 27/2013 −43 Sep 27/2013 −44 Sep 27/2013 −45 Sep 27/2013 −46 Sep 27/2013 −47 Sep 27/2013 −48 Sep 27/2013 −49 Sep 27/2013 − 50 Dec 22/2014 − 51 Jun 02/2014 − 52 Jun 02/2014 − 53 Dec 22/2014 − 54 Dec 22/2014 − 55 * May 25/2015 − 56 * May 25/2015 − 57 * May 25/2015 − 58 * May 25/2015 − 59 * May 25/2015 − 60 * May 25/2015 00 − 03 − 1 Feb 16/2010 −2 Feb 16/2010 − 3 Feb 16/2010 −4 Feb 16/2010 − 5 Feb 16/2010 − 6 Feb 16/2010 − 7 Feb 16/2010 − 8 Feb 16/2010 − 9 Feb 16/2010 − 10 Feb 16/2010 − 11 Feb 16/2010 − 12 Feb 16/2010 − 13 Jun 21/2010 − 14 Jun 21/2010 − 15 Jun 21/2010 − 16 Jun 21/2010 − 17 Jun 21/2010 − 18 Jun 21/2010 − 19 Jun 21/2010 −20 Jun 21/2010 −21 Jun 21/2010 −22 Jun 21/2010 −23 Jun 21/2010 −24 Jun 21/2010 −25 Jun 21/2010 −26 Jun 21/2010 −27 Jun 21/2010 −28 Jun 21/2010 −29 Jun 21/2010 − 30 Jun 21/2010 − 31 Jun 21/2010 − 32 Jun 21/2010 00 − 04 − 1 * May 25/2015 −2 * May 25/2015 − 3 * May 25/2015 

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* The asterisk indicates pages changed, added or deleted. PAGE PRINTED ON 10-9-201 5−4 * May 25/2015 − 5 * May 25/2015 − 6 * May 25/2015 − 7 * May 25/2015 − 8 * May 25/2015 − 9 * May 25/2015 − 10 * May 25/2015 − 11 * May 25/2015 − 12 * May 25/2015 − 13 * May 25/2015 − 14 * May 25/2015 01 − 00 − 1 Jun 08/2012 −2 Feb 16/2010 01 − 02 − 1 Feb 16/2010 −2 Feb 16/2010 − 3 Feb 16/2010 −4 Feb 16/2010 − 5 Feb 16/2010 − 6 Feb 16/2010 − 7 Feb 16/2010 − 8 Feb 16/2010 − 9 Feb 16/2010 − 10 Dec 20/2012 − 11 Sep 11/2013 − 12 Sep 11/2013 − 13 Sep 11/2013 − 14 Sep 11/2013 − 15 Sep 11/2013 − 16 Dec 22/2014 − 17 Dec 22/2014 − 18 Dec 22/2014 − 19 Dec 22/2014 −20 Mar 16/2015 02 − 00 − 1 Jun 02/2014 −2 Jun 02/2014 − 3 Sep 27/2013 −4 * May 25/2015 − 5 * May 25/2015 − 6 Feb 16/2010 02 − 01 − 1 Sep 27/2013 −2 Sep 27/2013 02 − 02 − 1 Feb 16/2010 −2 Feb 16/2010 02 − 03 − 1 Feb 16/2010 −2 Feb 16/2010 − 3 Feb 16/2010 −4 Feb 16/2010 − 5 Feb 16/2010 − 6 Feb 16/2010 − 7 Feb 16/2010 − 8 Feb 16/2010 02 − 04 − 1 Sep 27/2013 −2 Feb 16/2010 − 3 Sep 27/2013 −4 Sep 27/2013 − 5 Sep 27/2013 − 6 Sep 27/2013 − 7 Sep 27/2013 − 8 Sep 27/2013 02 − 05 − 1 Jun 02/2014 −2 Jun 02/2014 − 3 Jun 02/2014 −4 Jun 02/2014 − 5 Jun 02/2014 − 6 Jun 02/2014 − 7 Jun 02/2014 − 8 Jun 02/2014 − 9 Jun 02/2014 − 10 Jun 02/2014 − 11 Jun 02/2014 − 12 Jun 02/2014 − 13 Jun 02/2014 − 14 Jun 02/2014 − 15 Jun 02/2014 − 16 Jun 02/2014 02 − 06 − 1 Feb 16/2010 −2 Feb 16/2010 − 3 Feb 16/2010 −4 Feb 16/2010 − 5 Feb 16/2010 − 6 Feb 16/2010 − 7 Feb 16/2010 − 8 Feb 16/2010 02 − 07 − 1 Feb 16/2010 −2 Feb 16/2010 02 − 08 − 1 Sep 27/2013 −2 Sep 27/2013 − 3 Sep 27/2013 −4 Sep 27/2013 − 5 Sep 27/2013 − 6 Sep 27/2013 − 7 Sep 27/2013 − 8 * May 25/2015 02 − 09 − 1 Sep 11/2013 −2 Sep 11/2013 − 3 Sep 27/2013 −4 Sep 11/2013 − 5 Sep 11/2013 − 6 Sep 11/2013 − 7 Sep 11/2013 − 8 Sep 11/2013 03 − 00 − 1 Sep 27/2013 −2 Sep 27/2013 − 3 Sep 27/2013 −4 Dec 22/2014 03 − 01 − 1 Dec 22/2014 −2 Feb 16/2010 03 − 02 − 1 Feb 16/2010 −2 Feb 16/2010 03 − 03 − 1 Sep 27/2013 −2 Sep 27/2013 − 3 Sep 27/2013 −4 Sep 27/2013 − 5 Sep 27/2013 − 6 Sep 27/2013 

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* The asterisk indicates pages changed, added or deleted. PAGE PRINTED ON 10-9-201 503 − 04 − 1 Sep 27/2013 −2 Sep 27/2013 − 3 Sep 27/2013 −4 Sep 27/2013 − 5 Sep 27/2013 − 6 Sep 27/2013 − 7 Sep 27/2013 − 8 Sep 27/2013 − 9 Sep 27/2013 − 10 Sep 27/2013 − 11 Sep 27/2013 − 12 Sep 27/2013 03 − 05 − 1 Sep 27/2013 −2 Sep 27/2013 − 3 Sep 27/2013 −4 Sep 27/2013 − 5 Sep 27/2013 − 6 Sep 27/2013 03 − 06 − 1 Feb 14/2013 −2 Feb 16/2010 03 − 07 − 1 Feb 16/2010 −2 Feb 16/2010 03 − 08 − 1 Sep 27/2013 −2 Jun 02/2014 03 − 09 − 1 Sep 27/2013 −2 Sep 27/2013 − 3 Sep 27/2013 −4 Sep 27/2013 − 5 Sep 27/2013 − 6 Sep 27/2013 − 7 Sep 27/2013 − 8 Sep 27/2013 03 − 10 − 1 Sep 27/2013 −2 Feb 16/2010 03 − 11 − 1 Sep 27/2013 −2 Sep 27/2013 − 3 Sep 27/2013 −4 Sep 27/2013 − 5 Sep 27/2013 − 6 Feb 16/2010 03 − 12 − 1 Feb 16/2010 −2 Feb 16/2010 − 3 Feb 16/2010 −4 Sep 27/2013 − 5 Sep 27/2013 − 6 Sep 27/2013 03 − 13 − 1 Feb 16/2010 −2 Feb 16/2010 03 − 14 − 1 Jun 02/2014 −2 Jun 02/2014 − 3 Jun 02/2014 −4 Feb 16/2010 03 − 15 − 1 Sep 27/2013 −2 Sep 27/2013 − 3 Sep 27/2013 −4 Sep 27/2013 − 5 Sep 27/2013 − 6 Jun 07/2013 − 7 May 02/2011 − 8 May 02/2011 03 − 16 − 1 Jun 07/2013 −2 Feb 16/2010 03 − 17 − 1 Feb 16/2010 −2 Feb 16/2010 03 − 18 − 1 Jun 02/2014 −2 Jun 02/2014 − 3 Jun 02/2014 −4 Jun 02/2014 − 5 Jun 02/2014 − 6 Jun 02/2014 − 7 Jun 02/2014 − 8 Jun 15/2012 03 − 19 − 1 Dec 22/2014 −2 Dec 22/2014 − 3 Dec 22/2014 −4 Dec 22/2014 − 5 Dec 22/2014 − 6 Dec 22/2014 − 7 Dec 22/2014 − 8 Dec 22/2014 − 9 Dec 22/2014 − 10 Dec 22/2014 − 11 Dec 22/2014 − 12 Dec 22/2014 − 13 Dec 22/2014 − 14 Dec 22/2014 − 15 Dec 22/2014 − 16 Dec 22/2014 04 − 00 − 1 Sep 27/2013 −2 Sep 27/2013 04 − 01 − 1 Sep 27/2013 −2 Sep 27/2013 04 − 02 − 1 Feb 16/2010 −2 Feb 16/2010 − 3 Feb 16/2010 −4 Feb 16/2010 − 5 Dec 22/2014 − 6 Feb 16/2010 − 7 Jan 19/2011 − 8 Sep 27/2013 − 9 Sep 27/2013 − 10 * May 25/2015 − 11 Dec 22/2014 − 12 Dec 22/2014 − 13 * May 25/2015 − 14 Mar 16/2015 − 15 Mar 16/2015 − 16 Dec 22/2014 05 − 00 − 1 Jun 02/2014 −2 Dec 22/2014 − 3 Jun 02/2014 −4 Dec 22/2014 − 5 Sep 27/2013 

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* The asterisk indicates pages changed, added or deleted. PAGE PRINTED ON 10-9-201 5− 6 Jun 02/2014 − 7 * May 25/2015 − 8 * May 25/2015 − 9 Sep 27/2013 − 10 Feb 16/2010 05 − 01 − 1 Dec 22/2014 −2 Feb 16/2010 05 − 02 − 1 Feb 16/2010 −2 Feb 16/2010 − 3 Feb 16/2010 −4 Feb 16/2010 05 − 03 − 1 Jun 02/2014 −2 Jun 02/2014 − 3 Jun 02/2014 −4 Jun 02/2014 − 5 Jun 02/2014 − 6 Jun 02/2014 − 7 Jun 02/2014 − 8 Jun 02/2014 05 − 04 − 1 Feb 16/2010 −2 Sep 27/2013 − 3 Sep 27/2013 −4 Sep 27/2013 − 5 Sep 27/2013 − 6 Sep 27/2013 − 7 Sep 27/2013 − 8 Sep 27/2013 − 9 Sep 27/2013 − 10 Sep 27/2013 − 11 Sep 27/2013 − 12 Mar 16/2015 − 13 Sep 27/2013 − 14 Dec 22/2014 05 − 05 − 1 Jun 02/2014 −2 Jun 02/2014 − 3 Jun 02/2014 −4 Jun 02/2014 − 5 Jun 02/2014 − 6 Jun 02/2014 − 7 Jun 02/2014 − 8 Jun 02/2014 − 9 Jun 02/2014 − 10 Jun 02/2014 − 11 Jun 02/2014 − 12 Jun 02/2014 − 13 Jun 02/2014 − 14 Jun 02/2014 05 − 06 − 1 Feb 16/2010 −2 Sep 27/2013 05 − 07 − 1 Jun 02/2014 −2 Jun 02/2014 − 3 Jun 02/2014 −4 Jun 02/2014 − 5 Jun 02/2014 − 6 Jun 02/2014 05 − 08 − 1 Sep 27/2013 −2 Sep 27/2013 − 3 Sep 27/2013 −4 Sep 27/2013 − 5 Sep 27/2013 − 6 Sep 27/2013 05 − 09 − 1 Jan 31/2011 −2 Jan 31/2011 − 3 Feb 16/2010 −4 Dec 22/2014 − 5 Dec 22/2014 − 6 Feb 16/2010 05 − 10 − 1 Feb 16/2010 −2 Feb 16/2010 05 − 11 − 1 Feb 16/2010 −2 Sep 27/2013 − 3 Sep 27/2013 −4 Sep 27/2013 − 5 Sep 27/2013 − 6 Sep 27/2013 − 7 Sep 27/2013 − 8 Sep 27/2013 − 9 Sep 27/2013 − 10 Sep 27/2013 − 11 Sep 27/2013 − 12 Sep 27/2013 − 13 Sep 27/2013 − 14 Sep 27/2013 − 15 Sep 27/2013 − 16 Sep 27/2013 − 17 Sep 27/2013 − 18 Sep 27/2013 − 19 Sep 27/2013 −20 Sep 27/2013 −21 Sep 27/2013 −22 Sep 27/2013 05 − 12 − 1 Sep 27/2013 −2 Feb 16/2010 − 3 Feb 16/2010 −4 Sep 27/2013 − 5 Sep 27/2013 − 6 Sep 27/2013 − 7 Sep 27/2013 − 8 Sep 27/2013 − 9 Sep 27/2013 − 10 Feb 16/2010 05 − 13 − 1 Jun 21/2010 −2 Jun 21/2010 − 3 Jun 21/2010 −4 Feb 16/2010 − 5 Feb 16/2010 − 6 Feb 16/2010 − 7 Feb 16/2010 − 8 Jun 21/2010 − 9 Feb 16/2010 − 10 Jun 21/2010 − 11 Feb 16/2010 − 12 Feb 16/2010 − 13 Feb 16/2010 − 14 Feb 16/2010 − 15 Feb 16/2010 − 16 Feb 16/2010 − 17 Feb 16/2010 − 18 Feb 16/2010 

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* The asterisk indicates pages changed, added or deleted. PAGE PRINTED ON 10-9-201 505 − 14 − 1 Sep 27/2013 −2 Jun 02/2014 − 3 Sep 27/2013 −4 Jun 02/2014 − 5 Jun 02/2014 − 6 Jun 02/2014 − 7 Jun 02/2014 − 8 Jun 02/2014 − 9 Jun 02/2014 − 10 Sep 27/2013 05 − 15 − 1 Dec 22/2014 −2 Dec 22/2014 − 3 Dec 22/2014 −4 Dec 22/2014 − 5 Dec 22/2014 − 6 Dec 22/2014 − 7 Dec 22/2014 − 8 Dec 22/2014 − 9 Dec 22/2014 − 10 Dec 22/2014 − 11 Dec 22/2014 − 12 * May 25/2015 − 13 * May 25/2015 − 14 * May 25/2015 05 − 16 − 1 Sep 27/2013 −2 Sep 27/2013 − 3 Feb 16/2010 −4 Feb 16/2010 − 5 Feb 16/2010 − 6 Feb 16/2010 − 7 Sep 27/2013 − 8 Feb 16/2010 − 9 Sep 27/2013 − 10 Feb 16/2010 05 − 17 − 1 Feb 16/2010 −2 Feb 16/2010 05 − 18 − 1 Jan 31/2011 −2 Feb 16/2010 06 − 00 − 1 Jun 02/2014 −2 Jun 08/2012 − 3 Feb 16/2010 −4 Jun 02/2014 − 5 Jun 08/2012 − 6 Jun 02/2014 − 7 Jun 08/2012 − 8 Jun 08/2012 − 9 Jun 02/2014 − 10 Jun 02/2014 06 − 01 − 1 Feb 16/2010 −2 Feb 16/2010 − 3 Feb 16/2010 −4 Feb 16/2010 − 5 Feb 16/2010 − 6 Feb 16/2010 − 7 Feb 16/2010 − 8 Feb 16/2010 − 9 Feb 16/2010 − 10 Feb 16/2010 − 11 Feb 16/2010 − 12 Feb 16/2010 − 13 Feb 16/2010 − 14 Feb 16/2010 − 15 Feb 16/2010 − 16 Feb 16/2010 − 17 Feb 16/2010 − 18 Feb 16/2010 − 19 Feb 16/2010 −20 Feb 16/2010 −21 Feb 16/2010 −22 Feb 16/2010 −23 Feb 16/2010 −24 Feb 16/2010 −25 Feb 16/2010 −26 Feb 16/2010 −27 Feb 16/2010 −28 Feb 16/2010 06 − 02 − 1 Jun 02/2014 −2 Feb 16/2010 − 3 Feb 16/2010 −4 Feb 16/2010 − 5 Feb 16/2010 − 6 Feb 16/2010 − 7 Feb 16/2010 − 8 Feb 16/2010 − 9 Feb 16/2010 − 10 Feb 16/2010 − 11 Feb 16/2010 − 12 Feb 16/2010 − 13 Feb 16/2010 − 14 Feb 16/2010 − 15 Feb 16/2010 − 16 Feb 16/2010 − 17 Feb 16/2010 − 18 Feb 16/2010 − 19 Feb 16/2010 −20 Feb 16/2010 −21 Feb 16/2010 −22 Feb 16/2010 −23 Feb 16/2010 −24 Feb 16/2010 −25 Feb 16/2010 −26 Feb 16/2010 −27 Feb 16/2010 −28 Feb 16/2010 06 − 03 − 1 Jun 02/2014 −2 Jun 02/2014 − 3 Jun 02/2014 −4 Jun 02/2014 − 5 Feb 16/2010 − 6 Feb 16/2010 − 7 Feb 16/2010 − 8 Feb 16/2010 − 9 Feb 16/2010 − 10 Feb 16/2010 − 11 Feb 16/2010 − 12 Feb 16/2010 − 13 Feb 16/2010 − 14 Feb 16/2010 − 15 Feb 16/2010 − 16 Feb 16/2010 − 17 Feb 16/2010 − 18 Feb 16/2010 − 19 Feb 16/2010 −20 Feb 16/2010 −21 Feb 16/2010 −22 Feb 16/2010 −23 Feb 16/2010 

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### INTRODUCTION INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 01 1 LANDING DISTANCE FACTORS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 01 1 REJECTED TAKE OFF REJECTED TAKE-OFF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 02 1 Rejected Take-off Before Achieving V 1 

### . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 02 1 POWER PLANT POWER PLANT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 03 1 L ENG FIRE or R ENG FIRE or Severe Engine Damage (In Flight) . . . . . . . . . . . . . 03 03 1 L ENG FIRE or R ENG FIRE or Severe Engine Damage (On Ground) . . . . . . . . . . . 03 03 1 Double Engine Failure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 03 2 L REV DEPLOYED or R REV DEPLOYED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 03 5 L ENG OIL PRESS or R ENG OIL PRESS or Low Engine Oil Pressure Indication . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 03 6 Uncommanded Acceleration / ENGINE OVERSPD . . . . . . . . . . . . . . . . . . . . . . . . . 03 03 6 SMOKE/FIRE/FUMES SMOKE/FIRE/FUMES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 04 1 General Notes, Cautions and Warnings . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 04 1 Smoke/Fire/Fumes Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 04 1 Smoke or Fumes Removal Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 04 9 SMOKE AFT LAV or SMOKE FWD LAV . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 04 9 SMOKE AFT CARGO or SMOKE FWD CARGO . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 04 10 AIR CONDITIONING AND PRESSURIZATION AIR-CONDITIONING AND PRESSURIZATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 05 1 CABIN ALT (Warning Message) or Emergency Descent Procedure . . . . . . . . . . . . . 03 05 1 DIFF PRESS <TC> or <FAA> or <JAA> 

### . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 05 2 DIFF PRESS <AR> 

### . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 05 3 AUTOMATIC FLIGHT CONTROL SYSTEM AUTOMATIC FLIGHT CONTROL SYSTEM (AFCS) . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 06 1 AFCS MSG FAIL or Autopilot Failure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 06 1 Uncommanded Yaw Motion . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 06 1 

### EMERGENCY PROCEDURES Table of Contents 03 00 1 Rev. 8, Sep 27/2013 

### CHAPTER 3 - EMERGENCY PROCEDURES

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### AUXILIARY POWER UNIT AUXILIARY POWER UNIT (APU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 07 1 APU FIRE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 07 1 APU OVERSPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 07 1 APU OVERTEMP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 07 1 BLEED AIR LEAKS BLEED AIR LEAKS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 08 1 L BLEED DUCT or R BLEED DUCT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 08 1 DITCHING AND FORCED LANDING DITCHING AND FORCED LANDING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 1 Recommended Configuration . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 1 DITCHING OR FORCED LANDING IMMINENT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 1 Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 1 PLANNED DITCHING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 2 General Notes, Cautions and Warnings . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 2 Preliminary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 2 Approach . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 3 Prior to Water Contact . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 4 After Water Contact . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 4 FORCED LANDING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 5 General Notes, Cautions and Warnings . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 5 Preliminary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 5 Approach . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 6 Prior to Contact . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 6 After Contact . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 09 7 EVACUATION EVACUATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 10 1 Passenger Evacuation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 10 1 ELECTRICAL ELECTRICAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 11 1 EMER PWR ONLY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 11 1 Loss of all AC Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 11 3 

### EMERGENCY PROCEDURES Table of Contents 03 00 2 Rev. 8, Sep 27/2013

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### FLIGHT CONTROLS FLIGHT CONTROLS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 12 1 Aileron System Jammed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 12 1 Elevator System Jammed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 12 2 Rudder System Jammed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 12 3 Stabilizer Trim Runaway . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 12 4 Stall Recovery . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 12 5 FUEL SYSTEM FUEL SYSTEM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 13 1 LO FUEL (Caution Message) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 13 1 ICE AND RAIN PROTECTION ICE AND RAIN PROTECTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 14 1 WING OVHT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 14 1 ANTI-ICE DUCT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 14 1 L COWL A/I DUCT or R COWL A/I DUCT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 14 2 LANDING GEAR, WHEEL AND BRAKE SYSTEM LANDING GEAR, WHEEL AND BRAKE SYSTEM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 15 1 MLG BAY OVHT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 15 1 BRAKE OVHT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 15 1 GEAR DISAGREE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 15 2 LDG GEAR Lever Jammed in the UP Position . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 15 3 Landing Gear Up / Unsafe Landing Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 15 4 PARKING BRAKE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 15 6 During Landing – Excessive Asymmetry or Loss of Braking . . . . . . . . . . . . . . . . . . . 03 15 6 NOSE DOOR OPEN . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 15 7 PASSENGER DOOR PASSENGER DOOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 16 1 PASSENGER DOOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 16 1 AURAL/VISUAL WARNING SYSTEM AURAL/VISUAL WARNING SYSTEM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 17 1 Configuration Warning . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 17 1 

### EMERGENCY PROCEDURES Table of Contents 03 00 3 Rev. 8, Sep 27/2013

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### HYDRAULIC POWER HYDRAULIC POWER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 18 1 HYD 1 HI TEMP (Caution Message) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 18 1 HYD 2 HI TEMP (Caution Message) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 18 3 UNRELIABLE AIRSPEED UNRELIABLE AIRSPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 19 1 Unreliable Airspeed In-flight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03 19 1 LIST OF ILLUSTRATIONS HYDRAULIC POWER Figure 03 18 1 Maximum Landing Weight Limited by Maximum Brake Energy – Single Hydraulic System Failure . . . . . . . . . . . . . . . . . 03 18 8 

### EMERGENCY PROCEDURES Table of Contents 03 00 4 Rev. 10, Dec 22/2014

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### 1. UNRELIABLE AIRSPEED A. Unreliable Airspeed In-flight Indication: Pitch attitude, thrust setting or external noise not consistent with indicated airspeed. Large airspeed differences shown between primary flight displays and/or standby instrument. Loss of multiple airspeed indication. STALL FAIL , EFIS COMP MON , EFIS COMP INOP caution messages and/or red IAS flag. If above minimum safe altitude: (1) Autopilot ............................................................................................................Disengage (2) FDs ....................................................................................................................... Deselect (3) Use standby attitude indicator / ISI. 

## CAUTION Respect stall warning/stick shaker. (4) Proceed to step (7). If below minimum safe altitude: (1) Autopilot ............................................................................................................Disengage (2) FDs ....................................................................................................................... Deselect (3) Use standby attitude indicator / ISI. (4) Pitch/N 1 

### ...................................................................................................... 10 degrees/TO (5) Airplane .................................................................. Go-around, clean up and climb above minimum safe altitude Above 15000 feet: (6) Pitch/N 1 

### ...................................................................................................... 5 degrees/CLB 

## CAUTION Respect stall warning/stick shaker. 

### EMERGENCY PROCEDURES Unreliable Airspeed 03 − 19 − 1 Rev. 10, Dec 22/2014

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### (7) Set and monitor pitch and roll using standby attitude indicator or ISI. <1099> 

### (7) Set and monitor pitch and roll using PFD. <1025> or <1100> 

### When above minimum safe altitude: (8) Pitch/N 1 

### .......................................................... Set as per Table A to achieve approximate level flight. 

### EMERGENCY PROCEDURES Unreliable Airspeed 03 − 19 − 2 Rev. 10, Dec 22/2014

DOT Approved 

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### Table A – Level Flight Cruise – FLAPS 0 ALT (ft) Target Weight kg (lb) Expected Indicated Airspeed/ Mach 20412 (45000) 22680 (50000) 24948 (55000) 27216 (60000) 29484 (65000) KIAS/M 40000 Pitch (degree) 0.5 1.0 1.0 1.0 1.0 210 to 245 .70 to .81 N 1 

### (%) 79.6 80.6 81.6 82.7 84.3 35000 Pitch (degree) 0.0 0.0 0.5 0.5 0.5 230 to 275 .69 to .81 N 1 

### (%) 78.2 78.9 79.6 80.3 81.1 30000 Pitch (degree) − 0.5 − 0.5 0.0 0.0 0.5 250 to 290 – N 1 

### (%) 77.6 78.0 78.4 79.0 79.6 25000 Pitch (degree) − 1.0 − 0.5 0.0 0.0 0.5 250 to 290 – N 1 

### (%) 74.0 74.5 74.9 75.5 76.2 20000 Pitch (degree) − 1.0 − 0.5 0.0 0.0 0.5 250 to 290 – N 1 

### (%) 70.4 70.8 71.2 71.8 72.5 15000 Pitch (degree) − 1.0 − 0.5 0.0 0.0 0.5 250 to 290 – N 1 

### (%) 66.0 67.3 67.9 68.3 68.7 10000 Pitch (degree) 0.5 1.0 1.5 2.0 2.5 210 to 230 – N 1 

### (%) 55.1 55.9 56.7 57.6 58.7 5000 Pitch (degree) 0.5 1.0 1.5 2.0 2.5 210 to 230 – N 1 

### (%) 51.8 52.5 53.3 54.1 55.2 If any indicated speed is outside the expected indicated airspeed range, it should be considered UNRELIABLE. 

### EMERGENCY PROCEDURES Unreliable Airspeed 03 − 19 − 3 Rev. 10, Dec 22/2014

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### Table A – Level Flight Cruise – FLAPS 0 (continued) ALT (ft) Target Weight kg (lb) Expected Indicated Airspeed/ Mach 31751 (70000) 34019 (75000) 36287 (80000) 38329 (84500) – KIAS/M 40000 Pitch (degree) 1.0 – – – – 210 to 245 .70 to .81 N 1 

### (%) 85.6 – – – – 35000 Pitch (degree) 1.0 1.0 1.0 1.0 – 230 to 275 .69 to .81 N 1 

### (%) 82.0 82.9 84.1 85.7 – 30000 Pitch (degree) 0.5 1.0 1.0 1.5 – 250 to 290 – N 1 

### (%) 80.4 81.2 81.8 82.7 – 25000 Pitch (degree) 0.5 1.0 1.0 1.5 – 250 to 290 – N 1 

### (%) 76.9 77.8 78.5 79.3 – 20000 Pitch (degree) 0.5 1.0 1.5 1.5 – 250 to 290 – N 1 

### (%) 73.2 73.9 74.6 75.4 – 15000 Pitch (degree) 0.5 1.0 1.5 1.5 – 250 to 290 – N 1 

### (%) 69.3 70.2 70.9 71.7 – 10000 Pitch (degree) 3.0 3.0 3.5 4.0 – 210 to 230 – N 1 

### (%) 60.2 61.9 63.3 64.7 – 5000 Pitch (degree) 3.0 3.0 3.5 4.0 – 210 to 230 – N 1 

### (%) 56.4 58.0 59.3 60.6 – If any indicated speed is outside the expected indicated airspeed range, it should be considered UNRELIABLE. 

### EMERGENCY PROCEDURES Unreliable Airspeed 03 − 19 −4 Rev. 10, Dec 22/2014

DOT Approved 

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### NOTE Procedures for EFIS COMP MON, EFIS COMP INOP, STALL FAIL and RUD LIMITER caution messages and/or red IAS flag are incorporated in this procedure. (9) STALL PTCT, PUSHER switch (left or right) ...............................................................OFF (10) Autopilot or FD ...............................................................................................PTCH/ROLL NOTE 1. Pitch/Thrust settings will give approximate level flight, and may result in slight climb or descent. Adjust pitch to stop climb/descent; if displayed, VSI can be used. 2. Airspeed trend vector may be erroneous. 3. If overspeed warning sounds, select the affected AUDIO WARNING switch to DISABLE. 4. Altitude, Mode C and TCAS may be in error by up to 600 feet. 5. Groundspeed indication may be unreliable. 6. FMS cruise time and fuel predictions may be incorrect. 7. Mach trim may be inoperative or operate erratically. Disengage Mach trim if erratic stabilizer motion is observed. 8. Using the FD/autopilot in PTCH, ALT, HDG and ROLL modes will help reduce workload. 9. Rudder Travel Limiter (RTL) display on EICAS synoptic will display actual RTL limits even if RTL goal posts are amber. These limits may be inappropriate for the phase of flight. 

## CAUTION 1. Do not use any FD/autopilot SPEED mode. 2. Rudder travel limits may be inappropriate for phase of flight. For cruise and descent flight, excessive rudder input may result in unacceptable handling characteristics or exceedence of structural limits. For approach, landing and go-around flight, rudder authority may be limited. Differential thrustand aileron input may be required to assist in maintaining directional control. Select a runway with minimum cross-wind. (11) When the airplane is stabilized, proceed to EVALUATION within this section to regain use of PFD / airspeed if possible. 

### EMERGENCY PROCEDURES Unreliable Airspeed 03 − 19 − 5 Rev. 10, Dec 22/2014

DOT Approved 

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### EVALUATION (1) AIR DATA source selector ....................................................................... Select to NORM (2) Both PFDs and standby airspeed indicator / ISI ..........................................................................................................Compare airspeed (3) Determine which of the following conditions apply: If no indicated airspeed is considered reliable, proceed to CONDITION D . If both PFDs agree and the indicated airspeed is considered reliable, proceed to CONDITION A . If one PFD and standby airspeed indicator / ISI agree and the indicated airspeed is considered reliable, proceed to CONDITION B . If only one indicated airspeed is considered reliable, proceed to CONDITION C . 

## WARNING An airspeed should be considered reliable only if it is consistent with pitch, thrust and external noise and is consistent with the expected airspeed from Table A. CONDITION A – If both PFDs agree and the indicated airspeed is consistent with pitch, thrust and external noise, and the expected airspeed from Table A: (4) Use airspeed/altitude information per normal operations. (5) Accomplish remaining CAS messages. CONDITION B – If one PFD and standby airspeed indicator / ISI agree and the indicated airspeed is consistent with pitch, thrust and external noise, and the expected airspeed from Table A: (4) Autopilot ............................................................................................................Disengage (5) FDs ....................................................................................................................... Deselect (6) AIR DATA source selector ..............................................................Select to reliable side. (7) FDs ....................................................................................................... Engage, if desired . (8) Autopilot ............................................................................................... Engage, if desired. (9) Use airspeed/altitude information per normal operations. (10) Accomplish remaining CAS messages. 

### EMERGENCY PROCEDURES Unreliable Airspeed 03 − 19 − 6 Rev. 10, Dec 22/2014

DOT Approved 

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### CONDITION C – If only one indicated airspeed is consistent with pitch, thrust and external noise, and the expected airspeed from Table A: 

## WARNING Do not rely on only one airspeed unless it is in agreement with the expected airspeed column in Table A. Standby airspeed indicator / ISI is identified as reliable airspeed source: (4) Use airspeed/altitude information per normal operations. (5) Accomplish remaining CAS messages. One PFD is identified as reliable airspeed source: (4) Autopilot ............................................................................................................Disengage (5) FDs ....................................................................................................................... Deselect (6) AIR DATA source selector ..............................................................Select to reliable side. (7) FDs ....................................................................................................... Engage, if desired . (8) Autopilot ............................................................................................... Engage, if desired. (9) Use airspeed/altitude information per normal operations. (10) Accomplish remaining CAS messages. 

### EMERGENCY PROCEDURES Unreliable Airspeed 03 − 19 − 7 Rev. 10, Dec 22/2014

DOT Approved 

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### CONDITION D – If no indicated airspeed is consistent with pitch, thrust and external noise, and the expected airspeed from Table A: (4) Airspeed indications ............................................................................................Disregard (5) Pitch/N 1 

### .................................................................................................................Maintain (6) Land at the nearest suitable airport. NOTE 1. If environmental conditions (heavy rain, icing, ice crystals, volcanic ash, etc) are suspected to have caused unreliable airspeed, exit conditions as soon as possible, including descent, if required. 2. Plan to recover to an airfield with an ILS, under Visual Meteorological Conditions if possible. 3. The following may be unreliable: Ground proximity warning, Enhanced ground proximity warning, <2040> 

### Windshear detection, Flap overspeed, NOSE DOOR OPEN warning message Automatic function of passenger signs. 

## CAUTION If at any time down to and including minimum safe altitude, it is suspected that a reliable airspeed source may be available, restart the Unreliable Airspeed In-flight procedure in order to confirm airspeed. (7) Actual landing distance ........................................................................................ Increase Without Thrust Reversers With Thrust Reversers 1.25 (25%) 1.20 (20%) (8) When ready for descent, proceed to RECOVERY TO AN AIRPORT within this section. 

### EMERGENCY PROCEDURES Unreliable Airspeed 03 − 19 − 8 Rev. 10, Dec 22/2014

DOT Approved 

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### RECOVERY TO AN AIRPORT When ready to commence descent: 

## CAUTION Rudder travel limits may be inappropriate for phase of flight. For cruise and descent flight, excessive rudder input may result in unacceptable handling characteristics or exceedence of structural limits. For approach, landing and go-around flight, rudder authority may be limited. Differential thrust and aileron input may be required to assist in maintaining directional control. Select a runway with minimum cross-wind. (1) Pitch ...................................................................... Adjust as per Table B, and continue to adjust pitch during descent: Table B – Descent – FLAPS 0 – IDLE Altitude (ft) 0 5000 10000 15000 20000 25000 30000 35000 40000 Pitch (degree) − 2.5 − 2.5 − 3.0 − 3.5 − 3.5 − 3.5 − 3.0 − 3.0 − 2.0 (2) Thrust levers .............................................................................................................. I DLE NOTE With anti-ice ON, increase N 1 

### if required to obtain the minimum N 2 

### of 75% For an N 1 

### increase of 5%, add 0.5 degree to the pitch from Table B. For an N 1 

### increase of 10%, add 1.0 degree to the pitch from Table B. For an N 1 

### increase of 15%, add 1.5 degree to the pitch from Table B. 

## CAUTION Do not extend flaps until directed later in the procedure. The range of airspeeds possible in Table B could result in a significant flap overspeed and flap damage. The aircraft must be leveled off and slowed down before flaps can be extended. NOTE Plan to intercept a long final to allow time to re-configure for approach/landing and set pitch/N 1 

### . If intermediate level off is required during the descent: 

### EMERGENCY PROCEDURES Unreliable Airspeed 03 − 19 − 9 Rev. 10, Dec 22/2014

DOT Approved 

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### (3) Pitch/N 1 

### ........................................................ Set as per Table C, then adjust pitch to stop climb/descent. Table C – Level Flight – Cruise FLAPS 0 ALT (ft) Target Weight kg (lb) Expected Indicated Airspeed/ Mach 20412 (45000) 22680 (50000) 24948 (55000) 27216 (60000) 29484 (65000) KIAS/M 35000 Pitch (degree) 0.0 0.0 0.5 0.5 0.5 230 to 275 .69 to .81 N 1 

### (%) 78.2 78.9 79.6 80.3 81.1 30000 Pitch (degree) − 0.5 − 0.5 0.0 0.0 0.5 250 to 290 – N 1 

### (%) 77.6 78.0 78.4 79.0 79.6 25000 Pitch (degree) − 1.0 − 0.5 0.0 0.0 0.5 250 to 290 – N 1 

### (%) 74.0 74.5 74.9 75.5 76.2 20000 Pitch (degree) − 1.0 − 0.5 0.0 0.0 0.5 250 to 290 – N 1 

### (%) 70.4 70.8 71.2 71.8 72.5 15000 Pitch (degree) − 1.0 − 0.5 0.0 0.0 0.5 250 to 290 – N 1 

### (%) 66.0 67.3 67.9 68.3 68.7 If any indicated speed is outside the expected indicated airspeed range, it should be considered UNRELIABLE. 

### EMERGENCY PROCEDURES Unreliable Airspeed 03 − 19 − 10 Rev. 10, Dec 22/2014

DOT Approved 

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### Table C – Level Flight – Cruise FLAPS 0 (continued) ALT (ft) Target Weight kg (lb) Expected Indicated Airspeed/ Mach 31751 (70000) 34019 (75000) 36287 (80000) 38329 (84500) – KIAS/M 35000 Pitch (degree) 1.0 1.0 1.0 1.0 – 230 to 275 .69 to .81 N 1 

### (%) 82.0 82.9 84.1 85.7 – 30000 Pitch (degree) 0.5 1.0 1.0 1.5 – 250 to 290 – N 1 

### (%) 80.4 81.2 81.8 82.7 – 25000 Pitch (degree) 0.5 1.0 1.0 1.5 – 250 to 290 – N 1 

### (%) 76.9 77.8 78.5 79.3 – 20000 Pitch (degree) 0.5 1.0 1.5 1.5 – 250 to 290 – N 1 

### (%) 73.2 73.9 74.6 75.4 – 15000 Pitch (degree) 0.5 1.0 1.5 1.5 – 250 to 290 – N 1 

### (%) 69.3 70.2 70.9 71.7 – If any indicated speed is outside the expected indicated airspeed range, it should be considered UNRELIABLE. For continued descent: (3) Pitch ................................................................................................Adjust as per Table D: Table D – Descent – FLAPS 0 – IDLE Altitude (ft) 0 5000 10000 15000 20000 25000 30000 35000 40000 Pitch (degree) − 2.5 − 2.5 − 3.0 − 3.5 − 3.5 − 3.5 − 3.0 − 3.0 − 2.0 At initial approach altitude: (4) Pitch/N 1 

### ........................................................ Set as per Table E, then adjust pitch to stop climb/descent. 

### EMERGENCY PROCEDURES Unreliable Airspeed 03 − 19 − 11 Rev. 10, Dec 22/2014

DOT Approved 

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### Table E – Level Flight – Approach FLAPS 0 ALT (ft) Target Weight kg (lb) Expected Indicated Airspeed KIAS 20412 (45000) 22680 (50000) 24948 (55000) 27216 (60000) 29484 (65000) 15000 Pitch (degree) 0.5 1.0 1.5 2.0 2.5 210 to 230

N 1 

### (%) 58.7 59.5 60.3 61.3 62.4 10000 Pitch (degree) 0.5 1.0 1.5 2.0 2.5 210 to 230

N 1 

### (%) 55.1 55.9 56.7 57.6 58.7 5000 Pitch (degree) 0.5 1.0 1.5 2.0 2.5 210 to 230

N 1 

### (%) 51.8 52.5 53.3 54.1 55.2 0 Pitch (degree) 0.5 1.0 1.5 2.0 2.5 210 to 230

N 1 

### (%) 48.4 49.0 49.6 50.3 51.5 If any indicated speed is outside the expected indicated airspeed range, it should be considered UNRELIABLE. 

### EMERGENCY PROCEDURES Unreliable Airspeed 03 − 19 − 12 Rev. 10, Dec 22/2014

DOT Approved 

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### Table E – Level Flight – Approach FLAPS 0 (continued) ALT (ft) Target Weight kg (lb) Expected Indicated Airspeed KIAS 31751 (70000) 34019 (75000) 36287 (80000) 38329 (84500) – 15000 Pitch (degree) 3.0 3.0 3.5 4.0 – 210 to 230

N 1 

### (%) 63.9 65.5 67.1 68.6 – 10000 Pitch (degree) 3.0 3.0 3.5 4.0 – 210 to 230

N 1 

### (%) 60.2 61.9 63.3 64.7 – 5000 Pitch (degree) 3.0 3.0 3.5 4.0 – 210 to 230

N 1 

### (%) 56.4 58.0 59.3 60.6 – 0 Pitch (degree) 3.0 3.0 3.5 4.0 – 210 to 230

N 1 

### (%) 52.6 54.2 55.4 56.6 – If any indicated speed is outside the expected indicated airspeed range, it should be considered UNRELIABLE. NOTE

Allow sufficient time for stabilization prior to reconfiguring the airplane due to the pitch change as flaps are extended from 0 to 20. When stabilized: (5) FLAPS ............................................................................................................ Select to 20. (6) Pitch/N 1 

### .........................................................Set as per Table F, then adjust pitch to stop climb/descent. Table F – Approach (Level Flight) – FLAPS 20 – Gear UP Weight kg (lb) 20412 (45000) 22680 (50000) 24948 (55000) 27216 (60000) 29484 (65000) Pitch (degree) − 1.0 − 0.5 0.0 1.0 2.0 N 1 

### (%) 55.8 56.8 57.7 59.6 61.8 

### EMERGENCY PROCEDURES Unreliable Airspeed 03 − 19 − 13 Rev. 10, Dec 22/2014

DOT Approved 

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### Table F – Approach (Level Flight) – FLAPS 20 – Gear UP (continued) Weight kg (lb) 31751 (70000) 34019 (75000) 36287 (80000) 38329 (84500) – Pitch (degree) 2.5 3.5 4.0 4.5 – N 1 

### (%) 63.6 65.5 66.9 68.2 – NOTE Heading and ILS/VOR course deviation indicator information on the PFD are reliable and will aid situational awareness. (7) Final course .......................................................................................................... Intercept Upon intercept of final course (long final): (8) LDG GEAR lever ...........................................................................................................DN (9) FLAPS ............................................................................................................ Select to 30. (10) Pitch/N 1 

### ........................................................Set as per Table G, then adjust pitch to stop climb/descent. Table G – Approach (Level Flight) – FLAPS 30 – Gear DN Weight kg (lb) 20412 (45000) 22680 (50000) 24948 (55000) 27216 (60000) 29484 (65000) Pitch (degree) − 1.5 − 0.5 0.0 1.0 2.0 N 1 

### (%) 63.8 64.1 65.0 66.2 67.5 

### EMERGENCY PROCEDURES Unreliable Airspeed 03 − 19 − 14 Rev. 10, Dec 22/2014

DOT Approved 

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### Table G – Approach (Level Flight) – FLAPS 30 – Gear DN (continued) Weight kg (lb) 31751 (70000) 34019 (75000) 36287 (80000) 38329 (84500) – Pitch (degree) 3.0 4.0 5.0 6.0 – N 1 

### (%) 69.3 71.1 73.0 74.8 – 

## CAUTION Do not descend for final approach with flaps 30. The aircraft must remain level with gear down/flaps 30 or a flap overspeed and flap damage could result. Flaps 45 is selected at the start of the descent on the glideslope/glidepath. At glideslope capture or descent point: (11) FLAPS ............................................................................................................ Select to 45. (12) Pitch/N 1 

### ............................................................................................... Set as per Table H: Table H – Approach – FLAPS 45 – Gear DN – 3 degree G/S ALT (ft) Target Weight kg (lb) 20412 (45000) 22680 (50000) 24948 (55000) 27216 (60000) 29484 (65000) 15000 Pitch (degree) 0.5 0.5 0.5 1.0 1.0

N 1 

### (%) 59.9 62.6 65.5 67.4 69.6 10000 Pitch (degree) 0.5 0.5 0.5 1.0 1.0

N 1 

### (%) 55.9 58.5 60.9 63.2 65.5 5000 Pitch (degree) 0.5 0.5 0.5 1.0 1.0

N 1 

### (%) 52.1 54.7 57.0 59.2 61.4 0 Pitch (degree) 0.5 0.5 0.5 1.0 1.0

N 1 

### (%) 48.6 51.1 53.3 55.4 57.6 This table results in airspeeds equal to VREF 

### ± 10 kts. 

### EMERGENCY PROCEDURES Unreliable Airspeed 03 − 19 − 15 Rev. 10, Dec 22/2014

DOT Approved 

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### Table H – Approach – FLAPS 45 – Gear DN – 3 degree G/S (continued) ALT (ft) Target Weight kg (lb) 31751 (70000) 34019 (75000) 36287 (80000) 38329 (84500) – 15000 Pitch (degree) 1.0 1.0 1.0 1.0 –

N 1 

### (%) 71.8 74.0 75.9 78.0 – 10000 Pitch (degree) 1.0 1.0 1.0 1.0 –

N 1 

### (%) 67.6 69.7 71.5 73.6 – 5000 Pitch (degree) 1.0 1.0 1.0 1.0 –

N 1 

### (%) 63.5 65.6 67.4 69.4 – 0 Pitch (degree) 1.0 1.0 1.0 1.0 –

N 1 

### (%) 59.6 61.6 63.4 65.3 – This table results in airspeeds equal to VREF 

### ± 10 kts. (13) Pitch ......................................................................... Set to maintain glideslope/glidepath. (14) N 1 

### ...........................................................................Maintain as per Table H – Approach – FLAPS 45 – Gear DN – 3 degree G/S. 

### EMERGENCY PROCEDURES Unreliable Airspeed 03 − 19 − 16 Rev. 10, Dec 22/2014

DOT Approved 

### Airplane Flight Manual CSP C 012 PAGE PRINTED ON 9-22-201 5