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Airplane Flight Manual

BOMBARDIER GLOBAL EXPRESS · Maintenance Manual

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Overview

The document is the Airplane Flight Manual for the Bombardier Global Express (Model BD-700-1A10), detailing operational limitations, performance specifications, and maintenance guidelines. It includes revisions and updates to ensure compliance with safety and operational standards.

  • The manual is for Bombardier Global Express Model BD-700-1A10.
  • It includes revisions up to August 16, 2021.
  • The maximum takeoff weight (MTOW) options range from 42,411 kg to 45,132 kg.
  • The document is published by Bombardier Aerospace.
  • Technical assistance is available through a customer services hotline.
  • The manual must be operated in compliance with prescribed limitations.
  • It includes emergency and non-normal procedures.
  • The manual is subject to updates and revisions.

Document

Source

Originally published by regulations.gov. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

View original at regulations.gov

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Document details

Type
·
Maintenance Manual
Year
·
2021
File size
·
7.3 MB
Publisher
·
regulations.gov
Language
·
en

Specifications & performance

Extracted from this document.

Specifications

Mtow kg
·
42,411 to 45,132
Mtow (lb)
·
93,500 to 99,500
About this document
What is the Airplane Flight Manual?

The Airplane Flight Manual is a maintenance manual for the BOMBARDIER GLOBAL EXPRESS, dated 2021.

Where does the Airplane Flight Manual come from?

This copy of the Airplane Flight Manual was originally published by regulations.gov and is hosted on Sprinkle as a free, searchable reference copy.

What year was the Airplane Flight Manual published?

The Airplane Flight Manual — the BOMBARDIER GLOBAL EXPRESS maintenance manual on file — is dated 2021.

Documentation completeness
2/7

Most owners only have the POH. Here's the essential set for the BOMBARDIER GLOBAL EXPRESS.

  • Pilot's Operating Handbook / AFM
  • Checklist
  • Maintenance Manual
  • Parts Catalog (IPC)
  • Systems & Wiring
  • Service Bulletins on file
  • Type Certificate (TCDS)
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In this document

Record of Revisions

This section lists the revisions made to the manual, including dates and page numbers for updates.

Emergency Procedures

Details the procedures to follow in case of an emergency during flight.

Non-Normal Procedures

Outlines procedures to follow for non-standard situations that may arise during flight.

Performance

Provides information on the aircraft's performance metrics, including speeds and operational limits.

Technical Assistance

Offers contact information for technical support and assistance for in-flight emergencies.

Limitations

Specifies the operational limitations that must be adhered to while flying the aircraft.

Safety notes

  • The airplane must be operated in compliance with the limitations prescribed herein.
  • Consult the Terms and Conditions before using the manual.
  • Technical assistance is available for in-flight emergencies.

Full document text

Airplane Flight Manual BD−700−1A10 9002 thru 9174 incorporating SB 700−31−025 − BATCH 2+ IAC UPGRADE, and 9175 thru 9312, 9314 thru 9380, 9384 thru 9429 FIRST ISSUED: Aug 28/1998 REVISION 109: Aug 16/2021 Publication No. CSP 700−1A The Airplane must be operated in compliance with the LIMITATIONS prescribed herein. MODEL A/C EFFECTIVITY 42,411 kg / 93,500 lb MTOW or 43,091 kg / 95,000 lb MTOW or 43,545 kg / 96,000 lb MTOW or 44,452 kg / 98,000 lb MTOW or 45,132 kg / 99,500 lb MTOW GLOBAL EXPRESS* (MODEL BD−700−1A10) AIRPLANE FLIGHT MANUAL − CSP 700−1A Consult the Terms and Conditions by signing in to the Customer Portal (https://businessaircraft.bombardier.com/en) and navigating to LIBRARY −> Technical Publications −> Technical Publication Terms and Condition. Customer Services Hotline (Technical Assistance & In−flight Emergencies) North America: 1−866−JET−1247 (1−866−538−1247) International: +1−514−855−2999 Email: ac.yul@aero.bombardier.com User Comments (Technical Publications) North America: 1−866−JET−1247 (1−866−538−1247) International: +1−514−855−2999 Email: bbad.user.comments@aero.bombardier.com Ordering & Distribution (Technical Publications) North America: 1−866−JET−1247 (1−866−538−1247) International: +1−514−855−2999 Facsimile: 514−855−2770 Email: bbad.pubs.dist@aero.bombardier.com GL 700 AFM−1A Copyright © 1998−2021 by Bombardier Inc. All rights reserved. *Trademark of Bombardier Inc. or its subsidiaries. Printed in Canada Bombardier Aerospace P.O. Box 6087, Station Centre−ville Montreal, Quebec, Canada H3C 3G9 For more information regarding Technical Publications please contact: Bombardier Customer Services Business Aircraft To ease the ordering process, the following Document Identification Number should be used: Record of Revisions 00−01−101−−102 List of Effective Pages 00−03−1 to 00−03−10 00−03−1 to 00−03−10 Emergency Procedures 03−13−1 03−13−1 Non−Normal Procedures 05−00−12 05−00−12 05−04−4 to 05−04−6 05−04−4 to 05−04−6 05−15−11 to 05−15−14 05−15−11 to 05−15−14 Performance 06−00−4 06−00−4 06−00−7 06−00−7 06−03−11 to 06−03−12 06−03−11 to 06−03−12 06−03−31 06−03−31 06−07−3 to 06−07−8 06−07−3 to 06−07−8 06−08−2 06−08−2 06−08−5 06−08−5 06−08−7 06−08−7 Supplements 07−03−00−1 to 07−03−00−3 07−03−00−1 to 07−03−00−3 07−03−01−2 to 07−03−01−4 07−03−01−2 to 07−03−01−4 07−03−01−6 07−03−01−6 07−03−01−8 07−03−01−8 07−03−01−16 07−03−01−16 07−03−01−18 07−03−01−18 07−03−01−20 07−03−01−20 07−03−01−22 07−03−01−22 07−03−01−32 07−03−01−32 07−03−01−34 07−03−01−34 07−03−01−36 07−03−01−36 07−03−01−38 07−03−01−38 07−03−01−48 07−03−01−48 07−03−01−50 07−03−01−50 07−03−01−52 07−03−01−52 07−03−01−54 07−03−01−54 07−03−01−63 to 07−03−01−68 07−03−01−63 to 07−03−01−68 07−05−01−4 to 07−05−01−6 07−05−01−4 to 07−05−01−6 07−20−01−1 07−20−01−1 07−20−01−63 07−20−01−63 This is revision 109 to the Airplane Flight Manual, CSP 700−1A. To bring this manual up to date remove old pages and insert revised pages as detailed below: Revision 108 Revision 109 REV 109, Aug 16, 2021 Airplane Flight Manual CSP 700−1A Page 1 TRANSMITTAL LETTER REMOVE INSERT Title Page NOTE Record the date you insert this revision in the Record of Revisions at the front of the manual. 07−20−01−99 07−20−01−99 07−20−01−101 07−20−01−101 07−22−01−3 07−22−01−3 NOTE Page 07−20−01−1 is reisssued due to changes in the publishing software attributes. However, the data remains unchanged. REV 109, Aug 16, 2021 Airplane Flight Manual CSP 700−1A Page 2 TRANSMITTAL LETTER REMOVE INSERT Title Aug 16, 2021 TC Approval Page Aug 28, 1998 FAA Approval Page Dec 15, 1998 JAA Approval Page Sep 17, 1999 DNA Approval Page May 01, 2007 ANAC Approval Page Jul 15, 2009 CAAC Approval Page Apr 20, 2010 00−01 −1 Dec 01, 2003 −2 Dec 01, 2003 −3 Dec 01, 2003 −4 Dec 01, 2003 −5 Dec 01, 2003 −6 Dec 01, 2003 −7 Dec 01, 2003 −8 Dec 01, 2003 −9 Dec 01, 2003 −10 Dec 01, 2003 −11 Dec 01, 2003 −12 Dec 01, 2003 −13 Dec 01, 2003 −14 Dec 01, 2003 −15 Dec 01, 2003 −16 Dec 01, 2003 −17 Dec 01, 2003 −18 Dec 01, 2003 −19 Dec 01, 2003 −20 Dec 01, 2003 −21 Dec 01, 2003 −22 Dec 01, 2003 −23 Dec 01, 2003 −24 Dec 01, 2003 −25 Dec 01, 2003 −26 Dec 01, 2003 −27 Dec 01, 2003 −28 Dec 01, 2003 −29 Dec 01, 2003 −30 Dec 01, 2003 −31 Dec 15, 2003 −32 Jul 08, 2004 −33 Jul 08, 2004 −34 Nov 26, 2004 −35 Nov 26, 2004 −36 Nov 26, 2004 −37 Nov 26, 2004 −38 Dec 22, 2004 −39 Jan 21, 2005 −40 Apr 25, 2005 −41 Jul 21, 2005 −42 Feb 24, 2006 −43 Dec 01, 2005 −44 Feb 24, 2006 −45 Apr 17, 2006 −46 Aug 14, 2006 −47 Aug 14, 2006 −48 Nov 10, 2006 −49 Nov 10, 2006 −50 Nov 10, 2006 −51 Nov 10, 2006 −52 Jan 29, 2007 −53 Jun 15, 2007 −54 Sep 14, 2007 −55 Feb 11, 2008 −56 Feb 11, 2008 −57 Feb 11, 2008 −58 Apr 11, 2008 −59 Apr 11, 2008 −60 Apr 11, 2008 −61 Sep 29, 2008 −62 Sep 29, 2008 −63 Sep 29, 2008 −64 Feb 27, 2009 −65 Jul 10, 2009 −66 Sep 16, 2009 −67 Sep 16, 2009 −68 Dec 22, 2009 −69 Mar 12, 2010 −70 May 26, 2010 −71 Aug 03, 2010 −72 Aug 03, 2010 −73 Nov 09, 2010 −74 May 24, 2011 −75 May 18, 2012 −76 Jun 03, 2014 −77 Jun 03, 2014 −78 Sep 10, 2013 −79 Sep 10, 2013 −80 Nov 19, 2013 −81 Mar 03, 2014 −82 Jun 03, 2014 −83 Aug 29, 2014 −84 Nov 26, 2014 −85 Feb 16, 2015 −86 Feb 16, 2015 −87 May 11, 2015 −88 Nov 04, 2015 −89 Nov 04, 2015 −90 Nov 04, 2015 −91 Feb 10, 2016 −92 Feb 10, 2016 −93 May 04, 2016 −94 Oct 27, 2016 −95 Feb 06, 2018 −96 Jul 31, 2018 −97 Feb 07, 2019 −98 Feb 21, 2020 −99 Nov 11, 2020 −100 May 19, 2021 −101 Aug 16, 2021 −102 Aug 16, 2021 00−02 −1 Feb 09, 2011 −2 Feb 09, 2011 −3 Feb 09, 2011 −4 Feb 09, 2011 −5 Feb 09, 2011 −6 Feb 09, 2011 −7 Feb 09, 2011 −8 Feb 09, 2011 −9 Feb 09, 2011 −10 Feb 09, 2011 −11 Feb 09, 2011 −12 Aug 17, 2012 −13 Feb 06, 2018 −14 Feb 06, 2018 −15 Feb 06, 2018 −16 Feb 06, 2018 −17 Feb 06, 2018 −18 Feb 21, 2020 00−03 −1 Aug 16, 2021 −2 Aug 16, 2021 −3 Aug 16, 2021 −4 Aug 16, 2021 −5 Aug 16, 2021

Show full text

−6 Aug 16, 2021 −7 Aug 16, 2021 −8 Aug 16, 2021 DOT Approved REV 109, Aug 16, 2021 Airplane Flight Manual CSP 700−1A 00−03−1 LIST OF EFFECTIVE PAGES Page Date Page Date Page Date −9 Aug 16, 2021 −10 Aug 16, 2021 01−00 −1 May 24, 2011 −2 Dec 01, 2003 01−01 −1 Mar 12, 2010 −2 May 24, 2011 −3 Nov 26, 2014 −4 Nov 26, 2014 −5 May 24, 2011 −6 May 24, 2011 −7 May 24, 2011 −8 May 24, 2011 −9 May 24, 2011 −10 May 24, 2011 −11 May 24, 2011 −12 May 24, 2011 −13 May 24, 2011 −14 May 24, 2011 −15 Sep 10, 2013 −16 Jun 03, 2014 −17 Jun 03, 2014 −18 Jul 29, 2016 −19 Jan 30, 2017 −20 May 24, 2011 02−00 −1 May 04, 2016 −2 May 21, 2020 −3 Jul 31, 2018 −4 Jul 31, 2018 02−01 −1 Nov 09, 2010 −2 Dec 01, 2003 02−02 −1 May 04, 2016 −2 May 04, 2016 −3 May 04, 2016 −4 Sep 10, 2013 02−03 −1 Sep 16, 2009 −2 Aug 06, 2015 −3 May 04, 2016 −4 May 04, 2016 −5 May 04, 2016 −6 May 04, 2016 −7 Aug 06, 2015 −8 May 04, 2016 −9 May 04, 2016 −10 May 04, 2016 −11 May 04, 2016 −12 Sep 10, 2013 02−04 −1 Nov 10, 2006 −2 Aug 06, 2015 −3 May 26, 2010 −4 Feb 07, 2019 −5 May 19, 2021 −6 Nov 10, 2006 02−05 −1 May 21, 2020 −2 Dec 01, 2003 −3 Dec 01, 2003 −4 Dec 01, 2003 −5 Jan 21, 2005 −6 Jan 21, 2005 −7 Aug 17, 2012 −8 May 21, 2020 −9 May 21, 2020 −10 May 21, 2020 −11 May 21, 2020 −12 Jun 15, 2007 −13 Jun 15, 2007 −14 Jun 15, 2007 02−06 −1 Nov 26, 2004 −2 Nov 26, 2004 −3 Jul 31, 2018 −4 Jul 31, 2018 −5 Jul 31, 2018 −6 Jul 31, 2018 02−07 −1 Dec 01, 2003 −2 Dec 01, 2003 02−08 −1 Feb 22, 2021 −2 Jul 29, 2016 −3 Sep 18, 2017 −4 May 11, 2015 02−09 −1 Jul 29, 2016 −2 Jul 29, 2016 −3 Jul 29, 2016 −4 Jul 29, 2016 −5 Sep 18, 2017 −6 Jul 29, 2016 −7 Jul 29, 2016 −8 Jul 29, 2016 −9 Jul 29, 2016 −10 Jul 29, 2016 −11 Jul 29, 2016 −12 Jul 29, 2016 −13 Jul 29, 2016 −14 Mar 04, 2013 03−00 −1 Feb 22, 2021 −2 Feb 22, 2021 −3 Feb 21, 2020 −4 Jul 08, 2004 03−01 −1 Nov 09, 2010 −2 Nov 09, 2010 03−02 −1 Sep 10, 2013 −2 Jul 08, 2004 03−03 −1 Sep 10, 2013 −2 Nov 09, 2010 −3 Jun 03, 2014 −4 Feb 16, 2015 −5 May 11, 2015 −6 Feb 06, 2018 −7 Feb 06, 2018 −8 May 11, 2015 −9 May 11, 2015 −10 May 11, 2015 −11 May 11, 2015 −12 May 11, 2015 −13 Feb 22, 2021 −14 Feb 22, 2021 −15 Feb 22, 2021 −16 May 11, 2015 03−04 −1 Feb 10, 2016 −2 Feb 10, 2016 −3 Feb 10, 2016 −4 Feb 10, 2016 −5 Feb 10, 2016 −6 Feb 10, 2016 −7 Feb 10, 2016 −8 Feb 27, 2009 03−05 −1 Feb 10, 2016 −2 Feb 10, 2016 −3 Feb 10, 2016 −4 Feb 10, 2016 −5 Feb 10, 2016 −6 Nov 09, 2010 DOT Approved REV 109, Aug 16, 2021 Airplane Flight Manual CSP 700−1A 00−03−2 LIST OF EFFECTIVE PAGES Page Date Page Date Page Date 03−06 −1 Nov 09, 2010 −2 Jul 08, 2004 03−07 −1 Feb 10, 2016 −2 Feb 10, 2016 −3 Feb 10, 2016 −4 Feb 10, 2016 −5 Feb 10, 2016 −6 Feb 10, 2016 03−08 −1 Feb 10, 2016 −2 Jul 08, 2004 03−09 −1 Nov 30, 2011 −2 May 11, 2015 −3 May 11, 2015 −4 May 11, 2015 −5 May 11, 2015 −6 May 11, 2015 −7 May 11, 2015 −8 May 11, 2015 −9 May 11, 2015 −10 May 11, 2015 03−10 −1 Jun 03, 2014 −2 May 11, 2015 −3 May 11, 2015 −4 May 11, 2015 03−11 −1 Sep 29, 2008 −2 Sep 29, 2008 03−12 −1 May 21, 2020 −2 May 21, 2020 −3 May 21, 2020 −4 May 21, 2020 −5 May 21, 2020 −6 May 21, 2020 −7 May 21, 2020 −8 May 21, 2020 −9 May 21, 2020 −10 May 21, 2020 −11 May 21, 2020 −12 May 21, 2020 −13 May 21, 2020 −14 May 21, 2020 −15 May 21, 2020 −16 May 21, 2020 −17 May 21, 2020 −18 May 21, 2020 −19 May 21, 2020 −20 May 21, 2020 −21 May 21, 2020 −22 May 21, 2020 −23 May 21, 2020 −24 May 21, 2020 −25 May 21, 2020 −26 May 21, 2020 −27 May 21, 2020 −28 Feb 21, 2020 03−13 −1 Aug 16, 2021 −2 Jul 08, 2004 −3 Feb 16, 2015 −4 May 24, 2011 03−14 −1 Jul 29, 2016 −2 Mar 03, 2014 04−00 −1 Jan 30, 2017 −2 Dec 01, 2003 04−01 −1 Feb 24, 2006 −2 Dec 01, 2003 04−02 −1 Jan 30, 2017 −2 Jan 30, 2017 −3 Jan 30, 2017 −4 Jan 30, 2017 −5 May 06, 2019 −6 May 03, 2018 −7 May 06, 2019 −8 May 06, 2019 −9 Nov 11, 2020 −10 Nov 11, 2020 05−00 −1 Feb 10, 2016 −2 Jul 31, 2018 −3 Feb 07, 2019 −4 Feb 07, 2019 −5 Feb 07, 2019 −6 Jul 31, 2018 −7 Jul 31, 2018 −8 Jul 31, 2018 −9 Jul 31, 2018 −10 Jul 31, 2018 −11 Jul 31, 2018 −12 Aug 16, 2021 05−01 −1 Nov 09, 2010 −2 Jul 08, 2004 05−02 −1 Aug 06, 2015 −2 Jun 03, 2014 −3 May 04, 2016 −4 May 04, 2016 −5 Sep 10, 2013 −6 May 04, 2016 −7 May 06, 2019 −8 Feb 10, 2016 05−03 −1 Aug 14, 2006 −2 Sep 29, 2008 −3 Aug 29, 2014 −4 Jul 08, 2004 −5 May 24, 2011 −6 May 24, 2011 −7 Jun 03, 2014 −8 Feb 16, 2015 −9 May 11, 2015 −10 May 11, 2015 −11 May 24, 2011 −12 Feb 07, 2019 −13 Feb 07, 2019 −14 Aug 03, 2010 05−04 −1 Jan 29, 2007 −2 Jul 08, 2004 −3 Jul 31, 2018 −4 Aug 16, 2021 −5 Aug 16, 2021 −6 Aug 16, 2021 −7 Jul 31, 2018 −8 Feb 07, 2019 −9 Feb 07, 2019 −10 Feb 07, 2019 −11 Jul 31, 2018 −12 Jul 31, 2018 05−05 −1 Jul 29, 2016 −2 Jul 29, 2016 −3 Jul 29, 2016 −4 Aug 17, 2020 −5 May 03, 2018 −6 Mar 04, 2013 05−06 −1 Nov 10, 2006 −2 Nov 19, 2013 −3 Nov 19, 2013 DOT Approved REV 109, Aug 16, 2021 Airplane Flight Manual CSP 700−1A 00−03−3 LIST OF EFFECTIVE PAGES Page Date Page Date Page Date −4 Feb 10, 2016 05−07 −1 Sep 16, 2009 −2 Aug 29, 2014 −3 Sep 16, 2009 −4 Nov 26, 2004 05−08 −1 Dec 20, 2012 −2 Feb 16, 2015 −3 Dec 20, 2012 −4 May 11, 2015 −5 May 11, 2015 −6 May 11, 2015 −7 May 11, 2015 −8 May 11, 2015 −9 May 11, 2015 −10 May 11, 2015 −11 May 11, 2015 −12 May 11, 2015 −13 May 11, 2015 −14 May 11, 2015 −15 May 11, 2015 −16 Aug 03, 2010 05−09 −1 Feb 16, 2015 −2 Sep 29, 2008 −3 Feb 11, 2008 −4 Feb 11, 2008 05−10 −1 May 24, 2011 −2 May 24, 2011 −3 May 24, 2011 −4 Jul 31, 2018 −5 Oct 25, 2018 −6 Jul 31, 2018 −7 May 11, 2015 −8 May 11, 2015 −9 Jul 31, 2018 −10 Jul 31, 2018 −11 Jul 31, 2018 −12 May 11, 2015 −13 May 11, 2015 −14 Feb 06, 2018 −15 Jul 31, 2018 −16 Feb 06, 2018 −17 Feb 06, 2018 −18 May 11, 2015 −19 Jul 31, 2018 −20 Jul 31, 2018 −21 May 11, 2015 −22 May 11, 2015 −23 Feb 06, 2018 −24 Feb 06, 2018 −25 May 11, 2015 −26 May 11, 2015 −27 May 11, 2015 −28 May 11, 2015 −29 May 11, 2015 −30 May 11, 2015 −31 May 11, 2015 −32 Feb 10, 2016 −33 May 11, 2015 −34 May 11, 2015 05−11 −1 Jul 08, 2004 −2 Aug 06, 2015 −3 Jun 03, 2014 −4 Aug 06, 2015 −5 Aug 06, 2015 −6 Jun 03, 2014 −7 Feb 27, 2009 −8 Aug 06, 2015 −9 Sep 10, 2013 −10 Sep 10, 2013 −11 Sep 10, 2013 −12 Aug 06, 2015 −13 Aug 06, 2015 −14 Aug 06, 2015 −15 Aug 06, 2015 −16 Aug 06, 2015 −17 Aug 06, 2015 −18 Aug 06, 2015 −19 Aug 06, 2015 −20 Aug 06, 2015 −21 Aug 06, 2015 −22 Aug 06, 2015 −23 Aug 06, 2015 −24 Aug 06, 2015 −25 Aug 06, 2015 −26 Aug 06, 2015 05−12 −1 May 11, 2015 −2 May 11, 2015 −3 May 11, 2015 −4 May 11, 2015 −5 Jul 31, 2018 −6 May 11, 2015 −7 May 11, 2015 −8 May 11, 2015 −9 May 11, 2015 −10 May 11, 2015 −11 May 11, 2015 −12 Feb 06, 2018 −13 Jul 31, 2018 −14 May 11, 2015 −15 May 11, 2015 −16 May 11, 2015 −17 May 11, 2015 −18 May 11, 2015 −19 May 11, 2015 −20 May 11, 2015 −21 May 11, 2015 −22 May 11, 2015 05−13 −1 May 11, 2015 −2 May 11, 2015 −3 May 11, 2015 −4 May 11, 2015 −5 May 11, 2015 −6 May 11, 2015 −7 May 11, 2015 −8 May 11, 2015 −9 May 11, 2015 −10 May 11, 2015 −11 May 11, 2015 −12 May 04, 2016 −13 May 04, 2016 −14 May 04, 2016 −15 May 04, 2016 −16 May 11, 2015 05−14 −1 Aug 14, 2006 −2 Aug 14, 2006 −3 Jun 03, 2014 −4 Aug 14, 2006 −5 Aug 14, 2006 −6 Aug 14, 2006 −7 Jun 03, 2014 −8 Jun 03, 2014 −9 Jun 03, 2014 −10 Jun 03, 2014 −11 Jun 03, 2014 −12 Jun 03, 2014 −13 Jun 03, 2014 −14 May 03, 2018 −15 May 03, 2018 −16 May 03, 2018 −17 May 03, 2018 −18 May 03, 2018 −19 May 03, 2018 DOT Approved REV 109, Aug 16, 2021 Airplane Flight Manual CSP 700−1A 00−03−4 LIST OF EFFECTIVE PAGES Page Date Page Date Page Date −20 May 03, 2018 −21 May 03, 2018 −22 Jul 31, 2018 −23 Jul 31, 2018 −24 May 03, 2018 05−15 −1 May 11, 2015 −2 May 11, 2015 −3 May 11, 2015 −4 May 11, 2015 −5 Jul 31, 2018 −6 Jul 31, 2018 −7 May 11, 2015 −8 May 11, 2015 −9 May 11, 2015 −10 May 11, 2015 −11 Aug 16, 2021 −12 Aug 16, 2021 −13 Aug 16, 2021 −14 Aug 16, 2021 05−16 −1 Mar 03, 2014 −2 Mar 03, 2014 −3 Mar 03, 2014 −4 Mar 03, 2014 05−17 −1 Dec 01, 2005 −2 Jul 08, 2004 06−00 −1 Jan 21, 2005 −2 May 11, 2015 −3 Nov 26, 2014 −4 Aug 16, 2021 −5 May 11, 2015 −6 May 11, 2015 −7 Aug 16, 2021 −8 Sep 16, 2009 06−01 −1 Dec 01, 2003 −2 Dec 01, 2003 −3 Dec 15, 2003 −4 Dec 01, 2003 −5 Dec 01, 2003 −6 Dec 01, 2003 −7 Dec 01, 2003 −8 Nov 09, 2010 −9 Jan 21, 2005 −10 Jan 21, 2005 −11 May 06, 2019 −12 Jan 21, 2005 −13 Jan 21, 2005 −14 Jan 21, 2005 −15 May 06, 2019 −16 Jan 21, 2005 −17 May 06, 2019 −18 Jan 21, 2005 −19 Jan 21, 2005 −20 Jan 21, 2005 −21 Jan 21, 2005 −22 Jan 21, 2005 −23 Jan 21, 2005 −24 Jan 21, 2005 −25 Jan 21, 2005 −26 Jan 21, 2005 −27 Jan 21, 2005 −28 Jan 21, 2005 −29 Jan 21, 2005 −30 Jan 21, 2005 −31 Jan 21, 2005 −32 Jan 21, 2005 −33 Jan 21, 2005 −34 Jan 21, 2005 06−02 −1 Dec 01, 2003 −2 Dec 01, 2003 −3 Dec 01, 2003 −4 Dec 01, 2003 −5 Dec 01, 2003 −6 Dec 01, 2003 −7 Dec 01, 2003 −8 Dec 01, 2003 −9 Dec 01, 2003 −10 Dec 01, 2003 −11 Dec 01, 2003 −12 Dec 01, 2003 −13 Dec 01, 2003 −14 Dec 01, 2003 −15 Dec 01, 2003 −16 Dec 01, 2003 06−03 −1 Sep 18, 2017 −2 Jun 03, 2014 −3 Jun 03, 2014 −4 Jun 03, 2014 −5 Jun 03, 2014 −6 Sep 18, 2017 −7 May 11, 2015 −8 May 11, 2015 −9 May 11, 2015 −10 May 11, 2015 −11 Aug 16, 2021 −12 Aug 16, 2021 −13 May 11, 2015 −14 May 11, 2015 −15 May 11, 2015 −16 May 11, 2015 −17 May 11, 2015 −18 May 11, 2015 −19 May 11, 2015 −20 May 11, 2015 −21 May 11, 2015 −22 May 11, 2015 −23 Sep 18, 2017 −24 May 11, 2015 −25 May 11, 2015 −26 May 11, 2015 −27 May 11, 2015 −28 Sep 18, 2017 −29 May 11, 2015 −30 May 11, 2015 −31 Aug 16, 2021 −32 May 11, 2015 −33 May 11, 2015 −34 May 11, 2015 −35 May 11, 2015 −36 May 11, 2015 −37 May 11, 2015 −38 May 11, 2015 −39 May 11, 2015 −40 May 11, 2015 −41 May 11, 2015 −42 May 11, 2015 −43 May 11, 2015 −44 May 11, 2015 06−04 −1 Dec 01, 2003 −2 Dec 01, 2003 −3 Dec 01, 2003 −4 Dec 01, 2003 −5 Dec 01, 2003 −6 Dec 01, 2003 −7 Dec 01, 2003 −8 Dec 01, 2003 −9 Dec 01, 2003 −10 Dec 01, 2003 −11 Dec 01, 2003 −12 Dec 01, 2003 −13 Dec 01, 2003 −14 Dec 01, 2003 −15 Feb 10, 2016 DOT Approved REV 109, Aug 16, 2021 Airplane Flight Manual CSP 700−1A 00−03−5 LIST OF EFFECTIVE PAGES Page Date Page Date Page Date −16 Feb 10, 2016 −17 Dec 01, 2003 −18 Dec 01, 2003 −19 Dec 01, 2003 −20 Dec 01, 2003 −21 Feb 10, 2016 −22 Feb 10, 2016 −23 Feb 10, 2016 −24 Dec 01, 2003 06−05 −1 Sep 18, 2017 −2 Nov 26, 2014 −3 Sep 18, 2017 −4 Nov 26, 2004 06−06 −1 Nov 26, 2014 −2 Nov 26, 2014 −3 Dec 01, 2003 −4 Dec 01, 2003 −5 Nov 26, 2004 −6 Dec 01, 2003 −7 Nov 26, 2014 −8 Nov 26, 2014 −9 Dec 01, 2003 −10 Dec 01, 2003 −11 Dec 01, 2003 −12 Dec 01, 2003 06−07 −1 Dec 20, 2012 −2 Dec 01, 2003 −3 Aug 16, 2021 −4 Aug 16, 2021 −5 Aug 16, 2021 −6 Aug 16, 2021 −7 Aug 16, 2021 −8 Aug 16, 2021 06−08 −1 Dec 01, 2003 −2 Aug 16, 2021 −3 Nov 26, 2004 −4 Sep 16, 2009 −5 Aug 16, 2021 −6 Nov 26, 2004 −7 Aug 16, 2021 −8 Nov 26, 2004 −9 Nov 26, 2004 −10 Nov 26, 2004 −11 Sep 16, 2009 −12 Feb 27, 2009 −13 Sep 16, 2009 −14 Dec 01, 2003 −15 Dec 01, 2003 −16 Dec 01, 2003 −17 Dec 01, 2003 −18 Dec 01, 2003 −19 Dec 01, 2003 −20 Dec 01, 2003 07−00−00 −1 May 24, 2017 −2 May 19, 2021 −3 May 24, 2017 −4 Sep 16, 2009 07−00−01 −1 May 24, 2017 −2 May 19, 2021 07−01−00 −1 Mar 03, 2014 −2 Dec 01, 2003 07−01−01 −1 May 24, 2017 −2 May 04, 2016 −3 May 04, 2016 −4 May 24, 2017 −5 May 24, 2017 −6 May 24, 2017 07−01A−00 −1 May 24, 2017 −2 May 24, 2017 07−01A−01 −1 May 24, 2017 −2 May 24, 2017 −3 May 24, 2017 −4 May 24, 2017 −5 May 24, 2017 −6 May 24, 2017 07−02−00 −1 Aug 01, 2019 −2 Aug 01, 2019 07−02−01 −1 Nov 26, 2004 −2 Nov 26, 2004 −3 Nov 26, 2004 −4 Nov 26, 2004 −5 Nov 26, 2004 −6 Nov 26, 2004 −7 Aug 01, 2019 −8 Aug 01, 2019 −9 Aug 01, 2019 −10 Aug 01, 2019 −11 Aug 01, 2019 −12 Aug 01, 2019 −13 Aug 01, 2019 −14 Aug 01, 2019 −15 Aug 01, 2019 −16 Aug 01, 2019 −17 Aug 01, 2019 −18 Aug 01, 2019 −19 Aug 01, 2019 −20 Aug 01, 2019 −21 Aug 01, 2019 −22 Aug 01, 2019 −23 Aug 01, 2019 −24 Aug 01, 2019 −25 Aug 01, 2019 −26 Aug 01, 2019 −27 Aug 01, 2019 −28 Aug 01, 2019 −29 Aug 01, 2019 −30 Aug 01, 2019 07−03−00 −1 Aug 16, 2021 −2 Aug 16, 2021 −3 Aug 16, 2021 −4 Sep 29, 2008 07−03−01 −1 Nov 26, 2014 −2 Aug 16, 2021 −3 Aug 16, 2021 −4 Aug 16, 2021 −5 Sep 29, 2008 −6 Aug 16, 2021 −7 Sep 29, 2008 −8 Aug 16, 2021 −9 Sep 29, 2008 −10 Sep 29, 2008 −11 Sep 29, 2008 −12 Sep 29, 2008 −13 Sep 29, 2008 −14 Sep 29, 2008 −15 Sep 18, 2017 −16 Aug 16, 2021 −17 Sep 29, 2008 −18 Aug 16, 2021 −19 Sep 29, 2008 −20 Aug 16, 2021 −21 Sep 29, 2008 −22 Aug 16, 2021 −23 Aug 03, 2010 −24 Sep 29, 2008 −25 Sep 29, 2008 DOT Approved REV 109, Aug 16, 2021 Airplane Flight Manual CSP 700−1A 00−03−6 LIST OF EFFECTIVE PAGES Page Date Page Date Page Date −26 Sep 29, 2008 −27 Sep 29, 2008 −28 Sep 29, 2008 −29 Sep 29, 2008 −30 Sep 29, 2008 −31 Sep 18, 2017 −32 Aug 16, 2021 −33 Sep 29, 2008 −34 Aug 16, 2021 −35 Sep 29, 2008 −36 Aug 16, 2021 −37 Sep 29, 2008 −38 Aug 16, 2021 −39 Sep 29, 2008 −40 Sep 29, 2008 −41 Sep 29, 2008 −42 Sep 29, 2008 −43 Sep 29, 2008 −44 Sep 29, 2008 −45 Sep 29, 2008 −46 Sep 29, 2008 −47 Sep 18, 2017 −48 Aug 16, 2021 −49 Sep 29, 2008 −50 Aug 16, 2021 −51 Sep 29, 2008 −52 Aug 16, 2021 −53 Sep 29, 2008 −54 Aug 16, 2021 −55 Sep 29, 2008 −56 Sep 29, 2008 −57 Sep 29, 2008 −58 Sep 29, 2008 −59 Sep 29, 2008 −60 Sep 29, 2008 −61 Sep 29, 2008 −62 Sep 29, 2008 −63 Aug 16, 2021 −64 Aug 16, 2021 −65 Aug 16, 2021 −66 Aug 16, 2021 −67 Aug 16, 2021 −68 Aug 16, 2021 07−04−00 −1 May 21, 2020 −2 Dec 01, 2003 07−04−01 −1 May 21, 2020 −2 May 21, 2020 07−05−00 −1 May 11, 2015 −2 Dec 01, 2003 07−05−01 −1 Sep 14, 2007 −2 May 11, 2015 −3 May 11, 2015 −4 Aug 16, 2021 −5 Aug 16, 2021 −6 Aug 16, 2021 −7 May 11, 2015 −8 May 11, 2015 −9 May 11, 2015 −10 May 11, 2015 −11 May 11, 2015 −12 May 11, 2015 −13 May 11, 2015 −14 May 11, 2015 −15 May 11, 2015 −16 May 11, 2015 −17 May 11, 2015 −18 May 11, 2015 −19 May 11, 2015 −20 May 11, 2015 −21 May 11, 2015 −22 May 11, 2015 −23 May 11, 2015 −24 May 11, 2015 07−06−00 −1 May 04, 2016 −2 Dec 01, 2003 07−06−01 −1 Feb 06, 2018 −2 Feb 06, 2018 −3 Sep 18, 2017 −4 Sep 18, 2017 −5 Sep 18, 2017 −6 Dec 01, 2003 −7 Dec 01, 2003 −8 Dec 01, 2003 −9 Jun 03, 2014 −10 Sep 18, 2017 −11 Dec 01, 2003 −12 Mar 03, 2014 −13 Sep 18, 2017 −14 Nov 26, 2004 −15 Nov 26, 2004 −16 Dec 01, 2003 07−07−00 −1 Jun 03, 2014 −2 Nov 26, 2004 07−07−01 −1 Jun 03, 2014 −2 Jun 03, 2014 −3 Aug 06, 2015 −4 Jun 03, 2014 −5 Jun 03, 2014 −6 Jun 03, 2014 07−08−00 −1 Feb 21, 2020 −2 Dec 01, 2003 07−08−01 −1 Nov 09, 2010 −2 Feb 21, 2020 07−09−00 −1 May 11, 2015 −2 Dec 01, 2003 07−09−01 −1 Mar 04, 2013 −2 Jul 29, 2016 −3 Aug 06, 2015 −4 Aug 06, 2015 −5 May 11, 2015 −6 Aug 06, 2015 −7 May 11, 2015 −8 May 11, 2015 −9 May 11, 2015 −10 May 11, 2015 −11 May 11, 2015 −12 May 11, 2015 07−10−00 −1 Aug 14, 2006 −2 Dec 01, 2003 07−10−01 −1 Aug 14, 2006 −2 Nov 10, 2006 −3 Aug 14, 2006 −4 Dec 01, 2003 07−11−00 −1 Nov 30, 2011 −2 Nov 30, 2011 07−11−01 −1 Sep 10, 2013 −2 Nov 30, 2011 07−12−00 −1 Sep 29, 2008 −2 Nov 26, 2004 07−12−01 −1 Nov 26, 2004 −2 Sep 29, 2008 −3 Sep 29, 2008 −4 Nov 26, 2004 DOT Approved REV 109, Aug 16, 2021 Airplane Flight Manual CSP 700−1A 00−03−7 LIST OF EFFECTIVE PAGES Page Date Page Date Page Date −5 Nov 26, 2004 −6 Sep 29, 2008 −7 Sep 29, 2008 −8 Sep 29, 2008 −9 Sep 29, 2008 −10 Sep 29, 2008 −11 Sep 29, 2008 −12 Sep 29, 2008 07−13−00 −1 Dec 01, 2003 −2 Dec 01, 2003 07−13−01 −1 Dec 01, 2003 −2 Sep 29, 2008 07−14−00 −1 Dec 15, 2003 −2 Dec 15, 2003 07−14−01 −1 Nov 09, 2010 −2 Dec 15, 2003 07−15−00 −1 May 08, 2009 −2 Dec 01, 2003 07−15−01 −1 May 08, 2009 −2 May 08, 2009 07−16−00 −1 Aug 06, 2015 −2 Sep 29, 2008 07−16−01 −1 Sep 29, 2008 −2 Sep 29, 2008 −3 Sep 29, 2008 −4 Sep 29, 2008 −5 Nov 26, 2014 −6 Nov 26, 2014 −7 Sep 29, 2008 −8 Sep 29, 2008 −9 Sep 29, 2008 −10 Nov 26, 2014 −11 Sep 29, 2008 −12 Sep 29, 2008 −13 Sep 29, 2008 −14 Sep 29, 2008 −15 Sep 29, 2008 −16 Sep 29, 2008 −17 Sep 29, 2008 −18 Sep 29, 2008 −19 Sep 29, 2008 −20 Sep 29, 2008 −21 Sep 29, 2008 −22 Sep 29, 2008 −23 Feb 10, 2016 −24 Feb 10, 2016 −25 Feb 10, 2016 −26 Sep 29, 2008 −27 Sep 29, 2008 −28 Jun 03, 2014 −29 Sep 29, 2008 −30 Sep 29, 2008 −31 Sep 29, 2008 −32 Sep 29, 2008 −33 Sep 29, 2008 −34 Sep 29, 2008 −35 Sep 29, 2008 −36 Sep 29, 2008 −37 Sep 29, 2008 −38 Sep 29, 2008 −39 Sep 29, 2008 −40 Sep 29, 2008 −41 Sep 29, 2008 −42 Sep 29, 2008 −43 Sep 29, 2008 −44 Sep 29, 2008 07−17−00 −1 Dec 01, 2003 −2 Dec 01, 2003 07−17−01 −1 Dec 01, 2003 −2 Dec 01, 2003 07−20−00 −1 Feb 21, 2020 −2 Feb 21, 2020 07−20−01 −1 Aug 16, 2021 −2 Aug 06, 2015 −3 May 11, 2015 −4 May 11, 2015 −5 May 11, 2015 −6 May 11, 2015 −7 May 11, 2015 −8 Feb 21, 2020 −9 Feb 21, 2020 −10 Feb 21, 2020 −11 Feb 21, 2020 −12 Feb 21, 2020 −13 Feb 21, 2020 −14 Feb 21, 2020 −15 Feb 21, 2020 −16 Feb 21, 2020 −17 Feb 21, 2020 −18 Feb 21, 2020 −19 Feb 21, 2020 −20 Feb 21, 2020 −21 Feb 21, 2020 −22 Feb 21, 2020 −23 Feb 21, 2020 −24 Feb 21, 2020 −25 Feb 21, 2020 −26 Feb 21, 2020 −27 Feb 21, 2020 −28 Feb 21, 2020 −29 Feb 21, 2020 −30 Feb 21, 2020 −31 Feb 21, 2020 −32 Feb 21, 2020 −33 Feb 21, 2020 −34 Feb 21, 2020 −35 Feb 21, 2020 −36 Feb 21, 2020 −37 Feb 21, 2020 −38 Feb 21, 2020 −39 Feb 21, 2020 −40 Feb 21, 2020 −41 Feb 21, 2020 −42 Feb 21, 2020 −43 Feb 21, 2020 −44 Feb 21, 2020 −45 Feb 21, 2020 −46 Feb 21, 2020 −47 Feb 21, 2020 −48 Feb 21, 2020 −49 Feb 21, 2020 −50 Feb 21, 2020 −51 Feb 21, 2020 −52 Feb 21, 2020 −53 Feb 21, 2020 −54 Feb 21, 2020 −55 Feb 21, 2020 −56 Feb 21, 2020 −57 Feb 21, 2020 −58 Feb 21, 2020 −59 Feb 21, 2020 −60 Feb 21, 2020 −61 Feb 21, 2020 −62 Feb 21, 2020 −63 Aug 16, 2021 −64 Feb 21, 2020 −65 Feb 21, 2020 −66 Feb 21, 2020 DOT Approved REV 109, Aug 16, 2021 Airplane Flight Manual CSP 700−1A 00−03−8 LIST OF EFFECTIVE PAGES Page Date Page Date Page Date −67 Feb 21, 2020 −68 Feb 21, 2020 −69 Feb 21, 2020 −70 Feb 21, 2020 −71 Feb 21, 2020 −72 Feb 21, 2020 −73 Feb 21, 2020 −74 Feb 21, 2020 −75 Feb 21, 2020 −76 Feb 21, 2020 −77 Feb 21, 2020 −78 Feb 21, 2020 −79 Feb 21, 2020 −80 Feb 21, 2020 −81 Feb 21, 2020 −82 Feb 21, 2020 −83 Feb 21, 2020 −84 Feb 21, 2020 −85 Feb 21, 2020 −86 Feb 21, 2020 −87 Feb 21, 2020 −88 Feb 21, 2020 −89 Feb 21, 2020 −90 Feb 21, 2020 −91 Feb 21, 2020 −92 Feb 21, 2020 −93 Feb 21, 2020 −94 Feb 21, 2020 −95 Feb 21, 2020 −96 Feb 21, 2020 −97 Feb 21, 2020 −98 Feb 21, 2020 −99 Aug 16, 2021 −100 Feb 21, 2020 −101 Aug 16, 2021 −102 Feb 21, 2020 −103 Feb 21, 2020 −104 Feb 21, 2020 −105 Feb 21, 2020 −106 Feb 21, 2020 07−21−00 −1 May 04, 2016 −2 Nov 10, 2006 07−21−01 −1 Feb 16, 2015 −2 May 04, 2016 −3 Nov 10, 2006 −4 Nov 26, 2014 −5 Nov 26, 2014 −6 Nov 10, 2006 07−22−00 −1 Nov 04, 2015 −2 Dec 01, 2005 07−22−01 −1 Feb 06, 2018 −2 Feb 06, 2018 −3 Aug 16, 2021 −4 Jun 03, 2014 −5 May 03, 2018 −6 Feb 06, 2018 −7 Sep 18, 2017 −8 Jun 03, 2014 −9 Jun 03, 2014 −10 Jun 03, 2014 −11 Jun 03, 2014 −12 Jun 03, 2014 07−24−00 −1 Apr 11, 2008 −2 Aug 06, 2015 07−24−01 −1 May 11, 2015 −2 Aug 06, 2015 −3 Sep 18, 2017 −4 Sep 18, 2017 −5 Apr 11, 2008 −6 Apr 11, 2008 −7 Apr 11, 2008 −8 Apr 11, 2008 −9 Apr 11, 2008 −10 Apr 11, 2008 −11 Sep 18, 2017 −12 May 11, 2015 −13 May 11, 2015 −14 Apr 11, 2008 −15 Apr 11, 2008 −16 Apr 11, 2008 −17 Apr 11, 2008 −18 Apr 11, 2008 −19 Apr 11, 2008 −20 Apr 11, 2008 −21 Apr 11, 2008 −22 Apr 11, 2008 −23 Apr 11, 2008 −24 Apr 11, 2008 −25 Apr 11, 2008 −26 Apr 11, 2008 −27 Apr 11, 2008 −28 Apr 11, 2008 −29 Apr 11, 2008 −30 Apr 11, 2008 −31 Apr 11, 2008 −32 Apr 11, 2008 −33 Feb 10, 2016 −34 Feb 10, 2016 −35 Apr 11, 2008 −36 Apr 11, 2008 −37 Feb 10, 2016 −38 Apr 11, 2008 −39 Apr 11, 2008 −40 Apr 11, 2008 −41 Apr 11, 2008 −42 Sep 29, 2008 −43 Apr 11, 2008 −44 Apr 11, 2008 −45 Sep 18, 2017 −46 Apr 11, 2008 −47 Apr 11, 2008 −48 Apr 11, 2008 −49 Apr 11, 2008 −50 Apr 11, 2008 −51 Apr 11, 2008 −52 Sep 18, 2017 −53 Apr 11, 2008 −54 Apr 11, 2008 −55 Sep 18, 2017 −56 May 11, 2015 −57 Aug 06, 2015 −58 Apr 11, 2008 −59 Apr 11, 2008 −60 Apr 11, 2008 −61 Apr 11, 2008 −62 Apr 11, 2008 −63 Apr 11, 2008 −64 Apr 11, 2008 −65 Apr 11, 2008 −66 Apr 11, 2008 −67 Apr 11, 2008 −68 Apr 11, 2008 −69 Apr 11, 2008 −70 Apr 11, 2008 −71 Apr 11, 2008 −72 Apr 11, 2008 −73 Apr 11, 2008 −74 Apr 11, 2008 −75 May 11, 2015 −76 Apr 11, 2008 07−25−00 −1 Jun 15, 2007 −2 Jun 15, 2007 DOT Approved REV 109, Aug 16, 2021 Airplane Flight Manual CSP 700−1A 00−03−9 LIST OF EFFECTIVE PAGES Page Date Page Date Page Date 07−25−01 −1 Jun 15, 2007 −2 Sep 29, 2008 −3 Sep 29, 2008 −4 Sep 29, 2008 07−26−00 −1 Sep 16, 2009 −2 Sep 16, 2009 07−26−01 −1 Sep 16, 2009 −2 Sep 16, 2009 07−27−00 −1 Feb 11, 2008 −2 Feb 11, 2008 07−27−01 −1 Feb 11, 2008 −2 Sep 18, 2017 −3 Dec 22, 2009 −4 Feb 11, 2008 07−28−00 −1 Jun 15, 2007 −2 Jun 15, 2007 07−28−01 −1 Jun 15, 2007 −2 Jun 15, 2007 07−29−00 −1 May 19, 2021 −2 Dec 22, 2009 07−29−01 −1 May 19, 2021 −2 May 19, 2021 −3 May 19, 2021 −4 May 19, 2021 −5 May 19, 2021 −6 May 19, 2021 −7 May 19, 2021 −8 May 19, 2021 −9 May 19, 2021 −10 May 19, 2021 07−30−00 −1 Mar 04, 2013 −2 Mar 04, 2013 07−30−01 −1 Feb 21, 2020 −2 Mar 04, 2013 07−31−00 −1 Sep 10, 2013 −2 Sep 16, 2009 07−31−01 −1 Sep 10, 2013 −2 Sep 10, 2013 −3 May 11, 2015 −4 May 11, 2015 07−32−00 −1 May 21, 2020 −2 Mar 04, 2013 07−32−01 −1 May 21, 2020 −2 May 21, 2020 −3 May 21, 2020 −4 May 21, 2020 07−33−00 −1 May 11, 2015 −2 May 11, 2015 07−33−01 −1 May 11, 2015 −2 May 11, 2015 07−34−00 −1 Jul 29, 2016 −2 Sep 10, 2013 07−34−01 −1 Feb 22, 2021 −2 Jul 29, 2016 07−43−00 −1 Jun 03, 2014 −2 Jun 03, 2014 07−43−01 −1 Jun 03, 2014 −2 Jun 03, 2014 07−45−00 −1 Nov 26, 2014 −2 Nov 26, 2014 07−45−01 −1 Nov 26, 2014 −2 Nov 26, 2014 08−00−00 −1 Dec 01, 2003 −2 Dec 01, 2003 08−10−00 −1 Feb 22, 2021 −2 Jan 29, 2007 08−10−01 −1 Nov 10, 2006 −2 Dec 01, 2003 08−10−23 −1 Dec 01, 2003 −2 Dec 01, 2003 08−10−27 −1 Nov 10, 2006 −2 Nov 10, 2006 −3 Nov 10, 2006 −4 Nov 10, 2006 −5 Nov 10, 2006 −6 Nov 10, 2006 −7 Nov 10, 2006 −8 Nov 10, 2006 08−10−32 −1 Nov 10, 2006 −2 Nov 10, 2006 08−10−34 −1 Jan 29, 2007 −2 Jan 29, 2007 08−10−51 −1 Feb 22, 2021 −2 Dec 01, 2003 08−10−52 −1 Nov 10, 2006 −2 Nov 10, 2006 −3 Nov 10, 2006 −4 Nov 10, 2006 −5 Nov 10, 2006 −6 Nov 10, 2006 08−10−53 −1 Nov 10, 2006 −2 Jun 03, 2014 08−10−55 −1 Nov 10, 2006 −2 Nov 10, 2006 −3 Nov 10, 2006 −4 Nov 10, 2006 −5 Nov 10, 2006 −6 Nov 10, 2006 08−10−57 −1 Nov 10, 2006 −2 Nov 10, 2006 −3 Nov 10, 2006 −4 Nov 10, 2006 −5 Nov 10, 2006 −6 Nov 10, 2006 −7 Nov 10, 2006 −8 Nov 10, 2006 −9 Nov 10, 2006 −10 Nov 10, 2006 −11 Nov 10, 2006 −12 Nov 10, 2006 −13 Nov 10, 2006 −14 Nov 10, 2006 DOT Approved REV 109, Aug 16, 2021 Airplane Flight Manual CSP 700−1A 00−03−10 LIST OF EFFECTIVE PAGES Page Date Page Date Page Date GENERAL Introduction 06−01−1 General 06−01−1 Conversion Data 06−01−2 Temperature Conversion 06−01−2 Weight Conversion 06−01−4 Wind Component 06−01−6 Calibration 06−01−8 General 06−01−8 Airspeed and Altitude Position Error Correction (Slat IN / Flap 0) − Integrated Standby Instrument − Airplanes 9159 and Subsequent 06−01−8 Airspeed Position Error Correction − Integrated Standby Instrument (Slat OUT / Flap 0°, 6°, 16°, 30°) − Airplanes 9159 and Subsequent 06−01−10 Altitude Position Error Correction − Integrated Standby Instrument (Slat OUT / Flap 0°, 6°, 16°, 30°) − Airplanes 9159 and Subsequent 06−01−12 Airspeed Position Error Correction − Integrated Standby Instrument with SSEC Flag (Slat OUT / Flap 0°, 6°, 16°, 30°) − Airplanes 9159 and Subsequent 06−01−14 Altitude Position Error Correction − Integrated Standby Instrument with SSEC Flag (Slat OUT / Flap 0°, 6°, 16°, 30°) − Airplanes 9159 and Subsequent 06−01−16 Airspeed Position Error Correction − Standby Airspeed Indicator (Slat IN / Flap 0°) − Airplanes 9002 thru 9158 06−01−18 Altitude Position Error Correction − Standby Altimeter (Slat IN / Flap 0°) − Airplanes 9002 thru 9158 06−01−20 Airspeed Position Error Correction − Standby Airspeed Indicator (Slat OUT / Flap 0°, 6°, 16°, 30°) − Airplanes 9002 thru 9158 06−01−22 Altitude Position Error Correction − Standby Altimeter (Slat OUT / Flap 0°, 6°, 16°, 30°) − Airplanes 9002 thru 9158 06−01−24 Mach Number and Altitude Position Error Correction − Primary System (Slat IN / Flap 0°) 06−01−26 Flight Capabilities 06−01−28 Stall Speeds (VS ) 06−01−28 Maneuvering Capabilities 06−01−30 Performance Conditions and Configurations 06−01−33 Minimum Control Speed, Air (VMCA) 06−01−33 Minimum Control Speed, Ground (VMCG) 06−01−33 Minimum Control Speed, Landing (VMCL ) 06−01−33 PERFORMANCE TABLE OF CONTENTS CHAPTER 6 - PERFORMANCE 06−00−1 DOT Approved REV 44, Jan 21, 2005 Airplane Flight Manual CSP 700−1A 06−00−1 Page TABLE OF CONTENTS GENERAL Demonstrated Crosswind (Take-Off and Landing) 06−01−33 Maximum Tailwind (Take-Off and Landing) 06−01−33 Configurations and Thrusts 06−01−33 THRUST SETTINGS Thrust Settings 06−02−1 General 06−02−1 EPR Thrust Setting Tables 06−02−1 TAKE-OFF PERFORMANCE Introduction 06−03−1 General 06−03−1 Take−Off Performance − Slat OUT / Flap 6° 06−03−1 Maximum Allowable Take-Off Weight 06−03−1 Dry Runway Take-Off Field Length 06−03−6 Wet Runway Take-Off Field Length 06−03−11 Take-Off Speeds 06−03−15 Take−Off Performance − Slat OUT / Flap 16° 06−03−23 Maximum Allowable Take-Off Weight 06−03−23 Dry Runway Take-Off Field Length 06−03−28 Wet Runway Take-Off Field Length 06−03−31 Take-Off Speeds 06−03−34 Maximum Allowable Brake Temperature 06−03−41 Maximum Allowable Brake Temperature for Take-Off 06−03−41 Stabilizer Trim Setting 06−03−41 Stabilizer Trim Setting for Take-Off 06−03−41 OBSTACLE CLEARANCE Introduction 06−04−1 General 06−04−1 Take-Off Flight Path 06−04−1 Take-Off Flight Path 06−04−1 Maximum Take-Off Weight Limited by Obstacle Clearance Requirements 06−04−4 General 06−04−4 Obstacle Clearance Reference Climb Gradient 06−04−5 PERFORMANCE TABLE OF CONTENTS DOT Approved REV 84, May 11, 2015 Airplane Flight Manual CSP 700−1A 06−00−2 Page OBSTACLE CLEARANCE Net Take-Off Flight Path 06−04−14 Conversion From Geometric Height To Pressure Height 06−04−17 Net Acceleration Distance 06−04−19 Final Segment Net Climb Gradient 06−04−21 Examples − Obstacle Clearance Calculations 06−04−21 Gradient Loss 06−04−24 Gradient Loss in a Steady Turn 06−04−24 ENROUTE PERFORMANCE Introduction 06−05−1 General 06−05−1 Final Segment and Enroute Climb Speed 06−05−1 Final Segment and Enroute Climb Speed, VFTO − Slat IN / Flap 0° 06−05−1 Final Segment and Enroute Climb Gradient 06−05−3 Final Segment and Enroute Climb Gradient, Slat IN / Flap 0° 06−05−3 APPROACH AND LANDING CLIMB Introduction 06−06−1 General 06−06−1 Approach Climb Speed 06−06−1 Approach Climb Speed, VAC − Slat OUT / Flap 6° 06−06−1 Approach Climb Gradient 06−06−3 Approach Climb Gradient, Slat OUT / Flap 6°− Engine Bleed Closed 06−06−3 Approach Climb Gradient, Slat OUT / Flap 6°− Engine Bleed Open / Pack On 06−06−5 Landing Climb Speed 06−06−7 Landing Climb Speed, VLC − Slat OUT / Flap 30° 06−06−7 Landing Climb Gradient 06−06−9 Landing Climb Gradient, Slat OUT / Flap 30°− Engine Bleed Closed 06−06−9 Landing Climb Gradient, Slat OUT / Flap 30° − Engine Bleeds Open / Packs On 06−06−11 LANDING PERFORMANCE Introduction 06−07−1 General 06−07−1 PERFORMANCE TABLE OF CONTENTS DOT Approved REV 82, Nov 26, 2014 Airplane Flight Manual CSP 700−1A 06−00−3 Page LANDING PERFORMANCE Maximum Allowable Landing Weight 06−07−1 General 06−07−1 Maximum Landing Weight Limited by Climb Requirements − Slat OUT / Approach Flap 6°/ Landing Flap 30° 06−07−1 Landing Field Length and Speed 06−07−3 Landing Field Length and Landing Speed, Slat OUT / Flap 30° 06−07−3 Landing Distance Using Autobrake 06−07−7 Landing Distance Using Autobrake, Slat OUT / Flap 30° 06−07−7 PERFORMANCE DATA FOR OPERATION IN ICING CONDITIONS Introduction 06−08−1 General 06−08−1 Performance Corrections 06−08−1 General 06−08−1 Effects of Cowl Anti-Ice On 06−08−1 Effects of Wing and Cowl Anti-Ice On / Ice Accumulation 06−08−4 Take-Off Weight Limited by Climb Requirements, Slat OUT / Flap 6° − Anti-Ice On 06−08−10 Take-Off Weight Limited by Climb Requirements, Slat OUT / Flap 16° − Anti-Ice On 06−08−12 Final Segment and Enroute Climb Gradient, Slat IN / Flap 0° − Cowl Anti-Ice On 06−08−14 Final Segment and Enroute Climb Gradient, Slat IN / Flap 0° − Wing and Cowl Anti-Ice On 06−08−16 Maximum Landing Weight Limited by Climb Requirements − Slat OUT / Approach Flap 6° / Landing Flap 30° − Anti-Ice On 06−08−18 LIST OF ILLUSTRATIONS GENERAL Figure 06−01−1 Temperature Conversion 06−01−3 Figure 06−01−2 Weight Conversion 06−01−5 Figure 06−01−3 Wind Component 06−01−7 Figure 06−01−4 Airspeed and Altitude Position Error Correction − Integrated Standby Instrument (Slat IN / Flap 0°) 06−01−9 Figure 06−01−5 Airspeed Position Error Correction − Integrated Standby Instrument (Slat OUT / Flap 0°, 6°, 16°, 30°) 06−01−11 PERFORMANCE TABLE OF CONTENTS DOT Approved REV 109, Aug 16, 2021 Airplane Flight Manual CSP 700−1A 06−00−4 Page LIST OF ILLUSTRATIONS GENERAL Figure 06−01−6 Altitude Position Error Correction − Integrated Standby Instrument (Slat OUT / Flap 0°, 6°, 16°, 30°) 06−01−13 Figure 06−01−7 Airspeed Position Error Correction − Integrated Standby Instrument with SSEC Flag (Slat OUT / Flap 0°, 6°, 16°, 30°) 06−01−15 Figure 06−01−8 Altitude Position Error Correction − Integrated Standby Instrument with SSEC Flag (Slat OUT / Flap 0°, 6°, 16°, 30°) 06−01−17 Figure 06−01−9 Airspeed Position Error Correction − Standby Airspeed Indicator (Slat IN / Flap 0°) 06−01−19 Figure 06−01−10 Altitude Position Error Correction − Standby Altimeter (Slat IN / Flap 0°) 06−01−21 Figure 06−01−11 Airspeed Position Error Correction − Standby Airspeed Indicator (Slat OUT / Flap 0°, 6°, 16°, 30°) 06−01−23 Figure 06−01−12 Altitude Position Error Correction − Standby Altimeter (Slat OUT / Flap 0°, 6°, 16°, 30°) 06−01−25 Figure 06−01−13 Mach Number and Altitude Position Error Correction − Primary System (Slat IN / Flap 0°) 06−01−27 Figure 06−01−14 Stall Speeds (VS) 06−01−29 Figure 06−01−15 Maneuvering Capabilities 06−01−31 THRUST SETTINGS Figure 06−02−1 MTO Rating 06−02−2 Figure 06−02−2 GA Rating 06−02−4 Figure 06−02−3 MCT Rating at 110 KIAS 06−02−6 Figure 06−02−4 MCT Rating at 140 KIAS 06−02−8 Figure 06−02−5 MCT Rating at 170 KIAS 06−02−10 Figure 06−02−6 MCT Rating at 200 KIAS 06−02−12 Figure 06−02−7 MCT Rating at 230 KIAS 06−02−14 TAKE-OFF PERFORMANCE Figure 06−03−1 Take-Off Weight Limited by Climb Requirements − Slat OUT / Flap 6° 06−03−2 Figure 06−03−2 Take-Off Weight Limited by Brake Energy − Slat OUT/Flap 6° 06−03−4 Figure 06−03−3 Uncorrected Take-Off Field Length, Dry Runway, Slat OUT / Flap 6° 06−03−8 PERFORMANCE TABLE OF CONTENTS DOT Approved REV 84, May 11, 2015 Airplane Flight Manual CSP 700−1A 06−00−5 Page TAKE-OFF PERFORMANCE Figure 06−03−4 Corrected Take-Off Field Length, Dry Runway, Slat OUT / Flap 6° 06−03−9 Figure 06−03−5 Uncorrected Take-Off Field Length, Wet Runway, Slat OUT / Flap 6° 06−03−13 Figure 06−03−6 Corrected Take-Off Field Length, Wet Runway, Slat OUT / Flap 6° 06−03−14 Figure 06−03−7 Take-Off Decision Speed V1 − Slat OUT / Flap 6° − Wet Runway 06−03−18 Figure 06−03−8 Rotation Speed, VR − Slat OUT / Flap 6° 06−03−20 Figure 06−03−9 Take-Off Safety Speed, V2 − Slat OUT / Flap 6° 06−03−22 Figure 06−03−10 Take-Off Weight Limited by Climb Requirements − Slat OUT / Flap 16° 06−03−24 Figure 06−03−11 Take-Off Weight Limited by Brake Energy − Slat OUT / Flap 16° 06−03−26 Figure 06−03−12 Uncorrected Take-Off Field Length, Dry Runway, Slat OUT/ Flap 16° 06−03−29 Figure 06−03−13 Corrected Take-Off Field Length, Dry Runway, Slat OUT/ Flap 16° 06−03−30 Figure 06−03−14 Uncorrected Take-Off Field Length, Wet Runway, Slat OUT / Flap 16° 06−03−32 Figure 06−03−15 Corrected Take-Off Field Length, Wet Runway, Slat OUT / Flap 16° 06−03−33 Figure 06−03−16 Take-Off Decision Speed V1 − Slat OUT / Flap 16° − Wet Runway 06−03−36 Figure 06−03−17 Rotation Speed VR − Slat OUT / Flap 16° 06−03−38 Figure 06−03−18 Take-Off Safety Speed V2 − Slat OUT / Flap 16° 06−03−40 Figure 06−03−19 Stabilizer Trim Setting For Take-Off − Slat OUT / Flap 6° 06−03−42 Figure 06−03−20 Stabilizer Trim Setting For Take-Off − Slat OUT / Flap 16° 06−03−43 OBSTACLE CLEARANCE Figure 06−04−1 Take-Off Flight Path − Gross Level-off Height Less than 1500 Feet 06−04−2 Figure 06−04−2 Take-Off Flight Path − Gross Level-off Height Greater than 1500 Feet 06−04−3 Figure 06−04−3 Obstacle Clearance Reference Climb Gradient, Slat OUT / Flap 6° − Engine Bleed Closed 06−04−6 Figure 06−04−4 Obstacle Clearance Reference Climb Gradient, Slat OUT / Flap 6° − Engine Bleed Open / Packs On 06−04−8 PERFORMANCE TABLE OF CONTENTS DOT Approved REV 84, May 11, 2015 Airplane Flight Manual CSP 700−1A 06−00−6 Page OBSTACLE CLEARANCE Figure 06−04−5 Obstacle Clearance Reference Climb Gradient, Slat OUT / Flap 16° − Engine Bleed Closed 06−04−10 Figure 06−04−6 Obstacle Clearance Reference Climb Gradient, Slat OUT / Flap 16° − Engine Bleed Open / Packs On 06−04−12 Figure 06−04−7 Net Take−Off Flight Path − Close in Obstacles 06−04−15 Figure 06−04−8 Net Take−Off Flight Path − Far Obstacles 06−04−16 Figure 06−04−9 Geometric Height Above Airport to Pressure Height Above Airport Conversion 06−04−18 Figure 06−04−10 Net Acceleration Distance 06−04−20 ENROUTE PERFORMANCE Figure 06−05−1 Final Segment and Enroute Climb Speed, VFTO − Slat IN / Flap 0° 06−05−2 Figure 06−05−2 Final Segment and Enroute Climb Gradient, Slat IN / Flap 0° 06−05−4 APPROACH AND LANDING CLIMB Figure 06−06−1 Approach Climb Speed, VAC − Slat OUT / Flap 6° 06−06−2 Figure 06−06−2 Approach Climb Gradient, Slat OUT / Flap 6°− Engine Bleed Closed 06−06−4 Figure 06−06−3 Approach Climb Gradient, Slat OUT / Flap 6°− Engine Bleed Open / Pack On 06−06−6 Figure 06−06−4 Landing Climb Speed, VLC − Slat OUT / Flap 30° 06−06−8 Figure 06−06−5 Landing Climb Gradient, Slat OUT / Flap 30°− Engine Bleed Closed 06−06−10 Figure 06−06−6 Landing Climb Gradient, Slat OUT / Flap 30° − Engine Bleeds Open / Packs On 06−06−12 LANDING PERFORMANCE Figure 06−07−1 Maximum Landing Weight Limited by Climb Requirements − Slat OUT / Approach Flap 6°/ Landing Flap 30° 06−07−2 Figure 06−07−2 Actual Landing Distance and Landing Speed, Slat OUT / Flap 30° 06−07−5 Figure 06−07−3 Landing Field Length Required − Slat OUT / Flap 30° 06−07−6 Figure 06−07−4 Actual Distance From Touchdown to Full Stop Using Autobrake − Slat OUT/Flap 30° 06−07−8 PERFORMANCE TABLE OF CONTENTS DOT Approved REV 109, Aug 16, 2021 Airplane Flight Manual CSP 700−1A 06−00−7 Page PERFORMANCE DATA FOR OPERATION IN ICING CONDITIONS Figure 06−08−1 Take-Off Weight Limited by Climb Requirements, Slat OUT / Flap 6°− Anti-Ice On 06−08−11 Figure 06−08−2 Take-Off Weight Limited by Climb Requirements, Slat OUT / Flap 16° − Anti-Ice On 06−08−13 Figure 06−08−3 Final Segment and Enroute Climb Gradient, Slat IN / Flap 0° − Cowl Anti-Ice On 06−08−15 Figure 06−08−4 Final Segment and Enroute Climb Gradient, Slat IN / Flap 0° − Wing and Cowl Anti-Ice On 06−08−17 Figure 06−08−5 Maximum Landing Weight Limited by Climb Requirements − Slat OUT / Approach Flap 6° / Landing Flap 30° − Anti-Ice On 06−08−19 PERFORMANCE TABLE OF CONTENTS DOT Approved REV 62, Sep 16, 2009 Airplane Flight Manual CSP 700−1A 06−00−8 Page 1. INTRODUCTION A. General The Take-Off Performance section contains the charts used to obtain the take-off performance data for varying conditions of temperature, airport pressure altitude, and airplane weight for the specified take-off configurations. 2. TAKE-OFF PERFORMANCE - SLAT OUT / FLAP 6° A. Maximum Allowable Take-Off Weight The maximum allowable take-off weight is limited by the most restrictive of the following: • Maximum approved take-off weight (Refer to Chapter 2; LIMITATIONS − STRUCTURAL WEIGHT LIMITATION); or • Climb requirements; or • Tire limit speed; or • Brake energy available; or • Runway length available. (1) TAKE-OFF WEIGHT LIMITED BY CLIMB REQUIREMENTS The maximum take-off weight limited by climb requirements for a slat out / flap 6° take-off is determined from Figure 06−03−1, for varying conditions of ambient temperature, airport pressure altitude, engine bleed and pack usage. The weights presented in Figure 06−03−1 are limited by second segment climb gradient requirements, as per FAR 25.121 (b). The first segment climb and final segment climb gradient requirements, as per FAR 25.121 (a) and FAR 25.121 (c), respectively, are not limiting. With the APU on, reduce the take-off weight derived from Figure 06−03−1 by 250 kg (551 lb). Example: Associated Conditions: Ambient temperature = 25 °C Airport pressure altitude = 10,000 ft Engine bleed = Open Pack = On APU = Off As shown in the example on Figure 06−03−1, the maximum take-off weight limited by climb requirements is 33,400 kg (73,600 lb). The take-off weight in this case is less than the maximum approved take-off weight (Refer to Chapter 2; LIMITATIONS − STRUCTURAL WEIGHT LIMITATION) and is considered limiting. PERFORMANCE TAKE-OFF PERFORMANCE DOT Approved REV 94, Sep 18, 2017 Airplane Flight Manual CSP 700−1A 06−03−1 2. TAKE-OFF PERFORMANCE - SLAT OUT / FLAP 6° (CONT'D) A. Maximum Allowable Take-Off Weight (Cont’d) FM8603_001 watTo_f06_98k_2001_5_8 PERFORMANCE TAKE-OFF PERFORMANCE Take-Off Weight Limited by Climb Requirements − Slat OUT / Flap 6° Figure 06−03−1 DOT Approved REV 80, Jun 03, 2014 Airplane Flight Manual CSP 700−1A 06−03−2 2. TAKE-OFF PERFORMANCE - SLAT OUT / FLAP 6° (CONT'D) A. Maximum Allowable Take-Off Weight (Cont’d) (2) TAKE-OFF WEIGHT LIMITED BY MAXIMUM TIRE SPEED The tire limit speed of 210 mph (183 knots), does not restrict the maximum take-off weight for the slat OUT / flap 6° configuration. (3) TAKE-OFF WEIGHT LIMITED BY BRAKE ENERGY AVAILABLE The maximum take-off weight limited by the brake energy available in the brake system (with the Brake Temperature Monitoring System (BTMS) operative), for a slat OUT / flap 6° take-off, on dry or wet runways, is determined from Figure 06−03−2, for varying conditions of ambient temperature, airport pressure altitude, reported wind and runway slope. The effect of engine bleed and pack usage is negligible. The brake energy available is based on the brake status provided by the BTMS. The maximum take-off weight limited by brake energy can be determined for the following conditions: • when maximum brake energy is available (BTMS unit of 6 or less); or • when partial brake energy is available following a landing or a rejected take-off. The BTMS temperature reading of the warmest brake is to be used in the derivation of the maximum take-off weight. Example: Associated Conditions: Ambient temperature = 15 °C Airport pressure altitude = 10,000 ft Reported wind = 10 knots (headwind) Runway slope = +2% (uphill) Warmest brake readout = BTMS unit of 13 The example in Figure 06−03−2 shows that the maximum take-off weight limited by brake energy available is 36,550 kg (80,580 lb). If maximum brake energy is available (warmest brake readout before take-off is BTMS unit of 6 or below), then the maximum take-off weight limited by brake energy would be 42,200 kg (93,030 lb). PERFORMANCE TAKE-OFF PERFORMANCE DOT Approved REV 80, Jun 03, 2014 Airplane Flight Manual CSP 700−1A 06−03−3 2. TAKE-OFF PERFORMANCE - SLAT OUT / FLAP 6° (CONT'D) A. Maximum Allowable Take-Off Weight (Cont’d) FM8603_002 CHART_BTMS_GX_F06_PAGE1_2002_1_15 PERFORMANCE TAKE-OFF PERFORMANCE Take-Off Weight Limited by Brake Energy − Slat OUT/Flap 6° Figure 06−03−2 (Sheet 1 of 2) DOT Approved REV 80, Jun 03, 2014 Airplane Flight Manual CSP 700−1A 06−03−4 2. TAKE-OFF PERFORMANCE - SLAT OUT / FLAP 6° (CONT'D) A. Maximum Allowable Take-Off Weight (Cont’d) FM8603_003 CHART_BTMS_GX_F06_PAGE2_1999_3_12 PERFORMANCE TAKE-OFF PERFORMANCE Take-Off Weight Limited by Brake Energy − Slat OUT/Flap 6° Figure 06−03−2 (Sheet 2 of 2) DOT Approved REV 80, Jun 03, 2014 Airplane Flight Manual CSP 700−1A 06−03−5 2. TAKE-OFF PERFORMANCE - SLAT OUT / FLAP 6° (CONT'D) B. Dry Runway Take-Off Field Length The following charts are used to obtain the take-off field length required on a dry runway, for a given value of airplane weight, ambient temperature, airport pressure altitude (from sea level to 10,000 feet in 2,000−foot intervals), reported wind, runway slope and various bleed configurations. The take-off field length, as presented in these charts, is the most limiting of the following: • Take-off distance with all engines operating, multiplied by a factor of 1.15; • Take-off distance with one engine inoperative; and • Accelerate-stop distance. NOTE When the take-off crosswind exceeds 20 knots, the high crosswind take-off procedure must be used (refer to the Flight Crew Operating Manual, Chapter 4: NORMAL PROCEDURES − TAXIING AND TAKE-OFF − HIGH CROSSWIND TAKE-OFF). The corrected take-off field length must be increased by 520 meters (1,700 feet). The take-off field length for a slat OUT / flap 6° take-off on a dry runway, are given by the following: • Figure 06−03−3 provides the uncorrected take−off field length; • Figure 06−03−4 provides the take-off field length corrected for the effects of engine bleed / pack usage, runway slope and reported wind. Effectivity: • Airplanes 9002 thru 9158 not incorporating Service Bulletins: • SB 700−27−054, Modification − Control and Indication Systems − Modifications to Permit Zero Flap Take-Off Capability, or SB 700−32−034, Modification − Brake Control System − Introduction of Wheel Speed Transducer Part No. 140−209−4 (GW415−1050−9) or • Airplanes 9159 thru 9304 not incorporating Service Bulletins: • SB 700−27−059, Modification − Control and Indication Systems − Modifications to Permit Zero Flap Take-Off Capability with Full Performance, or SB 700−32−034, Modification − Brake Control System − Introduction of Wheel Speed Transducer Part No. 140−209−4 (GW415−1050−9). Figure 06−03−4 (sheet 2) provides the take-off field length factor for accommodating BCU characteristics at high speeds. PERFORMANCE TAKE-OFF PERFORMANCE DOT Approved REV 94, Sep 18, 2017 Airplane Flight Manual CSP 700−1A 06−03−6 2. TAKE-OFF PERFORMANCE - SLAT OUT / FLAP 6° (CONT'D) B. Dry Runway Take-Off Field Length (Cont’d) The uncorrected take-off field length can be interpolated linearly with altitude. Example: Associated Conditions: Ambient temperature = 15 °C Airport pressure altitude = 2,000 ft Engine bleed = Open Packs = On A/C weight = 40,000 kg (88,185 lb) Reported wind = 20 knots headwind Runway slope = + 1 % (uphill) The example in Figure 06−03−3 and Figure 06−03−4 shows that for the above associated conditions, the corrected take-off field length required is 1,715 meters (5,630 feet). PERFORMANCE TAKE-OFF PERFORMANCE DOT Approved REV 84, May 11, 2015 Airplane Flight Manual CSP 700−1A 06−03−7 2. TAKE-OFF PERFORMANCE - SLAT OUT / FLAP 6° (CONT'D) B. Dry Runway Take-Off Field Length (Cont’d) FM8603_004 TOFL_DRY_F06_GX_2002_1_12 PERFORMANCE TAKE-OFF PERFORMANCE Uncorrected Take-Off Field Length, Dry Runway, Slat OUT / Flap 6° Figure 06−03−3 DOT Approved REV 84, May 11, 2015 Airplane Flight Manual CSP 700−1A 06−03−8 2. TAKE-OFF PERFORMANCE - SLAT OUT / FLAP 6° (CONT'D) B. Dry Runway Take-Off Field Length (Cont’d) FM8603_005 TOFL_CORR_DRY_F06_GX_2001_9_13 PERFORMANCE TAKE-OFF PERFORMANCE Corrected Take-Off Field Length, Dry Runway, Slat OUT / Flap 6° Figure 06−03−4 (Sheet 1 of 2) DOT Approved REV 84, May 11, 2015 Airplane Flight Manual CSP 700−1A 06−03−9 2. TAKE-OFF PERFORMANCE - SLAT OUT / FLAP 6° (CONT'D) B. Dry Runway Take-Off Field Length (Cont’d) FM6720_033C Effectivity: Airplanes 9002 thru 9158 Service Bulletins: SB 700−27−054, Modification − Control and Indication Systems − Modifications to Permit Zero Flap Take−Off Capability, or Full Performance, not incorporating Airplanes 9159 thru 9304 Service Bulletins: not incorporating SB 700−32−034, Modification − Brake Control System − Introduction of Wheel Speed Transducer Part No. 140−209−4 (GW415−1050−9) SB 700−27−059, Modification − Control and Indication Systems − Modifications to Permit Zero Flap Take−Off Capability with SB 700−32−034, Modification − Brake Control System − Introduction of Wheel Speed Transducer Part No. 140−209−4 (GW415−1050−9) or or PERFORMANCE TAKE-OFF PERFORMANCE Corrected Take-Off Field Length, Dry Runway, Slat OUT / Flap 6° Figure 06−03−4 (Sheet 2 of 2) DOT Approved REV 84, May 11, 2015 Airplane Flight Manual CSP 700−1A 06−03−10 2. TAKE-OFF PERFORMANCE - SLAT OUT / FLAP 6° (CONT'D) C. Wet Runway Take-Off Field Length A wet runway condition has a deteriorating effect on the stopping performance of the airplane and appropriate corrections should be made to compensate for this degradation. The following charts are used to obtain the take-off field length required on a wet runway, for a given value of airplane weight, ambient temperature, airport pressure altitude (from sea level to 10,000 feet in 2,000−foot intervals), reported wind, runway slope, usage of thrust reversers and various bleed configurations. The take-off field length, as presented in these charts, is the most limiting of the following: • Take-off field length on a dry runway; • Take-off distance with all engines operating, multiplied by a factor of 1.15; • Take-off distance with one engine inoperative; and • Accelerate--stop distance. NOTE When the take-off crosswind exceeds 20 knots, the high crosswind take-off procedure must be used (refer to the Flight Crew Operating Manual, Chapter 4: NORMAL PROCEDURES − TAXIING AND TAKE-OFF − HIGH CROSSWIND TAKE-OFF). The corrected take-off field length must be increased by 520 meters (1,700 feet). The take-off field length for a slat OUT / flap 6° take-off on a wet runway, are given by the following: • Figure 06−03−5 provides the uncorrected take-off field length; • Figure 06−03−6 provides the take−off field length corrected for the effects of engine bleed / pack usage, runway slope, reported wind and thrust reverser(s) usage. With one or both thrust reversers inoperative, if the actual takeoff weight is less than 29,000 kg (63,935 lb), a weight of 29,000 kg (63,935 lb) must be used to determine the take−off field length. PERFORMANCE TAKE-OFF PERFORMANCE DOT Approved REV 109, Aug 16, 2021 Airplane Flight Manual CSP 700−1A 06−03−11 2. TAKE-OFF PERFORMANCE - SLAT OUT / FLAP 6° (CONT'D) C. Wet Runway Take-Off Field Length (Cont’d) Effectivity: • Airplanes 9002 thru 9158 not incorporating Service Bulletins: • SB 700−27−054, Modification − Control and Indication Systems − Modifications to Permit Zero Flap Take-Off Capability, or SB 700−32−034, Modification − Brake Control System − Introduction of Wheel Speed Transducer Part No. 140−209−4 (GW415−1050−9) or • Airplanes 9159 thru 9304 not incorporating Service Bulletins: • SB 700−27−059, Modification − Control and Indication Systems − Modifications to Permit Zero Flap Take-Off Capability with Full Performance, or SB 700−32−034, Modification − Brake Control System − Introduction of Wheel Speed Transducer Part No. 140−209−4 (GW415−1050−9). Where V 1 determined from Figure 06−03−7 is greater than 0.92 VR, determined from Figure 06−03−8, the take-off field length obtained from Figure 06−03−5 and Figure 06−03−6 must be increased by 15% (TOFL x 1.15). The uncorrected take-off field length can be interpolated linearly with altitude. Example: Associated Conditions: Ambient temperature = 15 °C Airport pressure altitude = 2,000 ft Engine bleed = Open Packs = On A/C weight = 40,000 kg (88,185 lb) Reported wind = 20 knots headwind Runway slope = + 1 % (uphill) Thrust reversers = Both operable The example in Figure 06−03−5 and Figure 06−03−6 shows that for the above associated conditions, the corrected take-off field length is 1,715 meters (5,630 feet). PERFORMANCE TAKE-OFF PERFORMANCE DOT Approved REV 109, Aug 16, 2021 Airplane Flight Manual CSP 700−1A 06−03−12 2. TAKE-OFF PERFORMANCE - SLAT OUT / FLAP 6° (CONT'D) C. Wet Runway Take-Off Field Length (Cont’d) FM8603_006 TOFL_WET_F06_GX_2002_1_12 PERFORMANCE TAKE-OFF PERFORMANCE Uncorrected Take-Off Field Length, Wet Runway, Slat OUT / Flap 6° Figure 06−03−5 DOT Approved REV 84, May 11, 2015 Airplane Flight Manual CSP 700−1A 06−03−13 2. TAKE-OFF PERFORMANCE - SLAT OUT / FLAP 6° (CONT'D) C. Wet Runway Take-Off Field Length (Cont’d) FM6603_007 tofl_corr_wet_f06_gx_2001_11_23 PERFORMANCE TAKE-OFF PERFORMANCE Corrected Take-Off Field Length, Wet Runway, Slat OUT / Flap 6° Figure 06−03−6 DOT Approved REV 84, May 11, 2015 Airplane Flight Manual CSP 700−1A 06−03−14 2. TAKE-OFF PERFORMANCE - SLAT OUT / FLAP 6° (CONT'D) D. Take-Off Speeds (1) TAKE-OFF DECISION SPEED, V 1 - DRY RUNWAY The take-off decision speed (V1 ) for a slat OUT / flap 6° take-off on a dry runway, is equal to the rotation speed (VR ). Use the appropriate VR chart. Refer to Figure 06−03−8. V 1 must not be less than V1MCG. Effectivity: • Airplanes 9002 thru 9158 not incorporating Service Bulletins: • SB 700−27−054, Modification − Control and Indication Systems − Modifications to Permit Zero Flap Take-Off Capability, or SB 700−32−034, Modification − Brake Control System − Introduction of Wheel Speed Transducer Part No. 140−209−4 (GW415−1050−9) or • Airplanes 9159 thru 9304 not incorporating Service Bulletins: • SB 700−27−059, Modification − Control and Indication Systems − Modifications to Permit Zero Flap Take-Off Capability with Full Performance, or SB 700−32−034, Modification − Brake Control System − Introduction of Wheel Speed Transducer Part No. 140−209−4 (GW415−1050−9). The take-off decision speed (V1 ) for slat OUT / flap 6° take-off on a dry runway, is established from the rotation speed (VR), Figure 06−03−8, multiplied by a VR factor of Figure 06−03−4 (sheet 2). (2) TAKE-OFF DECISION SPEED, V1 - WET RUNWAY The following charts are used to obtain the take-off decision speed (V1) for a slat OUT / flap 6° take-off on a wet runway, for a given value of airplane weight, ambient temperature, airport pressure altitude (from sea level to 10,000 feet in 2,000−foot intervals), reported wind, runway slope, usage of thrust reversers and various bleed configurations. V 1 must not be less than V1MCG. The take-off decision speed (V1) for a slat OUT / flap 6° take-off on a wet runway is determined from Figure 06−03−7. PERFORMANCE TAKE-OFF PERFORMANCE DOT Approved REV 84, May 11, 2015 Airplane Flight Manual CSP 700−1A 06−03−15 2. TAKE-OFF PERFORMANCE - SLAT OUT / FLAP 6° (CONT'D) D. Take-Off Speeds (Cont’d) Effectivity: • Airplanes 9002 thru 9158 not incorporating Service Bulletins: • SB 700−27−054, Modification − Control and Indication Systems − Modifications to Permit Zero Flap Take-Off Capability, or SB 700−32−034, Modification − Brake Control System − Introduction of Wheel Speed Transducer Part No. 140−209−4 (GW415−1050−9) or • Airplanes 9159 thru 9304 not incorporating Service Bulletins: • SB 700−27−059, Modification − Control and Indication Systems − Modifications to Permit Zero Flap Take-Off Capability with Full Performance, or SB 700−32−034, Modification − Brake Control System − Introduction of Wheel Speed Transducer Part No. 140−209−4 (GW415−1050−9). The take-off decision speed (V1 ) for slat OUT / flap 6° take-off on a wet runway, is established as the lower of: • V 1 determined from Figure 06−03−7; • V 1 determined from VR, Figure 06−03−8, and multiplied by a VR factor of 0.92. Example: Associated Conditions: Ambient temperature = 15 °C Airport pressure altitude = 2,000 ft A/C weight = 40,000 kg (88,185 lb) Runway slope = + 1% (uphill) Engine Bleed = Open Pack = On Reported wind = 20 knots headwind Thrust reversers = Both operable The example in Figure 06−03−7 shows that for the above associated conditions, V1 is equal to 117.0 KIAS. (3) MINIMUM V1 LIMITED BY CONTROL ON THE GROUND, V1MCG Applicable to both dry and wet runway operations: • V 1MCG (Slat OUT / Flap 6°) = 88 KIAS PERFORMANCE TAKE-OFF PERFORMANCE DOT Approved REV 84, May 11, 2015 Airplane Flight Manual CSP 700−1A 06−03−16 2. TAKE-OFF PERFORMANCE - SLAT OUT / FLAP 6° (CONT'D) D. Take-Off Speeds (Cont’d) FM8603_025 V1_WET_F06_GX_2002_1_11 PERFORMANCE TAKE-OFF PERFORMANCE Take-Off Decision Speed V1 − Slat OUT / Flap 6°− Wet Runway Figure 06−03−7 (Sheet 1 of 2) DOT Approved REV 84, May 11, 2015 Airplane Flight Manual CSP 700−1A 06−03−17 2. TAKE-OFF PERFORMANCE - SLAT OUT / FLAP 6° (CONT'D) D. Take-Off Speeds (Cont’d) FM8603_026 V1_CORR_WET_F06_GX_2001_12_2 PERFORMANCE TAKE-OFF PERFORMANCE Take-Off Decision Speed V1 − Slat OUT / Flap 6° − Wet Runway Figure 06−03−7 (Sheet 2 of 2) DOT Approved REV 84, May 11, 2015 Airplane Flight Manual CSP 700−1A 06−03−18

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