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CHALLENGER 604 Airplane Flight Manual

BOMBARDIER CHALLENGER 604 · Systems Description

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Overview

The Bombardier Challenger 604 Airplane Flight Manual provides essential operational guidelines and limitations for the CL-600-2816 model. It includes technical specifications, performance data, and safety information necessary for the safe operation of the aircraft.

  • The aircraft model is CL-600-2816 (Challenger 604).
  • Maximum Takeoff Weight (MTOW) options are 21,591 kg or 21,863 kg.
  • The manual was first issued on September 20, 1995.
  • The latest revision is Revision 103, dated November 28, 2016.
  • The manual is published by Bombardier Aerospace.
  • Contact information for Bombardier Customer Services is provided for technical assistance.
  • The document is proprietary and confidential.
  • It is essential to operate the aircraft in compliance with the prescribed limitations.

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
·
Systems Description
Year
·
2016
File size
·
1.9 MB
Publisher
·
regulations.gov
Language
·
en

Specifications & performance

Extracted from this document.

Specifications

Mtow kg
·
21,591 or 21,863
Mtow (lb)
·
47,600 or 48,200
About this document
What is the CHALLENGER 604 Airplane Flight Manual?

The CHALLENGER 604 Airplane Flight Manual is a systems description for the BOMBARDIER CHALLENGER 604, dated 2016.

Where does the CHALLENGER 604 Airplane Flight Manual come from?

This copy of the CHALLENGER 604 Airplane Flight Manual was originally published by regulations.gov and is hosted on Sprinkle as a free, searchable reference copy.

What year was the CHALLENGER 604 Airplane Flight Manual published?

The CHALLENGER 604 Airplane Flight Manual — the BOMBARDIER CHALLENGER 604 systems description on file — is dated 2016.

Documentation completeness
3/7

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Full document text

Airplane Flight Manual The Airplane must be operated In compliance with t he LIMITATIONS prescribed herein. MODEL CL-600-2816 (CL-604) 21,591 kg /47,600 lb MTOW or 21,863 kg /48.200 lb MTOW FIRST ISSUED: Sep 20/951 REVISION 103: Nov 28/16 BOMBARDIER CHALLENGER 604 Publication No . CH 604 AFM CH ALLENGER• 604 (MODEL CL-600-2816)CL- 604 AIRPLANE FLIGHT MANUAL Bombardo er Aerospace P 0 Box 6087 Stabon Centre-v llte Montrea t, Quebec , Canada H3C 3G9 http J/Www clc .bombardier.com For more In!ormation regarding Technical Publications please contact: Bombardier Customer Services Business Aircraft Customer Services Hotline (Technical Assistance & ln-lllght Emergencies) North America: 1-866-JET- 12 47 (1-866-538 - 1247) [Press 1) International· + 1-514-855-2999 [Press 1) Emaol ac.yul@aero.bombardier.com User Comments (Technocal Publicati ons ) North Amenca 1- 866-JET -1247 ( 1-866-538 - 1247) [Press 4 then option 2)lntemahonat· +1 - 514-855-2999 [Press 4 then opbon 2) Emaol bbad .user.comments@aero.bombardf er .com Ordering & Distribution (Technical Publocahons) North America. t-866-JET-1247 (1 - 866-538 - 1247) [Press 41hen option 1} lntomational: + 1-514-855-2999 [Press 4 then option 1) Facsimile: 514-855-2770 Email: bbad .pubs.dist@ aero.bombardler.com To ease the ordering process, the tollowing Document ldcntlllcatlon Number should be used CH 604 AFM 8otnbardlor Inc., par l ' ln term~ lal re de aes gtoupea, divisions ellou liliates corporallves. loumll loa pr,tenl.s rontolgnomonta au gouvememeot a litro confldonUol. Cos ronselgnements ont une tcnour conflc:k!nUelle. 1voc droit. de proprl,li, ot noua lea consid~ons exclus de rapplicltlon ct. Ia loi aur l'aecl!s a l'fnlormation. ll s pouvont euul conttituerun aecrel lnduslriel de noire socletO. La dlvulgoUon publlque de ces ren. sefg"""""'ts nulrall i Bombordler Inc . Toule Intention de ~~ diffuser en tout ou en partie dovra 6tre algnlftH 8 ravanco el par ecrit au vlu-prHident SeMces Juridlqua: au aJege social de Ia societct U tit ontondu que le present doeu~t eompren.~nt donnMs tec:hnka~s et autres infDfl'T\81:ions. eur papltr , diaquette, CD-ROM ou IOU1 autre aupport. ne don paa 6tre reprodu1t ou dtvulgue en tOU1 ou on partie, una l'autorluUon 6crite de 8ombardter. est Ia proprfet6 de Bombardier et demeure eonfldentiet, et quo tousles droits au .a brevets, drorta d'autour, marqliel de eomme-roe, secret$ lndU$1:rielt et tout autre droit do propriete lntellectuefle y rattac:hH appartlennent • 8ombard1er. Lo present doeumctn'-t les donn6H toc:hnlquoa ot autrea Informations qu ·n contlent ne d~vont pas etro modUI•a. tradulte, assembiQ ou organiM.t en aont lnvOf'M nl d6c:ompU6s, et dotvt:nt Otre uUUMa unlquomont pour mnlntonlr, e xp lo iter ou reparer l' avlon . Bombardier In c ., by Its groups, divisions and/or corporat.o aubaldlarlea, provides this Information to tho government tn contldonco. This Is proprieLBry contrdenllallnlormatlon which we contido r excluded from tho appllcallon o f tho A ccoll to Information Act nnd may also bo a trade: secrot ot our company . Public roloue ot this lnrorma llon would bO harmful to Bombordlor Inc, Any I nt e ntion to disclose such Inf ormation, or part the root, mus ·t be Indicated In edvanco ond In writing to tho Vlco President legal Services., Corpora to Oftlco. It Ia undoratood that this documontatJon, comprltlng tochnlcat data and other Information In any modll shall not bo reproduced or disclosed In whole or In pan wllhout Bombardier's wrl«t:n authorizallon. Is proprlatary and confidential 10 8omberdlor and lh:at all rights to patent, copyright, trademark. trade secntt and other Jntellectual property rights the~n balong to Bombardier . S\tC-h documentation. technl c.al data end other fniOfmatlon shall not be modified. l11intlatod, reverse auembled . roverao ongi MM&d or do-complied and shall be uMd ldety to maintain, operate or ret)llr the alrc,.ft Copynghl 0 1995-2016 "Y Bomt>anloertnc. AJI nghll '"""'"" "Tredomark of BombarO•er Inc 01 •Is subsid18Nti Pnf"IIOd '"Canada BOMBARDIER • c. ""' • ' .. 0 < • List of Effective Pages 00-03-1 CHALLENGER604 REV 103, Nov 28/16 Page Date Page Date Page Date Tltle Nov 28116 -48 Nov 07108 01-00 -1 Apr 16107 -49 Nov 07/08 -2 Feb 01/07 00-01 -1 Feb 01/07 -50 Nov 07/ 08 -2 Feb Ot/07 -51 Ju117/09 01-01 -1 Feb 01/07 -3 Feb01/07 -52 Feb 01/10 -2 Feb 01/07 -4 Feb 01/07 -53 Feb 01/10 -3 Mar 19/07 -5 Feb 01/07 -54 Feb 01110 -4 Feb 01/07 -6 Feb 01/07 -55 Jun 28110 -5 Feb 01/07 -7 Feb 01/07 -56 Jun 28110 -6 Feb 01/07 -8 Feb 01/07 -57 Jun 28/10 -7 Feb 01/07 -9 Feb 01/07 -58 Jun 28/10 -8 Jul 08/13 -10 Feb 01/07 -59 Sep 09/10 -9 Feb 01/07 -11 Feb 01/07 -60 Sep 09/10 - 10 Feb 01/07 - 12 Feb 01/07 -61 Sep 09/10 - 11 Feb 01/07 - 13 Feb 01/07 -62 Sep 09/10 - 12 Feb 01/07 - 14 Feb 01/07 -63 Dec 1 0/ 10 - 13 Oct20/09 - 15 Feb 01/07 -6 4 Mar 1 6/ 11 - 14 Oct 19/15 - 16 Feb 01/07 -65 Jun 30/ 11 - 15 Oct 20/09 - 17 Feb 01/07 -66 Jan 1 8/ 12 - 16 Oct 19/15 - 18 Feb 01/07 -67 Jan 18/12 - 17 Aug 30/16 - 19 Feb 01/07 -68 Mar 1 6/ 12 - 18 Aug 30/16 - 20 Feb 01/07 -69 Jun 26/12 - 19 Aug 30/16 -2 1 Feb 01/07 -70 Jul 08/13 -20 Aug 30/16 -22 Feb 01107 - 71 Sep 25/13 -23 Feb 01/07 -72 Jul 1 1/14 02-00 -1 Oct 20/09 -24 Feb 01/07 -73 Jun 11/15 -2 Mar 31/ 14 -25 Feb 01/07 -74 Oct 19/15 -3 Oct0 1/ 14 -26 Feb 01/07 -7 5 Jun 09/16 -4 Mar 31/14 -27 Feb 01/07 -76 Aug 30/16 -5 Oct 31/07 -28 Feb 01/07 -77 Nov 28116 -6 Oct 31/07 -29 Feb 01/07 -78 Nov 28/16 -30 Feb 01/07 02-01 -1 Mar 16111 -31 Feb 01/07 00-02 -1 Dec 10110 -2 Feb 01/07 -32 Feb01/07 -2 Dec 10110 -33 FebOt/07 -3 Dec 10110 02-02 -1 Feb 01/07 -34 Feb 01107 -4 Dec 10110 -2 Feb 01107 -35 Feb01/07 -5 Dec 101t0 -36 Feb 01101 -6 Dec 10110 02-03-1 Jan 1113 -37 Feb 01101 -7 Jul 08/13 -2 Jun 1115-38 Feb01/07 -8 Nov 28/16 -3 Jan 11/13 -39 FebOI/07 -4

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Jun 1115 -40 FebOI/07 00-03 -1 Nov28/16 -41 Feb 01/07 -2 Nov28/16 02-04 -1 Feb 01/07 -42 Mar 19107 -3 Nov 28/16 -2 Jan 11/13 -43 Apr 16/07 -4 Nov 28/16 -3 Oct 20109 -44 Jun 04/07 -5 Nov 28/16 -4 Nov 28/16 -45 Jun 08/07 -6 Nov 28/16 -5 Nov 28/16 -46 Oct 31/07 -7 Nov 28/16 -6 Oct 20/09 -47 Ocl31107 -8 Nov 28/16 DOT Approved CL-604 Air pl an e Flight Manual PSP 604- 1 aC'ND•OJO < • CHALLENGER 604 Page Date -7 Jan 11 / 13 -8 Oct 20/09 02-05 -1 Feb0 1/07 -2 Jul 08/13 -3 Feb01/07 -4 Feb 01/07 -5 Oct 31/07 -6 Feb 01/07 -7 Feb0 1/07 -8 Oct 31/07 -9 Oct 31/07 - 10 Oct 31/07 - 11 Nov 28/16 - 12 Nov 28/16 - 13 Jun 26/12 - 14 Oct 31/07 - 15 Mar 31/14 - 16 Mar 31/14 - 17 Mar 31/14 -18 Mar 31/14 -19 Mar 31/14 -20 Mar 31/14 02-06 - 1 Feb 01/07 -2 Feb 01/07 -3 Feb 01/07 -4 Feb 01/07 02-07 - 1 Feb 01/07 -2 Feb 01/07 02-08 - 1 Feb 01110 -2 Oct 01/14 -3 Oct 01/14 -4 Apr 16/07 02-09 -1 Aug 30/16 -2 Aug 30/16 -3 Aug 30/16 -4 Aug 30/ 16 03-00 -1 Nov 28/16 - 2 Jul 08/13 -3 Aug 30/16 -4 Feb 01 /07 03-01 - 1 Feb01/07 -2 Feb01 /07 DOT Approved List of Effective Pages Page Date 03-02 -1 Jun 30/11 -2 Jun 28/10 03-03 - 1 Nov 28/16 -2 Mar 11 /16 -3 Mar 16112 -4 Mar 16/12 -5 Mar 16/12 -6 Mar 16/12 -7 Mar 16/12 -a Nov 28/16 -9 Nov 28/16 -10 Mar16/12 -11 Nov 28/16 -12 Mar16/12 -13 Mar 16/12 -14 Mar 16/12 -15 Mar 16/12 -16 Nov 28/16 -17 Nov 28/16 -18 Nov 28/16 -19 Nov 28/16 -20 Nov 28/16 -21 Nov 28/16 -22 Nov 28/16 -23 Nov 28/16 -24 Nov 28/16 -25 Nov 28/16 -26 Nov 28/16 03-04 -1 Sep 25/13 -2 Sep 25/13 -3 Sep 25/13 -4 Sep 25/13 -5 Sep 25/13 -6 Sep 25/13 -7 Sep 25/13 -8 Sep 25/13 -9 Sep 25/13 -10 Sep 25/13 03-05 -1 Sep 09/ 10 -2 Sep09/ 10 -3 Jun 30/ 11 -4 Sep09/ 10 -5 Jun 30/ 11 -6 Jun 30/ 11 CL-604 Airplane Flight Manual PSP 604-1 00-03-2 REV 103, Nov 28/16 Page Date 03-06 - 1 Feb 01/07 -2 Jun 04/07 -3 Jul 08113 -4 Jul 08/13 03-07 - 1 Jun 26/12 -2 Jun 26/12 -3 Jun 26/12 -4 Sep09/10 03- 08 -1 Jul 08/13 -2 Ju l 08/13 -3 Ju l 08/13 -4 Sep 03/15 03-09 -1 Jun 28/10 -2 Jun 28/10 -3 Feb01!07 -4 Sep09/10 -5 Jun 28/10 -6 Jun 28/10 -7 Feb 01/07 -8 Sep 09/10 -9 Jun 28/10 - 10 Feb 01/07 03-10 - 1 Jun 30/11 -2 Jun 30/11 03- 11 - 1 Ocl3 1/07 -2 Oct31/07 - 3 Oct 31/07 -4 Feb 01110 03-12 - 1 Feb 01110 - 2 Feb 01110 -3 Feb 01/10 -4 Feb 01 110 - 5 Feb 01 /10 -6 Feb 01 / 10 - 7 Jun 28/10 - 8 Jun 28/10 - 9 Jun 28/10 - 10 Jun 11 /15 03- 13 - 1 Feb 01 / 07 -2 Feb 01/07 i) 0 ... .... 0 • II. "' CHALLENGER 604 List of Effective Pages 00-03-3 REV 103, Nov 28/16 Page Date Page Date Page Date 03-14 -1 Jul 08113 04-01 -1 Feb 01/07 04- 10-1 Jul 08/13 -2 Jul 08113 -2 Feb 01/07 -2 Jul 08/13 -3 Jul 08113 -3 Nov 07/08 -4 Jul 08113 04-02 -1 Jun 09/16 -4 Nov 07/08 -5 Jan 18112 -2 Jun 28110 -5 Nov07/08 -6 Feb 01/07 -3 Mar 16/1 1 -6 Nov 07/08 -4 Mar 16/1 1 03-15 -1 Aug 30/16 -5 Mar 16/1 1 04- 11 -1 Feb0 1/07 -2 Aug 30/16 -6 Jun 28/10 -2 Oct 19/15 -3 Aug 30116 -7 Mar 16/11 -4 Aug 30/16 -8 Jul08113 04-12 -1 Feb 01/07 -5 Aug 30/16 -9 Jul 08113 -2 Mar 16/12 -6 Aug 30/16 -10 Jul 06/13 -3 Mar 16/12 -7 Aug 30/16 -1 1 Nov 28116 -4 Mar 16/12 -8 Aug 30/16 -12 Nov 28116 -5 Mar 16/12 -9 Aug 30/16 -13 Jul 08/13 -6 Jun 28110 - 10 Aug 30/16 -14 Jul 08/13 - 11 Aug 30116 -15 Jul 08113 04- 13 -1 Nov 07/08 - 12 Aug 30116 -16 Jul 08113 -2 Nov 07/08 03- 16 -1 Aug 30/16 04-03 -1 Apr 16/07 04-14 -1 Nov 28116 -2 Aug 30/16 -2 Feb 01 /07 -2 Nov 28116 -3 Aug 30/16 -3 Feb 01 /07 -3 Nov 28116 -4 Aug 30/16 -4 Feb 01 /07 -4 Nov 28/16 -5 Aug 30/16 -5 Feb 01 /07 -5 Nov 28/16 -6 Aug 30/16 -6 Sep 09/10 -6 Nov 28116 -7 Aug30/16 -7 Jul 08113 -7 Nov 28116 -8 Aug30/16 -8 Jul 08/13 -8 Nov 28/16 -9 Aug 30/16 -9 Nov 28/16 -10 Aug 30/16 04-04 -1 Jut 08113 - 10 Nov 28/16 -1 1 Aug 30/16 -2 Jut 08113 - 11 Nov 28/16 -12 Aug 30/16 -3 Jut 08113 - 12 Nov 28/16 -4 Jun 28/10 03-17 -1 Aug 30/16 04- 15 - 1 Feb 01/07 -2 Aug 30116 04- 05 - 1 Feb 01/07 -2 Feb 01/07 -2 Feb01/07 - 3 Oct 20/09 03- 18 -1 Aug 30/ 16 -4 Oct 20/09 -2 Aug 30/ 16 04- 06 - 1 Feb01/07 -2 Feb01/07 04-16 -1 Oct 01/14 04-00 -1 Nov 28116 -2 Feb 01/07 -2 Jut 08/ 13 04-07 -1 Jun 04/07 -3 Jul 08/13 -2 Feb 01/07 04- 17 - 1 Oct 31 /07 -4 Nov 28/16 - 2 Feb 01 /07 -5 Nov 28116 04-08 -1 Apr 16/07 -6 Nov 28f16 -2 Fet>01/07 04-18 - 1 Feb 01107 -7 Nov 28/16 - 2 Feb 01 /07 -8 Feb01/07 04-09 -1 Feb01/07 -3 Feb 01 f07 -2 Jun 28/ 10 -4 Feb01 /07 DOT Approved CL-604 Airplane Flight Manual PSP 604-1 .o .... ... ., < • CHALLENGER 604 Page Date 04-19 -1 Nov07/08 -2 Feb01/07 -3 Feb01/07 -4 Feb01/07 -5 Feb 01/07 -6 Feb 01/07 -7 Feb 01/07 -8 Feb 01/07 04-20 -1 Mar16/1 1 -2 Nov 07/08 -3 N ov 28/16 -4 Nov 28/16 -5 Mar 16/12 -6 Jul 08/13 -7 Jan 06114 -8 Nov 28/16 -9 Nov 28/16 -10 Jul 08/13 - 11 Nov 28/16 -12 Aug 30/16 -13 Aug 30/16 -14 Aug 30/16 04-2 1 - 1 Feb 01/07 -2 Feb 01/07 05-00 - 1 Sep 03/15 -2 Jul 08/13 -3 Jun 28/10 -4 Mar 18/15 -5 Jun 28/10 -6 Nov 28/16 -7 Nov 28/16 -8 Feb 01 /07 05-01 -1 Feb01/07 - 2 Feb01/07 05-02 - 1 Jun 28/10 -2 Sep03/15 -3 Sep03/15 - 4 Sep03/15 -5 Sep03/15 -6 Sep03/15 -7 Jun 30/ 11 - 8 Jun 30/11 - 9 Jan 11 /13 -1 0 Jul 08/13 DOT Approved List of Effective Pages Page Date -1 1 Jun 30/1 1 -12 Jun 30/1 1 05-03 - 1 Mar 16/12 -2 Mar16/1 2 -3 Sep 03/15 -4 Sep 03/15 -5 Sep 03/15 -6 Sep 03/15 -7 Nov28/16 -8 Nov 28/16 05-04 - 1 Ju l 08/13 -2 Sep 03115 -3 Sep 03/15 -4 Sep 03/15 -5 Sep 03/15 -6 Sep 03/15 -7 Sep 03/15 -8 Sep 03/15 05-05 - 1 Sep 09/10 -2 Sep 09/10 -3 Sep 09/10 -4 Jan 06/14 -5 Apr 16107 -6 Jul 08/13 -7 Jan 06/14 -8 Jan 06/14 -9 Jan 06/14 -10 Jul 08/13 05-06 -1 Jun11/15 -2 Jun 11 /15 -3 Jun 11 / 15 -4 Jun 11 / 15 05-07 -1 Jun 26/ 12 -2 Jun 26/ 12 -3 Jun 26/ 12 -4 Sep 20/ 11 05-08 -1 Sep 09/ 10 -2 Sep 09/ 10 -3 Sep 09/ 10 -4 Sep 09/ 10 -5 Sep 09/ 10 -6 Sep 09/10 CL-604 Airplane Flight Manual PSP 604-1 00-03-4 REV 103, Nov 28/16 Page Date -7 Sep 09/10 -8 Sep 09/1 0 05-09 -1 Oct 31/07 - 2 Oct 31/07 -3 Mar 16/12 -4 Oct 31/07 -5 Feb 01/07 -6 Oct 31/07 -7 OC131/07 -8 Oct 31/07 05- 10 -1 Sep09/10 -2 Jun 28/10 05- 11 -1 Feb 01/07 -2 Feb 01/07 -3 Nov 07/08 -4 Feb 01/07 -5 Nov 28/16 -6 Nov 28/16 -7 Nov 28/16 -8 Oct 20/09 -9 Nov 28/16 -10 Feb 01110 -11 Nov28/ 16 -12 Nov28/ 16 -13 Feb 01/10 -14 Oct 20/09 -15 Nov28/ 16 - 16 Mar11 /16 - 17 Mar11 /16 - 18 Mar11/16 05-12 - 1 Mar 16/12 - 2 Nov 07108 - 3 Jun 28/10 - 4 Jun 28/10 -5 Feb 01 / 07 - 6 Feb 01 /07 -7 Jun 28/10 - 8 Jun 28/10 -9 Mar 16/ 11 - 10 Jun 28/10 - 11 Mar 16/1 1 - 12 Mar 16/ 11 - 13 Jun 30/1 1 - 14 Mar 31/14 - 15 Jun 28/10 • 0 ••• • ,. ' CHALLE:NGE:R 604 Page Date -16 M ar 16111 -17 Mar 16111 -18 Mar 16111 -19 Mar 16111 -20 Jun 28/10 -21 Mar 16111 -22 Mar31114 -23 Mar 31114 -24 Jun 28/10 -25 Mar 16111 -26 Mar 16111 -27 Jun 28/10 -28 Jun 28/10 -29 Jun 28/10 - 30 Mar 31 / 14 - 31 Jun 28/10 - 32 Jun 28/10 05- 13 - 1 Feb 01110 -2 Feb 01 110 -3 Feb 01/07 - 4 Mar 16112 -5 Mar 16112 -6 Feb 01/07 -7 Feb01/07 -8 Feb01/07 -9 Feb 01/10 -10 Nov07 /08 -1 1 Feb 01/10 -12 Nov07 /08 -13 Feb 01/10 -14 N ov07/08 05-14 - 1 Mar 16112 -2 Mar 16112 -3 Nov 28/16 -4 Nov 28/16 -5 Feb01'10 -6 Nov 28/16 -7 Nov28:16 -8 Sep09110 -9 Nov 28;16 -10 Feb 01110 -1 1 Nov 28/16 -12 Nov28/16 -13 Nov 28/16 -14 N ov28/16 DOT Approved List of Effective Pages Page Date 05-15 -1 Aug 30116 -2 Aug 30116 -3 Aug 30/16 -4 Aug 30116 -5 Aug 30116 -6 Aug 30116 05-16 - 1 Nov07 /08 -2 Nov07/08 -3 Nov07/08 -4 Mar 16111 -5 Mar 16111 -6 Nov 07 / 08 -7 Nov 07 / 08 - 8 Nov 07 / 08 - 9 Nov 07/08 - 10 Nov 07/08 05 - 17 - 1 Jun 04/07 - 2 Feb01/07 - 3 Aug30 /16 -4 Feb01/07 05-18 - 1 Feb01/ 10 - 2 Mar 16/12 -3 Mar 16112 - 4 Feb01/07 06-00 - 1 Feb01 /07 -2 Nov 07/08 -3 Nov07/08 -4 Nov07 /08 -5 Nov 07/08 -6 Nov 07108 06-01 - 1 Feb01/07 -2 Feb01/07 -3 Feb 01'07 -4 Feb Oli07 -5 Feb 01 /07 -6 Feb 01 / 07 -7 Feb 01 / 07 -8 Feb 01 / 07 -9 Feb 01 / 07 - 10 Feb 01 / 07 - 11 Feb 01 / 07 - 12 Feb 01/07 - 13 Feb 01/07 - 14 Feb 01/07 CL-604 Airplane Fllgh1 Manual PSP 604-1 00-03-5 REV 103 , N ov 28/16 Page Date -15 Feb 01/07 -16 Feb 01/07 -17 Feb01/07 -18 Feb01/07 -19 Feb 01/07 -20 Fe b 01/07 -21 Feb 01/07 -22 Feb 01/07 -23 Feb 01/07 -24 Feb 01/07 -25 Feb 01/07 -26 Feb 01/07 -27 Feb 01/07 -28 Feb 01/07 -29 Feb 01/07 -30 Feb 01 / 07 06-02 -1 Feb 01 / 07 -2 Feb 01 / 07 -3 Feb 0 1/ 07 -4 Feb 01 / 07 -5 Feb 0 1/ 07 -6 Feb 0 1/07 -7 Feb 0 1/07 -8 Feb 01/07 -9 Feb 01/07 -10 Feb 01/07 -11 Feb 01/07 -12 Feb 01/07 -13 Feb 01/07 -14 Feb 01/07 -15 Feb 01/07 - 16 Feb 01101 -17 Feb 01/07 - 18 Feb 01/07 - 19 Feb 01/07 -20 Feb 01/07 -2 1 Feb 01107 -22 Feb 01/07 06-03-1 Sep09110 -2 Feb 01/07 -3 Feb 01/07 -4 Feb 01/07 -5 Feb 0 1/07 -6 Jan 06/14 -7 Feb 0 1/07 -8 Jan 06/ 14 -9 Feb 0 1101 • c .•• • ' CHALLeNGeR 604 Pa ge Date -10 Feb 01/07 -11 Feb01/07 -12 Feb 01/07 -13 Feb 01/07 -14 Feb 01/07 -15 Feb01/07 -16 Nov07108 -17 Feb 01/07 -18 Feb 01/07 -19 Feb 01/07 -20 Feb 01 / 07 - 21 Feb 01 / 07 -22 Feb 01/07 -23 Feb 01/07 -24 Feb 01/07 -25 Feb 01/07 -26 Feb 01/07 -27 Feb 01/07 -28 Sep 09/10 -29 Feb 01101 - 30 Feb 01/07 06-04 - 1 Feb 01107 - 2 Feb 01107 -3 Feb 01107 -4 Feb 01107 -5 Feb 01101 -6 Feb 01101 7 Feb 01/07 - 8 Feb 01107 -9 Feb 01/07 - 10 Feb 01101 -11 Feb 01107 -12 Feb 01/07 -13 Feb01/07 -14 Feb01/07 -15 Feb01/07 -16 Feb01107 - 17 Feb 01101 - 18 Feb01107 06-05 -1 Feb 01/07 -2 Feb 01/07 -3 Feb01/07 -4 Feb 01/07 -5 Feb 01/07 -6 Feb 01/07 -7 Feb 01107 -8 Feb 01/07 DOT Approved Li st of Effective Pages Pag e Date 06-06 -1 Feb 01/07 -2 Feb 01/07 -3 Feb01/07 -4 Feb 01/07 -5 Feb01/07 -6 Feb 01 /07 -7 Feb01/ 07 -6 Feb01/ 07 -9 Feb01/07 -10 Feb01/ 07 -11 Feb01/07 -12 Feb01/07 -13 Feb01/07 -14 Feb01/07 - 15 Feb01/07 -16 Feb01/07 -17 Feb01/07 -18 Feb0 1/07 06-07 - 1 Feb0 1/07 -2 Feb01/07 -3 Feb 01/07 -4 Feb01/07 -5 Feb01/07 -6 Feb01/07 -7 Feb01/07 -8 Feb01/07 -9 Feb01/07 - 10 Feb01/07 06-08 - 1 Feb01/07 -2 Feb01/07 -3 Feb 01/07 -4 Feb 01107 -5 Feb01/07 -6 Feb01/07 07-00-01 -1 Jun 09'16 -2 Jun 09116 07-01-00 -1 Feb01/07 -2 Feb01/07 07-01-01 -1 Oct 19/15 -2 Oct 19115 07-01A-OO - 1 Oct19/15 -2 Oct 19/15 CL-604 A ir plane Fligh1 Manual PSP 604-1 00-03-6 REV 103, Nov 28/16 Page Date 07-01A-01 -1 Oct 19115 -2 Oct 19115 07-02-00 -1 Feb 01/07 -2 Feb 01/07 -3 Feb 01/07 -4 Feb 01/07 07-02-01 -1 Feb01/07 -2 Feb 01 /07 -3 Feb01 / 07 -4 Feb 01/07 -5 Feb 01/07 -6 Feb 01/07 -7 Feb 01/07 -8 Feb 01/07 -9 Feb 01107 -10 Feb 01107 -11 Feb 01107 -12 Feb 01107 -13 Feb 01107 -14 Feb 01107 -15 Feb 01107 -16 Feb 01107 -17 Feb 01107 -18 Feb 01107 -19 Feb 01 107 -20 Feb 01/07 -21 Feb 01/07 -22 Feb 01/07 -23 Feb 01/07 -24 Feb 01107 -25 Feb 01/07 -26 Feb 01/07 -27 Feb 01/07 -28 Feb 01/07 -29 Feb 01/07 -30 Feb 01101 -3 1 Feb 01/07 -32 Feb 01/07 -33 Feb 01/07 -34 Feb 01/07 -35 Feb 01/07 -36 Feb 01/07 -37 Feb 01/07 -36 Feb 01/07 -39 Feb01107 -40 Feb 01/07 41 Feb 01101 eo,.•O•IIIOoC .. CHALLENGER 604 Page Date -42 Feb0 1/07 -43 Feb01/07 -44 Feb01/07 - 45 Feb01/07 -46 Feb01/07 - 47 Feb01/07 -48 Feb01/07 07- 03-00 -1 Feb01/07 -2 Feb01/07 07-03-01 -1 Feb 01/07 -2 Feb01/07 -3 Feb01/07 -4 Feb 01 / 07 -5 Feb 01 / 07 -6 Feb 01 / 07 -7 Feb 01 / 07 -8 Feb 01 / 07 -9 Feb 01 /07 -10 Feb 01/07 -11 Feb 01/07 -12 Feb 01 / 07 07-04-00 -1 Feb 01/07 -2 Feb 01 / 07 07-04-0 1 -1 Jan 11/13 -2 Apr 16/07 -3 Feb 01/07 - 4 Feb 01110 -5 Feb 01/07 - 6 Feb 17/09 - 7 Feb 01 /07 - 8 Feb 01 /07 - 9 Feb 01 /07 - 10 Feb 01 /07 07-04A-OO -1 Feb 01/07 -2 Feb 01/07 07-04A-01 -1 Feb 01/07 -2 Jan 11 / 13 -3 Feb 01/07 -4 Feb0 1/07 -5 Feb 01/ 10 -6 Feb0 1/07 -7 Feb 17/09 -8 Feb0 1/07 DOT Approved List of Effective Pages Page Date -9 Feb 01/07 - 10 Feb 01 /07 - 11 Feb 01/07 - 12 Feb 01/07 -13 Feb 01/07 - 14 Feb 01107 07-049-00 -1 Feb 01/07 -2 Feb 01/07 07-049-01 -1 Feb 01/07 -2 Jan 11/13 -3 Feb 01 /07 -4 Feb 01 /07 -5 Feb 01 / 10 -6 Feb 01/07 -7 Feb 17/09 -8 Feb 01 /07 -9 Feb 01 /07 - 10 Feb 01/07 - 11 Feb 01/07 - 12 Feb 01/07 - 13 Feb 01/07 - 14 Feb 01/07 07-06- 00 - 1 Feb 01/07 -2 Feb 01/07 07-06-01 - 1 Feb 01/07 - 2 Feb 01/07 07-07-00 -1 Feb 01 /07 -2 Feb 01 /07 07-07-01 -1 Feb 01 /07 -2 Aug 30/16 -3 Feb 01 / 07 -4 Feb01 /07 07-08-00-1 Aug 30/16 -2 Jan 18/12 07-08-01 - 1 Oct 31/07 -2 Oct 19/15 -3 Oct 19/15 -4 Feb01 /07 -5 Oct 31/07 -6 Oct 31/07 -7 Oct 31/07 CL-604 Airplane Flight Manual PSP 604-1 00-03-7 REV 103, Nov 28/16 Page Date -8 Oct 31/07 -9 Oct 31/07 - 10 Oct 31/07 - 11 Oct 31/07 - 12 Jan 18/12 -13 Oct 31/07 - 14 Oct 31/07 - 15 Oct 31/07 - 16 Oct 31/07 - 17 Oct 31/07 - 18 Oct 31/07 - 19 Oct31107 -20 Jan 18/12 -21 Jan 18/12 - 22 Jan 18/12 -23 J an 18/12 -24 Aug 30/16 07-09-00 -1 Feb 01/10 -2 Feb01/07 07-09-01 -1 Feb01/10 -2 Feb 01/10 -3 Feb01/07 -4 Feb01/07 07-10-00 -1 Feb 01/07 -2 Feb0 1/07 07-10-01 -1 Feb 01/07 -2 Feb0 1/07 -3 Feb 01/07 -4 Feb0 1/07 07- 11 - 00 -1 Feb 17/09 -2 Jun 08/07 07-1 1-0 1 - 1 Feb 17/09 -2 Feb 17/09 -3 Feb 011 10 -4 Feb 17/09 07-12-00 -1 Jun11/15 -2 Oct 31/07 07-12-01 -1 Jun 08/07 -2 Jun 11115 -3 Jun 08/07 -4 Jan11/13 uo~••#fQ•Il#f CHALLeNGeR 604 Page Date -5 Jun 08/07 -6 Jun 08/07 -7 Jun 08/07 -8 Jun 08/07 -9 Jun 08/07 -10 Jun 08/07 07- 13-00 -1 Sep09/ 10 -2 Sep 09/10 07-13-01 -1 Sep 09/10 -2 Sep 09/10 -3 Sep 09/10 -4 Sep 09/10 - 5 Sep 09/10 -6 Sep 09/10 - 7 Sep 09/10 -8 Sep 09/10 -9 Sep 09/10 - 10 Sep 09/10 - 11 Sep 09/10 - 12 Sep 09/10 - 13 Sep 09/10 -14 Sep 09/10 - 15 Sep 09/10 -16 Sep09/10 -17 Sep09/10 -18 Sep09/10 -19 Sep09/10 -20 Sep09/10 -2 1 Sep 09/10 -22 Sep 09/10 -23 Sep 09/10 -24 Sep 09/10 -25 Sep 09/10 -26 Sep 09/10 -27 Sep 09/10 -28 Sep 09/10 -29 Sep 09/10 -30 Sep 09/10 -31 Sep 09/10 -32 Sep 09/10 -33 Sep 09/10 -34 Sep 09/10 -35 Sep 09/10 -36 Sep 09110 -37 Sep 09/10 -38 Sep 09/10 -39 Sep 09/10 DOT Approved List of Effective Pages Page Date -40 Sep09/10 -41 Sep09/10 -42 Sep09/10 07- 14-00 -1 Aug 30/16 -2 Mar 16/11 07- 14-01 -1 Aug 30/16 -2 Mar 16/1 1 -3 Mar 16/1 1 -4 Mar 1611 1 -5 Mar 1611 1 -6 Mar 1611 1 -7 Jan 18/12 -8 Mar 1611 1 -9 Aug 30/16 - 10 Aug 30/16 07-15-00 -1 Jan 18/12 -2 Jan 18/12 07- 15-01 -1 Jan 18/12 -2 Jan 18/12 07-16-00 -1 Jan 06114 -2 Jan 06/14 07-16-01 -1 Jan 06/14 -2 Jan 06/14 -3 Jan 06/14 -4 Jan 06/14 -5 Jan 06/14 -6 Jan 06/14 08-00-00 -1 Feb 01/07 -2 Feb 01/07 08-01-00 -1 Feb 01/07 -2 Feb 01/07 08-01-01 -1 Jan11/13 -2 Feb 01/07 08-01-23 -1 Oct31/07 -2 Feb01/07 08-01-32 -1 Feb01/07 -2 Feb01/07 CL-604 Airplane Flight Manual PSP 604-1 00-03-8 REV 103, Nov 28/16 Page Date 08-01-33 -1 Feb 01/07 -2 Feb 01/07 08-01-51 -1 Mar 16/1 1 -2 Feb 01/07 08-01-52 -1 Feb01/07 -2 Feb 01/07 -3 Feb0 1/07 -4 Feb0 1/07 08-01-53 - 1 Feb0 1/07 - 2 Feb01 /07 08 -01-55 - 1 Feb 0 1/07 - 2 Feb 01/07 -3 Feb 01/07 - 4 Feb 01/07 08-01 -56 - 1 Feb 01/07 - 2 Feb 01/07 08-01-57 - 1 Feb 01/07 -2 Feb 01/07 -3 Feb 01/07 - 4 Feb 01/07 -5 Feb 01 /07 -6 Feb 01 /07 I I I I I • • • ' EMERGENCY PROCEDURES CHALL~NG~R 604 Table of Contents CHAPTER 3- EMERGENCY PROCEDURES TABLE OF CONTENTS INTRODUCTION General Landing Distance Factors REJECTED TAKE- OFF ReJected Take-Off TABLE OF CONTENTS Rejected Take-Off Before Achteving V1 POWER PLANT Power Plant Engine Fire/Severe Engtne Damage (In Flight) Engine Fire/Severe Engine Damage (On Ground) Double Engine Failure Jet Pipe Overheat Engine Oil Pressure Low Uncommanded Thrust Reverser Deployment Post-Shutdown Engine Tall Ptpe Fire N 1/N2 Overspeed Engtne Overtemperature Engtne Starter Fails to Cutout Uncommanded Acceleration SMOKE OR FIRE Smoke/Fire/Fumes Smoke/Fire/Fumes Procedure Smoke or Fumes Removal Procedure AIR-CONDITIONING AND PRESSURIZATION Air-Condittoning and Pressurization Emergency Descent Procedure Uncontrollable Loss of Cabin Pressure High Rate of Cabin Pressurization or Over-Pressurization [oar Approved CL-604 Airplane Flight Manu al PSP 604-1 03-00-1 REV 103 , Nov 28/16 Page 03-00-1 03- 0 1-i 03-01-1 03-02-1 03-02-1 03-03-1 03-03-1 03-03-4 03-03-5 03-03-14 03-03-15 03-03-16 03-03-21 03-03-22 03-03-23 03-03-24 03-03-26 03-04-1 03-04-1 03-04-8 03-05-1 03-05-1 03-05-2 03-05-5 I I I .. ,- .... 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EMERGENCY PROCEDURES CHALLI:NGER 604 Table of Contents AUTOMATIC FLIGHT CONTROL SYSTEM Automatic Flight Control System Autopilot Failure AFCS Messages Failure Uncommanded Yaw Motion AUXILIARY POWER PLANT Auxlltary Power Plant APU Fire APU Overspeed APU Overtemperature BLEED AIR LEAKS Bleed Air Leaks 1OTH Stage, Left Bleed Duct Failure 1OTH Stage, Right Bleed Duct Failure 14TH Stage, LefVRight Bleed Duel Failure DITCHING AND FORCED LANDING Dttching and Forced Landing Dtlching or Forced Landing lmmtnent Planned Ditching Forced Landtng EMERGENCY EVACUATION Emergency Evacuation Emergency Evacuation Procedure ELECTRICAL Electrical Loss of All Normal Electrical Power FLIGHT CO NTRO LS Fltght Controls Atleron System Jammed Elevator System Jammed Rudder System Jammed [cor Approved CL-604 Airplane Flight Manual PSP 604-1 03-Q0-2 REV 89, Jul 08/13 Page 03-06-1 03-06- 1 03-06-2 03-06-3 03- 07- 1 03-07 - 1 03-07-2 03-07-3 03-08-1 03-08-1 03-08-3 03-08-4 03-09-1 03-09 -1 03-09-3 03-09 - 7 03-10-1 03-10 -1 03-11-1 03-11-1 03-12-1 03-12-1 03-12-3 03-12-5 I I I I I I I I I I I - • EMERGENCY PROCED URES CHALLE:NGE:R 604 T able of Contents FLIGHT CONTROLS Stabilizer Trim Runaway Stall Recovery FUEL SYSTEM Fuel System Low Fuel ICE AND RAIN PROTECTION Ice and Rain Protection Wing leading Edge Overheat Fuselage/Wing Anti-Ice Duc1 Failure INSTRUMENTS SYSTEM Instruments System Unreliable Airspeed LANDING GEAR, WHEEL AND BRAKE SYST EM landing Gear, Wheel and Brake System Gear UP Disagree Gear ON Disagree landtng Gear lever Jammed tn the UP Posilton landtng Gear Up/Unsafe Landtng Procedure Main landing Gear Bay Overheat Warntng Nose Door Fails Open Parking Brake On Excessive Asymmetry or Loss of Braking PASSENGER DOOR Passenger Door Passenger Door Failure AURAUVtSUAl WARNING SYSTEM AuraVVtsual Warning System Configuration Warning [ DOT Approved CL-604 Airplane Flight Manual PSP 604-1 03-00-3 REV 102, Aug 30/16 Page 03-12-7 03-12-10 03-13-1 03-13-1 03-14-1 03-14-1 03-14- 3 03-1 5-1 03- 15- 1 03-16- 1 03-16-1 03-16-2 03-1~ 03-16- 5 03-16-8 03-16-9 03-16-10 03-16-11 03-17-1 03-17-1 03-18-1 03-18-1 • . .... c CHALLeNGER 604 DOT Approved EMERGENCY PROCEDURES Table of Contents THIS PAGE INTENTIONALLY LEFT BLANK CL-604 Airplane Flight Manual PSP 604-1 03-0Q--4 REV 66. Feb 01/07 o o .-.. • .-•P • cn CHALLeNGeR 604 1. INSTRUMENTS SYSTEM A. Unreliable Airspeed EMERGENCY PROCEDURES 03-15-1 Instruments System REV 102, Aug 30/16 Indication: • Pitch attitude. thrust setting or external noise not consistent with indicated airspeed. • Large airspeed difference between PFDs and/or Standby Airspeed Indicator. • Loss of multiple airspeed indication. • EFIS COMP MON and EF IS COMP INOP caution messages on and/or amber lAS flag. Respect stall warni ng and stick pusher. (1) Autopilot ................................... ... ................. Disconnect (2) FDs ................................................................... Deselect Above minimum safe alt itude : (3) Proceed to step (6). Below minimum safe altitude: (3) Pltch/N 1 •.. • .• . •. . •••••• ••••. •.•••••••••••••••••••••••••.• 15 degrees/TO (4) Go-around ........................................................... Initiate Clean up and climb above When above 15,000 feet: (5) Pitch/N 1 • .•.• .. •.•...•••..•. . •. •.•.••••••••••••••• •• •• •• 10 degrees/CLB DOT Approved Cl-604 Airplane Flight Manual PSP 604-1 minimum safe altitude. • 0 &f • • • • • EMERGENCY PROCEDURES 03-15-2 CHALLENGER 604 Instruments System REV 102, Aug 30/16 1, INSTRUMENTS SYSTEM (CO NT'D) A. Unreliable Airspeed (Cont'd) When above minimum safe altitude: (6) Pilch/N 1 ................... . ............ ... ~ ................... .... ........ Set as per Table A to achieve approximate level flight. TABLE A- LEVEL FLIGHT CRUISE- FLAP 0 Expected WEIGHT kg (lb) Indicated Airspeed 11,794 13,608 15,876 18,144 20,412 21 ,772 KIAS MACH{26,000) (30,000) (35,000) (40,000) (45,000) (48,000) Pitch (0 ) 1.0 1.5 2.0 2.5 210 . 71 0 to to <t N, (o/o) 83.0 84.6 87.2 89.9 250 .82 Pitch (•) 1.5 2.0 2.5 2.5 3 .0 230 .69 ll) to to "' N, (o/o) 81 .8 82.7 83.9 85.7 87 .9 270 .80 Pitch (0 ) 1.5 2.0 2.5 2.5 3 .0 3.0 240 0 to "' N, (o/o) 79.9 80.4 81.3 82.3 83 .8 84.7 290 - :: Pitch (0 ) 0 1. 5 2.0 2.5 2.5 3 .0 3.0 2400 Ill to q N N, (o/o) 76.3 76 .7 77.5 78.3 79.5 80.3 r::: 290 w Pitch (0 ) 1.5 2.0 2.5 3.0 3.0 3.5 240 0 ::l 0 to 1:: N N, (o/o) 72 .9 73.3 74.0 74.9 75.9 76.7 290 1- ..J <t Pitch (0 ) 1.5 2.0 2.5 3.0 3.0 3.5 240 Ill to ... N, (o/o) 70 .5 70.8 71.5 72.3 73.3 74.0 290 Pitch (0 ) 2.0 2.5 3.5 4.0 4.5 5.0 205 0 to ... N, (o/o) 58.0 58.9 60.2 61.7 63.1 63.9 235 Pitch (•) 2.5 3.0 3.5 4.5 5.0 5.5 200 ll) N, (o/o) 54.8 55.7 570 58.3 59.7 60.5 to 230 If any Indicated speed is outside the expected Indicated airspeed range, It should be considered UNRELIABLE. DOT Approved NOTE EFIS Comparator Failure procedures for EFIS COMP MON and EFIS COMP INOP caution messages and/or amber lAS flag are contained within this procedure. CL-604 Airplane Flight Manual PSP 604-1 IJ<',., ... .,o,cn EMERGENCY PROCEDURES 03-15-3 CHALLENGER 604 I nstru ments System REV 102, Aug 30/16 1. INSTRUMENTS SYSTEM (CONT'D) A . Unreliable Airspeed (Cont"d) (7) Autopilot or FD .................................................. Engage basic PTCH/ROLL. NOTE 1. AutopiloVyaw damper should only be engaged once N1 is set. 2. Pitch/Thrust settings will give approximate level flight. and may result in slight climb or descent. Adjust pitch to stop climb/descen t. 3. Disregard low speed cue and airspeed trend vector as these may be erroneous. 4. If overspeed warn in g sounds, select the affected AUDIO WARNING switch to mute aural a nd disregard. 5. A nuisance NOSE DOOR O PEN warning message can be disregarded. 6. Al titude, Mode C and TCAS may be in error up to 600 feet. Vertical speed in dications may also be unreliable. 7. Groundspeed indication may be unreliable. 8. FMS cruise time and fuel predictions may be incorrect. 9. Mach trim may be inoperative or operate erratically. Disengage Mach trim if erratic stabilizer motion is observed. 10. Using the FD/autopilot in PTCH. ALT. H OG and ROLL modes will help reduce workload. Do not use FLC mode. (8) When the airplane is stabilized, proceed to TROUBLESHOOTING within this section to regain use of PFD/airspeed if possible. DOT Approved CL-604 Airplane Flight Manual PSP 604-1 • . < EMERGENCY PROCEDURES 03-15-4 CHALLENGER 604 Instruments System REV 102, Aug 30 /16 1. INSTRUMENTS SYSTEM (CO NT' D) A. Unreliable Airspeed (Cont'd) TROUBLESHOOTING {1) ADC source select or ...................................•........ Select to NORM. (2) Both PFDs and standby airspeed indicator . ................... ..................... ........ .. .. Compare airspeed. (3) Determine which of the following conditions apply: • If no indica ted airspeed is considered reliable, proceed to CONDITION D. • II both PFDs agree and the Indicated airspeed is considered reliable, proceed to CONDITION A. • If one PFD and the standby airspeed indicator agree and t he indicated airspeed ts considered reliable, proceed to CONDITION B. • II only one indica ted airspeed is considered reliabl e, proceed to CONDITION C. • WARNING I An airspeed should only be constdered reliable tf tt is consistent with pitch, thrust, extemal noise and the expect ed airspeed from Table A CONDITION A If both PFDs agree and the Indicated airspeed Is consistent with pitch , thrust , external noise , and the expec te d airspeed from Table A : (4) Use airspeed/altitude inlormatton per normal operations (5) Accomplish rematning CAS messages. ------ -END ---- --- CONDITION 8 If one PFD and the standby airspeed i nd icato r agree andthe indicated airspeed is consistent with pitch , thrust , external noise , and the expected airspeed from Table A: (4) Autopilot ....................................................... Disconnect (5) FDs ............................................................... Deselect (6) ADC source selector .. .•••............... ••..• . Select to reliable side. Refer to Chapter 6; PERFORMANCE. lor altemate static system position error correction charts. (7) FDs .. Engage If desired (8) Autopilot •.•••............. ••.•................. Engage tf desired (9) Use airspeedfaltttude tnformation per normal operations. (10) Accomplish remaimng CAS messages. ------- EN D---- --- DOT Approved CL-604 Airplane Flight Manual PSP 604-1 eo~••'-O'C" EMERGENCY PROCEDURES 03-15- 5 CHALLE:NGE:R 604 In stru me nts Sy s tem REV 102, Aug 30/ 16 1. INSTRUMENTS SYSTEM (CONT'D) CONDITION C If only one I nd icated ai rspeed is consistent wi th pi tch , thrust , exte rnal noise , and the expected airspeed from Table A: ~ WARNING I Do not rely on only one airspeed un less it is In agreement with the expected airspeed column in Table A. Standby airspeed indicator is identi fied as reliable airspeed source: (4) Use airspeed/altitude information per normal operations. (5) Accomplish remaining CAS messages. - END- One PFD is identified as reliable airspeed source : (4) Autopilot ....................................................... Disconnect (5) FDs .... .. ....... .. .......... ... ....................................... Deselect (6) ADC source selector ................................. .. ......... Select to reliable side. Refer to Chapter 6; PERFORMANCE, lor alternate static system position error correction charts. (7) FDs .......................... .. ........................................ Engage If desired. (8) Autopilot ............................................................ Engage If desired. (9) Use airspeed/altitude information per normal operations. (1 O) Accomplish remaining CAS messages. DOT Approved END ---- CL-604 Airplane Flight Manual PSP 604-1 • CJ ....... ~ • EMERGENCY PROCEDURES 03-15- 6 CHALLENGER 604 Instruments System REV 102 , Aug 30/16 1. INSTRUMENTS SYSTEM (CONT'D) CONDITION D If no indicated airspeed Is consistent with pitch , thrust, external noise, and the expected airspeed from Table A: (4) Airspeed indications ....................................... Disregard (5) Pilch/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, LNAV or VNAV under Visual Meteo ro log ical Conditions if possible. 3. The following may be unreliable: • Ground proximity warning • Windshear detection • Landing gear warning horn • Flap overspeed • NOSE DOOR OPEN warning message 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 procedure in order to confirm airspeed. (7) Actual landing distance .................................... Increase as applicable by factor given below: WITHOUT THRUST REVERSERS WITH THRUST REVERSERS 1.25 {25%) 1.20 (20%) (8) When ready for descent, proceed to RECOVERY TO AN AIRFIELD within this section. DOT Approved END CL-604 Airplane Flight Manual PSP 604-1 ."' ........ " • • EMERGENCY PROCEDURES 03-15-7 CHALLE:NGE:R 604 Instruments System REV 102 , Aug 30/16 1. INSTRUMENTS SYSTEM (CONT'D) RECOVERY TO AN AIRFIELD When ready to commence descent: (1) ANTI-ICE, WING swHch .............................. As required (2) ANTI-ICE, Land R COWL switch/lights ............................................. ... . As required (3) Pitch .....................................................................Adjust per Table Band continue to adjust pitch during descent. TABLE 8 ·DESCENT- FLAPS 0 ·IDLE Altitude (ft) 0 5,000 10,000 15,000 20,000 25 ,000 30 ,000 35,000 Pitch (0 ) -1.0 -1. 0 - 1.0 -1. 0 -2.0 -2.0 -2.0 -1.5 (4) Thrust levers...................................................... .... . IDLE NOTE • With anti-ice ON, increase N1 if required to obtain the minimum N2 ol78%. • For an N1 increase of 5% , add 0.5• to the pitch from Table B. • For an N1 increase of 10%. add 1• to the pitch from Table B. • For an N1 increase of 15%, add 2• to the pitch from Table B. Do not select flaps to 20• 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 and slowed down before flaps can be extended. (5) Descent Check ............................................ Accomplish (6) In-Range Check .. ........................................ Accomplish DOT App ro ved NOTE Plan to intercept a long final to allow ti me to re-configure for approach/landing and set pitch/N1• CL-604 Airplane Flight Manual PSP 604-1 40,000 -1.5 •<-~··411fl) ' . EMERGENCY PROCEDURES 03-15-8 CHA L LE:NGE:R 604 Instruments System REV 102. Aug 30/16 1. INSTRUMENTS SYSTEM (CO NT' D) If Intermediate level off is required during the descent: (7) Pitch/N1 .................................................................... Set as per Table C, then adjust pitch to stop climb/descent. TABLE C -LEVEL FLIGHT CRUISE- FLAP 0 Expected WEIGHT kg (lb) Indicated Airspeed 11,794 13,608 15,876 18 ,144 20,412 21 ,n2 (26,000) (30,000) (35,000) (40,000) (45,000) (48,000) KIAS MACH Pitch (•) 1.5 2.0 2.5 2.5 3.0 230 .69 "' to to "' N1 (%) 81.8 82 .7 83.9 85 .7 87.9 270 .80 I:: Pitch (•) 1.5 2.0 2.5 2.5 3.0 3.0 240 0 to 0 "' N1 (%) 79.9 80.4 81.3 82 .3 83.8 84.7 290 0 <:!_ Pitch (•) 1.5 2.0 2.5 2.5 3.0 3.0 240I!: w "' to 0 N N1 (%) 76.3 76.7 77.5 78.3 79.5 80.3 290 =>..... Pitch (0 ) 1.5 2.0 2.5 3.0 3.0 3.5 240 ~ 0 to ~ N N1 (%) 72 .9 73.3 74.0 74.9 75.9 76.7 290 Pitch (•) 1.5 2.0 2.5 3.0 3.0 3.5 240 II) to ... N1 (%) 70.5 70.8 71.5 72.3 73.3 74.0 290 If any Indicated speed Is outside the expected indicated airspeed range, it should be considered UNRELIABLE. For continued descent: (8) Pitch ..................................................................... Adjust per Table D and continue to Altitude (It) 0 Pitch (0 ) -1.0 DOT Approved adjust pitch during descent. TABLE 0- DESCENT- FLAPS 0 -IDLE 5,000 10,000 15,000 20,000 -1.0 -1.0 -1.0 -2.0 CL-604 Airplane Flight Manual PSP 604-1 25,000 30,000 35,000 40,000 -2.0 -2.0 -1.5 -1 .5 • 0 "" . .. ill C) ' . EMERGENCY PROCEDURES 03-15- 9 CHALLE:NGE:R 604 Instruments System REV 102, Aug 30/16 1. INSTRUMENTS SYSTEM (CONT'D) At Initial approach altitude: (9) Pitch/N1 .•.•.•...•..................•••.•.•.•.•••.•.•.••••••••.••••.•••••••• Set as per Table E, then adjust pitch to stop climb/descent. TABLE E- LEVEL FLIGHT APPROACH- FLAP 0 Expected WEIGHT kg (I b) Indicated Airspeed 11,794 13,608 15 , 876 18,144 20 ,412 21 ,772 KIAS (26,000) (30,000) (35,000) (40,000) (45,000) (48,000) Pitch (0 ) 2.0 2.5 3.5 4 .0 4.5 5.0 205 It) to ~ N1 (%) 61.1 62.2 63.6 65.3 67.0 68.0 240 ~ ::: c Pitch (•) 2.0 2.5 3.5 4.0 4.5 5.0 205 c c to <=!. ~ N1 (%) 58.0 58.9 60.2 61.7 63.1 63.9 ~ 235 ~ w Pitch (•) 2.5 3 .0 3.5 4 .5 5.0 5.5 200 c;::) It) to ~ N1 (%) 54.8 55.7 57.0 58.3 59.7 60 .5 230 ..J <( Pitch (0 ) 2.5 3.0 3.5 4.5 5.0 5.5 200 c N1 (%) 51.9 52.7 53.9 to 55.2 56.5 57.3 230 If any indicated speed Is outside the expected indicated airspeed range, it should be considered UNRELIABLE. DOT Approved NOTE Allow sufficient time for stabilization prior to re-configuring the airplane due to the pitch change as flaps are extended from o to 20. CL-604 Airplane Flight Manual PSP 604-1 • •• • • • EMERGENCY PROCEDURES 03-15-10 CHALLENGER 604 Instruments System REV 102, Aug 30116 1. INSTRUMENTS SYSTEM (CONT' O) When stab ili zed : ( 10) FLAPS ..................................................................Select to 20 . ( 11 ) Pitch/N1 ... ................................................................. Set as per Table F, then adjust pitch to stop climb/descent. TABLE F- LEVEL FLIGHT APPROACH- FLAPS 20- GEAR UP WEIGHT kg (lb) 11,794 13,608 15 ,876 18 ,144 20,412 21 ,772 (26,000) (30,000) (35,000) (40,000) (45,000) (48,000) Pitch (") 0.5 1.0 2.0 3.0 4.0 4.5 N, ( o/o) 61 .5 62.3 63.5 64 .9 66.6 676 (12) Final course ..................................................... Intercept Upon Intercept of final course (long final): (13) LOG GEAR lever ............................................... Select to ON. (14) FLAPS .................................................................. Select to 30 ". (15) Pitch/N1 .................................................................... Set as per Table G, then adjust pitch to stop climb/descent. TABLE G- LEVEL FLIGHT APPROACH- FLAPS 30 - GEAR ON Pi tch (") N1 ('l'o) WEIGHT kg (lb ) 11,794 13,608 15 ,876 18 , 144 20 ,412 ( 26 , 000 ) ( 30 ,000) ( 35 ,000) (40,000) (45, 00 0) -2 .0 -1.0 0.5 1.5 3.0 71 2 72.0 73 .0 74 .0 75 1 Do not descend for final approach with flaps 30 . The a1rcratt must remain level with gear down/flaps 30 ° or a nap overspeed and flap damage could result . Flaps 45• Is selected at the start of the descent on the glideslope/glldepath. 21 ,772 (48,000) 3.5 75.9 lo CL-604 Airplane Flight Manual DOTAp_p_ro_ v_ed __ _L______ __________________________ ~-------------J PSP 604-1 • ~ .. . .. . 0 ' . EMERGENCY PROCEDURES 03-15-11 CHALLENGER 604 Instruments System REV 102 , Aug 30/16 1. INSTRUMENTS SYSTEM (CONT'D) At glideslope capture or descent point : (16) FLAPS ............................................. ... .................. Se lect to 45 ". ( 17) Pitch/N 1 ................... .... ..................... .. ....... .. .. . Re-adjust as follows: TABLE H- APPROACH- FLAPS 45- GEAR ON- 3• GIS WEIGHT kg (lb) 11 ,794 13 ,608 15,876 18,144 20 ,412 (26,000) (30,000) (35,000) (40,000) (45,000) Pitch(") - 3.0 -3.0 -3.0 -3.0 -3.0 15,000 N, (%) 65.5 67 .7 71.2 77.3 74.9 E' Pitch (•) - 2.5 -2.5 -2.5 -2.5 -2.5 - 10,000 w N, (%) 60.8 62.5 66.3 69.8 72.8 0 ::J Pitch (•) 1- -2.0 -2.0 -2.0 -2.0 -2.0 ~ 5,000 N, (%) 55.9 57 .9 61.4 65.0 67.9 <( 0 Pitch (•) -2.0 -1.0 - 1.0 -1.0 -1.0 N, (%) 52.5 53.4 56.7 59.9 62.8 This table results in airspeeds equal to VR eF ~10 kts. ( 18) Pitch ......................................................................... Sel to maintain glideslope/giidepath. (19) N1 ................ .... .. .... .......... .... ..................................... Set as per Table H. (20) Before Landing Check ................................. Accomplish NOTE In the event of a go-around, perform the go-around in accordance with the boxed actions at the beginning of this procedure. DOT Approved END CL-604 Airplane Flight Manual PSP 604-1 21 ,772 (48,000) -3.0 76.7 -2.5 74.6 -2.0 69 .4 -1.0 64.2 OCt"'" <lifO> < • CHALLENGER 604 DOT Approved EMERGENCY PROCEDURES Instruments System THIS PAGE INTENTIONALLY LEFT BLANK CL- 604 Airplane Flight Manual PSP 604-1 03-15-12 REV 102 , Aug 30/16

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