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CHALLENGER 605 | Time Limits I Maintenance Checks

BOMBARDIER CHALLENGER 605 · Maintenance Manual

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Overview

This document outlines the time limits and maintenance checks for the Bombardier Challenger 605 aircraft. It includes airworthiness limitations, life limits for structures and systems, and maintenance requirements approved by Transport Canada.

  • Document is for Bombardier Challenger 605 maintenance.
  • Includes airworthiness limitations approved by Transport Canada.
  • Specifies mandatory discard times for structural life limits.
  • Records of maintenance checks are required.
  • Life limits for components are detailed.
  • Document is proprietary and confidential.
  • Revisions are recorded for updates.
  • Contact information for Bombardier support is provided.

Document

Source

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

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Document details

Type
·
Maintenance Manual
Year
·
2016
File size
·
651 KB
Publisher
·
regulations.gov
Language
·
en
About this document
What is the CHALLENGER 605 | Time Limits I Maintenance Checks?

The CHALLENGER 605 | Time Limits I Maintenance Checks is a maintenance manual for the BOMBARDIER CHALLENGER 605, dated 2016.

Where does the CHALLENGER 605 | Time Limits I Maintenance Checks come from?

This copy of the CHALLENGER 605 | Time Limits I Maintenance Checks was originally published by regulations.gov and is hosted on Sprinkle as a free, searchable reference copy.

What year was the CHALLENGER 605 | Time Limits I Maintenance Checks published?

The CHALLENGER 605 | Time Limits I Maintenance Checks — the BOMBARDIER CHALLENGER 605 maintenance manual on file — is dated 2016.

Documentation completeness
2/7

Most owners only have the POH. Here's the essential set for the BOMBARDIER CHALLENGER 605.

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

More BOMBARDIER CHALLENGER 605manuals & documents

In this document

Airworthiness Limitations

Specifies maintenance required by applicable airworthiness or operational rules.

Life Limits (Structures)

Details mandatory discard times for structural life limits of safe-life items.

Life Limits (Systems)

Outlines life limits for various aircraft systems.

Maintenance Checks

Describes the required maintenance checks and intervals.

Records and Reports

Emphasizes the importance of maintaining records of maintenance activities.

Certification Maintenance Requirements

Lists rules applicable to certification maintenance requirements.

Safety notes

  • Discard is mandatory at the expiration of specified structural life limits.
  • Individual component utilization must be recorded from initial installation.
  • Modification or reverse engineering of the document is prohibited.
  • All rights to intellectual property belong to Bombardier.
  • Use of the document is solely for maintenance, operation, or repair.

Full document text

Time Limits I Maintenance Checks MODEL NC EFFECTIVllY Cl-600-28 1G CCL-605 1 5-01 AND SUBS BOMBARDIER CHALLENGER 605 Publication No. CH 605 TLMC CHALLENGER* 605 TIME LIMITS I MAINTENANCE CHECKS Bombardier Aerospace P. 0. Box 6087, Station Centre-ville Montreal, Quebec, Canada H3C 3G9 http://www.cic.bombardier.com For more Information please contact Bombardier Business Aircraft Customer Support Technical Publications and Information Distributio n North America 1-866-273-2638 Outside North America 514-855-2751 Fax 514--855-2770 Ord eri ng To ease the ordenng process. tile following Document ldentiftcahon Number should be used: CH 605 TLMC Us er Comment Group 514-855-2373 Email bbad.user.comments@aero.bombardier com It Is understood that this documentation, comprising technical data and other Information in any media shall not be reproduced or disclosed In whole or In pan w•thoul Bombardier's wntten authorization. is proprietary and confidential to Bombardier and tllat all rights to patent. copyright, trademark, trade secret and other Intellectual property rights therein belong to Bombardier Such documen!abon. technical data and other information shall not be modified, translated, reverse assembled, reverse engineered or de-compiled and shall be used solely to maintain. operate or repair the atrcrafl. BOMBARDIER Copyright C l006 by Bombardier Inc All rights r...ervo<l "Tr.3domalk. of Bombard ier In c. or It& subsidJaOes Prirned m canada REVISION NO. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 110/<tfBARDI~R CHALLENGER 605 Cl- 605 TIME LIMITS/MAINTENANCE CHECKS RECORD OF REVISIONS A signature in the "INSERTE D BY" column shows lhal the pub li cation holder has incorporated the revision . ISSUE DATE DATE INSERTED Aug 1212009 Aug 1212009 Dec 10/2010 Dec 10/2010 Mar 16/2011 Mar 16/2011 Jun 30/2011 Jun 30/2011 Jan 18/2012 Jan 18/2012 Jun 2612012 Jun 2612012 Jan 11/2013 Jan 11/2013 Jul 0812013 Jul 0812013 Jan 0612014 Jan 06/2014 Jul 11 /2014 Jul1 1120 14 Jan 21/2015 Jan 21/2015 Jun 11/2015 Jun 1112015 Dec 01/2015 Dec 0112015 Jun 09/20 16 Jun 0912016 INSERTED BY Bombardier Bombardier Bombardier Bombardier Bombardier Bombardier Bombardier Bombardier Bombardier Bombardier Bombardier Bombardier Bombardier Bombardier DOMDARDI«R CHALLENGER 60S CL-605 TIME UMITSIMAINTENANCE CHECKS PART2 AIRWORTHINESS LIMITATIONS The Ailworthiness Limitations section is approved by Transport Canada and specifies maintenance required by any applicable airworthiness or operational rule unless an alternative program has been approved by the Minister of Transport. Approved by: Roop Dhaliwal Acting Chief. Engineering Airworthiness Branch. Transport Canada PART2 Cover Ju111 / 2014 BO M SAROIIrR CHALLENGER 605 CL~5 TIME LIMITS/MAINTENAN CE CHECKS PART2 AIRWORTHINESS LIMITATIONS LIST OF EFFECTIVE PAGES Section Effectivity Page Date Section Effectivity Page Date nile Page Cover Jul 1112014 5- 10-t9 ALL Jul11 12 014 Effective Pages 1 Jun 09120 16 5-10-25 Cover Jul11/2014 2 Jun 09120 16 5- 10-25 ALL Jul11 /2014 Effective Temporal)! Revisions Jun 09120 16 5-10-26 Cover Jul11 12014 Contents Jul1112014 5-10- 26 ALL Ju l 1112014 5-10-00 ALL 1 Jul1lf2014 5-10-30 Cover Ju l 1112014 5-10-05 ALL 1 Jul1 112014 5-10-30 ALL 1 Jul 111201 4 2 Jul1 112014 2 Ju t 1112014 3 Jul 1112014 3 Jun 0912016 4 Jun 09120 16 4 Jul 1 112014 5 Jun 0912016 5 Jul 11/2014 6 Jun 09/2016 6 Jan 2112015 7 Jun 09/2016 7 Dec 0112015 8 Jul1112014 5-10-10 ALL 1 Jul11/201 4 9 Jul1112014 2 Jul 11/2014 10 Jut 1112014 3 Jul 1112014 11 Jul1 112014 4 Jun 1112015 12 Jan 2112015 13 Jan 21/2015 5-10-11 ALL 1 Jul1112014 14 Jan 2112015 2 Jun 0912016 15 Jul11/2014 16 Dec 01/2015 5-10-13 ALL 1 Jul 1112014 17 Jul11/2014 2 Jul11/2014 18 Jul11/2014 19 Jul11/2014 5-10-15 ALL Jul 11 /2014 20 Jun 09/2016 21 Jul11/2014 5-10-19 Cover Jul11/2014 22 Jul1112014 23 Jul11/2014 24 Jul1112014 25 Jul1112014 26 Jul1112014 IEFFECTIVITY' AU PART2 Page 1 EFFECTIVE PAGES Jun 09/2016 Section Effectivity 5-10-30 ALL 5-10-40 5-10-40 ALL EFFECTIVITY: ALL QOMIJARDIER CHALLENGER 605 CL--605 TIME UMITS/MAINTENANCE CHECKS Page 27 28 29 30 Cover 1 2 3 4 5 6 7 8 9 10 11 12 13 14 Date Jul11/2014 Jul 11/2014 Jul 11/2014 Jul 1 112014 Jul1112014 Jun 09/2016 Jul11/20 14 Jul11/2014 Jul11f2014 Jul1112014 Jul11/2014 Jun 11/2015 Jun 11/2015 Jun 11/2015 Jun 11/2015 Jun 09/2016 Jun 09/2016 Jun 09/2016 Jun 09/2016 Section Effectivity Page PART2 EFFECTIVE PAGES Date Page2 Jun 09/2016 BO MDAR DI ER CHALLENGER 605 Cl-605 TIME U MITSIMAINTENANCE CHECKS PART2 AIRWORTHINESS LIMITATIONS TABLE OF CONTENTS Subject Section AIRWORTHINESS LIMITATIONS 5-10-00 Introduction and Rules 5-10- 05 Gene ral Scope Records an d reports Rules Ap pl icable to Airworthiness Umitations (Section 5- 10-30) Ru les Applicable to Certification Maintenance Requirements (section 5-1 0-40) Life Limits (Structures) 5-10-10 Life Limits (Systems) 5-10-11 RVS M Qualified Aircraft 5-10-13 Time Limits- Structures Service Bulletin 5-10-15 Incorporation Time Limi ts by A ircraft Effectivity 5-10-19 Introduc ti on Organization Tasks by Aircraft Effectivity- Custom Installations 5-10-25 Introduction Organization Tasks by Aircraft Effectivity - Repai rs 5-10-26 Introduction Organization Airworth iness Limitation Items 5-10-30 Ce rtification Maintenance Requirements 5 -1 0-40 EFFECTIVITY· ALL PART 2 CONTENTS Page 1 1 3 3 4 i 1 1 1 1 Page 1 Jul 11/2014 BOMBARO I BR CHALLENGER 605 Cl~OS TIME liMITS/MAINTENANCE CHECKS LIFE LIMITS (STRUCTURES) 1. The structural life limits of the Safe-Life items shown on the pages that follow are taken from the Structural Airworthiness Control Document. Discard is mandatory at the expiration of the specified structural life limit for the item. These life limit values may be superceded by the life limits contained in section 5-10-19 , for specific serialized components.

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~: Individual Main and Nose Landing gear component utilization must be recorded from the time of initial installation. IEFFECTIVITY ALL PART2 5-10-10 Page 1 Jul 11 /2014 m .,., m g < ~ )> F 01 t""'' ~)> O:IJ ~--~ Ql\) t.. £. - --u ~., ~~ .1>1\) Source Document Ref. No . Chapter 5 Task No . RAS6040X-990 27-15-04-101 • Rav. - (one star) RAS6040X- 990 27-42-01-101. Rev.B6 (one star) RAS6040X-990 27-42-01-108. Rev.B6 (one star) RAS6040X-990 32-11-00-102. Rev.B-9 (one star) RA$6040X-990 32-11-00-103. Rev.- (one star) RAS6040X-990 32-11-07-101 • Rev. - (one star) RAS6040X-990 32-11-07-102. Rev.-- (one star) RAS6040X-990 32-11-07-103. Rev.- (one star) RAS6040X-990 32-11-07-104 • Rev.- (one star) RAS6040X-990 32-11-10-101. Rev.- (one sta,r) Task Title Discard of the Aileron Anlifloat Spring, Part No . 600-10057-5/-6. Discard of the Horizontal Stabilizer Trim Actuator (HSTA), Part No. 604-92305-31517 (Vendor Part No. 6454-1/2/3). Discard of the Horizontal-Stabilizer Trim-Actuator (HSTA) Trunnion Support; Part No. 601 R92386-1/--3 and Hardware; Part No.s NAS6206-SD/-14D/-20D Discard of the Main Landing Gear (MLG) Filling, Part No. 19062-1 /-2 (NHA 19064-1031-104/-105/-1 06). Discard of the Main Landing Gear (MLG) Pintle Pin , Part No. 19036-3. Discard of the MLG Shock Strut Upper Pin, Part No. 19134-3. Discard of the MLG Shock Strut Lower Pin, Part No. 19146-3. Discard of the MLG Shock Strut Piston, Part No. 1911 4-1/-3 (NHA 19115-101/-103) . Discard of the MLG Shock Strut Cylinder, Part No. 19104-1/-3 (NHA 19105-101 /-1 03). Discard of the Main Landing Gear (MLG) Trailing Arm, Part No. 19083-3 (NHA 19064-103). Task Interval 10000 L COMPONENT 20000 L COMPONENT 20000 L COMPONENT 19250 L COMPONENT 19250 L COMPONENT 19250 L COMPONENT 19250 L COMPONENT 19250 L COMPONENT 19250 L COMPONENT 36430 L COMPONENT n ~ o llJ~ ;r: C) i )) l ~ ,.. Ill !!: ,.. ~ i ~ ~~ n o ~ "' -~ !!! ~ z "' ~ );1 0) ~ () ~ (II ""' m 'T1 'T1 m(') -i < ~ l> F 01 1""'0 ....... )> o:n ~--~ orv c.. £. - ~-u -"' "'co '="' ... ,., Source Document RAS604DX-990 Rev.- RAS6040X- 990 Rev. - RAS6040X-990 Rev. - RA$604DX-990 Rev. - RAS604DX- 990 Rev. - RAS604DX- 990 Rev. - RAS604DX- 990 Rev.A- 3 RAS604DX-990 Rev. - RAS604DX- 990 Rev.- RAS604DX- 990 Rev. - Ref. No. Chapter 5 Task No. 32- 11 - 10- 102. (one slar) 32-11-13-101. (one star) 32-2t-00-102. (one star) 32-21-00-103. (one star) 32- 21 - 00- 104. (one slar) 32 - 21 - 00-105. (one Slar) 32- 21-00-106. (one star) 32- 21-00-107. (one star) 32-21-07-102. (one star) 32-21-07-103. (one slar) Task Tille Discard or the MLG Main Rtting!Trailing Arm Pivot Pin, Part No. 19039-1 . Discard of the Main Landing Gear (MLG) Axle, Part No. 19050-3. Discard ol the NLG Main Fitting, Part No. 20081 1316 or 20091-1 (NHA 200811269 or 20090-101). Discard of the NLG Pivot (Trun ion) Pin (Main Fitting to Aircraft). Part No. 20081 1601. Discard ol the NLG Shock Strut Sliding Tube, Part No . 200811707. Discard or the NLG Drag Brace Lower Link, Part No. 200814311 (NHA 200814213). Discard of the NLG Drag Brace Upper Link, Part No. 20049- 11-3 (NHA 20050 -10 1). Discard of the NLG Drag Brace Hinge Pin, Part No. 200814624. Discard of the NLG Attachment Pin (Main Fit11ng to Drag Brace}. Part No. 200811721. Discard of the NLG Drag Brace Upper Pivot Pin, Part No. 200814601. Task Interval 19250 L COMPONENT 19250 L COMPONENT 19480 L COMPONENT 19480 L COMPONENT 19480 L COMPONENT 19480 L COMPONENT 19480 L COMPONENT 19480 L COMPONENT 19480 L COMPONENT 19480 L COMPONENT 0 ~ () b 5l ;x: 0 ~ )) 1 m ,... " r- 3: ,... ~ ~ ~ ~ !!: 1:'\ " ~ 'II ., ~ Ill .. ~ ~ . ~ 0') ~ 0 ~ <II ""' 01 m -n ..,m g < ~ )> F I -u_.)> OJJ .!_.-; 01\) <- c: ::> ~ ~-o i\)D> o<D ~ "' (II A I I Source Document Ref. No . Chapter 5 Task No . RAS60<1DX-990 32-21-13-101 • Rev.- (one star) RAS60<1DX-990 32-21-13-102. Rev. - (one s tar) RAS60<1DX-990 32-32-01-102 • Rev. - (one star) RAS60<1D X-990 32-32-01-103. Rev.- (one star) RAS60<10X-990 32-32-01-104. Rev. - (one star) RAS60<10X-990 32-32- 01 - 105. Rev.A-3 (one star) RAS60<1 DX-990 32-32-04- 101 • Rev. B18 (one star) RAS6040X-990 32-33-04-101 • Rev. B18 (one star) RAS6040X-990 57-24-00-101 • Rev. AS (one star) RASSO<IOX-990 57-50-00- 120 • Rev. - 4. 1.74 (one sta r) Task Title Discard of the NLG A~le FiHl ng, Part No. 200811308 ( NHA 200811218). Discard of the NLG Pin. Sliding Tube to End Fitting, Part No. 200811602. Discard of the M ain Landing Gear (MLG) Stay Side Pin, Part No. 6318-1/-3 (N HA 6350-1/-3). Discard of the Main Landing Gear (MLG) Side-Stay-Actuator Eye -Bolt (Rod- End), Part No. 19400 -2 (NHA 19400- 1). Discard of the Main Landing Gear (MLG) Side Slay Actuator Cylinder, Part No. 17027- 8 (NHA 17027 -9). Discard of the Main Landing Gear (MLG) Side Stay Actuator Piston, Part N o. 17014-6/-8. Discard of the Main Landing Gear (MLG) Uplock Assembly, Part No. 601RB5001-11/-31. Discard of the Nose Landing Gear (NLG) Uplock Assembly, Part No. 601 R85002-9/-91/-93. Discard of the Main Landing Gear (MLG) Side Brace Filling Shall, Part No. 601R10237-1/-3 Discard of the Inboard Flap Vane Beam, Part No. 600-14250-1 5/25/27/29. Tas k Interval 19480 L COMPONENT 19480 L COMPONENT 19250 L COMPO NENT 43890 L COMPONENT 43890 L COMPONENT 43890 L COMPONENT 140291 L COMPONENT 57229 L COMPONENT 60000 L COMPONENT 9600 L COMPONENT n ~ Oo 5: ;t 0 ~ li t ~ .... ..:E .... . ~ ~ ~ 1!: " 0 ~ "' -~ 111 "' ~ :tJ ~ ~ 0) ~ 0 ~ 01 "'en