Time Limits I 

Maintenance Checks 

MODEL NC EFFECTIVITY 

CL-600-2816 (CL-605) 5701 AND SUBS 

BOMBARDIER 

CHALLENGER 605 

Publication No. CH 605 TLMC 
REVISION NO. 

1 

2 

3 

4 

5 

6 

7 

8 

9 

10 

BOMBARDIER 

CHALLENGER 605 

CL-605 TIME LIMITS/MAINTENANCE CHECKS 

RECORD OF REVISIONS 

A signature in the "INSERTED BY" column shows that 

the publication holder has incorporated the revision. 

ISSUE DATE DATE INSERTED 

Aug 12/2009 Aug 12/2009 

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 26/2012 Jun 26/2012 

Jan 11/2013 Jan 11/2013 

Jul 08/2013 Jul 08/2013 

Jan 06/2014 Jan 06/2014 

Jul11/2014 Jul11/2014 

INSERTED BY 

Bombardier 

Bombardier 

Bombardier 

Bombardier 

Bombardier 

Bombardier 

Bombardier 

Bombardier 

Bombardier 

Bombardier 
BOMBARDIER 

CHALLENGER 605 

CL-605 TIME LIMITS/MAINTENANCE CHECKS 

PART2 

AIRWORTHINESS LIMITATIONS 

The Airworthiness 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 

Mar 16/2011 
BOMBARDII!R 

CHAL.L.ENGER 605 

CL-605 TIME LIMITS/MAINTENANCE CHECKS 

PART2 

AIRWORTHINESS LIMITATIONS 

LIST OF EFFECTIVE PAGES 

Section Effectivity Page Date Section Effectivity Page Date 

Title Page Cover Mar 16/2011 5-10-25 ALL Mar 16/2011 

Effective Pages 1 Jul11/2014 5-10-26 Cover Mar 16/2011 

2 Jul11/2014 

5-10-26 ALL Mar 16/2011 

Effective Temporary 

Revisions Jul11/2014 5-10-30 Cover Mar 16/2011 

Contents Jun 30/2011 5-10-30 ALL 1 Jul11/2014 

2 Mar 16/2011 

5-10-00 ALL Mar 16/2011 3 Jan 11/2013 

4 Mar 16/2011 

5-10-05 ALL 1 Mar 16/2011 5 Mar 16/2011 

2 Jan 06/2014 6 Jan 11/2013 

3 Jan 06/2014 7 Mar 16/2011 

4 Mar 16/2011 8 Mar 16/2011 

9 Mar 16/2011 

5-10-10 ALL 1 Mar 16/2011 10 Mar 16/2011 

2 Jul11/2014 11 Jan 18/2012 

3 Jul11/2014 12 Jan 18/2012 

4 Jul11/2014 13 Jan 18/2012 

14 Jan 18/2012 

5-10-11 ALL 1 Mar 16/2011 15 Jan 11/2013 

2 Jul 08/2013 16 Jan 11/2013 

17 Jul 08/2013 

5-10-13 ALL 1 Mar 16/2011 18 Jan 18/2012 

2 Mar 16/2011 19 Jan 18/2012 

20 Jan 18/2012 

5-10-15 ALL Mar 16/2011 21 Jan 18/2012 

22 Jan 11/2013 

5-10-19 Cover Mar 16/2011 23 Jan 18/2012 

24 Jan 18/2012 

5-10-19 ALL Mar 16/2011 25 Jan 18/2012 

26 Jul 08/2013 

5-10-25 Cover Mar 16/2011 27 Jul11/2014 

28 Jul 08/2013 

29 Jan 18/2012 

30 Jan 18/2012 

EFFECTIVITY: ALL PART2 Page 1 EFFECTIVE PAGES Jul11/2014 
Section Effectivity 

5-10-40 

5-10-40 ALL 

EFFECTIVITY: ALL 

BOMBARDIER 

CHALLENGER 605 

CL-605 TIME LIMITS/MAINTENANCE CHECKS 

Page 

Cover 

1 

2 

3 

4 

5 

6 

7 

8 

9 

10 

11 

12 

Date 

Mar 16/2011 

Mar 16/2011 

Mar 16/2011 

Mar 16/2011 

Mar 16/2011 

Jan 11/2013 

Jul11/2014 

Jul11/2014 

Jul11/2014 

Jul11/2014 

Jul11/2014 

Jul11/2014 

Jul11/2014 

Section Effectivity Page 

PART2 

EFFECTIVE PAGES 

Date 

Page 2 

Jul11/2014 
IJOMIJARDI£R 

CHAL.L.ENGER 605 

CL-605 TIME LIMITS/MAINTENANCE CHECKS 

PART2 

SECTION 5-1 0-40 

CERTIFICATION MAINTENANCE REQUIREMENTS 

Tasks by Chapter 5 Task Number 

EFFECTIVITY: ALL PART2 

5-10-40 Cover Mar 16/2011 
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Source Document Ref. No. Chapter 5 Task No. 

RBR604-167 21-31-00-101 ** 

Rev. E 7.1.1.50 (two stars) 

RBR604-119 21-33-01-101 ** 

Rev. B-3 7.1.1.9 (two stars) 

Task Title Task I

Functional Test of the Outflow Valves. 

Operational Test of the Cabin Pressure 

Acquisition Module. 
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Source Document Ref. No. 

RBR604-160 

Rev. NC-2 7.1.1 

Chapter 5 Task No. Task Title 

22-22-00-101 ** Operational Test of the Yaw Damper Linear 

(two stars) Actuators (SVL-4000 Relays). 

Task I
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Source Document Ref. No. Chapter 5 Task No. 

RBR604-129 24-21-00-101 * 

Rev. F-2 7.1.1 (one star) 

RBRB04-129 24-23-00-101 . 

Rev.F-2 7.1.2, 7.1.8 (one star) 

Task Title Task I

Functional Test of the Generator Control Unit 

(GCU) Overvoltage Protection Circuits. 

Operational Test of the Air Driven Generator 

(ADG). 

NOTE: Whichever interval occurs first. See 
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Source Document 

RBR604-105 

Rev. A-2 

RBR604-1 67 

Rev. E 

RBR604-167 

Rev. E 

RBR604-167 

Rev.E 

RBR604- 108 

Rev. NC-3 

RBR604-102 

Rev. A- 3 

RBR604-102 

Rev. A-3 

RBR604- 167 

Rev.E 

RBR604-102 

Rev. A- 3 

RBR604-102 

Rev.A-3 

Ref. No. Chapter 5 Task No. 

27-13-04-101 * 

7.1.1 .3 (one star) 

27-14-01-101 •• 

7.1.1 .51 (two stars) 

27-15-07-101 •• 

7.1.1.50 (two stars) 

27-21-00-101 •• 

7.1.1 .50 (two stars) 

27-23-00-101 •• 

7.1.1 .2 (two stars) 

27-31-13-102 •• 

7.1.1.10 (two stars) 

27-32-00-101 * 

7.1.1 .5 (one star) 

27-33-01-101 • 

7.1.1.50 (one star) 

27-34-04-101 • 

7.1.1.8 (one star) 

27-34-04-1 02 •• 

7.1.1.7 (two stars) 

Task Title Task I

Operational Test of the Roll Disconnect System. 

Functional Test of the Aileron Power Control 

Units (PCUs). 

Detailed Inspection of the Aileron Flutter 

Damper. 

Functional Test of the Rudder Backlash. 

Operational Test of the PCU Load Limiters. 

Functional Test of the Pitch Feel Simulator. 

Operational Test of the Elevator Disconnect 

System. 

Functional Test of the Elevator Backlash. 

Functional Test of the Elevator Flutter Dampers. 

Detailed Inspection of the Elevator Flutter 

Dampers. 
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Source Document Ref. No. Chapter 5 Task No. 

MBR604-112 27-35-01-105 •• 

Rev. C-1 (two stars) 

27-35-04-101. 

(one star) 

RSI C-1830 

Rev. NC N/A 

RBR604-300 

Rev. E 3.10.1 

RBR604-112 27-35-04-1 02 • 

Rev. C-1 7.1.10 (one star) 

RBR604-300 27-35-10-101 •• 

Rev. E 3.11 .1 (two stars) 

RBR604-103 27-41-00-101 •• 

Rev. C-3 Add 2 7.1.1 (two stars) 

Task Title 

Functional Test for the Flap and Sideslip 

Compensation Monitor of the Stall Protection 

System 

Functional Test of the Angle of Attack (AOA) 

Transducer Linearity 

Part Number 600-59154-3 

Part Number 600-59154-5 

Restoration of the Angle of Attack (AOA) 

Transducer, Part No. 600-59154-5 

Functional Test for the Stall Protection System 

(SPS) Stick Pusher Capstan Shaft, Part No. 

600-59156-7 (Vendor Part No. 501-1258-01) 

Operational Test (BITE) of the 

Horizontal-Stabilizer Trim-Control System 

(HSTCS) 

PHASE-IN: For aircraft with more than 400 

hours since task 27-41-00-201 was done, this 

task must be accomplished at or before the next 

400 hour inspection but no later than May 01, 

2013, whichever occurs first. 

Task I

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Source Document Ref. No. Chapter 5 Task No. 

RBS-604-1 00 27-42-01-109 . 

Rev. E-25 Add. 21 2.1 (one star) 

Task Title 

Restoration (Overhaul) of the Horizontal 

Stabilizer Trim Actuator, Part No. 604-92305-7 

and Subs (Vendor Part No. 8454-3 and Subs) 

PHASE-IN: As follows or as mandated 

per AD: a) 500 H from January 31/2014 with 

a calendar cap of November 2015 for the 

units exceeding either 9600 H or 8420 L, 

whichever comes first, or b) No PHASE-IN 

for all other HSTAs. 

NOTE: Remove HST A from aircraft and send 

to vendor for the following: 

1. Vendor to perform restoration and replace 

the parts that follow: Primary Housing P/N 

8396-140 (included in P/N 8396-1 00) and 

Subs, Secondary Housing P/N 261881804 

(included in P/N 8396-2030) and Subs, 

Secondary Spur Gear (CH2) P/N 

261405307 and Subs, Primary Pinion 

(CH1) P/N 8396-043 and Subs, and 

Secondary Pinion (CH2) P/N 8396-044 

and Subs 

2. Vendor to perform the following tasks: 

Functional Check of the Torque Limiters, 

Detailed Inspection of the Secondary Load 

Path Indicator, and Special Detailed 

Inspection of the Primary Spur Gear. 

Task I

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Source Document 

RBR604-103 

Rev. C-4 Add. 3 I 

RBR604- 111 

Rev. NC-3 

Ref. No. Chapter 5 Task No. 

-

27-42-01-111 * 

7.1.14 (one star) 

27-51-04-101 • 

7.1.1.1 (one star) 

Task Title 

NOTE: When this task is performed, credit 

can be taken for task 27-42-01-111 * 

and MRB 27-40-00-202 and their 

time reset to zero. Repeat interval for 

task 27-42-01-111 *is 5000 H. 

Detailed Inspection of the Horizontal Stabilizer 

Trim Actuator (HST A) Secondary Load Path 

Indicator, Part No. 604-92305-7 and Subs 

(Vendor Part No. 8454-3 and Subs). 

NOTE: When task 27-42-01-109*, VSB 

8454-27-008, or MRB 27-40-00-202 are 

performed, credit can be taken for task 

27-42-01-111 * and its time reset to zero. 

Repeat interval for task 27-42-01-111 * is 

5000 H. 

Functional Test of the Flap Control Unit (All 

Drivers-On Circuit). 

Task I

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Source Document 

RAP604- 172 

Rev. J13 

RBR604-167 

Rev.E 

RBR604-167 

Rev. E 

Ref. No. Chapter 5 Task No. 

28-15-43-1 01 •• 

(two stars) 

-· 28-24-00-1 01 • 

7.1.1.50 (one star) 

28-31-00-101 • 

7.1.50 (one star) 

Task Title Task I

Functional Test of the Tail Tank Restrictor. 

Operational Test of the Auxiliary Power Unit 

(APU) Fuel Feed Shutoff-Valve and Negative-G 

Shutoff-Valve for Internal Leaks. 

Operational Test of the Dump Valve. 
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Detailed Inspection of the Wing Anti-Ice Duct 

Piccolo- Tube. NOTE: Consideration should be given to accomplishing this task in conjunction with task 57-10-00-208 which requires the removal of the wing leading edge. 
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Source Document Ref. No. Chapter 5 Task No. 

RBR604-133 36-21-00-101 * 

Rev. A Add. 1 7.1 .1.1 (one star) 

Task Title 

Functional Test of the Leading Edge Thermal 

Switches 

NOTE: Consideration should be given to 

accomplishing this task in conjunction with task 

57-10-00-208 which requires the removal of 

the wing leading edge 

Task 
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............ ~I\) Source Document Ref. No. Chapter 5 Task No. RBR604-300 76-11-00-101 •• Rev.E 3.9.1 (two stars) RBR604-300 Rev. F2 Add 2 Task Title Functional Test of the Engine Throttle Control Gearbox Part No. 2800140-005/-007 NOTE: Threshold (T) interval is 1600 H. First Repeat (R1) interval is 1600 H. Next Repeat (R2) is 1600 H. Subsequent Repeat intervals (R3) are 1000 H. Part No. 2100140-010 Task 

Se

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