# 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 16/2011m"T1"T1m0-l<=i)>rr011"'0-'-)>O:IJ1_,orvIll..........cn-ui\)llla<a_.,CD............SourceDocumentRef.No.Chapter5TaskNo.RBR604-16721-31-00-101**Rev.E7.1.1.50(twostars)RBR604-11921-33-01-101**Rev.B-37.1.1.9(twostars)TaskTitleTaskIntervalFunctionalTestoftheOutflowValves.1600HOperationalTestoftheCabinPressure2400HAcquisitionModule.AllowableExtension'40H40H00•;x:0......,...,.i'-'tl-1,.,...f:!...""'0m 

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_.m _.I\) 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 Interval Allowable Extension 4800H 40H 0 

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### ....o.w 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 Interval
Functional Test of the Generator Control Unit 1600 H

(GCU) Overvoltage Protection Circuits. Operational Test of the Air Driven Generator 1600 H

(ADG). or24 M

NOTE : Whichever interval occurs first. See NOTE Allowable Extension 40 H 40H 0 

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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- 1 02 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 Interval Operational Test of the Roll Disconnect System. 800 H
Functional Test of the Aileron Power Control 800 H

Units (PCUs). Detailed Inspection of the Aileron Flutter 800 H

Damper . Functional Test of the Rudder Backlash

. 800 H Operational Test of the PCU Load Limiters

. 3200 H
Functional Test of the Pitch Feel S i mulator. 1600 H Operational Test of the Elevator Disconnect 800 H

System . Functional Test of the Elevator Backlash. 800 H
Functional Test of the Elevator Flutter Dampers

. 4800 H

Detailed Inspection of the Elevator Flutter 800 H
Dampers. Allowable Extension 40H 40 H 40 H 40 H 40H 40 H 40 H 40H 40H 40H I ' 0 

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# I 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 Interval 4800 

### H 300 

### H COMPONENT 100 H COMPONENT 7200 H COMPONENT 1600 H 400 H Allowable Extension 40 H N/A N/A 40 H 40H 40 H i 0 

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# I 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 Pr i mary Spur Gear. Task Interval 

### 9600 H COMPONENT or 8420 L COMPONENT whichever occurs first ' Allowable I Extension I 

### N/A 0 

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# ~(h **~**m,.,,.,m<)>rr01I""U-t.)>OJJ01\)c....c............""'0!\)Illo<O_.coSourceDocumentRBR604-103Rev.C-4Add.3IRBR604-111Rev.NC-3Ref.No.Chapter5TaskNo.-27-42-01-111*7.1.14(onestar)27-51-04-101•7.1.1.1(onestar)TaskTitleNOTE:Whenthistaskisperformed,creditcanbetakenfortask27-42-01-111*andMRB27-40-00-202andtheirtimeresettozero.Repeatintervalfortask27-42-01-111*is5000H.DetailedInspectionoftheHorizontalStabilizerTrimActuator(HSTA)SecondaryLoadPathIndicator,PartNo.604-92305-7andSubs(VendorPartNo.8454-3andSubs).NOTE:Whentask27-42-01-109*,VSB8454-27-008,orMRB27-40-00-202areperformed,creditcanbetakenfortask27-42-01-111*anditstimeresettozero.Repeatintervalfortask27-42-01-111*is5000H.FunctionalTestoftheFlapControlUnit(AllDrivers-OnCircuit).TaskIntervalAllowableExtension5000HN/ACOMPONENT4800H40H0001g;t())i3:....013:....-1'II..!!!"'0"'(/)

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_.CD **~CXl** Source Document Ref. No. Chapter 5 Task No

. RBR604-300 27-53-00-101 ••
Rev.F4 (two stars) Task Title Restoration of the Outboard Flap Actuator

P/N 600-93000-113/-114/-115/-116
where the component flight cycles are known P/N 600-93000-113/-114/-115/-116

for replaced actuators where the total component flight cycles are unknown.

The 2000 landing interval to be calculated from the date of TR 5-2-6

(May 12/201 0). PHASE-IN: For actuators that have exceeded 9600 landings, replace the actuator within 300 hours of the date on

TR

5-2-6 or by Dec 31/2010, whichever
occurs first. NOTE: During restoration

, the following components must be replaced: Worm
Gear, P/N 2041076 Helical Gear, P/N 2041074 or 2041077 Retaining Key, P/N NAS558-P404-2 Torque Shunt Washer, P/N 2047125 Thrust Bearing, P/N NT A 1828 Thrust Washer

, P/N TRA 1828 Task Interval 9600 L COMPONENT 2000 L COMPONENT Allowable Extension 50 L 50 L 0 

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_.<1> .::>.co 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 Interval
Functional Test of the Tail Tank Restrictor. 

### 15000 H Operational Test of the Auxiliary Power Unit 

### 2400 H

(APU) Fuel Feed Shutoff-Valve and Negative-G Shutoff-Valve for Internal Leaks. Operational Test of the Dump Valve. 

### 400 H Allowable Extension 

### 50H 40H 40 H

0 

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# Source Document Ref. No. Chapter 5 Task No.
RBR604 -1 67 30-11-00-101 ••

Rev . A Add

. 1 7

. 1

. 1

. 50 (two stars) 

# Task Title Task Interval

Detailed Inspection of the Wing Anti-Ice Duct 6400 H

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. Allowable Extension 

# 40 H 0 

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### om ............ **~** ...... 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 Interval Allowable Extension 6400 H 40H 0 

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# 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 Interval 

# See NOTE 5000 H COMPONENT Allowable Extension 1 

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