# Time Limits 

# I

Maintenance Checks

MODEL A/C EFFECTIVITY

CL

- 600-2816 (CL-604) 5301 TO 5665



# BOMBARDIER 

# CHALLENGER 604

Publication No

. CH 604 TLMC

# REVISION NO.

1

2

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5

6

7

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9

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11

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14

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22 BOMBARDIER 

# CHALLENGER 604

CL-604 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

Jan 30/98 Jan 30/98

May 01/98 May 01/98

Sep 11/98 Sep 11/98

May 20/99 May 20/99

Oct 15/1999 Oct 15/1999

Feb 14/2000 Feb 14/2000

Dec 15/2000 Dec 15/2000

Jul27/2001 Jul27/2001

Feb 03/2003 Feb 03/2003

Jun 21/2004 Jun 21/2004

Jun 21/2005 Jun 21/2005

Jan 10/2007 Jan 10/2007

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

Jul 11/2014 Jul11/2014 INSERTED BY

Bombardier

Bombardier

Bombardier

Bombardier

Bombardier

Bombardier

Bombardier

Bombardier

Bombardier

Bombardier

Bombardier

Bombardier

Bombardier

Bombardier

Bombardier

Bombardier

Bombardier

Bombardier

Bombardier

Bombardier

Bombardier

Bombardier

# BOMBARDIER 

# CHALLENGER 604

CL-604 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 : Robert 

# J. Mather

Chief

, Engineering Airworthiness Branch, Transport Canada



# PART2 Cover

Mar 16/2011

# BOMBARDIER 

# CHALLENGER 604

CL-604 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 Cover Mar 16/2011

Effective Pages 1 Jul11/2014 5-10-25 

# ALL Mar 16/2011

2 Jul 11/2014

5-10-26 Cover Mar 16/2011

Effective Temporary

Revisions Jul11/2014 5-10-26 

# ALL Mar 16/2011

Contents Jan 06/2014 5-10-30 Cover Mar 16/2011

5-10-00 

# ALL Mar 16/2011 5-10-30 

# ALL 1 Jul11/2014

2 Mar 16/2011

5-10-05 

# ALL 1 Mar 16/2011 3 Jan 11/2013

2 Jan 06/2014 4 Mar 16/2011



# 3 Jan 06/2014 5 Mar 16/2011

4 Jan 06/2014 6 Mar 16/2011

5 Mar 16/2011 7 Mar 16/2011

8 Mar 16/2011

5-10-10 

# ALL 1 Mar 16/2011 9 Mar 16/2011

2 Jul11/2014 10 Mar 16/2011

3 Jul11/2014 11 Jan 18/2012

4 Jul11/2014 12 Jan 18/2012

13 Jan 18/2012

5-10-11 

# ALL 1 Mar 16/2011 14 Jan 18/2012

2 Jan 11/2013 15 Jul 08/2013

3 Jul 08/2013 16 Jul 08/2013

17 Mar 16/2011

5-10-13 

# ALL 1 Mar 16/2011 18 Mar 16/2011

2 Mar 16 / 2011 19 Mar 16 / 2011

20 Mar 16/2011

5-10-15 

# ALL Mar 16/2011 21 Jan 11/2013

22 Jan 18/2012

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

24 Jan 18/2012

5-10-19 

# ALL Mar 16/2011 25 Jul 08/2013

26 Mar 16/2011

27 Jul 11/2014

28 Jul 08/2013



# EFFECTIVITY: ALL 

# PART2

Page 1 

# EFFECTIVE PAGES Jul11/2014

# Section Effectivity

5-10-30 ALL

5-10-40

5-10-40 ALL



# EFFECTIVITY: ALL BOMBARDIER 

# CHALLENGER 604

CL-604 TIME LIMITS/MAINTENANCE CHECKS



# Page

29

30

Cover

1

2

3

4

5

6



# 7

8

9

10

11

12

13

14 

# Date

Mar 16/2011

Mar 16/2011

Mar 16/2011

Mar 16/2011

Mar 16/2011

Mar 16/2011

Mar 16/2011

Jul 08/2013

Jul11/2014

Jul11/2014

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

# BOMBARDIER 

# CHALLENGER 604

CL-604 TIME LIMITS/MAINTENANCE CHECKS



# PART2

SECTION 5-10-40

CERTIFICATION MAINTENANCE REQUIREMENTS

Tasks by Chapter 5 Task Number

EFFECTIVITY: ALL 

# PART2



# 5-10-40 Cove r

Mar 16/2011CJlm"'T1"'T1m(")-l<=i:-<;:)>rrI"'U........::t>OJJ_h-i01\)Ill...........0>""'0!\)Illo<O_.co............SourceDocumentRef.No.RBR604-119Rev.82Add.27.1.1.1'7.1.1.2,7.1.1.6,7.1.1.7Chapter5TaskNo.TaskTitleTaskInterval21-31-00-101••FunctionalTestoftheOutflowValves.1600H(twostars)AllowableExtension40H00111J:o)imI""'Illr-'-'0-1,.,[!!(/)01m1111m(")-I<rrI"'U....t..)>OJJ_h--1Ql\.)s:Ql...,__..())""0--OJ1\)<0Sm--"1\)SourceDocumentRef.No.RBR604-160Rev.NC7.1.1Chapter5TaskNo.TaskTitleTaskInterval22-22-00-101**OperationalTestoftheYawDamperLinear4800H(twostars)Actuators(SVL-4000Relays).AllowableIExtensionJ40HII(");J:o)imI""Illr-)>"0-t,.,'[11111:ti(")m"'T1"'T1m()-i<)>rr01I"'U-!..)>o:nI-I01\)s:::Ill.........cn-u!\)Illo<e_.,(l)....(.VSourceDocumentRBR604-129Rev.CRBR604-129Rev.ERef.No.Chapter5TaskNo.24-21-00-101•7.1.1(onestar)24-23-00-101.7.1.2(onestar)TaskTitleTaskIntervalFunctionalTestoftheGeneratorControlUnit1600H(GCU)OvervoltageProtectionCircuits.OperationalTestoftheAirDrivenGenerator1600H(ADG).or24MNOTE:Whicheverintervaloccursfirst.SeeNOTEAllowableExtension40H40H00111;J:o)imt"'ll!r-)>tl-ti!:lz"""UJ01m.,.,m()-i<)>rr1-o.......)>O:DQl\)Ill.........."tto<O_.CD......SourceDocumentRBR604-105Rev.ARBR604-105Rev.ARBR604-105Rev.ARBR604-108Rev.NC1RBR604-108Rev.NC1RBR604-102Rev.A2RBR604-102Rev.ARBR604-102Rev.ARBR604-102Rev.ARBR604-102Rev.ARef.No.Chapter5TaskNo.27-13-04-101.7.1.1.3(onestar)27-14-01-101••7.1.1.11(twostars)27-15-07-101••7.1.1.10(twostars)27-21-00-101••7.1.1.5(twostars)27-23-00-101••7.1.1.2(twostars)27-31-13-102••7.1.1.10(twostars)27-32-00-101.7.1.1.5(onestar)27-33-01-101•7.1.1.10(onestar)27-34-04-101.7.1.1.8(onestar)27-34-04-102••7.1.1.7(twostars)TaskTitleTaskIntervalOperationalTestoftheRollDisconnectSystem.800HFunctionalTestoftheAileronPowerControl800HUnits(PCUs).DetailedInspectionoftheAileronFlutter800HDamper.FunctionalTestoftheRudderBacklash.800HOperationalTestofthePCULoadLimiters.3200HFunctionalTestofthePitchFeelSimulator.1600HOperationalTestoftheElevatorDisconnect800HSystem.FunctionalTestoftheElevatorBacklash.800HFunctionalTestoftheElevatorFlutterDampers.4800HDetailedInspectionoftheElevatorFlutter800HDampers.AllowableExtension40H40H40H40H40HN/A40H40H40H40H0r-0111J.g;c0)ilmt"Illt").-1'"'111111:ti01m"'T1"'T1m<)>rrI""U-t..)>OJJQl'\)c....r::000""0i\)PJo<O_.(!)WOlIISourceDocumentRBR604-112Rev.C-2RBR604-112Rev.C-2RBR604-112Rev.C-2RSIC-1830Rev.NCRBR604-300Rev.ERef.No.Chapter5TaskNo.27-35-01-103.7.1.4(onestar)27-35-01-104.7.1.3,7.1.6(onestar)27-35-01-105••7.1.8(twostars)27-35-04-101•(onestar)N/A3.10.1TaskTitleFunctionalTestoftheStallProtectionSystem(SPS)FlapInput(Aircraft5301to5560PreSB604-27-005)FunctionalTestofthePhaseAdvanceandSideslipCompensation(Aircraft5301to5560PreSB604-27-005)FunctionalTestfortheFlapandSideslipCompensationMonitoroftheStallProtectionSystem(Aircraft5561andSubsand5301to5560PostSB604-27-005)FunctionalTestoftheAngleofAttack(AOA)TransducerLinearityPartNumbers600-59154-1and600-59154-3NOTE:The300hourCOMPONENTcheckintervalstartsatthemostrecentofthefollowing:-theinstallationdate-theincorporationdateofSBA604-27-011PARTA-thelasttimeSBA604-27-011PARTCwasdonePartNumber600-59154-5TaskInterval100H400H4800H300HCOMPONENT100HCOMPONENTAllowableExtension10H40H40HN/AN/A0r-0IllJ,g;J:o)ilmI"""Illr-).if.'\0-4,.,'111111:ti0"Ill01mi1i1m()-i<)>rrI"'U-&.)>OJJ.h-i01\)c....c.....-'"'Ui\)S:Uo<O_,<D.j:>.O'JISourceDocumentRBR604-112Rev.C-1RBR604-300Rev.ERBR604-103Rev.C-3Add2RBS-604-100Rev.E-25Add.21Ref.No.Chapter5TaskNo.27-35-04-102*7.1.10(onestar)27-35-10-101**3.11.1(twostars)27-41-00-101**7.1.1(twostars)27-42-01-109*2.1(onestar)TaskTitleRestorationoftheAngleofAttack(AOA)Transducer,PartNo.600-59154-5FunctionalTestfortheStallProtectionSystem(SPS)StickPusherCapstanShaft,PartNo.600-59156-7(VendorPartNo.501-1258-01)PHASE-INThistaskmustbeaccomplishedatorbeforethenext1600hourinspection.OperationalTest(BITE)oftheHorizontal-StabilizerTrim-ControlSystem(HSTCS)PHASE-IN:Foraircraftwithmorethan400hourssincetask27-41-00-201wasdone,thistaskmustbeaccomplishedatorbeforethenext400hourinspectionbutnolaterthanMay01,2013,whicheveroccursfirst.Restoration(Overhaul)oftheHorizontalStabilizerTrimActuator,PartNo.604-92305-7andSubs(VendorPartNo.8454-3andSubs)PHASE-IN:AsfollowsorasmandatedperAD:a)500HfromJanuary31/2014withacalendarcapofNovember2015fortheunitsexceedingeither9600Hor8420L,whichevercomesfirst,orb)NoPHASE-INforallotherHSTAs.TaskInterval7200HCOMPONENT1600H400H9600HCOMPONENTor8420LCOMPONENTwhicheveroccursfirstAllowableExtensionN/A40H40HN/AI0OQJ;J:o)i,...OJ,...)>-t\11...['1111:ti001m"T1"T1m('))>rr1""'0...a..)>OJJ.h--tQF\)c....!:..i\3!,l).j:>.-..JSourceDocumentRef.No.Chapter5TaskNo.TaskTitleNOTE:RemoveHSTAfromaircraftandsendtovendorforthefollowing:1.Vendortoperformrestorationandreplacethepartsthatfollow:PrimaryHousingP/N8396-140(includedinP/N8396-100)andSubs,SecondaryHousingP/N261881804(includedinP/N8396-2030)andSubs,SecondarySpurGear(CH2)P/N261405307andSubs,PrimaryPinion(CH1)P/N8396-043andSubs,andSecondaryPinion(CH2)P/N8396-044andSubs2.Vendortoperformthefollowingtasks:FunctionalCheckoftheTorqueLimiters,DetailedInspectionoftheSecondaryLoadPathIndicator,andSpecialDetailedInspectionofthePrimarySpurGear.NOTE:Whenthistaskisperformed,creditcanbetakenfortask27-42-01-111*andMRS27-40-00-202andtheirtimeresettozero.Repeatintervalfortask27-42-01-111*is5000H.TaskIntervalAllowableExtension06.;J:o)imJ""'IIJ,....3:,...)>-1,.,"""(/)01m"'Tl"'Tlm()-I<)>rr1""'0--'")>OJJ1,--101\)c....c::j\)lllSourceDocumentIRBR604-103Rev.C-4Add.3RBR604-111Rev.NC1Ref.No.Chapter5TaskNo.27-42-01-111•7.1.14(onestar)27-51-04-101•7.1.1.1(onestar)TaskTitleDetailedInspectionoftheHorizontalStabilizerTrimActuator(HSTA)SecondaryLoadPathIndicator,PartNo.604-92305-7andSubs(VendorPartNo.8454-3andSubs).NOTE:Whentask27-42-01-109*,VSB8454-27-008,orMRS27-40-00-202areperformed,creditcanbetakenfortask27-42-01-111*anditstimeresettozero.Repeatintervalfortask27-42-01-111*is5000H.FunctionalTestoftheFlapControlUnit(AllDrivers-OnCircuit).TaskIntervalAllowableExtension5000HN/ACOMPONENT4800H40HII0OQJ;J:omt"'OJr-).ir.\0-t£11111:tJ0

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

RBR604 - 300 27-53-00-1 01 ••

Rev.F4 (two sta r s) 

## 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 rep l aced actuators where the total

component flight cycles are unknown.

The 2000 landing interval to be

calculated from the date of TR 5-2-45

(May 12/2010). PHASE-IN: For actuators that have

exceeded 9600 landings

, replace the

actuator within 300 hou r s of the date on

TR

5-2-45 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 Bear i ng

, P/N NT A 1828

Thrust Washer, P/N TRA 1828 Task Interval Allowable Extension



## 9600 L 50 L COMPONENT 2000 L 50 L COMPONENT I 0 

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

RAP604-172 28-15-43-101 ••

Rev.

J13 (two stars)

RBR604-131 28-24-00-1 01 •

Rev . A 7 .1.1.1 1 (one star)

RBR604-142 28-31-00-101 •

Rev.B

7.1.13 (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



## 50 

## H 40 

## H 40H I I

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

RBR604-133 30-11-00-101 ••

Rev.

A Add. 1 

## 7 .1. 1.2 (two stars) 

## Task Title



## Detailed Inspection of the Wing Anti-Ice Duct

Piccolo- Tube. PHASE-IN: 

## For aircraft that have exceeded

6400 hours on the date of Temporary Revision

5-2-41 (Feb 16/2009)

, do task 30-11-00-101 

## **

at the earliest opportunity, but no later than the

next scheduled 6400 hour inspection or next due

compliance of task 57-10-00-208, whichever

comes first. Task Interval Allowable Extension



## 6400H 40 H 0 

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

RBR604-300 32-31-01-101

Rev.D2 RBR604-300 32-31-01-102

Rev. D2 RBR604-300 32-31-01-103

Rev.D2 6

, 9 

## Task Title

Restoration of the Landing Gear Control Handle

Assembly , Part No. 601 R50967-7 (Vendor Part

No. 7-45502-1 ) with suffix A after S/N.



## NOTE : For Landing Gear Control Handle

Assemblies that have been in service for more

than

150 landings at the time of issue of

Temporary Revision 5-2-8

, restoration is

required within the next 150 landings (Refer to

Service Bulletin 604-32-017)

Restoration of the Landing Gear Control Handle

Assembly Part No. 601 R50967-7 (Vendor Part

No. 7-45502-1) with suffix B after S/N or Part

No. 601 R50967-9 (Vendor Part No.

7-45502-3) . Detailed inspection of the Landing Gear Control

Handle Assembly

, Part No. 601 R50967-7

(Vendor Part No. 7-45502-1) with suffix B after

S/N or Part No. 601 R50967-9 (Vendor Part No.

7-45502-3). 

## NOTE: For Landing Gear Control Handle

Assemblies that have been in service for more

than

450 landings at the time of issue of

Temporary Revision 5-2-8, detailed inspection

is required within the next 150 landings. 

## Task Interval 300 L 3600 L 600 L Allowable Extension 

## N/A 60 L

60 L 0 r-



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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 PHASE-IN: 

## For aircraft that have exceeded

6400 hours on the date of Temporary Revision

5-2-42 (Feb 16/2009)

, do task 36-21-00-101*

at the earliest opportunity

, but no later than the

next scheduled 6400 hour inspection or next

due compliance of task 57-1 0-00-208,

whichever comes first. Task Interval Allowable Extension



## 6400H 40 H 0 r- 

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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. 2100140-005/-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. Refer to section 5-1 0-05

,

paragraph

5

. 0

. PHASE-IN: 

## For aircraft with less than

4000 H, 

## carry out this test within 1600 H

from Temporary Revision 5-2-31 dated

Mar 22/2007. For aircraft with 4000 H or

more , carry out this test within 1000 H

from Temporary Revision 5-2-31 dated

Mar 22/2007

.

Part No. 21 00140-01 0 Task Interval Allowable Extension



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