# Canadair Temporary Revision 600-1/24-2

Copy: No revision named ("TR_600-1_24-2"), 92 pages: PDF https://openairdocs.org/files/sha256/79/bb/79bbba4fd043c368e23950f46f394495da22997b4da41f2a54d558b2ee366699; text https://openairdocs.org/service-documents/bombardier/tr-600-1-24-2/file/79bbba4fd043.md. Rights: © Bombardier Inc. Filed by the FAA in regulations.gov docket FAA-2015-7529; AD 2017-13-09 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.

## Details

- Manufacturer: [Bombardier](https://openairdocs.org/service-documents/bombardier.md) (issued as Canadair)
- Type: Other document (Temporary Revision)
- Number: 600-1/24-2
- Page: https://openairdocs.org/service-documents/bombardier/tr-600-1-24-2

## ADs that cite it (1) (OpenAirDocs)

Newest first, with the revision each names, as OpenAirDocs read it from the AD's text.

- [AD 2017-13-09](https://openairdocs.org/ad/2017-13-09.md), effective Aug 3, 2017: No revision named

Also cited in [1 proposed AD](https://openairdocs.org/service-documents/bombardier/tr-600-1-24-2/proposed.md).

## Text (92 pages)

Rights: © Bombardier Inc. Filed by the FAA in regulations.gov docket FAA-2015-7529; AD 2017-13-09 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. Each page's text from the PDF; open the PDF at a page with #page=N.

### Page 1

DOT Approved
Jan 18/16
600−1 US Page 1
TEMPORARY REVISION NO. 600−1/24−2
LETTER OF TRANSMITTAL
Reason For Issue
To advise the flight crew of restricted operation from runways contaminated by
wet or dry ice and to prohibit the use of thrust reversers, on airplanes not
incorporating Part C of Alert Service Bulletin A600−0769.
Instructions for Insertion of This Temporary Revision
1. Insert the Log of Temporary Revisions in the front pages of the Airplane
Flight Manual.
2. Remove and destroy the pages and the letter of transmittal of Temporary
Revision No. 600−1/24−1.
3. Insert this Temporary Revision in the Airplane Flight Manual as instructed at
the top of each page.
4. The pages affected by this Temporary Revision are:
INTRODUCTION, page 4
LIMITATIONS, pages 6, 6(LBA), 8B, 8D, 27, 32
EMERGENCY PROCEDURES, pages 4A, 6C, 14, 15, 16A, 16B, 16C, 17, 31, 34, 35
NORMAL PROCEDURES, pages 6, 7. 8, 9, 10, 16A, 46, 47, 56, 57, 58, 59
ABNORMAL PROCEDURES, pages 4, 5, 16, 28, 30, 31, 32, 32B, 34F, 40, 40B, 41, 
42, 43, 44, 45, 49, 52
PERFORMANCE, pages 46, 128, 130, 132
5. Record the insertion of the Temporary Revision on the Log of Temporary
Revisions.
6. Retain this page for record purposes.
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 2

(No text on this page.)

### Page 3

DOT Approved
Apr 29/11
600−1 US Log of Temporary RevisionsPage 5
LOG OF TEMPORARY REVISIONS
TR/No. Subject DOT Approval Status Date
600−1/17 To advise the flight
crew of a revision to
ensure sufficient heat
is available for wing
anti-icing.
W. Jupp
16 Aug 2006
Incorporated by
Rev. 93
600−1/18 To advise the flight
crew of a revision to
the stall protection
system test.
W. Jupp
30 Jan 2007
Incorporated by
Rev. 92
600−1/19 Not used
600−1/20 To advise the flight
crew of additional
operating limitations
related to operation
safety enhancement.
W. Jupp
07 Mar 2008
Superseded by
TR 600-1/20-1
600−1/20−1 To advise the flight
crew of additional
operating limitations
related to operation
safety enhancement.
W. Jupp
20 Mar 2008
Superseded by
TR 600-1/20-2
600−1/20−2 To advise the flight
crew of additional
operating limitations
related to operation
safety enhancement.
R.W. Walker
07 Aug 2008
Incorporated by
Rev. 92
600−1/21 To advise the flight
crew of the
introduction of a Stall
Recovery procedure.
W. Istchenko
26 May 2010
Incorporated by
Rev. 94
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 4

DOT Approved
Jan 18/16
600−1 USLog of Temporary RevisionsPage 6
LOG OF TEMPORARY REVISIONS
TR/No. Subject DOT Approval Status Date
600−1/22 To advise the flight
crew of the addition of
information regarding
nose wheel steering
failure.
W. Istchenko
07 Jan 2011
Incorporated by
Rev. 95
600−1/23 To advise the flight
crew of limitations and
performance penalties
for operation with a
cracked windshield
faceply.
W. Istchenko
01 Sep 2011
Incorporated by
Rev. 96
600−1/24 To advise the flight
crew of restricted
operation from
contaminated runways
and to prohibit the use
of thrust reversers.
W. Istchenko
20 Jun 2014
Superseded by
TR 600-1/24-1
600−1/24−1 To advise the flight
crew of restricted
operation from runways
contaminated by wet or
dry ice, and to
prohibit the use of
thrust reversers.
W. Istchenko
27 Apr 2015
Superseded by
TR 600-1/24-2
600−1/24−2 To advise the flight
crew of restricted
operation from runways
contaminated by wet or
dry ice and to prohibit
the use of thrust
reversers, on airplanes
not incorporating
Part C of Alert Service
Bulletin A600−0769.
W. Istchenko
18 Jan 2016
Active
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 5

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 1 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in INTRODUCTION
Facing Page 4
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: Add the following:
Service Bulletin No. Title
A600-0769 Special Check/Modification − Exhaust −
Thrust Reverser Actuator Attachments
Installation/Replacement to Prevent
Inadvertent Thrust Reverser Deployment
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 6

(No text on this page.)

### Page 7

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 2 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in LIMITATIONS
Facing Page 6
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: Add the following to paragraph 4.C.:
On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, take-off and landing on runways contaminated by wet or dry ice
is prohibited. Operations on all other runways as defined in UNAPPROVED
SUPPLEMENT 3 − OPERATION ON CONTAMINATED RUNWAYS is permitted.
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 8

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### Page 9

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 3 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in LIMITATIONS
Facing Page 6(LBA)
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: Add the following to paragraph 4.C.:
On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, take-off and landing on runways contaminated by wet or dry ice
is prohibited. Operations on all other runways as defined in UNAPPROVED
SUPPLEMENT 3 − OPERATION ON CONTAMINATED RUNWAYS is permitted.
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 10

(No text on this page.)

### Page 11

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 4 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in LIMITATIONS
Facing Page 8B
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, delete the following NOTE from paragraph 4.I.:
N O T E
2. To prevent wing contamination from reverse
jet blast, operating the thrust reversers
during taxi operations on wet and
contaminated surfaces should be avoided.
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 12

(No text on this page.)

### Page 13

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 5 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in LIMITATIONS
Facing Page 8D
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: Add the following to paragraph 4.K.:
On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, take-off and landing on runways contaminated by wet or dry ice
is prohibited. Operations on all other runways as defined in UNAPPROVED
SUPPLEMENT 3 − OPERATION ON CONTAMINATED RUNWAYS is permitted.
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 14

(No text on this page.)

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### Page 16

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 6 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in LIMITATIONS
Facing Page 27
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: Add the following to paragraph 9.D.(3):
On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, the actual landing distance must be determined by
reference to the landing distance chart without credit for ground
spoilers (refer to PERFORMANCE − LANDING).
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 17

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 7 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in LIMITATIONS
Facing Page 32
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: Replace paragraph 9.K. with the following:
K. THRUST REVERSERS
Take-off with a REVERSER UNLOCKED or a thrust reverser UNSAFE TO ARM
light on is prohibited.
On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, use of thrust reversers is prohibited.
On airplanes incorporating Part C of Alert Service Bulletin A600−0769:
/C0083 The thrust reversers are approved for ground use only.
/C0083 The thrust reverser pre-flight checks (NORMAL PROCEDURES) must be
successfully accomplished prior to each take-off.
/C0083 Thrust reversers are intended for use during full stop landings.  Do
not attempt a go-around manoeuvre after deployment of the thrust
reversers on the ground.
/C0083 Application of reverse thrust above 56% N1 is not permitted atairspeeds below 60 KIAS.
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 18

(No text on this page.)

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### Page 20

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 8 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in EMERGENCY PROCEDURES
Facing Page 4A
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, delete the following CAUTION from paragraph 2.D.:
C A U T I O N
With thrust reversers deployed, a nose-up
pitching tendency will occur at high power
settings, particularly at aft centre of
gravity light weights. This tendency is
controllable with elevator and may be
minimized by ensuring that nose wheel
touchdown is achieved and nose down elevator
applied, before selecting reverse thrust.
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 21

(No text on this page.)

### Page 22

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 9 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in EMERGENCY PROCEDURES
Facing Page 6C
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, delete the following CAUTION from paragraph 3.A.:
C A U T I O N
With thrust reversers deployed, a nose-up
pitching tendency will occur at high power
settings, particularly at aft centre of
gravity light weights. This tendency is
controllable with elevator and may be
minimized by ensuring that nose wheel
touchdown is achieved and nose down elevator
applied, before selecting reverse thrust.
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 23

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 10 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in EMERGENCY PROCEDURES
Facing Page 14
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, delete the following CAUTION from paragraph 8.A.:
C A U T I O N
With thrust reversers deployed, a nose-up
pitching tendency will occur at high power
settings, particularly at aft centre of
gravity light weights. This tendency is
controllable with elevator and may be
minimized by ensuring that nose wheel
touchdown is achieved and nose down elevator
applied, before selecting reverse thrust.
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 24

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 11 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in EMERGENCY PROCEDURES
Facing Page 15
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, delete the following NOTE from paragraph 8.A.:
N O T E
3. If use of thrust reversers is required and
ADG is only source of power, ADG manual
deploy handle must be pulled.
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 25

(No text on this page.)

### Page 26

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 12 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in EMERGENCY PROCEDURES
Facing Page 16A
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, delete the following CAUTION from paragraph 9.B.:
C A U T I O N
With thrust reversers deployed, a nose-up
pitching tendency will occur at high power
settings, particularly at aft centre of
gravity light weights. This tendency is
controllable with elevator and may be
minimized by ensuring that nose wheel
touchdown is achieved and nose down elevator
applied, before selecting reverse thrust.
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 27

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 13 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in EMERGENCY PROCEDURES
Facing Page 16B
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, delete the following CAUTION from paragraph 9.C.:
C A U T I O N
With thrust reversers deployed, a nose-up
pitching tendency will occur at high power
settings, particularly at aft centre of
gravity light weights. This tendency is
controllable with elevator and may be
minimized by ensuring that nose wheel
touchdown is achieved and nose down elevator
applied, before selecting reverse thrust.
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 28

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 14 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in EMERGENCY PROCEDURES
Facing Page 16C
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, delete the following CAUTION from paragraph 9.D.:
C A U T I O N
With thrust reversers deployed, a nose-up
pitching tendency will occur at high power
settings, particularly at aft centre of
gravity light weights. This tendency is
controllable with elevator and may be
minimized by ensuring that nose wheel
touchdown is achieved and nose down elevator
applied, before selecting reverse thrust.
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 29

(No text on this page.)

### Page 30

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 15 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in EMERGENCY PROCEDURES
Facing Page 17
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, delete the following CAUTION from paragraph 10.A.:
C A U T I O N
With thrust reversers deployed, a nose-up pitching
tendency will occur at high power settings,
particularly at aft centre of gravity light weights.
This tendency is controllable with elevator and may
be minimized by ensuring that nose wheel touchdown
is achieved and nose down elevator applied, before
selecting reverse thrust.
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 31

(No text on this page.)

### Page 32

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 16 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in EMERGENCY PROCEDURES
Facing Page 31
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, replace the CAUTION in paragraph 13.G. with the following:
C A U T I O N
When landing with anti-skid system OFF, extreme
caution is required during braking to avoid tire
damage.
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 33

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 17 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in EMERGENCY PROCEDURES
Facing Page 34
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, delete the following CAUTION from paragraph 14.B.:
C A U T I O N
With thrust reversers deployed, a nose-up
pitching tendency will occur at high power
settings, particularly at aft centre of
gravity light weights. This tendency is
controllable with elevator and may be
minimized by ensuring that nose wheel
touchdown is achieved and nose down elevator
applied, before selecting reverse thrust.
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 34

(No text on this page.)

### Page 35

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 19 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in EMERGENCY PROCEDURES
Facing Page 35 (Cont’d)
A. ENGINE FAILURE OR REJECTED TAKE-OFF BEFORE ACHIEVING V 1 (Cont’d)
(6) Aileron and rudder Use as required to maintain. . . . . . . . . . . . 
directional control.
(7) Nose wheel steering
(below 60 KIAS) Use as required to maintain. . . . . . . . . . . . . . . 
directional control (on
airplanes 1004, 1009, 1052 and
subsequent and on airplanes
incorporating Canadair Service
Bulletin 600-0096, Modification
− Nose Landing Gear − Steering).
If required:
(8) Emergency Evacuation
Procedure Accomplish Refer to EMERGENCY EVACUATION.. . . . . . . . . . . . . . 
After rejected take-off, procedures associated with cooling of wheels,
brakes and tires must be observed (refer to SYSTEMS OPERATION − LANDING
GEAR WHEELS AND BRAKES).
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 36

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 18 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in EMERGENCY PROCEDURES
Facing Page 35
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, replace paragraph 15.A. with the following:
A. ENGINE FAILURE OR REJECTED TAKE-OFF BEFORE ACHIEVING V 1
Rejection of the take-off must be initiated no later than V1.
(1) Thrust levers Move rapidly to LOW IDLE.. . . . . . . . . . . . . . . . 
C A U T I O N
Light braking is not recommended during rough
runway operation.
(2) Wheel brakes Apply. . . . . . . . . . . . . . . . 
N O T E
During rough runway operation, the anti-skid system may
provide degraded brake effectiveness when light braking
(less than 25% full pedal deflection) is applied.
If at any time after the airplane weight is firmly on
the wheels, the normal or expected deceleration rate is
not achieved, immediately release the brakes and firmly
re-apply heavy anti-skid braking until a safe stop is
assured.  (Full release of the brake pedals resets the
anti-skid system and permits full and optimum braking
performance on re-application.  It is not necessary to
switch off the anti-skid system).
(3) Flight spoilers Extend. . . . . . . . . . . . 
If fitted:
(4) Ground spoilers Extend. . . . . . . . . . . . 
(5) Maximum braking Maintain until a safe stop on runway is. . . . . . . . . . 
assured.
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 37

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 20 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in NORMAL PROCEDURES
Facing Page 6
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, delete paragraph 2.G.
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 38

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 21 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in NORMAL PROCEDURES
Facing Page 7
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, replace paragraph 2.I. with the following:
I. BEFORE TAKE-OFF
On airplanes 1072, 1086 and subsequent and on airplanes incorporating
Canadair Service Bulletin 600-0350, Modification − Engine Speed
Indicating  − N1 Fan Speed Indicator:
(1) T.O./NORM N 1 fan speed indicator
trim switch...................T.O. Observe 0.0% to 2.0% (maximum)
increase in indicated N1 rpm.
(2) Minimum N 1 for take-off....Establish for prevailing OAT/Altitude
(refer to PERFORMANCE − THRUST
SETTINGS).
(3) Continuous ignition As required Refer to LIMITATIONS −. . . 
OPERATING LIMITATIONS.
If engine synchronization system is fitted:
(4) ENGINE SYNC switch OFF. . . . . . . . . . . . 
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 39

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 22 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in NORMAL PROCEDURES
Facing Page 8
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, replace paragraph 2.J. with the following:
J. AFTER TAKE-OFF
On airplanes 1072, 1086 and subsequent and on airplanes incorporating
Canadair Service Bulletin 600-0350, Modification − Engine Speed
Indicating  − N1 Fan Speed Indicator:
(1) T.O./NORM N 1 fan speed indicator
trim switch...................NORM
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 40

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 23 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in NORMAL PROCEDURES
Facing Page 9
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, replace paragraphs 2.L. and 2.M. with the following:
L. BEFORE LANDING
(1) Continuous ignition As required Refer to LIMITATIONS −. . . 
OPERATING LIMITATIONS.
If engine synchronization system is fitted and engaged:
(2) ENGINE SYNC switch SET for approximately 5 seconds then. . . . . . . . . . . . 
OFF.
M. AFTER LANDING
After touchdown when nose wheel is on the ground and spoilers deployed:
(1) Thrust levers LOW IDLE if required.. . . . . . . . . . . . 
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 41

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 24 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in NORMAL PROCEDURES
Facing Page 10
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, replace paragraph 2.N. with the following:
N. ENGINE SHUTDOWN
C A U T I O N
If ITT rises above 250/C0095C following engine
shutdown, carry out an engine dry motoring
cycle immediately to reduce ITT.
Prior to shutdown, operate the engine at HIGH IDLE or below for a minimum
of two minutes.
(1) BLEED AIR, ACU L and R
switch/lights Press out OFF light on (see NOTE).. . . . . . . . . . . 
(2) BLEED AIR, L ENG and
R ENG switch/lights Press out BLEED CLOSED lights on.. . . . . 
(3) AC POWER, GEN 1 and GEN 2
control switches OFF GEN OFF lights on.. . . . . . . . . . . . . . 
(4) FUEL CONTROL, L TANK
and R TANK, PUMP
switch/lights Press out ON lights out.. . . . . . . . . . . 
(5) Thrust levers SHUT OFF. . . . . . . . . . . . 
N O T E
The ACUs should not be selected off if the
APU is providing air conditioning.
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 42

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### Page 44

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 25 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in NORMAL PROCEDURES
Facing Page 16A
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, delete the following NOTE from paragraph 4.A.:
N O T E
3. To prevent wing contamination from reverse
jet blast, operating the thrust reversers
during taxi operations on wet and
contaminated surfaces should be avoided.
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 45

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 26 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in NORMAL PROCEDURES
Facing Page 46
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, delete paragraph 18.A.
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 46

(No text on this page.)

### Page 47

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 28 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in NORMAL PROCEDURES
Facing Page 47 (Cont’d)
20. LANDING PROCEDURE (Cont’d)
(6) Wheel brakes Apply as soon as possible.. . . . . . . . . . . . . . . . 
C A U T I O N
Light braking is not recommended during rough
runway operation.
(7) Maximum braking Maintain until safe stop on runway is. . . . . . . . . . 
assured.
(8) Rudder and aileron Use as required to maintain. . . . . . . . . . . . 
directional control.
(9) Nose wheel steering Use as required to maintain. . . . . . . . . . . 
directional control (if
Canadair Service Bulletin
600-0380, Modification − Nose
Gear − Steer by Wire is not
incorporated, do not use nose
wheel steering above 60 KIAS).
N O T E
1. Indicated airspeed is the primary approach
reference, however the pilot may use the ADI
FAST/SLOW indicator as a secondary reference
for approach with flaps at 45 degrees.
2. During rough runway operation, the anti-skid
system may provide degraded brake
effectiveness when light braking (less than
25% full pedal deflection) is applied.
3. If at any time after the airplane weight is
firmly on the wheels, the normal or expected
deceleration rate is not achieved,
immediately release the brakes and firmly
re-apply heavy anti-skid braking until a safe
stop is assured.  (Full release of the brake
pedals resets the anti-skid system and
permits full and optimum braking performance
on re-application.  It is not necessary to
switch off the anti-skid system).
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 48

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 27 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in NORMAL PROCEDURES
Facing Page 47
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, replace paragraph 20. with the following:
20. LANDING PROCEDURE
Approach through 50 feet height point at speed of 1.3 Vs (refer to
PERFORMANCE − LANDING) on stabilized glideslope of 3 degrees with gear down
and flaps at 45 degrees.
A. PROCEDURE
(1) Continuous ignition Set as required (refer to. . . . . . . . . . . 
LIMITATIONS − OPERATING
LIMITATIONS).
If wing anti-ice is off:
(2) Thrust levers Reduce to LOW IDLE at 50 feet.. . . . . . . . . . . . . . 
If engines and wing anti-ice are selected on:
(2) Thrust levers................Reduce to HIGH IDLE (Soft Detent) at
50 feet.  Maintain this setting
until touchdown, then reduce to
LOW IDLE.
(3) Airplane attitude Maintain until close to runway.  Perform. . . . . . . . 
partial flare and touchdown
without holding off.
N O T E
If icing accumulation on the wheels and
brakes is suspected, carry out a positive
landing to ensure initial wheel spin up and
breakout of frozen brakes.
(4) Flight Spoilers Extend immediately after main wheel. . . . . . . . . . . . 
touchdown.
On airplane 1004 to 1085 without Canadair Service Bulletin 600-0452
Modification − Ground Spoilers − Auto Deployment:
(5) Ground Spoilers Extend immediately after main wheel. . . . . . . . . . . . 
touchdown.
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 49

TR 600−1/24−2
Page 29 of 57
DOT Approved
Jan 18/16
600−1 US
TEMPORARY REVISION NO. 600−1/24−2
Insert in NORMAL PROCEDURES
Facing Page 56
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, delete steps 23.E.(30) and 23.F.(8).
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 50

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 30 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in NORMAL PROCEDURES
Facing Page 57
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, delete step 23.G.(2).
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 51

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 31 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in NORMAL PROCEDURES
Facing Page 58
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, delete step 23.I.(17).
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 52

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 32 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in NORMAL PROCEDURES
Facing Page 59
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, delete step 23.K.(1) and (2).
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 53

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 33 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in ABNORMAL PROCEDURES
Facing Page 4
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, delete the following CAUTION from paragraph 3.B.:
C A U T I O N
With thrust reversers deployed, a nose-up
pitching tendency will occur at high power
settings, particularly at aft centre of
gravity light weights. This tendency is
controllable with elevator and may be
minimized by ensuring that nose wheel
touchdown is achieved and nose down elevator
applied, before selecting reverse thrust.
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 54

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### Page 55

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 35 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in ABNORMAL PROCEDURES
Facing Page 5 (Cont’d)
C. SINGLE ENGINE APPROACH AND LANDING (Cont’d)
(6) Maximum braking Maintain until safe stop on runway is. . . . . . . . . . 
assured.
(7) Rudder and aileron Use as required to maintain. . . . . . . . . . . . 
directional control.
(8) Nose wheel steering
(below 60 KIAS) ....Use as required to maintain. . . . . . . . . . . 
directional control (on airplanes
1004, 1009, 1052 and subsequent
and on airplanes incorporating
Canadair Service Bulletin
600−0096, Modification − Nose
Landing Gear − Steering).
For single engine autopilot approach, use flaps at 20 degrees but add
18 KIAS to speed determined above (13 KIAS on airplanes incorporating
Canadair Service Bulletin 600−0462, Modification − Autopilot System −
Improvement).  Minimize power changes and uncoordinated flight.
N O T E
1. Single engine go-around capability is not
assured with flaps angles greater than 20
degrees.
2. On airplanes 1086 and subsequent and
airplanes incorporating Canadair Service
Bulletin 600−0452, Modification − Ground
Spoilers − Auto Deployment, the actual
landing distance must be determined by
reference to the landing distance chart
without credit for ground spoilers (refer to
PERFORMANCE − LANDING).
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 56

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 34 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in ABNORMAL PROCEDURES
Facing Page 5
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, replace paragraph 3.C. with the following:
C. SINGLE ENGINE APPROACH AND LANDING
Approach until landing is assured with flaps at 20 degrees.
(1) Airspeed Maintain at a minimum of 12 KIAS above. . . . . . . . . . . . . . . . . 
VREF  for flaps at 45 degrees
(refer to PERFORMANCE −
LANDING).
(2) Continuous ignition Set as required (refer to. . . . . . . . . . . 
LIMITATIONS − OPERATING
LIMITATIONS).
(3) Flight spoilers Extend immediately after main wheel. . . . . . . . . . . . 
touchdown.
(4) Ground spoilers Extend immediately after main wheel. . . . . . . . . . . . 
touchdown.  On airplanes 1086
and subsequent and airplanes
incorporating Canadair Service
Bulletin 600−0452, Modification
− Ground Spoilers − Auto
Deployment, ground spoilers
deploy automatically after main
wheel touchdown.
(5) Wheel brakes Apply as soon as possible.. . . . . . . . . . . . . . . . 
N O T E
On rough runway surfaces, if degradation of
braking performance is experienced, the
anti-skid system may be reset and braking
performance recovered by momentarily
releasing and firmly reapplying wheel brakes.
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 57

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 36 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in ABNORMAL PROCEDURES
Facing Page 16
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, delete the following CAUTION from paragraph 7.E.:
C A U T I O N
With thrust reversers deployed, a nose-up
pitching tendency will occur at high power
settings, particularly at aft centre of
gravity light weights. This tendency is
controllable with elevator and may be
minimized by ensuring that nose wheel
touchdown is achieved and nose down elevator
applied, before selecting reverse thrust.
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

### Page 58

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### Page 59

DOT Approved
Jan 18/16
600−1 US TR 600−1/24−2Page 37 of 57
TEMPORARY REVISION NO. 600−1/24−2
Insert in ABNORMAL PROCEDURES
Facing Page 28
REASON FOR ISSUE: To advise the flight crew of restricted operation from
runways contaminated by wet or dry ice and to prohibit the
use of thrust reversers, on airplanes not incorporating
Part C of Alert Service Bulletin A600−0769.
ACTION: On airplanes not incorporating Part C of Alert Service Bulletin
A600−0769, replace the CAUTION in step (3) of paragraph 13.C. with the
following:
C A U T I O N
Improper landing technique during a flaps failure
can generate nose gear loads sufficient to cause
structural damage.
To prevent damage:
/C0083 After main gear touchdown, gently lower the
nose to the runway.
/C0083 Apply brakes only after nose wheel touchdown.
MODEL CL−600−1A11
AIRPLANE FLIGHT MANUAL
(WINGLETS)

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