DOT Approved

Jun 20/14

41,100 US Page 1

TEMPORARY REVISION NO. 600/29

LETTER OF TRANSMITTAL

Reason For Issue

To advise the flight crew of restricted operation from contaminated runways and

to prohibit the use of thrust reversers.

Instructions for Insertion of This Temporary Revision

1. Insert the Log of Temporary Revisions in the front pages of the Airplane

Flight Manual.

2. Insert this Temporary Revision in the Airplane Flight Manual as instructed at

the top of each page.

3. The pages affected by this Temporary Revision are:

LIMITATIONS, pages 6, 8B, 8D, 27, 31

NORMAL PROCEDURES, pages 6, 7. 8, 8A, 9, 13, 46, 49, 59, 60, 72A, 87, 88A, 

89, 90, 90B, 92F, 98, 99, 100, 100A, 100B, 101, 102,

105, 108, 113, 114, 115, 116

EMERGENCY PROCEDURES, pages 4A, 6C, 14, 15, 16A, 16B, 16C, 17, 31, 34, 35

PERFORMANCE, pages 30, 104, 106, 108

4. Record the insertion of the Temporary Revision on the Log of Temporary

Revisions.

5. Retain this page for record purposes.

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 1 of 55

TEMPORARY REVISION NO. 600/29

Insert in LIMITATIONS

Facing Page 6

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Replace paragraph 3.C. with the following:

C. RUNWAY SURFACE

Take-off and landing on runways contaminated by standing water, slush,

snow or ice is prohibited.

Operations on wet runways as defined in UNAPPROVED SUPPLEMENT 3 −

OPERATION ON CONTAMINATED RUNWAYS is permitted.

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 2 of 55

TEMPORARY REVISION NO. 600/29

Insert in LIMITATIONS

Facing Page 8B

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete the following NOTE from paragraph 3.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
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 3 of 55

TEMPORARY REVISION NO. 600/29

Insert in LIMITATIONS

Facing Page 8D

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Add the following to paragraph 3.K.:

Take-off and landing on runways contaminated by standing water, slush,

snow or ice is prohibited.

Operations on wet runways as defined in UNAPPROVED SUPPLEMENT 3 −

OPERATION ON CONTAMINATED RUNWAYS is permitted.

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 4 of 55

TEMPORARY REVISION NO. 600/29

Insert in LIMITATIONS

Facing Page 27

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Replace paragraph 8.D.(3) with the following:

(3) Ground Spoilers

The actual landing distance must be determined by reference to the

landing distance chart without credit for ground spoilers (refer to

PERFORMANCE − LANDING).

On airplanes 1004 to 1085 which do not incorporate Canadair Service

Bulletin 600-0452, Modification − Ground Spoilers − Auto Deployment:

The spoiler lever must not be selected to the GROUND SPOILER position

in flight.

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 5 of 55

TEMPORARY REVISION NO. 600/29

Insert in LIMITATIONS

Facing Page 31

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Replace paragraph 8.I. with the following:

I. THRUST REVERSERS

Use of thrust reversers is prohibited.

Take-off with a REVERSER UNLOCKED or a thrust reverser UNSAFE TO ARM

light on is prohibited.

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 6 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 6

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete paragraph 1.G.

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 7 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 7

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Replace paragraph 1.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 N1 fan speed indicator

trim switch...................T.O. Observe 0.0% to 2.0% (maximum)

increase in indicated N1 rpm.

(2) Minimum N1 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
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 8 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 8

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Replace paragraph 1.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 N1 fan speed indicator

trim switch...................NORM

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 9 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 8A

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Replace paragraphs 1.L. and 1.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
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 10 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 9

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Replace paragraph 1.N. with the following:

N. ENGINE SHUTDOWN

C A U T I O N

If ITT rises above 250C 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
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 11 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 13

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete the following NOTE from paragraph 3.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
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 12 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 46

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete paragraph 17.A.

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 14 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 49 (Cont’d)

19. LANDING PROCEDURE (Cont’d)

(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.

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
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 13 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 49

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Replace paragraph 19. with the following:

19. 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.

(6) Wheel brakes . . . . . . . . . . . . . . . . Apply as soon as possible.

C A U T I O N

Light braking is not recommended during rough

runway operation.

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 15 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 59

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete the following CAUTION from paragraph 23.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
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 16 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 60

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Replace paragraph 23.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.

C A U T I O N

Light braking is not recommended during rough

runway operation.

(5) Wheel brakes . . . . . . . . . . . . . . . . Apply as soon as possible.

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).

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 17 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 60 (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
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 18 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 72A

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete the following CAUTION from paragraph 27.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
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 19 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 87

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Replace the CAUTION in step (3) of paragraph 33.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:

 After main gear touchdown, gently lower the

nose to the runway.

 Apply brakes only after nose wheel touchdown.

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 20 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 88A

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Replace the CAUTION in step (1) of paragraph 33.G. with the following:

C A U T I O N

If a ground spoiler disconnect occurs late on

final approach, particularly in turbulence,

lateral control requirements may exceed that

which is available with the remaining aileron

control. If this occurs use full aileron and

rudder, as required, to maintain wings level and,

if necessary, initiate a go-around so as to make

an approach and landing using 20 degrees flap.

Refer to PERFORMANCE − LANDING.

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 21 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 89

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete the following CAUTION from paragraph 33.I.:

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
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 22 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 90

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete the following CAUTION from paragraph 33.J.:

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
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 23 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 90B

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete the following CAUTION from paragraph 33.K.:

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
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 24 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 92F

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete the following CAUTION from paragraph 34.I.:

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
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 25 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 98

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete the following CAUTION and NOTE from paragraph 35.G.:

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.

N O T E

Maximize use of reverse thrust.

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 26 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 99

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete the following NOTE and CAUTION from paragraph 35.I.:

N O T E

3. Maximize use of reverse thrust.

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
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 27 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 100

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete the following NOTE and CAUTION from paragraph 35.J.:

N O T E

2. Maximize use of reverse thrust.

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
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 28 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 100A

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Replace the CAUTION in paragraph 35.K. with the following:

C A U T I O N

When landing with anti-skid system OFF, extreme

caution is required during braking in order to avoid

tire damage.

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 29 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 100B

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Replace the CAUTION in paragraphs 36.A. and 36.B. with the following:

C A U T I O N

Extreme caution is required during manual

braking to avoid tire damage.

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 30 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 101

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Replace the CAUTION in paragraph 36.C. with the following:

C A U T I O N

Extreme caution is required during manual

braking to avoid tire damage.

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 31 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 102

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Replace paragraph 36.E. with the following:

E. NOSE WHEEL STEERING FAILURE

Without Canadair Service Bulletin 600-0380, Modification − Nose Wheel −

Steer by Wire incorporated:

Indication: WOW I/P FAIL light on, or steering handwheel will not

self-centre.

(1) N/W STEER switch Cycle OFF then ARMED. . . . . . . . . . . . . 

(2) Nose wheel steering . . . . . . . . . Check responsiveness and ensure

normal operation.

N O T E

Check nose wheel steering responsiveness by

taxiing forward and checking proper aircraft

response to left/right handwheel inputs and

rudder pedal inputs.

If indication persists:

(3) N/W STEER switch OFF . . . . . . . . . . . . . . 

N O T E

1. When landing with the nosewheel steering

inoperative, select the longest runway

available with minimum turbulence and

crosswind.

2. Use differential braking, rudder and engine

thrust as required to assist directional

control.

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 32 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 102 (Cont’d)

E. NOSE WHEEL STEERING FAILURE (Cont’d)

With Canadair Service Bulletin 600-0380, Modification − Nose Wheel −

Steer by Wire incorporated:

Indication: Nose wheel steering FAIL, or WOW I/P FAIL light on, or

steering handwheel will not self-centre.

During Taxi:

(1) Nose wheel Center using differential braking as . . . . . . . . . . . . . . . . . 

required.

(2) Nose wheel steering

handwheel Ensure centered. . . . . . . . . . . . . . . . . . . 

(3) Rudder pedals . . . . . . . . . . . . . . Ensure centered.

N O T E

The N/W STEER switch must be cycled to OFF

and then back to ARMED to enable centering of

the nosewheel.

(4) N/W STEER switch Cycle OFF then ARMED. . . . . . . . . . . . . (5) Nose wheel steering . . . . . . . . . Check responsiveness and ensure

normal operation.

N O T E

Check nose wheel steering responsiveness by

taxiing forward and checking proper aircraft

response to left/right handwheel inputs and

rudder pedal inputs.

If indication persists:

(6) N/W STEER switch OFF . . . . . . . . . . . . . . 

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 33 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 102 (Cont’d)

E. NOSE WHEEL STEERING FAILURE (Cont’d)

With Canadair Service Bulletin 600-0380, Modification − Nose Wheel −

Steer by Wire incorporated:

In Flight:

N O T E

Centering of the nosewheel steering

handwheel, rudder pedals and/or cycling the

N/W STEER switch will not enable centering of

the nosewheel.

(1) N/W STEER switch OFF . . . . . . . . . . . . . . 

N O T E

1. When landing with the nosewheel steering

inoperative, select the longest runway

available with minimum turbulence and

crosswind.

2. Use differential braking, rudder and engine

thrust as required to assist directional

control.

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 34 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 105

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete the following CAUTION from paragraph 38.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
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 35 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 108

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete the following CAUTION from step (9) of paragraph 40.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
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 36 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 113

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete steps 42.E.(30) and 42.F.(8).

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 37 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 114

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete step 42.G.(2).

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 38 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 115

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete step 42.I.(17).

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 39 of 55

TEMPORARY REVISION NO. 600/29

Insert in NORMAL PROCEDURES

Facing Page 116

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete steps 42.K.(1) and (2).

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 40 of 55

TEMPORARY REVISION NO. 600/29

Insert in EMERGENCY PROCEDURES

Facing Page 4A

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete the following CAUTION from paragraph 1.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
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 41 of 55

TEMPORARY REVISION NO. 600/29

Insert in EMERGENCY PROCEDURES

Facing Page 6C

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete the following CAUTION from paragraph 2.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
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 42 of 55

TEMPORARY REVISION NO. 600/29

Insert in EMERGENCY PROCEDURES

Facing Page 14

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete the following CAUTION from paragraph 7.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
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 43 of 55

TEMPORARY REVISION NO. 600/29

Insert in EMERGENCY PROCEDURES

Facing Page 15

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete the following NOTE from paragraph 7.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
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 44 of 55

TEMPORARY REVISION NO. 600/29

Insert in EMERGENCY PROCEDURES

Facing Page 16A

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete the following CAUTION from paragraph 8.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
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 45 of 55

TEMPORARY REVISION NO. 600/29

Insert in EMERGENCY PROCEDURES

Facing Page 16B

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete the following CAUTION from paragraph 8.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
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 46 of 55

TEMPORARY REVISION NO. 600/29

Insert in EMERGENCY PROCEDURES

Facing Page 16C

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete the following CAUTION from paragraph 8.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
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 47 of 55

TEMPORARY REVISION NO. 600/29

Insert in EMERGENCY PROCEDURES

Facing Page 17

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete the following CAUTION from paragraph 9.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
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 48 of 55

TEMPORARY REVISION NO. 600/29

Insert in EMERGENCY PROCEDURES

Facing Page 31

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Replace the CAUTION in paragraph 12.G. with the following:

C A U T I O N

When landing with anti-skid system OFF, extreme

caution is required during braking in order to avoid

tire damage.

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 49 of 55

TEMPORARY REVISION NO. 600/29

Insert in EMERGENCY PROCEDURES

Facing Page 34

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete the following CAUTION from paragraph 13.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
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 51 of 55

TEMPORARY REVISION NO. 600/29

Insert in EMERGENCY PROCEDURES

Facing Page 35 (Cont’d)

A. ENGINE FAILURE OR REJECTED TAKE-OFF BEFORE ACHIEVING V1 (Cont’d)

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
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 50 of 55

TEMPORARY REVISION NO. 600/29

Insert in EMERGENCY PROCEDURES

Facing Page 35

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Replace paragraph 14.A. with the following:

A. ENGINE FAILURE OR REJECTED TAKE-OFF BEFORE ACHIEVING V1

Rejection of the take-off must be initiated no later than V1.

(1) Thrust levers Move rapidly to LOW IDLE. . . . . . . . . . . . . . . . . 

(2) Wheel brakes . . . . . . . . . . . . . . . . Apply

N O T E

On rough runway surfaces, if a 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.

(3) Flight spoilers Extend . . . . . . . . . . . . 

If fitted:

(4) Ground spoilers . . . . . . . . . . . . Extend

(5) Maximum braking . . . . . . . . . . Maintain until a safe stop on runway is

assured.

(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).

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 52 of 55

TEMPORARY REVISION NO. 600/29

Insert in PERFORMANCE

Facing Page 30

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Replace paragraph 6.C. with the following:

C. DEMONSTRATED CROSSWIND (LANDING AND TAKE-OFF)

The maximum demonstrated crosswind component on a dry runway is 26.5 knots

(reported wind at 33 feet (10 meters) tower height), and is not limiting for

take-off or landing.

During a take-off, a rejected take-off or a landing in a strong crosswind,

harsh use of the lateral controls may be necessary to keep the wings level.

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 53 of 55

TEMPORARY REVISION NO. 600/29

Insert in PERFORMANCE

Facing Page 104

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Replace paragraph 11.H.(1) with the following:

(1) Actual landing distances for varying conditions of airplane weight,

airport pressure altitude and wind are provided by Figure 58.

Associated conditions:

Landing gear : Down

Flaps : 45 degrees

Engines : Both operating at LOW IDLE (Wing

 anti-ice system off) or

: Both operating at HIGH IDLE (Engines

 and wing anti-ice systems on − refer to

 NORMAL PROCEDURES − LANDING PROCEDURE).

Speed : 1.3 VS at 50 feet

Engine bleed air valves : As required

ACUs : On or Off

Engines and wing anti-ice : As required

Stall Protection System : Fully operative

 Altitude Compensation

Flight spoilers : Extended after touchdown

Brakes : Full application after touchdown

Anti-skid system : Fully operative

The example on Figure 58 shows that at an airplane weight of 34,000 lb

(15,420 kg), airport pressure altitude at sea level and with a 20 knot

headwind, actual landing distance is 888 metres (2915 feet) and required

landing field length is 1481 metres (4858 feet).

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 54 of 55

TEMPORARY REVISION NO. 600/29

Insert in PERFORMANCE

Facing Page 106

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete paragraph 11.H.(2) and Figure 59.

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL
DOT Approved

Jun 20/14

41,100 US TR 600/29

Page 55 of 55

TEMPORARY REVISION NO. 600/29

Insert in PERFORMANCE

Facing Page 108

REASON FOR ISSUE: To advise the flight crew of restricted operation from

contaminated runways and to prohibit the use of thrust

reversers.

ACTION: Delete the reference to Figure 59 in paragraph 11.I. and delete the

following NOTE from paragraph 11.I.(1):

N O T E

2. On airplanes 1086 and subsequent and

airplanes incorporating Canadair Service

Bulletin 600−0452, Modification − Ground

Spoilers − Auto Deployment, the factor to be

applied to the landing distance derived from

Figure 59 is 1.75 (75%).

MODEL CL−600−1A11

AIRPLANE FLIGHT MANUAL