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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 − N1Fan Speed Indicator: (1) T.O./NORM N1fan speed indicator trim switch...................T.O. Observe 0.0% to 2.0% (maximum) increase in indicated N1rpm. (2) Minimum N1for 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 MANUALDOT 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 − N1Fan Speed Indicator: (1) T.O./NORM N1fan speed indicator trim switch...................NORM MODEL CL−600−1A11 AIRPLANE FLIGHT MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 MANUALDOT 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 VSat 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 MANUALDOT 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 MANUALDOT 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