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44,600
Tire Pressures vs Maximum Take-Off Weight (MTOW)
(25.75 x 6.75 - 14 PR Tires)
Figure 8 LIMITATIONS
Page 29
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MODEL CL-600-2A12
AIRPLANE FLIGHT MANUAL
PSP 601-1A-1
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Page 30
Tire pressures vs Maximum Take-Off Weight (MTOW)
(A/C incorporating Service Bulletin 601-0360)
(25.75 x 6.75 - 14 PR tires)
Figure 9
DOT Approved
Sep 25/90
44,600
DOT Approved
Jan 19/07
44,600/45,100
LIMITATIONS
Page 31
8. SYSTEMS LIMITATIONS (Cont’d)
O. THRUST REVERSERS
Thrust reversers are approved for ground use only.
The thrust reverser pre-flight checks (NORMAL PROCEDURES) must be
successfully accomplished and the proper indications obtained on each
operative thrust reverser prior to each take-off.
Thrust reversers are intended for use during full stop landings. Do not
attempt a go-around manoeuvre after deployment of the thrust reversers.
Application of reverse thrust above 60% N1 is not permitted at airspeeds
below 60 KIAS.
The maximum demonstrated crosswind component approved for use of reverse
thrust is 24 knots (at 33 feet (10 meters) tower height). This value was
demonstrated on a dry runway and is considered limiting.
P. TAXI LIGHTS
Taxi lights must be switched off whenever the airplane is stationary in
excess of 10 minutes.
Q. AIR DATA SYSTEM
On airplanes incorporating Canadair Service Bulletin 601−0484, Reduced
Vertical Separation Minimum (RVSM) − 1000 Ft. Aircraft Qualification
Requirements;
 The ADC source coupled to the active autopilot must be the same as that
coupled to the ATC transponder during flight in RVSM airspace.
 If alternate static source is selected, airplane must not be operated
in RVSM airspace.
9. CONFIGURATION DEVIATION LIST
If the airplane is to be operated with certain secondary airframe and/or
nacelle parts missing, operation must be in accordance with the limitations
specified in the basic Airplane Flight Manual, and as amended by the
Configuration Deviation List (Appendix 1).
MODEL CL−600−2A12
AIRPLANE FLIGHT MANUAL
PSP 601−1A−1

　
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