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severity of pull-up manoeuvers:
Flaps up: -1.0 G to 2.56 G
Flaps down: 0.0 G to 2.0 G
DOT Approved
LIMITATIONS °(l
Page 20
canadair
chauenqer
MODEL CL-600-2A12
AIRPLANE FLIGHT MANUAL
PSP 601-1A-1
8. SYSTEMS LIMITATIONS (Cont'd)
A. AIR CONDITIONING AND PRESSURIZATION (STRUCTURAL LIMITATIONS)
The maximum relief differential pressure is 9.20 psi.
During taxi, take-off and landing, the pressure differential must not
exceed 1.0 psi.
B. AUTOMATIC FLIGHT CONTROL SYSTEM
Operation of the autopilot is prohibited at altitudes below 200 feet above
ground level.
The autopilot must be disengaged at speeds below VR^p.
The autopilot is not approved for continued approach following engine
failure on final approach (refer to EMERGENCY PROCEDURES - AUTOMATIC FLIGHT
CONTROL SYSTEM EMERGENCIES).
Maximum flap angle for single engine autopilot coupled approach is 20
degrees with VR E F + 20 KIAS.
DOT Approved
Mar 10/89 LIMITATIONS
44,600 Page 21
canadair
chanenqer
MODEL CL-600-2A12
AIRPLANE FLIGHT MANUAL
PSP 601-1A-1
8. SYSTEMS LIMITATIONS (Cont'd)
　
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