BOMBARDIER Challenger 601-3A CL-600-2B16 Pilot Training Manual page 388

1. Normally, landing gear downlocks are
engaged:
A. Hydraulically
B. Mechanically
C. Electrically
D. None of the above
2. If the solenoid-operated landing gear han-
dle locking device fails to disengage at
lift-off, and neither WOW FAIL light is
illuminated:
A. Depress the DN LCK REL button to
free the handle.
B. The gear cannot be retracted.
C. Pull the applicable circuit breaker to
free the handle.
D. Override the locking device by ap-
plying more force to raise the handle.
3. Landing gear down and locked indica-
tions are:
A. Three green position indicator lights
illuminated, red handle lights flash-
ing
B. Three green position indicator lights
illuminated
C. No lights illuminated
D. Three green position indicator lights ex-
tinguished, red handle lights flashing
4. Emergency extension of the landing gear
is accomplished:
A. Pneumatically
B. Hydraulically only
C. Electrically
D. By manual release, free-fall, and hy-
draulically assisted downlocking
CL-600-2B16 PILOT TRAINING MANUAL
QUESTIONS
5.
6.
7.
8.
9.
FOR TRAINING PURPOSES ONLY
FlightSafety Canada
If the nosewheels are driven past 55°, the
disengaged rack and pinion should be:
A. Reengaged hydraulically
B. Reengaged without hydraulic power
C. Disconnected and the nosewheels
centered
D. None of the above
Brake pressure is provided by:
A. Both the No. 1 and No. 3 hydraulic
systems
B. Both the No. 1 and No. 2 hydraulic
systems
C. Both the No. 2 and No. 3 hydraulic
systems
D. The No. 3 hydraulic system only
The brake antiskid system provides:
A. Modulated skid protection for each
wheel
B. Locked wheel protection
C. Touchdown protection
D. All the above
When the parking brakes are set:
A. The brake metering valves are me-
chanically latched open, allowing
available hydraulic system pressure to
be applied to the brakes.
B. Pressure from hydraulic system No.
1 is applied to the brake assemblies.
C. The brake assemblies are mechani-
cally locked.
D. They cannot be released until pressure
in hydraulic system No. 2 is depleted.
The emergency brakes are applied with:
A. No. 1 hydraulic system pressure
B. Nitrogen pressure
C. There is no emergency brake system.
D. Master cylinder pressure
CL 601-3A/R 14-15
Lt é e
Lt d .