BOMBARDIER Challenger 601-3A CL-600-2B16 Pilot Training Manual page 347

1. The electrical power supply for automatic
pressurization control is supplied from:
A. DC bus 2
B. Battery bus
C. Essential DC bus
D. AC bus 2
2. If cabin pressure differential exceeds the
normal limit, it will be controlled by the:
A. Overpressure limiter
B. Pneumatic relay
C. Altitude limiter
D. Negative pressure-relief valve
3. The power supply for selection of the
emergency pressurization is from:
A. AC bus 2
B. DC bus 1
C. AC bus 1
D. The battery bus
CL-600-2B16 PILOT TRAINING MANUAL
QUESTIONS
4.
5.
FOR TRAINING PURPOSES ONLY
FlightSafety Canada
When the EMERgency DEPRESSuriza-
tion switchlight is pushed, it will:
A. Open the ram-air valve and close the
engine bleed-air valves.
B. Close the engine bleed-air valves and
both footwarmer and demist valves.
C. Open the ram-air valve and the emer-
gency pressurization valve.
D. Open the electropneumatic outflow valve.
During operation of the emergency pres-
surization, cabin altitude, differential,
and rate of change are controlled by the:
A. MANual REGulator and manual rate
selector only
B. Overpressure-relief valves
C. Automatic controller or manual reg-
ulator
D. Cabin altitude limiter
Lt é e
Lt d .
CL 601-3A 12-11