BOMBARDIER Challenger 601-3A CL-600-2B16 Pilot Training Manual page 89

1. The primary Challenger electrical sys-
tem is:
A. 115-volt AC
B. 30-volt DC
C. 24-volt DC
D. 30-volt AC
2. A constant generator speed is ensured by
the:
A. GCU
B. ADG
C. CSD
D. RAT
3. The number of AC generators is:
A. 1
B. 2
C. 3
D. 4
4. Emergency in-flight AC power is pro-
vided by:
A. IDG
B. ADG
C. GCU
D. CSD
5. The CSD oil quantity is checked by:
A. Looking at a pop-out indicator
B. Reading a gage
C. Viewing a sight glass
D. Monitoring a light.
6. While on the ground, AC power can be
supplied by the engines or by a(n):
A. APU generator
B. External DC connector
C. ADG
D. CSD
CL-600-2B16 PILOT TRAINING MANUAL
QUESTIONS
7.
8.
9.
10. Primary DC power is supplied by a(n):
FOR TRAINING PURPOSES ONLY
FlightSafety Canada
A source of emergency in-flight AC power
is:
A. IDG
B. CSD
C. ADG
D. TRU
If the ADG is inadvertently deployed, it
can be retracted:
A. By depressing the reset switch
B. With a manual crank
C. By holding the deploy button down for
3 seconds
D. Only on the ground
If the OVLD light illuminates:
A. Generator load has exceeded 34.5 kva.
B. Automatic operation of GTC's is in-
hibited.
C. Both sides of the GLC are deener-
gized.
D. Both A and B are correct.
A. Inverter
B. TRU
C. Converter
D. ADG
L t é e
L t d .
CL 601-3A 2-29