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

1. The engine-driven fuel pumps are nor-
mally supplied with fuel by the:
A. Main ejectors
B. Standby electric pumps
C. Scavenge ejectors
D. Transfer ejectors
2. If the main ejectors fail, the engine-driven
fuel pumps will be supplied with fuel by:
A. Gravity
B. Scavenge ejectors
C. Standby electric pumps
D. Transfer ejectors
3. Fuel imbalance between the main tanks
is corrected by:
A. Transfer ejectors
B. Scavenge ejectors
C. Standby pumps
D. Gravity crossflow
4. The scavenge ejectors:
A. Transfer fuel from the auxiliary tanks
to the main tanks.
B. Provide a flow of fuel from the main
tanks to the collector tanks.
C. Supply fuel to the engine-driven
pumps.
D. Transfer fuel from the main tanks to
the auxiliary tank and correct a fuel
imbalance when the crossflow valve
is open.
5-18 CL 601-3R
CL-600-2B16 PILOT TRAINING MANUAL

QUESTIONS

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FOR TRAINING PURPOSES ONLY
FlightSafety Canada
Flapper valves in the main tanks prevent:
A. Reverse flow of fuel from the main
tanks to the auxiliary tank
B. Reverse flow of fuel from the auxil-
iary tank to the main tanks
C. Gravity flow of fuel from the out-
board main tank sections to the in-
board main tank section
D. Reverse flow of fuel from the inboard
main tank sections to the outboard
main tank sections
Fuel for the APU is normally supplied by:
A. The left scavenge ejector
B. An electric pump in the right main
tank
C. An electric pump in the left main tank
D. The right main ejector
In case of a negative G condition, fuel for
the APU is supplied by:
A. The left main ejector
B. An electric pump in the right collec-
tor tank
C. An electric pump in the left collector
tank
D. All the above
The pump switchlights on the fuel con-
trol panel control the:
A. APU fuel pump
B. Main ejectors
C. Standby electric pumps
D. Differential pressure check valve
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