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1.
Hydraulic systems No. 1 and No. 2 each
have:
A. One engine-driven pump and one elec-
trically driven pump
B. Two electrically driven pumps
C. One engine-driven pump only
D. One electrically driven pump only
2.
The hydraulic reservoirs are:
A. Unpressurized
B. Pressurized by engine bleed air
C. Pressurized by a bootstrap system
D. Pressurized by a nitrogen precharge
3.
Motor-operated firewall shutoff valves
are installed in the:
A. Suction lines to all hydraulic pumps
B. Suction lines to all electrically driven
pumps
C. Pressure lines of the two engine-
driven pumps
D. Suction lines of the two engine-
driven pumps
4.
The 3B pump operates:
A. Only when the ADG is deployed
B. Only when switched on with the NO.
3 ELECT PUMP switch
C. Automatically when the ADG is de-
ployed, or when switched on with the
NO.3B ELECT PUMP switch
D. When the ADG is deployed and the
N O . 3 E L E C T P U M P s w i t c h i s
placed on
5.
Fluid filtration occurs:
A. Only in the pressure system
B. Only in the return system
C. Only in the bypass system
D. In the pressure system, the return sys-
tem, and the case drain system
13-10 CL 601-3A/R
CL-600-2B16 PILOT TRAINING MANUAL
QUESTIONS
6.
7.
8.
FOR TRAINING PURPOSES ONLY
FlightSafety Canada
If the left generator fails in flight, B
pump(s):
A. In the No. 2 system will be inoperative
B. In the No. 1 system will be inoperative
C. In both the No. 1 and No. 2 systems
will be inoperative
D. In the No. 3 system will be inoperative
The three hydraulic systems are:
A. Always hydraulically interconnected
B. Never hydraulically interconnected
C. Interconnected under certain condi-
tions
D. None of the above
In flight, when a No. 1 and No. 2 gener-
ator failure occurs while the APU is not
operating, hydraulic pressure in system
No. 3 is provided by:
A. The 3B pump
B. The 3A and 3B pumps
C. Engine-driven pumps
D. None of the above
L t é e
L t d .
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