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

1. The CF 34 engine may be defined as a:
A. Single-spool, medium-bypass turbofan
B. Nonmodular, single-spool turbofan
C. Twin-spool, high-bypass turbofan
D. High-bypass geared turbofan
2. The compressor surge margin is main-
tained by:
A. Variable compressor inlet and stator
guide vanes
B. A fuel pressure-operated bleed strap
C. Variable fan inlet and compressor inlet
guide vanes
D. Pneumatically operated compressor
bleed valves
3. When checking the engine instruments
with battery power only, the indication on
the oil pressure indicator is:
A. The blue power-on segments will re-
main extinguished.
B. All segments on the left scale will be
illuminated.
C. Both scale segments will flash on and
off alternately.
D. Alternate segments will illuminate
for both left and right scales.
4. The primary thrust indicator for CF34
engine is the:
A. N rpm
1
B. ITT
C. N rpm
2
D. Fuel flow
5. Fan rpm limiting is a sole function of the:
A. Position of the variable-geometry
system
B. Jump and rate system in the FCU
C. FCU governor
D. Speed control ECU on the FCU
7-30 CL 601-3A
CL-600-2B16 PILOT TRAINING MANUAL

QUESTIONS

6.
7.
8.
9.
FOR TRAINING PURPOSES ONLY
FlightSafety Canada
Electrical power for engine ignition is
supplied by the:
A. Battery bus and essential AC bus
B. Essential DC bus
C. AC bus 1 and AC bus 2
D. Self-contained exciters on each engine
Prior to engine starting, ITT is indicating
150°C; the starting procedure is:
A. Select Ignition A or B, but not both.
B. Advance the throttle as soon as start
is initiated.
C. Motor the engine with the throttle at
IDLE for 15 seconds.
D. Motor the engine without fuel or ig-
nition until ITT drops below 120°C.
For an in-flight engine start, the ATS may
be used if:
A. N rpm is greater than 55%.
2
B. N rpm is less than 55%.
1
C. N and N are within 5%.
1 2
D. N rpm is 55% or less.
2
One recommended airspeed range for a
windmilling airstart is:
A. 200 KIAS below 10,000 feet if N
not indicating
B. 300 KIAS to VMO between 10,000
feet and 21,000 feet
C. 250 KIAS at all altitudes
D. 300 KIAS below 10,000 feet if N
stable or decreasing
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