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

1. The area other than the engine and APU
compartments that is provided with fire
detection is the:
A. Nose landing gear bay
B. Avionics bay
C. Main landing gear wheel bays
D. Baggage compartment
2. One of the Firex bottles discharges be-
cause of thermal overpressure; the indi-
cation that can be seen is:
A. Illumination of a LOW PRESS light
B. A frangible disc is missing.
C. Illumination of a SQUIB light
D. A pop-out warning button
3. A fire sensing loop suddenly becomes
pinched; the cockpit indication is:
A. Illumination of the associated FIRE
light
B. Illumination of the associated BOT-
TLE ARMED light
C. Illumination of the OVHT light
D. Illumination of the associated FIRE
WARN FAIL light
4. Illumination of an ENG FIRE light is ac-
companied by:
A. Illumination of a BOTTLE ARMED
light
B. Ringing of a fire bell
C. Illumination of an OVHT light
D. Sounding of a horn
5. If, during the warn test operation, the
APU BOTTLE ARMED switchlight fails
to illuminate, it indicates:
A. The APU is not operating.
B. The APU squib is unserviceable.
C. The APU Firex bottle pressure is low.
D. The fire detection loop is grounded.
8-16 CL 601-3A/R
CL-600-2B16 PILOT TRAINING MANUAL

QUESTIONS

6.
7.
8.
9.
FOR TRAINING PURPOSES ONLY
FlightSafety Canada
The number of Firex bottles that can be
discharged into a single engine com-
partment is:
A. 1
B. 2
C. 3
D 4
The engine fire bottles are located in the:
A. Nose compartment
B. Within each engine pylon
C. In the rear equipment bay
D. Beneath the lavatory sink
Depressing the LH ENG FIRE switchlight:
A. Closes the left engine fuel shutoff
valve
B. Closes the No. 1 hydraulic shutoff
valve
C. Closes the left bleed-air shutoff valve
D. All the above
With the APU operating and the APU
FIRE switchlight extinguished, pushing
the APU FIRE switchlight causes:
A. The APU to shut down
B. The APU fire bottle to discharge
C. The APU FIRE WARN FAIL light to
illuminate
D. The APU SQUIB light to illuminate
L t é e
L t d .