1.
Engine fire extinguisher containers are lo-
cated in:
A. The engine nacelles.
B. The tailcone.
C. Above the baggage compartment.
D. The engine pylons.
2.
The power-off preflight of the engine fire
extinguishers includes:
A. Checking the condition of the red and
yellow blowout discs and the bottle
pressure.
B. Activating the system TEST switch
to FIRE DET.
C. Checking the condition of the fire
sensing loop.
D. Checking the condition of the fire de-
tection control unit/s.
3.
Depressing a FIRE PUSH button closes
the following:
A. The fuel shutoff valve.
B. The bleed air pressure regulator and
shutoff valve.
C. The hydraulic shutoff valve and the
thrust reverser isolation valve.
D. All of the above.
4.
There is a smoke detector located:
A. In the tailcone baggage compartment.
B. At the rear of the cabin.
C. In the tailcone equipment compart-
ment.
D. This airplane does not have a smoke
detector.
5.
When an overheat/fire condition is de-
tected within an engine nacelle, all of the
following warnings are activated except:
A. A red “FIRE” is displayed within the
appropriate engine ITT arc on EICAS.
B. A repeating voice message, “Left or
right engine fire” will be heard.
C. A red “FIRE” light is displayed on
the CWP, along with a master warn-
ing light and chime.
D. A red “FIRE PUSH” light is illumi-
nated on the engine/fuel control panel.
6.
The following indications are presented
with activation of an APU fire:
A. Fire Push switch on APU control
panel illuminated.
B. Wa r n i n g h o r n i n l e f t w h e e l w e l l
sounds.
C. Red “APU FIRE” CAS message is
posted.
D. Both a. and c. are correct.
L E A R J E T 4 5
P I L O T T R A I N I N G M A N U A L
8-12
FOR TRAINING PURPOSES ONLY
FlightSafety
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