1.
Engine fire detection and/or overheat is
sensed by:
A. Thermocouples
B. Thermostats
C. Continuous-wire sensing elements
D. Thermistors
2.
The fire-extinguishing container charge
is indicated by:
A. A red disc on the rear fuselage
B. A gage on each container
C. Armed lights
D. A yellow disc on the rear fuselage
3.
Engine fire extinguisher containers are
located in:
A. The nacelles
B. The engine pylons
C. The tailcone
D. The baggage compartment
4.
If the fire persists after activating a
fire bottle:
A. A second fire bottle can be dis-
charged into the affected area.
B. The second fire bottle can only be
used on an opposite-side fire.
C. The first fire bottle can be dis-
charged a second time.
D. No further activation of the system
is possible; both bottles discharge
simultaneously when either
ARMED button is pressed.
5.
Airplanes with glareshield warning
lights—When the left FIRE light is
depressed:
A. It discharges one extinguisher into
the left nacelle.
B. It closes the main fuel and hydraulic
shutoff valves for the left engine
and arms the left ARMED lights.
C. It discharges one extinguisher and
arms the second.
D. It ruptures the yellow discharge
indicator disc.
6.
Airplanes without glareshield warning
lights—When the left FIREWALL
SHUTOFF switch is actuated:
A. It closes the main fuel and hydraulic
shutoff valves for the left engine
and arms the No. 1 and No. 2 dis-
charge switches.
B. It discharges one extinguisher into
the left nacelle.
C. It discharges one extinguisher and
arms the second.
D. It ruptures the yellow discharge
indicator disc.
8-6
FOR TRAINING PURPOSES ONLY
LEARJET 20 SERIES PILOT TRAINING MANUAL
FlightSafety
international
QUESTIONS