a. Engine nacelles
b. Lavatory waste disposal compartment
c. Baggage compartments
d. All of the above - Correct Answer d. All of the above
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-+ optional for the apu
-fire protection panel only (engine, apu, baggage,cargo)
-lavatory detection indication is in the cabin only
2. The 24 hour system checks carried out by the flight crew include?
a. Beta backup test
b. Engine fire test
c. Baggage smoke warning test
d. B and C - Correct Answer d. B and C
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pre engine start every 24 hours includes cargo smoke test, flight compartment door test.
every flight engine fire test
3. Engine fire is indicated by illumination of
a. Both ENGINE FIRE PRESS TO RESET lights and the Master Warning lights
b. The CHECK FIRE DET Warning light
c. A PULL FUEL/HYD OFF handle light
,d. All of the above - Correct Answer d. All of the above
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see afm section 3 emergency procedure
4. What provisions do the Dash 8-400 have for Main and Nose Gear Ground Lock?
a. Lock pins for both Main Gears and for the Nose Gear
b. Lock pins for both Main Gears and hydraulic for Nose Gear
c. Lock pins for both Main Gears and external ground lock for Nose Gear
d. There is no provisions for Ground Lock of the Landing Gear - Correct Answer c. Lock pins for both
Main Gears and external ground lock for Nose Gear
--
ground lock pins are supplied for main gears,, ground lock mechanism for nose gear is controlled from
the outside
5. Performing the Flow Checklist and performing item LANDING GEAR SEL/LIGHTS/HORN on ground, you
notice the Landing Gear Door Lights is illuminated as well. This indicates?
a. An abnormal situation and you have to call for maintenance
b. The Door Ground lock pins are still installed in the hydraulic doors
c. The Landing gear Door lights are always illuminated on ground
d. The Landing gear Hydraulic Doors are open - Correct Answer d. The Landing gear Hydraulic Doors are
open
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the amber door advisory lights come on to shope the hydraulic operated gear doors are open
6. Weight-on-Wheels (WOW) proximity sensor signal
,a. Will allow the gear to retract on ground
b. Will prevent inadvertent gear retraction on the ground
c. Are situated on the landing gears doors only
d. Will be accessible through the PACIS system - Correct Answer b. Will prevent inadvertent gear
retraction on the ground
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pseu proximity sensor electronics unit monitors and controls landing gear. pseu monitors wt on wheels,
to prevent inadvertent retraction, if WOW fails, wt on wheels caution light
7. How are the gear and doors uplocked?
a. Electrically
b. Hydraulically
c. Mechanically
d. Mechanically and hydraulically - Correct Answer d. Mechanically and hydraulically
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mechanical-gear lever
hydraulic- operated by #2 hydraulic,
8. What is the maximum speed (VLO) were it is safe to extend the landing gear?
a. 215 kts
b. 173 kts
c. 152 kts
d. 200 kts - Correct Answer d. 200 kts
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limitations
, 9. An alternate landing gear extension is required when?
a. No. 1 hydraulic system fluid is zero
b. The #1 HYD ISO VLV caution light is illuminated
c. The #2 AC GEN caution light is illuminated
d. No. 2 hydraulic system fluid is zero or with the illumination of the LDG GEAR INOP caution light -
Correct Answer d. No. 2 hydraulic system fluid is zero or with the illumination of the LDG GEAR INOP
caution light
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alternate extension is used in case of:
-ldg gear inop caution light
-landing gear indication fails
-loss of #2 hyd pressure
10. Maximum main fuel tank imbalance between contents of fuel tanks is?
a. 143 kg
b. 272 kg
c. 571 kg
d. 952 kg - Correct Answer b. 272 kg
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limitations
11. With power failure to the FQC, the total fuel quantity indication on the FUEL page will show?
a. Zero
b. Full