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A320 Induction Technical Test

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A320 Induction Technical Test
A320 Induction Technical Test
Total Marks: 50 Test Duration: 2hrs
1) The normal priority for supplying electrical power to the AC busses is:
a) External power, engine generators then APU
b) External power, APU, then engine generators
c) APU, external power then engine generators
d) Engine generators, external power then APU
2) What is the maximum altitude at which the APU may be started using the batteries only? a) 15, 000 ft
b) 30, 000 ft
c) 25, 000 ft
d) 39, 000 ft
3) Can APU be used for Wing Anti Ice?
a) No
b) Yes but only below FL150
c) Yes but only when one pack is OFF
d) Yes can be used without any restrictions.
4) In normal flight in closed circuit configuration, the avionics ventilation system controls the temperature of the cooling air by:
a) Adding air conditioned air to the flow
b) Extracting air overboard
c) Passing air through a skin heat exchanger
d) None of the above.
5) What is the Max negative Differential pressure for the cabin?
a) 0 psi.
b) 1 psi.
c) 2 psi.
d) 8.6 psi.
Page 1 of 13
A320 Induction Technical Test
6) Electrical heating is used for :
a) Engine Anti Icing
b) Wing Anti Icing
c) Probes, Windows ,Windshield
d) None of the above
7) When would you select RAM AIR ON?
a) If additional cooling is required on the ground.
b) Dual pack failure or smoke removal.
c) When pack temperatures are too high.
d) Only when there is smoke in the cabin.
8) With the center tank pump mode SEL switch in AUTO; the center tank pumps:
a) Run for two minutes after both engines are running.
b) Will not restart until slats are retracted in flight.
c) Continue to run until five minutes after the center tank is empty before getting latched off.
d) All the above.
9) What does an amber line across the last two digits of the fuel quantity mean?
a) The fuel quantity indication is inaccurate.
b) The fuel quality is not good and should be checked.
Page 2 of 13
A320 Induction Technical Test
c) A disagreement between fuel

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