ELECTRIC POWER SYSTEM – Air – DGCA Question Bank For Politics

#1. In an electrical circuit the reverse current cut-out relay will open:

when battery voltage exceeds generator voltage.

when circuit voltage is less than generator voltage.

when the main output C/B is reset.

when the batteries are flat.

#2. A generator cut-out is provided:

to prevent the battery over heating.

to prevent the battery from being overcharged.

to allow the generator to be isolated in a crash.

to prevent discharge of the battery through the generator.

#3. A generator cut-out will open when:

circuit loads equal the battery voltage.

the air temperature reaches 45 C.

circuit loads equal the generator voltage.

generator voltage falls below battery voltage.

#4. A generator cut-out is fitted to prevent:

the battery discharging through the generator windings.

the generator overcharging the battery.

fire in the event of overloading the system.

out of phasing.

#5. In the event of the cut-out points sticking in the closed position, the most probable results, when the engine stopped would be:

gain of engine power.

a burnt out generator.

loss of residual magnetism.

no apparent reaction.

#6. To prevent circulating currents when more than one generator is being connected to the same bus bar:

reverse current relays are fitted.

the generators are connected in series.

rectifiers are fitted.

differential cut-outs are used.

#7. A generator cut-out is fitted:

in series with the generator output.

in the diode circuit.

in parallel with the generator output.

in the field circuit.

#8. On a 28 volt system with a 24 volt battery the cut-out contacts close at approximately:

36 volts.

24 volts.

28 volts.

26 volts.

#9. A component whose job is similar to a generator cut out is:

a rectifier.

a converter.

an inverter.

a reverse current relay.

#10. If the cut-out is open, the battery is feeding the loads which are:

in series with the battery.

in parallel with the battery.

in sequence with the cut-out.

cross coupled.

#11. In a two engine aircraft with two generators, there would be:

one ammeter for each generator and one voltmeter switchable to indicate either generator voltage or battery voltage.

one voltmeter for each generator. and one ammeter switchable to indicate either generator current or battery current.

one ammeter showing the total output and one switchable voltmeter .

one ammeter and one voltmeter each showing the average current and voltage output.

#12. A generator converts mechanical energy to electrical by:

electro magnetic spring action.

electro magnetic induction.

electrostatic induction.

electro dynamic induction.

#13. In an aircraft electrical system which incorporates a voltmeter, the voltmeter indicates:

the flow in the electrical system before the battery cut-out contacts close.

the rate of flow at all times.

the pressure in the electrical system before and after the cut-out contacts close.

the flow in the electrical system after the battery cut-out contacts close.

#14. If the generator warning light comes on in flight it indicates that:

the generator is feeding the battery bus bar.

the generator is not feeding the battery bus bar.

the battery has failed.

a rectifier is faulty.

#15. A generator failure is usually indicated by:

the ammeter reading decreasing or showing a discharge and a red warning lamp lighting.

the voltmeter reading increasing, the ammeter reading showing discharge and a red lamp lighting.

the current consuming devices failing to operate.

the motor speed increasing.

#16. A generator warning light will be illuminated:

when the battery voltage exceeds that of the generator and the cut-out has opened.

at night only.

when the generator is supplying current to a fully charged battery, and no electrical loads are switched on.

when the battery charge current is lower than required to maintain its fully charged state.

#17. If a generator fails in flight:

the voltmeter will read maximum.

the ammeter reading will decrease.

load sharing circuits will operate.

the watt metre will show a increase.

#18. If one generator fails you should:

switch off the good generator.

stop and feather the engine concerned.

switch off the failed generator and continue normal use of the electrical system.

switch off the failed generator, and cut down on the electrical services being used.

#19. A generator is brought ‘on the line’ when it is:

connected in series with other generators.

switched into the electrical circuit in parallel with the other generators.

connected with the ground batteries for starting.

connected to a phase reducer.

#20. In a twin engine aircraft, fitted with two generators, if one should fail:

the failed generator must be isolated.

cut down the air supply to reduce five risks.

the failed generator must be stopped.

both generators must be switched off.

#21. A generator is brought ‘on line’ via the battery cut-out by an increase in:

the battery voltage.

the radio by pass switch.

the generator voltage.

the generator field voltage.

#22. Generator failure is indicted by:

load sharing circuits connecting.

a decrease or discharge in ammeter readings and generator warning light on.

an increase in voltmeter readings, a discharge in ammeter reading and generator warning light on.

failure of electrically driven instruments.

#23. In a twin engine aircraft, with a generator fitted to both engines, the starboard generator fails. Will:

the starboard engine cut.

the port engine cut.

both engines run normally.

the engine with the failed generator will automatically feather.

#24. Loads on a bus bar are:

in series with the generator so that the voltage can be reduced.

in parallel so the voltage can be varied.

in parallel so the current can be reduced.

determined by the cross sectional area of the lead cable.

#25. When the battery master switch is switched off in flight:

the generators are disconnected from the bus bar.

the battery is isolated from the bus bar.

the battery is discharged through the bonding circuit diodes.

the battery may overheat.

#26. A generator is taken ‘off’ line by:

the battery switch.

operation of the field switch.

opening of the cut-out.

removing of all loads.

#27. If the ammeter reads plus 5 amp after engine shut down:

some switches have been left ‘on’.

the battery is charging.

the generator field switch is ‘on’.

the ammeter is defective.

#28. If the ammeter shows ‘no’ charge, yet the battery remains charged. Would you look for:

loose battery connections.

defective voltage regulator.

defective C/B.

defective ammeter.

#29. A field switch in the generator circuit is:

kept in the ‘on’ position.

connected in the armature circuit.

to ‘shut off’ the generator field.

to disconnect the battery.

#30. During flight a malfunction of the generator cut-out would be indicated by:

overheating of the battery.

the ammeter.

lights going out.

the current limiter.

#31. A short circuit in a “single pole” electrical circuit would be caused:

by a broken conductor between the source of supply and an item of equipment.

by an open circuit between loads in parallel.

when wiring between the source of supply and an item of equipment goes down to earth.

by an open circuit between an item of equipment and earth.

#32. In a “2 pole” electrical circuit, a short of the conductors would result in:

an item of equipment operating automatically without switches.

the component not working.

an increase in voltage.

an item of equipment burning out because of a large current flow.

#33. The indicating range of an ammeter can be increased by fitting;

A shunt fitted in parallel with the instrument.

A shunt fitted in parallel with the load A shunt fitted in parallel with the load

A shunt fitted in series with the instrument

A multiplier fitted in parallel with the instrument

#34. An electrical system which uses the aircraft structure as a return path for current, is known as:

a diode pole circuit.

an earth return circuit.

a single phase circuit.

a dipole circuit.

#35. On a single pole circuit, if the positive conductor is shorted to the aircraft structure:

the electrical component will operate.

the fuse will blow.

the circuit will be under loaded.

the load will only operate at half speed.

#36. In a double pole circuit:

the systems polarity will change.

the current is supplied by one wire and the current is returned through the aircraft bonding system.

the current passes out through one wire and is returned through a second wire.

the current passes out through one wire and is returned via the aircraft’s immune circuit.

#37. In a earth return circuit if the conductor is open circuited:

the fuse will blow.

the bus bars will overheat.

the load will not operate.

the generator will burn out.

#38. A ‘hot bus’ is:

the bus bar always connected to the battery

the bus bar that supplies the galley power

the bus bar that supplies the nom-essential loads

the bus bar that supplies the essential loads

#39. The earth return system of aircraft wiring is that:

one lead from the battery and one lead from the component is connected to the aircraft structure.

one lead from the battery is earthed and both leads of the components are earthed.

the negative sides of the system are connected direct to the positive side of the battery.

rectifiers are cross connected.

#40. A dipole circuit is one where:

diode valves are used.

three conductors are used.

the aircraft structure is used for the earth return.

two conductor wires are used.

Dgca Question Bank For Pilots

Results