P ATG Electrical

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    P ATG Electrical

    The magneto is driven:

    Electrically;Mechanically;Pneumatically.

    Theory Low B 1

    The purpose of the alternator and generator is to:

    Provide electrical current to start the engine;Provide electrical current to operate the magnetos;Provide electrical current to recharge the battery.

    Theory Low C 1

    Why is it important to check that the earthing wire for the magnetos is not broken:

    To ensure that the magnetos can be switched on by electrical current;

    To ensure that the magnetos will stop producing a spark when isolated;To ensure that you can isolate the electrical system in case of electrical fire.

    App Low B 1An alternator is:

    a BatteryAn AC generatorCharged continously by the battery

    Theory Low B 1

    Whilst flying in the GF area the pilot notices that the left /zero ammeter is indicating zero. What could be theproblem?

    Failed battery;The alternator is no longer charging the battery;There is no spark being supplied by the magnetos

    Theory Medium B 1

    The pilot notices that the turn co-ordinator, oil temperature gauge and fuel quantity gauge are not operating,what could be the problem.

    Vacuum pump failure;Pitot tube blocked;Electrical failure.Theory Medium C 1

    As well as the additional safety factor, dual ignition systems also provide:

    Improved engine performance;Better heat control of the engine;Easier starting.

    Theory Medium A 1

    A pilot inadvertently switches the master switch off in flight. The following will be affected:

    The engine will stop;

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    The ASI and Altimeter will mis-read;Most electrical equipment would be inoperative. ie: Radios, Oil temp and fuel quantity gauges.

    Theory Medium C 1

    Aircraft magnetos obtain electrical energy from:

    BatteriesAlternatorsself-contained magnets

    Theory Medium C 1

    The probable reason an engine continues to run after the ignition switch has been turned off is:

    faulty magneto timinga broken magneto ground wirea cracked intake manifold

    Theory Medium B 1

    A Fuse / Circuit breaker:

    Can be replaced/reset on the ground onlyIs self resetting after the fault has been rectifiedMay be replaced/reset manually after the fault has been rectified

    Theory Medium C 1

    Warning of an electrical overload would be given by:

    Low ampsHigh ampsNo amp indication

    Theory Medium B 1

    If the switch of a magneto becomes disconnected in flight:

    the affected magneto will automatically be isolated.the alternative magneto will maintain ignition.the affected magneto will continue to provide a spark

    Theory High C 1

    What actions must a pilot take in order to resolve a suspected alternator problem?

    Switch all electrical components off.If you can reset the alternator; reset it, otherwise broadcast intentions then switch off unnecessary electricsand return to the field.Broadcast intentions and return to the field using as little power as possible so the alternator cansupply a charge to the aircraft systems.

    App High B 1

    Accelerating the magneto momentarily to generate high voltage at very low RPM is the function of the:

    Left Magneto;

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    Right Magneto;Impulse Coupling.

    Theory High C 1

    Fuses are fitted:

    In parallel with the loadIn series with the loadIn parallel with the circuit breakers

    Theory High B 1