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TECH GENERAL — CH.36

AC Generation and DistributionAircraft & Engines — DGCA CPL practice questions

Question 1 of 5

The standard AC frequency in aircraft electrical systems is:

A.50 Hz
B.60 Hz
C.400 Hz
D.1000 Hz

All 5 questions — AC Generation and Distribution

Aircraft & Engines · DGCA CPL. The correct option is marked on each.

  1. Q1. The standard AC frequency in aircraft electrical systems is:

    • A.50 Hz
    • B.60 Hz
    • C.400 Hz
    • D.1000 Hz

    Why: Aircraft use 400 Hz three-phase AC — higher frequency permits smaller, lighter machines.

  2. Q2. A Constant Speed Drive Unit (CSDU) is used to:

    • A.Drive the alternator at constant speed despite varying engine RPM
    • B.Regulate DC voltage
    • C.Start the engine
    • D.Synchronise the propellers

    Why: The hydromechanical CSDU converts variable engine speed to constant output speed, holding the 400 Hz frequency. Combined with the generator it forms an IDG.

  3. Q3. A Transformer Rectifier Unit (TRU) converts:

    • A.DC to AC
    • B.115V AC to 28V DC
    • C.28V DC to 115V AC
    • D.400 Hz to 50 Hz

    Why: The TRU steps the 115V AC down and rectifies it to 28V DC. The opposite job — battery DC to essential AC — is done by an inverter.

  4. Q4. Before AC generators can be paralleled onto a common bus, they must match in:

    • A.Temperature and pressure
    • B.Voltage, frequency and phase sequence
    • C.RPM only
    • D.Field current

    Why: Voltage, frequency and phase rotation must be synchronised; the system then shares real (kW) and reactive (kVAR) load equally.

  5. Q5. Static wicks on trailing edges serve to:

    • A.Improve aileron response
    • B.Discharge airframe static electricity safely into the atmosphere
    • C.Detect icing
    • D.Reduce drag

    Why: They bleed off static build-up, preventing interference with communications; bonding straps keep all metal parts at equal potential.