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Questions and Answers

What component does the GARRET 36-280 use for monitoring and control?

  • Full Authority Digital Electronic Control (FADEC) (correct)
  • Basic Control Unit
  • Manual Control Panel
  • Analog Control System
  • What happens when the low oil pressure light illuminates?

  • The APU will automatically shut down. (correct)
  • The APU continues to operate normally.
  • The maintenance light illuminates.
  • A warning is sent to the cockpit.
  • Which APU model has a 60-second cooldown option?

  • GARRET 36-280
  • SUNDSTRAND APS 2000
  • GARRET 85-129 (correct)
  • None of the above
  • What does the APU fire warning light indicate?

    <p>A fire in the APU</p> Signup and view all the answers

    Which model uses a maintenance light to indicate non-critical failures?

    <p>Both B and C</p> Signup and view all the answers

    What happens when the APU turbine speed exceeds its allowable rpm?

    <p>Overspeed light illuminates amber.</p> Signup and view all the answers

    What type of compressor does the GARRET 85-129 feature?

    <p>Two-stage centrifugal compressor</p> Signup and view all the answers

    What does the APU fire control handle do when pulled?

    <p>Arms the APU bottle discharge switch.</p> Signup and view all the answers

    What type of impellers does the SUNDSTRAND APS 2000 use?

    <p>Single centrifugal impeller</p> Signup and view all the answers

    Which of the following indicates a critical failure in the APU?

    <p>Fault light illuminated amber</p> Signup and view all the answers

    What is the purpose of the APU in an airplane?

    <p>To make the airplane self-sufficient by providing on ground electrical power</p> Signup and view all the answers

    How much KVA can the APU generator supply during flight operation?

    <p>50 KVA</p> Signup and view all the answers

    What feature automatically transfers power to an alternate generator when needed?

    <p>Bus Transfer Switch</p> Signup and view all the answers

    Which component converts 115V AC to 28V DC power?

    <p>Transformer/Rectifier Units</p> Signup and view all the answers

    What is the first action taken when ground power is available?

    <p>Engine generators are tripped off generator buses</p> Signup and view all the answers

    What is the maximum load displayed by the generator AC ammeter?

    <p>60 KVA</p> Signup and view all the answers

    Which of the following statements is true about operating the APU bleed air?

    <p>Using APU bleed air for air conditioning during takeoff improves takeoff performance</p> Signup and view all the answers

    What happens to the APU in the event of overspeed?

    <p>It shuts down automatically</p> Signup and view all the answers

    What is a feature of the APU designed to minimize exhaust noise heard by passengers?

    <p>Acoustically treated air inlet and exhaust duct</p> Signup and view all the answers

    What is the role of the Constant Speed Drive (CSD) in the electrical power system?

    <p>To maintain a constant speed for the generator</p> Signup and view all the answers

    Study Notes

    Electrical Power System

    • Three electrical generators power the aircraft (two engine driven, one APU driven)
    • APU provides self-sufficiency, supplying on-ground electrical power
    • Automatic Bus Transfer System increases electrical power reliability
    • Onboard power system annunciator and test modules monitor and detect malfunctions

    Constant Speed Drive (CSD) and Generator

    • CSD and generators are driven by each engine to produce 115 volts, 400Hz, three-phase AC power.
    • Each CSD supplies 50 KVA.
    • A Variable Speed Constant Frequency (VSCF) generator also produces 50 KVA
    • Transformer/Rectifier units convert 115V AC to 28V DC for other systems.
    • The APU generator provides 50/60 KVA (ground/flight).

    APU Generator Bus Switches

    • Connecting APU generator to generator buses #1 or #2.
    • Disconnecting from #1 or #2 generator buses.
    • APU can supply power to both generator buses during ground operations. During flight, APU can only power one generator bus.

    Ground Power and Bus Transfer

    • Enables use of ground power if available
    • Tripping engine/APU generators from buses when using ground power.
    • Automatic bus transfer system switches to the opposite generator if needed.
    • Isolates DC systems when the transfer switch is shut off.

    Auxiliary Power Unit (APU)

    • Garrett 85-129 and 36-280 models are used.
    • Sundstrand APS 2000 system controls and indicates APU operation.
    • APU mounted on accessory drive pad.
    • 60 KVA ground power, 50 KVA flight operation.
    • Supplies bleed air for air conditioning (and engine startup), optimizing takeoff.

    APU Starting

    • APU starts with airplane battery or external DC power.
    • Automatic shutdown happens with overspeed, high oil temperature, low oil pressure, or fire.

    Exhaust Noise Reduction

    • Noise reduced by acoustically treated inlet and exhaust ducts, and distance from cabin and ground service points.

    APU Access and Maintenance

    • APU readily accessible for inspection, maintenance, or removal through large fuselage access door.

    Garrett 85-129 Components

    • Two-stage centrifugal compressor with one radical inflow turbine.
    • Accessories grouped at the front.

    Garrett 36-280 Components

    • Two centrifugal impellers and a single centrifugal turbine with a containment ring.

    Fire Protection System

    • APU housed in a fire protection shroud to contain fires.
    • Fault causes "DET INOP" light and master warning lights activation.

    Controls & Indicators

    • Panel located on the forward head panel
    • Includes APU switch (on/off/start positions, cooldown option)
    • Maintenance light illuminates when oil tank is low.
    • Provides indicators on the APU fire system
    • Includes lights to warn of non-critical and critical failures.
      • Oil low pressure
      • Overspeed condition
      • Critical part failure.
    • Contains AC ammeter to display current.
    • Provides exhaust gas temperature indicator

    APU Fire Protection Controls

    • Illuminated red light = APU fire.
    • Fire warning horn when fire detected.
    • APU fire control handle activates system
    • Bottle discharge switch triggers fire suppression.

    Pneumatics

    • APU pressurizes air for engine starting
    • Air source obtained from onboard APU or external ground cart.
    • Uses 5th stage compressor air section for flight, and 9th stage for low-engine.
    • Precooler system to control air temperature.
    • APU used for air conditioning up to 17,000 ft altitude

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