Boeing 737 Flight Deck Electrical System Quiz
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Questions and Answers

What system provides emergency oxygen for the flight crew and passengers?

  • Passenger oxygen system (correct)
  • Flight crew oxygen system
  • Anti-Ice system
  • Air Systems A/C pack valves
  • Which system is responsible for controlling the pressurization and altitude warning on the aircraft?

  • Thrust reversers
  • Starter valves
  • Manual pressurization control (correct)
  • Engines N1 and N2
  • What lights indicate that the BLEED TRIP OFF function is active?

  • PACK lights (correct)
  • STANDBY POWER OFF light
  • PACK lights (correct)
  • General standby compass light
  • Which instrument should the Captain monitor for fire protection in the APU and engines?

    <p>Oil pressure, oil temperature</p> Signup and view all the answers

    What is the purpose of the upper display unit on the engines, APU?

    <p>To display N1, N2, EGT</p> Signup and view all the answers

    Which lights indicate that the STANDBY POWER is OFF?

    <p>PACK lights</p> Signup and view all the answers

    Which system is responsible for preventing ice buildup on critical components of the aircraft?

    <p>Anti-Ice system</p> Signup and view all the answers

    What does the Captain's pitot probe heat help prevent?

    <p>Ice buildup</p> Signup and view all the answers

    What is indicated by the Electrical STANDBY POWER OFF light being illuminated?

    <p>Standby power system inactive</p> Signup and view all the answers

    What is a crucial function of the Engines' thrust reversers?

    <p>To reverse the direction of engine rotation after landing</p> Signup and view all the answers

    Study Notes

    Electrical System Overview

    • Transfer bus 2 prioritizes the shedding of galleys and main bus during overload situations.
    • If overload persists, transfer bus 1's galleys and main bus are shed next.
    • In case of continued overload, in-flight entertainment (IFE) buses are the last to be shed.
    • Automatic load restoration occurs when there is increased generator capacity; manual restoration is possible using the CAB/UTIL Power Switch.

    APU Load Shedding

    • When the APU is the sole power source in flight, all galley and main buses are automatically shed.
    • If overload continues, both IFE buses are also shed.
    • On the ground, the APU can support a full electrical load but will shed galley and main buses to manage overload.
    • Manual restoration of power can be performed similarly by toggling the CAB/UTIL Power Switch.

    Power Source Management

    • The APU GEN switch connects APU power to both transfer buses; the last selected source powers both.
    • It is not possible to independently power transfer buses with different sources (APU and external).
    • Engine generators can power transfer buses by temporarily switching the generator switch ON.

    Transfer Bus Operations

    • When external power or APU is supplying, and engine generators are applied, the system maintains power continuity.
    • In flight, engine generators usually power their respective transfer buses, and backups are facilitated automatically through bus tie breakers (BTBs).
    • If an engine generator fails, the other engine generator can supply power to both transfer buses.

    System Redundancy Features

    • The APU can power either or both transfer buses and is equipped with an automatic generator on-line feature.
    • Upon APU shutdown or failure, engine generators automatically connect to their respective transfer buses, activating this process only once during flight.

    Bus Tie System

    • Either generator or the APU can power both transfer buses; an automatic transfer system activates if any source disconnects.
    • The BUS TRANS switch in AUTO ensures power redirection to the unpowered transfer bus via BTBs.

    Flight Deck Auxiliary Power System

    • Comprises power converters and AC outlets for Flight Deck personal electronic devices (PEDs).
    • Protective devices prevent tampering with the outlets; correct insertion of plugs is required for power activation.

    Automatic Load Shedding

    • Single generator operations shed electrical loads incrementally by sensing actual load levels.
    • A specific list identifies essential equipment functional on battery power when all generators are inoperative.

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    Description

    Test your knowledge on the electrical system of the Boeing 737 flight deck, including the operation of the Bus Trans switch and the Auxiliary Power System. Explore how the transfer buses are powered and controlled in different scenarios.

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