Aircraft On-Board Maintenance Systems
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Questions and Answers

What is the primary purpose of the On-Board Maintenance System?

  • To assist maintenance personnel in fault-finding of complex avionics systems (correct)
  • To improve aircraft aerodynamics
  • To monitor aircraft performance during flight
  • To reduce the cost of aircraft maintenance
  • Which of the following systems is NOT part of the On-Board Maintenance System?

  • Report printing system
  • Data loading system
  • Electronic flight instrument system (correct)
  • Central Maintenance System
  • What is the main function of the Central Maintenance Computers (CMC) in the Central Maintenance System?

  • To store maintenance data
  • To enable the mechanic to extract maintenance data and initialise tests on aircraft systems (correct)
  • To display aircraft performance data
  • To control aircraft flight systems
  • What is the benefit of using the On-Board Maintenance System?

    <p>It minimises ground time and increases the efficiency of maintenance processes</p> Signup and view all the answers

    What is the function of the Multipurpose Control and Display Units (MCDU) in the Central Maintenance System?

    <p>To display maintenance data</p> Signup and view all the answers

    What type of maintenance is supported by the On-Board Maintenance System?

    <p>Both scheduled and unscheduled maintenance</p> Signup and view all the answers

    What type of system is used in conjunction with the aircraft ECAM or EICAS cockpit display systems?

    <p>Central Maintenance Computer</p> Signup and view all the answers

    What type of warnings are transmitted to the Central Maintenance Computer (CMC)?

    <p>Only primary and independent warnings</p> Signup and view all the answers

    What is the function of the CMC's Central Processing Unit (CPU)?

    <p>To organize the received data into reports</p> Signup and view all the answers

    What is included in the post or current flight report?

    <p>All ECAM warning/caution and failure messages</p> Signup and view all the answers

    What is stored in the CMC for the Previous Flight Report (PFR)?

    <p>All ECAM and failure messages recorded during the 63 previous flight legs</p> Signup and view all the answers

    What information is included in the data stored in the CMC?

    <p>The leg heading, date, flight number, city pair, and A/C identification</p> Signup and view all the answers

    What is a characteristic of Type 3 systems?

    <p>They have a discrete input for initialising or resetting the test.</p> Signup and view all the answers

    What is the purpose of the Multifunction Control Display Unit (MCDU)?

    <p>To provide access to data from the CMC system and test aircraft systems.</p> Signup and view all the answers

    Where are the data concerning all aircraft systems stored?

    <p>In the CMC's non-volatile memories.</p> Signup and view all the answers

    What is the function of the Central Maintenance Computers (CMCs)?

    <p>To acquire and process BITE information from aircraft systems.</p> Signup and view all the answers

    How do Type 1, 2, and 3 systems send their BITE information?

    <p>In parallel to both Central Maintenance Computers.</p> Signup and view all the answers

    What is the purpose of the CMS menu?

    <p>To provide access to CMC functions for operators.</p> Signup and view all the answers

    What is the primary tool used to select and update system software in the Boeing 777 aircraft?

    <p>Cursor Control Device (CCD) of the Maintenance Access Terminal (MAT)</p> Signup and view all the answers

    What is the consequence of incorrect software loading procedures in aircraft operations?

    <p>Disastrous sequence of events</p> Signup and view all the answers

    Where can software downloads be initiated in an aircraft?

    <p>Both in-flight and on-ground</p> Signup and view all the answers

    What happens after the computer acknowledges the request from the MCDU for software downloading?

    <p>The data is sorted into files</p> Signup and view all the answers

    What is the primary purpose of the data loader selector switch in the Airbus system?

    <p>To select the computer for software loading</p> Signup and view all the answers

    Why are software and system functional and confidence checks performed after software loading?

    <p>To prevent software mismatches or glitches</p> Signup and view all the answers

    What type of computer systems are typically used in Class 1 EFB systems?

    <p>Commercial Off-the-Shelf (COTS)-based computer systems</p> Signup and view all the answers

    What is required before Class 2 EFB systems can be used in an aircraft?

    <p>Airworthiness approval</p> Signup and view all the answers

    Where are additional display units usually installed in the cockpit?

    <p>Side panels</p> Signup and view all the answers

    What is the main difference between Class 1 and Class 2 EFB systems?

    <p>Class 1 is not attached to a mounting device, while Class 2 is</p> Signup and view all the answers

    What type of devices are Class 1 EFB systems considered?

    <p>Portable Electronic Devices (PEDs)</p> Signup and view all the answers

    Which document defines the classes of EFB hardware configurations?

    <p>All of the above</p> Signup and view all the answers

    Study Notes

    On-Board Maintenance Systems (OMS)

    • OMS is designed to assist maintenance personnel in fault-finding of complex avionics systems, minimizing ground time and improving maintenance process efficiency.
    • OMS consists of:
      • Central Maintenance System (CMS)
      • Data loading system
      • Electronic library system
      • Report printing system

    Central Maintenance System (CMS)

    • CMS enables mechanics to extract maintenance data concerning most aircraft systems and initialize tests on these systems.
    • Main components of CMS:
      • Central Maintenance Computers (CMC 1 and 2)
      • Multipurpose Control and Display Units (MCDU 1, 2, and 3)
    • CMS is used in conjunction with aircraft Electronic Centralised Aircraft Monitoring (ECAM) or Engine Indication and Crew Alerting System (EICAS) cockpit display systems.

    Central Maintenance Computer (CMC)

    • CMC receives primary and independent warnings or maintenance status type warnings from system BITEs.
    • CMC correlates messages with aircraft parameters to amalgamate fault information with time, date, flight phase, etc.
    • CMC stores maintenance data for retrieval, including:
      • Leg heading, date, flight number, city pair from, start time, and A/C identification
      • Warning messages transmitted ATA Sub ATA
      • Calculated warning code and type
    • CMC compiles a Previous Flight Report (PFR) by storing all ECAM and failure messages recorded during the 63 previous flight legs.

    Multifunction Control Display Unit (MCDU)

    • MCDU consists of a screen for data display, an alphanumeric keyboard, and line keys used to send commands to connected systems.
    • MCDU provides access to data from the CMC system and allows testing of aircraft systems, including self-tests and guided tests for system fault-finding.

    Data Loading

    • Data loading is similar to loading software onto a home computer.
    • Operator uses the Cursor Control Device (CCD) of the Maintenance Access Terminal (MAT) to select and update required system software.
    • Correct software loads and configurations are critical to aircraft operations, and software mismatches can cause disastrous sequences of events.

    Electronic Flight Bag (EFB)

    • EFB is an electronic device used on flight decks to perform various tasks that previously required reference books, aeronautical charts, and mathematical calculations.
    • The Civil Aviation Authorities define three EFB classes:
      • Class 1: Portable, Commercial Off-the-Shelf (COTS)–based computer systems used for aircraft operations.
      • Class 2: Portable, COTS-based computer systems used for aircraft operations, connected to aircraft power and mounting device on the flight deck.

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    Description

    Learn about the On-Board Maintenance System (OMS) designed to assist maintenance personnel in fault-finding of complex avionics systems. This system is a common framework for various functions supporting aircraft maintenance and engineering follow-up activities.

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