Aircraft On-Board Maintenance System (OMS) Introduction
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Questions and Answers

What is the primary function of the On-Board Maintenance System (OMS)?

  • To provide real-time weather updates to the pilots
  • To perform automatic maintenance tasks
  • To assist maintenance personnel in fault-finding of complex avionics systems (correct)
  • To monitor aircraft performance during flight
  • What is the main benefit of the On-Board Maintenance System (OMS)?

  • It increases the weight of the aircraft
  • It reduces the need for human maintenance personnel
  • It minimizes ground time, increases efficiency, and improves cost-effectiveness (correct)
  • It only supports line maintenance
  • Which component of the Central Maintenance System (CMS) is used to extract maintenance data?

  • Central Maintenance Computers (CMC) (correct)
  • Electronic library system
  • Multipurpose Control and Display Units (MCDU)
  • Data loading system
  • What is the purpose of the Electronic library system in the On-Board Maintenance System (OMS)?

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

    What is the benefit of the On-Board Maintenance System (OMS) in terms of engineering follow-up?

    <p>It supports systems, aircraft, and fleet monitoring</p> Signup and view all the answers

    What is the purpose of the Report printing system in the On-Board Maintenance System (OMS)?

    <p>To print maintenance reports</p> Signup and view all the answers

    What is the primary purpose of the ARINC 429 link between CMC 1 and CMC 2?

    <p>To enable cross talk and exchange general data between the two computers</p> Signup and view all the answers

    What is the purpose of the flight warning computers?

    <p>To monitor system failures and display warnings on the ECAM</p> Signup and view all the answers

    How are system failures classified on the ECAM display?

    <p>In three categories based on their operational and safety consequences</p> Signup and view all the answers

    What happens to warnings on the ECAM display at the end of the flight?

    <p>They are automatically cancelled</p> Signup and view all the answers

    What type of failures are displayed as warnings in real-time on the ECAM?

    <p>Class 1 failures with operational consequences for the current flight</p> Signup and view all the answers

    Where are fault codes and messages stored in case of a system failure?

    <p>In a non-volatile memory system</p> Signup and view all the answers

    What type of failure is the loss of one engine's hydraulic pump?

    <p>Class 2</p> Signup and view all the answers

    Where are the systems affected by Class 2 failures identified?

    <p>ECAM STATUS page</p> Signup and view all the answers

    What is the primary function of electronic flight bags on flight decks?

    <p>To perform tasks previously requiring reference books and mathematical calculations</p> Signup and view all the answers

    According to the Civil Aviation Authorities, how many classes of EFB hardware are defined?

    <p>Three</p> Signup and view all the answers

    What type of system computer can memorise failures occurring in the last 64 flights?

    <p>Type 1</p> Signup and view all the answers

    What is a characteristic of Class 1 EFB systems?

    <p>They are not attached to a mounting device on the flight deck</p> Signup and view all the answers

    What is the output connection for Type 2 system computers?

    <p>ARINC 429 bus</p> Signup and view all the answers

    What is possible with Class 2 EFB systems?

    <p>They can connect to avionics equipment</p> Signup and view all the answers

    What is the primary purpose of the CMC in relation to system computers?

    <p>To facilitate troubleshooting</p> Signup and view all the answers

    What message is displayed on the data loader LCD throughout the transfer?

    <p>TRANSFER IN PROG</p> Signup and view all the answers

    What is the typical capacity of a standard 3.5-inch disk used in older data loaders?

    <p>1.44 MB</p> Signup and view all the answers

    What type of failure has neither operational nor safety consequences for the aircraft?

    <p>Class 3</p> Signup and view all the answers

    What is the term for Class 1 EFB systems?

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

    What type of media is commonly used in newer data loaders?

    <p>PCMCIA cards</p> Signup and view all the answers

    What is a difference between Class 1 and Class 2 EFB systems?

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

    What is the purpose of loading Field Loadable Software (FLS) into the target hardware?

    <p>To load new software onto the aircraft</p> Signup and view all the answers

    Where should a copy of the loaded Loadable Software Aircraft Part (LSAP) be kept?

    <p>On-board the aircraft</p> Signup and view all the answers

    Who is authorized to issue a Certificate of Release to Service after loading a Loadable Software Aircraft Part (LSAP)?

    <p>Line/base maintenance staff</p> Signup and view all the answers

    Study Notes

    On-Board Maintenance System (OMS)

    • Developed to assist maintenance personnel in fault-finding of complex avionics systems
    • Uses a range of techniques to minimize ground time, improve maintenance efficiency, and reduce costs
    • Consists of Central Maintenance System (CMS), Data Loading System, Electronic Library System, and Report Printing System

    Central Maintenance System (CMS)

    • Enables mechanics to extract maintenance data and initialize tests on aircraft systems
    • Main components include Central Maintenance Computers (CMC 1 and 2) and Multipurpose Control and Display Units (MCDU 1, 2, and 3)
    • CMC 1 and CMC 2 are interfaced via an ARINC 429 link for cross-talk and can exchange general data

    Flight Warning Computers and ECAM Displays

    • Monitor operational data to display warnings and system information
    • Warnings are displayed automatically with the relevant flight phase and can be recalled from non-volatile memory
    • Failures are classified into three categories based on operational and safety consequences

    Failure Classification

    • Class 1: Failures with operational consequences for the current flight
    • Class 2: Failures with no operational consequences for the current flight
    • Class 3: Failures with no operational or safety consequences for the aircraft

    Aeroplane System Computers

    • Linked to CMC with different hardware interfaces and BITE characteristics
    • Categorized into three types based on memory and connection to CMC:
      • Type 1: Connected to both CMCs, can memorize failures from last 64 flights
      • Type 2: Memorizes failures from last flight, can initialize system tests

    Electronic Flight Bag (EFB)

    • Classified into three classes by Civil Aviation Authorities
    • Class 1: Portable, COTS-based, connected to certified power source, no administrative control required
    • Class 2: Portable, COTS-based, connected to aircraft power, airworthiness approval required
    • Class 3: Installed, aircraft-powered, airworthiness approval required

    Data Loading

    • Older data loaders use 3.5-inch disks (1.44 MB) or CD-ROMs (700+ MB)
    • Newer media include PCMCIA cards or USB sticks
    • Software Management: Field Loadable Software (FLS) loaded into target hardware using Portable Data Loader (PDL) or Airborne Data Loader (ADL)

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    Description

    Learn about the On-Board Maintenance System (OMS) designed to assist maintenance personnel in fault-finding complex avionics systems. Understand its functions and role in aircraft maintenance and engineering follow-up.

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