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  • SAE AIR 5924 : 2013

    Current The latest, up-to-date edition.
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    GUIDELINES FOR THE INTEGRATION OF ELECTRONIC ENGINE CONTROL SYSTEMS FOR TRANSPORT CATEGORY (PART 25) AND GENERAL AVIATION (PART 23) AIRCRAFT

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  16-01-2013

    Publisher:  SAE International

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    Table of Contents - (Show below) - (Hide below)

    1. SCOPE
    2. REFERENCES
    3. APPLICABILITY
    4. THRUST AND POWER CONTROL
    5. USE OF SENSORS, AIRCRAFT SIGNALS, AND DATA
    6. INSTRUMENTATION AND FLIGHT-CREW INTERFACES
    7. MAINTENANCE CONSIDERATIONS
    8. HARDWARE AND ENVIRONMENTAL ISSUES
    9. CERTIFICATION
    10. NOTES

    Abstract - (Show below) - (Hide below)

    Specifies methodologies and approaches that have been used to install and integrate full-authority-digital-engine-control (FADEC) systems on transport category aircraft.

    General Product Information - (Show below) - (Hide below)

    Committee E-36
    Document Type Revision
    Publisher SAE International
    Status Current
    Supersedes

    Standards Referencing This Book - (Show below) - (Hide below)

    FAA AC 23.1311-1 : 2011 INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES
    FAA AC 21-16 : 2011 RTCA DOCUMENT DO-160 VERSIONS D, E, F, AND G, "ENVIRONMENTAL CONDITIONS AND TEST PROCEDURES FOR AIRBORNE EQUIPMENT"
    SAE ARP 5107 : 2006 GUIDELINES FOR TIME-LIMITED-DISPATCH (TLD) ANALYSIS FOR ELECTRONIC ENGINE CONTROL SYSTEMS
    RTCA DO 178 : C2011 SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION
    FAA AC 20-88 : A GUIDELINES ON THE MARKING OF AIRCRAFT POWERPLANT INSTRUMENTS (DISPLAYS)
    FAA AC 20-53 : 2006 PROTECTION OF AIRCRAFT FUEL SYSTEMS AGAINST FUEL VAPOR IGNITION CAUSED BY LIGHTNING
    FAA AC 25-11 : 2014 ELECTRONIC FLIGHT DISPLAYS
    FAA AC 20-136 : 2011 AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION
    FAA AC 20-158 : 2014 THE CERTIFICATION OF AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEMS FOR OPERATION IN THE HIGH-INTENSITY RADIATED FIELDS (HIRF) ENVIRONMENT
    SAE AIR 6181 : 2011 ELECTRONIC PROPULSION CONTROL SYSTEM/AIRCRAFT INTERFACE CONTROL DOCUMENTS
    SAE AS 755 : 2014 AIRCRAFT PROPULSION SYSTEM PERFORMANCE STATION DESIGNATION
    FAA AC 25-13 : 0 REDUCED AND DERATED TAKEOFF THRUST (POWER) PROCEDURES
    FAA AC 33.28-1 : 0 COMPLIANCE CRITERIA FOR 14 CFR SECTION 33.28, AIRCRAFT ENGINES, ELECTRICAL AND ELECTRONIC ENGINE CONTROL SYSTEMS
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