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  • FAA AC 33.28-1 : 0

    Current The latest, up-to-date edition.

    COMPLIANCE CRITERIA FOR 14 CFR SECTION 33.28, AIRCRAFT ENGINES, ELECTRICAL AND ELECTRONIC ENGINE CONTROL SYSTEMS

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date: 

    Publisher:  Federal Aviation Administration

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

    1 PURPOSE
    2 RELATED REGULATIONS
    3 RELATED REFERENCE MATERIAL
    4 APPLICABILITY

    Abstract - (Show below) - (Hide below)

    Gives guidance and acceptable methods, but not the only methods, that may be used to demonstrate compliance with Section 33.28 of Title 14 of the Code of Federal Regulations (14 CFR 33.28), Electrical and electronic engine control systems.

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

    Document Type Standard
    Publisher Federal Aviation Administration
    Status Current

    Standards Referenced By This Book - (Show below) - (Hide below)

    FAA AC 20-115 : 2017 AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( )
    FAA AC 20-174 : 2011 DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS
    FAA AC 20-170 : 2013 INTEGRATED MODULAR AVIONICS DEVELOPMENT, VERIFICATION, INTEGRATION, AND APPROVAL USING RTCA/DO-297 AND TECHNICAL STANDARD ORDER-C153
    FAA AC 23-24 : 2005 AIRWORTHINESS COMPLIANCE CHECKLISTS FOR COMMON PART 23 SUPPLEMENTAL TYPE CERTIFICATE (STC) PROJECTS
    FAA AC 00-69 : 2017 BEST PRACTICES FOR AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( )
    FAA AC 23-16 : 0 POWERPLANT GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES AND AIRSHIPS
    FAA 8110.49 : 2011 SOFTWARE APPROVAL GUIDELINES
    FAA AC 00-66 : 2015 SELECTION OF CYCLIC REDUNDANCY CODE AND CHECKSUM ALGORITHMS TO ENSURE CRITICAL DATA INTEGRITY
    MIL-HDBK-516 Revision C:2014 AIRWORTHINESS CERTIFICATION CRITERIA
    SAE ARP 6109 : 2014 ELECTRONIC ENGINE CONTROL HARDWARE CHANGE MANAGEMENT
    FAA AC 20-156 : 2006 AVIATION DATABUS ASSURANCE
    SAE AIR 5924 : 2013 GUIDELINES FOR THE INTEGRATION OF ELECTRONIC ENGINE CONTROL SYSTEMS FOR TRANSPORT CATEGORY (PART 25) AND GENERAL AVIATION (PART 23) AIRCRAFT
    FAA AC 20-145 : 2003 GUIDANCE FOR INTEGRATED MODULAR AVIONICS (IMA) THAT IMPLEMENT TSO-C153 AUTHORIZED HARDWARE ELEMENTS

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

    MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
    MIL-HDBK-217 Revision F:1991 RELIABILITY PREDICTION OF ELECTRONIC EQUIPMENT
    MIL-STD-461 Revision G:2015 REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
    MIL-STD-462 Revision D:1993 MEASUREMENT OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS
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