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  • FAA AC 23-15 : 2003

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    SMALL AIRPLANE CERTIFICATION COMPLIANCE PROGRAM

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  01-01-2003

    Publisher:  Federal Aviation Administration

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

    1 Purpose
    2 Cancellation
    3 Related Regulations And Documents
    4 Background
    5 Acceptable Method Of Compliance
    LIST OF ILLUSTRATIONS

    Abstract - (Show below) - (Hide below)

    Gives a compilation of historically acceptable means of compliance to specifically selected sections of 14 CFR part 23 that have become burdensome for small, simple, low performance airplanes (see Applicability section below) to show compliance.

    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 23.1311-1 : 2011 INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES
    FAA AC 23-24 : 2005 AIRWORTHINESS COMPLIANCE CHECKLISTS FOR COMMON PART 23 SUPPLEMENTAL TYPE CERTIFICATE (STC) PROJECTS
    FAA AC 23-19 : 2007 AIRFRAME GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES
    FAA AC 23-11 : 2009 14 CFR PART 23 TYPE CERTIFICATION OF AN AIRPLANE ORIGINALLY CERTIFICATED TO EUROPEAN AVIATION SAFETY AGENCY (EASA) (CS-VLA) STANDARDS OR JOINT AVIATION REQUIREMENTS - VERY LIGHT AIRPLANE (JAR-VLA)
    FAA AC 23-16 : 0 POWERPLANT GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES AND AIRSHIPS

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

    FAA AC 23.1311-1 : 2011 INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES
    RTCA DO 178 : C2011 SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION
    FAA AC 20-121 : A AIRWORTHINESS APPROVAL OF LORAN-C NAVIGATION SYSTEMS FOR USE IN THE U.S. NATIONAL AIRSPACE SYSTEM (NAS) AND ALASKA
    FAA AC 20-53 : 2006 PROTECTION OF AIRCRAFT FUEL SYSTEMS AGAINST FUEL VAPOR IGNITION CAUSED BY LIGHTNING
    FAA AC 20-136 : 2011 AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION
    FAA AC 21-22 : 0 INJURY CRITERIA FOR HUMAN EXPOSURE TO IMPACT
    FAA AC 23-8 : 2011 FLIGHT TEST GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES
    FAA AC 23.1309-1 : 2011 SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES
    FAA AC 21-40 : 2007 GUIDE FOR OBTAINING A SUPPLEMENTAL TYPE CERTIFICATE
    FAA AC 23-17 : 2011 SYSTEMS AND EQUIPMENT GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES AND AIRSHIPS
    FAA AC 20-130 : 0 AIRWORTHINESS APPROVAL OF NAVIGATION OR FLIGHT MANAGEMENT SYSTEMS INTEGRATING MULTIPLE NAVIGATION SENSORS
    FAA AC 23.629-1 : 2004 MEANS OF COMPLIANCE WITH TITLE 14 CFR, PART 23, SECTION 23.629, FLUTTER
    FAA AC 23.562-1 : 0 DYNAMIC TESTING OF PART 23 AIRPLANE SEAT/RESTRAINT SYSTEMS AND OCCUPANT PROTECTION
    FAA AC 20-115 : 2017 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 AC 20-135 : 0 POWERPLANT INSTALLATION AND PROPULSION SYSTEM COMPONENT FIRE PROTECTION TEST METHODS, STANDARDS AND CRITERIA
    FAA AC 23-11 : 2009 14 CFR PART 23 TYPE CERTIFICATION OF AN AIRPLANE ORIGINALLY CERTIFICATED TO EUROPEAN AVIATION SAFETY AGENCY (EASA) (CS-VLA) STANDARDS OR JOINT AVIATION REQUIREMENTS - VERY LIGHT AIRPLANE (JAR-VLA)
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