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  • FAA AC 33-2 : 2013

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    GENERAL TYPE CERTIFICATION GUIDELINES FOR TURBINE ENGINES

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  01-01-2013

    Publisher:  Federal Aviation Administration

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

    1. Purpose
    2. Applicability
    3. Cancellation
    4. Related Documents
    5. Related Reading Material
    6. General Type Certification Process
    7. Surplus Military Aircraft Engines and Parts
    8. Data Plates
    9. Part 33 Guidance Material

    Abstract - (Show below) - (Hide below)

    Specifies general guidance concerning type certification projects for aircraft turbine engines.

    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 20-73 : 2006 AIRCRAFT ICE PROTECTION
    MIL HDBK 516 : C AIRWORTHINESS CERTIFICATION CRITERIA
    FAA AC 23-16 : 0 POWERPLANT GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES AND AIRSHIPS
    FAA AC 33-6 : 2017 WELD REPAIR OF ALUMINUM CRANKCASES AND CYLINDERS OF PISTON ENGINES
    FAA AC 23-24 : 2005 AIRWORTHINESS COMPLIANCE CHECKLISTS FOR COMMON PART 23 SUPPLEMENTAL TYPE CERTIFICATE (STC) PROJECTS
    FAA AC 120-77 : 0 MAINTENANCE AND ALTERATION DATA
    FAA AC 43-207 : 2002 CORRELATION, OPERATION, DESIGN, AND MODIFICATION OF TURBOFAN/JET ENGINE TEST CELLS
    FAA 8110.4 : 2011 TYPE CERTIFICATION
    SAE AIR 1904 : 2012 TIRE SPRAY SUPPRESSION - AIRPLANE DESIGN AND CONSIDERATION FOR
    SAE AIR 4766/2 : 2011 AIRBORNE CHEMICALS IN AIRCRAFT CABINS
    SAE AIR 4766 : 2012 AIR QUALITY FOR COMMERCIAL AIRCRAFT CABINS
    FAA AC 33.27-1 : 2011 ENGINE AND TURBOSUPERCHARGER ROTOR OVERSPEED REQUIREMENTS OF 14 CFR SECTION 33.27
    FAA AC 33.15-1 : 0 MANUFACTURING PROCESS OF PREMIUM QUALITY TITANIUM ALLOY ROTATING ENGINE COMPONENTS
    FAA AC 33.4-2 : 0 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS: IN-SERVICE INSPECTION OF SAFETY CRITICAL TURBINE ENGINE PARTS AT PIECE-PART OPPORTUNITY
    FAA AC 20-147 : 2014 TURBOJET, TURBOPROP, TURBOSHAFT, AND TURBOFAN ENGINE INDUCTION SYSTEM ICING AND ICE INGESTION

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

    MIL E 5007 : D ENGINE, AIRCRAFT, TURBOJET AND TURBOFAN, GENERAL SPECIFICATION FOR
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