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  • SAE AS 18802 : 2013

    Current The latest, up-to-date edition.
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    FUEL AND OIL LINES, AIRCRAFT, INSTALLATION OF

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  09-08-2013

    Publisher:  SAE International

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

    1. SCOPE
    2. APPLICABLE DOCUMENTS
    3. REQUIREMENTS
    4. QUALITY ASSURANCE PROVISIONS
    5. PREPARATION FOR DELIVERY
    6. NOTES

    Abstract - (Show below) - (Hide below)

    Covers the requirements for installation of fuel and oil lines in aircraft, except those lines furnished as part of the engine.

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

    Committee AE-5
    Document Type Standard
    Publisher SAE International
    Status Current
    Supersedes

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

    DEFSTAN 00-970(PT0)/9(2012) : 2012 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/17(2016) : 2016 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/7(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/14(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/11(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/13(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/15(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/12(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/8(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/16(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/10(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    JSSG-2009 Revision A:2013 AIR VEHICLE SUBSYSTEMS (JOINT SERVICE SPECIFICATION GUIDE)

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

    MIL-T-8606 Revision C:1973 TUBING, STEEL, CORROSION RESISTANT (18-8 STABILIZED AND EXTRA LOW CARBON)
    MS33786 Revision B:2013 FITTING, INSTALLATION, FLARED TUBE AND HOSE, SWIVEL
    MIL T 5578 : C TANK, FUEL, AIRCRAFT, SELF-SEALING
    MIL-F-18280 Revision F:1995 FITTING, FLARELESS TUBE, FLUID CONNECTION
    MIL H 25579 : E HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR
    MIL H 8794 : D HOSE, RUBBER, HYDRAULIC, FUEL AND OIL RESISTANT
    MS33515 Revision J:1973 FITTING END, STANDARD DIMENSIONS FOR BULKHEAD FLARELESS TUBE CONNECTIONS
    AND10104 : REV 5 TUBING, STEEL, CORROSION RESISTANT, ROUND, STANDARD DIMENSIONS FOR
    MS21919 Revision E:1981 CLAMP, LOOP TYPE, CUSHIONED, SUPPORT
    MS33656 Revision J:1987 FITTING END, STANDARD DIMENSIONS FOR FLARED TUBE CONNECTION AND GASKET SEAL
    MIL T 6396 : E TANKS, AIRCRAFT PROPULSION FLUID SYSTEM, INTERNAL REMOVABLE, NON-SELF-SEALING
    MS33583 Revision C:1993 TUBING END, DOUBLE FLARE, STANDARD DIMENSIONS FOR
    MIL-STD-143 Revision B:1969 STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF
    MS33584 Revision C:1990 TUBING END, STANDARD DIMENSIONS FOR FLARED
    MS33611 Revision A:1983 TUBE BEND RADII
    MIL H 8795 : D HOSE ASSEMBLY, RUBBER HYDRAULIC, FUEL AND OIL RESISTANT
    MIL T 5579 : 0 TANK, SELF-SEALING OIL, AIRCRAFT
    AND10064 : LATEST FITTINGS - INSTALLATION OF FLARED TUBE, STRAIGHT THREADED CONNECTORS
    MS33514 Revision G:1990 FITTING END, STANDARD DIMENSIONS FOR FLARELESS TUBE CONNECTION AND GASKET SEAL (ASG)
    MIL-B-5087 Revision B:1964 BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS
    MS28741 Revision K:2010 HOSE ASSEMBLY, DETACHABLE END FITTING, MEDIUM PRESSURE
    MIL C 22263 : B COUPLING FUEL LINE, FLEXIBLE, 125 PSI, GENERAL SPECIFICATION FOR
    MIL-S-7742 Revision D:1991 SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES, GENERAL SPECIFICATION FOR
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