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  • SAE AS 8181 : 1997

    View superseded by
    Withdrawn A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
    View superseded by

    DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS, GENERAL SPECIFICATION FOR

    Available format(s):  Hardcopy, PDF

    Withdrawn date:  01-06-2002

    Language(s):  English

    Published date:  01-01-1997

    Publisher:  SAE International

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

    Foreword
    1 Scope
    2 Applicable documents
    3 Quality assurance provisions
    4 Preparation for delivery
    6 Notes

    Abstract - (Show below) - (Hide below)

    Defines requirements for ice detectors.

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

    Committee G-12
    Development Note Supersedes MIL D 8181 (B). (09/2004)
    Document Type Standard
    Publisher SAE International
    Status Withdrawn
    Superseded By
    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)/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)/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)/10(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS

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

    MS33540 Revision J:1986 SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR
    MIL L 7808 : K (1) LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE
    MIL-STD-129 Revision R:2014 Military Marking for Shipment and Storage
    MIL-STD-704 Revision F:2004 AIRCRAFT ELECTRIC POWER CHARACTERISTICS
    MIL-STD-130 Revision N:2007 IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY
    MIL P 8585 : LATEST PRIMER COATING, ZINC CHROMATE, LOW-MOISTURE SENSITIVITY
    MIL-D-6055 Revision D:1987 DRUM, METAL REUSABLE, SHIPPING AND STORAGE [CAP FROM 88 TO 510 CUBIC INCHES]
    MIL-D-70327 Base Document:1959 DRAWINGS, ENGINEERING AND ASSOCIATED LISTS
    MS33678 Revision A:2004 CONNECTOR, RECEPTACLE, ELECTRICAL, INTEGRAL MOUNTING
    MIL E 5400 : T ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR
    MIL-STD-831 Base Document:1963 TEST REPORTS, PREPARATION OF
    MS33588 Revision E:1984 NUTS, SELF LOCKING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY USAGE REQUIREMENTS FOR
    MS20995 Revision E:1974 WIRE, SAFETY OR LOCK
    MIL P 7936 : LATEST PARTS AND EQUIPMENT, AERONAUTICAL, PREPARATION FOR DELIVERY
    MIL-STD-143 Revision B:1969 STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF
    MIL E 5557 : LATEST
    MIL A 8625 : F ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS
    MIL-P-116 Revision J:1988 PRESERVATION, METHODS OF
    MIL C 5015 : G CONNECTOR, ELECTRICAL, CIRCULAR THREADED AN TYPE, GENERAL SPECIFICATION FOR
    MIL-STD-202 Revision H:2015 ELECTRONIC AND ELECTRICAL COMPONENT PARTS
    QQ-P-416 Revision F:1991 PLATING, CADMIUM (ELECTRODEPOSITED)
    MIL S 6743 : LATEST SWITCHES, PUSHBUTTON AND LIMIT
    MIL-B-5087 Revision B:1964 BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS
    MIL-S-7742 Revision D:1991 SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES, GENERAL SPECIFICATION FOR
    MIL N 25027 : G NUT, SELF-LOCKING, 250 DEGREES F, 450 DEGREES F, AND 800 DEGREES F
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