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  • MIL I 8700 : A

    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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    INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR

    Available format(s):  Hardcopy, PDF

    Superseded date:  23-08-1999

    Language(s): 

    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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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)

    Describes the requirements for the installation and test of electronic equipment in piloted aircraft.

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

    Committee FSC MISC
    Development Note A NOTICE 1 - Notice of Cancellation/Superseded by SAE AS 8700. (07/2005)
    Document Type Standard
    Publisher US Military Specs/Standards/Handbooks
    Status Superseded
    Superseded By

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

    DEFSTAN 00-970(PT1)SEC6/10(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    DEFSTAN 00-970(PT1)SEC6/9(2012) : 2012 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT
    DEFSTAN 00-970(PT1)SEC6/15(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    DEFSTAN 00-970(PT1)SEC6/13(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    DEFSTAN 00-970(PT1)SEC6/14(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    DEFSTAN 00-970(PT7)SEC7/1(2006) : 2006 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
    DEFSTAN 00-970(PT1)SEC6/12(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    DEFSTAN 00-970(PT7)SEC2/SUPP6/6(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 6: EQUIPMENT (SUBPART F)
    DEFSTAN 00-970(PT1)SEC6/4(2006) : 2006 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT A/C - SECTION 6: EQUIPMENT
    DEFSTAN 00-970(PT1)SEC6/11(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    DEFSTAN 00-970(PT7)SEC2/SUPP6/5(2015) : INTERIM DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 6: EQUIPMENT (SUBPART F)
    DEFSTAN 00-970(PT7)SEC7/2(2007) : 2007 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
    DEFSTAN 00-970(PT1)SEC6/8(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT
    DEFSTAN 00-970(PT7)SEC7/3(2010) : 2010 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
    DEFSTAN 00-970(PT1)SEC6/6(2010) : 2010 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    MIL D 23222 : A DEMONSTRATION REQUIREMENTS FOR HELICOPTERS
    MIL I 8673 : 0 INSTALLATION AND TEST OF AIRCRAFT FLEXIBLE WEAPONS SYSTEMS
    DEFSTAN 00-970(PT1)SEC6/7(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    DEFSTAN 00-970(PT1)SEC6/5(2007) : 2007 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 6: EQUIPMENT
    MIL F 23447 : 0 FIRE WARNING SYSTEMS, AIRCRAFT, RADIATION SENSING TYPE, TEST AND INSTALLATION OF
    DEFSTAN 00-970(PT1)SEC6/16(2016) : 2016 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    MIL-C-81774A:1973 CONTROL PANEL, AIRCRAFT, GENERAL REQUIREMENTS FOR
    MIL D 8708 : C DEMONSTRATION REQUIREMENTS FOR AIRPLANES

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

    MS 24435 : A POWER RECEPTACLE, AIRCRAFT, ELECTRONIC TEST EQUIPMENT, WIRING OF
    MIL STD 970 : 0 STANDARDS AND SPECIFICATIONS, ORDER OF PREFERENCE FOR THE SELECTION OF
    MIL STD 130 : N IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY
    MIL C 7762 : A COMPASS, INSTALLATION OF
    MIL R 7705 : B RADOME, GENERAL SPECIFICATION FOR
    MIL E 6051 : D ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM
    MIL P 7788 : F PANEL, INFORMATION INTEGRALLY ILLUMINATED
    MIL STD 889 : C DISSIMILAR METALS
    MIL E 5400 : T ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR
    MIL C 6781 : B CONTROL PANEL, AIRCRAFT EQUIPMENT, RACK OR CONSOLE MOUNTED
    MIL HDBK 216 : 0 RF TRANSMISSION LINES AND FITTINGS (NOTICE 10)
    MS 21047 : F NUT SELF LOCKING PLATE TWO LUG LOW HEIGHT STEEL 125 KSI FTU 450 DEG (ASG)
    MIL M 81288 : 0 MOUNTING BASES, FLEXIBLE PLASTIC FOAM
    MIL STD 882 : E STANDARD PRACTICE FOR SYSTEM SAFETY
    MIL F 15733 : G FILTERS & CAPACITORS, RADIO FREQUENCY INTERFERENCE
    MIL F 25173 : A FASTENER, CONTROL PANEL, AIRCRAFT EQUIPMENT
    MIL STD 100 : G ENGINEERING DRAWINGS
    MIL A 9094 : D ARRESTER, LIGHTNING, GENERAL SPECIFICATION FOR
    MIL C 172 : C CASES: BASES, MOUNTING & MOUNTS, VIBRATION (FOR USE WITH ELECTRONIC EQUIPMENT)
    MIL B 5087 : B BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS
    MIL W 5088 : L WIRING, AEROSPACE VEHICLE
    MIL HDBK 660 : B FABRICATION OF RIGID WAVEGUIDE ASSEMBLIES (SWEEP BENDS AND TWISTS)
    MS 21048 : F NUT SELF LOCKING PLATE TWO LUG LOW HEIGHT CRES 125 KSI FTU 450 DEG AND 800 DEG F
    MIL E 7080 : B ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF
    MIL N 7513 : F NOMENCLATURE ASSIGNMENT, CONTRACTORS METHOD FOR OBTAINING
    MIL F 7179 : G FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM
    MIL STD 877 : 0 ANTENNA SUBSYSTEMS, AIRBORNE, CRITERIA FOR DESIGN AND LOCATION OF
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