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  • MIL-A-8591 Revision H:1990

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    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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    AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE); GENERAL DESIGN CRITERIA FOR

    Available format(s):  PDF

    Superseded date:  12-12-2005

    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. PACKAGING
    6. NOTES

    Abstract - (Show below) - (Hide below)

    Describes structural and mechanical design criteria to which airborne stores, suspension equipment and associated interfaces shall be designed.

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

    Committee FSC 15GP
    Development Note H NOTICE 1 - Notice of Cancellation/Superseded by MIL STD 8591 (12/2005)
    Document Type Standard
    Publisher US Military Specs/Standards/Handbooks
    Status Superseded
    Superseded By

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

    MIL-M-8856 Revision B:1990 MISSILE, GUIDED, STRUCTURAL INTEGRITY, GENERAL SPECIFICATION FOR
    MIL-STD-2156 Base Document:1983 LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR
    DEFSTAN 00-970(PT13)/5(2012) : 2012 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT
    MIL-M-8555 Revision C:1984 MISSILE, GUIDED, DESIGN AND CONSTRUCTION, GENERAL SPECIFICATION
    DEFSTAN 00-970(PT13)/12(2016) : 2016 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT
    DEFSTAN 00-970(PT13)/8(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT
    MIL-A-22847 Base Document:1961 AIR REFUELING STORE SYSTEM; D-704
    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)/11(2013) : 2013 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
    MIL L 21910 : NOTICE 1 LAUNCHER, ROCKET LAU-10/A
    DEFSTAN 00-69(PT2)/1(1998) : 1998 AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM - PART 2: DESIGN PRINCIPLES AND PRACTICES FOR, AND GUIDE TO, THE IMPLEMENTATION OF THE AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM
    MIL-HDBK-244 Revision A:1990 GUIDE TO AIRCRAFT - STORES COMPATIBILITY
    MIL-A-19736 Revision A:1960 AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR
    MIL STD 1763 : A AIRCRAFT STORES CERTIFICATION PROCEDURES
    MIL-T-85230 Revision A:1992 TARGET, TOW, AERIAL, TDU-34/A
    DEFSTAN 05-73/1(1986) : 1986 DESIGN OF AIRCRAFT STORES FOR FIXED WING AIRCRAFT AND HELICOPTERS
    DEFSTAN 00-970(PT1)SEC9/5(2007) : 2007 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 9: MILITARY SPECIFIC SYSTEMS
    SAE AS 4764 : 2017 VALIDATION METHODS FOR MIL-STD-1760 AIRCRAFT STATION INTERFACES
    MIL-STD-2131 Revision A:1991 LAUNCHER, EJECTION GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR
    DEFSTAN 07-85(PT1)/3(2006) : 2006 DESIGN REQUIREMENTS FOR WEAPONS AND ASSOCIATED SYSTEMS - PART 1: MANDATORY DESIGN REQUIREMENTS
    MIL-HDBK-1760 Revision A:2004 AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM
    MIL-W-81560 Base Document:1967 WEAPON, BIOLOGICAL AND CHEMICAL GENERAL DESIGN SPECIFICATION FOR
    MIL-F-85596 Base Document:1983 FIN, RETARDER, AIR INFLATABLE BSU-85/B
    MIL-D-23222 Revision A:1971 DEMONSTRATION REQUIREMENTS FOR HELICOPTERS
    MIL C 85629 : A (1) CONTROL MONITOR SET GUIDED WEAPON, AN/AWW-13
    MIL-T-18232 Revision B:1968 TARGET, AERIAL, POWERED, DESIGN AND CONSTRUCTION OF GENERAL SPECIFICATION FOR
    MIL-HDBK-1763 Base Document:1998 AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES
    DEFSTAN 00-970(PT13)/7(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT
    SAE AS 47641 : 2017 VALIDATION METHODS FOR MIL-STD-1760B AIRCRAFT STATION INTERFACES
    DEFSTAN 10-21/1(1976) : 1976 AMD 2 AIRCRAFT EJECTOR RELEASE UNITS FOR CONVENTIONAL MUNITIONS
    DEFSTAN 00-970(PT1)SEC9/4(2006) : 2006 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT A/C - SECTION 9: MILITARY SPECIFIC SYSTEMS
    STANAG 7081 : 0 STANDARD RAIL FOR LAUNCH OF 0-68 KILOGRAM (0-150 POUND) MISSILES FROM HELICOPTERS
    DEFSTAN 00-970(PT13)/11(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT
    DEFSTAN 13-8/4(1978) : 1978 DIMENSIONAL REQUIREMENTS FOR AIRBORNE STORES, ASSOCIATED SUSPENSION AND RELEASE SYSTEMS AND ELECTRICAL CONTROL CONNECTIONS
    DEFSTAN 00-970(PT13)/6(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT
    DEFSTAN 00-970(PT13)/4(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT
    DEFSTAN 00-970(PT13)/9(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT
    MIL-B-38977 Base Document:1968 Bomb, Practice BDU-38/B
    MIL-I-8671 Revision D:1994 INSTALLATION OF DROPPABLE STORES AND ASSOCIATED RELEASE SYSTEMS
    DEFSTAN 00-970(PT13)/3(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT
    MIL T 8676 : 0 TESTING OF AIRCRAFT ROCKET LAUNCHERS
    MIL-STD-1289 Revision D:2003 AIRBORNE STORES GROUND FIT AND COMPATIBILITY, REQUIREMENTS
    MIL-T-18404 Base Document:1955 TORPEDOES, ENVIRONMENTAL REQUIREMENTS; GENERAL SPECIFICATION FOR
    SAE AS 4270 : 2017 VALIDATION METHODS FOR MIL-STD-1760 MISSION STORES
    DEFSTAN 10-20/1(1976) : 1976 SUSPENSION UNITS WITH RELEASE CAPABILITY FOR CONVENTIONAL MUNITIONS CARRIED ON HELICOPTERS
    MIL-S-81340 Revision B:1979 SIGNAL, UNDERWATER SOUND (SUS) MARK 84 AND MODS
    MIL F 38642 : A FIN ASSEMBLY, BOMB, MXU-469/B AND MXU-467/B
    MIL-D-8708 Revision C:1991 DEMONSTRATION REQUIREMENTS FOR AIRPLANES
    MIL-L-48063 Revision A:1973 LAUNCHER, ROCKET, LAU 68B/A SHIPPING ASSEMBLY
    MIL-C-85392 Base Document:1987 CONTROL MONITOR SET, GUIDED WEAPON, AN/AWW-7D, GENERAL SPECIFICATION FOR
    MIL-STD-1606 Revision A:1983 TECHNICAL INFORMATION REQUIREMENTS FOR AIR LAUNCHED GUIDED MISSILE PROPOSALS
    MIL B 38634 : LATEST BOMB, FIRE, BLU 32A B
    DEFSTAN 00-970(PT13)/10(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT
    MIL-C-85283 Revision B:1994 CONTROL MONITOR SET, GUIDED WEAPON, AN/AWW-9
    MIL-C-85373 Revision A:1987 CONTROL MONITOR SET, GUIDED WEAPON, AN/AWW 12A
    DEFSTAN 00-970(PT1)SEC9/6(2010) : 2010 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 9: MILITARY SPECIFIC SYSTEMS

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

    STANAG 3558 : 2002 LOCATION OF ELECTRICAL CONNECTORS FOR AIRCRAFT STORES
    MIL-STD-2088 Revision B:2007 BOMB RACK UNIT (BRU), SINGLE STORE, AIRCRAFT
    MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
    MIL-T-7743 Revision F:1993 TESTING, STORE SUSPENSION AND RELEASE EQUIPMENT, GENERAL SPECIFICATION FOR
    ANSI Y10.7 : 1954 LETTER SYMBOLS/AERONAUTICAL SCIENCES
    MS3314 Base Document:1967 LUG, SUSPENSION, (1000LB CLASS ) AIRBORNE EQUIPMENT
    MIL-A-8870 Revision C:1993 AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE
    MIL-STD-1760 Revision E:2007 AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM
    STANAG 3575 : 0 AIRCRAFT STORES EJECTOR RACKS
    STANAG 3726 : 1996 BAIL (PORTAL) LUGS FOR THE SUSPENSION OF AIRCRAFT STORES
    MIL-A-8868 Revision B:1987 AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS
    STANAG 3441 : 2007 DESIGN OF AIRCRAFT STORES
    MIL-M-8856 Revision B:1990 MISSILE, GUIDED, STRUCTURAL INTEGRITY, GENERAL SPECIFICATION FOR
    MIL-A-8860 Revision B:1987 AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR
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