MIL-A-8591 Revision H:1990
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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Superseded date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
Superseded by
Publisher
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PACKAGING
6. NOTES
Describes structural and mechanical design criteria to which airborne stores, suspension equipment and associated interfaces shall be designed.
| Committee |
FSC 15GP
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| DevelopmentNote |
H NOTICE 1 - Notice of Cancellation/Superseded by MIL STD 8591 (12/2005)
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| DocumentType |
Standard
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| Pages |
87
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Superseded
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| SupersededBy |
| 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 AS4764A | 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 AS47641A | 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 AS4270A | 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 |
| 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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