MIL-I-8500 Revision D:1980
Current
Current
The latest, up-to-date edition.
INTERCHANGEABILITY AND REPLACEABILITY OF COMPONENT PARTS FOR AEROSPACE VEHICLES
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Important note : Users cannot be edited or removed once added to your Multi user PDF.Provides dimensional interchangeability and replaceability requirements for parts, subassemblies, assemblies, sets, units and installation provisions for aerospace vehicles. Coverage includes classification, applicable documents, working lists, forms, contents,responsibility for inspection, quality conformance inspection, control media, and interchangeability and replaceability.
| Committee |
FSC MISC
|
| DevelopmentNote |
D NOTICE 2 - Notice of Reinstatement. (10/2002)
|
| DocumentType |
Standard
|
| Pages |
27
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
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| MIL-M-8555 Revision C:1984 | MISSILE, GUIDED, DESIGN AND CONSTRUCTION, GENERAL SPECIFICATION |
| MIL-PRF-85676 Revision A:2006 | LIGHTING, EMERGENCY EGRESS, SUBASSEMBLY |
| MIL-A-85055 Base Document:1979 | Avionics System Performance Specification for A-4M/AV-8 Bombing Set, Angle Rate AN/ASB-19(V) |
| MIL-L-50794 Base Document:1973 | Linear Shaped Charge Assembly |
| MIL-DTL-32151 Revision A:2006 | IMPULSE CARTRIDGE, CCU-71/A |
| MIL-D-8684 Revision B:1959 | DATA AND TESTS, ENGINEERING, CONTACT REQUIREMENTS FOR AIR LAUNCHED GUIDED MISSILE SYSTEMS |
| MIL-I-38338 Revision D:1991 | INDICATOR, OIL QUANTITY, CONTINUOUS TRANSMISSION, NUCLEONIC |
| MIL-A-23121 Revision C:1970 | AIRCREW ENVIRONMENTAL, ESCAPE AND SURVIVAL COCKPIT CAPSULE SYSTEM, GENERAL SPECIFICATION FOR |
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| 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)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
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| 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 |
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| MIL-S-83427 Base Document:1974 | SURVIVAL KIT CONTAINERS, CNU-129(V)/P AND CNU-130/P |
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| MIL-D-8685 Revision B:1967 | DATA AND TESTS, ENGINEERING, CONTRACT REQUIREMENTS FOR GUIDED MISSILE TARGET SYSTEMS |
| DSCC 87065 : C#CAN | SWITCH (COAXIAL L-BAND) RF TRANSMISSION LINE (1P2T REMOTE) FAILSAFE |
| SAE ARP94910 | Aerospace - Vehicle Management Systems - Flight Control Design, Installation and Test of, Military Unmanned Aircraft, Specification Guide For |
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| AFGS-87266 Base Document:1992 | AIRCRAFT COCKPIT TRANSPARENCY SYSTEM |
| MIL-E-87236 Base Document:1985 | |
| MIL-A-85116 Base Document:1980 | Actuator, Piston, Miniature |
| MIL-S-81551 Base Document:1968 | SWITCH, TOGGLE, HERMETICALLY SEALED, GENERAL SPECIFICATION FOR |
| MIL-S-85510 Base Document:1981 | Seats, Helicopter Cabin, Crashworthy, General Specification for |
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| SAE ARP4729A | Document for 270 Voltage Direct Current (270 V DC) System |
| MIL-DTL-32188 Base Document:2005 | INITIATOR, MECHANICAL ACTUATED JAU-25/A |
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| MIL-F-85596 Base Document:1983 | FIN, RETARDER, AIR INFLATABLE BSU-85/B |
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| MIL-I-8673 Base Document:1955 | INSTALLATION AND TEST OF AIRCRAFT FLEXIBLE WEAPONS SYSTEMS |
| MIL-R-7705 Revision B:1975 | RADOME, GENERAL SPECIFICATION FOR |
| MIL-DTL-32193 Base Document:2005 | INITIATOR, EXPLOSIVE ACTUATED, JAU-29/A |
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| SAE ARP 4058 : 2017 | GENERAL SPECIFICATION GUIDE FOR MECHANICAL GEARED ROTARY ACTUATORS |
| SAE AS1297B | Reducers, Pneumatic Pressure, Missile |
| MIL-PRF-57267 Base Document:2017 | COUPLING, AERIAL PRESSURE REFUELING TYPE MA-5 |
| MIL-DTL-9490 Revision E:2008 | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-I-85889 Base Document:1988 | IGNITER, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
| MIL-A-25896 Revision E:1983 | ADAPTER, PRESSURE FUEL SERVICING, NOMINAL 2.5 INCH DIAMETER |
| MIL O 38338 : C (1) | OIL QUANTITY GAGING SYSTEM, CONTINUOUS TRANSISTORIZED NUCLEONIC, GENERAL SPECIFICATION FOR |
| MIL-DTL-32186 Revision A:2012 | EXPLOSIVE SEQUENCE CONTROL |
| MIL-DTL-32154 Revision A:2011 | CORD ASSEMBLY, DETONATING, SHIELDED MILD |
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| SAE AS4073A | Air Cycle Air Conditioning Systems for Military Air Vehicles |
| MIL-DTL-32194 Revision B:2009 | IMPULSE CARTRIDGE, CCU-72/A |
| MIL-T-18232 Revision B:1968 | TARGET, AERIAL, POWERED, DESIGN AND CONSTRUCTION OF GENERAL SPECIFICATION FOR |
| JSSG-2010-12 Base Document:1998 | Crew Systems Deployable Aerodynamic Decelerator (DAD) Systems Handbook |
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| MIL-W-81752 Revision A:1987 | WINDSHIELDED SYSTEM, FIXED WING AIRCRAFT - GENERAL SPECIFICATION FOR |
| MIL-C-87970 Base Document:1982 | CONTROL SET, GYROSCOPE, ATTITUDE HEADING AN/ASN-129 |
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| MIL-DTL-32045 Base Document:2000 | CARTRIDGE SET, REDUCED CHARGE PRIMARY |
| MIL-B-25820 Revision B:1967 | BOMB, LOADING PRACTICE BDU-6/E AND BDU-35/E |
| MIL-W-5013 Revision L:1991 | WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR |
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| ASME Y14.100 : 2017 | ENGINEERING DRAWING PRACTICES - ENGINEERING DRAWING AND RELATED DOCUMENTATION PRACTICES |
| MIL-STD-280 Revision A:1969 | DEFINITIONS OF ITEM LEVELS, ITEM EXCHANGEABILITY, MODELS, AND RELATED TERMS |
| MIL-STD-480 Revision B:1988 | CONFIGURATION CONTROL - ENGINEERING CHANGES, DEVIATIONS AND WAIVERS |
| DOD-D-1000 Revision B:1977 | DRAWINGS, ENGINEERING AND ASSOCIATED LISTS |
| MIL-Q-9858 Revision A:1963 | QUALITY PROGRAM REQUIREMENTS |
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