MIL-HDBK-244 Revision A:1990
Current
Current
The latest, up-to-date edition.
GUIDE TO AIRCRAFT - STORES COMPATIBILITY
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Important note : Users cannot be edited or removed once added to your Multi user PDF.Covers all aspects of aircraft and weapons compatibility; mechanical, electrical, structural, aerodynamic, etc.
| Committee |
FSC 15GP
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| DevelopmentNote |
A NOTICE 1 - Notice of Validation. (09/2014)
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| DocumentType |
Standard
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| Pages |
144
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| ProductNote |
NEW CHILD NOT 2 2019 IS NOW ADDED
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Current
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| 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)/17(2016) : 2016 | 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)/15(2015) : 2015 | 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)/13(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)/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 |
| DEFSTAN 00-970(PT0)/16(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| 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 STD 1763 : A | AIRCRAFT STORES CERTIFICATION PROCEDURES |
| MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
| MIL-HDBK-1760 Revision A:2004 | AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
| MIL-I-8671 Revision D:1994 | INSTALLATION OF DROPPABLE STORES AND ASSOCIATED RELEASE SYSTEMS |
| MIL-HDBK-1763 Base Document:1998 | AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES |
| MIL-A-8865 Revision B:1987 | AIRPLANE STRENGTH AND RIGIDITY MISCELLANEOUS LOADS |
| MIL-T-8679 Base Document:1954 | TEST REQUIREMENTS, GROUND HELICOPTER |
| STANAG 3558 : 2002 | LOCATION OF ELECTRICAL CONNECTORS FOR AIRCRAFT STORES |
| STANAG 3605 : 0 | COMPATIBILITY OF ARMING SYSTEMS AND EXPENDABLE AIRCRAFT STORES |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| MIL-F-8785 Revision C:1980 | FLYING QUALITIES OF PILOTED AIRPLANES |
| MIL-STD-2088 Revision B:2007 | BOMB RACK UNIT (BRU), SINGLE STORE, AIRCRAFT |
| STANAG 3791 : 1999 | INTEROPERABILITY OF NATO AIRCRAFT AND STORES - AOP-11 |
| MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
| MIL-A-8863 Revision C:1993 | AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES |
| STANAG 3837 : 0 | AIRCRAFT STORES ELECTRICAL INTERCONNECTION SYSTEM |
| MIL-STD-220 Revision C:2009 | Method of Insertion Loss Measurement |
| MIL-A-8591 Revision H:1990 | AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE); GENERAL DESIGN CRITERIA FOR |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL-A-8869 Revision B:1987 | AIRPLANE STRENGTH AND RIGIDITY NUCLEAR WEAPONS EFFECTS |
| DOD STD 1686 : 0 | ELECTROSTATIC DISCHARGE CONTROL PROGRAM FOR PROTECTION OF ELECTRICAL AND ELECTRONIC PARTS ASSEMBLIES AND EQUIPMENT (EXCLUDING ELECTRICALLY INITIATED EXPLOSIVE DEVICES)(METRIC) |
| STANAG 3525 : 0 | SAFETY DESIGN REQUIREMENTS - AIRBORNE FUZING SYSTEMS |
| MIL-E-6051 Revision D:1967 | ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM |
| MIL-A-8870 Revision C:1993 | AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE |
| MIL-STD-1316 Revision F:2017 | Fuze Design, Safety Criteria for |
| MIL-STD-1760 Revision E:2007 | AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
| MIL-I-8672 Revision B:1969 | INSTALLATION AND TEST OF AIRCRAFT PYROTECHNIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR [ASG] |
| STANAG 3898 : 2009 | AIRCRAFT STORES INTERFACE MANUAL (ASIM) - AOP-12 |
| MIL I 23659 : C | INITIATOR, ELECTRIC, GENERAL DESIGN SPECIFICATION |
| MIL-STD-1512 Base Document:1972 | ELECTROEXPLOSIVE SUBSYSTEMS, ELECTRICALLY INITIATED, DESIGN REQUIREMENTS AND TEST METHODS |
| MIL-I-8671 Revision D:1994 | INSTALLATION OF DROPPABLE STORES AND ASSOCIATED RELEASE SYSTEMS |
| MIL C 38999 : J | CONNECTOR, ELECTRICAL, CIRCULAR, MINIATURE, HIGH DENSITY, QUICK DISCONNECT (BAYONET THREADED & BREECH COUPLING) ENVIRONMENT RESISTANT, REMOVABLE CRIMP & HERMETIC SOLDER CONTACTS |
| DOD HDBK 263 : LATEST | ELECTROSTATIC DISCHARGE CONTROL HANDBOOK FOR PROTECTION OF ELECTRICAL AND ELECTRONIC PARTS, ASSEMBLIES AND EQUIPMENT (EXCLUDING ELECTRICALLY INITIATED EXPLOSIVE DEVICES)METRIC |
| STANAG 3575 : 0 | AIRCRAFT STORES EJECTOR RACKS |
| MIL-E-5007 Revision D:1973 | ENGINE, AIRCRAFT, TURBOJET AND TURBOFAN, GENERAL SPECIFICATION FOR |
| STANAG 3556 : 0 | AIRCRAFT STORE EJECTOR CARTRIDGES |
| MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
| MIL F 15733 : G | FILTERS & CAPACITORS, RADIO FREQUENCY INTERFERENCE |
| 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 |
| MIL-HDBK-235-1 Revision C:2010 | MILITARY OPERATIONAL ELECTROMAGNETIC ENVIRONMENT PROFILES - PART 1: GENERAL GUIDANCE |
| MIL STD 1763 : A | AIRCRAFT STORES CERTIFICATION PROCEDURES |
| MIL-A-8867 Revision C:1987 | AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS |
| MIL-D-81303 Revision A:1966 | DESIGN AND EVALUATION OF CARTRIDGES FOR STORES SUSPENSION EQUIPMENT |
| MIL-A-8861 Revision B:1986 | AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS |
| MIL-A-8866 Revision C:1987 | AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE |
| MIL-STD-1472 Revision G:2012 | HUMAN ENGINEERING |
| MIL-STD-1319 Revision A:1976 | ITEM CHARACTERISTICS AFFECTING TRANSPORTABILITY AND PACKAGING AND HANDLING EQUIPMENT DESIGN |
| STANAG 3899 : 0 | GROUND FIT AND COMPATIBILITY CRITERIA FOR AIRCRAFT STORES |
| MIL-D-8708 Revision C:1991 | DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
| MIL A 87221 : 0 | AIRCRAFT STRUCTURES, GENERAL SPECIFICATION FOR REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
| MIL-STD-462 Revision D:1993 | MEASUREMENT OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS |
| MIL-B-81006 Revision B:1968 | BOMB, FREE FALL, DEMONSTRATION OF DISPERSION REQUIREMENTS FOR |
| MIL-H-8501 Revision A:1961 | HELICOPTER FLYING AND GROUND HANDLING QUALITIES, GENERAL REQUIREMENTS FOR (AF USE MIL F 83300) |
| MIL-B-5087 Revision B:1964 | BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS |
| MIL-S-8698 Base Document:1954 | STRUCTURAL DESIGN REQUIREMENTS, HELICOPTERS [ASG] |
| MIL-STD-1289 Revision D:2003 | AIRBORNE STORES GROUND FIT AND COMPATIBILITY, REQUIREMENTS |
| STANAG 3842 : 2008 | RAIL LAUNCHED MISSILE/LAUNCHER MECHANICAL INTERFACE |
| 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 |
| MIL-STD-1553 Revision B:1978 | DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA |
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