MIL-R-85895 Base Document:1988
|
RACK, BOMB EJECTOR, AIRCRAFT BRU-32/A |
MIL A 85670 : 0
|
ANTENNA, BROADBAND AS-3191/A, AS-3792/A, AND AS -3793/A |
AFGS-87213 Revision B:1993
|
DISPLAYS, AIRBORNE, ELECTRONICALLY/OPTICALLY GENERATED |
MIL-A-6271 Revision C:1976
|
ANTENNA, SUBSYSTEM FOR VHF AIRBORNE COMMUNICATION EQUIPMENT GENERAL SPECIFICATION FOR |
MIL-HDBK-253 Base Document:1978
|
GUIDANCE FOR THE DESIGN AND TEST OF SYSTEMS PROTECTED AGAINST THE EFFECTS OF ELECTROMAGNETIC ENERGY |
MIL-R-29583 Base Document:1992
|
RADIO SET |
MIL-M-8555 Revision C:1984
|
MISSILE, GUIDED, DESIGN AND CONSTRUCTION, GENERAL SPECIFICATION |
MIL A 87136 : NOTICE 1
|
ANTENNAS, AIRBORNE GENERAL SPECIFICATION FOR |
MIL-I-83152 Revision B:1974
|
INDICATOR, INDICATED-AIRSPEED AVU-22/A (INDICATOR-TRANSDUCER) |
MIL-L-6503 Revision H:1975
|
LIGHTING EQUIPMENT, AIRCRAFT, GENERAL SPECIFICATION FOR INSTALLATION OF |
MIL-A-85055 Base Document:1979
|
AVIONICS SYSTEM PERFORMANCE SPECIFICATION FOR A-4M/AV-8 BOMBING SET, ANGLE RATE AN/ASB-19(V) |
MIL-STD-7080 Base Document:1994
|
SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT |
MIL-G-25597 Revision D:1973
|
GYROSCOPE, DISPLACEMENT, ROLL AND PITCH, TYPE MD-1 |
MIL A 85097/13 : NOTICE 1
|
AIRCREW ESCAPE PROPULSION SYSTEMS (AEPS), ROCKET MOTOR, CANOPY JETTISON, MARK 109 MOD O LOADED ASSEMBLY |
MIL-D-70789 Revision A:1992
|
DYNAMIC REFERENCE UNIT (DRU) |
SAE AIR 5128 : 2012
|
ELECTRICAL BONDING OF AIRCRAFT FUEL SYSTEMS |
MIL DTL 0085097/13 : B
|
AIRCREW ESCAPE PROPULSION SYSTEMS (AEPS) ROCKET MOTOR, CANOPY JETTISON, MARK 109 MOD 0 (LOADED ASSEMBLY) |
MIL D 87213 : 0
|
DISPLAYS/OPTICALLY GENERATED REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
DEFSTAN 00-970(PT0)/9(2012) : 2012
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL BULL 343 : A
|
DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
DEFSTAN 00-970(PT0)/7(2011) : 2011
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-A-81973 Base Document:1974
|
AIRCREW AUTOMATED ESCAPE SYSTEMS, TEST VEHICLES FOR GROUND TRACK PERFORMANCE TESTING, ROCKET AND/OR JET ENGINE PROPELLED; GENERAL SPECIFICATION FOR |
DEFSTAN 00-970(PT0)/14(2014) : 2014
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-W-5088 Revision L:1991
|
Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
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 |
MIL F 9490 : D
|
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
DEFSTAN 00-970(PT0)/10(2013) : 2013
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-R-81876 Revision B:1988
|
RECEIVER, TRANSMITTER RADIO SET AN/APX-100(V) |
MIL-H-25475 Revision B:1971
|
HYDRAULIC SYSTEM, MISSILE, DESIGN, INSTALLATION TESTS AND DATE REQUIREMENTS, GENERAL REQUIREMENTS FOR |
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-H-8891 Revision A:1978
|
HYDRAULIC SYSTEMS, MANNED FLIGHT VEHICLES TYPE 111 DESIGN, INSTALLATION AND DATA REQUIREMENTS FOR, GENERAL SPECIFICATION FOR |
MIL-HDBK-244 Revision A:1990
|
GUIDE TO AIRCRAFT - STORES COMPATIBILITY |
MIL R 23016 : A
|
RADIO SET AN/ARC-94 |
MIL A 28875 : 0
|
AMPLIFIER, RADIO FREQUENCY AND MICROWAVE, SOLID STATE, GENERAL SPECIFICATION FOR |
MIL-STD-2156 Base Document:1983
|
LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
MIL-H-5440 Revision H:1993
|
HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR |
MIL-A-19736 Revision A:1960
|
AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR |
MIL-W-8160 Revision D:1961
|
WIRING, GUIDED MISSILE, INSTALLATION OF, GENERAL SPECIFICATION FOR |
MIL-STD-877 Base Document:1968
|
ANTENNA SUBSYSTEMS, AIRBORNE, CRITERIA FOR DESIGN AND LOCATION OF |
MIL-I-85671 Base Document:1987
|
INDICATOR, FREQUENCY CHANNEL ID-2121A/ARC, ID-2229A/ARC AND ID-2303/ARC |
MIL-P-5994 Revision D:1972
|
PUMP, HYDRAULIC, ELECTRIC MOTOR DRIVEN, VARIABLE DELIVERY, GENERAL SPECIFICATION FOR |
MIL-T-63534 Base Document:1981
|
TURRET SUBSYSTEM, UNIVERSAL, (UTS) FOR ARMAMENT SUBSYSTEM, HELICOPTER, 20MM, M97E1 AND M97E2, TURRET CONTROL UNIT FOR |
MIL-STD-1541 Revision A:1987
|
ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS FOR SPACE SYSTEMS |
MIL P 52955 : A
|
POSITION & AZIMUTH DETERMINING SYSTEM (PADS), AN/USQ-70(U) |
MIL-E-7080 Revision B:1962
|
ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF |
MIL-P-83927 Revision B:1981
|
POWER SUPPLIES, GUIDED MISSILE LAUNCHERS, SINGLE TYPES PP-2401B/A PP-2401C/A PP-2401D/A, PP-4285/A, PP-4286/A, AND COMPOSITE TYPE PP-4506/A AND PS-1037 |
MIL-STD-2131 Revision A:1991
|
LAUNCHER, EJECTION GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
MIL-F-7179 Revision G:1993
|
FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM |
MIL C 15370 : F
|
COUPLERS, DIRECTIONAL GENERAL SPECIFICATION FOR |
SAE AS 8700 : 1999
|
INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
SAE AS 8181 : 1997
|
DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS, GENERAL SPECIFICATION FOR |
MIL-I-18802 Revision A:1962
|
INSTALLATION OF FUEL AND OIL LINES, AIRCRAFT |
SAE ARP 4729 : 2017
|
DOCUMENT FOR 270 VOLTAGE DIRECT CURRENT (270 V DC) SYSTEM |
MIL-HDBK-1760 Revision A:2004
|
AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
MIL-C-85518 Base Document:1984
|
COMPUTER SET, STANDARD AIRBORNE AN/AYK-14(V) GENERAL SPECIFICATION FOR |
SAE AS 18802 : 2013
|
FUEL AND OIL LINES, AIRCRAFT, INSTALLATION OF |
MIL C 85629 : A (1)
|
CONTROL MONITOR SET GUIDED WEAPON, AN/AWW-13 |
MIL-I-8673 Base Document:1955
|
INSTALLATION AND TEST OF AIRCRAFT FLEXIBLE WEAPONS SYSTEMS |
SAE AS 4764 : 2017
|
VALIDATION METHODS FOR MIL-STD-1760 AIRCRAFT STATION INTERFACES |
MIL-R-7705 Revision B:1975
|
RADOME, GENERAL SPECIFICATION FOR |
MIL I 18373 : B
|
INSTRUMENT AND NAVIGATION EQUIPMENT, AIRCRAFT, INSTALLATION OF |
NASA HDBK 4001 : 0
|
ELECTRICAL GROUNDING ARCHITECTURE FOR UNMANNED SPACECRAFT |
MIL-A-6224 Revision E:1976
|
ANTENNA SUBSYSTEM FOR UHF AIRBORNE COMMUNICATIONS EQUIPMENT, GENERAL SPECIFICATION FOR |
MIL-I-8700 Revision A:1970
|
INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-P-87210 Base Document:1984
|
PNEUMATIC POWER SYSTEMS, HIGH PRESSURE |
SAE ARP 1616 : 2017
|
SELF-SEALING BREAKAWAY VALVES FOR CRASH-RESISTANT AIRCRAFT FUEL AND OIL SYSTEMS |
MIL-F-8615 Revision D:1976
|
FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG] |
MIL-HDBK-272 Revision A:1993
|
NUCLEAR WEAPONS SYSTEMS, SAFETY DESIGN AND EVALUATION CRITERIA FOR |
JSSG-2006 Base Document:1998
|
JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
NASA MSFC SPEC 250 : 1963
|
PROTECTIVE FINISHES FOR SPACE VEHICLE STRUCTURES AND ASSOCIATED FLIGHT EQUIPMENT GENERAL SPECIFICATION FOR |
MIL P 17842 : NOTICE 1
|
POWER PLANT VIBRATION ISOLATOR, DESIGN AND INSTALLATION REQUIREMENTS |
NASA MSFC HDBK 670 : 1991
|
GENERAL ENVIRONMENTAL TEST GUIDELINES (GETG) FOR PROTOFLIGHT INSTRUMENTS AND EXPERIMENTS |
MIL-T-63520 Base Document:1981
|
TURRET SUBSYSTEM, UNIVERSAL (UTS) FOR ARMAMENT SUBSYSTEM, HELICOPTER, 20MM, M97E1 AND M97E2, GUN CONTROL ASSEMBLY FOR |
MIL-N-49098 Revision A:1990
|
NAVIGATIONAL SET, DOPPLER AN/ASN-128()(XE-2) |
MIL-D-8181 Revision B:1965
|
DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS GENERAL SPECIFICATION FOR |
MIL-A-25730 Revision C:1976
|
ANTENNA SUBSYSTEMS FOR AIRBORNE IDENTIFICATION AND NAVIGATION EQUIPMENT, GENERAL SPECIFICATION FOR |
MIL-I-8671 Revision D:1994
|
INSTALLATION OF DROPPABLE STORES AND ASSOCIATED RELEASE SYSTEMS |
ADS-13F-HDBK : 1997
|
AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES |
MIL-T-18232 Revision B:1968
|
TARGET, AERIAL, POWERED, DESIGN AND CONSTRUCTION OF GENERAL SPECIFICATION FOR |
MIL-T-63536 Base Document:1981
|
TURRET SUBSYSTEM, UNIVERSAL (UTS) FOR ARMAMENT SUBSYSTEM, HELICOPTER, 20MM, M97E1 AND M97E2, LOGIC CONTROL UNIT ASSEMBLY FOR |
SAE AS 4270 : 2017
|
VALIDATION METHODS FOR MIL-STD-1760 MISSION STORES |
SAE MA 2241 : 2015
|
COUPLING ASSEMBLY, THREADLESS, FLEXIBLE, FIXED CAVITY, SELF-BONDING, METRIC |
SAE AIR 4728 : 2013
|
REFERENCES, SPACECRAFT AND SPACECRAFT SERVICING, FLUID SYSTEM COMPONENTS (ABBREVIATIONS, ACRONYMS, DEFINITIONS, APPLICABLE DOCUMENTS AND ENVIRONMENTAL CONDITIONS) |
MIL-D-19326 Revision H:1990
|
DESIGN AND INSTALLATION OF LIQUID OXYGEN SYSTEMS IN AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-STD-1512 Base Document:1972
|
ELECTROEXPLOSIVE SUBSYSTEMS, ELECTRICALLY INITIATED, DESIGN REQUIREMENTS AND TEST METHODS |
DOD STD 1788 : LATEST
|
AVIONICS INTERFACE DESIGN STANDARD (METRIC) |
MIL-I-85112 Base Document:1978
|
INDICATOR SET, VERTICAL SCALE |
MIL-H-23799 Base Document:1963
|
HOSE ASSEMBLY, METAL, TRANSFER, LIQUID OXYGEN |
MIL A 83366 : 0
|
ANTENNA ASSEMBLIES, AIRBORNE, GENERAL SPECIFICATION FOR |
MIL-I-83456 Base Document:1974
|
INSTALLATION OF SEGMENTED LIGHTNING DIVERTER STRIPS ON AIRCRAFT RADOMES, GENERAL SPECIFICATION FOR |
MIL-A-85505 Base Document:1983
|
ALTIMETER, STANDBY, TYPES 1 AND 2 |
MIL-L-85762 Revision A:1988
|
LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION |
MIL-A-83212 Revision A:1976
|
ALTIMETER, PRESSURE AAU-27/A |
MIL-A-85672 Base Document:1987
|
AMPLIFIER, RADIO FREQUENCY AM-7177A/ARC |
MIL-W-18326 Revision A:1956
|
WELDING OF MAGNESIUM ALLOYS, GAS AND ARC, MANUAL AND MACHINE PROCESSES FOR |
MIL-D-8708 Revision C:1991
|
DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
SAE AS 47641 : 2017
|
VALIDATION METHODS FOR MIL-STD-1760B AIRCRAFT STATION INTERFACES |
MIL-C-87970 Base Document:1982
|
CONTROL SET, GYROSCOPE, ATTITUDE HEADING AN/ASN-129 |
MIL-E-6051 Revision D:1967
|
ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM |
MIL-STD-463 Revision A:1977
|
DEFINITION AND SYSTEM OF UNITS, ELECTROMAGNETIC INTERFERENCE TECHNOLOGY |
MIL-I-8672 Revision B:1969
|
INSTALLATION AND TEST OF AIRCRAFT PYROTECHNIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR [ASG] |
MIL-A-55368 Base Document:1972
|
AIRBORNE DATA ANNOTATION SYSTEM AN/AYA-10() |
MIL-C-81883 Base Document:1976
|
CONTROL GROUP, ELECTRIC POWER OK-XXX (V) A GENERAL SPECIFICATION FOR |
MIL-L-5667 Revision B:1964
|
LIGHTING EQUIPMENT, AIRCRAFT INSTRUMENT PANEL, GENERAL SPECIFICATION FOR INSTALLATION OF [ASG] |
MIL I 83361 : (4)
|
INDICATOR, PRESSURE OIL, DUAL EGU-18/A, 0-100 PSI |
MIL-P-85576 Revision B:1987
|
POWER SUPPLY PP-2581C/A |
SAE AIR 5774 : 2012
|
COMPOSITE FUEL TANKS, FUEL SYSTEM DESIGN CONSIDERATIONS |
SAE AS 5994A:2000(S2013)
|
PUMP UNITS, HYDRAULIC, ELECTRIC MOTOR DRIVEN, VARIABLE DELIVERY |