|
MIL T 5842 : B
|
TRANSPARENT AREAS ON AIRCRAFT SURFACES [WINDSHIELDS AND CANOPIES] RAIN REMOVING AND WASHING SYSTEMS FOR, DEFROSTING, DEICING, DEFOGGING, GENERAL SPECIFICATION FOR |
|
MIL M 8555 : C
|
MISSILE, GUIDED, DESIGN AND CONSTRUCTION, GENERAL SPECIFICATION |
|
MIL-PRF-85676 Revision A:2006
|
LIGHTING, EMERGENCY EGRESS, SUBASSEMBLY |
|
MIL A 85055 : 0
|
AVIONICS SYSTEM PERFORMANCE SPECIFICATION FOR A-4M/AV-8 BOMBING SET, ANGLE RATE AN/ASB-19(V) |
|
MIL L 50794 : 0
|
LINEAR SHAPED CHARGE ASSEMBLY |
|
MIL DTL 32151 : A
|
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 : D
|
INDICATOR, OIL QUANTITY, CONTINUOUS TRANSMISSION, NUCLEONIC |
|
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)/11(2013) : 2013
|
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)/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 |
|
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 |
|
MIL R 85880 : 0
|
ROCKET, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
|
MIL L 21910 : NOTICE 1
|
LAUNCHER, ROCKET LAU-10/A |
|
MIL STD 2156 : 0
|
LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
|
MIL E 50796 : 0
|
EXPANDING SHIELDED MILD DETONATING CORD ASSEMBLY |
|
MIL M 25047 : C
|
MARKINGS AND EXTERIOR FINISH COLORS FOR AIRPLANES, AIRPLANE PARTS, AND MISSILES (BALLISTIC MISSILES EXCLUDED) |
|
MIL V 7899 : C
|
VALVE, CHECK, AIRCRAFT FUEL SYSTEM |
|
MIL S 83427 : 0
|
SURVIVAL KIT CONTAINERS, CNU-129(V)/P AND CNU-130/P |
|
MIL-STD-2131 Revision A:1991
|
LAUNCHER, EJECTION GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
|
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 ARP 94910 : 2012
|
AEROSPACE - VEHICLE MANAGEMENT SYSTEMS - FLIGHT CONTROL DESIGN, INSTALLATION AND TEST OF, MILITARY UNMANNED AIRCRAFT, SPECIFICATION GUIDE FOR |
|
SAE AS 94900 : 2007
|
AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL-PRF-81975 Revision C:2008
|
COUPLINGS, REGULATED, AERIAL PRESSURE REFUELING TYPE MA-2, TYPE MA-3 AND TYPE MA-4 |
|
AFGS 87266 : 0
|
AIRCRAFT COCKPIT TRANSPARENCY SYSTEM |
|
MIL E 87236 : 0
|
|
|
MIL A 85116 : 0
|
ACTUATOR, PISTON, MINIATURE |
|
MIL S 81551 : 0
|
SWITCH, TOGGLE, HERMETICALLY SEALED, GENERAL SPECIFICATION FOR |
|
MIL S 85510 : 0
|
|
|
MIL-DTL-7899 Revision D:2014
|
VALVES, CHECK, AIRCRAFT FUEL SYSTEM |
|
SAE ARP 4729 : 2017
|
DOCUMENT FOR 270 VOLTAGE DIRECT CURRENT (270 V DC) SYSTEM |
|
MIL DTL 32188 : 0
|
INITIATOR, MECHANICAL ACTUATED JAU-25/A |
|
MIL C 85518 : 0
|
COMPUTER SET, STANDARD AIRBORNE AN/AYK-14(V) GENERAL SPECIFICATION FOR |
|
MIL F 85596 : 0
|
FIN, RETARDER, AIR INFLATABLE BSU-85/B |
|
MIL C 85629 : A (1)
|
CONTROL MONITOR SET GUIDED WEAPON, AN/AWW-13 |
|
MIL DTL 82889 : A
|
DETONATING CORD ASSEMBLY (DCA) |
|
MIL I 8673 : 0
|
INSTALLATION AND TEST OF AIRCRAFT FLEXIBLE WEAPONS SYSTEMS |
|
MIL-R-7705 Revision B:1975
|
RADOME, GENERAL SPECIFICATION FOR |
|
MIL DTL 32193 : 0
|
INITIATOR, EXPLOSIVE ACTUATED, JAU-29/A |
|
SAE ARP 1616 : 2017
|
SELF-SEALING BREAKAWAY VALVES FOR CRASH-RESISTANT AIRCRAFT FUEL AND OIL SYSTEMS |
|
SAE ARP 4058 : 2017
|
GENERAL SPECIFICATION GUIDE FOR MECHANICAL GEARED ROTARY ACTUATORS |
|
SAE AS 1297 : 2008(S2014)
|
REDUCERS, PNEUMATIC PRESSURE, MISSILE |
|
MIL PRF 57267 : 0
|
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 : 0
|
IGNITER, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
|
MIL A 25896 : E
|
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 : A
|
EXPLOSIVE SEQUENCE CONTROL |
|
MIL DTL 32154 : A
|
CORD ASSEMBLY, DETONATING, SHIELDED MILD |
|
MIL S 81771 : A
|
SEAT SYSTEM; AIRCREW, CRASH RESISTANT; GENERAL SPECIFICATION FOR |
|
SAE AS 4073 : 2013(R2018)
|
AIR CYCLE AIR CONDITIONING SYSTEMS FOR MILITARY AIR VEHICLES |
|
MIL DTL 32194 : B
|
IMPULSE CARTRIDGE, CCU-72/A |
|
MIL T 18232 : B
|
TARGET, AERIAL, POWERED, DESIGN AND CONSTRUCTION OF GENERAL SPECIFICATION FOR |
|
JSSG 2010 12 : 0
|
CREW SYSTEMS DEPLOYABLE AERODYNAMIC DECELERATOR (DAD) SYSTEMS HANDBOOK |
|
SAE ARP 5812 : 2017
|
ACTUATORS, LINEAR MECHANICAL, GENERAL SPECIFICATION GUIDE |
|
MIL S 48405 : 0
|
SHIELDED AND CONFINED MILD DETONATING CORD ASSEMBLIES |
|
MIL S 38399 : A
|
STARTER, PNEUMATIC, AIRCRAFT ENGINE GENERAL SPECIFICATION FOR |
|
MIL W 81752 : A
|
WINDSHIELDED SYSTEM, FIXED WING AIRCRAFT - GENERAL SPECIFICATION FOR |
|
MIL C 87970 : 0
|
CONTROL SET, GYROSCOPE, ATTITUDE HEADING AN/ASN-129 |
|
MIL M 4803 : D
|
MOTOR-GENERATOR, 400 HZ PRECISE OUTPUT, GENERAL REQUIREMENTS FOR |
|
MIL N 25161 : C
|
NOZZLE, AERIAL PRESSURE REFUELING, TYPE MA-2 |
|
EIA 836 CD : B2010(R2015)
|
CONFIGURATION MANAGEMENT DATA EXCHANGE AND INTEROPERABILITY |
|
MIL DTL 32045 : 2000
|
CARTRIDGE SET, REDUCED CHARGE PRIMARY |
|
MIL B 25820 : B
|
BOMB, LOADING PRACTICE BDU-6/E AND BDU-35/E |
|
MIL-W-5013 Revision L:1991
|
WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL T 81821 : 0
|
TRAINERS, MAINTENANCE, EQUIPMENT AND SERVICES GENERAL SPECIFICATION FOR |