MIL-T-5842 Revision B:1985
|
TRANSPARENT AREAS ON AIRCRAFT SURFACES [WINDSHIELDS AND CANOPIES] RAIN REMOVING AND WASHING SYSTEMS FOR, DEFROSTING, DEICING, DEFOGGING, GENERAL SPECIFICATION FOR |
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 |
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 |
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 |
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 Base Document:1988
|
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 Base Document:1983
|
LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
MIL-E-50796 Base Document:1973
|
EXPANDING SHIELDED MILD DETONATING CORD ASSEMBLY |
MIL-M-25047 Revision C:1968
|
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 Base Document:1974
|
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 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
|
|
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 Base Document:2005
|
INITIATOR, MECHANICAL ACTUATED JAU-25/A |
MIL-C-85518 Base Document:1984
|
COMPUTER SET, STANDARD AIRBORNE AN/AYK-14(V) GENERAL SPECIFICATION FOR |
MIL-F-85596 Base Document:1983
|
FIN, RETARDER, AIR INFLATABLE BSU-85/B |
MIL C 85629 : A (1)
|
CONTROL MONITOR SET GUIDED WEAPON, AN/AWW-13 |
MIL-DTL-82889 Revision A:2004
|
DETONATING CORD ASSEMBLY (DCA) |
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 |
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 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 |
MIL-S-81771 Revision A:1975
|
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 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 |
SAE ARP 5812 : 2017
|
ACTUATORS, LINEAR MECHANICAL, GENERAL SPECIFICATION GUIDE |
MIL-S-48405 Base Document:1973
|
Shielded and Confined Mild Detonating Cord Assemblies |
MIL-S-38399 Revision A:1975
|
STARTER, PNEUMATIC, AIRCRAFT ENGINE GENERAL SPECIFICATION FOR |
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 |
MIL M 4803 : D
|
MOTOR-GENERATOR, 400 HZ PRECISE OUTPUT, GENERAL REQUIREMENTS FOR |
MIL-N-25161 Revision C:1969
|
NOZZLE, AERIAL PRESSURE REFUELING, TYPE MA-2 |
EIA 836 CD : B2010(R2015)
|
CONFIGURATION MANAGEMENT DATA EXCHANGE AND INTEROPERABILITY |
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 |
MIL-T-81821 Base Document:1969
|
TRAINERS, MAINTENANCE, EQUIPMENT AND SERVICES GENERAL SPECIFICATION FOR |
ASME Y14.100 : 2017
|
ENGINEERING DRAWING PRACTICES - ENGINEERING DRAWING AND RELATED DOCUMENTATION PRACTICES |