|
15 MIL-C- 25200 |
CABLE ASSEMBLIES, SPECIAL WEAPONS, ELECTRICAL, GENERAL REQUIREMENTS FOR |
|
18 MIL-B- 38664 |
BOMB, FRAGMENTATION, BLU-63/B METAL PARTS FOR |
|
18 MIL-E- 9393 |
EXTERNAL STORE INSTALLATIONS, GENERAL DESIGN CRITERIA FOR |
|
18 MIL-HDBK- 1455 |
DISPENSER AND SUB-MUNITION, AIR DELIVERED, SAFETY DESIGN AND SAFETY QUALIFICATION CRITERIA FOR |
|
AIR FORCE A-A- 1895 |
TAPE, SOUND RECORDING, 1/4-INCH, GENERAL PURPOSE |
|
AIR FORCE A-A- 1896 |
TAPE, SOUND RECORDING, 1/4-INCH, MASTERING |
|
AIR FORCE A-A- 50653 |
MAINTENANCE STAND, SELF-PROPELLED, SCISSORS LIFT |
|
AIR FORCE A-A- 50742 |
AIRCRAFT MOVER, ELECTRICALLY POWERED |
|
AIR FORCE A-A- 50747 |
POUCH, AMMUNITION MAGAZINE, 9MM |
|
AIR FORCE A-A- 50748 |
HOLSTER, HIP, PISTOL, SEMI-AUTOMATIC 9MM |
|
AIR FORCE A-A- 50766 |
BUS, MOTOR, 16 PASSENGER |
|
AIR FORCE A-A- 58006 |
4-WHEEL DRIVEN, MULTI-PURPOSE TRACTOR |
|
AIR FORCE A-A- 58026 |
TRACTOR, AIRCRAFT TOWING, U-30 |
|
AIR FORCE A-A- 58036 |
STAIRCASE, AIRCRAFT BOARDING |
|
AIR FORCE A-A- 58045 |
TRACTOR, AIRCRAFT TOWING, MB-2 |
|
AIR FORCE A-A- 58091 |
TRAILER, TANK MOUNTED, RECOVERABLE AVIATION TURBINE FUEL (BOWSERS): 200, 400, AND 600 GALLON CAPACITY |
|
AIR FORCE A-A- 59103 |
TRUCK, TANK A/S32A-24, POTABLE WATER |
|
AIR FORCE A-A- 59111 |
SERVICING/DEICING MAINTENANCE PLATFORM, HIGH REACH, TRUCK MOUNTED |
|
AIR FORCE A-A- 59145 |
SPRAYING UNIT, DEICING, TRUCK MOUNTED |
|
AIR FORCE A-A- 59196 |
TRUCK, AIRCRAFT SERVICING (AST), 3 TON HIGH LIFT, FOR LOADING C-5 AIRCRAFT UPPER DECK |
|
AIR FORCE A-A- 59210 |
TRACTOR, AIRCRAFT TOWING, MB-4 |
|
AIR FORCE A-A- 59259 |
TRUCK, AIRCRAFT REFUELING, HYDRANT |
|
AIR FORCE A-A- 59312 |
TRACTOR, AIRCRAFT TOWING, FLIGHT LINE |
|
AIR FORCE A-A- 59417 |
THERMAL IMAGING SYSTEM |
|
AIR FORCE A-A- 59576 |
TOW BAR, FOR AIRCRAFT TOWING (KC-10 AIRCRAFT) |
|
AIR FORCE A-A- 59687 |
ROBOT, EXPLOSIVE ORDNANCE DISPOSAL (EOD) |
|
AIR FORCE A-A- 59716 |
STAIRCASE, AIRCRAFT BOARDING-CHASSIS MOUNTED, MOTORIZED (MSTA) |
|
AIR FORCE A-A- 59768 |
PALLET, CARGO, INTERMODAL, ASSOCIATE |
|
AIR FORCE AN6009 |
COUPLING-AUTOMATIC OXYGEN |
|
AIR FORCE AN6044 |
ADAPTER-PORTABLE OXYGEN RECHARGER ORIFICE |
|
AIR FORCE AN6200 |
VALVE, HYDRAULIC PRESSURE RELIEF, CLASS AB |
|
AIR FORCE AN6295 |
REGULATOR-10 GPM HYDRAULIC PRESSURE |
|
AIR FORCE AN6506 |
BELT ASSEMBLY - TROOP AND TURRET GUNNER'S SAFETY |
|
AIR FORCE AN6516 |
SNAP-COILED SPRING TYPE PARACHUTE |
|
AIR FORCE AN8020 |
BRACKET-FLYERS RELIEF TUBE HORIZONTAL |
|
AIR FORCE AN8031 |
PAD - TANK STRAP |
|
AIR FORCE AND10573 |
RIM CONTOURS 26 X 6.6, 30 X 7.7, 32 X 8.8, 34 X 9.9, 36 X 11, 38 X 11, 40 X 12 AND 44 X 13, TYPE VII, EXTRA HIGH PRESSURE, MAIN LAINDING GEAR WHEELS |
|
AIR FORCE AND10576 |
RIM CONTOURS 24 X 7.7, TYPE VII EXTRA HIGH PRESSURE, MAIN LANDING GEAR WHEEL |
|
AIR FORCE AND10578 |
RIM CONTOURS 5.00-5, TYPE III LOW PRESSURE, HELICOPTER LANDING GEAR WHEEL |
|
AIR FORCE AND10581 |
RIM CONTOURS 20 X 4.4, TYPE VII EXTRA HIGH PRESSURE, LANDING GEAR WHEEL |
|
AIR FORCE AND10583 |
RIM CONTOURS 25.00-28, TYPE III LOW PRESSURE, MAIN LANDING GEAR |
|
AIR FORCE DOD-E- 83578 |
EXPLOSIVE ORDNANCE FOR SPACE VEHICLES, GENERAL SPECIFICATION FOR (METRIC) |
|
AIR FORCE DOD-HDBK- 343 |
DESIGN, CONSTRUCTION, AND TESTING REQUIREMENTS FOR ONE OF A KIND SPACE EQUIPMENT |
|
AIR FORCE DOD-STD- 1578 |
NICKEL-CADMIUM BATTERY USAGE PRACTICES FOR SPACE VEHICLES |
|
AIR FORCE DOD-W- 83575 |
WIRING HARNESS, SPACE VEHICLE, DESIGN AND TESTING, GENERAL SPECIFICATION FOR |
|
AIR FORCE JSSG- 2000 |
AIR SYSTEM |
|
AIR FORCE JSSG- 2007 |
ENGINES, AIRCRAFT, TURBINE |
|
AIR FORCE JSSG- 2009 |
AIR VEHICLES SUBSYSTEMS |
|
AIR FORCE JSSG-2010- 10 |
CREW SYSTEMS OXYGEN SYSTEMS HANDBOOK |
|
AIR FORCE JSSG-2010- 12 |
CREW SYSTEMS DEPLOYABLE AERODYNAMIC DECELERATOR (DAD) SYSTEMS HANDBOOK |
|
AIR FORCE JSSG-2010- 5 |
CREW SYSTEMS AIRCRAFT LIGHTING HANDBOOK |
|
AIR FORCE JSSG-2010- 7 |
CREW SYSTEMS CRASH PROTECTION HANDBOOK |
|
AIR FORCE MIL-A- 25165 |
AIRCRAFT EMERGENCY ESCAPE SYSTEM, IDENTIFICATION OF |
|
AIR FORCE MIL-A- 25367 |
ANTENNA AT-536/ARN |
|
AIR FORCE MIL-A- 27038 |
ADAPTER KIT, WEAPON TO SUPPORT ADU-92/A |
|
AIR FORCE MIL-A- 27039 |
ADAPTER KIT, WEAPON TO SUPPORT ADU-103/C |
|
AIR FORCE MIL-A- 27071 |
AMPLIFIER-LOUDSPEAKER AM-2639/U |
|
AIR FORCE MIL-A- 27130 |
AMPLIFIER-POWER SUPPLY GROUP AN/GRA-62( ) |
|
AIR FORCE MIL-A- 27143 |
AMPLIFIER-POWER SUPPLY GROUP AN/TKA-3( ) |
|
AIR FORCE MIL-A- 38156 |
ALTIMETER SET, ELECTRONIC AN-APN-150(V) |
|
AIR FORCE MIL-A- 38202 |
AIRCRAFT ARRESTING SYSTEM BAK-12A/E32A; PORTABLE, ROTARY FRICTION |
|
AIR FORCE MIL-A- 38630 |
ADAPTER CLUSTER BOMB, ADU-253A/B LOADING, ASSEMBLING AND PACKING |
|
AIR FORCE MIL-A- 5498 |
ACCUMULATORS, HYDRAULIC, CYLINDRICAL 3000 PSI, AIRCRAFT |
|
AIR FORCE MIL-A- 5731 |
ADAPTER KIT MX-479-ARN-6 |
|
AIR FORCE MIL-A- 5999 |
ANTENNA SUBSYSTEM FOR AIRCRAFT MARKER BEACON EQUIPMENT GENERAL SPECIFICATION FOR |
|
AIR FORCE MIL-A- 6348 |
AMPLIFIER AM-203C/ARA-19 |
|
AIR FORCE MIL-A- 6824 |
ADAPTER, AMMUNITION CHUTE, BOX END, 20 MM. TYPE L-4 |
|
AIR FORCE MIL-A- 6825 |
ADAPTER, AMMUNITION CHUTE, GUN END, 20MM, TYPE L-3 |
|
AIR FORCE MIL-A- 8064 |
ACTUATORS AND ACTUATING SYSTEMS, AIRCRAFT, ELECTROMECHANICAL GENERAL REQUIREMENTS FOR |
|
AIR FORCE MIL-A- 8118 |
AERIAL DELIVERY KIT ASSEMBLY, CARGO, GENERAL SPECIFICATION FOR |
|
AIR FORCE MIL-A- 8255 |
ANALYZER, ELECTRICAL PULSE IP-223( )-ALA-5 |
|
AIR FORCE MIL-A- 83116 |
AIR CONDITIONING SUBSYSTEMS, AIR-CYCLE, AIRCRAFT AND AIRCRAFT-LAUNCHED MISSILES, GENERAL SPECIFICATION FOR |
|
AIR FORCE MIL-A- 83136 |
ARRESTING HOOK INSTALLATION, RUNWAY ARRESTING SYSTEM, AIRCRAFT, EMERGENCY |
|
AIR FORCE MIL-A- 83444 |
AIRPLANE DAMAGE TOLERANCE REQUIREMENTS |
|
AIR FORCE MIL-A- 83462 |
ARCTIC CUSHIONS - CLOTHING, CHU-10/P AND CHU-11/P |
|
AIR FORCE MIL-A- 83577 |
ASSEMBLIES, MOVING MECHANICAL, FOR SPACE AND LAUNCH VEHICLES, GENERAL SPECIFICATION FOR |
|
AIR FORCE MIL-A- 83783 |
ADAPTER, TEST, MX-9042/G |
|
AIR FORCE MIL-A- 8421 |
AIR TRANSPORTABILITY REQUIREMENTS, GENERAL SPECIFICATION FOR |
|
AIR FORCE MIL-A- 87166 |
AERIAL REFUELING RECEIVER SUBSYSTEMS |
|
AIR FORCE MIL-A- 87221 |
AIRCRAFT STRUCTURES, GENERAL SPECIFICATION FOR |
|
AIR FORCE MIL-A- 8860 |
AIRPLANE STRENGTH AND RIGIDITY, GENERAL SPECIFICATION FOR |
|
AIR FORCE MIL-A- 8865 |
AIRPLANE STRENGTH AND RIGIDITY MISCELLANEOUS LOADS |
|
AIR FORCE MIL-A- 8871 |
AIRPLANE STRENGTH AND RIGIDITY FLIGHT AND GROUND OPERATIONS TESTS |
|
AIR FORCE MIL-A- 8892 |
AIRPLANE STRENGTH AND RIGIDITY, VIBRATION |
|
AIR FORCE MIL-A- 8893 |
AIRPLANE STRENGTH AND RIGIDITY, SONIC FATIGUE |
|
AIR FORCE MIL-A- 8897 |
ACCUMULATORS, HYDRAULIC, CYLINDRICAL 3,000 PSI, AIRCRAFT, TYPE II SYSTEMS |
|
AIR FORCE MIL-A- 9286 |
AF AMPLIFIER AM-476( )/AIC-10 |
|
AIR FORCE MIL-A- 9511 |
ANTENNA GROUP AN-FRA-24( ) AND AN-FRA-25 |
|
AIR FORCE MIL-B- 14910 |
BOMB, GENERAL PURPOSE, 750 POUND, M117A2 AND M117A3 LOADING, ASSEMBLING AND MARKING |
|
AIR FORCE MIL-B- 25846 |
BOMB, PRACTICE, PROFILE BDU-8/B |
|
AIR FORCE MIL-B- 26793 |
BLOWER, GASOLINE ENGINE DRIVEN, TYPE A-1 |
|
AIR FORCE MIL-B- 27871 |
BEACON SET, RADIO AN/URT-21 |
|
AIR FORCE MIL-B- 27935 |
BEACON-TRANSPONDER SET, TACAN, AN/TRN-17( ) |
|
AIR FORCE MIL-B- 3402 |
BLOWER, GASOLINE-DRIVEN, AIRCRAFT VENTILATION, PORTABLE, 2,900 CFM, TYPE A-2 |
|
AIR FORCE MIL-B- 38401 |
BEACON SET, RADIO AN/URT-33 |
|
AIR FORCE MIL-B- 38666 |
BOMB, DEMOLITION, BLU-31/B, EXPLOSIVE LOADING REQUIREMENTS |
|
AIR FORCE MIL-B- 38686 |
BOOSTER, FUZE BBU-23/B |
|
AIR FORCE MIL-B- 38687 |
BOMB, BLAST, CRADLED BLU-82/B |
|
AIR FORCE MIL-B- 38977 |
BOMB, PRACTICE BDU-38/B |
|
AIR FORCE MIL-B- 5428 |
BELT, SAFETY, SHOULDER, HARNESS, TROOP, TYPE D-2 |
|
AIR FORCE MIL-B- 5935 |
BOMBING NAVIGATIONAL SYSTEMS, MA SERIES, GENERAL SPECIFICATION FOR |
|
AIR FORCE MIL-B- 6703 |
BELT, TROOP AND TURRET GUNNER'S SAFETY |
|
AIR FORCE MIL-B- 8075 |
BRAKE CONTROL SYSTEMS, ANTISKID, AIRCRAFT WHEELS, GENERAL SPECIFICATION FOR |
|
AIR FORCE MIL-B- 83183 |
BARRIER, AIRCRAFT ARRESTING |
|
AIR FORCE MIL-B- 83787 |
BELTS, AIRCRAFT SAFETY, LAP, TROOP, TYPES MD-1 AND MD- 2 |
|
AIR FORCE MIL-B- 8437 |
BELT, AIRCRAFT SAFETY, LAP, TROOP TYPE MC-1A |
|
AIR FORCE MIL-B- 87162 |
BAFFLE MATERIAL, EXPLOSION SUPPRESSION, EXPANDED ALUMINUM MESH, FOR AIRCRAFT FUEL TANKS |
|
AIR FORCE MIL-B- 87167 |
BELT, AIRCRAFT SAFETY, HBU-12/A |
|
AIR FORCE MIL-C- 25213 |
CRADLE, BOMB TRANSPORT AND LOADING, TYPE MB-1 |
|
AIR FORCE MIL-C- 25223 |
CHARGE, SPOTTING, BOMB, TYPE MA-1 |
|
AIR FORCE MIL-C- 25488 |
CASE, COMPUTER, MB-8 FLIGHT COMPUTER |
|
AIR FORCE MIL-C- 25548 |
CONTROL, PUBLIC ADDRESS SET C-1614/AIC-13 |
|
AIR FORCE MIL-C- 25674 |
CONVERTER, LIQUID OXYGEN TYPE ME-3 |
|
AIR FORCE MIL-C- 25737 |
COMMUNICATION - IDENTIFICATION - NAVIGATION SUB-SYSTEM AN/ASQ-30 |
|
AIR FORCE MIL-C- 25918 |
CARTRIDGE ACTUATED DEVICES, AIRCRAFT CREW EMERGENCY ESCAPE, GENERAL SPECIFICATION FOR |
|
AIR FORCE MIL-C- 26237 |
CRADLE, AIRCRAFT-MISSILE COMPONENTS MMU-1/E |
|
AIR FORCE MIL-C- 26339 |
CARRIER, PASSENGER, CARGO, UTILITY, FULL TRACK, OVER-THE- SNOW TYPE |
|
AIR FORCE MIL-C- 26432 |
CODER - DECODER GROUPS FOR RADAR SETS |
|
AIR FORCE MIL-C- 26837 |
CONTROL, ANTENNA C-1830( )-GPS |
|
AIR FORCE MIL-C- 27240 |
CONTROL, RADIO SET C-1057B-ARC-34 |
|
AIR FORCE MIL-C- 27336 |
CONVERTER, LIQUID OXYGEN TYPE GCU-17/A |
|
AIR FORCE MIL-C- 27480 |
CAP, SAFETY, PRESSURE FUEL SERVICING, AIRCRAFT NOMINAL 4- INCH DIAMETER |
|
AIR FORCE MIL-C- 27505 |
CARTRIDGE, ENGINE STARTER MXU-41/A |
|
AIR FORCE MIL-C- 27635 |
CONTROL, CONVERTER RECEIVER C-2563/ARR |
|
AIR FORCE MIL-C- 27652 |
CONVERTER, LIQUID OXYGEN GCU-20/A |
|
AIR FORCE MIL-C- 27691 |
CARGO HANDLING SYSTEM, AIRCRAFT A/A32H-4 |
|
AIR FORCE MIL-C- 27755 |
COMMUNICATION CENTRAL AN/MRC-101( ) |
|
AIR FORCE MIL-C- 27786 |
CONTROL-INDICATOR C-6224( )/FYQ-9 |
|
AIR FORCE MIL-C- 27788 |
COMPUTER-PROJECTOR CONTROL C-6226( )/FYQ-9 |
|
AIR FORCE MIL-C- 27789 |
CONTROL, DISPLAY UNIT C-6311( )/FYQ-9 |
|
AIR FORCE MIL-C- 38257 |
CONTROL, TRANSPONDER SET C-6280 ( )(P)/APX |
|
AIR FORCE MIL-C- 38271 |
CONNECTOR, OXYGEN MASK TO REGULATOR CRU-60/P |
|
AIR FORCE MIL-C- 38373 |
CAP, FLUID TANK FILLER |
|
AIR FORCE MIL-C- 38747 |
COVERING, FLOOR, MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR |
|
AIR FORCE MIL-C- 38972 |
CARTRIDGE, BOMB EJECTION CCU-9/B |
|
AIR FORCE MIL-C- 38973 |
CARTRIDGE, BOMB EJECTION CCU-10/B |
|
AIR FORCE MIL-C- 46722 |
CHASSIS, TRAILER: 1 TO 5 TON, 4 WHEEL GENERAL PURPOSE |
|
AIR FORCE MIL-C- 5011 |
CHARTS; STANDARD AIRCRAFT CHARACTERISTICS AND PERFORMANCE, PILOTED AIRCRAFT |
|
AIR FORCE MIL-C- 5435 |
CYLINDER, OXYGEN, LOW PRESSURE, PORTABLE, TYPE A- 6 |
|
AIR FORCE MIL-C- 5499 |
CORES: AIRCRAFT HIGH-PRESSURE AIR VALVE |
|
AIR FORCE MIL-C- 5500 |
CAPS: HIGH PRESSURE AIR VALVE |
|
AIR FORCE MIL-C- 5650 |
CORD; ELASTIC EXERCISER |
|
AIR FORCE MIL-C- 6369 |
CONTROL PANEL C-759( )-A |
|
AIR FORCE MIL-C- 6386 |
CONTAINER, AIRCRAFT FIRE EXTINGUISHER, BROMOCHLOROMETHANE, TYPE B-1A |
|
AIR FORCE MIL-C- 6591 |
COMPRESSOR UNIT, AIRCRAFT, ELECTRIC MOTOR DRIVEN, GENERAL SPECIFICATION FOR |
|
AIR FORCE MIL-C- 6635 |
CANOPY, PARACHUTE, RIBBON, GENERAL SPECIFICATION FOR CONSTRUCTION OF |
|
AIR FORCE MIL-C- 7244 |
CAP AND ADAPTER UNIT, TANK FILLER |
|
AIR FORCE MIL-C- 8174 |
CONTROL, RECEIVER C-996 ( )/A |
|
AIR FORCE MIL-C- 83894 |
CLIP, SAFETY, ARMING WIRE RETAINING |
|
AIR FORCE MIL-C- 8414 |
CONTROL PANEL C-423( )/A |
|
AIR FORCE MIL-C- 8425 |
CONTROL, DIRECTION FINDER C-1513( )/A |
|
AIR FORCE MIL-C- 8703 |
CHAIN ASSEMBLY, SINGLE LEG, 10,000 POUND CAPACITY, TYPE MA- 1 |
|
AIR FORCE MIL-C- 8720 |
CONTROL-INDICATOR, J-2 MAGNETIC COMPASS, TYPE ML-1 |
|
AIR FORCE MIL-C- 8838 |
CYLINDER, PNEUMATIC ACTUATING, AIRCRAFT UTILITY SYSTEM, GENERAL SPECIFICATION FOR |
|
AIR FORCE MIL-C- 9226 |
CONTROL, PANEL C-826/AIC-10 |
|
AIR FORCE MIL-C- 9544 |
COUPLER, ANTENNA CU-547( )/GR |
|
AIR FORCE MIL-C- 9717 |
CHARGER, GUN, CALIBER .50, SEMI-AUTOMATIC MAU-1/A |
|
AIR FORCE MIL-D- 25082 |
DIRECTION FINDER GROUP AN, ANA-25, BENCH, PREFLIGHT, AND FLIGHT TESTS OF |
|
AIR FORCE MIL-D- 27568 |
DUMMY WARHEAD, GUIDED MISSILE MDU-16/A |
|
AIR FORCE MIL-D- 27729 |
DETECTING SYSTEM, FLAME - SMOKE, AIRCRAFT AND AEROSPACE VEHICLES, GENERAL PERFORMANCE, INSTALLATION AND TEST OF |
|
AIR FORCE MIL-D- 38402 |
DIRECTION FINDER GROUP AN/ARA-50 GENERAL SPECIFICATION FOR |
|
AIR FORCE MIL-D- 38636 |
DISPENSER, BOMB AND ROCKET, SUU-20B/A, TRAINING TYPE AND GUN ASSEMBLY, BOMB EJECTOR, SUU-20B/A |
|
AIR FORCE MIL-D- 7253 |
DETECTION SYSTEM, FIRE, THERMOCOUPLE, INSTALLATION OF |
|
AIR FORCE MIL-D- 7269 |
DISPENSING SYSTEM, CHAFF, MANUAL, INSTALLATION OF |
|
AIR FORCE MIL-D- 7602 |
DRIVE, TURBINE, AIR, AIRCRAFT ACCESSORY, GENERAL SPECIFICATION FOR |
|
AIR FORCE MIL-D- 8778 |
DATA FOR EVALUATION AND DEVELOPMENT OF ROTARY WING AIRCRAFT |
|
AIR FORCE MIL-D- 9056 |
DECELERATION PARACHUTE SYSTEMS, AIRCRAFT, GENERAL REQUIREMENTS FOR |
|
AIR FORCE MIL-D- 9412 |
DATA FOR AEROSPACE GROUND EQUIPMENT (AGE) |
|
AIR FORCE MIL-D- 9564 |
SCREW, MACHINE-DOUBLE HEXAGON EXTENDED WASHER HEAD, DRILLED, PD SHANK, AMS5731, .164-36 UNJF-3A |
|
AIR FORCE MIL-DTL- 19328 |
CONVERTER, LIQUID OXYGEN, 5 LITER, MB-5A |
|
AIR FORCE MIL-DTL- 25666 |
CONVERTER, LIQUID OXYGEN, CAPACITANCE TYPE GAUGING, GENERAL SPECIFICATION FOR |
|
AIR FORCE MIL-DTL- 25666/1 |
CONVERTER, LIQUID OXYGEN GCU-2A/A |
|
AIR FORCE MIL-DTL- 25666/3 |
CONVERTER, LIQUID OXYGEN GCU-10/A |
|
AIR FORCE MIL-DTL- 25666/5 |
CONVERTER, LIQUID OXYGEN GCU-17/A |
|
AIR FORCE MIL-DTL- 25666/6 |
CONVERTER, LIQUID OXYGEN GCU-20/A |
|
AIR FORCE MIL-DTL- 25666/7 |
CONVERTER, LIQUID OXYGEN TYPE ME-3 |
|
AIR FORCE MIL-DTL- 25959 |
TIE DOWNS, CARGO, AIRCRAFT |
|
AIR FORCE MIL-DTL- 27443 |
PALLETS, CARGO, AIRCRAFT, TYPE HCU-6/E AND HCU-12/E |
|
AIR FORCE MIL-DTL- 32074 |
EXPLOSIVE, PLASTIC-BONDED, CAST AFX-757 |
|
AIR FORCE MIL-DTL- 45500 |
GUN, AUTOMATIC, 20MM, GENERAL SPECIFICATION FOR |
|
AIR FORCE MIL-DTL- 5886 |
CYLINDER, AIRCRAFT OXYGEN, LOW PRESSURE, NONSHATTERABLE |
|
AIR FORCE MIL-DTL- 5886/1 |
CYLINDER, AIRCRAFT OXYGEN, LOW PRESSURE, NONSHATTERABLE |
|
AIR FORCE MIL-DTL- 6645 |
PARACHUTES, PERSONNEL, GENERAL SPECIFICATION FOR |
|
AIR FORCE MIL-DTL- 7560 |
VALVE ASSEMBLY, OXYGEN CYLINDER, BAILOUT |
|
AIR FORCE MIL-DTL- 7560/1 |
VALVE ASSEMBLY, OXYGEN CYLINDER, BAILOUT |
|
AIR FORCE MIL-DTL- 83352 |
SIGNAL KIT, PERSONNEL, DISTRESS, A/P25S-5A |
|
AIR FORCE MIL-DTL- 9479 |
SEAT SYSTEM, UPWARD EJECTION, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
AIR FORCE MIL-DTL- 9814 |
STAND, CABLE REWIND, REVERSIBLE, THU-4/E |
|
AIR FORCE MIL-E- 25366 |
ELECTRICAL AND ELECTRONIC EQUIPMENT, GUIDED MISSILE, INSTALLATION OF, GENERAL SPECIFICATION FOR |
|
AIR FORCE MIL-E- 27005 |
EXPLOSIVE KIT, PARACHUTE RELEASE MLU-5/B AND EXPLOSIVE KIT, PARACHUTE RELEASE MLU-7/B |
|
AIR FORCE MIL-E- 38020 |
ENGAGING DEVICE, AIRCRAFT ARRESTING BARRIER BAK- 11/F |
|
AIR FORCE MIL-E- 5352 |
EXTINGUISHING SYSTEM, FIRE, AIRCRAFT, INSTALLATION OF |
|
AIR FORCE MIL-E- 83252 |
EMERGENCY OXYGEN SUPPLY, CHLORATE CANDLE AIRCRAFT CRU- 74/P |
|
AIR FORCE MIL-E- 87145 |
ENVIRONMENTAL CONTROL, AIRBORNE |
|
AIR FORCE MIL-E- 87235 |
EMERGENCY ESCAPE, AIRCRAFT |
|
AIR FORCE MIL-F- 25352 |
FLUTTER, DIVERGENCE, AND REVERSAL IN AIRCRAFT, PREVENTION OF |
|
AIR FORCE MIL-F- 25648 |
FIRE AND EXPLOSION SUPPRESSION UNITS, AIRCRAFT FUEL TANK AND FUEL TANK CAVITY, GENERAL SPECIFICATION FOR |
|
AIR FORCE MIL-F- 25682 |
FILTER AND FILTER ELEMENT, FLUID PRESSURE, HYDRAULIC, ABSOLUTE, 25 MICRON, MINUS 65 DEG. TO PLUS 450 AND PLUS 600 DEG. F |
|
AIR FORCE MIL-F- 5508 |
FUSES, AIRCRAFT AUTOMATIC QUANTITY-MEASURING, HYDRAULIC |
|
AIR FORCE MIL-F- 5577 |
FITTINGS, TANK, POWERPLANT FLUID, REMOVABLE, GENERAL SPECIFICATION FOR |
|
AIR FORCE MIL-F- 7417 |
FIXED GUN AND ROCKET INSTALLATION, ENGINEERING TESTS OF |
|
AIR FORCE MIL-F- 8261 |
FUNGUS RESISTANCE TESTS, AERONAUTICAL AND ASSOCIATED MATERIALS, GENERAL SPECIFICATION FOR |
|
AIR FORCE MIL-F- 83691 |
FLIGHT TEST DEMONSTRATION REQUIREMENTS FOR DEPARTURE RESISTANCE AND POST-DEPARTURE CHARACTERISTICS OF PILOTED AIRPLANES |
|
AIR FORCE MIL-F- 83860/1 |
FILTER ELEMENTS, FLUID PRESSURE, HYDRAULIC AIRCRAFT, DISPOSABLE, 5 MICRON ABSOLUTE |
|
AIR FORCE MIL-F- 83861/1 |
FILTER ELEMENTS, FLUID PRESSURE, HYDRAULIC AIRCRAFT, DISPOSABLE, 5 MICRON ABSOLUTE |
|
AIR FORCE MIL-F- 83861/2 |
FILTER ELEMENTS, NONCLEANABLE, FLUID PRESSURE, HYDRAULIC LINE, 15 ABSOLUTE, 5 MICRON, TYPE II SYSTEM |
|
AIR FORCE MIL-F- 8815/1 |
FILTER, FLUID, PRESSURE, HYDRAULIC LINE, 3000 PSI ABSOLUTE 15 MICRON, STYLE A, BYPASS, -65 DEGREES TO PLUS 275 DEGREES F |
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AIR FORCE MIL-F- 8815/2 |
FILTER, FLUID, PRESSURE, HYDRAULIC LINE, 3000 PSI ABSOLUTE 15 MICRON, STYLE B, NON BYPASS, -65 DEGREES TO +275 DEGREES F |
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AIR FORCE MIL-F- 8815/3 |
FILTER ELEMENT, FLUID, PRESSURE, HYDRAULIC LINE, 3000 PSI ABSOLUTE 15 MICRONS, -65 DEGREES TO +275 DEGREES F |
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AIR FORCE MIL-G- 5514 |
GLAND DESIGN; PACKING, HYDRAULIC, GENERAL REQUIREMENTS FOR |
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AIR FORCE MIL-G- 6652 |
GRIP ASSEMBLY, CONTROLLER, AIRCRAFT, TYPE B-7A |
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AIR FORCE MIL-G- 83016 |
GAUGE, AIRCRAFT WHEEL, INTEGRAL, TIRE PRESSURE INDICATING |
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AIR FORCE MIL-G- 83063 |
GALLEY, AIRCRAFT, GENERAL REQUIREMENTS FOR |
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AIR FORCE MIL-H- 5364 |
HARNESSES, SHOULDER SAFETY, GENERAL SPECIFICATION FOR |
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AIR FORCE MIL-H- 6017 |
HOSE ASSEMBLY, LOW PRESSURE, FOR BREATHING OXYGEN |
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AIR FORCE MIL-H- 6536 |
HORN AND VALVE, CREW MEMBERS' RELIEF, PRESSURIZED AIRCRAFT |
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AIR FORCE MIL-H- 83265 |
HOOK CABLE SUPPORT, RETRACTABLE BAK-14/F FOR AIRCRAFT ARRESTING SYSTEMS |
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AIR FORCE MIL-H- 83267 |
HOISTING UNIT, AIRCRAFT MAINTENANCE HLU-213/E; HELICOPTER SERVICING, 8,000 POUND CAPACITY |
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AIR FORCE MIL-H- 87969 |
HEADS, MAGNETIC TAPE, INSTRUMENTATION IRIG WIDE BAND GROUP II |
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AIR FORCE MIL-H- 87990 |
ALUMINUM HONEYCOMB SANDWICH ASSEMBLIES, MANUFACTURE OF |
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AIR FORCE MIL-H- 8890 |
HYDRAULIC COMPONENTS, TYPE III, (-65 DEG. TO +450 DEG. F), GENERAL SPECIFICATION FOR |
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AIR FORCE MIL-H- 8891 |
HYDRAULIC SYSTEMS, MANNED FLIGHT VEHICLES, TYPE III DESIGN, INSTALLATION & DATA REQUIREMENTS FOR, GENERAL SPECIFICATION FOR |
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AIR FORCE MIL-HDBK- 1530 |
AIRCRAFT STRUCTURAL INTEGRITY PROGRAM, GENERAL GUIDELINES FOR |
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AIR FORCE MIL-HDBK- 1547 |
ELECTRONIC PARTS, MATERIALS, AND PROCESSES FOR SPACE AND LAUNCH VEHICLES |
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AIR FORCE MIL-HDBK- 162 |
UNITED STATES RADAR EQUIPMENT |
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AIR FORCE MIL-HDBK- 162/1 |
RADAR EQUIPMENT, UNITED STATES CH-1 1 MAR 79 |
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AIR FORCE MIL-HDBK- 1783 |
ENGINE STRUCTURAL INTEGRITY PROGRAM (ENSIP) |
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AIR FORCE MIL-HDBK- 1791 |
DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT |
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AIR FORCE MIL-HDBK- 1797 |
FLYING QUALITIES OF PILOTED AIRCRAFT |
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AIR FORCE MIL-HDBK- 1811 |
MASS PROPERTIES CONTROL FOR SPACE VEHICLES |
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AIR FORCE MIL-HDBK- 23 |
STRUCTURAL SANDWICH COMPOSITES |
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AIR FORCE MIL-HDBK- 339 |
CUSTOM LARGE SCALE INTEGRATED CIRCUIT DEVELOPMENT AND ACQUISITION FOR SPACE VEHICLES |
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AIR FORCE MIL-HDBK- 340 |
TEST REQUIREMENTS FOR LAUNCH, UPPER-STAGE, AND SPACE VEHICLES VOL II: APPLICATIONS GUIDELINES |
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AIR FORCE MIL-HDBK- 340 |
TEST REQUIREMENTS FOR LAUNCH, UPPER-STAGE, AND SPACE VEHICLES VOL I: BASELINES |
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AIR FORCE MIL-HDBK- 340 |
TEST REQUIREMENTS FOR LAUNCH, UPPER-STAGE, AND SPACE VEHICLES VOL I: BASELINES |
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AIR FORCE MIL-HDBK- 348 |
SATELLITE CONTROL NETWORK HARDWARE AND SOFTWARE OPERATIONAL ACCEPTANCE PROCESS |
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AIR FORCE MIL-HDBK- 349 |
MANUFACTURE AND INSPECTION OF ADHESIVE BONDED, ALUMINUM HONEYCOMB SANDWICH ASSEMBLIES FOR AIRCRAFT |
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AIR FORCE MIL-HDBK- 5 |
METALLIC MATERIALS AND ELEMENTS FOR AEROSPACE VEHICLE STRUCTURES |
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AIR FORCE MIL-HDBK- 500 |
KEY SUPPLIER PROCESSES FOR AVIATION AND SPACE SECTORS ACQUISITION AND SUSTAINMENT PROGRAMS |
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AIR FORCE MIL-HDBK- 83575 |
GENERAL HANDBOOK FOR SPACE VEHICLE WIRING HARNESS DESIGN AND TESTING |
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AIR FORCE MIL-HDBK- 83578 |
CRITERIA FOR EXPLOSIVE SYSTEMS AND DEVICES USED ON SPACE VEHICLES |
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AIR FORCE MIL-HDBK- 87213 |
ELECTRONICALLY/OPTICALLY GENERATED AIRBORNE DISPLAYS |
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AIR FORCE MIL-HDBK- 87244 |
AVIONICS/ELECTRONICS INTEGRITY |
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AIR FORCE MIL-I- 27543 |
INTERCOMMUNICATION SET AN/AIC-18 |
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AIR FORCE MIL-I- 38243 |
INTERROGATOR SET AN/APX-65 |
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AIR FORCE MIL-I- 38357 |
INDICATOR, BEARING-DISTANCE-HEADING ID-1103A/ARN |
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AIR FORCE MIL-I- 5585 |
INSTALLATION OF LOW PRESSURE OXYGEN EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION OF |
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AIR FORCE MIL-I- 6181 |
INTERFERENCE CONTROL REQUIREMENTS, AIRCRAFT EQUIPMENT |
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AIR FORCE MIL-I- 8303 |
INDICATOR, COURSE 1D-351/ARN |
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AIR FORCE MIL-I- 83456 |
INSTALLATION OF SEGMENTED LIGHTNING DIVERTER STRIPS ON AIRCRAFT RADOMES, GENERAL SPECIFICATION FOR |
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AIR FORCE MIL-I- 9229 |
INDICATOR COURSE, ID-387/ARN |
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AIR FORCE MIL-I- 9475 |
INSTALLATION DESIGN OF LIQUID OXYGEN SYSTEMS IN AIRCRAFT, GENERAL SPECIFICATIONS FOR |
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AIR FORCE MIL-J- 26015 |
JACK, AIRCRAFT HYDRAULIC, AXLE, 35 TON CAPACITY, TYPE F- 2 |
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AIR FORCE MIL-J- 8245 |
JACK, AIRCRAFT LANDING GEARS, 50 TON CAPACITY, TYPE F- 3A |
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AIR FORCE MIL-J- 83278 |
JACK, HYDRAULIC, TRIPOD MMU-129/E, 60 TON CAPACITY 72 TO 144 INCH RANGE |
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AIR FORCE MIL-J- 8711 |
JACK PADS, AIRCRAFT, DESIGN AND INSTALLATION OF |
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AIR FORCE MIL-L- 25245 |
LAUNCHER, SHORT RAIL, TYPE MA-5 |
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AIR FORCE MIL-L- 38637 |
LUG, BOMB, SUSPENSION, 1000 POUND MAU-76/A |
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AIR FORCE MIL-L- 38671 |
LUG, SUSPENSION, BOMB MAU-129/A, "T" TYPE |
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AIR FORCE MIL-L- 6378 |
LADDERS, FOLDING REFUELING |
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AIR FORCE MIL-L- 87139 |
LANDING GEAR SYSTEMS |
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AIR FORCE MIL-L- 9799 |
LAUNCHER, ROCKET LAU-18/A |
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AIR FORCE MIL-M- 25047 |
MARKINGS AND EXTERIOR FINISH COLORS FOR AIRPLANES, AIRPLANE PARTS, AND MISSILES (BALLISTIC MISSILES EXCLUDED) |
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AIR FORCE MIL-M- 27274 |
MASK, OXYGEN MBU-5/P |
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AIR FORCE MIL-M- 27733 |
MODIFICATION AND MARKING PROCEDURES FOR TEST EQUIPMENT IN AEROSPACE VEHICLES (CLASS II MODIFICATIONS) |
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AIR FORCE MIL-M- 27741 |
MULTIPLEXER SET, AN/FCC-17( ), AN/FCC-21 ( ), AN/FCC-22( ), AN/MCC-12( ) (MOBILE AND FIXED INSTALLATION) |
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AIR FORCE MIL-M- 38310 |
MASS PROPERTIES CONTROL REQUIREMENTS FOR MISSILE AND SPACE VEHICLES |
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AIR FORCE MIL-M- 5776 |
MAINTENANCE PLATFORM, AIRCRAFT ADJUSTABLE, 13 TO 20 FEET TYPE B-2 |
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AIR FORCE MIL-M- 5777 |
MAINTENANCE PLATFORM, AIRCRAFT, ADJUSTABLE, 3 TO 10 FEET, TYPE B-1 |
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AIR FORCE MIL-M- 7404 |
MAINTENANCE PLATFORM, AIRCRAFT, ADJUSTABLE, 3 TO 7 FEET TYPE B-4A |
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AIR FORCE MIL-M- 7405 |
MAINTENANCE PLATFORM, AIRCRAFT, TYPE B-5A |
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AIR FORCE MIL-M- 83869 |
MASK ASSEMBLY, OXYGEN, FIRE FIGHTER'S |
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AIR FORCE MIL-M- 87163 |
MASK, OXYGEN MBU-12/P |
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AIR FORCE MIL-M- 87973 |
MAINTENANCE PLATFORM SELF-PROPELLED, BOOM, LIFT, 40, 60, AND 80 FOOT |
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AIR FORCE MIL-M- 87977 |
MAINTENANCE PLATFORM, AIRCRAFT |
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AIR FORCE MIL-N- 25161 |
NOZZLE, AERIAL PRESSURE REFUELING, TYPE MA-2 |
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AIR FORCE MIL-N- 27444 |
NET, CARGO TIEDOWN, PALLETS, HCU-7/E, HCU-15/C, HCU-11/C, AND HCU-16/C |
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AIR FORCE MIL-N- 27647 |
NET CARGO TIEDOWN, PALLET HCU-11/C |
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AIR FORCE MIL-N- 27822 |
NETWORK, COMBINING MX-3569( )/FCC-17 |
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AIR FORCE MIL-O- 27335 |
OXYGEN SYSTEM, SURVIVAL CONTAINER-OXYGEN KIT, GENERAL SPECIFICATION FOR |
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AIR FORCE MIL-O- 27959 |
OPERATION CENTRAL AN/TSQ-61 |
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AIR FORCE MIL-O- 87226 |
OXYGEN SYSTEMS, AIRCRAFT, GENERAL SPECIFICATION FOR |
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AIR FORCE MIL-O- 9292 |
OPTICAL GROUP, BOMBSIGHT, TYPE MA-4 |
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AIR FORCE MIL-P- 27431 |
PURGING KIT, CONVERTER SYSTEM, LIQUID OXYGEN, KMU- 78/E |
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AIR FORCE MIL-P- 38633 |
PRIMER, STAB, FOR WDU-4A/A WARHEAD |
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AIR FORCE MIL-P- 38683 |
POLYMER, URETHANE, LIQUID |
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AIR FORCE MIL-P- 5175 |
PLATE, ANCHOR, AIRCRAFT TROOP SEAT |
|
AIR FORCE MIL-P- 5517 |
PLASTIC PARTS IN AIRCRAFT HYDRAULIC EQUIPMENT, GENERAL TESTS FOR |
|
AIR FORCE MIL-P- 5518 |
PNEUMATIC SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION, GENERAL REQUIREMENTS FOR |
|
AIR FORCE MIL-P- 5954 |
PUMP UNIT, HYDRAULIC, ELECTRIC MOTOR DRIVEN FIXED DISPLACEMENT |
|
AIR FORCE MIL-P- 5994 |
PUMP UNITS, HYDRAULIC, ELECTRIC MOTOR DRIVEN, VARIABLE DELIVERY |
|
AIR FORCE MIL-P- 6525 |
PUMP, FUEL TRANSFER, AERIAL REFUELING, GENERAL SPECIFICATION FOR |
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AIR FORCE MIL-P- 6640 |
PNEUMATIC BAG, AIRCRAFT LIFTING, 12 TON CAPACITY, TYPE F2 |
|
AIR FORCE MIL-P- 83037 |
PLATFORM, CARGO, AERIAL DELIVERY A/E29H-1 |
|
AIR FORCE MIL-P- 83126 |
PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
|
AIR FORCE MIL-P- 83927 |
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-1037C |
|
AIR FORCE MIL-P- 8564 |
PNEUMATIC SYSTEM COMPONENTS, AERONAUTICAL, GENERAL SPECIFICATION FOR |
|
AIR FORCE MIL-P- 87141 |
PARACHUTES |
|
AIR FORCE MIL-P- 9873 |
PASSENGER AND CARGO VEHICLES; GENERAL SPECIFICATION FOR MAINTAINABILITY FEATURES OF |
|
AIR FORCE MIL-PRF- 26392 |
DUMMY CONVERTERS, LIQUID OXYGEN INDICATOR SYSTEM, 10- LITER CRU-23/A AND 25-LITER CRU-24/A |