MIL-M-87113 Revision A:1993
|
MASK, OXYGEN, MBU-10/P |
MIL-B-44421 Base Document:1991
|
Body Armor, Small Arms Protective, Aircrew, Survival (No S/S Document) |
MIL-J-26149 Revision E:1988
|
JACK, HYDRAULIC, AIRCRAFT MAINTENANCE, GENERAL SPECIFICATION FOR |
MIL STD 680 : B NOTICE 1
|
CONTRACTOR STANDARDIZATION PROGRAM REQUIREMENTS |
MIL F 27272 : B
|
FITTING, TETRAFLUOROETHYLENE HOSE, HIGH TEMPERATURE, MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
MIL-I-7721 Revision D:1992
|
INDICATOR, VERTICAL SPEED, 3-INCH |
MIL-I-38121 Revision C:1989
|
INDICATOR, PRESSURE, EGU-9/A |
MIL-R-8236 Revision F:1995
|
REEL, SHOULDER HARNESS, INERTIA LOCK |
MIL I 27197 : C
|
INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED |
MIL S 5765 : F
|
STRAND, WIRE ROPE, ARMORED STEEL |
MIL H 26626 : D
|
HOSE ASSEMBLY, TETRAFLUOROETHYLENE, OXYGEN |
MIL-A-5885 Revision D:1987
|
ACCELEROMETER, AIRCRAFT |
MIL-I-85071 Revision A:1992
|
INVERTERS, AIRCRAFT, DC TO AC, GENERAL SPECIFICATION FOR |
MIL-STD-7080 Base Document:1994
|
SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT |
MIL F 5373 : D
|
FUSEHOLDER, BLOCK TYPE, AIRCRAFT |
MIL-I-82787 Base Document:1990
|
IGNITER ASSEMBLY, ROCKET MOTOR MK 104 |
MIL-C-44417 Base Document:1991
|
CARRIER, BODY ARMOUR, SMALL ARMS PROTECTIVE, AIRCREW, SURVIVAL |
MIL-T-27305 Revision C:1987
|
TRANSFORMER AND INDUCTORS [AUDIO, POWER AND HIGH POWER PULSE] INDUCTOR, POWER TF5S04ZZ |
MIL BULL 147 : E
|
SPECIFICATIONS AND STANDARDS OF NON-GOVERNMENT ORGANIZATIONS RELEASED FOR FLIGHT VEHICLE DESIGN AND CONSTRUCTION |
MIL-T-83823 Base Document:1991
|
TRUCK, FIRE FIGHTING (STRUCTURAL OR BRUSH STRUCTURAL) |
MIL-STD-1662 Revision C:1992
|
ORDNANCE ALTERATION (ORDALT) INSTRUCTIONS, PREPARATION OF |
SAE AS 5944 : 1999
|
SLINGS, AIRCRAFT, 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 |
MIL-C-4751 Revision D:1983
|
CASTERS, RIGID AND SWIVEL, PRECISION HEAVY DUTY, AND SHOCK ABSORBING |
MIL-HDBK-1587 Base Document:1996
|
MATERIALS AND PROCESS REQUIREMENTS FOR AIR FORCE WEAPON SYSTEM |
MIL-T-83303 Revision C:1988
|
TRUCK, FIREFIGHTING, AIRFIELD RAMP, 4X4, A/S32P-20, TWIN AGENT, SKID MOUNTED |
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 |
MIL F 83798 : B
|
FITTING, RUBBER HOSE, LIGHTWEIGHT MEDIUM PRESSURE, GENERAL SPECIFICATION FOR |
MIL-W-5088 Revision L:1991
|
WIRING, AEROSPACE VEHICLE |
MIL C 38159 : B
|
CONNECTOR, ELECTRIC, RAMP POWER, 480/277 VOLTS, GENERAL SPECIFICATION FOR |
DEFSTAN 00-970(PT0)/12(2014) : 2014
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-C-7580 Revision C:1989
|
COUPLING, FIRE HOSE, REUSABLE HIGH PRESSURE |
MIL T 28800 : E
|
TEST EQUIPMENT FOR USE WITH ELECTRICAL AND ELECTRONIC EQUIPMENT GENERAL SPECIFICATION FOR |
DEFSTAN 00-970(PT0)/13(2014) : 2014
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-T-83965 Revision B:1990
|
TRUCK, FIRE FIGHTING, A/S32P-10, FORCIBLE ENTRY |
DEFSTAN 00-970(PT0)/8(2011) : 2011
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL V 5523 : D
|
VALVE, RELIEF, HYDRAULIC PRESSURE |
MIL-D-23615 Revision C:1993
|
DESIGN AND EVALUATION OF CARTRIDGE ACTUATED DEVICES |
MIL P 23928 : D
|
PANEL, ELECTRICAL, POWER DISTRIBUTION AND MANUAL TRANSFER, CIRCUIT BREAKER TYPE |
SAE AS 53731 : 2014
|
FUSE HOLDER, BLOCK TYPE, AIRCRAFT |
MIL-STD-973 Base Document:1992
|
CONFIGURATION MANAGEMENT |
MIL-A-47312 Revision A:1992
|
ACTUATOR, HYDRAULIC |
MIL-A-27195 Revision A:1989
|
ACCELEROMETER, AIRCRAFT, MECHANICAL ABU-6/A |
MIL-T-85230 Revision A:1992
|
TARGET, TOW, AERIAL, TDU-34/A |
MIL V 6164 : E
|
VALVE, AIRCRAFT, AIR HIGH PRESSURE |
MIL-R-81553 Revision B:1992
|
REGULATOR, CHEST MOUNTED, OXYGEN, POSITIVE PRESSURE, CRU-79/P |
DOD 4120.3M : 1993
|
DEFENSE STANDARDIZATION PROGRAM (DSP) POLICIES AND PROCEDURES OFFICE OF THE ASSISTANT SECRETARY OF DEFENSE PRODUCTION AND LOGISTICS |
MIL-A-27471 Revision C:1993
|
ADAPTER, PRESSURE-REDUCER, IN-LINE CRU-43A/A |
MIL-C-83821 Base Document:1990
|
CRANE, WHEEL MOUNTED, CRASH, ROUGH TERRAIN, HYDRAULIC FULL REVOLVING, 4X4, DED, FIGHTER TYPE AIRCRAFT |
MIL-I-82826 Base Document:1985
|
IGNITER ASSEMBLY |
MIL-C-21049 Revision F:1990
|
COUPLING ASSEMBLIES, QUICK DISCONNECT, AIRCRAFT LIQUID OXYGEN SYSTEMS |
MIL-HDBK-2097 Revision A:1997
|
ACQUISITION OF SUPPORT EQUIPMENT AND ASSOCIATED INTEGRATED LOGISTICS SUPPORT |
MIL C 38271 : B
|
CONNECTOR, OXYGEN MASK TO REGULATOR CRU-60/P |
MIL-STD-2131 Revision A:1991
|
LAUNCHER, EJECTION GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
MIL-C-4150 Revision J:1989
|
CASE, TRANSIT AND STORAGE, WATERPROOF AND WATER-VAPORPROOF |
MIL-F-7179 Revision G:1993
|
FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM |
SAE AS 55151 : 2001
|
PUMP, HYDRAULIC, RAM, HAND DRIVEN |
SAE ARP 1616 : 2017
|
SELF-SEALING BREAKAWAY VALVES FOR CRASH-RESISTANT AIRCRAFT FUEL AND OIL SYSTEMS |
SAE AS 8700 : 1999
|
INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-F-3541 Revision C:1989
|
FITTING, LUBRICATION, GENERAL SPECIFICATION FOR |
MIL E 917 : E
|
ELECTRIC POWER EQUIPMENT, BASIC REQUIREMENTS (NAVAL SHIPBOARD USE) |
MIL-C-38404 Revision E:1992
|
COUPLING, HOSE, REATTACHABLE SCREW-ON |
MIL-M-27274 Revision E:1993
|
MASK, OXYGEN MBU-5/P |
MIL T 5350 : E
|
TRANSMITTER, SYNCHRO OPERATED, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-M-85522 Revision A:1991
|
MONITOR, OXYGEN CRU-91/A |
MIL-I-27304 Revision E:1977
|
INDICATOR, RATE OF FLOW |
MIL-B-9972 Revision B:1994
|
BRAZING, NICKEL, ALLOY, GENERAL SPECIFICATION FOR |
MIL C 9401 : B
|
CANOPY, PARACHUTE, RING SLOT, GENERAL SPECIFICATION FOR CONSTRUCTION OF 0ASG] |
MIL-STD-965 Revision B:1993
|
PARTS CONTROL PROGRAM |
MIL-I-25863 Revision D:1990
|
INDICATOR, ELECTRICAL TACHOMETER 0-110 PERCENT RPM, 2-INCH SIZE, INTEGRALLY LIGHTED |
MIL-A-47309 Revision A:1991
|
AMPLIFIER, PNEUMATIC |
MIL-A-24780 Base Document:1992
|
ACTUATING ASSEMBLY, SINGLE LINEAR MOTION, FOR THE REMOTE ACTUATION OF QUICK ACTING VALVES, GENERAL SPECIFICATION FOR |
MIL B 8111 : F
|
BOX SET, WOOD, NESTED, ORGANIZATIONAL EQUIPMENT TYPE MG AND 1A |
MIL I 6839 : C
|
INDICATOR, POSITION, LANDING GEAR |
MIL-C-83864 Revision A:1982
|
CONTAINER, INNER, SURVIVAL KIT |
MIL-I-8700 Revision A:1970
|
INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL I 25689 : A NOTICE 1
|
INDICATOR, ELECTRICAL TACHOMETER |
MIL-I-85889 Base Document:1988
|
IGNITER, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
MIL C 83867 : B
|
CONNECTOR, OXYGEN MASK HOSE NON-EJECTION TYPE |
MIL S 9479 : C
|
|
MIL-H-21722 Revision B:1992
|
HOOK, THRUST STABILIZING, JATO-45OO POUNDS NOMINAL THRUST |
MIL-H-21660 Revision A:1992
|
HOOK, THRUST, JATO - 1000 POUNDS NOMINAL THRUST |
MIL-V-27296 Revision C:1993
|
VALVE, OXYGEN MASK, COMBINATION INHALATION AND EXHALATION |
MIL-A-18717 Revision C:1993
|
ARRESTING HOOK INSTALLATIONS, AIRCRAFT |
MIL-S-5944 Revision C:1990
|
SLING, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL H 26499 : C
|
HOSE ASSEMBLY, METAL, FLEXIBLE, BREATHING OXYGEN |
MIL-STD-1399-502 Revision A:1995
|
INTERFACE STANDARD FOR SHIPBOARD SYSTEMS, ELECTRONIC SYSTEMS PARAMETERS, SECTION 502 ELECTRONIC SYSTEMS PARAMETERS |
MIL-STD-1476 Revision C:1993
|
METRIC SYSTEM APPLICATION IN NEW DESIGN |
MIL H 83797 : 0
|
HOSE, RUBBER, LIGHTWEIGHT, MEDIUM PRESSURE, GENERAL SPECIFICATION FOR |
MIL-W-5013 Revision L:1991
|
WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL S 12285 : D
|
SWITCH, THERMOSTATIC |
MIL L 7961 : C
|
LIGHT, INDICATOR, PRESS TO TEST |
MIL-I-38391 Base Document:1965
|
INDICATOR, ELECTRICAL TACHOMETER, ERU-12/A 0-350 RPM (ROTOR), 0-7000 RPM (ENGINE) |
MIL A 83419 : C
|
ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
MIL V 47306 : B
|
VALVE, STOP LIFT CHECK |
MIL V 87255 : 0
|
VALVE, PRESSURE, ANTI-G SUIT, HIGH FLOW |
MIL-A-81403 Base Document:1967
|
ALTIMETER-ENCODER, AAU-21/A |
MIL-D-19326 Revision H:1990
|
DESIGN AND INSTALLATION OF LIQUID OXYGEN SYSTEMS IN AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL A 5503 : E
|
ACTUATOR, AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
MIL-T-8598 Revision B:1990
|
TRANSMITTER, TEMPERATURE, ELECTRICAL RESISTANCE, FLUSH-MOUNTED, FREE AIR |
MIL D 26392 : C
|
DUMMY CONVERTERS, LIQUID OXYGEN INDICATOR SYSTEM 10 LITER CRU-23/A AND 25 LITER CRU-24/A |
MIL-A-27670 Revision D:1994
|
AMPLIFIER-INDICATOR GROUP, INDICATED AIRSPEED A/A24G-10 |
MIL-A-83212 Revision A:1976
|
ALTIMETER, PRESSURE AAU-27/A |
MIL-I-83245 Revision A:1994
|
INDICATOR SET, OIL PRESSURE A/A24J-17 |
MIL-R-25410 Revision G:1991
|
REGULATORS, OXYGEN, DILUTER-DEMAND AUTOMATIC-PRESSURE BREATHING |
MIL-D-18300 Revision H:1993
|
DESIGN EXAMINATIONS, ENGINEERING AVIONIC SYSTEMS/EQUIPMENT GENERAL REQUIREMENTS FOR |
MIL-T-26963 Revision D:1992
|
TESTER, PRESSURE GAGE, HYDRAULIC, PORTABLE TYPE MP-1 |
MIL L 25370 : E
|
LIFE PRESERVER INFLATING ASSEMBLY, MA-1 |
MIL-B-55252 Revision B:1992
|
BATTERIES, NON-RECHARGEABLE, MAGNESIUM |
MIL-I-27848 Revision B:1994
|
INDICATOR, HORIZONTAL SITUATION AQU-4/A |
MIL D 83753 : NOTICE 2
|
DISPENSER, BOMB, TYPE SUU-21/A |
MIL-C-5414 Revision G:1993
|
COMPUTER, AIR NAVIGATION DEAD RECKONING TYPE MB 4A AND TYPE CPU 26A/P |
MIL-R-5049 Revision D:1989
|
RING, WIPER, PISTON ROD |
MIL C 7115 : F
|
CONVERTER, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-I-26299 Revision G:1990
|
INDICATORS, RATE OF FLOW, 0-5,000 PPH, INTEGRALLY LIGHTED |
MIL-P-38268 Revision C:1988
|
AURAL PROTECTORS, SOUND |
MIL-V-47311 Base Document:1989
|
VALVE, PNEUMATIC EXHAUST |