MIL-T-38034 Revision E:1970
|
TIMER, FIRE CONTROL, BOMBING, DUAL |
MIL-STD-2156 Base Document:1983
|
LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
MIL-A-53100 Base Document:1990
|
ARCTIC FUEL SYSTEM SUPPLY POINT (AFSSP) |
MIL-HDBK-113 Revision C:1989
|
GUIDE FOR THE SELECTION OF LUBRICANTS, FUNCTIONAL FLUIDS, PRESERVATIVES AND SPECIALITY PRODUCTS FOR USE IN GROUND EQUIPMENT SYSTEMS |
MIL-M-8555 Revision C:1984
|
MISSILE, GUIDED, DESIGN AND CONSTRUCTION, GENERAL SPECIFICATION |
MIL I 25688 : A
|
INDICATOR, ELECTRICAL TACHOMETER ERU-3/A. CRANKSHAFT SPEED 500-4,000 RPM, 3 1/4 INCH SIZE |
MIL-C-52980 Revision B:1988
|
COMPRESSOR, RECIPROCATING AND ROTARY, GASOLINE ENGINE DRIVEN, AIR |
MIL H 81014 : A NOTICE 1
|
HOOK, HELICOPTER, EXTERNAL CARGO, 20,000 POUND CAPACITY, TYPE C |
MIL-B-385 Revision G:1985
|
BREAKERS, PAVING, PNEUMATIC-POWERED (7/8-INCH HEXAGON BY 2-3/4-INCH CHUCK AND 7/8-INCH HEXAGON BY 3-1/4-INCH CHUCK) |
MIL-D-8684 Revision B:1959
|
DATA AND TESTS, ENGINEERING, CONTACT REQUIREMENTS FOR AIR LAUNCHED GUIDED MISSILE SYSTEMS |
MIL-I-27202 Revision A:1980
|
INDICATOR, ELECTRICAL TACHOMETER, 0-110 PERCENT RPM 2-INCH SIZE, INTEGRALLY LIGHTED |
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 |
MIL-P-52327 Revision C:1990
|
PUMPS, CENTRIFUGAL, ELECTRIC-MOTOR-DRIVEN, POSITIVE PRIME, PETROLEUM PRODUCTS, AIRFIELD DEFUELLING AND RECEIVING |
MIL-C-13874 Revision K:1992
|
COMPRESSORS, RECIPROCATING AND ROTARY, AIR, ELECTRIC MOTOR DRIVEN |
MIL-HDBK-1587 Base Document:1996
|
MATERIALS AND PROCESS REQUIREMENTS FOR AIR FORCE WEAPON SYSTEM |
MIL BULL 343 : A
|
DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
DEFSTAN 00-970(PT0)/14(2014) : 2014
|
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)/7(2011) : 2011
|
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 |
MIL-R-85880 Base Document:1988
|
ROCKET, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
MIL-C-0052980 Revision C:1994
|
COMPRESSORS, RECIPROCATING AND ROTARY, AIR DIESEL-ENGINE-DRIVEN, OR GASOLINE-ENGINE-DRIVEN |
GG-T-35 Revision C:1989
|
TABLE; DRAWING, TRACING, AND SCRIBING |
MIL-T-52942 Revision C:1996
|
TRUCK, FIRE FIGHTING: PUMPER, 1000 GPM; LADDER/WATER TOWER COMBINATION |
MIL-C-13899 Revision F:1985
|
COMPRESSOR UNIT, ROTARY: AIR, WHEELBARROW-FRAME-MOUNTED, TWO PNEUMATIC TIRES, GASOLINE-ENGINE-DRIVEN, 60-CFM, 6.5-PSIG |
MIL C 7958 : A
|
CONTROL, PUSH PULL, FLEXIBLE AND RIGID |
MIL-M-25393 Revision A:1969
|
MANUAL, TECHNICAL, INTERMEDIATE MAINTENANCE INSTRUCTIONS (AIRBORNE EQUIPMENT) |
MIL M 38797 : NOTICE 1
|
MANUAL, TECHNICAL, OPERATION INSTRUCTIONS AND MAINTENANCE INSTRUCTIONS (FOR VARIOUS TYPES OF EQUIPMENT) |
MIL T 38170 : F
|
TANK, MOBILE STORAGE, LIQUID OXYGEN TMU 27/M |
MIL-STD-1250 Revision A:1992
|
CORROSION PREVENTION AND DETERIORATION CONTROL IN ELECTRONIC COMPONENTS AND ASSEMBLIES |
MIL H 81529 : 0
|
HOOK, HELICOPTER EXTERNAL CARGO, 6,000 POUND CAPACITY TYPE A |
MIL-P-5994 Revision D:1972
|
PUMP, HYDRAULIC, ELECTRIC MOTOR DRIVEN, VARIABLE DELIVERY, GENERAL SPECIFICATION FOR |
MIL-T-25363 Revision D:1973
|
TANK, PNEUMATIC PRESSURE, AIRCRAFT, GLASS FIBER |
MIL-A-27195 Revision A:1989
|
ACCELEROMETER, AIRCRAFT, MECHANICAL ABU-6/A |
MIL G 26611 : D
|
GENERATOR, TACHOMETER GEU-7/A, MINIATURE |
MIL S 25057 : B
|
SCREEN SYSTEM, AIR INLET, AIRCRAFT TURBINE ENGINE, GENERAL SPECIFICATION FOR |
MIL-I-5133 Revision C:1953
|
INDICATOR, ATTITUDE TYPE J 8 |
MIL-S-8512 Revision D:1974
|
SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF |
MIL-HDBK-1250 Revision A:1995
|
CORROSION PREVENTION AND DETERIORATION CONTROL IN ELECTRONIC COMPONENTS AND ASSEMBLIES |
MIL-S-6150 Revision D:1987
|
STARTER, ENGINE, ELECTRICAL, DIRECT CRANKING, AIRCRAFT 28 VOLT DC |
MIL-STD-2131 Revision A:1991
|
LAUNCHER, EJECTION GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
MIL L 58085 : A
|
LIGHT, BEACON, ANTI COLLISION AIRCRAFT |
MIL-S-83129 Revision A:1972
|
SPECTROMETER, FLUID ANALYSIS A/E35U-3 |
MIL-C-52037 Revision F:1990
|
COMPRESSOR UNIT, RECIPROCATING, POWER DRIVEN, AIR, 15 CFM 3,500 PSI |
MIL-B-45022 Revision F:1992
|
BLAST CLEANING CABINETS |
MIL C 4928 : A
|
CHARGER, BATTERY, SILICON DIODE, TYPE A-1 |
MIL-DTL-85110 Revision B:1997
|
BAR, REPEATABLE RELEASE HOLDBACK (RRHB), AIRCRAFT LAUNCHING, GENERAL REQUIREMENT FOR |
MIL I 25689 : A NOTICE 1
|
INDICATOR, ELECTRICAL TACHOMETER |
MIL-E-87235 Base Document:1985
|
EMERGENCY ESCAPE, AIRCRAFT (REQUEST FOR ISSUE MUST BE SENT VIA ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
MIL-M-38789 Revision A:1970
|
MANUAL, TECHNICAL, OVERHAUL INSTRUCTIONS AND OVERHAUL INSTRUCTIONS WITH ILLUSTRATED PARTS BREAKDOWN (FOR VARIOUS EQUIPMENT AND ACCESSORIES) |
MIL-S-18471 Revision G:1983
|
|
MIL-T-18232 Revision B:1968
|
TARGET, AERIAL, POWERED, DESIGN AND CONSTRUCTION OF GENERAL SPECIFICATION FOR |
MIL-B-467 Revision E:1988
|
BREAKER, PAVING: PNEUMATIC |
MIL-I-25863 Revision D:1990
|
INDICATOR, ELECTRICAL TACHOMETER 0-110 PERCENT RPM, 2-INCH SIZE, INTEGRALLY LIGHTED |
MIL-D-7106 Revision C:1987
|
DRIFTMETER, ELECTRICALLY DRIVEN GYRO STABILIZED |
MIL S 25073 : 0
|
|
MIL G 6162 : B
|
GENERATOR AND STARTER GENERATOR, ELECTRIC DIRECT CURRENT, NOMINAL 30 VOLTS AIRCRAFT GENERAL SPECIFICATION |
GGG-L-795 Revision E:1990
|
LUBRICATING UNIT, POWER OPERATED, AND PUMPING UNITS, PRESSURE LUBRICATING, DRUM MOUNTING |
JSSG-2006 Base Document:1998
|
JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
MIL-M-5166 Revision D:1983
|
MANUAL, TECHNICAL, ASSEMBLY, SERVICING AND ORGANIZATIONAL MAINTENANCE INSTRUCTIONS, [FOR GUIDED MISSILES AND PILOTLESS AIRCRAFT] |
MIL-I-85889 Base Document:1988
|
IGNITER, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
MIL-S-26547 Revision C:1985
|
STARTER-GENERATOR ENGINE STU-6A |
MIL G 8360 : A
|
GAGE, PRESSURE, DIAL INDICATING, MANIFOLD PRESSURE, 10-75 IN MERCURY TYPE MB 1 |
MIL-I-26689 Revision C:1981
|
INDICATOR, HORIZONTAL SITUATION, AQU-2/A |
MIL-I-58067 Revision A:1977
|
INDICATOR, VERTICAL VELOCITY, RAPID RESPONSE ACCELERATION SENSITIVE, GENERAL SPECIFICATION FOR |
MIL-S-6551 Revision A:1981
|
|
MIL-A-25915 Revision A:1980
|
ACCELEROMETER, AIRCRAFT, PILOTS WARNING, TYPE MA-2 |
MIL M 9864 : B
|
MANUALS, TECHNICAL: ORGANIZATIONAL MAINTENANCE (MISSILE AND SPACE SYSTEMS) |
MIL A 25088 : C
|
|
MIL-P-52405 Revision C:1990
|
PUMPS, CENTRIFUGAL, ELECTRIC-MOTOR-DRIVEN (FOR WATER) |
MIL-H-27269 Revision A:1977
|
HORIZONTAL SITUATION INDICATOR GROUP AF A24J AND 1 |
DOD-HDBK-791 Base Document:1988
|
MAINTAINABILITY DESIGN TECHNIQUES |
MIL-S-81771 Revision A:1975
|
Seat System; Aircrew, Crash Resistant; General Specification for |
MIL-C-8412 Revision B:1969
|
COMPASS, MAGNETIC, SLAVED GYRO, TYPE J-4 |
MIL-P-83126 Revision A:1980
|
PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
MIL-P-85034 Base Document:1976
|
POWER PACKAGE, EMERGENCY AC/DC GENERATOR, RAM AIR TURBINE DRIVEN |
MIL-M-25394 Revision A:1969
|
MANUAL, TECHNICAL, OVERHAUL INSTRUCTIONS AND INTERMEDIATE MAINTENANCE INSTRUCTIONS (FOR ENGINES) |
ADS-13F-HDBK : 1997
|
AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES |
MIL-E-38453 Revision A:1971
|
ENVIRONMENTAL CONTROL, ENVIRONMENTAL PROTECTION, AND ENGINE BLEED AIR SYSTEMS, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-I-38391 Base Document:1965
|
INDICATOR, ELECTRICAL TACHOMETER, ERU-12/A 0-350 RPM (ROTOR), 0-7000 RPM (ENGINE) |
MIL-P-85573 Base Document:1983
|
POWER UNIT AIRCRAFT AUXILIARY, GAS TURBINE, GENERAL SPECIFICATION FOR |
MIL-W-26217 Revision B:1985
|
WINCH, DRUM, POWER OPERATED AF E24H 1, CARGO LOADING, 4OOO POUND CAPACITY, VARIABLE SPEED, 28V DC PORTABLE |
MIL-A-27261 Revision A:1966
|
ACCELEROMETER, AIRCRAFT |
MIL-HDBK-275 Revision A:1976
|
GUIDE FOR SELECTION OF LUBRICANTS, FLUIDS AND COMPOUNDS FOR USE IN FLIGHT VEHICLES AND COMPONENTS |
MIL-G-23083 Revision C:1972
|
GYROSCOPE, RATE SWITCHING MS 17399 |
MIL-I-25479 Revision A:1987
|
INDICATOR, MACH NUMBER, SENSITIVE, SERVOED, RANGE .5 TO 1.O, TYPE ME-5 |
MIL-A-27330 Revision B:1987
|
ACCELEROMETER, ELECTRICAL, LINEAR TRU-3/A |
MIL T 83174 : B (3)
|
TRANSMITTER, ACCELEROMETER, AXIAL |
MIL-G-26988 Revision C:1971
|
GAGE, LIQUID QUANTITY, CAPACITOR TYPE TRANSISTORIZED, GENERAL SPECIFICATION FOR |
MIL-I-27680 Revision C:1973
|
INDICATOR, ATTITUDE, ARU-12/A, REMOTE |
MIL-I-27623 Revision C:1972
|
INDICATOR, ATTITUDE, REMOTE STANDBY, 2 INCH |
MIL-I-83117 Revision B:1975
|
INDICATOR, ANGLE OF ATTACK |
MIL-I-25941 Revision D:1986
|
INDICATOR, TURN AND SLIP, 2-INCH SIZE, INTEGRALLY LIGHTED |
MIL-I-25645 Revision D:1970
|
INDICATOR, LIQUID OXYGEN QUANTITY, CAPACITANCE TYPE, GENERAL SPECIFICATION FOR |
MIL-I-27848 Revision B:1994
|
INDICATOR, HORIZONTAL SITUATION AQU-4/A |
MIL-I-38258 Base Document:1965
|
INDICATOR, ATTITUDE ARU 18/A DIRECTOR |
MIL-M-63038 Revision D:1993
|
MANUAL. TECHNICAL, ORGANIZATION OR AVIATION UNIT, DIRECT SUPPORT OR AVIATION INTERMEDIATE, AND GENERAL SUPPORT MAINTENANCE |
MIL-I-27619 Revision G:1974
|
INDICATORS, ATTITUDE DIRECTOR |
MIL-A-53099 Base Document:1990
|
ARCTIC FORWARD AREA REFUELLING EQUIPMENT (AFARE) |
MIL-W-5013 Revision L:1991
|
WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL T 25627 : C
|
TRANSMITTER, SYNCHRO, ANGLE OF ATTACK OR SIDESLIP |