|
MIL T 38034 : E
|
TIMER, FIRE CONTROL, BOMBING, DUAL |
|
MIL STD 2156 : 0
|
LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
|
MIL A 53100 : 0
|
ARCTIC FUEL SYSTEM SUPPLY POINT (AFSSP) |
|
MIL HDBK 113 : C
|
GUIDE FOR THE SELECTION OF LUBRICANTS, FUNCTIONAL FLUIDS, PRESERVATIVES AND SPECIALITY PRODUCTS FOR USE IN GROUND EQUIPMENT SYSTEMS |
|
MIL M 8555 : C
|
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 : B
|
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 : G
|
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 : B
|
DATA AND TESTS, ENGINEERING, CONTACT REQUIREMENTS FOR AIR LAUNCHED GUIDED MISSILE SYSTEMS |
|
MIL I 27202 : A
|
INDICATOR, ELECTRICAL TACHOMETER, 0-110 PERCENT RPM 2-INCH SIZE, INTEGRALLY LIGHTED |
|
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)/14(2014) : 2014
|
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)/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 |
|
MIL R 85880 : 0
|
ROCKET, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
|
MIL C 0052980 : C
|
COMPRESSORS, RECIPROCATING AND ROTARY, AIR DIESEL-ENGINE-DRIVEN, OR GASOLINE-ENGINE-DRIVEN |
|
GG T 35 : C
|
TABLE; DRAWING, TRACING, AND SCRIBING |
|
MIL T 52942 : C
|
TRUCK, FIRE FIGHTING: PUMPER, 1000 GPM; LADDER/WATER TOWER COMBINATION |
|
MIL C 13899 : F
|
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 : A
|
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 : A
|
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 : D
|
PUMP, HYDRAULIC, ELECTRIC MOTOR DRIVEN, VARIABLE DELIVERY, GENERAL SPECIFICATION FOR |
|
MIL T 25363 : D
|
TANK, PNEUMATIC PRESSURE, AIRCRAFT, GLASS FIBER |
|
MIL A 27195 : A
|
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 : C
|
INDICATOR, ATTITUDE TYPE J 8 |
|
MIL S 8512 : D
|
SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF |
|
MIL HDBK 1250 : A
|
CORROSION PREVENTION AND DETERIORATION CONTROL IN ELECTRONIC COMPONENTS AND ASSEMBLIES |
|
MIL S 6150 : D
|
STARTER, ENGINE, ELECTRICAL, DIRECT CRANKING, AIRCRAFT 28 VOLT DC |
|
MIL STD 2131 : A
|
LAUNCHER, EJECTION GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
|
MIL L 58085 : A
|
LIGHT, BEACON, ANTI COLLISION AIRCRAFT |
|
MIL S 83129 : A
|
SPECTROMETER, FLUID ANALYSIS A/E35U-3 |
|
MIL C 52037 : F
|
COMPRESSOR UNIT, RECIPROCATING, POWER DRIVEN, AIR, 15 CFM 3,500 PSI |
|
MIL B 45022 : F
|
BLAST CLEANING CABINETS |
|
MIL C 4928 : A
|
CHARGER, BATTERY, SILICON DIODE, TYPE A-1 |
|
MIL DTL 85110 : B
|
BAR, REPEATABLE RELEASE HOLDBACK (RRHB), AIRCRAFT LAUNCHING, GENERAL REQUIREMENT FOR |
|
MIL I 25689 : A NOTICE 1
|
INDICATOR, ELECTRICAL TACHOMETER |
|
MIL E 87235 : 0
|
EMERGENCY ESCAPE, AIRCRAFT (REQUEST FOR ISSUE MUST BE SENT VIA ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
|
MIL M 38789 : A
|
MANUAL, TECHNICAL, OVERHAUL INSTRUCTIONS AND OVERHAUL INSTRUCTIONS WITH ILLUSTRATED PARTS BREAKDOWN (FOR VARIOUS EQUIPMENT AND ACCESSORIES) |
|
MIL S 18471 : G
|
|
|
MIL T 18232 : B
|
TARGET, AERIAL, POWERED, DESIGN AND CONSTRUCTION OF GENERAL SPECIFICATION FOR |
|
MIL B 467 : E
|
BREAKER, PAVING: PNEUMATIC |
|
MIL I 25863 : D
|
INDICATOR, ELECTRICAL TACHOMETER 0-110 PERCENT RPM, 2-INCH SIZE, INTEGRALLY LIGHTED |
|
MIL D 7106 : C
|
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 : E
|
LUBRICATING UNIT, POWER OPERATED, AND PUMPING UNITS, PRESSURE LUBRICATING, DRUM MOUNTING |
|
JSSG 2006 : 0
|
JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
|
MIL M 5166 : D
|
MANUAL, TECHNICAL, ASSEMBLY, SERVICING AND ORGANIZATIONAL MAINTENANCE INSTRUCTIONS, [FOR GUIDED MISSILES AND PILOTLESS AIRCRAFT] |
|
MIL I 85889 : 0
|
IGNITER, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
|
MIL S 26547 : C
|
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 : C
|
INDICATOR, HORIZONTAL SITUATION, AQU-2/A |
|
MIL I 58067 : A
|
INDICATOR, VERTICAL VELOCITY, RAPID RESPONSE ACCELERATION SENSITIVE, GENERAL SPECIFICATION FOR |
|
MIL S 6551 : A
|
|
|
MIL A 25915 : A
|
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 : C
|
PUMPS, CENTRIFUGAL, ELECTRIC-MOTOR-DRIVEN (FOR WATER) |
|
MIL H 27269 : A
|
HORIZONTAL SITUATION INDICATOR GROUP AF A24J AND 1 |
|
DOD HDBK 791 : 0
|
MAINTAINABILITY DESIGN TECHNIQUES |
|
MIL S 81771 : A
|
SEAT SYSTEM; AIRCREW, CRASH RESISTANT; GENERAL SPECIFICATION FOR |
|
MIL C 8412 : B
|
COMPASS, MAGNETIC, SLAVED GYRO, TYPE J-4 |
|
MIL P 83126 : A
|
PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
|
MIL P 85034 : 0
|
POWER PACKAGE, EMERGENCY AC/DC GENERATOR, RAM AIR TURBINE DRIVEN |
|
MIL M 25394 : A
|
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 : A
|
ENVIRONMENTAL CONTROL, ENVIRONMENTAL PROTECTION, AND ENGINE BLEED AIR SYSTEMS, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL I 38391 : 0
|
INDICATOR, ELECTRICAL TACHOMETER, ERU-12/A 0-350 RPM (ROTOR), 0-7000 RPM (ENGINE) |
|
MIL P 85573 : 0
|
POWER UNIT AIRCRAFT AUXILIARY, GAS TURBINE, GENERAL SPECIFICATION FOR |
|
MIL W 26217 : B
|
WINCH, DRUM, POWER OPERATED AF E24H 1, CARGO LOADING, 4OOO POUND CAPACITY, VARIABLE SPEED, 28V DC PORTABLE |
|
MIL A 27261 : A
|
ACCELEROMETER, AIRCRAFT |
|
MIL HDBK 275 : A
|
GUIDE FOR SELECTION OF LUBRICANTS, FLUIDS AND COMPOUNDS FOR USE IN FLIGHT VEHICLES AND COMPONENTS |
|
MIL G 23083 : C
|
GYROSCOPE, RATE SWITCHING MS 17399 |
|
MIL I 25479 : A
|
INDICATOR, MACH NUMBER, SENSITIVE, SERVOED, RANGE .5 TO 1.O, TYPE ME-5 |
|
MIL A 27330 : B
|
ACCELEROMETER, ELECTRICAL, LINEAR TRU-3/A |
|
MIL T 83174 : B (3)
|
TRANSMITTER, ACCELEROMETER, AXIAL |
|
MIL G 26988 : C
|
GAGE, LIQUID QUANTITY, CAPACITOR TYPE TRANSISTORIZED, GENERAL SPECIFICATION FOR |
|
MIL I 27680 : C
|
INDICATOR, ATTITUDE, ARU-12/A, REMOTE |
|
MIL I 27623 : C
|
INDICATOR, ATTITUDE, REMOTE STANDBY, 2 INCH |
|
MIL I 83117 : B
|
INDICATOR, ANGLE OF ATTACK |
|
MIL I 25941 : D
|
INDICATOR, TURN AND SLIP, 2-INCH SIZE, INTEGRALLY LIGHTED |
|
MIL I 25645 : D
|
INDICATOR, LIQUID OXYGEN QUANTITY, CAPACITANCE TYPE, GENERAL SPECIFICATION FOR |
|
MIL I 27848 : B
|
INDICATOR, HORIZONTAL SITUATION AQU-4/A |
|
MIL I 38258 : 0
|
INDICATOR, ATTITUDE ARU 18/A DIRECTOR |
|
MIL M 63038 : D
|
MANUAL. TECHNICAL, ORGANIZATION OR AVIATION UNIT, DIRECT SUPPORT OR AVIATION INTERMEDIATE, AND GENERAL SUPPORT MAINTENANCE |
|
MIL I 27619 : G
|
INDICATORS, ATTITUDE DIRECTOR |
|
MIL A 53099 : 0
|
ARCTIC FORWARD AREA REFUELLING EQUIPMENT (AFARE) |
|
MIL W 5013 : L
|
WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL T 25627 : C
|
TRANSMITTER, SYNCHRO, ANGLE OF ATTACK OR SIDESLIP |