MIL M 87113 : A
|
MASK, OXYGEN, MBU-10/P |
MIL I 83294 : 0
|
INSTALLATION REQUIREMENT, AIRCRAFT PROPULSION SYSTEMS, GENERAL SPECIFICATION FOR |
MIL T 5842 : B
|
TRANSPARENT AREAS ON AIRCRAFT SURFACES [WINDSHIELDS AND CANOPIES] RAIN REMOVING AND WASHING SYSTEMS FOR, DEFROSTING, DEICING, DEFOGGING, GENERAL SPECIFICATION FOR |
MIL STD 2156 : 0
|
LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
MIL A 83577 : B
|
ASSEMBLIES, MOVING MECHANICAL, FOR SPACE AND LAUNCH VEHICLES, GENERAL SPECIFICATION FOR |
MIL STD 001303 : C
|
PAINTING OF NAVAL ORDNANCE EQUIPMENT |
MIL M 8555 : C
|
MISSILE, GUIDED, DESIGN AND CONSTRUCTION, GENERAL SPECIFICATION |
MIL A 85055 : 0
|
AVIONICS SYSTEM PERFORMANCE SPECIFICATION FOR A-4M/AV-8 BOMBING SET, ANGLE RATE AN/ASB-19(V) |
MIL R 8236 : F
|
REEL, SHOULDER HARNESS, INERTIA LOCK |
MIL STD 7080 : 0
|
SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT |
MIL I 82787 : 0
|
IGNITER ASSEMBLY, ROCKET MOTOR MK 104 |
MIL L 50794 : 0
|
LINEAR SHAPED CHARGE ASSEMBLY |
MIL-D-8684 Revision B:1959
|
DATA AND TESTS, ENGINEERING, CONTACT REQUIREMENTS FOR AIR LAUNCHED GUIDED MISSILE SYSTEMS |
MIL D 82687 : 0
|
DEVICE, ARMING FIRING, ROCKET MOTOR MARK 298 MOD O |
DOD E 83578 : A
|
EXPLOSIVE ORDNANCE FOR SPACE VEHICLES, GENERAL SPECIFICATION FOR (METRIC) |
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)/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)/11(2013) : 2013
|
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 H 8891 : A
|
HYDRAULIC SYSTEMS, MANNED FLIGHT VEHICLES TYPE 111 DESIGN, INSTALLATION AND DATA REQUIREMENTS FOR, GENERAL SPECIFICATION FOR |
MIL F 18264 : D
|
FINISHES: ORGANIC, WEAPONS SYSTEM, APPLICATION AND CONTROL OF |
MIL-H-5440 Revision H:1993
|
HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR |
MIL A 19736 : A
|
AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR |
MIL E 50796 : 0
|
EXPANDING SHIELDED MILD DETONATING CORD ASSEMBLY |
MIL STD 1250 : A
|
CORROSION PREVENTION AND DETERIORATION CONTROL IN ELECTRONIC COMPONENTS AND ASSEMBLIES |
MIL M 25047 : C
|
MARKINGS AND EXTERIOR FINISH COLORS FOR AIRPLANES, AIRPLANE PARTS, AND MISSILES (BALLISTIC MISSILES EXCLUDED) |
MIL A 83469 : 0
|
ADJUSTER, LAP BELT, 1-3/4 INCH WEBBING |
MIL S 25057 : B
|
SCREEN SYSTEM, AIR INLET, AIRCRAFT TURBINE ENGINE, GENERAL SPECIFICATION FOR |
MIL B 81365 : 0
|
BLEED AIR SYSTEMS, GENERAL SPECIFICATIONS FOR |
MIL E 7080 : B
|
ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF |
MIL HDBK 1250 : A
|
CORROSION PREVENTION AND DETERIORATION CONTROL IN ELECTRONIC COMPONENTS AND ASSEMBLIES |
MIL STD 1516 : B
|
UNIFIED CODE FOR COATINGS AND FINISHES FOR DOD MATERIAL |
MIL I 82826 : 0
|
IGNITER ASSEMBLY |
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 |
MIL DTL 85110 : B
|
BAR, REPEATABLE RELEASE HOLDBACK (RRHB), AIRCRAFT LAUNCHING, GENERAL REQUIREMENT FOR |
SAE AS 8700 : 1999
|
INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL C 22751 : D
|
COATING SYSTEM, EPOXY-POLYAMIDE, CHEMICAL AND SOLVENT RESISTANT, PROCESS FOR APPLICATION OF |
MIL S 83576 : 0
|
SOLAR CELL ARRAYS, SPACE VEHICLE, DESIGN AND TESTING, GENERAL SPECIFICATION FOR |
MIL C 18187 : A
|
COATING, PROTECTIVE, APPLICATION TO FABRIC SURFACE OF AIRCRAFT |
MIL-STD-1303 Revision B:1975
|
PAINTING OF NAVAL ORDNANCE EQUIPMENT |
MIL I 8673 : 0
|
INSTALLATION AND TEST OF AIRCRAFT FLEXIBLE WEAPONS SYSTEMS |
MIL C 81907 : 0
|
COATING SYSTEM, POLYURETHANE, ALIPHATIC, WEATHER RESISTANT, PROCESS FOR APPLICATION OF |
MIL C 8507 : D
|
COATING, WASH PRIMER (PRETREATMENT) FOR METALS, APPLICATION OF (FOR AERONAUTICAL USE) |
MIL I 8700 : A
|
INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
JSSG 2006 : 0
|
JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
MIL I 85889 : 0
|
IGNITER, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
MIL S 81771 : A
|
SEAT SYSTEM; AIRCREW, CRASH RESISTANT; GENERAL SPECIFICATION FOR |
MIL-R-7051 Revision A:1966
|
RELAY BANK, BOMB SALVO CIRCUIT 3 UNIT, 28 VOLT DC TYPE A 1 |
DOD E 8983 : C
|
ELECTRONIC EQUIPMENT, AEROSPACE, EXTENDED SPACE ENVIRONMENT, GENERAL SPECIFICATION FOR |
MIL STD 805 : B
|
TOWING FITTING AND PROVISIONS FOR FIXED WING AIRCRAFT, DESIGN, REQUIREMENTS FOR |
MIL P 83126 : A
|
PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
MIL R 23139 : B
|
ROCKET MOTORS, SURFACE LAUNCHED, DEVELOPMENT AND QUALIFICATION REQUIREMENTS FOR |
ADS-13F-HDBK : 1997
|
AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES |
MIL T 18232 : B
|
TARGET, AERIAL, POWERED, DESIGN AND CONSTRUCTION OF GENERAL SPECIFICATION FOR |
JSSG 2010 12 : 0
|
CREW SYSTEMS DEPLOYABLE AERODYNAMIC DECELERATOR (DAD) SYSTEMS HANDBOOK |
MIL S 48405 : 0
|
SHIELDED AND CONFINED MILD DETONATING CORD ASSEMBLIES |
MIL C 18263 : F
|
COLOR, EXTERIOR, NAVAL AIRCRAFT, REQUIREMENTS FOR |
MIL T 81838 : 0
|
TANK, FUEL, AIRCRAFT, AUXILIARY EXTERNAL 300 GALLON, TYPE AERO 1D |
MIL W 18326 : A
|
WELDING OF MAGNESIUM ALLOYS, GAS AND ARC, MANUAL AND MACHINE PROCESSES FOR |
DOD HDBK 343 : 0
|
DESIGN, CONSTRUCTION, & TESTING REQUIREMENTS FOR ONE OF A KIND SPACE EQUIPMENT |
MIL HDBK 1568 : 0
|
MATERIAL AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN AEROSPACE WEAPONS SYSTEMS |
MIL D 83753 : NOTICE 2
|
DISPENSER, BOMB, TYPE SUU-21/A |
MIL-I-8672 Revision B:1969
|
INSTALLATION AND TEST OF AIRCRAFT PYROTECHNIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR [ASG] |
MIL C 8779 : E
|
COLOR, INTERIOR, AIRCRAFT, REQUIREMENTS FOR |
MIL T 5955 : C
|
TRANSMISSION SYSTEM, VTOL-STOL GENERAL REQUIREMENTS FOR |
MIL-W-5013 Revision L:1991
|
WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR |