MIL-M-87113 Revision A:1993
|
MASK, OXYGEN, MBU-10/P |
MIL-I-83294 Base Document:1971
|
INSTALLATION REQUIREMENT, AIRCRAFT PROPULSION SYSTEMS, GENERAL SPECIFICATION FOR |
MIL-T-5842 Revision B:1985
|
TRANSPARENT AREAS ON AIRCRAFT SURFACES [WINDSHIELDS AND CANOPIES] RAIN REMOVING AND WASHING SYSTEMS FOR, DEFROSTING, DEICING, DEFOGGING, GENERAL SPECIFICATION FOR |
MIL-STD-2156 Base Document:1983
|
LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
MIL-A-83577 Revision B:1988
|
ASSEMBLIES, MOVING MECHANICAL, FOR SPACE AND LAUNCH VEHICLES, GENERAL SPECIFICATION FOR |
MIL STD 001303 : C
|
PAINTING OF NAVAL ORDNANCE EQUIPMENT |
MIL-M-8555 Revision C:1984
|
MISSILE, GUIDED, DESIGN AND CONSTRUCTION, GENERAL SPECIFICATION |
MIL-A-85055 Base Document:1979
|
AVIONICS SYSTEM PERFORMANCE SPECIFICATION FOR A-4M/AV-8 BOMBING SET, ANGLE RATE AN/ASB-19(V) |
MIL-R-8236 Revision F:1995
|
REEL, SHOULDER HARNESS, INERTIA LOCK |
MIL-STD-7080 Base Document:1994
|
SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT |
MIL-I-82787 Base Document:1990
|
IGNITER ASSEMBLY, ROCKET MOTOR MK 104 |
MIL-L-50794 Base Document:1973
|
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 Base Document:1980
|
DEVICE, ARMING FIRING, ROCKET MOTOR MARK 298 MOD O |
DOD-E-83578 Revision A:1987
|
EXPLOSIVE ORDNANCE FOR SPACE VEHICLES, GENERAL SPECIFICATION FOR (METRIC) |
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 |
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 |
MIL BULL 343 : A
|
DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
MIL-W-5088 Revision L:1991
|
Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
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 |
MIL-N-8984 Base Document:1972
|
NUT, SELF-LOCKING, STEEL, 260 KS1 FTU 450 DEGREES F |
MIL-N-8985 Base Document:1972
|
NUT, SELF-LOCKING STEEL, 180 KS1 FTU 450 DEGREES F |
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-H-8891 Revision A:1978
|
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 Revision A:1960
|
AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR |
MIL-E-50796 Base Document:1973
|
EXPANDING SHIELDED MILD DETONATING CORD ASSEMBLY |
MIL-STD-1250 Revision A:1992
|
CORROSION PREVENTION AND DETERIORATION CONTROL IN ELECTRONIC COMPONENTS AND ASSEMBLIES |
MIL-M-25047 Revision C:1968
|
MARKINGS AND EXTERIOR FINISH COLORS FOR AIRPLANES, AIRPLANE PARTS, AND MISSILES (BALLISTIC MISSILES EXCLUDED) |
MIL-A-83469 Base Document:1976
|
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 Base Document:1966
|
BLEED AIR SYSTEMS, GENERAL SPECIFICATIONS FOR |
MIL-E-7080 Revision B:1962
|
ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF |
MIL-HDBK-1250 Revision A:1995
|
CORROSION PREVENTION AND DETERIORATION CONTROL IN ELECTRONIC COMPONENTS AND ASSEMBLIES |
MIL-STD-1516 Revision B:1990
|
UNIFIED CODE FOR COATINGS AND FINISHES FOR DOD MATERIAL |
MIL-I-82826 Base Document:1985
|
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 Revision B:1997
|
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 Revision D:1971
|
COATING SYSTEM, EPOXY-POLYAMIDE, CHEMICAL AND SOLVENT RESISTANT, PROCESS FOR APPLICATION OF |
MIL-S-83576 Base Document:1974
|
SOLAR CELL ARRAYS, SPACE VEHICLE, DESIGN AND TESTING, GENERAL SPECIFICATION FOR |
MIL-C-18187 Revision A:1965
|
COATING, PROTECTIVE, APPLICATION TO FABRIC SURFACE OF AIRCRAFT |
MIL-STD-1303 Revision B:1975
|
PAINTING OF NAVAL ORDNANCE EQUIPMENT |
MIL-I-8673 Base Document:1955
|
INSTALLATION AND TEST OF AIRCRAFT FLEXIBLE WEAPONS SYSTEMS |
MIL-C-81907 Base Document:1972
|
COATING SYSTEM, POLYURETHANE, ALIPHATIC, WEATHER RESISTANT, PROCESS FOR APPLICATION OF |
MIL-C-8507 Revision D:1963
|
Coating, Wash Primer (Pretreatment) for Metals, Application of (for Aeronautical Use) |
MIL-I-8700 Revision A:1970
|
INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
JSSG-2006 Base Document:1998
|
JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
MIL-I-85889 Base Document:1988
|
IGNITER, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
MIL-S-81771 Revision A:1975
|
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 Revision C:1977
|
ELECTRONIC EQUIPMENT, AEROSPACE, EXTENDED SPACE ENVIRONMENT, GENERAL SPECIFICATION FOR |
MIL-STD-805 Revision B:1987
|
TOWING FITTING AND PROVISIONS FOR FIXED WING AIRCRAFT, DESIGN, REQUIREMENTS FOR |
MIL-P-83126 Revision A:1980
|
PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
MIL-R-23139 Revision B:1965
|
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 Revision B:1968
|
TARGET, AERIAL, POWERED, DESIGN AND CONSTRUCTION OF GENERAL SPECIFICATION FOR |
JSSG-2010-12 Base Document:1998
|
Crew Systems Deployable Aerodynamic Decelerator (DAD) Systems Handbook |
MIL-S-48405 Base Document:1973
|
Shielded and Confined Mild Detonating Cord Assemblies |
MIL-C-18263 Revision F:1971
|
COLOR, EXTERIOR, NAVAL AIRCRAFT, REQUIREMENTS FOR |
MIL-T-81838 Base Document:1971
|
TANK, FUEL, AIRCRAFT, AUXILIARY EXTERNAL 300 GALLON, TYPE AERO 1D |
MIL-W-18326 Revision A:1956
|
WELDING OF MAGNESIUM ALLOYS, GAS AND ARC, MANUAL AND MACHINE PROCESSES FOR |
DOD-HDBK-343 Base Document:1986
|
DESIGN, CONSTRUCTION, & TESTING REQUIREMENTS FOR ONE OF A KIND SPACE EQUIPMENT |
MIL-HDBK-1568 Base Document:1996
|
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 Revision E:1988
|
COLOR, INTERIOR, AIRCRAFT, REQUIREMENTS FOR |
MIL-T-5955 Revision C:1970
|
TRANSMISSION SYSTEM, VTOL-STOL GENERAL REQUIREMENTS FOR |
MIL-W-5013 Revision L:1991
|
WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR |