|
MIL-S-26547 Revision C:1985
|
STARTER-GENERATOR ENGINE STU-6A
|
|
MIL-F-63428 Base Document:1981
|
FEED ASSEMBLY, AMMO FOR ARMAMENT SUBSYSTEM, HELICOPTER, 20MM, M97E1 AND M97E2
|
|
MIL-E-23001 Revision B:1976
|
ELECTRIC GENERATING SYSTEM, VARIABLE SPEED CONSTANT FREQUENCY, AIRCRAFT, GENERAL SPECIFICATION FOR
|
|
MIL T 6396 : E
|
TANKS, AIRCRAFT PROPULSION FLUID SYSTEM, INTERNAL REMOVABLE, NON-SELF-SEALING
|
|
MIL-W-63328 Base Document:1979
|
WARHEAD GM, HE, M248 INERT PARTS FOR
|
|
MIL-Q-45970 Revision A:1975
|
QUALITY ASSURANCE FOR WEAPONS AND SUPPORT MATERIAL
|
|
MIL-S-22141 Revision B:1976
|
STEEL, INVESTMENT CASTINGS ALLOY AND CARBON
|
|
MIL-A-23121 Revision C:1970
|
AIRCREW ENVIRONMENTAL, ESCAPE AND SURVIVAL COCKPIT CAPSULE SYSTEM, GENERAL SPECIFICATION FOR
|
|
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
|
|
MIL F 9490 : D
|
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
|
|
MIL-W-63150 Base Document:1977
|
WEAPONS AND SUPPORT MATERIAL STANDARD QUALITY ASSURANCE PROVISIONS FOR
|
|
MIL-STD-2156 Base Document:1983
|
LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR
|
|
MIL F 16377 : G
|
FIXTURE, LIGHTING, INCANDESCENT, GENERAL LIGHTING 100 WATTS, 120 VOLTS, DRIPPROOF 15 DEGREES, SYMBOLS 89 & 90.2
|
|
MIL-A-19736 Revision A:1960
|
AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR
|
|
QQ-A-596 Revision E:1981
|
ALUMINUM ALLOY PERMANENT AND SEMI-PERMANENT MOLD CASTINGS
|
|
MIL S 867 : A
|
STEEL CASTING, CORROSION RESISTING AUSTENITIC
|
|
MIL V 7899 : C
|
VALVE, CHECK, AIRCRAFT FUEL SYSTEM
|
|
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-S-8512 Revision D:1974
|
SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF
|
|
MIL L 38671 : A
|
LUG, SUSPENSION, BOMB MAU-129/A, "T" TYPE
|
|
MIL-S-83427 Base Document:1974
|
SURVIVAL KIT CONTAINERS, CNU-129(V)/P AND CNU-130/P
|
|
MIL-STD-789 Revision C:1983
|
CONTRACTOR TECHNICAL INFORMATION CODING OF REPLENISHMENT PARTS
|
|
MIL-S-48303 Base Document:1973
|
SWITCH ASSEMBLY. M167
|
|
MIL-S-85510 Base Document:1981
|
|
|
MIL L 24560 : 0
|
LIGHTS AND GLASSWARE FOR NAVIGATION, SIGNAL AND WARNING, NAVAL SHIPBOARD USE, GENERAL SPECIFICATION FOR
|
|
MIL E 24021 : J NOTICE 1
|
ELECTRIC POWER MONITORS, EXTERNAL, AIRCRAFT
|
|
MIL-P-45971 Base Document:1975
|
PRODUCT ENGINEERING QUALITY ENGINEERING SYSTEM (PEQES) FOR WEAPONS AND SUPPORT MATERIAL
|
|
SAE AMS 5348 : 2017
|
STEEL CASTINGS, TUBULAR, CENTRIFUGAL, CORROSION RESISTANT, 15CR - 4.6NI - 0.22 (CB+TA) - 2.8CU, SOLUTION HEAT TREATED
|
|
MIL-P-5238 Revision C:1974
|
PUMP, CENTRIFUGAL, FUEL BOOSTER, AIRCRAFT, GENERAL SPECIFICATION FOR
|
|
MIL G 6162 : B
|
GENERATOR AND STARTER GENERATOR, ELECTRIC DIRECT CURRENT, NOMINAL 30 VOLTS AIRCRAFT GENERAL SPECIFICATION
|
|
JSSG-2006 Base Document:1998
|
JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES
|
|
MIL H 24653 : 0
|
HASP, HIGH SECURITY, SHROUDED FOR SHIPBOARD DOORS AND HATCHES USING HIGH AND MEDIUM SECURITY PADLOCK
|
|
MIL-S-58095 Revision A:1986
|
SEAT SYSTEM: CRASH RESISTANCE, NON-EJECTION, AIRCREW, GENERAL SPECIFICATION FOR
|
|
MIL-B-87167 Base Document:1985
|
BELT, AIRCRAFT SAFETY, HBU-12/A
|
|
MIL-I-83751 Base Document:1967
|
INDICATOR, SAFETY LEVEL, RF
|
|
MIL-A-25896 Revision E:1983
|
ADAPTER, PRESSURE FUEL SERVICING, NOMINAL 2.5 INCH DIAMETER
|
|
MIL-E-85583 Revision A:1987
|
ELECTRIC POWER GENERATING CHANNEL, VARIABLE INPUT SPEED, ALTERNATING CURRENT, 400 HZ, AIRCRAFT, GENERAL SPECIFICATION FOR
|
|
MIL-P-83126 Revision A:1980
|
PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR
|
|
MIL-S-38399 Revision A:1975
|
STARTER, PNEUMATIC, AIRCRAFT ENGINE GENERAL SPECIFICATION FOR
|
|
MIL-D-63516 Base Document:1981
|
DRIVE ASSEMBLY, GUN FOR ARMAMENT SUBSYSTEM, HELICOPTER, 20MM, M97E1 AND M97E2
|
|
MIL-F-8615 Revision D:1976
|
FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG]
|
|
MIL-S-7470 Revision A:1975
|
SHAFT, POWER TRANSMISSION, AIRCRAFT ACCESSORY, GENERAL SPECIFICATION FOR
|
|
MIL-S-63429 Base Document:1981
|
SLIDER ASSEMBLY FOR ARMAMENT SUBSYSTEM, HELICOPTER 20MM, M97E1 AND M97E2
|
|
MIL-W-18326 Revision A:1956
|
WELDING OF MAGNESIUM ALLOYS, GAS AND ARC, MANUAL AND MACHINE PROCESSES FOR
|
|
MIL-R-46509 Revision A:1982
|
ROCKET MOTOR, XM30, METAL PARTS FOR
|
|
MIL-P-85315 Base Document:1979
|
Pump, Ejector, Air Vehicle Fuel, General Specification For
|
|
NASA MSFC STD 506 : 1988
|
MATERIALS AND PROCESSES CONTROL
|
|
DOD-C-85050 Base Document:1982
|
CHARGERS, BATTERY, NICKEL-CADMIUM, AIRCRAFT, GENERAL SPECIFICATION FOR
|
|
QQ-A-601 Revision F:1981
|
ALUMINUM ALLOY SAND CASTINGS
|
|
MIL-A-81724 Base Document:1969
|
ADAPTER, LAUNCHER, AIRCRAFT, ADU-299/E
|
|
SAE AMS S 22141 : 1998
|
STEEL, INVESTMENT CASTINGS - ALLOY AND CARBON
|
