|
MIL I 6870 : E
|
INSPECTION PROGRAM REQUIREMENTS NONDESTRUCTIVE FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS |
|
MIL F 63428 : 0
|
FEED ASSEMBLY, AMMO FOR ARMAMENT SUBSYSTEM, HELICOPTER, 20MM, M97E1 AND M97E2 |
|
MIL-W-21157 Revision A:1971
|
WELDMENT, STEEL, CARBON AND LOW ALLOY (YIELD STRENGTH 3O,OOO - 6O,OOO PS1) |
|
MIL A 83577 : B
|
ASSEMBLIES, MOVING MECHANICAL, FOR SPACE AND LAUNCH VEHICLES, GENERAL SPECIFICATION FOR |
|
MIL P 60596 : B
|
PROJECTILE, HE, 8 INCH M106 METAL PARTS ASSEMBLY |
|
MIL W 63071 : A
|
WARHEAD, FOR DEMOLITION KIT, M180 METAL PARTS FOR |
|
MIL P 64008 : 0
|
PROJECTILE, 155MM: XM825 METAL PARTS ASSEMBLY |
|
MIL P 50345 : F
|
PROJECTILES,155MM:M483A1-M718/M741-M692/M731 METAL PARTS ASSEMBLY |
|
MIL L 28654 : C
|
LIFTING, LAUNCHING AND SIDE CARRYING EQUIPMENT FOR PONTOONS ON 1179 CLASS LST VESSELS |
|
MIL S 83030 : A
|
STEEL ALLOY, CARBURIZING, BARS AND BILLETS, STEEL NICKEL-CHROMIUM (3310, 3316, AND 9310), PREMIUM QUALITY |
|
MIL L 50794 : 0
|
LINEAR SHAPED CHARGE ASSEMBLY |
|
NASA KSC SPEC Z 0013 : 1969
|
PENETRANT, MAGNETIC PARTICLE AND ULTRASONIC INSPECTION REQUIREMENTS FOR, SPECIFICATION FOR |
|
MIL S 45933 : 0
|
STUD, KEYRING LOCKED, 125 AND 160 KSI FTU, GENERAL SPECIFICATION FOR |
|
MIL P 60584 : A
|
PROJECTILE, 155MM, SMOKE, WP, M110 METAL PARTS ASSEMBLY |
|
MIL-Q-45970 Revision A:1975
|
QUALITY ASSURANCE FOR WEAPONS AND SUPPORT MATERIAL |
|
MIL E 6843 : C
|
ELECTRODE, WELDING, COVERED, LOW ALLOY STEEL (PRIMARILY FOR AIRCRAFT AND WEAPON APPLICATIONS) |
|
NASA MSFC STD 1249 : 1985
|
NDE GUIDELINES AND REQUIREMENTS FOR FRACTURE CONTROL PROGRAMS |
|
MIL W 8611 : A
|
WELDING, METAL ARC AND GAS STEELS AND CORROSION AND HEAT RESISTANT ALLOYS PROCESS FOR |
|
MIL R 81841 : 0
|
ROTARY FLAP PEENING OF METAL PARTS |
|
MIL STD 1943 : 0
|
WELDING REPAIR OF STEEL CASTINGS (OTHER THAN ARMOR) METAL-ARC, MANUAL |
|
DOD N 70329 : 0
|
NUT, PLAIN, ROUND, BALL AND ROLLER BEARINGS, METRIC, GENERAL SPECIFICATION FOR |
|
MIL-H-8775 Revision D:1976
|
HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR |
|
DOD STD 1312/9 : LATEST
|
FASTENER TEST METHODS, METRIC, METHOD 9, STRESS CORROSION |
|
MIL F 5508 : B
|
FUSE, AIRCRAFT AUTOMATIC QUANTITY MEASURING HYDRAULIC |
|
MIL W 63150 : 0
|
WEAPONS AND SUPPORT MATERIAL STANDARD QUALITY ASSURANCE PROVISIONS FOR |
|
DOD I 63274 : A
|
INSERT, SCREW THREAD THIN WALL, LOCKED IN, METRIC, GENERAL SPECIFICATION FOR |
|
MIL F 29419 : 0
|
FRAME, SHIPPING [SIXCON] |
|
MIL I 45934 : 0
|
INSERT, SCREW THREAD, KEYRING LOCKED, SELF LOCKING AND NON SELF LOCKING, 125, 180, AND 220 KSI FTU: GENERAL SPECIFICATION FOR |
|
MIL T 38170 : F
|
TANK, MOBILE STORAGE, LIQUID OXYGEN TMU 27/M |
|
MIL A 83469 : 0
|
ADJUSTER, LAP BELT, 1-3/4 INCH WEBBING |
|
MIL A 45940 : 0
|
ARMAMENT SUBSYSTEM, HELICOPTER, 7.62 MM MACHINE GUN: DOOR MOUNTED, LIGHT WEIGHT, M24 (LESS M60D MACHINE GUN) |
|
MIL S 12515 : C
|
SURFACE HARDENING, FLAME AND INDUCTION (FOR FERROUS ALLOYS) |
|
MIL M 47230 : 0
|
MAGNETIC PARTICLE INSPECTION: SOUNDNESS REQUIREMENTS FOR MATERIALS, PARTS, AND WELDMENTS |
|
MIL P 60601 : B
|
PROJECTILE, 105MM, WP, M416 METAL PARTS ASSEMBLY |
|
MIL S 8512 : D
|
SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF |
|
MIL S 7108 : A
|
STEEL, ALLOY (MANGANESE SILICON NICKEL) BARS AND FORGING STOCK (AIRCRAFT QUALITY) (ASG) |
|
MIL H 8890 : 0
|
HYDRAULIC COMPONENTS, TYPE 111 [65 DEGREES TO PLUS 450 DEGREES F] GENERAL SPECIFICATION FOR [ASG] |
|
MIL-P-8564 Revision D:1970
|
PNEUMATIC SYSTEM COMPONENTS, AERONAUTICAL, GENERAL SPECIFICATION FOR [ASG] |
|
MIL R 46259 : A NOTICE 1
|
ROCKET MOTOR, M3A2 PARTS FOR |
|
SAE MA 2005 : 2015
|
TUBE FITTINGS, AEROSPACE FLUID SYSTEMS, SEPARABLE, FOR 24 DEGREE CONE, GENERAL SPECIFICATION, METRIC |
|
MIL V 5527 : A
|
VALVE, AIRCRAFT, HYDRAULIC THERMAL EXPANSION RELIEF |
|
SAE AMS R 81841 : 2001
|
ROTARY FLAP PEENING OF METAL PARTS |
|
MIL P 50398 : 0
|
PROJECTILE, 165MM, TP M624, METAL PARTS |
|
DOD N 70333 : 0
|
NUT, PLAIN AND SELF-LOCKING, CLINCH, METRIC (SELF-CLINCHING, KNURLED COLLAR) FIXED AND FLOATING, GENERAL SPECIFICATION FOR |
|
DOD P 63245 : A (2)
|
PROJECTILE, HE, 155MM, XM795 METAL PARTS ASSEMBLY |
|
MIL F 50877 : 0
|
FIN & CLOSURE ASSEMBLY FOR ROCKET MOTOR 2.75 INCH SR 105 PARTS OF |
|
MIL P 45971 : 0
|
PRODUCT ENGINEERING QUALITY ENGINEERING SYSTEM (PEQES) FOR WEAPONS AND SUPPORT MATERIAL |
|
MIL STD 1252 : 0
|
INERTIA FRICTION WELDING PROCESS, PROCEDURE AND PERFORMANCE QUALIFICATION |
|
MIL P 81985 : 0
|
PEENING OF METALS |
|
MIL H 85042 : A
|
HOOKS, BOMB RACK, GENERAL SPECIFICATION FOR |
|
NASA KSC SPEC Z 0001 : 1975
|
SPECIFICATION FOR PIPE, 36% NICKEL, IRON-BASE (INVAR 36) |
|
MIL S 81054 : A
|
STEEL, BARS AND FORGINGS, CHROMIUM NICKEL MOLYBDENUM VANADIUM (FOR TORPEDO MK 46 MOD O) |
|
MIL H 53062 : 0
|
HOSE ASSEMBLY, RUBBER LIGHTWEIGHT, COLLAPSIBLE 6 INCH; FOR POL SERVICE |
|
MIL-G-10944 Revision B:1965
|
GAGE, DIMENSIONAL CONTROL |
|
MIL-B-45457 Revision A:1969
|
BOMB, FIRE,750-POUND, M116A2 (W/O FUZE COMPONENTS AND FILLING) |
|
MIL S 58112 : 0
|
SLING, MULTI LEG, HELICOPTER, EXTERNAL CARGO |
|
MIL S 6049 : A
|
STEEL, CHROME NICKEL MOLYBDENUM [8740] BARS, RODS AND FORGING STOCK FOR AIRCRAFT APPLICATION |
|
MIL T 6735 : A
|
TUBING, CHROME-MOLYBDENUM, 4135 STEEL, SEAMLESS AIRCRAFT QUALITY |
|
SAE AMS P 81985 : 2001
|
PEENING OF METALS |
|
SAE AMS S 7108 : 2016
|
STEEL, ALLOY (MANGANESE-SILICON-NICKEL), BARS AND FORGING STOCK (AIRCRAFT QUALITY) |
|
SAE AS 39631 : 1999
|
UNIVERSAL JOINT, ANTIFRICTION BEARINGS |
|
SAE AMS S 6098 : 1999
|
STEEL, CHROME-NICKEL-MOLYBDENUM (8735) BARS AND REFORGING STOCK (AIRCRAFT QUALITY) |
|
MIL-R-5632 Revision B:1972
|
ROD, AND WIRE, STEEL WELDING [FOR AIRCRAFT] |
|
SAE AMS T 5066 : 2015
|
TUBING, CARBON STEEL (1025), (AIRCRAFT QUALITY) |
|
MIL S 18728 : D
|
STEEL PLATE, SHEET, AND STRIP, ALLOY, 8630, AIRCRAFT QUALITY |
|
MIL T 5684 : B
|
TIE RODS; ROUND AND SQUARE, AIRCRAFT |
|
DOD S 63275 : A
|
STUD, SCREW THREAD, LOCKED IN, RING LOCKED, SERRATED, METRIC AND RING LOCK SERRATED METRIC, GENERAL SPECIFICATION FOR |
|
MIL B 8948 : A
|
BEARINGS, PLAIN, ROD END, TFE LINED, SELF-ALIGNING |
|
MIL S 6050 : A
|
STEEL, CHROME NICKEL MOLYBDENUM [8630] BARS AND REFORGING STOCK [AIRCRAFT QUALITY] |
|
MIL S 5000 : E
|
STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS AND REFORGING STOCK |
|
MIL-P-14825 Revision A:1972
|
PROJECTILE, 152MM, HEAT, M409 METAL PARTS, LESS FLUTED LINER |
|
MIL R 8573 : A
|
RESERVOIRS, AIR, NONSHATTERABLE STEEL |
|
MIL B 87167 : 0
|
BELT, AIRCRAFT SAFETY, HBU-12/A |
|
MIL N 58106 : 0
|
NET, HELICOPTER CARGO CARRYING EXTERNAL 5,000 AND 10,000 POUND CAPACITIES |
|
GGG B 440 : B
|
BLADE, CIRCULAR SAW, WOODCUTTING |
|
MIL R 85363 : 0
|
ROCKET MOTOR MARK 23 MODS 2 & 3 |
|
MIL S 8503 : B
|
STEEL BARS, CHROME-VANADIUM (6150) AIRCRAFT QUALITY |
|
MIL S 6098 : A
|
STEEL, CHROME-NICKEL-MOLYBDENUM [8735] BARS AND REFORGING STOCK [AIRCRAFT] |
|
MIL I 46175 : A
|
|
|
MIL P 83126 : A
|
PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
|
MIL W 48274 : 0
|
WARHEAD SECTION, GM, TRAINING, XM201 PARTS AND ASSEMBLING |
|
MIL S 48405 : 0
|
SHIELDED AND CONFINED MILD DETONATING CORD ASSEMBLIES |
|
MIL S 38399 : A
|
STARTER, PNEUMATIC, AIRCRAFT ENGINE GENERAL SPECIFICATION FOR |
|
MIL A 8897 : A
|
ACCUMULATORS, HYDRAULIC CYLINDRICAL, 3,000 PSI AIRCRAFT TYPE 11 SYSTEMS |
|
MIL R 50754 : 0
|
ROCKET MOTOR XM119 METAL PARTS ASSEMBLY |
|
MIL D 63516 : 0
|
DRIVE ASSEMBLY, GUN FOR ARMAMENT SUBSYSTEM, HELICOPTER, 20MM, M97E1 AND M97E2 |
|
MIL-P-48323 Revision C:1984
|
PROJECTILE, 8 INCH, HE, RA, M650 ROCKET MOTOR BODY ASSEMBLY |
|
DOD W 63474 : B
|
WASHERS, SPRING TENSION, METRIC, GENERAL SPECIFICATION FOR |
|
DOD I 63276 : A
|
INSERT, SCREW THREAD, LOCKED IN, RING LOCKED, SERRATED, METRIC AND RING LOCK SERRATED METRIC |
|
MIL A 45941 : 0
|
ARMAMENT SUBSYSTEM, HELICOPTER, 7.62 MM MACHINE GUN: DOOR MOUNTED, LIGHT WEIGHT, M23 (LESS M60D MACHINE GUN) |
|
MIL W 48271 : A
|
WARHEAD METAL PARTS ASSEMBLY M251 PARTS AND ASSEMBLING |
|
MIL S 7470 : A
|
SHAFT, POWER TRANSMISSION, AIRCRAFT ACCESSORY, GENERAL SPECIFICATION FOR |
|
MIL-S-63348 Revision A:1981
|
SUBMACHINE GUN, 5.56MM, PORT FIRING, M231 |
|
MIL-S-29398 Revision C:1984
|
SLING SYSTEM, HELICOPTER EXTERNAL CARGO 40,000 POUND CAPACITY |
|
MIL W 48866 : A
|
WARHEAD SECTION, GM, PRACTICE LIGHTWEIGHT, M252 AND SHIPPING AND STORAGE CONTAINER, XM612, SPARE PARTS FOR |
|
MIL S 63429 : 0
|
SLIDER ASSEMBLY FOR ARMAMENT SUBSYSTEM, HELICOPTER 20MM, M97E1 AND M97E2 |
|
MIL W 12133 : D
|
WASHER, SPRING TENSION GENERAL SPECIFICATION FOR |
|
MIL S 8690 : B
|
STEEL, CHROME NICKEL MOLYBDENUM 8620, BARS AIRCRAFT QUALITY |
|
MIL M 29417 : 0
|
MODULE, FUEL PUMP [SIXCON] |
|
MIL A 45947 : 0
|
ARMAMENT SUBSYSTEM, HELICOPTER, 7.62 MM MACHINE GUN: RAMP MOUNTED, LIGHT WEIGHT, M41 (LESS M60D MACHINE GUN) |
|
MIL B 85107 : B
|
BEARING, SPIN (SIDEWINDER) |
|
MIL E 8697 : E
|
ELECTRODE, WELDING, COVERED LOW HYDROGEN HEAT TREATABLE STEEL |
|
MIL H 21594 : C
|
HOOKPOINT, AIRCRAFT ARRESTING |
|
MIL I 45916 : B
|
INSERT,SCREW THREAD - THREAD CUTTING AND THREAD FORMING |
|
MIL M 29460 : 0
|
MODULE, WATER PUMP (SIXCON) |
|
MIL T 6736 : B
|
TUBING, CHROME MOLYBDENUM 4130 STEEL, SEAMLESS, AIRCRAFT QUALITY [ASG] |
|
DOD N 63548 : 0
|
NUT, PLAIN, HEXAGON, WHEEL MOUNTING, METRIC, GENERAL SPECIFICATION FOR |
|
MIL S 6709 : A
|
STEEL, CHROME-MOLYBDENUM-ALUMINUM; BARS, RODS, BILLETS AND FORGING STOCK (FOR NITRIDING) (AIRCRAFT QUALITY) |
|
MIL-I-83387 Revision A:1982
|
INSPECTION PROCESS, MAGNETIC RUBBER |
|
MIL B 51322 : NOTICE 1
|
BOMB, FIRE, 500 POUND BLU-11/B |
|
WW T 696 : E
|
TRAPS, STEAM |
|
MIL W 46132 : NOTICE 4
|
WELDING, FUSION, ELECTRON BEAM, PROCESS FOR |
|
MIL R 5149 : B
|
ROCKET ENGINE, LIQUID PROPELLANT GENERAL SPECIFICATION FOR |
|
MIL R 25532 : A
|
ROCKET MOTOR, AERONAUTICAL, QUALIFICATION TEST FOR |
|
MIL A 63425 : 0
|
ADAPTOR, RECOIL MECHANISM ARMAMENT SUBSYSTEM, HELICOPTER, 20 MM: M97E1 AND M97E2 |
|
MIL-S-8699 Revision A:1957
|
STEEL BARS AND FORGING STOCK [4330] VANADIUM MODIFIED, AIRCRAFT QUALITY |
|
MIL S 7420 : B
|
STEEL BARS, ALLOY, CHROMIUM HIGH CARBON E 52100 [AIRCRAFT QUALITY] |
|
NASM1312-11:2017
|
FASTENER TEST METHODS METHOD 11 TENSION FATIGUE |
|
MIL-P-50569 Revision C:1982
|
PROJECTILE, 155MM, HE, ROCKET ASSISTED M549 SERIES, MOTOR BODY BONDING ASSEMBLY FOR |
|
DOD N 63476 : 0
|
NUT, PLAIN, WELDING, GENERAL SPECIFICATION FOR, METRIC |
|
DOD STD 35/126 : 0
|
AUTOMATED ENGINEERING DOCUMENT PREPARATION SYSTEM, CYLINDERS, ACTUATING, LINEAR |
|
MIL F 38635 : D
|
FIN ASSEMBLY, BOMB, MAU-91A/B AND MAU-91B/B |
|
DOD STD 1312/11 : LATEST
|
FASTENER, TEST METHODS METRIC, METHOD 11, TENSION FATIGUE (S/S BY DOD STD 1312-111) |
|
SAE AMS S 6050 : 1998
|
STEEL, CHROME-NICKEL-MOLYBDENUM (8630) BARS AND REFORGING STOCK (AIRCRAFT QUALITY) |