MIL-I-6868 Revision E:1976
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
INSPECTION PROCESS, MAGNETIC PARTICLE
Available format(s)
PDF
Superseded date
23-07-2013
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.Describes magnetic particle inspection.
| DocumentType |
Standard
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| Pages |
25
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Superseded
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| Standards | Relationship |
| SAE AMS2640K | Similar to |
| MIL I 6870 : E | INSPECTION PROGRAM REQUIREMENTS NONDESTRUCTIVE FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS |
| MIL-F-63428 Base Document:1981 | 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 Revision B:1988 | ASSEMBLIES, MOVING MECHANICAL, FOR SPACE AND LAUNCH VEHICLES, GENERAL SPECIFICATION FOR |
| MIL-P-60596 Revision B:1990 | PROJECTILE, HE, 8 INCH M106 METAL PARTS ASSEMBLY |
| MIL-W-63071 Revision A:1980 | WARHEAD, FOR DEMOLITION KIT, M180 METAL PARTS FOR |
| MIL P 64008 : 0 | PROJECTILE, 155MM: XM825 METAL PARTS ASSEMBLY |
| MIL-P-50345 Revision F:1994 | PROJECTILES,155MM:M483A1-M718/M741-M692/M731 METAL PARTS ASSEMBLY |
| MIL-L-28654 Revision C:1988 | LIFTING, LAUNCHING AND SIDE CARRYING EQUIPMENT FOR PONTOONS ON 1179 CLASS LST VESSELS |
| MIL-S-83030 Revision A:1968 | STEEL ALLOY, CARBURIZING, BARS AND BILLETS, STEEL NICKEL-CHROMIUM (3310, 3316, AND 9310), PREMIUM QUALITY |
| MIL-L-50794 Base Document:1973 | Linear Shaped Charge Assembly |
| NASA KSC SPEC Z 0013 : 1969 | PENETRANT, MAGNETIC PARTICLE AND ULTRASONIC INSPECTION REQUIREMENTS FOR, SPECIFICATION FOR |
| MIL-S-45933 Base Document:1971 | 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 Revision C:1967 | 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 Revision A:1957 | WELDING, METAL ARC AND GAS STEELS AND CORROSION AND HEAT RESISTANT ALLOYS PROCESS FOR |
| MIL-R-81841 Base Document:1972 | ROTARY FLAP PEENING OF METAL PARTS |
| MIL-STD-1943 Base Document:1985 | 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-P-5673 Revision D:1983 | PIN, STRAIGHT HEADED |
| MIL-B-8907 Revision A:1983 | BOLT, ALLOY STEEL, SHEAR AND TENSILE (156 KSI FSU AND 260 KSI FTU, 450 DEGREE F) EXTERNAL WRENCHING, FLANGED HEAD |
| MIL-U-3963 Revision A:1958 | UNIVERSAL JOINT, ANTIFRICTION BEARINGS |
| MIL-STD-1312-9 Revision A:1984 | FASTENER TEST METHODS - METHOD 9, STRESS CORROSION |
| MIL BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
| MIL-B-83050 Revision D:1985 | BOLT, SELF RETAINING, IMPEDANCE TYPE |
| MIL-S-7839 Revision B:1973 | SCREW, STRUCTURAL, AIRCRAFT |
| MIL I 45910 : C | INSERT, SCREW THREAD LOCKED IN & RING LOCKED 1 SERRATED GENERAL SPECIFICATION FOR |
| MIL-T-81364 Base Document:1966 | T-BOLT, 180,000 PSI TYPE 431 STAINLESS STEEL, MANUFACTURING PROCESS REQUIREMENTS |
| DOD-STD-1312-111 Base Document:1984 | FASTENER TEST METHODS, METRIC METHOD 111, TENSION FATIGUE |
| MIL-H-8775 Revision D:1976 | HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR |
| MIL-STD-1312-11 Revision A:1984 | FASTENER TEST METHODS, METHOD 11, TENSION AND FATIGUE |
| MIL-B-8831 Revision B:1982 | BOLT, 180 KSI FTU AND 180 KSI FSU 450 DEG F PROTRUDING AND FLUSH HEAD, GENERAL SPECIFICATION FOR |
| MIL-W-45595 Revision D:1985 | WASHER, RECESSED, SADDLE AND SHOULDERED METAL |
| 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 |
| MIL-STD-1312-5 Revision A:1984 | FASTENER TEST METHODS, METHOD 5, STRESS DURABILITY |
| 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 Base Document:1977 | WEAPONS AND SUPPORT MATERIAL STANDARD QUALITY ASSURANCE PROVISIONS FOR |
| DOD-I-63274 Revision A:1983 | Insert, Screw Thread-Thin Wall, Locked in, Metric, General Specification for |
| MIL-F-29419 Base Document:1985 | FRAME, SHIPPING [SIXCON] |
| MIL-I-45934 Base Document:1971 | 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 Base Document:1976 | ADJUSTER, LAP BELT, 1-3/4 INCH WEBBING |
| MIL-A-45940 Base Document:1971 | ARMAMENT SUBSYSTEM, HELICOPTER, 7.62 MM MACHINE GUN: DOOR MOUNTED, LIGHT WEIGHT, M24 (LESS M60D MACHINE GUN) |
| MIL-S-12515 Revision C:1983 | SURFACE HARDENING, FLAME AND INDUCTION (FOR FERROUS ALLOYS) |
| MIL-M-47230 Base Document:1974 | MAGNETIC PARTICLE INSPECTION: SOUNDNESS REQUIREMENTS FOR MATERIALS, PARTS, AND WELDMENTS |
| MIL-P-60601 Revision B:1981 | PROJECTILE, 105MM, WP, M416 METAL PARTS ASSEMBLY |
| MIL-S-8512 Revision D:1974 | SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF |
| MIL-S-7108 Revision A:1955 | STEEL, ALLOY (MANGANESE SILICON NICKEL) BARS AND FORGING STOCK (AIRCRAFT QUALITY) (ASG) |
| MIL-H-8890 Base Document:1961 | 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 MA2005B | Tube Fittings, Aerospace Fluid Systems, Separable, For 24° Cone, General Specification, Metric (ISO 7169) |
| MIL-V-5527 Revision A:1951 | VALVE, AIRCRAFT, HYDRAULIC THERMAL EXPANSION RELIEF |
| SAE AMSR81841 | Rotary Flap Peening of Metal Parts |
| MIL-P-50398 Base Document:1979 | PROJECTILE, 165MM, TP M624, METAL PARTS |
| DOD-N-70333 Base Document:1985 | 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 Base Document:1971 | FIN & CLOSURE ASSEMBLY FOR ROCKET MOTOR 2.75 INCH SR 105 PARTS OF |
| MIL-P-45971 Base Document:1975 | PRODUCT ENGINEERING QUALITY ENGINEERING SYSTEM (PEQES) FOR WEAPONS AND SUPPORT MATERIAL |
| MIL-STD-1252 Base Document:1975 | INERTIA FRICTION WELDING PROCESS, PROCEDURE AND PERFORMANCE QUALIFICATION |
| MIL-P-81985 Base Document:1974 | PEENING OF METALS |
| MIL-H-85042 Revision A:1983 | HOOKS, BOMB RACK, GENERAL SPECIFICATION FOR |
| NASA KSC SPEC Z 0001 : 1975 | SPECIFICATION FOR PIPE, 36% NICKEL, IRON-BASE (INVAR 36) |
| MIL-S-81054 Revision A:1976 | STEEL, BARS AND FORGINGS, CHROMIUM NICKEL MOLYBDENUM VANADIUM (FOR TORPEDO MK 46 MOD O) |
| MIL-H-53062 Base Document:1986 | 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 Base Document:1989 | SLING, MULTI LEG, HELICOPTER, EXTERNAL CARGO |
| MIL-S-6049 Revision A:1967 | 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 AMSP81985 | Peening of Metals |
| SAE AMSS7108B | Steel, Alloy (Manganese-Silicon-Nickel), Bars and Forging Stock (Aircraft Quality) |
| SAE AS39631A | Univeral Joint, Antifriction Bearings |
| SAE AMSS6098A | 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 AMST5066A | Tubing, Carbon Steel (1025), (Aircraft Quality) |
| MIL S 18728 : D | STEEL PLATE, SHEET, AND STRIP, ALLOY, 8630, AIRCRAFT QUALITY |
| MIL-T-5684 Revision B:1981 | TIE RODS; ROUND AND SQUARE, AIRCRAFT |
| DOD-S-63275 Revision A:1982 | STUD, SCREW THREAD, LOCKED IN, RING LOCKED, SERRATED, METRIC AND RING LOCK SERRATED METRIC, GENERAL SPECIFICATION FOR |
| MIL-B-8948 Revision A:1972 | Bearing, Plain, Rod End, TFE Lined, Self-Aligning |
| MIL-S-6050 Revision A:1967 | Steel, Chrome-Nickel-Molybdenum (8630) Bars and Reforging Stock (Aircraft Quality) |
| MIL-S-5000 Revision E:1982 | 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 Revision A:1957 | RESERVOIRS, AIR, NONSHATTERABLE STEEL |
| MIL-B-87167 Base Document:1985 | BELT, AIRCRAFT SAFETY, HBU-12/A |
| MIL-N-58106 Base Document:1982 | NET, HELICOPTER CARGO CARRYING EXTERNAL 5,000 AND 10,000 POUND CAPACITIES |
| GGG-B-440 Revision B:1964 | Blade, Circular Saw, Woodcutting |
| MIL-R-85363 Base Document:1981 | Rocket Motor Mark 23 Mods 2 & 3 |
| MIL-S-8503 Revision B:1978 | STEEL BARS, CHROME-VANADIUM (6150) AIRCRAFT QUALITY |
| MIL-S-6098 Revision A:1967 | STEEL, CHROME-NICKEL-MOLYBDENUM [8735] BARS AND REFORGING STOCK [AIRCRAFT] |
| MIL-I-46175 Revision A:1983 | |
| MIL-P-83126 Revision A:1980 | PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
| MIL-W-48274 Base Document:1974 | WARHEAD SECTION, GM, TRAINING, XM201 PARTS AND ASSEMBLING |
| MIL-S-48405 Base Document:1973 | Shielded and Confined Mild Detonating Cord Assemblies |
| MIL-S-38399 Revision A:1975 | STARTER, PNEUMATIC, AIRCRAFT ENGINE GENERAL SPECIFICATION FOR |
| MIL A 8897 : A | ACCUMULATORS, HYDRAULIC CYLINDRICAL, 3,000 PSI AIRCRAFT TYPE 11 SYSTEMS |
| MIL-R-50754 Base Document:1996 | ROCKET MOTOR XM119 METAL PARTS ASSEMBLY |
| MIL-D-63516 Base Document:1981 | 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 Revision B:1994 | WASHERS, SPRING TENSION, METRIC, GENERAL SPECIFICATION FOR |
| DOD-I-63276 Revision A:1983 | INSERT, SCREW THREAD, LOCKED IN, RING LOCKED, SERRATED, METRIC AND RING LOCK SERRATED METRIC |
| MIL-A-45941 Base Document:1971 | ARMAMENT SUBSYSTEM, HELICOPTER, 7.62 MM MACHINE GUN: DOOR MOUNTED, LIGHT WEIGHT, M23 (LESS M60D MACHINE GUN) |
| MIL-W-48271 Revision A:1984 | WARHEAD METAL PARTS ASSEMBLY M251 PARTS AND ASSEMBLING |
| MIL-S-7470 Revision A:1975 | 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 Revision A:1980 | WARHEAD SECTION, GM, PRACTICE LIGHTWEIGHT, M252 AND SHIPPING AND STORAGE CONTAINER, XM612, SPARE PARTS FOR |
| MIL-S-63429 Base Document:1981 | SLIDER ASSEMBLY FOR ARMAMENT SUBSYSTEM, HELICOPTER 20MM, M97E1 AND M97E2 |
| MIL W 12133 : D | WASHER, SPRING TENSION GENERAL SPECIFICATION FOR |
| MIL-S-8690 Revision B:1978 | STEEL, CHROME NICKEL MOLYBDENUM 8620, BARS AIRCRAFT QUALITY |
| MIL-M-29417 Base Document:1984 | MODULE, FUEL PUMP [SIXCON] |
| MIL-A-45947 Base Document:1972 | ARMAMENT SUBSYSTEM, HELICOPTER, 7.62 MM MACHINE GUN: RAMP MOUNTED, LIGHT WEIGHT, M41 (LESS M60D MACHINE GUN) |
| MIL-B-85107 Revision B:1988 | BEARING, SPIN (SIDEWINDER) |
| MIL-E-8697 Revision E:1972 | ELECTRODE, WELDING, COVERED LOW HYDROGEN HEAT TREATABLE STEEL |
| MIL-H-21594 Revision C:1986 | Hookpoint, Aircraft Arresting |
| MIL I 45916 : B | INSERT,SCREW THREAD - THREAD CUTTING AND THREAD FORMING |
| MIL-M-29460 Base Document:1990 | MODULE, WATER PUMP (SIXCON) |
| MIL-T-6736 Revision B:1965 | TUBING, CHROME MOLYBDENUM 4130 STEEL, SEAMLESS, AIRCRAFT QUALITY [ASG] |
| DOD-N-63548 Base Document:1982 | NUT, PLAIN, HEXAGON, WHEEL MOUNTING, METRIC, GENERAL SPECIFICATION FOR |
| MIL-S-6709 Revision A:1965 | 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 Revision E:1984 | 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 Base Document:1981 | 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 Revision B:1958 | 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 Base Document:1981 | NUT, PLAIN, WELDING, GENERAL SPECIFICATION FOR, METRIC |
| DOD-STD-35-126 Base Document:1978 | 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 AMSS6050B | Steel, Chrome-Nickel-Molybdenum (8630) Bars and Reforging Stock (Aircraft Quality) |
| VV K 220 : LATEST | KEROSENE, WATER-WHITE, DEODORIZED (FOR USE IN INSECTISIDES) |
| SAE AMS 3040 : 2014 | MAGNETIC PARTICLES, NONFLUORESCENT, DRY METHOD |
| SAE AMS3045E | Magnetic Particles, Fluorescent Wet Method, Oil Vehicle, Ready-to-Use |
| MIL-STD-410 Revision E:1991 | NONDESTRUCTIVE TESTING PERSONNEL QUALIFICATION AND CERTIFICATION (EDDY CURRENT, LIQUID PENETRANT, MAGNETIC PARTICLE, RADIOGRAPHIC AND ULTRASONIC) |
| SAE AMS3042E | Magnetic Particles, Nonfluorescent Wet Method, Dry Powder |
| SAE AMS3043D | Magnetic Particles, Nonfluorescent Wet Method, Oil Vehicle, Aerosol Packaged |
| AWS A2.2 : LATEST | REPLACED |
| SAE AMS2301K | Steel Cleanliness, Aircraft Quality Magnetic Particle Inspection Procedure |
| SAE AMS3041E | Magnetic Particles, Nonfluorescent Wet Method, Oil Vehicle, Ready-to-Use |
| SAE AMS 3044G : 2014 | MAGNETIC PARTICLES, FLUORESCENT, WET METHOD, DRY POWDER |
| MIL I 6870 : E | INSPECTION PROGRAM REQUIREMENTS NONDESTRUCTIVE FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS |
| SAE AMS2303F | Steel Cleanliness, Aircraft Quality Martensitic Corrosion-Resistant Steels Magnetic Particle Inspection Procedure |
| MIL C 45662 : 0 | CALIBRATION SYSTEM REQUIREMENTS |
| MIL-L-9909 Revision A:1985 | LIGHT, ULTRAVIOLET, METALS EXAMINING |
| SAE AMS2300L | Steel Cleanliness, Premium Aircraft-Quality Magnetic Particle Inspection Procedure |
| MIL-M-6867 Revision C:1969 | MAGNETIC INSPECTION UNITS |
| SAE AMS3046F | Magnetic Particles, Fluorescent Wet Method, Oil Vehicle, Aerosol Packaged |
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