MIL-I-6868 Revision E:1976
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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 (S/S by MIL-STD-1949)
08-03-1976
23-07-2013
Describes magnetic particle inspection.
| DocumentType |
Standard
|
| Pages |
25
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
This specification covers general requirements and tests for performing magnetic particle inspection.
| 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 30,000-60,000 Psi |
| MIL-A-83577 Revision B:1988 | Assemblies, Moving Mechanical, for Space and Launch Vehicles, General Specification for (No S/S Document) |
| MIL-P-60596 Revision B:1990 | Projectile, HE, 8 Inch M106 Metal Parts Assembly (No S/S Document) |
| 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 - M718A1/M741A1 - M692/M731 Metal Parts Assembly |
| MIL-L-28654 Revision C:1988 | Lifting, Launching, and Side Carrying Equipment for Pontoons on 1179 Class LST Vessels (S/S by A-L-2924) |
| MIL-S-83030 Revision A:1968 | Steel Alloy, Carburizing, Bars and Billets, Steel Nickel-Chromium (3310, 3316, and 9310), Premium Quality (See Notice 4 for Replacement Information) |
| 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 (NO S/S DOCUMENT) |
| 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 (S/S BY MIL-W-63150) |
| MIL-E-6843 Revision C:1967 | Electrodes, Welding Covered, Low-Alloy Steel (Primarily for Aircraft and Weapon Applications) (S/S by AWS-A5.5) |
| 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 (S/S BY MIL-STD-2219) |
| MIL-R-81841 Base Document:1972 | Rotary Flap Peening of Metal Parts (S/S by SAE-AMS2590) |
| MIL-STD-1943 Base Document:1985 | WELDING REPAIR OF STEEL CASTINGS (OTHER THAN ARMOR) METAL-ARC, MANUAL (S/S BY ASTM-A488/A488M) |
| DOD N 70329 : 0 | NUT, PLAIN, ROUND, BALL AND ROLLER BEARINGS, METRIC, GENERAL SPECIFICATION FOR |
| MIL-P-5673 Revision D:1983 | PIN, STRAIGHT, HEADED (S/S BY NASM5673) |
| MIL-B-8907 Revision A:1983 | Bolt, Alloy Steel, Shear and Tensile (156 KSI FSU and 260 KSI FTU, 450 Degrees F) External Wrenching, Flanged Head (S/S by NASM8907) |
| MIL-U-3963 Revision A:1958 | UNIVERSAL JOINT, ANTIFRICTION BEARINGS |
| MIL-STD-1312-9 Revision A:1984 | FASTENER TEST METHODS METHOD 9, STRESS CORROSION (S/S BY NASM1312-9) |
| MIL BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
| MIL-B-83050 Revision D:1985 | Bolt, Self-Retaining, Impedance Type (S/S by NASM83050) |
| MIL-S-7839 Revision B:1973 | SCREW, STRUCTURAL, AIRCRAFT (S/S BY NASM7839) |
| 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 (NO S/S DOCUMENT) |
| DOD-STD-1312-111 Base Document:1984 | FASTENER TEST METHODS, METRIC METHOD 111 TENSION FATIGUE (S/S BY NAM1312-111) |
| MIL-H-8775 Revision D:1976 | Hydraulic System Components, Aircraft and Missiles General Specification for (S/S by SAE-AS8775) |
| MIL-STD-1312-11 Revision A:1984 | FASTENER TEST METHODS METHOD 11, TENSION FATIGUE (S/S BY NASM1312-11) |
| MIL-B-8831 Revision B:1982 | Bolt, 180 KSI FTU and 180 KSI FSU, 450 Degrees F Protruding and Flush Head, General Specification for (S/S by NASM8831) |
| MIL-W-45595 Revision D:1985 | Washers, Shouldered, Recessed, Saddle, Concave and Convex (S/Sby NASM45595) |
| MIL-N-8984 Base Document:1972 | NUT, SELF-LOCKING, STEEL, 260 KSI FTU, 450 DEG. F (S/S BY NASM8984) |
| MIL-N-8985 Base Document:1972 | NUT, SELF LOCKING STEEL, 180 KSI FTU, 450 DEGREE F (S/S BY NASM8985) |
| MIL-STD-1312-5 Revision A:1984 | FASTENER TEST METHODS METHOD 5, STRESS DURABILITY (S/S BY NASM1312-5) |
| 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 Materiel 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)(No S/S Document) |
| 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 (No S/S Document) |
| 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 (No S/S Document) |
| MIL-A-45940 Base Document:1971 | Armament Subsystem, Helicopter, 7.62MM Machine Gun, door Mounter, 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 (S/S BY MIL-STD-1907) |
| MIL-P-60601 Revision B:1981 | PROJECTILE, 105MM, WP, M416 METAL PARTS ASSEMBLY (NO S/S DOCUMENT) |
| 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) (S/S BY SAE-AMS6425) |
| MIL-H-8890 Base Document:1961 | Hydraulic Components, Type III (-65 Degrees to Plus 450 Degrees F) General Specification for (ASG) |
| MIL-P-8564 Revision D:1970 | Pneumatic System Components, Aeronautical, General Specification for |
| 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 | VALVES, 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 (No S/S Document) |
| DOD P 63245 : A (2) | PROJECTILE, HE, 155MM, XM795 METAL PARTS ASSEMBLY |
| MIL-F-50877 Base Document:1971 | Fin and Closure Assembly for Rocket Motor 2.75 Inch, SR 105, Parts for (No S/S Document) |
| MIL-P-45971 Base Document:1975 | Product Engineering Quality Engineering System (PEQES),for Weaponsand Support Materiel (No S/S Document) |
| 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 0) |
| MIL-H-53062 Base Document:1986 | Hose Assembly, Rubber, Lightweight, Collapsible 6 Inch for POL Service (S/S MIL-H-0053073) |
| 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 (No S/S Document) |
| MIL-S-58112 Base Document:1989 | SLING, MULTI-LEG, HELICOPTER, EXTERNAL CARGO (NO S/S DOCUMENT) |
| MIL-S-6049 Revision A:1967 | STEEL, CHROME-NICKEL-MOLYBDENUM (8740) BARS AND REFORGING STOCK (AIRCRAFT QUALITY) (S/S BY SAE-AMS6322, SAE-AMS6325 AND SAE-AMS6327) |
| 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 | RODS AND WIRE, STEEL, WELDING (FOR AIRCRAFT APPLICATIONS) (S/S BY SAE-AMS6457, SAE-AMS6452, SAE-AMS6456, SAE-AMS6459, SAE-AMS6331, SAE-AMS6461, SAE-AMS6462, SAE-AMS6458, SAE-AMS5027 AND SAE-AMS5028) |
| 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 Rod: Round and Square, Aircraft (No S/S Document) |
| DOD-S-63275 Revision A:1982 | Stud, Screw Thread, Locked in, Ring Locked, Serrated, Metric and Ring, Lock, Serrated, Metric, General Specification for (No S/S Document) |
| 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) (Future acquisitions for this material should refer to SAE-AMS6280) |
| MIL-S-5000 Revision E:1982 | STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS, AND FORGING STOCK (S/S BY SAE-AMS-S-5000) |
| MIL-P-14825 Revision A:1972 | Projectile, 152mm, Heat, M409 Metal Parts, Less Fluted Liner |
| MIL-R-8573 Revision A:1957 | Reservoir, 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 (NO S/S DOCUMENT) |
| 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) (ASG) (S/S BY SAE-AMS6448) |
| MIL-S-6098 Revision A:1967 | STEEL, CHROME-NICKEL-MOLYBDENUM (8735) BARS AND REFORGING STOCK (AIRCRAFT) (S/S BY SAE-AMS-S-6098) |
| MIL-I-46175 Revision A:1983 | Inspection and Testing of Ductile Cast Iron Grade 100-70-03, Ultrasonic (No S/S Document) |
| 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 (No S/S Document) |
| 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 (No S/S Document) |
| 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 (NO S/S DOCUMENT) |
| 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 (No S/S Document) |
| 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, General Specification for |
| MIL-A-45941 Base Document:1971 | Armament Subsystem, Helicopter, 7.62MM 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 (No S/S Document) |
| 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 (S/S BY SAE-AMS6274) |
| MIL-M-29417 Base Document:1984 | Module, Fuel Pump (SIXCON) (No S/S Document) |
| MIL-A-45947 Base Document:1972 | Armament Subsystem, Helicopter, 7.62MM Machine Gun: Ramp Mounted, Light Weight, M41 (Less M60D Machine Gun) |
| MIL-B-85107 Revision B:1988 | Bearing, Spin (Sidewinder) (No S/S Document) |
| MIL-E-8697 Revision E:1972 | Electrodes, Welding, Covered, Low-Hydrogen, Heat-Treatable Steel (No S/S Document) |
| 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) (No S/S Document) |
| MIL-T-6736 Revision B:1965 | TUBING, CHROME-MOLYBDENUM, 4130 STEEL, SEAMLESS AND WELDED, AIRCRAFT QUALITY (USERS MAY REFER TO SAE-AMS-T-6736) AS A POSSIBLE REPLACEMENT) |
| DOD-N-63548 Base Document:1982 | Nut, Plain, Hexagon, Wheel Mounting, Metric General Specification for (No S/S Document) |
| MIL-S-6709 Revision A:1965 | STEEL, CHROME-MOLYBDENUM-ALUMINUM; BARS, RODS, BILLETS AND FORGING STOCK (FOR NITRIDING) (AIRCRAFT QUALITY) (S/S BYSAE-AMS6470 AND SAE-AMS6472) |
| MIL-I-83387 Revision A:1982 | Inspection Process, Magnetic Rubber (S/S by SAE-AMS-I-83387) |
| MIL B 51322 : NOTICE 1 | BOMB, FIRE, 500 POUND BLU-11/B |
| WW-T-696 Revision E:1984 | Traps, Steam (S/S by A-A-60001) |
| 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 | Adapter, Recoil Mechanism Armament Subsystem, Helicopter, 20MM, M97E1 and M97E2 |
| MIL-S-8699 Revision A:1957 | STEEL BARS AND FORGING STOCK (4330) VANADIUM MODIFIED, AIRCRAFT QUALITY (S/S BY SAE-AMS6411 AND SAE-AMS6427) |
| MIL-S-7420 Revision B:1958 | STEEL BARS, ALLOY, CHROMIUM, HIGH CARBON E52100 (AIRCRAFT QUALITY) (S/S BY SAE-AMS6440, SAE-AMS6444 AND SAE-AMS6447) |
| MIL-P-50569 Revision C:1982 | Projectile, 155MM, HE, Rocket Assisted M549 Series, Motor Body Bonding Assembling For |
| DOD-N-63476 Base Document:1981 | Nut, Plain, Welding, General Specification for, Metric (No S/S Document) |
| DOD-STD-35-126 Base Document:1978 | Automated Engineering Document Preparation System, Cylinders, Actuating, Linear (No S/S Document) |
| 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 AMS3045E | Magnetic Particles, Fluorescent Wet Method, Oil Vehicle, Ready-to-Use |
| MIL-STD-410 Revision E:1991 | NONDESTRUCTIVE TESTING PERSONNEL QUALIFICATION AND CERTIFICATION (SEE NAS410 AS A POSSIBLE REPLACEMENT) |
| SAE AMS3042E | Magnetic Particles, Nonfluorescent Wet Method, Dry Powder |
| SAE AMS3043D | Magnetic Particles, Nonfluorescent Wet Method, Oil Vehicle, Aerosol Packaged |
| SAE AMS2301K | Steel Cleanliness, Aircraft Quality Magnetic Particle Inspection Procedure |
| SAE AMS3041E | Magnetic Particles, Nonfluorescent Wet Method, Oil Vehicle, Ready-to-Use |
| 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, Metal Examining (No S/S Document) |
| SAE AMS2300L | Steel Cleanliness, Premium Aircraft-Quality Magnetic Particle Inspection Procedure |
| MIL-M-6867 Revision C:1969 | Magnetic Inspection Units (No S/S Document) |
| SAE AMS3046F | Magnetic Particles, Fluorescent Wet Method, Oil Vehicle, Aerosol Packaged |
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