MIL-STD-453 Revision C:1984
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
INSPECTION, RADIOGRAPHIC
Available format(s)
PDF
Superseded date
12-12-1996
Publisher
1. SCOPE
1.1 Purpose
1.2 Application
2. REFERENCED DOCUMENTS
2.1 Issue of documents
2.2 Other publications
3. DEFINITIONS
3.1 Component
3.2 Contracting agency
3.3 Definition
3.4 Densitometer
3.5 Energy
3.6 Film holders or cassettes
3.7 Filters
3.8 Government Procurement Agency
3.9 Intensifying screen
3.10 NDT facility
3.11 Masking
3.12 Material thickness
3.13 Maximum effective radiation source dimension
3.14 Multiple film technique
3.15 Penetrameter/Image Quality Indicator (IQI)
3.16 Penetrameter sensitivity
3.17 Prime contractor
3.18 Radiograph
3.19 Radiographic inspection
3.20 Radiographic contrast
3.21 Radiographic quality level
3.22 Radiographic film density
3.23 Recording medium
3.24 Source
3.25 Source-to-film distance
3.26 Subcontractor
3.27 Unsharpness
4. GENERAL REQUIREMENTS
4.1 Inspection
4.1.1 Responsibility for inspection
4.2 Personnel
4.2.1 Personnel qualification
4.3 Laboratory installations
4.3.1 Safety
4.3.2 Radiographic exposure areas
APPENDIX
10. Scope
10.1 Scope
20. Referenced documents
20.1 Government documents
20.1.1 Specifications, standards and handbooks
30. Definitions
40. General requirements
40.1 Qualifications
50. Detailed requirements
50.1 Procedures
50.2 Acceptance criteria
50.3 Documentation
50.4 Qualification of personnel
50.5 Qualification period
50.6 Notification of qualification
60. Notes
60.1 Intended use
60.2 Approval of documentation
60.3 Data requirements
Specifies the radiographic inspection criteria for metallic and non-metallic materials to control the quality of radiographic images. Coverage includes referenced documents, definitions, responsibility for inspection, personnel qualification, radiographic exposure areas, and laboratory installations. Also gives detailed appendices.
| Committee |
AREA NDTI
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| DevelopmentNote |
SUPERSEDED BY ASTM E 1742-
|
| DocumentType |
Standard
|
| Pages |
53
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Superseded
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| Supersedes |
| Standards | Relationship |
| SAE AMS 2635 : 1999 | Similar to |
| MIL-P-63430 Base Document:1981 | PROJECTILE, 155MM, TEST, NON-HAZ M718/M741 TYPES LOADING, ASSEMBLING AND PACKING OF |
| MIL C 81984 : B | CARTRIDGE, IMPULSE, MARK 107 MOD 1 |
| MIL-W-50986 Revision A:1982 | WARHEAD, 2.75 INCH ROCKET, HE DUAL PURPOSE M247 WITH OR WITHOUT FUZE, LOADING |
| MIL I 6870 : E | INSPECTION PROGRAM REQUIREMENTS NONDESTRUCTIVE FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS |
| MIL C 70781 : 0 | CARTRIDGE, 60MM: SMOKE, MARKING, M722 ASSEMBLING, MARKING AND PACKING |
| MIL-C-82890 Base Document:1993 | CARTRIDGE, FIRE EXTINGUISHER CCU-120/A |
| MIL-I-60281 Revision A:1992 | INITIATOR, CARTRIDGE ACTUATED, M28, ASSEMBLY |
| MIL-W-21157 Revision A:1971 | WELDMENT, STEEL, CARBON AND LOW ALLOY (YIELD STRENGTH 3O,OOO - 6O,OOO PS1) |
| MIL-W-46291 Revision C:1996 | WARHEAD, GUIDED MISSILE, HE, M17A1 LOADING, ASSEMBLING AND PACKING |
| MIL-B-44421 Base Document:1991 | Body Armor, Small Arms Protective, Aircrew, Survival (No S/S Document) |
| MIL-I-46576 Revision A:1994 | INITIATOR, CARTRIDGE ACTUATED, M5A2 ASSEMBLY |
| MIL-STD-2175 Revision A:1993 | CASTING, CLASSIFICATION AND INSPECTION OF |
| MIL-W-50422 Revision A:1974 | WARHEAD, HE, M18A1 LOADING AND ASSEMBLY |
| MIL-A-83577 Revision B:1988 | ASSEMBLIES, MOVING MECHANICAL, FOR SPACE AND LAUNCH VEHICLES, GENERAL SPECIFICATION FOR |
| MIL-P-63143 Revision A:1979 | PROJECTILE, 8 INCH, HE, RA, M650 ACCESSORIES FOR |
| MIL-F-70601 Base Document:1986 | FUZE, TIME, XM768 METAL PARTS LOADING ASSEMBLING AND PACKING |
| MIL-DTL-82876 Revision A:1995 | CATAPULT, AIRCRAFT EJECTION SEAT, CKU-5B/A ASSEMBLY |
| MIL-C-48171 Base Document:1975 | CARTRIDGE, 81MM, HE, M374A3 LOADING, ASSEMBLING AND PACKING |
| MIL-S-48567 Base Document:1977 | SLEEVE AND GRAIN ASSEMBLY |
| MIL F 27272 : B | FITTING, TETRAFLUOROETHYLENE HOSE, HIGH TEMPERATURE, MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
| MIL-W-63328 Base Document:1979 | WARHEAD GM, HE, M248 INERT PARTS FOR |
| MIL A 87136 : NOTICE 1 | ANTENNAS, AIRBORNE GENERAL SPECIFICATION FOR |
| MIL-F-46488 Revision B:1981 | FUSE, BASE DETONATING, M534A1 LOADING, ASSEMBLING AND PACKING |
| MIL-B-007883 Revision C:1968 | BRAZING OF STEELS, COPPER, COPPER ALLOYS, NICKEL ALLOYS, ALUMINUM AND ALUMINUM ALLOYS |
| MIL-C-46982 Revision B:1969 | Cartridge, 4.2 Inch, HE, M329A1 with Supplementary Charge, with Fuze PD, M557, Loading, Assembling and Packing |
| MIL-R-81202 Revision D:1981 | RECEIVER ASSEMBLY, NITROGEN, FOR LAU-7 SERIES LAUNCHERS |
| MIL-P-63203 Base Document:1983 | PROJECTILE, 155MM, HE, RA, M549A1 AFT (M37 EXTRUDED) PROPELLANT GRAIN FOR |
| MIL-P-48648 Base Document:1986 | PROJECTILE, 155MM, TEST, NON-HAZARDOUS, M718A1/M741A1 TYPES LOADING, ASSEMBLING AND PACKING OF |
| MIL-C-22362 Revision D:1986 | CARTRIDGE, IMPULSE, MK 18 MOD O |
| MIL P 18761 : C | PRIMER, PERCUSSION, MK 22, MOD 2 |
| MIL-C-85254 Base Document:1981 | CHARGE, LINEAR SHAPED |
| MIL-C-82891 Base Document:1993 | CARTRIDGE, IMPULSE, MARK 14 MOD 1 |
| MIL-U-46126 Base Document:1968 | URANIUM ALLOY FOR BODY SECTION CENTER OF AMMUNITION COMPONENTS |
| MIL-P-70533 Base Document:1990 | PROJECTILE, 105 MM, HE, RA XM913/XM927 ROCKET PROPELLANT FOR |
| MIL-STD-1595 Revision A:1982 | QUALIFICATION OF AIRCRAFT, MISSILE AND AEROSPACE FUSION WELDERS |
| MIL C 51335 : B NOTICE 2 | CANISTER, 105MM, CS, XM8 |
| MIL I 85547 : B | IGNITER, ROCKET MOTOR, PVU-3/E |
| MIL-C-48098 Revision B:1982 | CHARGE, SPOTTING, PROJECTILE LOADING, ASSEMBLING, AND PACKING |
| NASA MSFC SPEC 560 : 1988 | THE FUSION WELDING OF STEEL, CORROSION AND HEAT RESISTANT ALLOYS |
| MIL-P-48764 Revision A:1979 | PROJECTILE, 155MM, HE, ROCKET ASSISTED, M549 AND M549A1, AFT (AHH) PROPELLANT GRAIN FOR |
| MIL-T-5021 Revision D:1969 | MILITARY SPECIFICATION. TESTS; AIRCRAFT AND MISSILE WELDING OPERATORS' QUALIFICATION |
| MIL-P-63138 Base Document:1977 | PROJECTILE, 8-INCH, HE, RA, M650 PROPELLANT GRAIN FOR |
| MIL-C-27505 Revision B:1967 | Cartridge, Engine Starter MXU-4A/A |
| MIL-L-50794 Base Document:1973 | LINEAR SHAPED CHARGE ASSEMBLY |
| MIL-C-60827 Revision A:1992 | CARTRIDGE IMPULSE, XM259, ASSEMBLY |
| MIL R 82619 : 0 | ROCKET MOTOR, MARK 81 MOD O (LOADED ASSEMBLY) |
| MIL-M-85657 Base Document:1984 | MOTOR, ROCKET, 2.75 INCH, MARK 66 MODS |
| MIL-A-82772 Base Document:1989 | ASSEMBLY, AFT CLOSURE, IN-PROCESS REQUIREMENTS FOR |
| MIL-STD-372 Base Document:1988 | WELDING, GAS METAL-ARC AND GAS TUNGSTEN-ARC, ALUMINUM ALLOYS, READILY WELDABLE FOR STRUCTURES, EXCLUDING ARMOR |
| MIL-STD-1185 Base Document:1979 | WELDING, HIGH HARDNESS ARMOR |
| MIL-Q-45970 Revision A:1975 | QUALITY ASSURANCE FOR WEAPONS AND SUPPORT MATERIAL |
| MIL-STD-2104 Base Document:1990 | WELDING, TUNGSTEN ARC, GAS, MANUAL (GTAW-MA) REQUIREMENTS FOR |
| MIL-E-6843 Revision C:1967 | ELECTRODE, WELDING, COVERED, LOW ALLOY STEEL (PRIMARILY FOR AIRCRAFT AND WEAPON APPLICATIONS) |
| MIL-P-50573 Revision C:1979 | PROJECTILE, 155MM, HE, ROCKET ASSISTED M549 & M549A1 FORWARD (AHH) PROPELLANT GRAIN FOR |
| MIL-D-60568 Revision B:1967 | Delay Element, Cartridge, M13 Assembly |
| MIL-C-71134 Base Document:1992 | CARTRIDGE, HE, 120MM, M933W/FUZE M745 LOADING, ASSEMBLING AND PACKING |
| MIL-P-48749 Revision D:1986 | PROJECTILE, 155MM, HE: M483A1 LOADING, ASSEMBLING AND PACKING |
| MIL-A-82950 Base Document:1995 | ACTUATOR, BELLOWS ATU-117/P |
| MIL-C-48135 Base Document:1973 | CARTRIDGE, 105 MM, HE M1, (MOD) LOADING, ASSEMBLING AND PACKING |
| MIL-P-18711 Revision A:1955 | PRIMER, ELECTRIC, MARK 37 MOD 2 |
| MIL-STD-1943 Base Document:1985 | WELDING REPAIR OF STEEL CASTINGS (OTHER THAN ARMOR) METAL-ARC, MANUAL |
| MIL-W-50258 Revision A:1971 | WARHEAD SECTION, 762MM ROCKET, PRACTICE: M38 METAL PARTS FOR |
| MIL-DTL-82884 Revision A:1996 | CARTRIDGE, IMPULSE, CCU-69A/A |
| MIL-D-82687 Base Document:1980 | DEVICE, ARMING FIRING, ROCKET MOTOR MARK 298 MOD O |
| MIL-C-60570 Revision B:1992 | Cartridge, Delay, M114 Assembly |
| MIL F 85406 : 0 | FUSE SYSTEM, JOINT SERVICE ELECTRONIC BOMB FMU-139/B |
| MIL-W-48381 Base Document:1974 | WARHEAD SECTION, GM, PRACTICE, LIGHTWEIGHT, M252E1 PARTS AND ASSEMBLING |
| MIL-C-85257 Base Document:1981 | CORD ASSEMBLY, DETONATING |
| SAE MAM 5401 : 2003 | NICKEL ALLOY, CORROSION AND HEAT RESISTANT, INVESTMENT CASTINGS 62NI - 21.5CR - 9.0MO - 3.6CB VACUUM MELTED, VACUUM CAST AS CAST |
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-S-45909 Revision C:1989 | STUD, LOCKED IN - RING LOCKED SERRATED |
| MIL BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
| DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-A-21180 Revision D:1984 | ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH |
| MIL I 45910 : C | INSERT, SCREW THREAD LOCKED IN & RING LOCKED 1 SERRATED GENERAL SPECIFICATION FOR |
| 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)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL F 8789 : D | FITTING END, ATTACHABLE HYDRAULIC, HIGH PRESSURE HOSE |
| DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-D-23615 Revision C:1993 | DESIGN AND EVALUATION OF CARTRIDGE ACTUATED DEVICES |
| MIL C 23661 : A | CARTRIDGE, IMPULSE, MARK 45 MOD O |
| MIL-S-8802 Revision F:1990 | SEALING COMPOUND, TEMPERATURE-RESISTANT, INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES, HIGH ADHESION |
| MIL-W-63150 Base Document:1977 | WEAPONS AND SUPPORT MATERIAL STANDARD QUALITY ASSURANCE PROVISIONS FOR |
| MIL-T-46604 Revision B:1993 | THRUSTER, CARTRIDGE ACTUATED, M13, ASSEMBLY |
| MIL-B-85599 Base Document:1983 | BOOSTER, FUSE, MARK 60 MOD 2 |
| MIL-I-60231 Revision B:1995 | IGNITION ELEMENT, ELECTRIC, M55 ASSEMBLY |
| MIL-DTL-48568 Revision D:1996 | CATAPULT, AIRCRAFT EJECTION SEAT, CKU-7/A ASSEMBLY |
| MIL-G-82932 Base Document:1994 | GAS GENERATOR, M17, REMANUFACTURED ASSEMBLY |
| MIL-F-29419 Base Document:1985 | FRAME, SHIPPING [SIXCON] |
| SAE AMS 5340 : 2018 | STEEL, CORROSION RESISTANT, INVESTMENT CASTINGS, 14CR - 4.25NI - 2.25MO - 0.25CB - 3.25CU, HOMOGENIZATION AND SOLUTION HEAT TREATED |
| MIL C 87104 : 0 | COAXIAL ASSEMBLIES, GENERAL SPECIFICATION FOR |
| MIL-C-60872 Revision A:1992 | CARTRIDGE, DELAY, XM271, ASSEMBLY |
| MIL-W-22248 Revision A:1971 | WELDMENTS, ALUMINUM AND ALUMINUM ALLOY |
| MIL-C-82894 Base Document:1994 | CARTRIDGE, FIRE EXTINGUISHER, CCU-126/A |
| MIL-C-60643 Revision A:1992 | CARTRIDGE, IMPULSE, M127 ASSEMBLY |
| MIL-I-46625 Revision C:1990 | INITIATOR, CARTRIDGE ACTUATED, M3A2, ASSEMBLY |
| SAE AMS 2680 : 2010 | ELECTRON-BEAM WELDING, FOR FATIGUE CRITICAL APPLICATIONS |
| MIL-T-46616 Revision C:1992 | THRUSTER, CARTRIDGE ACTUATED, M3A3 ASSEMBLY |
| MIL-P-48762 Base Document:1975 | PROJECTILE, 155MM, HE, ROCKET ASSISTED, M549, INERT, STIMULATED PARTS AND LOADING |
| MIL-A-82769 Base Document:1989 | ASSEMBLY, AFT CLOSURE, SILICONE RUBBER, ROOM TEMPERATURE VULCANIZING, IN-PROCESS REQUIREMENTS FOR |
| MIL C 46241 : F | CARTRIDGE, AIRCRAFT EJECTION SEAT, CATAPULT, M36 |
| MIL-STD-1252 Base Document:1975 | INERTIA FRICTION WELDING PROCESS, PROCEDURE AND PERFORMANCE QUALIFICATION |
| MIL-E-50796 Base Document:1973 | EXPANDING SHIELDED MILD DETONATING CORD ASSEMBLY |
| MIL-C-46239 Revision C:1991 | CARTRIDGE, IMPULSE, M31A2 ASSEMBLY |
| QQ-A-596 Revision E:1981 | ALUMINUM ALLOY PERMANENT AND SEMI-PERMANENT MOLD CASTINGS |
| MIL-S-8512 Revision D:1974 | SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF |
| MIL-DTL-82935 Base Document:1996 | CARTRIDGE, IMPULSE, CCU-132/A |
| MIL C 60247 : A | CARTRIDGE, INITIATOR, DELAY M155 |
| MIL-C-46941 Revision A:1993 | CARTRIDGE, IMPULSE, M146 ASSEMBLY |
| MIL-W-63329 Revision A:1986 | WARHEAD GM, HE, M248 LOADING, ASSEMBLY & PACKING |
| MIL-P-50257 Base Document:1969 | PROJECTILE 8 INCH, HE, M404 LOADING, ASSEMBLING AND PACKING. |
| MIL-STD-1261 Revision C:1988 | ARC WELDING PROCEDURES FOR CONSTRUCTIONAL STEELS |
| MIL-C-46615 Revision D:1991 | CARTRIDGE, IMPULSE, M29A2 ASSEMBLY |
| MIL-C-82722 Base Document:1982 | CATAPULT, AIRCRAFT EJECTION SEAT, CKU-5/A REWORK ASSEMBLY |
| MIL-C-60456 Base Document:1967 | CARTRIDGE, 105MM, HE, ROCKET ASSISTED, XM548 ACCESSORIES FOR |
| MIL-C-60604 Revision A:1992 | CARTRIDGE, THRUSTER, M119 |
| MIL-C-23933 Revision B:1971 | CARTRIDGE, IMPULSE, MARK 44 MOD O |
| MIL-C-46995 Revision C:1969 | CARTRIDGE 81MM, HE, M374 LOADING, ASSEMBLING AND PACKING |
| SAE AMS 3263 : 1997 | SEALING COMPOUND, POLYTHIOETHER, AMBIENT CURE OR IMMEDIATE HEAT CURE FOR AIRCRAFT STRUCTURES, FUEL RESISTANT WITH INTERMITTENT USE TO 400 MDCF (204 MDCC) |
| MIL I 60283 : A | INITIATOR, CARTRIDGE ACTUATED, M27 ASSEMBLY |
| MIL-P-46258 Revision C:1979 | PROJECTILE, 8 INCH, HE, M106, LOADING, ASSEMBLING, AND PACKING |
| MIL C 82876 : 1993 | CATAPULT, AIRCRAFT EJECTION SEAT, CKU-5B/A ASSEMBLY |
| SAE ARP 899 : 2013 | TUBE FITTINGS, FLUID SYSTEMS, PERMANENT TYPE, GENERAL REQUIREMENTS FOR |
| SAE ARP 1675 : 2014 | STRUCTURAL WELDBONDING OF ALUMINUM STRUCTURES |
| NEMA XR 14-1990 (R1995, R2000) | RECOMMENDED PRACTICES FOR LOAD-BEARING MECHANICAL ASSEMBLIES USED IN DIAGNOSTIC IMAGING |
| MIL-R-85880 Base Document:1988 | ROCKET, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
| MIL I 50699 : A | INITIATOR, PROPELLANT ACTUATED, JAU-2/A25 ASSEMBLY |
| NASA KSC SPEC Z 0006 : 1995 | INDUCTION BRAZING, AEROSPACE TUBING FITTINGS, SPECIFICATION FOR |
| MIL-R-29565 Revision A:1990 | ROCKET MOTOR, MK 125 MOD 1 |
| MIL-B-85464 Base Document:1981 | BOOSTER, FUSE, MARK 38 MOD 2 |
| MIL I 50374 : A | INITIATOR, PROPELLANT ACTUATED, M104 ASSEMBLY |
| MIL-C-46946 Revision B:1994 | CARTRIDGE, IMPULSE, M43 ASSEMBLY |
| MIL-I-82877 Base Document:1992 | IGNITION ELEMENT, PVU-15/B |
| NASA KSC SPEC Z 0005 : 1995 | BRAZING - STEEL, COPPER, ALUMINIUM, NICKEL, AND MAGNESIUM ALLOYS, SPECIFICATION FOR |
| MIL-W-8604 Revision A:1982 | WELDING, FUSION, ALUMINUM ALLOYS, PROCESSING AND PERFORMANCE OF |
| MIL-M-48185 Revision B:1992 | MUNITION FOR PROJECTILE, 155MM, MA692/M731, DETONATING CORD ASSEMBLY FOR |
| MIL-D-60873 Revision A:1992 | DELAY ELEMENT, CARTRIDGE, XM69, ASSEMBLY |
| MIL C 82922 : 1994 | CARTRIDGE, IMPULSE, CCU-123/E (EARTH ANCHOR CARTRIDGE) |
| MIL F 83296 : 0 | FITTING, TETRAFLUOROETHYLENE HOSE, HIGH TEMPERATURE, HIGH PRESSURE (3,000 PSI HYDRAULIC AND PNEUMATIC) |
| MIL-W-87105 Base Document:1977 | WAVEGUIDE ASSEMBLIES, GENERAL SPECIFICATION FOR |
| MIL-S-63383 Base Document:1980 | SAFE AND ARMING (NON-HAZARDOUS) ASSEMBLY M718/M741 |
| MIL-C-85253 Base Document:1981 | CODE DETONATING |
| MIL-P-48649 Base Document:1986 | PROJECTILE, 155MM, M718A1/M741A1 TYPES, LOADING, ASSEMBLING AND PACKING OF |
| MIL C 82884 : 1993 | CARTRIDGE, IMPULSE CCU-69A/A |
| MIL-M-29460 Base Document:1990 | MODULE, WATER PUMP (SIXCON) |
| MIL C 48568 : B | CATAPULT, AIRCRAFT EJECTION SEA, CKU-7/A ASSEMBLY |
| QQ-M-38 Revision B:1969 | MAGNESIUM ALLOY DIE CASTINGS (AZ91A) |
| MIL-C-70996 Base Document:1991 | CARTRIDGE, HE, 81MM, M821E1/M889E1 W/FUZE M734/M935 LOADING, ASSEMBLING AND PACKING |
| MIL P 85759 : 0 | PROPELLANT GRAIN, MARK 93 MOD O |
| MIL-P-48187 Revision C:1992 | PROJECTILE, 155MM, HE: M692 AND M731 LOADING, ASSEMBLING AND PACKING |
| MIL-P-18920 Revision B:1981 | PRIMER, ELECTRIC, MK 42 MODS 0, 1 & 2 |
| MIL-P-18716 Revision C:1991 | PRIMER, ELECTRIC, MARK 48 MOD 2 |
| MIL-P-48091 Revision G:1988 | PROJECTILE, 8 INCH: HE: M509A1 LOADING, ASSEMBLING & PACKING |
| MIL-R-11470 Revision A:1971 | RADIOGRAPHIC INSPECTION, QUALIFICATION OF EQUIPMENT, OPERATORS AND PROCEDURES |
| MIL-B-60381 Revision B:1972 | BURSTER, PROJECTILE, XM53 LOADING ASSEMBLING AND PACKING |
| MIL D 50648 : A | DELAY ELEMENT, CARTRIDGE M75 ASSEMBLY |
| MIL-R-50753 Revision A:1972 | ROCKET MOTOR M199 ASSEMBLY |
| MIL I 60286 : B NOTICE 2 | INITIATOR, CARTRIDGE ACTUATED, M53, ASSEMBLY |
| MIL-B-9972 Revision B:1994 | BRAZING, NICKEL, ALLOY, GENERAL SPECIFICATION FOR |
| MIL-HDBK-349 Base Document:1994 | MANUFACTURE AND INSPECTION OF ADHESIVE BONDED, ALUMINUM HONEYCOMB SANDWICH ASSEMBLIES FOR AIRCRAFT |
| MIL-P-45971 Base Document:1975 | PRODUCT ENGINEERING QUALITY ENGINEERING SYSTEM (PEQES) FOR WEAPONS AND SUPPORT MATERIAL |
| MIL-P-50202 Revision A:1977 | PROPELLANT CHARGE, ROCKET, FOR DEMOLITION KIT, CRATERING, M180 |
| MIL-M-14927 Revision B:1977 | MOTOR, ROCKET, LAUNCH, M114 LOADING, ASSEMBLING AND PACKING |
| MIL U 46045 : D | URANIUM ALLOY, WROUGHT, BARS, BILLETS, AND TUBULAR SHAPES |
| MIL P 60377 : B | PROJECTILE, 155MM, HE, M107 LOADING, ASSEMBLING AND PACKING |
| MIL R 85769 : 1986 | ROCKET MOTOR, MK 117 MOD O |
| MIL C 22653 : C | CARTRIDGE, IMPULSE, MARK 19 MOD O |
| NASA MSFC SPEC 504 : 1990 | WELDING, ALUMINIUM ALLOYS |
| MIL I 85760 : 0 | IGNITER, MK 304 MOD O |
| MIL-C-82733 Revision A:1988 | CARTRIDGE, IMPULSE, CCU-22/A/A ASSEMBLY |
| MIL B 60426 : A | BURSTER, PROJECTILE, XM54, LOADING, ASSEMBLING AND PACKING |
| MIL-DTL-60247 Revision B:1995 | CARTRIDGE, DELAY, M155 ASSEMBLY |
| MIL-F-63253 Base Document:1977 | FUSE, BASE DETONATING, M578 LOADING, ASSEMBLING AND PACKING FOR RENOVATION |
| MIL-C-46228 Revision B:1991 | CARTRIDGE, DELAY, M93, ASSEMBLY |
| MIL-P-18704 Revision A:1992 | PRIMER, LOCK, COMBINATION, MARK 15 MOD 2 |
| MIL-STD-1265 Revision A:1987 | RADIOGRAPHIC INSPECTION, CLASSIFICATION AND SOUNDNESS REQUIREMENTS FOR STEEL CASTINGS |
| MIL-F-63412 Base Document:1981 | FUZE PROBE ASSEMBLY, PNEUMATIC ASSEMBLING & PACKING (TOW) |
| SAE AS 7100/1 : 2008 | NATIONAL AEROSPACE AND DEFENSE CONTRACTORS ACCREDITATION PROGRAM (NADCAP) SURVEY CHECKLISTS FOR THE NDT SUPPLIERS ACCREDITATION PROGRAM |
| NASA MSFC SPEC 766 : 1982 | FUSION WELDING TITANIUM AND TITANIUM ALLOYS |
| MIL-R-5632 Revision B:1972 | ROD, AND WIRE, STEEL WELDING [FOR AIRCRAFT] |
| MIL-I-85889 Base Document:1988 | IGNITER, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
| SAE AS 7114/4 : 2008 | NADCAP REQUIREMENTS FOR NONDESTRUCTIVE TESTING FACILITY RADIOGRAPHY |
| MIL-S-63257 Revision B:1985 | SAFETY AND ARMING DEVICE, GUIDED MISSILE, M143, LOADING, ASSEMBLING AND PACKING FOR |
| MIL-R-23452 Revision A:1982 | ROCKET MOTOR MARK 25 MODS O, 1 AND 2 |
| MIL-R-85363 Base Document:1981 | ROCKET MOTOR MARK 23 MODS 2 & 3 |
| MIL-DTL-82922 Revision A:1995 | CARTRIDGE, IMPULSE, CCU-123/E (EARTH ANCHOR CARTRIDGE) |
| MIL-I-46175 Revision A:1983 | |
| MIL-T-46692 Revision B:1993 | THRUSTER, CARTRIDGE ACTUATED. M16, ASSEMBLY |
| MIL-T-45499 Revision C:1993 | THRUSTER, CARTRIDGE ACTUATED, M1A2 ASSEMBLY |
| MIL-P-83126 Revision A:1980 | PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
| MIL C 46200 : B | CARTRIDGE, IMPULSE, M42A1 ASSEMBLY |
| MIL-W-48274 Base Document:1974 | WARHEAD SECTION, GM, TRAINING, XM201 PARTS AND ASSEMBLING |
| MIL C 50647 : A | CARTRIDGE DELAY M293 ASSEMBLY |
| 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-B-29604 Base Document:1994 | Body Armor, Hard, Small Arms Protective, PRU-61/P22P-15 |
| MIL-G-85258 Base Document:1981 | GENERATOR, GAS PRESSURE, PROPELLANT ACTUATED BBU-18/B |
| MIL I 82929 : A | INITIATOR, EXPLOSIVE ACTUATED, JAN-24/A |
| MIL A 85097 : B | AIRCREW ESCAPE PROPULSION SYSTEMS (AEPS), PROCUREMENT SPECIFICATION FOR |
| MIL C 63106 : A | COUNTERMEASURE, CHAFF: M-1 |
| MIL-S-63382 Base Document:1980 | SAFE AND ARMING (PARTIAL LOADING)ASSEMBLY FOR MINES, M718/M741 SYSTEM |
| MIL-DTL-0023933 Revision C Interim Revision:1995 | CARTRIDGE, IMPULSE, MARK 44 MOD 0 |
| MIL-P-48323 Revision C:1984 | PROJECTILE, 8 INCH, HE, RA, M650 ROCKET MOTOR BODY ASSEMBLY |
| MIL-P-48189 Revision D:1992 | PROJECTILE, 155MM, HE, M692 AND M731 HOUSING, TIMING AND FUZING FOR |
| MIL-W-50848 Revision D:1984 | WARHEAD, GUIDED MISSILE HE M250 LOADING ASSEMBLING AND PACKING |
| MIL-F-70518 Base Document:1984 | FLARE, INFRARED TRACKING, MARK 33 MOD O (ARMY) PARTS FOR AND LOADING, ASSEMBLING AND PACKING |
| SAE AIR 4728 : 2013 | REFERENCES, SPACECRAFT AND SPACECRAFT SERVICING, FLUID SYSTEM COMPONENTS (ABBREVIATIONS, ACRONYMS, DEFINITIONS, APPLICABLE DOCUMENTS AND ENVIRONMENTAL CONDITIONS) |
| SAE AMS T 81915 : 2016 | TITANIUM AND TITANIUM-ALLOY CASTINGS, INVESTMENT |
| SAE J 427 : 2018 | PENETRATING RADIATION INSPECTION |
| SAE ARP 1611 : 2014 | QUALITY INSPECTION PROCEDURE, COMPOSITES TRACER FLUOROSCOPY AND RADIOGRAPHY |
| MIL A 5503 : E | ACTUATOR, AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
| MIL-P-63238 Revision B:1986 | PROJECTILE, 155MM, AT M718/M741 LOADING, ASSEMBLING AND PACKING OF |
| MIL-E-46511 Revision A:1975 | EXPLOSIVE HARNESS ASSEMBLY MISSILE ROCKET, XM84 LOADING ASSEMBLY AND PACKING |
| MIL-P-82866 Revision A:1994 | PRIMER, ELECTRIC, MARK 153 MOD 1 |
| MIL F 50864 : B | FUZE, PIBD, M549, LESS SPITBACK METAL PARTS AND LOADING, ASSEMBLING AND PACKAGING |
| MIL-P-82691 Revision A:1989 | PROPELLANT GRAIN, IGNITER |
| MIL-STD-1512 Base Document:1972 | ELECTROEXPLOSIVE SUBSYSTEMS, ELECTRICALLY INITIATED, DESIGN REQUIREMENTS AND TEST METHODS |
| MIL-W-14746 Revision B:1980 | WARHEAD, GUIDED MISSILE, H.E. M155 LOADING, ASSEMBLING AND PACKING |
| MIL-STD-1576 Base Document:1984 | ELECTROEXPLOSIVE SUBSYSTEM SAFETY REQUIREMENTS AND TEST METHODS FOR SPACE SYSTEMS |
| MIL-B-85685 Base Document:1988 | BOOSTER, FUZE, MARK 60 MOD 3 |
| MIL-G-82841 Base Document:1986 | |
| MIL-S-7470 Revision A:1975 | SHAFT, POWER TRANSMISSION, AIRCRAFT ACCESSORY, GENERAL SPECIFICATION FOR |
| MIL-T-81838 Base Document:1971 | TANK, FUEL, AIRCRAFT, AUXILIARY EXTERNAL 300 GALLON, TYPE AERO 1D |
| MIL-W-48866 Revision A:1980 | WARHEAD SECTION, GM, PRACTICE LIGHTWEIGHT, M252 AND SHIPPING AND STORAGE CONTAINER, XM612, SPARE PARTS FOR |
| MIL A 83366 : 0 | ANTENNA ASSEMBLIES, AIRBORNE, GENERAL SPECIFICATION FOR |
| MIL-W-48369 Base Document:1974 | WARHEAD SECTION, GM, PRACTICE, LIGHTWEIGHT, M252 PARTS AND ASSEMBLING |
| MIL-C-23931 Revision D:1985 | CARTRIDGE, IMPULSE, MARK 9 MOD O |
| MIL-M-29417 Base Document:1984 | MODULE, FUEL PUMP [SIXCON] |
| MIL-E-82778 Base Document:1989 | EXIT CONE ASSEMBLY, IN-PROCESS REQUIREMENTS FOR |
| MIL-D-46606 Revision B:1991 | DELAY ELEMENT, CARTRIDGE, M8 ASSEMBLY |
| MIL P 82790 : NOTICE 1 | PROPELLANT GRAIN, RADIOGRAPHIC INSPECTION OF IN-PROCESS REQUIREMENTS FOR |
| MIL-STD-2103 Base Document:1990 | WELDING, ELECTRON BEAM, REQUIREMENTS FOR |
| MIL-B-46957 Revision B:1977 | BURSTER, PROJECTILE, M48 LOADING, ASSEMBLING AND PACKING |
| MIL-P-70505 Base Document:1984 | PROJECTILE, 155mm: XM864 PROPELLANT GRAIN |
| MIL-P-63140 Revision A:1980 | PROJECTILE, 8-INCH, HE, RA, M650 DELAY ASSEMBLY FOR |
| MIL-P-63142 Revision B:1990 | PROJECTILE, 8 INCH, RA, M650 LOADING ASSEMBLING AND PACKING |
| MIL-C-22079 Revision C:1985 | CARTRIDGE, IMPULSE, MARK 17 MOD 1 |
| SAE AMS 7295 : 1993 | RADIOGRAPHIC FILM AND PAPER, INDUSTRIAL GRADE |
| MIL-M-46062 Revision C:1985 | MAGNESIUM ALLOY CASTINGS, HIGH STRENGTH |
| MIL-L-85297 Base Document:1980 | LEAD, EXPLOSIVE MARK 24 MOD O MARK 25 MOD O |
| MIL-R-46509 Revision A:1982 | ROCKET MOTOR, XM30, METAL PARTS FOR |
| MIL-W-63377 Base Document:1987 | WARHEAD, ILLUMINATING, M257, W/M442 FUZE (2.75 INCH ROCKET ILLUMINATING FLARE) |
| MIL-C-14750 Revision B:1989 | CARTRIDGE, 60 MM, HE, M49A4 LOADING, ASSEMBLING AND PACKING |
| MIL-C-82865 Base Document:1989 | CARTRIDGE, IMPULSE, MARK 152 MOD 0, MARK 153 MOD 0, MARK 154 MOD 0, &MARK 155 MOD 0 |
| MIL-P-48870 Base Document:1976 | PROJECTILE, 155MM, TEST. M692 LOADING, ASSEMBLING AND PACKING |
| NASA MSFC STD 481 : 1966 | RADIOGRAPHIC INSPECTION AND ACCEPTANCE STANDARDS FOR FUSION-WELDED JOINTS - IN STAINLESS AND HEAT-RESISTANT STEEL |
| NASA MSFC SPEC 259 : 1962 | RADIOGRAPHIC INSPECTION: SOUNDNESS REQUIREMENTS FOR FUSION WELDS IN ALUMINIUM AND MAGNESIUM ALLOY SHEET AND PLATE MATERIAL (SPACE VEHICLE COMPONENTS) |
| MIL-STD-1264 Revision B:1989 | RADIOGRAPHIC INSPECTION FOR SOUNDNESS OF WELDS IN STEEL BY COMPARISON TO GRADED ASTM E 390 REFERENCE RADIOGRAPHS |
| MIL-P-63141 Revision B:1985 | PROJECTILE, 8-INCH, HE, RA, M650 BOOSTER AUXILIARY PA-500 & BOOSTER ASSEMBLY PA-524 FOR |
| MIL-D-60572 Revision B:1994 | DELAY ELEMENT, CARTRIDGE, M28 ASSEMBLY |
| MIL-P-50538 Base Document:1970 | PROJECTILE 155MM HE M449A1 LOADING, ASSEMBLING AND PACKING |
| MIL-STD-645 Revision B:1981 | DIP BRAZING OF ALUMINUM ALLOYS |
| MIL-S-48747 Revision B:1982 | SAFE AND ARMING DEVICE FOR MINES, M718/M741 SYSTEM |
| SAE AS 4488 : 2013 | TUBULAR ASSEMBLIES, FUSION WELDED, INSPECTION PROCESSES AND ACCEPTANCE STANDARDS FOR |
| MIL-B-44314 Base Document:1987 | BODY ARMOR, SMALL ARMS PROTECTIVE, AIRCREWMAN |
| MIL DTL 0022362 : E | CARTRIDGE, IMPULSE, MARK 18 MOD 0 |
| MIL-E-8697 Revision E:1972 | ELECTRODE, WELDING, COVERED LOW HYDROGEN HEAT TREATABLE STEEL |
| MIL-C-45408 Revision C:1992 | CARTRIDGE, IMPULSE, M44A1 ASSEMBLY |
| MIL-C-60235 Revision B:1989 | CARTRIDGE, IMPULSE, M91 ASSEMBLY |
| MIL-HDBK-728-5 Revision A:1994 | RADIOGRAPHIC TESTING - VOLUME 5 |
| WW-T-696 Revision E:1984 | TRAPS, STEAM |
| MIL C 45195 : E | CARTRIDGE, 105 MM, HE, M1, LOADING ASSEMBLING AND PACKING |
| DOD P 63252 : NOTICE 1 | PROJECTILE, 155 MM, HE, XM795 LOADING, ASSEMBLING AND PACKING |
| MIL W 46132 : NOTICE 4 | WELDING, FUSION, ELECTRON BEAM, PROCESS FOR |
| MIL F 63107 : C | FLARE, AIRCRAFT COUNTERMEASURE: M206 |
| MIL R 5149 : B | ROCKET ENGINE, LIQUID PROPELLANT GENERAL SPECIFICATION FOR |
| MIL-P-64005 Base Document:1985 | PROJECTILE, 155MM, GB2, M687, METAL PARTS ASSEMBLY WITH LOADED OGIVE |
| SAE AMS 2689 : 2016 | FUSION WELDING TITANIUM AND TITANIUM ALLOYS |
| MIL T 60201 : C | THRUSTER, CARTRIDGE ACTUATED, M25A1 ASSEMBLY |
| MIL-T-46626 Revision C:1994 | THRUSTER, CARTRIDGE ACTUATED, M2A2 ASSEMBLY |
| QQ-A-601 Revision F:1981 | ALUMINUM ALLOY SAND CASTINGS |
| MIL-P-63066 Base Document:1976 | PROJECTILE, 155MM, SPECIAL TEST, FOR M692 AND M731 LOADING, ASSEMBLING AND PACKING OF |
| MIL-P-50569 Revision C:1982 | PROJECTILE, 155MM, HE, ROCKET ASSISTED M549 SERIES, MOTOR BODY BONDING ASSEMBLY FOR |
| MIL-W-48757 Base Document:1975 | WARHEAD SECTION, GM, HE: M251 AND M251A1 SPARE PARTS FOR |
| MIL-C-46274 Revision C:1992 | CARTRIDGE, IMPULSE, M94 ASSEMBLY |
| MIL-C-60575 Revision A:1992 | CARTRIDGE, THRUSTER, M141 ASSEMBLY |
| DOD-STD-35-126 Base Document:1978 | AUTOMATED ENGINEERING DOCUMENT PREPARATION SYSTEM, CYLINDERS, ACTUATING, LINEAR |
| MIL-C-46221 Revision B:1992 | CARTRIDGE, IMPULSE, M37 ASSEMBLY |
| SAE AMS STD 2175 : 2003 | CASTINGS, CLASSIFICATION AND INSPECTION OF |
| AWS A2.4 : 2012 | STANDARD SYMBOLS FOR WELDING, BRAZING, AND NONDESTRUCTIVE EXAMINATION |
| ASTM E 446 : 2015 : REDLINE | Standard Reference Radiographs for Steel Castings Up to 2 in. (50.8 mm) in Thickness |
| ASTM E 186 : 2015 : REDLINE | Standard Reference Radiographs for Heavy-Walled (2 to 4<fraction><num>1</num><den>2</den></fraction > in. (50.8 to 114 mm)) Steel Castings |
| MIL-STD-410 Revision E:1991 | NONDESTRUCTIVE TESTING PERSONNEL QUALIFICATION AND CERTIFICATION (EDDY CURRENT, LIQUID PENETRANT, MAGNETIC PARTICLE, RADIOGRAPHIC AND ULTRASONIC) |
| ASTM E 155 : 2015 : REDLINE | Standard Reference Radiographs for Inspection of Aluminum and Magnesium Castings |
| ASTM E 242 : 2015 : REDLINE | Standard Reference Radiographs for Appearances of Radiographic Images as Certain Parameters are Changed |
| ASTM E 390 : 2015 : REDLINE | Standard Reference Radiographs for Steel Fusion Welds |
| ASTM E 192 : 2015 : REDLINE | Standard Reference Radiographs of Investment Steel Castings for Aerospace Applications |
| ASTM E 272 : 2015 : REDLINE | Standard Reference Radiographs for High-Strength Copper-Base and Nickel-Copper Alloy Castings |
| ASTM E 280 : 2015 : REDLINE | Standard Reference Radiographs for Heavy-Walled (4<fraction><num>1</num><den>2</den></fraction > to 12 in. (114 to 305 mm)) Steel Castings |
| ASTM E 310 : 2015 : REDLINE | Standard Reference Radiographs for Tin Bronze Castings |
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