SAE AMS 2301 : 2015
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
STEEL CLEANLINESS, AIRCRAFT QUALITY MAGNETIC PARTICLE INSPECTION PROCEDURE
Hardcopy , PDF
05-22-2020
English
01-01-2015
1. SCOPE
2. APPLICABLE DOCUMENTS
3. TECHNICAL REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. ACKNOWLEDGMENT
7. REJECTIONS
8. NOTES
Specifies steel cleanliness requirements in inch/pound units for aircraft-quality ferro-magnetic steels, other than hardenable corrosion resistant steels, by magnetic particle inspection methods.
Committee |
AMS-E
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DevelopmentNote |
Supersedes SAE MAM 2301. (07/2007)
|
DocumentType |
Standard
|
Pages |
14
|
PublisherName |
SAE International
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Status |
Superseded
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SupersededBy | |
Supersedes |
MIL-S-6758 Revision B:1993 | STEEL, CHROME-MOLYBDENUM (4130) BARS AND REFORGING STOCK (AIRCRAFT QUALITY) |
SAE AMS 6299 : 2014 | STEEL BARS, FORGINGS, AND TUBING, CARBURIZING, 0.50CR - 1.8NI - 0.25MO (0.17 - 0.23C) (SAE 4320H) |
SAE AMS 6263 : 2016 | STEEL BARS, FORGINGS, AND TUBING, 1.2CR - 3.2NI - 0.12MO (0.11 - 0.17C) (9315) |
SAE AMS 6350 : 2015 | STEEL SHEET, STRIP, AND PLATE, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130) |
SAE AMS 6327L : 2017 | STEEL BARS AND FORGINGS, 0.50CR - 0.55NI - 0.25MO (0.38 - 0.43C) (SAE 8740), HEAT TREATED, 125 KSI (862 MPA) TENSILE STRENGTH (COMPOSITION SIMILAR TO UNS G87400) |
SAE AMS 6351 : 2015 | STEEL, SHEET, STRIP, AND PLATE, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130), SPHEROIDIZED |
MIL S 81081 : A | STEEL; SHEET, CHROMIUM NICKEL MOLYBDENUM VANADIUM (FOR TORPEDO MARK 46 MOD O) |
SAE AMS6328N : 2017 | STEEL, BARS, FORGINGS, AND TUBING, 0.50CR - 0.55NI - 0.25MO (0.48 TO 0.53C) (SAE 8750) |
SAE AMS 6434 : 2016 | STEEL, SHEET, STRIP, AND PLATE, 0.78CR - 1.8NI - 0.35MO - 0.20V (0.33 - 0.38C) (4335 MOD) |
SAE AMS 6433 : 2015 | STEEL, SHEET, STRIP, AND PLATE 0.75MN - 0.78CR - 1.8NI - 0.35MO - 0.20V (0.33 - 0.38C) (4335 MOD) |
SAE AMS 6361 : 2014 | STEEL TUBING, SEAMLESS, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130) 125 KSI (862 MPA) TENSILE STRENGTH |
SAE AMS 6282 : 2015 | STEEL TUBING, MECHANICAL, 0.50CR - 0.55NI - 0.25MO (0.33 - 0.38C) (SAE 8735) |
SAE AMS 6492 : 2013 | STEEL BARS, FORGINGS, AND TUBING, 1.0CR - 3.25NI - 0.40MO (0.17 - 0.22C) AIRCRAFT QUALITY |
SAE AMS 6302K : 2017 | LOW-ALLOY STEEL, HEAT-RESISTANT, BARS, FORGINGS, AND TUBING, 0.65SI - 1.25CR - 0.50MO - 0.25V (0.28 - 0.33C) |
SAE AMS 6303 : 2018 | STEEL BARS AND FORGINGS, LOW ALLOY, HEAT-RESISTANT, 0.65SI - 1.25CR - 0.50MO - 0.85V (0.25 - 0.30C) |
SAE AMS 6360 : 2013 | STEEL TUBING, SEAMLESS, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130), NORMALIZED OR STRESS RELIEVED |
MIL-HDBK-1587 Base Document:1996 | MATERIALS AND PROCESS REQUIREMENTS FOR AIR FORCE WEAPON SYSTEM |
SAE AMS 6396 : 2015 | STEEL SHEET, STRIP, AND PLATE, 0.80CR - 1.8NI - 0.25MO (0.49 - 0.55C) ANNEALED |
SAE AMS 6352 : 2013 | STEEL SHEET, STRIP, AND PLATE, 0.95CR - 0.20MO (0.33 - 0.38C) (SAE 4135) |
MIL-STD-1587 Revision D:2017 | MATERIAL AND PROCESS REQUIREMENTS FOR AEROSPACE WEAPONS SYSTEMS |
BS 5S 100:1993 | Procedure for inspection, testing and acceptance of wrought steels (other than plate, sheet, strip and tube) |
SAE AMS 6370 : 2016 | STEEL, BARS, FORGINGS, AND RINGS, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130) |
SAE AMS 6322 : 2014 | STEEL BARS, FORGINGS, AND RINGS, 0.50CR - 0.55NI - 0.25MO (0.38 - 0.43C) (SAE 8740) |
SAE AMS 6427 : 2014 | STEEL BARS, FORGINGS, AND TUBING, 0.88CR - 1.8NI - 0.42MO - 0.08V (0.25 - 0.33C) (4330 MOD) |
SAE AMS 6547 : 2013 | STEEL BARS, FORGINGS, AND TUBINGS, 1.0CR - 3.2NI - 0.2MO - (0.12 - 0.17C), AIRCRAFT QUALITY |
SAE AMS 6382 : 2014 | STEEL, BARS, FORGINGS, AND RINGS 0.95CR - 0.20MO (0.38 - 0.43C) (SAE 4140) ANNEALED |
SAE AMS 6432 : 1973 | STEEL BARS, FORGINGS, AND TUBING, 1.05CR - 0.55NI - 1.0MO - 0.12V (0.43-0.49C) |
SAE AMS 6274 : 2016 | STEEL BARS, FORGINGS AND TUBING, 0.50CR - 0.55NI - 0.20MO (0.18 - 0.23C) (SAE 8620) |
SAE AMS 6300 : 2015 | STEEL BARS AND FORGINGS, 0.25MO (0.35 - 0.40C) (SAE 4037) |
SAE ARP 1917 : 2013 | CLARIFICATION OF TERMS USED IN AEROSPACE METALS SPECIFICATIONS |
SAE AMS 6359 : 2015 | STEEL, SHEET, STRIP, AND PLATE 0.80CR - 1.8NI - 0.25MO (0.38 - 0.43C) (SAE 4340) |
SAE AMS 6494 : 2016 | STEEL BARS, FORGINGS, AND TUBING, 1.0CR - 2.50NI - 2.0MO - 1.10SI (0.10 - 0.20C) AIRCRAFT-QUALITY |
SAE AMS 6264 : 2014 | STEEL, CARBURIZING GRADE, BARS, FORGINGS, AND TUBING 1.2CR - 3.2NI - 0.12MO (0.14 - 0.20C) (9317) |
SAE AMS 6290 : 2013 | STEEL, BARS AND FORGINGS, CARBURIZING, 1.8NI - 0.25MO (0.11 - 0.17C) (SAE 4615) |
SAE AMS 6348 : 2013 | STEEL, BARS, 0.95CR - 0.20MO (0.28 TO 0.33C) (SAE 4130), NORMALIZED |
SAE AMS 6422K : 2016 | STEEL, BARS, FORGINGS, AND TUBING, 0.80CR - 0.85NI - 0.20MO - 0.003B - 0.04V (0.38 - 0.43C) (MODIFIED 98BV40) |
SAE J 421 : 2018 | CLEANLINESS RATING OF STEELS BY THE MAGNETIC PARTICLE METHOD |
SAE AMS S 6758 : 2017 | STEEL, CHROME-MOLYBDENUM (4130) BARS AND REFORGING STOCK (AIRCRAFT QUALITY) |
SAE AMS 6451 : 2015 | STEEL, SPRING WIRE, 1.4SI - 0.65CR (0.51 - 0.59C) (SAE 9254) OIL TEMPERED |
SAE AMS 6412 : 2015 | STEEL, BARS AND FORGINGS 0.80CR - 1.8NI - 0.25MO (0.35 - 0.40C) (4337) |
BS 6S 100:2010 | Aerospace series. Procedure for inspection, testing and acceptance of wrought steels (other than plate, sheet, strip and tube) |
SAE AMS 6280 : 2017 | STEEL BARS, FORGINGS, AND RINGS, 0.50CR - 0.55NI - 0.20MO (0.28 - 0.33C) (SAE 8630) |
SAE AMS 6304 : 2016 | LOW-ALLOY STEEL, HEAT-RESISTANT, BARS, FORGINGS, AND TUBING, 0.95CR - 0.55MO - 0.30V (0.40 - 0.50C) |
SAE AMS 6320 : 2017 | STEEL BARS, FORGINGS, AND RINGS 0.50CR - 0.55NI - 0.25MO (0.33 - 0.38C) (8735) |
SAE AMS 6484 : 2016 | STEEL, BARS, FORGINGS, AND TUBING 0.80CR - 1.8NI - 0.25MO (0.38 - 0.43C) (SAE 4340) NORMALIZED AND TEMPERED |
SAE AMS 6455 : 2016 | STEEL, SHEET, STRIP, AND PLATE, 0.95CR - 0.22V (0.48 - 0.53C) (SAE 6150) |
MIL-S-81054 Revision A:1976 | STEEL, BARS AND FORGINGS, CHROMIUM NICKEL MOLYBDENUM VANADIUM (FOR TORPEDO MK 46 MOD O) |
SAE AMS 6423 : 2016 | STEEL BARS, FORGINGS, AND TUBING, 0.92CR - 0.75NI - 0.52MO - 0.003B - 0.04V (MODIFIED 98BV40) |
SAE AMS 6325 : 2015 | STEEL, BARS, AND FORGINGS 0.50CR - 0.55NI - 0.25MO (0.38 - 0.43C) (SAE 8740) HEAT TREATED, 105 KSI (724 MPA) TENSILE STRENGTH |
SAE AMS 6358 : 2016 | STEEL SHEET, STRIP, AND PLATE, 0.50CR - 0.55NI - 0.25MO (0.38 - 0.43C) (SAE 8740) |
SAE AIR 4777 : 2013(R 2018) | NONDESTRUCTIVE INSPECTION (NDI) METHODS USED DURING PRODUCTION AND OPERATION OF AIRCRAFT WHEELS AND BRAKES |
SAE AMS 6385 : 2015 | STEEL SHEET, STRIP, AND PLATE, LOW ALLOY, HEAT-RESISTANT, 0.65SI - 1.25CR - 0.50MO - 0.25V (0.27 - 0.33C) |
SAE AMS 6539 : 2013 | STEEL BARS, FORGINGS, AND TUBING, 1.7CR - 3.8NI - 0.3MO - (0.32-0.38 C), AIRCRAFT-QUALITY |
SAE AMS 6292 : 2014 | STEEL BARS AND FORGINGS, CARBURIZING 1.8NI - 0.25MO (0.15 - 0.20C) (SAE 4617) |
SAE AMS 6324 : 2014 | STEEL BARS, FORGINGS, AND TUBING, 0.65CR - 0.70NI - 0.25MO (0.38 - 0.43C) (8740 MODIFIED) |
SAE AMS 6415 : 2016 | STEEL, BARS, FORGINGS, AND TUBING 0.80CR - 1.8NI - 0.25MO (0.38 - 0.43C) (SAE 4340) |
SAE AMS 6381 : 2017 | STEEL, MECHANICAL TUBING, 0.95CR - 0.20MO (0.38 - 0.43C) (SAE 4140) |
SAE AMS 6270 : 2014 | STEEL, BARS, FORGINGS, AND TUBING 0.50CR - 0.55NI - 0.20MO (0.13 - 0.18C) (SAE 8615) |
SAE AMS 6365 : 2014 | STEEL TUBING, SEAMLESS, 0.95CR - 0.20MO (0.33 - 0.38C) (SAE 4135), NORMALIZED OR STRESS RELIEVED |
ASTM E 709 : 2015 : REDLINE | Standard Guide for Magnetic Particle Testing |
SAE AMS 6281 : 2015 | STEEL, MECHANICAL TUBING, 0.50CR - 0.55NI - 0.20MO (0.28 - 0.33C) (SAE 8630) |
AGMA 2101 : D | FUNDAMENTAL RATING FACTORS AND CALCULATION METHODS FOR INVOLUTE SPUR AND HELICAL GEAR TEETH (METRIC EDITION) |
SAE AMS 6470 : 2014 | STEEL, NITRIDING, BARS, FORGINGS, AND TUBING 1.6CR - 0.35MO - 1.13AL (0.38 - 0.43C) (135 MOD) |
AGMA 2001 : D | FUNDAMENTAL RATING FACTORS AND CALCULATION METHODS FOR INVOLUTE SPUR AND HELICAL GEAR TEETH |
SAE AMS 6374 : 2016 | STEEL TUBING, SEAM-FREE, ROUND, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130), 95.0 KSI (655 MPA) TENSILE STRENGTH |
SAE AMS S 6098 : 1999 | STEEL, CHROME-NICKEL-MOLYBDENUM (8735) BARS AND REFORGING STOCK (AIRCRAFT QUALITY) |
SAE AMS T 5066 : 2015 | TUBING, CARBON STEEL (1025), (AIRCRAFT QUALITY) |
MIL S 18728 : D | STEEL PLATE, SHEET, AND STRIP, ALLOY, 8630, AIRCRAFT QUALITY |
AGMA 923 : B | METALLURGICAL SPECIFICATIONS OF STEEL GEARING |
SAE AMS 6294 : 2014 | STEEL BARS AND FORGINGS, CARBURIZING 1.8NI - 0.25MO (0.17 - 0.22C) (SAE 4620) |
SAE AMS6450K : 2017 | STEEL, SPRING WIRE 0.95CR - 0.22V (0.48 - 0.53C) (SAE 6150) ANNEALED AND COLD DRAWN |
SAE AMS 6260S : 2016 | STEEL, BARS, FORGINGS, AND TUBING, 1.2CR - 3.2NI - 0.12MO (0.07 - 0.13C) (9310) |
MIL-S-8503 Revision B:1978 | STEEL BARS, CHROME-VANADIUM (6150) AIRCRAFT QUALITY |
SAE AMS 6430J : 2017 | STEEL, BARS, FORGINGS, TUBING, AND RINGS, 0.75MN - 0.78CR - 1.8NI - 0.35MO - 0.20V (0.32 - 0.38C), (4335 MODIFIED) |
MIL-S-18729 Revision C:1965 | STEEL PLATE, SHEET, AND STRIP, ALLOY, 4130, AIRCRAFT QUALITY |
SAE AMS 6372 : 2017 | STEEL, MECHANICAL TUBING, 0.95CR - 0.20MO (0.33 - 0.38C) (SAE 4135) |
ADS-13F-HDBK : 1997 | AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES |
SAE AMS 6496 : 2013 | STEEL BARS, FORGINGS, AND TUBING, NITRIDING, 1.4CR - 1.2MO - 0.3V (0.29 - 0.36C) AIRCRAFT-QUALITY FOR BEARING APPLICATIONS |
SAE AMS 6362 : 2014 | STEEL TUBING, SEAMLESS, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130), 150 KSI (1034 MPA) TENSILE STRENGTH |
SAE AMS 6272 : 2014 | STEEL BARS, FORGINGS, AND TUBING 0.50CR - 0.55NI - 0.20MO (0.15 - 0.20C) (SAE 8617) |
SAE AMS 6312 : 2015 | STEEL BARS, FORGINGS, AND TUBING, 1.8NI - 0.25MO (0.38 - 0.43C) (4640) |
SAE AMS S 6050 : 1998 | STEEL, CHROME-NICKEL-MOLYBDENUM (8630) BARS AND REFORGING STOCK (AIRCRAFT QUALITY) |
SAE AMS 6323 : 2017 | STEEL, MECHANICAL TUBING 0.50CR - 0.55NI - 0.25MO (0.38 - 0.43C) (SAE 8740) |
SAE AMS 6250 : 2015 | STEEL BARS, FORGINGS, AND TUBING, 1.5CR - 3.5NI (0.07 - 0.13C) (3310) |
SAE AMS 6437 : 2015 | STEEL, SHEET, STRIP, AND PLATE, 5.0CR - 1.3MO - 0.50V (0.38 - 0.43C) (H-11) |
SAE AMS 6373 : 2016 | STEEL, WELDED TUBING, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130) |
SAE AMS 6448 : 2013 | STEEL, BARS, FORGINGS AND TUBING 0.95CR - 0.22V (0.48 - 0.53C) (SAE 6150) |
SAE AMS 6346 : 2013 | STEEL BARS, 0.95CR - 0.20MO (0.28 TO 0.33C) (SAE 4130), HARDENED AND TEMPERED, 125 KSI (862 MPA) TENSILE STRENGTH |
SAE AMS 6424 : 2017 | STEEL BARS, FORGINGS, AND TUBING 0.80CR - 1.8NI - 0.25MO (0.49 - 0.55C) |
ISO 81400-4:2005 | Wind turbines Part 4: Design and specification of gearboxes |
SAE AMS 6356 : 2015 | STEEL, SHEET, STRIP, AND PLATE, 0.95CR - 0.20MO - (0.30 - 0.35C) (4132) |
MIL-I-6868 Revision E:1976 | INSPECTION PROCESS, MAGNETIC PARTICLE |
SAE AMS 6342 K:1990(S2015) | STEEL BARS, FORGINGS, AND TUBING, 0.80CR - 1.0NI - 0.25MO (0.38 - 0.43C) (SAE 9840) |
SAE AMS 6421 : 2016 | STEEL BARS, FORGINGS, AND TUBING 0.80CR - 0.85NI - 0.20MO - 0.003B (0.35 - 0.40C) (MODIFIED 98B37) |
MIL-S-8690 Revision B:1978 | STEEL, CHROME NICKEL MOLYBDENUM 8620, BARS AIRCRAFT QUALITY |
AGMA 2004 : C | GEAR MATERIALS, HEAT TREATMENT AND PROCESSING MANUAL |
SAE AMS 6395 : 2015 | STEEL SHEET, STRIP, AND PLATE, 0.95CR - 0.20MO (0.38 - 0.43C) (SAE 4140) |
SAE AMS 6413 : 2016 | STEEL, MECHANICAL TUBING 0.80CR - 1.8NI - 0.25MO (0.35 - 0.40C) (4337) |
SAE AMS 6475 : 2013 | STEEL, NITRIDING, BARS, FORGINGS, AND TUBING, 1.1CR - 3.5NI - 0.25MO - 1.2AL (0.21 - 0.26C) |
MIL-T-13915 Revision E:1987 | TUBE, STEEL , SEAMLESS, FOR CANNONS AND RECOILLESS RIFLES |
09/30199785 DC : 0 | BS 6S 100 - PROCEDURE FOR INSPECTION, TESTING AND ACCEPTANCE OF WROUGHT STEELS (OTHER THAN PLATE, SHEET, STRIP AND TUBE) |
SAE MAM 6304 : 1994 | LOW-ALLOY STEEL, HEAT-RESISTANT, BARS, FORGINGS, AND TUBING, 0.95CR - 0.55MO - 0.30V (0.40 - 0.50C) |
BS ISO 81400-4:2005 | Wind turbines Design and specification of gearboxes |
SAE AMS 6357 : 2015 | STEEL SHEET, STRIP, AND PLATE, 0.50CR - 0.55NI - 0.25MO (0.33 - 0.38C) (8735) |
SAE AMS 6407 : 2017 | STEEL, BARS, FORGINGS, AND TUBING, 1.2CR - 2.0NI - 0.45MO (0.27 - 0.33C) |
SAE AMS 6317K : 2017 | STEEL BARS AND FORGINGS, 1.8NI - 0.25MO (0.38 - 0.43C) (4640), HEAT TREATED, 125 KSI (862 MPA) TENSILE STRENGTH |
SAE AMS 6349 : 2017 | STEEL BARS, 0.95CR - 0.20MO (0.38 TO 0.43C) (SAE 4140), NORMALIZED |
SAE AMS7301J:2003(S2017) | Steel, Highly-Stressed Springs 0.95Cr - 0.20V (0.48 - 0.53C) (SAE 6150) Case Hardened(STABILIZED Aug 2017) |
SAE AMS 6440 : 2015 | STEEL, BARS, FORGINGS, AND TUBING, 1.45CR (0.93 - 1.05C) (SAE 52100), FOR BEARING APPLICATIONS |
SAE AMS 6330 : 2017 | STEEL BARS, FORGINGS, AND TUBING, 0.65CR - 1.25NI (0.33 - 0.38C) |
SAE AMS 6371L : 2017 | STEEL, MECHANICAL TUBING, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130) |
SAE AMS 6345 : 2015 | STEEL, SHEET, STRIP, AND PLATE, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130), NORMALIZED OR OTHERWISE HEAT TREATED |
ASTM A 646/A646M : 2017 : REDLINE | Standard Specification for Premium Quality Alloy Steel Blooms and Billets for Aircraft and Aerospace Forgings |
SAE AMS 6428 : 2014 | STEEL, BARS, FORGINGS, AND TUBING 0.78CR - 1.8NI - 0.35MO - 0.20V (0.32 - 0.38C) (4335 MOD) |
SAE AMS 6472 : 2014 | STEEL, BARS AND FORGINGS, NITRIDING 1.6CR - 0.35MO - 1.1AL (0.38 - 0.43C) (135 MOD) HARDENED AND TEMPERED, 112 KSI (772 MPA) TENSILE STRENGTH |
ASME B46.1 : 2009 | SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY) |
ASTM E 10 : 2017-05 | TEST METHOD FOR BRINELL HARDNESS OF METALLIC MATERIALS |
ASTM E 1444 : 2005 | Standard Practice for Magnetic Particle Testing |
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