SAE AMS2301K
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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Steel Cleanliness, Aircraft Quality Magnetic Particle Inspection Procedure
Available format(s)
Hardcopy , PDF
Superseded date
22-05-2020
Superseded by
Language(s)
English
Published date
21-05-2015
Publisher
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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.
| DevelopmentNote |
Supersedes SAE MAM 2301. (07/2007)
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| DocumentType |
Standard
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| Pages |
14
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| PublisherName |
SAE International
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| Status |
Superseded
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| SupersededBy | |
| Supersedes |
This specification covers steel cleanliness requirements in inch/pound units for aircraft-quality ferro-magnetic steels, other than hardenable corrosion resistant steels (See AMS2303), by magnetic particle inspection methods. This specification contains sampling, specimen preparation, inspection procedures and cleanliness rating criteria (See 8.5).
| MIL-S-6758 Revision B:1993 | STEEL, CHROME-MOLYBDENUM (4130) BARS AND REFORGING STOCK (AIRCRAFT QUALITY) |
| SAE AMS6299F | Steel Bars, Forgings, and Tubing, Carburizing 0.50Cr - 1.8Ni - 0.25Mo (0.17 - 0.23C) (SAE 4320H) |
| SAE AMS6263M | Steel Bars, Forgings, and Tubing 1.2Cr - 3.2Ni - 0.12Mo (0.11 - 0.17C) (9315) |
| SAE AMS6350N | Steel Sheet, Strip, and Plate 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130) |
| SAE AMS6327L | Steel Bars and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 125 ksi (862 MPa) Tensile Strength |
| SAE AMS6351K | 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 | Steel, Bars, Forgings, and Tubing 0.50Cr - 0.55Ni - 0.25Mo (0.48 to 0.53C) (8750) |
| SAE AMS6434H | Steel, Sheet, Strip, and Plate 0.78Cr - 1.8Ni - 0.35Mo - 0.20V (0.33 - 0.38C) (4335 Mod) |
| SAE AMS6433G | Steel, Sheet, Strip, and Plate 0.75Mn - 0.78Cr - 1.8Ni - 0.35Mo - 0.20V (0.33 - 0.38C) (4335 Mod) |
| SAE AMS6361F | Steel Tubing, Seamless 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130) 125 ksi (862 MPa) Tensile Strength |
| SAE AMS6282J | Steel Tubing, Mechanical 0.50Cr - 0.55Ni - 0.25Mo (0.33 - 0.38C) (SAE 8735) |
| SAE AMS6492A | Steel Bars, Forgings, and Tubing 1.0Cr - 3.25Ni - 0.40Mo (0.17 - 0.22C) Aircraft Quality |
| SAE AMS6302K | Low-Alloy Steel, Heat-Resistant, Bars, Forgings, and Tubing 0.65Si - 1.25Cr - 0.50Mo - 0.25V (0.28 - 0.33C) |
| SAE AMS6303J | Steel Bars and Forgings, Low Alloy, Heat-Resistant 0.65Si - 1.25Cr - 0.50Mo - 0.85V (0.25 - 0.30C) |
| SAE AMS6360M | 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 AMS6396F | Steel Sheet, Strip, and Plate 0.80Cr - 1.8Ni - 0.25Mo (0.49 - 0.55C) Annealed |
| SAE AMS6352K | 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 AMS6370P | Steel, Bars, Forgings, and Rings 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130) |
| SAE AMS6322P | Steel Bars, Forgings, and Rings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) |
| SAE AMS6427M | Steel Bars, Forgings, and Tubing 0.88Cr - 1.8Ni - 0.42Mo - 0.08V (0.28 - 0.33C) (4330 Mod) |
| SAE AMS6547 | Steel Bars, Forgings, and Tubing 1.0Cr - 3.2Ni - 0.2Mo (0.12 – 0.17C) Aircraft-Quality |
| SAE AMS6382P | Steel, Bars, Forgings, and Rings 0.95Cr - 0.20Mo (0.38 - 0.43C) (SAE 4140) Annealed |
| SAE AMS6432C | Steel Bars, Forgings, and Tubing, 1.05Cr - 0.55Ni - 1.0Mo - 0.12V (0.43 - 0.49C) |
| SAE AMS6274R | Steel, Bars, Forgings, and Tubing 0.50Cr - 0.55Ni - 0.20Mo (0.18 - 0.23C) (SAE 8620) |
| SAE AMS6300G | Steel Bars and Forgings 0.25Mo (0.35 - 0.40C) (SAE 4037) |
| SAE ARP1917A | Clarification of Terms Used in Aerospace Metals Specifications |
| SAE AMS6359K | Steel, Sheet, Strip, and Plate 0.80Cr - 1.8Ni - 0.25Mo (0.38 - 0.43C) (SAE 4340) |
| SAE AMS6494B | Steel Bars, Forgings, and Tubing 1.0Cr – 2.50Ni – 2.0Mo – 1.10Si (0.10 – 0.20C) Aircraft-Quality |
| SAE AMS6264L | Steel, Carburizing Grade, Bars, Forgings, and Tubing 1.2Cr - 3.2Ni - 0.12Mo (0.14 - 0.20C) (9317) |
| SAE AMS6290J | Steel, Bars and Forgings, Carburizing 1.8Ni - 0.25Mo (0.11 - 0.17C) (SAE 4615) |
| SAE AMS6348D | Steel, Bars 0.95Cr - 0.20Mo (0.28 to 0.33C) (SAE 4130) Normalized |
| SAE AMS6422K | Steel, Bars, Forgings, and Tubing 0.80Cr - 0.85Ni - 0.20Mo - 0.003B - 0.04V (0.38 - 0.43C) (Modified 98BV40) |
| SAE J421_201801 | Cleanliness Rating of Steels by the Magnetic Particle Method |
| SAE AMSS6758B | Steel, Chrome-Molybdenum (4130) Bars and Reforging Stock (Aircraft Quality) |
| SAE AMS6451D | Steel, Spring Wire 1.4Si - 0.65Cr (0.51 - 0.59C) (SAE 9254) Oil Tempered |
| SAE AMS6412N | 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 AMS6280M | Steel Bars, Forgings, and Rings 0.50Cr - 0.55Ni - 0.20Mo (0.28 – 0.33C) (SAE 8630) |
| SAE AMS6304M | Low-Alloy Steel, Heat-Resistant, Bars, Forgings, and Tubing 0.95Cr - 0.55Mo - 0.30V (0.40 - 0.50C) |
| SAE AMS6320P | Steel Bars, Forgings, and Rings 0.50Cr - 0.55Ni - 0.25Mo (0.33 – 0.38C) (8735) |
| SAE AMS6484E | Steel, Bars, Forgings, and Tubing 0.80Cr - 1.8Ni - 0.25Mo (0.38 - 0.43C) (SAE 4340) Normalized and Tempered |
| SAE AMS6455L | 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 AMS6423H | Steel Bars, Forgings, and Tubing 0.92Cr – 0.75Ni – 0.52Mo – 0.003B – 0.04V (Modified 98BV40) |
| SAE AMS6325K | 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 AMS6358K | Steel Sheet, Strip, and Plate 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) |
| SAE AIR4777B | Nondestructive Inspection (NDI) Methods Used During Production and Operation of Aircraft Wheels and Brakes |
| SAE AMS6385K | Steel Sheet, Strip, and Plate, Low Alloy, Heat-Resistant 0.65Si - 1.25Cr - 0.50Mo - 0.25V (0.27 - 0.33C) |
| SAE AMS6539 | Steel Bars, Forgings, and Tubing 1.7Cr – 3.8Ni – 0.3Mo (0.32 – 0.38 C) Aircraft-Quality |
| SAE AMS6292J | Steel Bars and Forgings, Carburizing 1.8Ni - 0.25Mo (0.15 - 0.20C) (SAE 4617) |
| SAE AMS6324J | Steel Bars, Forgings, and Tubing 0.65Cr - 0.70Ni - 0.25Mo (0.38 – 0.43C) (8740 Modified) |
| SAE AMS6415U | Steel, Bars, Forgings, and Tubing 0.80Cr - 1.8Ni - 0.25Mo (0.38 - 0.43C) (SAE 4340) |
| SAE AMS6381J | Steel, Mechanical Tubing 0.95Cr - 0.20Mo (0.38 - 0.43C) (SAE 4140) |
| SAE AMS6270Q | Steel, Bars, Forgings, and Tubing 0.50Cr - 0.55Ni - 0.20Mo (0.13 - 0.18C) (SAE 8615) |
| SAE AMS6365K | 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 AMS6281J | 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 AMS6470N | 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 AMS6374D | Steel Tubing, Seam-Free, Round 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130) 95.0 ksi (655 MPa) Tensile Strength |
| SAE AMSS6098A | Steel, Chrome-Nickel-Molybdenum (8735) Bars and Reforging Stock (Aircraft Quality) |
| SAE AMST5066A | 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 AMS6294J | Steel Bars and Forgings, Carburizing 1.8Ni - 0.25Mo (0.17 - 0.22C) (SAE 4620) |
| SAE AMS6450K | Steel, Spring Wire 0.95Cr - 0.22V (0.48 - 0.53C) (SAE 6150) Annealed and Cold Drawn |
| SAE AMS6260S | 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 AMS6430J | 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 AMS6372N | 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 AMS6496A | Steel Bars, Forgings, and Tubing, Nitriding 1.4Cr - 1.2Mo - 0.3V (0.29 - 0.36C) Aircraft-Quality for Bearing Applications |
| SAE AMS6362G | Steel Tubing, Seamless 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130) 150 ksi (1034 MPa) Tensile Strength |
| SAE AMS6272M | Steel Bars, Forgings, and Tubing 0.50Cr - 0.55Ni - 0.20Mo (0.15 - 0.20C) (SAE 8617) |
| SAE AMS6312J | Steel Bars, Forgings, and Tubing 1.8Ni - 0.25Mo (0.38 - 0.43C) (4640) |
| SAE AMSS6050B | Steel, Chrome-Nickel-Molybdenum (8630) Bars and Reforging Stock (Aircraft Quality) |
| SAE AMS6323M | Steel, Mechanical Tubing 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) |
| SAE AMS6250M | Steel Bars, Forgings, and Tubing 1.5Cr - 3.5Ni (0.07 - 0.13 C) (3310) |
| SAE AMS6437J | Steel, Sheet, Strip, and Plate 5.0Cr - 1.3Mo - 0.50V (0.38 - 0.43C) (H-11) |
| SAE AMS6373H | Steel, Welded Tubing 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130) |
| SAE AMS6448L | Steel, Bars, Forgings, and Tubing 0.95Cr - 0.22V (0.48 – 0.53C) (SAE 6150) |
| SAE AMS6346B | Steel Bars 0.95Cr - 0.20Mo (0.28 to 0.33C) (SAE 4130) Hardened and Tempered, 125 Ksi (862 MPa) Tensile Strength |
| SAE AMS6424G | 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 AMS6356H | 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 AMS6342K | Steel Bars, Forgings, and Tubing 0.80Cr - 1.0Ni - 0.25Mo (0.38 - 0.43C) (SAE 9840) |
| SAE AMS6421G | 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 AMS6395H | Steel Sheet, Strip, and Plate 0.95Cr - 0.20Mo - (0.38 - 0.43C) (SAE 4140) |
| SAE AMS6413M | Steel, Mechanical Tubing 0.80Cr - 1.8Ni - 0.25Mo (0.35 - 0.40C) (4337) |
| SAE AMS6475K | 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 MAM6304B | 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 AMS6357L | Steel Sheet, Strip, and Plate 0.50Cr - 0.55Ni - 0.25Mo (0.33 - 0.38C) (8735) |
| SAE AMS6407K | Steel, Bars, Forgings, and Tubing 1.2Cr - 2.0Ni - 0.45Mo (0.27 – 0.33C) |
| SAE AMS6317K | Steel Bars and Forgings 1.8Ni - 0.25Mo (0.38 – 0.43C) (4640) Heat Treated, 125 ksi (862 MPa) Tensile Strength |
| SAE AMS6349E | Steel Bars 0.95Cr - 0.20Mo (0.38 to 0.43C) (SAE 4140) Normalized |
| SAE AMS7301J | Steel, Highly-Stressed Springs 0.95Cr - 0.20V (0.48 - 0.53C) (SAE 6150) Case Hardened |
| SAE AMS6440S | Steel, Bars, Forgings, and Tubing 1.45Cr (0.93 - 1.05C) (SAE 52100) For Bearing Applications |
| SAE AMS6330J | Steel Bars, Forgings, and Tubing 0.65Cr - 1.25Ni (0.33 – 0.38C) |
| SAE AMS6371L | Steel, Mechanical Tubing 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130) |
| SAE AMS6345D | 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 AMS6428K | Steel, Bars, Forgings, and Tubing 0.78Cr - 1.8Ni - 0.35Mo - 0.20V (0.32 - 0.38C) (4335 Mod) |
| SAE AMS6472F | 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 |
| SAE AMS6475L | Steel, Nitriding, Bars, Forgings, and Tubing 1.1Cr - 3.5Ni - 0.25Mo - 1.2Al (0.21 - 0.26C) |
| 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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