SAE AMS2640K
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
View Superseded by
MAGNETIC PARTICLE INSPECTION
Hardcopy , PDF
English
01-04-1996
01-04-1996
1. SCOPE
2. APPLICABLE DOCUMENTS
3. TECHNICAL REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. ACKNOWLEDGMENT
7. REJECTIONS
8. NOTES
Specifies procedures for wet and dry methods of magnetic particle inspection.
| DocumentType |
Standard
|
| Pages |
9
|
| PublisherName |
SAE International
|
| Status |
Withdrawn
|
| SupersededBy | |
| Supersedes |
| Standards | Relationship |
| MIL-I-6868 Revision E:1976 | Similar to |
| 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) |
| SAE MA4070 | Pins, Procurement Specification For, Metric |
| SAE AS1177B | Nondestructive Inspection Standards for Bolts and Screws |
| MIL BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
| MIL-T-81364 Base Document:1966 | T-BOLT, 180,000 PSI, TYPE 431 STAINLESS STEEL, MANUFACTURING PROCESS REQUIREMENTS (NO S/S DOCUMENT) |
| SAE AMS5351G | Steel Castings, Sand, Corrosion and Moderate Heat Resistant 13Cr Normalized and Tempered |
| SAE MA1784 | Spacers and Washers, Procurement Specification For, Metric |
| SAE MA1937A | Nut, Hex, Free Running, Procurement Specification For, Metric |
| SAE AMS5328E | Steel Castings, Investment 0.80Cr - 1.8Ni - 0.35Mo (0.28 - 0.36C) (SAE 4330 Modified) Annealed |
| SAE AMS5412A | Steel Castings, Vacuum Melted, Vacuum Cast, Investment, Corrosion-Resistant 13Cr - 8.0Ni - 2.2Mo - 1.1Al (195 ksi (1344 MPa) Tensile Strength (Condition H1000) Homogenized, Solution, and Precipitation Heat Treated |
| MS172236THRUMS172270 Revision B:1974 | NUT, SPANNER, BEARING RETAINING, AERONAUTICAL (ASG) (S/S BY SAE-AS172236THRUAS172270) |
| SAE J420_201801 | Magnetic Particle Inspection |
| MIL-Q-22631 Revision B:1964 | Quality Control of Metal Wrought Products Except Forgings Procured to Non-Governmental Specification (No S/S Document) |
| SAE AMS5348C | Steel Castings, Tubular, Centrifugal, Corrosion Resistant 15Cr - 4.6Ni - 0.22 (Cb+Ta) - 2.8Cu Solution Heat Treated |
| SAE AMS7304F | Springs, Steel 0.85 - 1.05C Hardened and Tempered After Forming |
| SAE AMSS6098A | Steel, Chrome-Nickel-Molybdenum (8735) Bars and Reforging Stock (Aircraft Quality) |
| SAE AMST5066A | Tubing, Carbon Steel (1025), (Aircraft Quality) |
| SAE AMS5115J | Wire, Carbon Steel 0.60 - 0.75C Hardened and Tempered |
| MIL-S-8503 Revision B:1978 | STEEL BARS, CHROME-VANADIUM (6150) (AIRCRAFT QUALITY) (ASG) (S/S BY SAE-AMS6448) |
| MIL-S-18729 Revision C:1965 | STEEL PLATE, SHEET, AND STRIP, ALLOY, 4130, AIRCRAFT QUALITY (S/S BY SAE-AMS6350, SAE-AMS6351 OR SAE-AMS6345) |
| SAE AMS5330E | Steel Castings, Investment 0.80Cr - 1.8Ni - 0.35Mo (0.38 - 0.46C) (SAE 4340 Modified) Annealed |
| MIL-S-8690 Revision B:1978 | STEEL, CHROME-NICKEL-MOLYBDENUM, 8620, BARS, AIRCRAFT QUALITY (S/S BY SAE-AMS6274) |
| AN103901THRUAN104000 Revision 3:1986 | BOLT - DRILLED HEX HEAD, 6 HOLES, .3125-24 |
| MIL R 25532 : A | ROCKET MOTOR, AERONAUTICAL, QUALIFICATION TEST FOR |
| SAE AMS3046F | Magnetic Particles, Fluorescent Wet Method, Oil Vehicle, Aerosol Packaged |
| SAE AMSS6050B | Steel, Chrome-Nickel-Molybdenum (8630) Bars and Reforging Stock (Aircraft Quality) |
| SAE AMS3161C | Oil, Odorless Heavy Solvent |
| SAE AMS3160J | Solvent, Petroleum |
| SAE AMS2350BA | Standards and Test Methods |
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