SAE AMS 2630 : 2010
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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INSPECTION, ULTRASONIC, PRODUCT OVER 0.5 INCH (12.7 MM) THICK
Hardcopy , PDF
08-08-2018
English
01-01-2010
Important note : All end users must be registered with an Account prior to user licenses being assigned.Describes procedures for ultrasonic inspection, by pulse-echo procedures, of flat, rectangular, round, cylindrical, and contoured products having a thickness or cross-sectional dimension greater than 0.50 inch (12.7 mm), using either contact or immersion methods, and using the longitudinal-wave or shear-wave modes or combinations of the two, as necessary.
| Committee |
AMS-K
|
| DocumentType |
Standard
|
| Pages |
21
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy |
| SAE AMS 7898 : 2002 | TUNGSTEN SHEET, STRIP, PLATE, AND FOIL, PRESSED, SINTERED, AND WROUGHT |
| SAE AMS 2681 : 2014 | WELDING, ELECTRON-BEAM |
| SAE ARP 4784 : 2013 | DEFINITIONS AND LIMITS, METAL MATERIAL DEFECTS AND SURFACE AND EDGE FEATURES, FLUID COUPLINGS, FITTINGS AND HOSE ENDS |
| SAE AMS 6946 : 2014 | TITANIUM ALLOY, SHEET, STRIP, AND PLATE 4AL - 2.5V - 1.5FE, ANNEALED |
| ASTM F 1314 : 2018 : REDLINE | Standard Specification for Wrought Nitrogen Strengthened 22 Chromium–13 Nickel–5 Manganese–2.5 Molybdenum Stainless Steel Alloy Bar and Wire for Surgical Implants (UNS S20910) |
| ASTM F 2581 : 2012 | Standard Specification for Wrought Nitrogen Strengthened 11Manganese-17Chromium-3Molybdenum Low-Nickel Stainless Steel Alloy Bar and Wire for Surgical Implants (UNS S29225) |
| ASTM F 562 : 2013 : REDLINE | Standard Specification for Wrought 35Cobalt-35Nickel-20Chromium-10Molybdenum Alloy for Surgical Implant Applications (UNS R30035) |
| ASTM F 2581 : 2012 : R2017 | Standard Specification for Wrought Nitrogen Strengthened 11Manganese-17Chromium-3Molybdenum Low-Nickel Stainless Steel Alloy Bar and Wire for Surgical Implants (UNS S29225) |
| SAE AMS 2680 : 2010 | ELECTRON-BEAM WELDING, FOR FATIGUE CRITICAL APPLICATIONS |
| SAE AMS 2376 : 2017 | QUALIFICATION, APPROVAL, AND CONTROL OF PREMIUM-QUALITY FORGINGS ALLOY STEELS AND HEAT-TREATABLE CORROSION AND HEAT RESISTANT STEELS AND ALLOYS |
| ASTM F 3273 : 2017 | Standard Specification for Wrought Molybdenum-47.5 Rhenium Alloy for Surgical Implants (UNS R03700) |
| ASTM F 2229 : 2012 : REDLINE | Standard Specification for Wrought, Nitrogen Strengthened 23Manganese-21Chromium-1Molybdenum Low-Nickel Stainless Steel Alloy Bar and Wire for Surgical Implants (UNS S29108) |
| FAA AC 33-6 : 2017 | WELD REPAIR OF ALUMINUM CRANKCASES AND CYLINDERS OF PISTON ENGINES |
| SAE AMS 4871 : 2010(S2015) | ALUMINUM BRONZE, CENTRIFUGAL AND CHILL CASTINGS, 85CU - 11AL - 3.6FE, SOLUTION HEAT TREATED AND TEMPERED |
| SAE AIR 4777 : 2013(R 2018) | NONDESTRUCTIVE INSPECTION (NDI) METHODS USED DURING PRODUCTION AND OPERATION OF AIRCRAFT WHEELS AND BRAKES |
| ASTM F 1295 : 2016 : REDLINE | Standard Specification for Wrought Titanium-6Aluminum-7Niobium Alloy for Surgical Implant Applications (UNS R56700) |
| SAE ARP 1317 : 1994 | ELECTRON BEAM WELDING |
| SAE AMS 4870 : 2012 | ALUMINUM BRONZE, CENTRIFUGAL AND CHILL CASTINGS 85CU - 11AL - 3.6FE AS CAST (COMPOSITION SIMILAR TO UNS C95420) |
| SAE AMS 4362 : 2014 | FORGINGS, MAGNESIUM ALLOY, 5.5ZN - 0.45ZR (ZK60A-T5), PRECIPITATION HEAT TREATED |
| SAE AMS 4881 : D2012(R2018) | NICKEL-ALUMINUM-BRONZE, MARTENSITIC, SAND, CENTRIFUGAL AND CONTINUOUS CASTINGS, 78CU - 11AL - 5.1NI - 4.8FE, QUENCH HARDENED AND TEMPER ANNEALED |
| SAE AMS 6543 : 2016 | STEEL, BARS AND FORGINGS, 2.0CR - 10NI - 8.0CO - 1.0MO (0.10 - 0.14C) (HY-180), DOUBLE VACUUM MELTED, SOLUTION HEAT TREATED, MARAGE HARDENABLE |
| ASTM F 3160 : 2016 | Standard Guide for Metallurgical Characterization of Absorbable Metallic Materials for Medical Implants |
| SAE MAM 4141 : 1990 | ALUMINUM ALLOY, DIE FORGINGS, 5.6ZN - 2.5MG - 1.6CU - 0.23CR (7075-T73) SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 6544 : 2013 | STEEL, PLATE, 2.0CR - 10NI - 8.0CO - 1.0MO (0.10 - 0.14C) (HY-180), DOUBLE VACUUM MELTED, SOLUTION HEAT TREATED |
| SAE AMS 5852 : 2001 | NICKEL ALLOY, CORROSION AND HEAT RESISTANT, BILLETS AND PREFORMS 55NI 15CR 17CO 5.0MO 3.5TI 4.0AI 0.025B, POWDER METALLURGY PRODUCT, HOT ISOSTATICALLY PRESSED |
| ASTM F 1537 : 2011 : REDLINE | Standard Specification for Wrought Cobalt-28Chromium-6Molybdenum Alloys for Surgical Implants (UNS R31537, UNS R31538, and UNS R31539) |
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