SAE AMS2644F
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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 MATERIAL, PENETRANT
Hardcopy , PDF
11-04-2019
English
01-01-2013
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1 SCOPE
2 APPLICABLE DOCUMENTS
3 TECHNICAL REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PREPARATION FOR DELIVERY
6 ACKNOWLEDGEMENT
7 REJECTIONS
8 NOTES
This specification Establishes the classification, technical requirements, tests, and test procedures for the qualification, approval, and quality verification of all materials used in the liquid penetrant methods of inspection with the exception of those excluded in the application section.
| Committee |
AMS-K
|
| DevelopmentNote |
Supersedes SAE AMS 3155 and SAE AMS 3156. (12/2008) Supersedes SAE AMS 3157. (01/2009)
|
| DocumentType |
Standard
|
| Pages |
28
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| MIL-STD-1580 Revision B:2003 | DESTRUCTIVE PHYSICAL ANALYSIS FOR ELECTRONIC, ELECTROMAGNETIC, AND ELECTROMECHANICAL PARTS |
| I.S. EN 16603-32-01:2014 | SPACE ENGINEERING - FRACTURE CONTROL |
| 16/30336547 DC : 0 | BS EN 16602-70-39 - SPACE PRODUCT ASSURANCE - PART 70-39: WELDING OF METALLIC MATERIALS FOR FLIGHT HARDWARE |
| ASTM E 1417/E1417M : 2016 : REDLINE | Standard Practice for Liquid Penetrant Testing |
| MIL-STD-866 Revision C:2007 | Grinding of Chrome Plated Steel and Steel Parts Heat Treated to 180,000 PSI or Over |
| ASTM E 1210 : 2016 : REDLINE | Standard Practice for Fluorescent Liquid Penetrant Testing Using the Hydrophilic Post-Emulsification Process |
| MIL-HDBK-115 Revision C:2016 | U.S. ARMY REVERSE ENGINEERING HANDBOOK (GUIDELINES AND PROCEDURES) |
| SAE AMSA21180C | ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH |
| ASTM E 1220 : 2016 : REDLINE | Standard Practice for Visible Penetrant Testing Using Solvent-Removable Process |
| SAE AIR4777B | NONDESTRUCTIVE INSPECTION (NDI) METHODS USED DURING PRODUCTION AND OPERATION OF AIRCRAFT WHEELS AND BRAKES |
| DIN 29595:2007-04 | Welding in aerospace - Fusion welded metallic components - Requirements |
| FAA AC 33-6 : 2017 | WELD REPAIR OF ALUMINUM CRANKCASES AND CYLINDERS OF PISTON ENGINES |
| MS9769 Revision B:2008 | REDUCER, TUBE - STRAIGHT, TUBE TO BOSS |
| A-A-58050 Revision A:2000 | FLUORESCENT PENETRANT INSPECTION UNITS INTEGRALLY ASSEMBLED SINGLE UNIT AND SEPARATE MODULAR STATION TYPES |
| SAE AMS I 83387 : 2016 | INSPECTION PROCESS, MAGNETIC RUBBER |
| SAE AMS4993F | TITANIUM ALLOY, BLENDED POWDER COMPACTS, SINTERED, 6AL - 4V |
| BS EN 16603-32-01:2014 | Space engineering. Fracture control |
| 15/30319706 DC : 0 | BS EN 1279-6 - GLASS IN BUILDING - INSULATING GLASS UNITS - PART 6: FACTORY PRODUCTION CONTROL AND PERIODIC TESTS |
| SAE AMS4242C | ALUMINUM ALLOY, CASTINGS, 4.7CU - 0.60AG - 0.35MN - 0.25MG - 0.25TI (B201.0-T7), SOLUTION HEAT TREATED AND OVERAGED |
| SAE AMS2647F | FLUORESCENT PENETRANT INSPECTION, AIRCRAFT AND ENGINE COMPONENT MAINTENANCE |
| SAE AMSA22771D | ALUMINUM ALLOY FORGINGS, HEAT TREATED |
| MIL-STD-1501 Revision F:2011 | Chromium Plating, Low Embrittlement, Electrodeposition |
| SAE AMS 2453 : 2015 | LOW STRESS GRINDING OF STEEL PARTS HEAT TREATED TO 180 KSI OR OVER, AND LOW STRESS GRINDING OF CHROME PLATING APPLIED TO STEEL PARTS HEAT TREATED TO 180 KSI OR OVER |
| ASTM E 2982 : 2014 | Standard Guide for Nondestructive Testing of Thin-Walled Metallic Liners in Filament-Wound Pressure Vessels Used in Aerospace Applications |
| EN 16603-32-01:2014 | Space engineering - Fracture control |
| SAE AMS 5391 : 2014 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS, 73NI - 0.14C - 13CR - 4.5MO - 2.3CB (NB) - 0.75TI - 6.0AL - 0.010B - 0.10ZR VACUUM CAST, AS-CAST |
| SAE AMS4035K | ALUMINUM ALLOY, SHEET AND PLATE, 4.4CU - 1.5MG - 0.60MN (2024-0) ANNEALED; OR WHEN SPECIFIED, 'AS FABRICATED' (2024-F) |
| SAE AMS4045L | ALUMINUM ALLOY SHEET AND PLATE 5.6ZN - 2.5MG - 1.6CU - 0.23CR 7075: (-T6 SHEET, -T651 PLATE) SOLUTION AND PRECIPITATION HEAT TREATED |
| CFR 49(PTS100-177) : OCT 2017 | TRANSPORTATION |
| ASTM G 41 : 1990 | PRACTICE FOR DETERMINING CRACKING SUSCEPTIBILITY OF METALS EXPOSED UNDER STRESS TO A HOT SALT ENVIRONMENT |
| CFR 29(PT1910.1000 TO END) : 0 | LABOR - OCCUPATIONAL SAFETY AND HEALTH ADMINISTRATION, DEPARTMENT OF LABOR |
| ASTM D 93 : 2016-07 | TEST METHODS FOR FLASH POINT BY PENSKY-MARTENS CLOSED CUP TESTER |
| ASTM E 2275 : 2014 : REDLINE | Standard Practice for Evaluating Water-Miscible Metalworking Fluid Bioresistance and Antimicrobial Pesticide Performance |
| SAE AMS6350N | STEEL SHEET, STRIP, AND PLATE, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130) |
| SAE AMS4916K | TITANIUM ALLOY SHEET, STRIP, AND PLATE 8AL - 1MO - 1V DUPLEX ANNEALED |
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