SAE AMS 2175 : 2010
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
CASTINGS, CLASSIFICATION AND INSPECTION OF
Available format(s)
Hardcopy , PDF
Superseded date
02-09-2019
Language(s)
English
Published date
01-01-2010
Publisher
1. SCOPE
2. APPLICABLE DOCUMENTS
3. TECHNICAL REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. ACKNOWLEDGMENT
7. REJECTIONS
8. NOTES
Sets up non-destructive testing methods, sampling frequency, and acceptance criteria for the inspection of metal castings.
| Committee |
AMS-B
|
| DevelopmentNote |
Supersedes SAE AMS STD 2175 (10/2003)
|
| DocumentType |
Standard
|
| Pages |
20
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| SAE AMS 5349 : 2013 | STEEL, CORROSION-RESISTANT, INVESTMENT CASTINGS, 13CR, FREE MACHINING; HARDENED AND TEMPERED |
| SAE AMS 5346 : 2014 | STEEL, CORROSION-RESISTANT, INVESTMENT CASTINGS, 15CR - 4.6NI - 0.22CB (NB) - 2.8CU, SOLUTION AND PRECIPITATION HEAT TREATED (H925), 180 KSI (1241 MPA) TENSILE STRENGTH (15-5) |
| SAE AMS 4992 : 2014 | CASTING, STRUCTURAL INVESTMENT, TITANIUM ALLOY 6AL - 4V HOT ISOSTATICALLY PRESSED |
| SAE AMS 2694 : 2013 | IN-PROCESS WELDING OF CASTINGS |
| SAE AMS A 21180 : 2017 | ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH |
| MIL-DTL-23599 Revision C:2017 | Hook, Rescue |
| SAE AMS 5396 : 2014 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS, 65NI - 28MO - 5.5FE - 0.40V (N-12MV), AS-CAST |
| SAE AMS 4284 : 2017 | ALUMINUM ALLOY CASTINGS, PERMANENT MOLD, 7.0SI - 0.30MG (356.0-T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 4217 : 2018 | ALUMINUM ALLOY, CASTINGS, 7.0SI - 0.32MG (356.0-T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 4223 : 2015 | ALUMINUM ALLOY, CASTINGS, 4.5CU - 0.70AG - 0.30MN - 0.25MG - 0.25TI (A201.0-T4), SOLUTION HEAT TREATED AND NATURALLY AGED |
| SAE AMS 4241 : 2015 | ALUMINUM ALLOY CASTINGS, 7.0SI - 0.58MG - 0.15TI - 0.06BE (D357.0-T6), SOLUTION AND PRECIPITATION HEAT TREATED, DENDRITE ARM SPACING (DAS) CONTROLLED |
| SAE AMS 5390 : 2014 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS, 47.5NI - 22CR - 1.5CO - 9MO - 0.60W - 18.5FE (N-12MV) AS-CAST |
| SAE AMS 4280 : 2014 | ALUMINUM ALLOY CASTINGS, PERMANENT MOLD, 5.0SI - 1.2CU - 0.5MG (355.0-T71), SOLUTION HEAT TREATED AND OVERAGED |
| SAE AMS 5401 : 2004 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS, 62NI - 21.5CR - 9.0MO - 3.6CB (NB), VACUUM MELTED, VACUUM CAST, AS CAST |
| MIL-STD-2088 Revision B:2007 | BOMB RACK UNIT (BRU), SINGLE STORE, AIRCRAFT |
| DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-DTL-87104 Revision C:2014 | COAXIAL ASSEMBLIES, GENERAL SPECIFICATION FOR |
| MIL-PRF-7115 Revision G:2012 | CONVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR |
| SAE AMS5356D:2016(R2022) | Steel, Corrosion-Resistant, Investment Castings 15Cr - 4.6Ni - 0.22Cb - 2.8Cu Solution and Precipitation Heat Treated (H1100) 130 ksi (896 MPa) Tensile Strength |
| SAE AMS5350K:2017(R2022) | Steel, Corrosion and Moderate Heat-Resistant, Investment Castings 12.5Cr (410) Hardened and Tempered |
| MIL STD 11991 : A | GENERAL STANDARD FOR PARTS, MATERIALS, AND PROCESSES |
| SAE AMS 4286 : 2015 | ALUMINUM ALLOY CASTINGS, PERMANENT MOLD, 7.0SI - 0.32MG (356.0-T51), AS-CAST THEN PRECIPITATION HEAT TREATED |
| SAE AMS 5366 : 2012 | STEEL, CORROSION AND HEAT RESISTANT, INVESTMENT CASTING 25CR - 20NI (CK-20) AS-CAST |
| MIL-DTL-16377 Revision J:2014 | Fixtures, Lighting; and Associated Parts; Shipboard Use, General Specification for |
| MIL-STD-1587 Revision D:2017 | MATERIAL AND PROCESS REQUIREMENTS FOR AEROSPACE WEAPONS SYSTEMS |
| SAE AMS 4235 : 2015 | ALUMINUM ALLOY CASTINGS, 4.6CU - 0.35MN - 0.25MG - 0.22TI (A206.0-T7), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 4290 : 2017 | ALUMINUM ALLOY, DIE CASTINGS 9.5SI - 0.50MG (360.0-F), AS CAST |
| SAE AMS 4484 : 2013 | MAGNESIUM ALLOY CASTINGS, PERMANENT MOLD, 9.0AL - 2.0ZN (AZ92A-T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 4406 : 2018 | Aluminum Alloy, Centrifugal Castings 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (709.0-T61) Hot Isostatically Pressed, Solution and Precipitation Heat Treated |
| SAE AMS 4210 : 2012 | ALUMINUM ALLOY, CASTINGS - 5.0SI - 1.2CU - 0.50MG (355.0-T51) PRECIPITATION HEAT TREATED |
| SAE AMS 5399 : 2012 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS, 52NI - 19CR - 11CO - 9.8MO - 3.2TI - 1.6AL - 0.006B, VACUUM-MELTED, VACUUM-CAST, SOLUTION HEAT TREATED |
| SAE AMS 4985 : 2014 | TITANIUM ALLOY, INVESTMENT CASTINGS 6AL - 4V 130 UTS, 120 YS, 6% EL HOT ISOSTATICALLY PRESSED ANNEAL OPTIONAL OR WHEN SPECIFIED |
| SAE ARP 5794 : 2014 | CENTRIFUGAL AIRCRAFT FUEL PUMP REQUIREMENTS, DESIGN AND TESTING, AEROSPACE STANDARD |
| SAE AMS 4873 : 2016 | ALUMINUM BRONZE ALLOY, SAND CASTINGS - 85CU - 11AL - 3.6FE - SOLUTION HEAT TREATED AND TEMPERED |
| SAE AMS 5383 : 2012 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS, 52.5NI - 19CR - 3.0MO - 5.1CB(NB) - 0.90TI - 0.60AL - 18FE, VACUUM MELTED HOMOGENIZATION AND SOLUTION HEAT TREATED |
| SAE AMS 5377 : 2013 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS 73NI - 12CR - 4.5MO - 2.0CB - 0.70TI - 0.05C - 6.0AL - 0.010 - 0.10ZR VACUUM CAST, AS-CAST |
| SAE AMS 4892 : 2017 | ALLOY CASTINGS, CORROSION AND HEAT-RESISTANT, 66NI - 29CU - 4.0SI, AS CAST |
| SAE AMS 5347 : 2014 | STEEL, CORROSION-RESISTANT, INVESTMENT CASTINGS, 15CR - 4.6NI - 0.22CB (NB) - 2.8CU, SOLUTION AND PRECIPITATION HEAT TREATED (H1000), 150 KSI (1034 MPA) TENSILE STRENGTH (15-5) |
| SAE AMS 4483 : 2013 | MAGNESIUM ALLOY CASTINGS, PERMANENT MOLD, 10AL (AM100A-T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 5356 : 2016 | STEEL, CORROSION RESISTANT, INVESTMENT CASTINGS, 15CR - 4.6NI - 0.22CB - 2.8CU, SOLUTION AND PRECIPITATION HEAT TREATED (H1100), 130 KSI (896 MPA) TENSILE STRENGTH |
| SAE AMS 5387 : 2015 | ALLOY, CORROSION AND HEAT RESISTANT, INVESTMENT CASTINGS, 60CO - 29CR - 4.5W, AS CAST |
| SAE AMS 5342 : 2014 | STEEL, CORROSION-RESISTANT, INVESTMENT CASTINGS, 16CR - 4.1NI - 0.28CB (NB) - 3.2CU, HOMOGENIZATION, SOLUTION, AND PRECIPITATION HEAT TREATED (H1100), 130 KSI (896 MPA) TENSILE STRENGTH (17-4) |
| SAE AMS 4285 : 2017 | ALUMINUM ALLOY CASTINGS, CENTRIFUGAL, 7.0SI - 0.30MG (356.0-T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| MIL-HDBK-115 Revision C:2016 | U.S. ARMY REVERSE ENGINEERING HANDBOOK (GUIDELINES AND PROCEDURES) |
| MIL-PRF-81975 Revision C:2008 | COUPLINGS, REGULATED, AERIAL PRESSURE REFUELING TYPE MA-2, TYPE MA-3 AND TYPE MA-4 |
| SAE AMS 4249B : 2012 (R2018) | ALUMINUM ALLOY CASTINGS 7.0SI - 0.58MG - 0.15TI - 0.06BE (D357.0-T6) SOLUTION AND PRECIPITATION HEAT TREATED (REQUIRING FATIGUE AND FRACTURE TOUGHNESS TESTING) |
| MIL-DTL-6396 Revision F:2008 | TANKS, FUEL, OIL, COOLING FLUIDS, INTERNAL, REMOVABLE NON-SELF-SEALING |
| SAE AMS 5344 : 2013 | STEEL, CORROSION-RESISTANT, INVESTMENT CASTINGS, 16CR - 4.1NI - 0.28CB - 3.2CU, HOMOGENIZATION, SOLUTION, AND PRECIPITATION HEAT TREATED (H900), 180 KSI (1241 MPA) TENSILE STRENGTH (17-4) |
| SAE AMS 5412 : 2012R(2018) | STEEL CASTINGS, VACUUM MELTED, VACUUM CAST, INVESTMENT, CORROSION RESISTANT 13CR - 8.0NI - 2.2MO - 1.1AI (195,000 PSI (1344 MPA) TENSILE STRENGTH (CONDITION H1000) HOMOGENIZED, SOLUTION, AND PRECIPITATION HEAT TREATED |
| SAE AMS 4439 : 2012 | MAGNESIUM ALLOY CASTINGS, 4.2ZN - 1.2 RARE EARTHS - 0.7ZR (ZE41A-T5), PRECIPITATION HEAT TREATED |
| SAE AMS 5343 : 2014 | STEEL, CORROSION-RESISTANT, INVESTMENT CASTINGS, 16CR - 4.1NI - 0.28CB (NB) - 3.2CU, HOMOGENIZATION, SOLUTION, AND PRECIPITATION HEAT TREATED (H1000), 150 KSI (1034 MPA) TENSILE STRENGTH (17-4) |
| SAE AMS 5338 : 2017 | STEEL, INVESTMENT CASTINGS, 0.95CR - 0.20MO (0.35 - 0.45C) (4140 MOD), NORMALIZED OR NORMALIZED AND TEMPERED |
| SAE AMS 4482 : 2012 | CAST ALUMINUM ALLOY COMPOSITE 4.6 CU - 3.4TI - 1.4B - 0.75AG - 0.27MG (A205.0/TIB2/3P-T7P) SAND CAST, SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 4225 : 2018 | ALUMINUM ALLOY, HEAT-RESISTANT, CASTINGS, 5.0CU - 1.5NI - 0.25MN - 0.25SB - 0.25CO - 0.20TI - 0.20ZR (203.0-T6), SOLUTION HEAT TREATED AND PRECIPITATION HEAT TREATED |
| SAE AMS 5388 : 2014 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS 53.3NI - 16.5CR - 17MO - 4.5W - 5.8FE - 0.40V (CW-12MW), AS-CAST |
| SAE AMS 4212 : 2016 | Aluminum Alloy Castings 5.0Si - 1.2Cu - 0.50Mg (355.0-T6) Solution and Precipitation Heat Treated |
| SAE AMS 5400 : 2014 | STEEL, CORROSION-RESISTANT, INVESTMENT CASTINGS, 15CR - 4.6NI - 0.22CB - 2.8CU, SOLUTION AND PRECIPITATION HEAT TREATED (H935), 170 KSI (1172 MPA) TENSILE STRENGTH |
| SAE AMS 4443 : 2017 | MAGNESIUM ALLOY, SAND CASTINGS, 4.5ZN - 0.75ZR (ZK51A-T5) PRECIPITATION HEAT TREATED |
| SAE AMS 5385 : 2013 | COBALT ALLOY, CORROSION AND HEAT RESISTANT, INVESTMENT CASTINGS, 62MO - 27CR - 2.8NI - 5.5MO, AS-CAST |
| SAE AMS 7918 : 2016 | BERYLLIUM ALUMINUM ALLOY INVESTMENT CASTINGS, 64.9BE - 30AL - 3AG - 1CO - 0.75GE, AS CAST |
| SAE AMS 5410 : 2017 | NICKEL ALLOY, CORROSION AND HEAT RESISTANT, INVESTMENT CASTINGS, 61NI - 16CR - 8.5CO - 1.8MO - 2.6W - 0.85CB (NB) - 3.4TI - 1.8TA - 3.4AL - 0.010B - 0.05ZR, VACUUM MELTED, VACUUM CAST AS CAST, OR SOLUTION TREATED, OR SOLUTION AND PRECIPITATION HARDENED |
| NASA STD 6016(INT) : 2006 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
| NASA STD 5005 : 2013 | STANDARD FOR THE DESIGN AND FABRICATION OF GROUND SUPPORT EQUIPMENT |
| NASA STD 5005(INT) : 2007 | THE DESIGN AND FABRICATION OF GROUND SUPPORT EQUIPMENT |
| NASA KSC DE 512-SM : 2012 | FACILITY SYSTEMS, GROUND SUPPORT SYSTEMS, AND GROUND SUPPORT EQUIPMENT GENERAL DESIGN REQUIREMENTS |
| NASA STD 6016 : 2016 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
| NASA MSFC STD 3716 : 2017 | STANDARD FOR ADDITIVELY MANUFACTURED SPACEFLIGHT HARDWARE BY LASER POWDER BED FUSION IN METALS |
| NASA JSC 27301 : 2009 | MATERIALS AND PROCESSES SELECTION, CONTROL, AND IMPLEMENTATION PLAN FOR JSC FLIGHT HARDWARE |
| MIL-PRF-21480 Revision B:2010 | GENERATOR SYSTEM, ELECTRIC POWER, 400 HERTZ, ALTERNATING CURRENT, AIRCRAFT - GENERAL SPECIFICATION FOR |
| MIL-PRF-57267 Base Document:2017 | COUPLING, AERIAL PRESSURE REFUELING TYPE MA-5 |
| SAE AMS 4219 : 2015 | ALUMINUM ALLOY CASTINGS, 7.0SI - 0.55MG - 0.12TI - 0.06BE (A357.0 T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| MIL-DTL-9490 Revision E:2008 | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-DTL-7899 Revision D:2014 | VALVES, CHECK, AIRCRAFT FUEL SYSTEM |
| SAE AMS 4214 : 2013 | CASTINGS, ALUMINUM ALLOY SAND, 5.0SI - 1.2CU - 0.50MG (355.0-T71), SOLUTION HEAT TREATED AND OVERAGED |
| SAE AMS 4261 : 2017 | ALUMINUM ALLOY CASTINGS, INVESTMENT, 7.0SI - 0.32MG (356.0-T51), PRECIPITATION HEAT TREATED |
| MIL-DTL-2036 Revision E:2014 | ENCLOSURES FOR ELECTRIC AND ELECTRONIC EQUIPMENT, NAVAL SHIPBOARD |
| SAE AMS 5368 : 2012 | STEEL, CORROSION-RESISTANT, INVESTMENT CASTINGS 15CR - 4.0NI - 2.3MO - 0.09N SOLUTION HEAT TREATED |
| 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 AMS 4893 : 2017 | ALLOY CASTINGS, CORROSION AND HEAT-RESISTANT, 66NI - 29CU - 4.0SI, SOLUTION TREATED |
| SAE AMS 5334 : 2013 | STEEL, INVESTMENT CASTINGS, 0.50CR - 0.55NI - 0.20MO (0.25 - 0.35C) (SAE 8630 MOD), NORMALIZED AND TEMPERED |
| ASTM E 1417/E1417M : 2016 : REDLINE | Standard Practice for Liquid Penetrant Testing |
| SAE AMS 4236 : 2015 | ALUMINUM ALLOY CASTINGS, 4.6CU - 0.35MN - 0.25MG - 0.22TI (A206.0-T4), SOLUTION HEAT TREATED AND NATURALLY AGED |
| SAE AMS 4229 : 2015 | ALUMINUM ALLOY CASTINGS, HIGH STRENGTH, 4.5CU - 0.70AG - 0.30MN - 0.25MG - 0.25TI (A201.0-T7), SOLUTION HEAT TREATED AND OVERAGED |
| SAE AMS 4452 : 2012 | MAGNESIUM ALLOY, INVESTMENT CASTINGS, 8.7AL - 0.70ZN - 0.22MN (AZ91C-T6) SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 4215 : 2013 | ALUMINUM ALLOY, CASTINGS, 5.0SI - 1.2CU - 0.50MG (C355.0-T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 4453 : 2012 | MAGNESIUM ALLOY, INVESTMENT CASTINGS, 9.0AL - 2.0ZN (AZ92A-T6) SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 5357 : 2017 | STEEL, CORROSION RESISTANT, INVESTMENT CASTINGS, 15CR - 4.6NI - 0.22CB - 2.8CU, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
| SAE AMS 5339 : 2017 | STEEL, MARAGING, INVESTMENT CASTINGS, 17NI - 10CO - 4.6MO - 0.30TI - 0.06AL, VACUUM MELTED, HOMOGENIZED, OVERAGED AND SOLUTION HEAT TREATED |
| SAE AMS 4281 : 2014 | ALUMINUM ALLOY CASTINGS, PERMANENT MOLD, 5.0SI - 1.2CU - 0.50MG (355.0-T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 5352 : 2015 | STEEL, CORROSION-RESISTANT, INVESTMENT CASTINGS, 17CR - 0.55MO (0.95 - 1.20C), ANNEALED |
| SAE AMS 4455 : 2012 | MAGNESIUM ALLOY, INVESTMENT CASTINGS, 10AL (AM100A-T6) SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 5333 : 2017 | STEEL, INVESTMENT CASTINGS, 0.50CR - 0.55NI - 0.25MO (0.11 - 0.17C) (SAE 8615), NORMALIZED |
| SAE AMS 5350 : 2017 | STEEL, CORROSION AND MODERATE HEAT-RESISTANT, INVESTMENT CASTINGS, 12.5CR (410), HARDENED AND TEMPERED |
| SAE AMS 5336 : 2017 | STEEL, INVESTMENT CASTINGS, 0.95CR - 0.20MO (0.25 - 0.35C) (4130 MOD) NORMALIZED OR NORMALIZED AND TEMPERED |
| SAE AMS 5360 : 2012 | STEEL, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS, 17CR - 13NI - 1.9MO, SOLUTION HEAT TREATED |
| SAE AMS 5380 : 2013 | COBALT ALLOY, CORROSION AND HEAT RESISTANT, INVESTMENT CASTINGS, 50.5CO - 26CR - 15NI - 6.0MO, AS-CAST |
| SAE AMS5337E : 2017 | STEEL, MARAGING, INVESTMENT CASTINGS, 18.5NI - 9.0CO - 5.0MO - 0.70TI - 0.12AL, VACUUM MELTED, HOMOGENIZED, OVERAGED, AND SOLUTION HEAT TREATED |
| SAE AMS 5354 : 2012 | STEEL, CORROSION AND HEAT RESISTANT, INVESTMENT CASTINGS, 13CR - 2.0NI - 3.0W, HARDENED AND TEMPERED TO 32 - 38 HRC |
| SAE AMS 5364 : 2012 | STEEL, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS, 19.5CR - 10.5NI - 0.65CB (CF-8C), SOLUTION HEAT TREATED |
| SAE AMS 4471 : 2014 | CAST ALUMINUM ALLOY COMPOSITE 4.6CU - 3.4TI - 1.4B - 0.75AG - 0.27MG (205.0/TIB[2]/3P-T7P) INVESTMENT CAST, SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 5402 : 2004 | NICKEL ALLOY, CORROSION AND HEAT RESISTANT, INVESTMENT CASTINGS 62NI - 21.5CR - 9.0MO - 3.6CB (NB) AS CAST |
| MIL-STD-1568 Revision D:2015 | Materials and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems |
| SAE AMS 5353E : 2007(R2015) | STEEL, CORROSION-RESISTANT, INVESTMENT CASTINGS, 16CR - 1.8NI - 0.08N, AS CAST |
| SAE AMS 4242 : 2015 | ALUMINUM ALLOY, CASTINGS, 4.7CU - 0.60AG - 0.35MN - 0.25MG - 0.25TI (B201.0-T7), SOLUTION HEAT TREATED AND OVERAGED |
| ASTM F 3318 : 2018 | Standard for Additive Manufacturing – Finished Part Properties – Specification for AlSi10Mg with Powder Bed Fusion – Laser Beam |
| SAE AMS5401C:2004(R2023) | Nickel Alloy, Corrosion- and Heat-Resistant, Investment Castings 62Ni - 21.5Cr - 9.0Mo - 3.6Cb (Nb) Vacuum Melted, Vacuum Cast As Cast |
| SAE AMS4992D:2023 | Casting, Structural Investment, Titanium Alloy 6Al - 4V Hot Isostatically Pressed |
| ASTM E 446 : 2015 : REDLINE | Standard Reference Radiographs for Steel Castings Up to 2 in. (50.8 mm) in Thickness |
| ASTM E 186 : 2015 : REDLINE | Standard Reference Radiographs for Heavy-Walled (2 to 4<fraction><num>1</num><den>2</den></fraction > in. (50.8 to 114 mm)) Steel Castings |
| NAS410:2003 | NAS CERTIFICATION & QUALIFICATION OF NONDESTRUCTIVE TEST PERSONNEL |
| ASTM E 155 : 2015 : REDLINE | Standard Reference Radiographs for Inspection of Aluminum and Magnesium Castings |
| ASTM E 1320 : 2015 : REDLINE | Standard Reference Radiographs for Titanium Castings |
| ASTM E 1255 : 2016 : REDLINE | Standard Practice for Radioscopy |
| ASTM E 2104 : 2015 : REDLINE | Standard Practice for Radiographic Examination of Advanced Aero and Turbine Materials and Components |
| ASTM E 192 : 2015 : REDLINE | Standard Reference Radiographs of Investment Steel Castings for Aerospace Applications |
| ASTM E 1444 : 2005 | Standard Practice for Magnetic Particle Testing |
| ASTM E 272 : 2015 : REDLINE | Standard Reference Radiographs for High-Strength Copper-Base and Nickel-Copper Alloy Castings |
| ASTM E 280 : 2015 : REDLINE | Standard Reference Radiographs for Heavy-Walled (4<fraction><num>1</num><den>2</den></fraction > to 12 in. (114 to 305 mm)) Steel Castings |
| ASTM E 310 : 2015 : REDLINE | Standard Reference Radiographs for Tin Bronze Castings |
| ASTM E 2422 : 2017 : REDLINE | Standard Digital Reference Images for Inspection of Aluminum Castings |
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