SAE AMS2773E
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
HEAT TREATMENT, CAST NICKEL ALLOY AND COBALT ALLOY PARTS
02-05-2022
11-02-2013
1 SCOPE
2 APPLICABLE DOCUMENTS
3 TECHNICAL REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PREPARATION FOR DELIVERY
6 ACKNOWLEDGMENT
7 REJECTIONS
8 NOTES
Describes the engineering requirements for heat treatment, by part fabricators (users) or their vendors or subcontractors, of parts made of cast nickel or cobalt alloys and of fabricated assemblies in which cast nickel or cobalt alloys are the primary structural components.
| Committee |
AMS-F
|
| DocumentType |
Revision
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| NASA STD 6016 : 2016 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
| SAE AMS5402C | NICKEL ALLOY, CORROSION AND HEAT RESISTANT, INVESTMENT CASTINGS 62NI - 21.5CR - 9.0MO - 3.6CB (NB) AS CAST |
| 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 |
| BB-H-1168 Revision D:2010 | HELIUM, TECHNICAL |
| 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 |
| MIL-PRF-27407 Revision D:2014 | PROPELLANT PRESSURIZING AGENT, HELIUM |
| CGA G 11.1 : 2016 | COMMODITY SPECIFICATION FOR ARGON |
| MIL A 18455 : C | ARGON, TECHNICAL |
| ASTM E 384 : 2017 : REDLINE | Standard Test Method for Microindentation Hardness of Materials |
| SAE AMS5382J | COBALT ALLOY, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS, 54CO - 25.5CR - 10.5NI - 7.5A, AS-CAST |
| 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 5396 : 2014 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS, 65NI - 28MO - 5.5FE - 0.40V (N-12MV), AS-CAST |
| 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 |
| ASTM E 10 : 2017-05 | TEST METHOD FOR BRINELL HARDNESS OF METALLIC MATERIALS |
| SAE AMS2750E | PYROMETRY |
| SAE ARP1820B | CHORD METHOD OF EVALUATING SURFACE MICROSTRUCTURAL CHARACTERISTICS |
| MIL-PRF-27201 Revision E:2013 | PROPELLANT, HYDROGEN |
| SAE AMS2769B | HEAT TREATMENT OF PARTS IN A VACUUM |
| MIL-PRF-27401 Revision G:2013 | Propellant Pressurizing Agent, Nitrogen |
| SAE AMS5410B | 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 |
| SAE AMS5383E | 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 |
| CGA G 10.1 : 2016 | COMMODITY SPECIFICATION FOR NITROGEN |
| 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 |
| SAE ARP 1962 : 1995 | TRAINING AND APPROVAL OF HEAT-TREATING PERSONNEL |
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