SAE AMS 2801 : 2014
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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 OF TITANIUM ALLOY PARTS
Hardcopy , PDF
10-09-2022
English
27-02-2014
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1 SCOPE
2 APPLICABLE DOCUMENTS
3 TECHNICAL REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PREPARATION FOR DELIVERY
6 ACKNOWLEDGEMENT
7 REJECTIONS
8 NOTES
Includes engineering requirements for heat treatment by part fabricators (users) or their vendors or subcontractors.
| Committee |
AMS-G
|
| DocumentType |
Standard
|
| Pages |
15
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| MS27225 Revision C:2007 | Nipple Assembly 45 Degrees, Adapter, Hose to Tube, Reusable, Hydraulic, Fuel and Oil Lines |
| SAE AMS 4289 : 2013 | ALUMINUM ALLOY CASTINGS, 7.0SI - 0.55MG - 0.12TI (F357.0-T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AS 7102 : 2008 | NATIONAL AEROSPACE AND DEFENSE CONTRACTORS ACCREDITATION PROGRAM, REQUIREMENTS FOR HEAT TREATING |
| ASTM F 3302 : 2018 | Standard for Additive Manufacturing – Finished Part Properties – Standard Specification for Titanium Alloys via Powder Bed Fusion |
| SAE AMS H 81200 : 2014 | HEAT TREATMENT OF TITANIUM AND TITANIUM ALLOYS |
| ASTM F 2924 : 2014 : REDLINE | Standard Specification for Additive Manufacturing Titanium-6 Aluminum-4 Vanadium with Powder Bed Fusion |
| NASA STD 6016 : 2016 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
| NASA MSFC SPEC 3717 : 2017 | SPECIFICATION FOR CONTROL AND QUALIFICATION OF LASER POWDER BED FUSION METALLURGICAL PROCESSES |
| ASTM F 3001 : 2014 : REDLINE | Standard Specification for Additive Manufacturing Titanium-6 Aluminum-4 Vanadium ELI (Extra Low Interstitial) with Powder Bed Fusion |
| MS27223 Revision C:2007 | Nipple Assembly 90 Degrees, Adapter, Hose to Tube, Reusable, Hydraulic, Fuel and Oil Lines 1/4 Inch through 2 Inch Tube Sizes |
| ASTM F 3301 : 2018 | Standard for Additive Manufacturing – Post Processing Methods – Standard Specification for Thermal Post-Processing Metal Parts Made Via Powder Bed Fusion |
| SAE AMS 4914 : 2014 | TITANIUM ALLOY COLD ROLLED SHEET AND STRIP, 15V - 3AL - 3CR - 3SN, SOLUTION HEAT TREATED |
| SAE AMS 2368 : 2017 | SAMPLING AND TESTING OF WROUGHT TITANIUM RAW MATERIAL EXCEPT FORGINGS AND FORGING STOCK |
| SAE AMS 4938 : 2013 | FORGINGS, TITANIUM ALLOYS HEAT-TREATED, FINISHED-PART PROPERTIES: SHORT-TRANSVERSE TENSILE, FRACTURE TOUGHNESS, AND LONGITUDINAL TIME-DEPENDENT-TENSION |
| BB-H-1168 Revision D:2010 | HELIUM, TECHNICAL |
| MIL-PRF-27407 Revision D:2014 | PROPELLANT PRESSURIZING AGENT, HELIUM |
| MIL A 18455 : C | ARGON, TECHNICAL |
| SAE AMS 2750 : 2012 | PYROMETRY |
| SAE AMS 4901 : 2015 | TITANIUM SHEET, STRIP, AND PLATE, COMMERCIALLY PURE, ANNEALED, 70.0 KSI (485 MPA) |
| SAE ARP 1962 : 1995 | TRAINING AND APPROVAL OF HEAT-TREATING PERSONNEL |
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