MIL-F-83142 Revision A:1969
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Forging, Titanium Alloys, Premium Quality (See Notice 5 for Replacement Information)
12-01-1969
05-15-2006
1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISION
5. PREPARATION FOR DELIVERY
6. NOTES
Requirements for aircraft and aerospace quality titanium alloy forgings.
| DevelopmentNote |
A NOTICE 1 - Notice of Validation. A NOTICE 2 - Notice of Validation. A NOTICE 3 - Notice of Inactivation for New Design. A NOTICE 4 - Notice of Validation. A NOTICE 5 - Notice of Cancellation/Superseded by SAE AMS 4931, SAE AMS 4965 and SAE AMS T 9047. (05/2006)
|
| DocumentType |
Standard
|
| Pages |
20
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
This specification covers unalloyed titanium and titanium alloy forgings suitable for aircraft and aerospace components.
| Standards | Relationship |
| SAE AMS4970K | Similar to |
| SAE AMS4971K | Similar to |
| SAE AMS4979H | Similar to |
| SAE AMS4966P | Similar to |
| SAE AMS4978G | Similar to |
| MIL-A-8860 Revision B:1987 | Airplane Strength and Rigidity, General Specification for |
| MIL-HDBK-1587 Base Document:1996 | Materials and Process Requirements for Air Force Weapons Systems (S/S by MIL-STD-1587) |
| MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-STD-2156 Base Document:1983 | Launcher, Rail, Guided Missile, Aircraft, General Design Criteria for |
| MIL-STD-2131 Revision A:1991 | Launcher, Ejection, Guided Missile, Aircraft, General Design Criteria for |
| MIL-STD-1547 Revision B:1992 | Electronic Parts, Materials, and Processes for Space and Launch Vehicles |
| SAE AS8860 | Landing Gear Structural Requirements as Listed in the MIL-886X Series of Specifications |
| MIL A 87221 : 0 | AIRCRAFT STRUCTURES, GENERAL SPECIFICATION FOR REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
| JSSG-2006 Base Document:1998 | Aircraft Structures |
| MIL-HDBK-270 Revision A:1991 | Metallic Materials for Low Magnetic Applications, Magnetic Permeability and Electrical Conductivity, Characteristics of (Metric) |
| MIL-W-5013 Revision L:1991 | Wheel and Brake Assemblies, Aircraft General Specification For |
| MIL I 8950 : B | INSPECTION, ULTRASONIC, WROUGHT METALS, PROCESS FOR |
| MIL I 6866 : B | INSPECTION, PENETRANT METHOD OF |
| ASTM E 8 : 2004 | Standard Test Methods for Tension Testing of Metallic Materials |
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