MIL A 8892 : 0
Superseded
View Superseded by
AIRPLANE STRENGTH AND RIGIDITY, VIBRATION
English
07-23-2013
Covers general requirements and criteria for control of structural vibrations in design and construction of airplanes, comfort. Also covers flight and ground tests required to determine vibration characteristics.
| DocumentType |
Standard
|
| Pages |
19
|
| ProductNote |
New child NOT 1 1987 is added
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
| MIL A 8893 : 0 | AIRPLANE STRENGTH AND RIGIDITY, SONIC FATIGUE |
| MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-S-8812 Revision D:1975 | Steering System, Aircraft General Requirements for |
| MIL T 25920 : C | TESTS, GROUND AND FLIGHT, AIRCRAFT GAS TURBINE PROPULSION SYSTEM INSTALLATION |
| JSSG-2006 Base Document:1998 | Aircraft Structures |
| MIL A 8893 : 0 | AIRPLANE STRENGTH AND RIGIDITY, SONIC FATIGUE |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL-A-8870 Revision C:1993 | Airplane Strength and Rigidity Vibration, Flutter, and Divergence |
| MIL A 8862 : 0 | AIRPLANE STRENGTH AND RIGIDITY, LANDPLANE, LANDING AND GROUND HANDLING LOADS |
| MIL-S-8812 Revision D:1975 | Steering System, Aircraft General Requirements for |
| MIL-A-8868 Revision B:1987 | Airplane Strength and Rigidity Data and Reports (No S/S Document) |
| MIL P 17842 : NOTICE 1 | POWER PLANT VIBRATION ISOLATOR, DESIGN AND INSTALLATION REQUIREMENTS |
| MIL-A-8866 Revision C:1987 | Airplane Strength and Rigidity Reliability Requirements, Repeated Loads, Fatigue and Damage Tolerance |
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