MIL-A-8866 Revision C:1987
Current
Current
The latest, up-to-date edition.
Airplane Strength and Rigidity Reliability Requirements, Repeated Loads, Fatigue and Damage Tolerance
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Published date
20-05-1987
Publisher
€15.75
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PACKAGING
6. NOTES
Describes strength and rigidity requirements for repeated loading condition applicable to Navy procured airplanes.
| DevelopmentNote |
Partially Supersedes MIL A 008866 (B). C NOTICE 1 - Notice of Validation. (06/2004)
|
| DocumentType |
Standard
|
| Pages |
18
|
| ProductNote |
NEW CHILD NOT 2 2019 IS NOW ADDED
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
This specification defines the strength and rigidity requirements for repeated loading condition applicable to Navy procured airplanes.
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| MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-HDBK-244 Revision A:1990 | Guide to Aircraft/Stores Compatibility |
| MIL A 83444 : 0 | AIRPLANE DAMAGE TOLERANCE REQUIREMENTS |
| MIL STD 1763 : A | AIRCRAFT STORES CERTIFICATION PROCEDURES |
| MIL-A-8870 Revision C:1993 | Airplane Strength and Rigidity Vibration, Flutter, and Divergence |
| MIL-A-8867 Revision C:1987 | Airplane Strength and Rigidity Ground Tests |
| MIL-STD-2066 Base Document:1981 | CATAPULTING AND ARRESTING GEAR FORCING FUNCTIONS FOR AIRCRAFT STRUCTURAL DESIGN (S/S BY MIL-HDBK-2066) |
| MIL-A-8868 Revision B:1987 | Airplane Strength and Rigidity Data and Reports (No S/S Document) |
| MIL-DTL-9490 Revision E:2008 | Flight Control Systems - Design, Installation and Test of Piloted Aircraft, General Specification for |
| JSSG-2006 Base Document:1998 | Aircraft Structures |
| MIL-A-8861 Revision B:1986 | Airplane Strength and Rigidity Flight Loads |
| ADS-13F-HDBK : 1997 | AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES |
| MIL-HDBK-1763 Base Document:1998 | Aircraft/Stores Compatibility: Systems Engineering Data Requirements and Test Procedures |
| MIL A 8892 : 0 | AIRPLANE STRENGTH AND RIGIDITY, VIBRATION |
| MIL-A-8863 Revision C:1993 | Airplane Strength and Rigidity Ground Loads for Navy Acquired Airplanes |
| MIL-STD-2066 Base Document:1981 | CATAPULTING AND ARRESTING GEAR FORCING FUNCTIONS FOR AIRCRAFT STRUCTURAL DESIGN (S/S BY MIL-HDBK-2066) |
| MIL-A-8870 Revision C:1993 | Airplane Strength and Rigidity Vibration, Flutter, and Divergence |
| MIL-L-22589 Revision D:1991 | Launching System, Nose Gear Type, Aircraft |
| MIL-A-8868 Revision B:1987 | Airplane Strength and Rigidity Data and Reports (No S/S Document) |
| MIL-A-8867 Revision C:1987 | Airplane Strength and Rigidity Ground Tests |
| MIL-A-8861 Revision B:1986 | Airplane Strength and Rigidity Flight Loads |
| MIL-D-8708 Revision C:1991 | Demonstration: Aircraft Weapon Systems, General Specification for |
| MIL-A-8860 Revision B:1987 | Airplane Strength and Rigidity, General Specification for |
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