MIL-A-8868 Revision B:1987
Withdrawn
Airplane Strength and Rigidity Data and Reports (No S/S Document)
05-20-1987
05-04-1998
1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PACKAGING
6. NOTES
Covers data necessary to show compliance with the design and test requirements of MIL-A-8860 through MIL-A-8870 for the acquisition of naval airplanes. Shows dependent relationship between schedules for structural engineering analyses and testing and schedules for manufacturing.
| DevelopmentNote |
B NOTICE 1 - Notice of Cancellation without replacement. (06/2004)
|
| DocumentType |
Standard
|
| Pages |
89
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
This specification contains the requirements for data necessary to show compliance with the design and test requirements of MIL-A-8860 through MIL-A-8870 for the acquisition of naval airplanes, and to show the dependent relationship between the schedules for structural engineering analyses and testing and schedules for manufacturing.
| MIL A 8893 : 0 | AIRPLANE STRENGTH AND RIGIDITY, SONIC FATIGUE |
| MIL-A-8860 Revision B:1987 | Airplane Strength and Rigidity, General Specification for |
| MIL-A-8866 Revision C:1987 | Airplane Strength and Rigidity Reliability Requirements, Repeated Loads, Fatigue and Damage Tolerance |
| MIL-M-8555 Revision C:1984 | Missile, Guided, Design and Construction, General Specification for (No S/S Document) |
| MIL-A-8869 Revision B:1987 | Airplane Strength and Rigidity Nuclear Weapons Effects |
| MIL-HDBK-2066 Base Document:1999 | Catapulting and Arresting Gear Forcing Functions for Aircraft Structural Design |
| MIL-D-8684 Revision B:1959 | Data and Tests, Engineering, Contact Requirements for Air Launched Guided Missile Systems (No S/S Document) |
| SAE AS8860 | Landing Gear Structural Requirements as Listed in the MIL-886X Series of Specifications |
| MIL-HDBK-244 Revision A:1990 | Guide to Aircraft/Stores Compatibility |
| MIL-A-8865 Revision B:1987 | Airplane Strength and Rigidity Miscellaneous Loads |
| MIL STD 1763 : A | AIRCRAFT STORES CERTIFICATION PROCEDURES |
| MIL-A-8591 Revision H:1990 | Airborne Stores, Suspension Equipment and Aircraft-Store Interface (Carriage Phase); General Design Criteria for (S/S by MIL-STD-8591) |
| MIL-D-8685 Revision B:1967 | Data and Tests, Engineering, Contract Requirements for Guided Missile Target Systems (No S/S Document) |
| 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-T-81259 Revision B:1991 | Tie-downs, Airframe Design, Requirements for (S/S by MIL-STD-81259) |
| MIL-HDBK-1763 Base Document:1998 | Aircraft/Stores Compatibility: Systems Engineering Data Requirements and Test Procedures |
| MIL A 008870 : A | AIRPLANE STRENGTH AND RIGIDITY FLUTTER, DIVERGENCE AND OTHER AEROELASTIC INSTABILITIES |
| MIL A 008862 : A | AIRPLANE STRENGTH AND RIGIDITY, LANDING AND GROUND HANDLING LOADS |
| 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 A 8892 : 0 | AIRPLANE STRENGTH AND RIGIDITY, VIBRATION |
| MIL-A-8871 Revision A:1971 | Airplane Strength and Rigidity Flight and Ground Operations Tests (for Future Procure. (see MIL-A-87221) |
| MIL-D-8708 Revision C:1991 | Demonstration: Aircraft Weapon Systems, General Specification for |
| MIL-W-5013 Revision L:1991 | Wheel and Brake Assemblies, Aircraft General Specification For |
| MIL HDBK 5 : G_VOL2 | METALLIC MATERIALS AND ELEMENTS FOR AEROSPACE VEHICLE STRUCTURES |
| MIL-STD-1530 Revision D:2016 | Aircraft Structural Integrity Program (ASIP) |
| MIL-A-8870 Revision C:1993 | Airplane Strength and Rigidity Vibration, Flutter, and Divergence |
| MIL-M-81260 Revision A:1971 | Manual, Technical, Aircraft/System/Equipment Maintenance |
| MIL-L-8552 Revision C:1965 | Landing Gear, Aircraft Shock Absorber (Air-Oil Type) |
| MIL-A-8871 Revision A:1971 | Airplane Strength and Rigidity Flight and Ground Operations Tests (for Future Procure. (see MIL-A-87221) |
| MIL-A-8867 Revision C:1987 | Airplane Strength and Rigidity Ground Tests |
| DOD-D-1000 Revision B:1977 | Drawings, Engineering and Associated Lists (S/S by MIL-DTL-31000) |
| MIL-A-8866 Revision C:1987 | Airplane Strength and Rigidity Reliability Requirements, Repeated Loads, Fatigue and Damage Tolerance |
| 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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