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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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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.

Committee
FSC 1510
DevelopmentNote
Partially Supersedes MIL A 008866 (B). C NOTICE 1 - Notice of Validation. (06/2004)
DocumentType
Standard
Pages
16
ProductNote
NEW CHILD NOT 2 2019 IS NOW ADDED
PublisherName
US Military Specs/Standards/Handbooks
Status
Current

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SAE AS 8860 : 2012 LANDING GEAR STRUCTURAL REQUIREMENTS AS LISTED IN THE MIL-886X SERIES OF SPECIFICATIONS
MIL-A-23121 Revision C:1970 AIRCREW ENVIRONMENTAL, ESCAPE AND SURVIVAL COCKPIT CAPSULE SYSTEM, GENERAL SPECIFICATION FOR
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
MIL-A-8868 Revision B:1987 AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS
MIL-DTL-9490 Revision E:2008 FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
JSSG-2006 Base Document:1998 JOINT SERVICE SPECIFICATION GUIDE - 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
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
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 REQUIREMENTS FOR AIRPLANES
MIL-A-8860 Revision B:1987 AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR

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