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
|
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
|
SAE AS 8860 : 2012
|
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
|
MIL-D-8685 Revision B:1967
|
DATA AND TESTS, ENGINEERING, CONTRACT REQUIREMENTS FOR GUIDED MISSILE TARGET SYSTEMS
|
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-T-81259 Revision B:1991
|
TIE DOWN, AIRFRAME DESIGN, REQUIREMENTS FOR
|
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, TESTS, STRENGTH AND RIGIDITY FLIGHT AND GROUND OPERATIONS
|
MIL-D-8708 Revision C:1991
|
DEMONSTRATION REQUIREMENTS FOR AIRPLANES
|
MIL-W-5013 Revision L:1991
|
WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR
|