|
MIL A 8893 : 0
|
AIRPLANE STRENGTH AND RIGIDITY, SONIC FATIGUE |
|
SAE AIR 5451 : 2017
|
A GUIDE TO LANDING GEAR SYSTEM INTEGRATION |
|
MIL A 8862 : 0
|
AIRPLANE STRENGTH AND RIGIDITY, LANDPLANE, LANDING AND GROUND HANDLING LOADS |
|
MIL-STD-8591 Base Document:2005
|
AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE) |
|
MIL-A-8866 Revision C:1987
|
AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE |
|
MIL-A-23121 Revision C:1970
|
AIRCREW ENVIRONMENTAL, ESCAPE AND SURVIVAL COCKPIT CAPSULE SYSTEM, GENERAL SPECIFICATION FOR |
|
DEFSTAN 00-970(PT0)/9(2012) : 2012
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
DEFSTAN 00-970(PT0)/17(2016) : 2016
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
DEFSTAN 00-970(PT0)/7(2011) : 2011
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
DEFSTAN 00-970(PT0)/14(2014) : 2014
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
DEFSTAN 00-970(PT0)/12(2014) : 2014
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
DEFSTAN 00-970(PT0)/13(2014) : 2014
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
DEFSTAN 00-970(PT0)/11(2013) : 2013
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
DEFSTAN 00-970(PT0)/15(2015) : 2015
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
DEFSTAN 00-970(PT0)/8(2011) : 2011
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
MIL F 9490 : D
|
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
|
DEFSTAN 00-970(PT0)/10(2013) : 2013
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
DEFSTAN 00-970(PT0)/16(2015) : 2015
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
MIL-HDBK-244 Revision A:1990
|
GUIDE TO AIRCRAFT - STORES COMPATIBILITY |
|
MIL STD 1763 : A
|
AIRCRAFT STORES CERTIFICATION PROCEDURES |
|
MIL B 38608 : A
|
BOMB, FIRE, BLU-23/B |
|
MIL-A-8870 Revision C:1993
|
AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE |
|
MIL-A-8863 Revision C:1993
|
AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES |
|
MIL-A-8591 Revision H:1990
|
AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE); GENERAL DESIGN CRITERIA FOR |
|
SAE ARP 94910 : 2012
|
AEROSPACE - VEHICLE MANAGEMENT SYSTEMS - FLIGHT CONTROL DESIGN, INSTALLATION AND TEST OF, MILITARY UNMANNED AIRCRAFT, SPECIFICATION GUIDE FOR |
|
MIL-S-8812 Revision D:1975
|
STEERING SYSTEM, AIRCRAFT GENERAL REQUIREMENTS FOR |
|
MIL-A-8867 Revision C:1987
|
AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS |
|
MIL-A-8868 Revision B:1987
|
AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS |
|
MIL-T-81259 Revision B:1991
|
TIE DOWN, AIRFRAME DESIGN, REQUIREMENTS FOR |
|
MIL-D-23222 Revision A:1971
|
DEMONSTRATION REQUIREMENTS FOR HELICOPTERS |
|
MIL-HDBK-1763 Base Document:1998
|
AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES |
|
MIL-R-7705 Revision B:1975
|
RADOME, GENERAL SPECIFICATION FOR |
|
MIL A 008870 : A
|
AIRPLANE STRENGTH AND RIGIDITY FLUTTER, DIVERGENCE AND OTHER AEROELASTIC INSTABILITIES |
|
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-23622 Base Document:1963
|
ACTUATOR, AIRCRAFT, ELECTRO-MECHANICAL, LINEAR, DIRECT CURRENT |
|
MIL-A-18717 Revision C:1993
|
ARRESTING HOOK INSTALLATIONS, AIRCRAFT |
|
MIL-A-83136 Revision A:1990
|
ARRESTING HOOK INSTALLATION, RUNWAY ARRESTING SYSTEM, AIRCRAFT, EMERGENCY |
|
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 |
|
MIL-L-87139 Base Document:1979
|
LANDING GEAR SYSTEMS REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES. WRIGHT-PATTERSON AFB OH 45433-6503 |
|
MIL-A-8871 Revision A:1971
|
AIRPLANE, TESTS, STRENGTH AND RIGIDITY FLIGHT AND GROUND OPERATIONS |
|
SAE AS 94900 : 2007
|
AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL-W-81752 Revision A:1987
|
WINDSHIELDED SYSTEM, FIXED WING AIRCRAFT - GENERAL SPECIFICATION FOR |
|
SAE ARP 1311 : 2015
|
LANDING GEAR STRUCTURES AND MECHANISMS |
|
SAE ARP 1538 : 2013
|
ARRESTING HOOK INSTALLATION, LAND-BASED AIRCRAFT |
|
JSSG-2009 Revision A:2013
|
Air Vehicle Subsystems |
|
MIL-D-8708 Revision C:1991
|
DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
|
MIL B 38634 : LATEST
|
BOMB, FIRE, BLU 32A B |
|
MIL-W-5013 Revision L:1991
|
WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR |
|
SAE AS 8860 : 2012
|
LANDING GEAR STRUCTURAL REQUIREMENTS AS LISTED IN THE MIL-886X SERIES OF SPECIFICATIONS |