Structural design of aircraft auxiliary fuel tank
Structural design of aircraft auxiliary fuel tank, Total:23 items.
The international standard classification for "Structural design of aircraft auxiliary fuel tank" includes: .
The Chinese standard classification for "Structural design of aircraft auxiliary fuel tank" includes: Fuel system and its accessories , General technical requirements .
Professional Standard - Aviation
- HB 6118-1987 Technical Specification for FYX-1400 Type Decomposable Auxiliary Oil Tank of Aircraft
- HB 7296-1996 Aircraft external fuel tank
- HB 8603-2021 Design requirements for aircraft composite aileron structures
- HB 7495-1997 General Design Requirements for Civil Aircraft Structure
- HB/Z 325-1998 Guide for Design and Installation of Aircraft Flexible Tank
- HB 8718-2023 Requirements for Structural integrity ofaircraft
- HB 7671-2000 Requirements for Anti-corrosion Design of Airplane Structure
- HB/Z 65-1981 Dry Air Sealing Technology of Aircraft Auxiliary Fuel Tank
- HB 6210-1989 Technical specification for FYX-800 type splitter aircraft auxiliary oil tank
- HB 7495-2016 General design requirements for civil aircraft airframe structures
Military Standard of the People's Republic of China-General Armament Department
- GJB 655-1989 General specification for aircraft fuel drop tanks
- GJB 4864-2003 Aircraft fuel auxiliary tank series model spectrum
- GJB 3960-2000 Inspection and Acceptance Procedures for Military Aircraft Fuel Auxiliary Tanks
- GJB 287-1987 Lifting lugs with 762mm lifting distance for aircraft auxiliary fuel tanks
- GJB 288-1987 Technical conditions for lifting lugs with 762mm lifting distance for aircraft auxiliary fuel tanks
- GJB 4863-2003 Aircraft fuel drop tank connection interface requirements
- GJB 655A-2003 General specification for aircraft fuel drop tanks
- GJB 5276-2004 General specification for aircraft auxiliary fuel tank pylons
- GJB 5556-2006 Test requirements for auxiliary external fuel tank of aircraft
U.S. Military Regulations and Norms
- ARMY ADS 29-1986 STRUCTUML DESIGN CRITERIA FOR ROTARY WING AIRCRAFT
SCC
- MIL MIL-T-18847C-1986 TANK, FUEL, AIRCRAFT, AUXILIARY EXTERNAL, DESIGN AND INSTALLATION OF
Society of Automotive Engineers (SAE)
- SAE AIR1664A-2019 Aircraft Flexible Tanks General Design and Installation Recommendations
- SAE AIR1664-1994 AIRCRAFT FLEXIBLE TANKS GENERAL DESIGN AND INSTALLATION RECOMMENDATIONS
