aircraft design
aircraft design, Total:42 items.
The international standard classification for "aircraft design" includes: Ground service and maintenance equipment .
The Chinese standard classification for "aircraft design" includes: Basic standards and general methods , Engineering fire protection , Special vehicles .
Group Standards of the People's Republic of China
- T/AOPA 0013-2019 Ultra-light Vehicle - Aircraft design
Professional Standard - Aviation
- HB 8541-2018 Design requirements of aircraft iron bird
- HB 7490-1997 Design and Installation Requirements for Aircraft Armor
General Administration of Quality Supervision, Inspection and Quarantine of the People's Republic of China
- GB 50284-2008 Code for fire protection design of aircaft hangar
- GB/T 23419-2009 Aircraft - Four - wheel - Drive tow tractors - Performance requirements factors for design
- GB 50284-1998 Code for fire protection design of aircraft hangar
Military Standard of the People's Republic of China-General Armament Department
- GJB 2691-1996 Military aircraft design final flight test outline and reporting requirements
Association of German Mechanical Engineers
- VDI 5911 Blatt 1-2022 Occupant protection for small aircraft Aircraft design
- VDI 5911 Blatt 1-2022 Occupant protection for small aircraft Aircraft design
United States Navy
- NAVY MIL-B-8584 C (1)-1985 BRAKE SYSTEMS, WHEEL, AIRCRAFT DESIGN OF
- NAVY MIL-B-8584 C-1970 BRAKE SYSTEMS, WHEEL, AIRCRAFT DESIGN OF
Society of Automotive Engineers (SAE)
- SAE AS8584-2007 Brake Systems, Wheel, Aircraft, Design of
- SAE AIR1904B-2017 Tire Spray Suppression - Airplane Design and Consideration for
- SAE AIR1904B-2022 Tire Spray Suppression - Airplane Design and Consideration for
- SAE AIR1904A-2000 TIRE SPRAY SUPPRESSION - AIRPLANE Design Consideration and Testing for
- SAE ARP5632-2021 Rotorcraft: Application of Existing Aircraft Designed Tires, Wheels and Brakes
- SAE ARP5632-2010 Rotorcraft: Application of Existing Aircraft Designed Tires, Wheels and Brakes
SAE - SAE International
- SAE AS8584-2002 Brake Systems@ Wheel@ Aircraft@ Design of
- SAE AIR1904B-2001 Tire Spray Suppression - Airplane Design and Consideration for
- SAE AIR1904A-1997 Tire Spray Suppression - Airplane Design Consideration and Testing for
- SAE AIR1904-1985 Tire Spray Suppression - Airplane Design Consideration and Testing for
American Society for Testing and Materials (ASTM)
- ASTM F2317/F2317M-05(2007) Standard Specification for Design of Weight-Shift-Control Aircraft
- ASTM F2317/F2317M-16 Standard Specification for Design of Weight-Shift-Control Aircraft
- ASTM F2317/F2317M-05 Standard Specification for Design of Weight-Shift-Control Aircraft
- ASTM F2317/F2317M-16a Standard Specification for Design of Weight-Shift-Control Aircraft
- ASTM F2245-15 Standard Specification for Design and Performance of a Light Sport Airplane
- ASTM F2245-16 Standard Specification for Design and Performance of a Light Sport Airplane
- ASTM F2245-14 Standard Specification for Design and Performance of a Light Sport Airplane
- ASTM F2352-14 Standard Specification for Design and Performance of Light Sport Gyroplane Aircraft
- ASTM F2352-14(2022) Standard Specification for Design and Performance of Light Sport Gyroplane Aircraft
- ASTM F2352-05(2008) Standard Specification for Design and Performance of Light Sport Gyroplane Aircraft
ESDU - Engineering Sciences Data Unit
- ESDU 03014-2004 Surface flow visualisation in aircraft design
Korean Agency for Technology and Standards (KATS)
- KS W 0614-2002(2012) PNEUMATIC SYSTEMS, AIRCRAFT; DESIGN, INSTALLATION, AND DATA REQUIREMENTS FOR
NATO - North Atlantic Treaty Organization
- STANAG 3441-1994 Design of Aircraft Stores (ED 6 AMD 0)
- STANAG 3441-1996 Design of Aircraft Stores (ED 7 AMD 0)
- STANAG 3441-1984 Design of Aircraft Stores (ED 4 AMD 4)
- STANAG 3441-1992 Design of Aircraft Stores (ED 5 AMD 0)
RTCA - RTCA@ Inc.
- RTCA DO-307 CHG 1-2008 Aircraft Design and Certification for Portable Electronic Device (PED) Tolerance
- RTCA DO-307A-2016 Aircraft Design and Certification for Portable Electronic Device (PED) Tolerance
US-RTCA
- RTCA DO-307-2007 Aircraft Design and Certification for Portable Electronic Device (PED) Tolerance
SCC
- MIL MIL-P-5518D-1993 PNEUMATIC SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION, GENERAL REQUIREMENTS FOR (SUPERSEDING MIL-P-5518C)
Japanese Industrial Standards Committee (JISC)
- JIS W 0701:1992 Flight control systems -- Design, installation and test of piloted aircraft, general specification for
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