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RU
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aircraft system
aircraft system, Total:342 items.
In the international standard classification, aircraft system involves: Transport, Aircraft and space vehicles in general, Materials for aerospace construction, On-board equipment and instruments, Quality, Company organization and management, Aerospace electric equipment and systems, Structure and structure elements, Vocabularies, Aerospace engines and propulsion systems, Cargo equipment, Agricultural machines, implements and equipment, Valves, Aerospace fluid systems and components, Passenger and cabin equipment, Electrical accessories, Road vehicle systems, Mobile services, Electromagnetic compatibility (EMC).
IX-ICAO, aircraft system
- ICAO 10019-2015 Manual on Remotely Piloted Aircraft Systems (RPAS)
- ICAO AN 10-6-2021 Annex 10 - Aeronautical Telecommunications - Volume VI: Communication Systems and Procedures Relating to Remotely Piloted Aircraft Systems C2 Link
Military Standard of the People's Republic of China-General Armament Department, aircraft system
- GJB 5561-2006 Requirement for preparation of aircraft system diagram manual
- GJB 1397-1992 Aircraft electrical system flight test requirements
- GJB 7261-2011 Aircraft flight parameter system parameter names, symbols and mnemonic definitions
- GJB 5282-2004 General specifications for electric servos for military aircraft flight control systems
- GJB 1003A-2006 General specification for aircraft fuel system
- GJB 2187-1994 General specifications for aircraft propulsion systems
- GJB 1003-1990 General specification for aircraft fuel systems
- GJB 1194-1991 General specifications for aircraft aerodynamic systems
- GJB 2187A-2015 General specifications for aircraft propulsion systems
- GJB 3368-1998 General specification for aircraft oxygen systems
- GJB 1476-1992 General requirements for aircraft flight test system modification
- GJB 2191-1994 General specification for manned aircraft flight control systems
- GJB 1907-1994 General specification for aircraft fuel system accessories
- GJB 1482-1992 General specification for accessories for aircraft hydraulic systems
- GJB 1481-1992 General specification for accessories for aircraft pneumatic systems
- GJB 2022A-2012 Requirements for aircraft fuel system installation and test
- GJB 3275-1998 Aircraft fire-extinguishing system installation and testing requirements
- GJB 2022-1994 Aircraft fuel system installation and testing requirements
- GJB 2537-1995 General specification for windshield systems for fixed-wing aircraft
Aeronautical Radio Inc., aircraft system
Professional Standard - Aviation, aircraft system
- HB 5940-1986 Electromagnetic Compatibility Requirements for Aircraft Systems
- HB 7083-1994 Aircraft System Equipment Definition Chart Requirements
- HB/Z 211-1992 Military Aircraft Systems Work Breakdown Structure
- HB 7758-2004 Work breakdown structures and codes for aircraft systems
- HB 8412-2014 Electrical bonding requirement for civil aircraft systems
- HB 6204-1989 Aircraft Electrical System Flight Test Requirements
- HB 7170-1995 Aircraft fuel system flight test requirements
- HB 7745-2004 Characteristics of aircraft electrical systems
- HB 8418-2014 Requirements for flight test of civil aircraft oxygen system
- HB 8452-2014 Requirements for flight test of civil aircraft fuel system
- HB 8468-2014 Requirements for flight test of civil aircraft electric system
- HB 6486-2008 Terms and definitions of aireraft flight control system
- HB 6486-1991 aircraft flight control system terminology
- HB 7080-1994 General requirements for aircraft bleed air system
- HB 6754-1993 General specification for aircraft hydraulic systems
- HB 8434-2014 General specification of flight management system for civil aircraft
- HB 8437-2014 General requirements for flight control system of civil aircraft
- HB 8471-2014 Requirements for flight test of civil aircraft flight control system
- HB 8435-2014 General specification for flight control computer system of civil aircraft
- HB 8470-2014 Ground test requirements for flight control system of civil aircraft
- HB 8505-2014 Design requirements for commercial aircraft fuel system
- HB 8506-2014 Test requirements for commercial aircraft hydraulic systems
- HB 7117-2014 General requirements for civil aircraft hydraulic systems
- HB 8403-2014 General requirements for civil aircraft fuel system
- HB 8441-2014 General requirements for civil aircraft electric power system
- HB 8442-2014 General requirements for oxygen supply system of civil aircraft
- HB 8445-2014 General requirements of the freight systems for the civil airplane
- HB 8450-2014 General requirements for pneumatic systems of civil aircraft
- HB 8488-2014 General requirements of civil aircraft water system
- HB 8484-2014 Design requirements for oxygen system of civil aircraft
- HB 6483-1990 Aircraft Fuel System Piping Installation Requirements
- HB 6081-1986 Aircraft aerodynamic system design and installation requirements
- HB 6505-1991 General requirements for aircraft power supply system design
- HB/Z 336-1999 Load Analysis Method of Aircraft Bleed Air System
- HB 7391-1996 Design requirements for oxygen supply system of passenger aircraft
- HB/Z 302-1997 Design guide for civil aircraft power supply system
- HB 7685-2001 Aircraft fuel system pollution control requirements
- HB/Z 146-1989 General design specification for aircraft fuel system
- HB 6507-1991 General specification for aircraft fuel system accessories
- HB 7117-1994 General specification for civil aircraft hydraulic system
- HB 8436-2014 Design and installation requirements for flight control system of civil aircraft
- HB 7708-2002 Requirements for oil systems aircarft installattion and test
- HB 8451-2014 Requirements for electrical bonding of civil aircraft fuel system
- HB 6484-1990 Schematic Recommended Symbols for Aircraft Fuel System
- HB 6514-1991 General specification for windshield system of fixed-wing aircraft
American Society for Testing and Materials (ASTM), aircraft system
- ASTM F3061/F3061M-22b Standard Specification for Systems and Equipment in Aircraft
- ASTM F3061/F3061M-23 Standard Specification for Systems and Equipment in Aircraft
- ASTM F3061/F3061M-16a Standard Specification for Systems and Equipment in Small Aircraft
- ASTM F3061/F3061M-23a Standard Specification for Systems and Equipment in Aircraft
- ASTM F3061/F3061M-22a Standard Specification for Systems and Equipment in Aircraft
- ASTM F3061/F3061M-22 Standard Specification for Systems and Equipment in Aircraft
- ASTM F3061/F3061M-16b Standard Specification for Systems and Equipment in Small Aircraft
- ASTM F3061/F3061M-19a Standard Specification for Systems and Equipment in Small Aircraft
- ASTM F3061/F3061M-19 Standard Specification for Systems and Equipment in Small Aircraft
- ASTM F3061/F3061M-17 Standard Specification for Systems and Equipment in Small Aircraft
- ASTM F3061/F3061M-15 Standard Specification for Systems and Equipment in Small Aircraft
- ASTM F3153-22 Standard Specification for Verification of Aircraft Systems and Equipment
- ASTM F3061/F3061M-20 Standard Specification for Systems and Equipment in Small Aircraft
- ASTM F2849-10 Standard Practice for Handling of Unmanned Aircraft Systems at Divert Airfields
- ASTM F3246-18 Standard Specification for Quality Assurance for Manufacturers of Aircraft Systems
- ASTM F3230-20 Standard Practice for Safety Assessment of Systems and Equipment in Small Aircraft
- ASTM F3230-20a Standard Practice for Safety Assessment of Systems and Equipment in Small Aircraft
- ASTM F3322-18 Standard Specification for Small Unmanned Aircraft System (sUAS) Parachutes
- ASTM F3230-17 Standard Practice for Safety Assessment of Systems and Equipment in Small Aircraft
- ASTM F2849-10(2019) Standard Practice for Handling of Unmanned Aircraft Systems at Divert Airfields
- ASTM F3230-21 Standard Practice for Safety Assessment of Systems and Equipment in Small Aircraft
- ASTM F3230-21a Standard Practice for Safety Assessment of Systems and Equipment in Small Aircraft
- ASTM F3366-19 Standard Specification for General Maintenance Manual (GMM) for a small Unmanned Aircraft System (sUAS)
- ASTM F330-89(1999) Standard Test Method for Bird Impact Testing of Aerospace Transparent Enclosures
- ASTM F3309/F3309M-20 Standard Practice for Simplified Safety Assessment of Systems and Equipment in Small Aircraft
- ASTM F3309/F3309M-18 Standard Practice for Simplified Safety Assessment of Systems and Equipment in Small Aircraft
- ASTM F3309/F3309M-21 Standard Practice for Simplified Safety Assessment of Systems and Equipment in Small Aircraft
- ASTM F3266-18 Standard Guide for Training for Remote Pilot in Command of Unmanned Aircraft Systems (UAS) Endorsement
- ASTM F3365-23 Standard Practice for Compliance Audits to ASTM Standards on Unmanned Aircraft Systems
- ASTM F2512-07 Standard Practice for Quality Assurance in the Manufacture of Light Unmanned Aircraft System
- ASTM F2612-07 Standard Practice for Design and Manufacture of Turbine Engines for Unmanned Aircraft System
- ASTM F3532-22 Standard Practice for Protection of Aircraft Systems from Intentional Unauthorized Electronic Interactions
- ASTM F3196-18 Standard Practice for Seeking Approval for Beyond Visual Line of Sight (BVLOS) Small Unmanned Aircraft System (sUAS) Operations
- ASTM F2584-06 Standard Practice for Maintenance and Development of Maintenance Manuals for Light Unmanned Aircraft System (UAS)
- ASTM F2689-08 Standard Practice for Design and Manufacture of Reciprocating Spark Ignition Engines for Unmanned Aircraft Systems
- ASTM F3227/F3227M-21a Standard Specification for Environmental Systems in Aircraft
- ASTM F3227/F3227M-21 Standard Specification for Environmental Systems in Aircraft
- ASTM F3227/F3227M-22 Standard Specification for Environmental Systems in Aircraft
- ASTM F3227/F3227M-20 Standard Specification for Aircraft Environmental Systems
- ASTM F3231/F3231M-17 Standard Specification for Electrical Systems in Small Aircraft
- ASTM F3227/F3227M-17 Standard Specification for Environmental Systems in Small Aircraft
- ASTM F3269-21 Standard Practice for Methods to Safely Bound Behavior of Aircraft Systems Containing Complex Functions Using Run-Time Assurance
未注明发布机构, aircraft system
- GJB 4855-2003 Classification and coding of military aircraft systems
- BS G 133:1951(2009) Specification for Electro - magnetic indicators for extra low voltage aircraft systems
- SAE AIR4253B-2018 Description of Actuation Systems for Aircraft with Fly-By-Wire Flight Control Systems
- GJB 3212-1998 Aircraft fuel system flight test requirements
- SAE AS8043-1986 Restraint Systems for Civil Aircraft
United States Navy, aircraft system
- NAVY MIL-M-81260 A NOTICE 1-1997 MANUALS, TECHNICAL, AIRCRAFT/SYSTEM/EQUIPMENT MAINTENANCE
- NAVY MIL-M-81260 A (1)-1971 MANUALS, TECHNICAL, AIRCRAFT/SYSTEM/EQUIPMENT MAINTENANCE
- NAVY MIL-M-81260 A-1971 MANUALS, TECHNICAL, AIRCRAFT/SYSTEM/EQUIPMENT MAINTENANCE
- NAVY MIL-M-8609 B NOTICE 2-1996 MOTORS, DIRECT-CURRENT, 28-VOLT SYSTEM, AIRCRAFT, GENERAL SPECIFICATION FOR
- NAVY MIL-M-8609 B VALID NOTICE 1-1987 MOTORS, DIRECT-CURRENT, 28-VOLT SYSTEM, AIRCRAFT, GENERAL SPECIFICATION FOR
- NAVY MIL-M-8609 B-1965 MOTORS, DIRECT-CURRENT, 28-VOLT SYSTEM, AIRCRAFT, GENERAL SPECIFICATION FOR
- NAVY MIL-M-7969 C NOTICE 1-1996 MOTORS, ALTERNATING CURRENT, 400-CYCLE, 115/200-VOLT SYSTEM, AIRCRAFT, GENERAL SPECIFICATION FOR
- NAVY MIL-M-7969 C-1965 MOTORS, ALTERNATING CURRENT, 400-CYCLE, 115/200-VOLT SYSTEM, AIRCRAFT, GENERAL SPECIFICATION FOR
- NAVY MIL-T-18606 (1)-1969 TEST PROCEDURES FOR AIRCRAFT ENVIRONMENTAL SYSTEMS
- NAVY MIL-T-18606-1955 TEST PROCEDURES FOR AIRCRAFT ENVIRONMENTAL SYSTEMS
- NAVY MIL-G-85536 VALID NOTICE 1-1991 GUN SYSTEM, 25-MM, AIRCRAFT A/A49E-10
- NAVY MIL-G-85536 (1)-1987 GUN SYSTEM, 25-MM, AIRCRAFT A/A49E-10
- NAVY MIL-G-85536-1984 GUN SYSTEM, 25-MM, AIRCRAFT A/A49E-10
- NAVY MIL-S-8812 D (1)-1977 STEERING SYSTEM: AIRCRAFT, GENERAL REQUIREMENTS FOR
- NAVY MIL-S-8812 D-1975 STEERING SYSTEM: AIRCRAFT, GENERAL REQUIREMENTS FOR
- NAVY MIL-C-22284 A NOTICE 1-1996 CONTAINER, AIRCRAFT FIRE EXTINGUISHING SYSTEM, BROMOTRIFLUOROMETHANE, CF3BR
- NAVY MIL-C-22284 A (1)-1995 CONTAINER, AIRCRAFT FIRE EXTINGUISHING SYSTEM, BROMOTRIFLUOROMETHANE, CF3BR
- NAVY MIL-C-22284 A-1965 CONTAINER, AIRCRAFT FIRE EXTINGUISHING SYSTEM, BROMOTRIFLUOROMETHANE, CF3BR
- NAVY MIL-F-17874 B (1)-1985 FUEL SYSTEMS: AIRCRAFT, INSTALLATION AND TEST OF
- NAVY MIL-F-17874 B-1965 FUEL SYSTEMS: AIRCRAFT, INSTALLATION AND TEST OF
- NAVY MIL-O-19838 NOTICE 2-1996 OIL SYSTEMS, AIRCRAFT, INSTALLATION AND TEST OF
- NAVY MIL-O-19838 VALID NOTICE 1-1991 OIL SYSTEMS, AIRCRAFT, INSTALLATION AND TEST OF
- NAVY MIL-O-19838 (1)-1957 OIL SYSTEMS, AIRCRAFT, INSTALLATION AND TEST OF
- NAVY MIL-O-19838-1956 OIL SYSTEMS, AIRCRAFT, INSTALLATION AND TEST OF
- NAVY QPL-19069-2013 Valve, Check, Hydraulic, Aircraft, Type II Systems
- NAVY MIL-L-22589 D-1991 LAUNCHING SYSTEM, NOSE GEAR TYPE, AIRCRAFT
Society of Automotive Engineers (SAE), aircraft system
- SAE AIR6110-2011 Contiguous Aircraft/System Development Process Example
- SAE AIR6110-2020 Contiguous Aircraft/System Development Process Example
- SAE AIR1196-1992 1992 Bibliography on Fuel Handling and Contamination in Aircraft Systems
- SAE AIR4061A-1999 Guidelines for Integration of Engine Monitoring Functions With On-Board Aircraft Systems
- SAE AIR4061A-1996 Guidelines for Integration of Engine Monitoring Functions with On-Board Aircraft Systems
- SAE ARP4754-1996 Certification Considerations for Highly-Integrated or Complex Aircraft Systems
- SAE AIR5924-2004 Guidelines for the Integration of Electronic Engine Control Systems with Transport Category Aircraft Systems
- SAE AIR4094-1990 Aircraft Flight Control Systems Descriptions
- SAE ARP5707-2010 Pilot Training Recommendations for Unmanned Aircraft Systems (UAS) Civil Operations
- SAE AIR4061B-2012 Guidelines for Integrating Typical Engine Health Management Functions Within Aircraft Systems
- SAE ARP7042-2022 Recommended Practice: Development Planning for Design of Additive Manufactured Components in an Aircraft System
- SAE ARD50055-1998 Aircraft Electrical Systems
- SAE ARP1088A-2004 Aircraft Indicating Systems
- SAE ARP1088-1991 AIRCRAFT INDICATING SYSTEMS
- SAE ARP1088B-2015 Aircraft Indicating Systems
- SAE AIR4253B-2012 Description of Actuation Systems for Aircraft with Fly-By-Wire Flight Control Systems
- SAE AIR4094-1994 AIRCRAFT FLIGHT CONTROL SYSTEMS DESCRIPTIONS
- SAE AIR4253-1999 DESCRIPTION OF ACTUATION SYSTEMS FOR AIRCRAFT WITH FLY-BY-WIRE FLIGHT CONTROL SYSTEMS
- SAE AS8043A-2000 Restraint Systems for Civil Aircraft
- SAE AS8043B-2014 Restraint Systems for Civil Aircraft
- SAE AS8043C-2023 Restraint Systems for Civil Aircraft
- SAE AS1975A-1992 HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE, ARAMID REINFORCED, 275 °F, STANDARD DUTY, 4000/3000 lbf/in2, HYDRAULIC, AIRCRAFT SYSTEMS
- SAE AS1975C-2007 Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000/4000 psi, 275 °F, Standard Duty, Hydraulic, Aircraft Systems
- SAE MA1975-2015 Hose Assemblies, Polytetrafluoroethylene, Aramid Reinforced, 135 °C, Standard Duty, 28 000/21 000 kPa, Hydraulic, Aircraft Systems
- SAE AIR1223-1993 INSTALLATION OF LIQUID OXYGEN SYSTEMS IN CIVIL AIRCRAFT
- SAE AIR1223A-2012 Installation of Liquid Oxygen Systems in Civil Aircraft
- SAE AIR1223A-1971 Installation of Liquid Oxygen Systems in Civil Aircraft
- SAE ARINC609-1987 DESIGN GUIDANCE FOR AIRCRAFT ELECTRICAL POWER SYSTEMS
- SAE AIR7975-2019 Aircraft Fuel System Design Guidelines
- SAE AIR825/14-2021 Basic Aircraft Oxygen Systems Design
- SAE ARP6277-2021 Commercial Aircraft Hydraulic System Sizing
- SAE ARP1088C-2021 Aircraft Indicating Systems Optical Performance
- SAE AIR5829-2018 Air in Aircraft Hydraulic Systems
- SAE AIR1749A-2020 Aircraft Fuel System Pressure Definitions
- SAE ARP6205-2023 Transport Airplane Fuel System Lightning Protection
- SAE AIR860-1992 AIRCRAFT ELECTRICAL HEATING SYSTEMS
- SAE AIR860A-2006 Aircraft Electrical Heating Systems
- SAE AIR4253A-2001 Description of Actuation Systems for Aircraft with Fly-By-Wire Flight Control Systems
- SAE AS1975SUP1-2013 Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000/4000 psi, 275 °F, Standard Duty, Hydraulic, Aircraft Systems (Supplement 1)
- SAE AIR5128A-2012 Electrical Bonding of Aircraft Fuel Systems
- SAE AIR1326A-1997 Aircraft Fuel System Vapor-Liquid Ratio Parameter
- SAE ARP217-1951 TESTING OF PROTOTYPE AIRPLANE AIR CONDITIONING SYSTEMS
- SAE AIR5128A-2022 Electrical Bonding of Aircraft Fuel Systems
- SAE AIR1326A-2020 Aircraft Fuel System Vapor-Liquid Ratio Parameter
- SAE AS6502-2022 Aircraft Propulsion System Performance Nomenclature
- SAE AIR1083A-1991 HYDRAULIC SYSTEM SURVIVABILITY FOR MILITARY AIRCRAFT
- SAE AIR5005-2000 Aerospace - Commercial Aircraft Hydraulic Systems
- SAE AIR5005A-2015 Aerospace - Commercial Aircraft Hydraulic Systems
- SAE AIR1903A-2021 Overview and History of Aircraft Inerting Systems
- SAE AS8584B-2013 Brake Systems, Wheel, Military Aircraft
- SAE AIR5744-2020 Aircraft Thermal Management System Engineering
- SAE AIR5128-1997 ELECTRICAL BONDING OF AIRCRAFT FUEL SYSTEM PLUMBING SYSTEMS
- SAE AIR790B-1999 Considerations on Ice Formation in Aircraft Fuel Systems
- SAE AIR6326-2023 Aircraft Electrical Power Systems Modeling and Simulation Definitions
- SAE ARP1401A-2007 Aircraft Fuel System and Component Icing Test
- SAE ARP1401B-2012 Aircraft Fuel System and Component Icing Test
- SAE AIR5128-2007 ELECTRICAL BONDING OF AIRCRAFT FUEL SYSTEM PLUMBING SYSTEMS
- SAE ARP85E-1991 Air Conditioning Systems For Subsonic Airplanes
- SAE ARP85E-2007 Air Conditioning Systems For Subsonic Airplanes
- SAE ARP85F-2018 Air Conditioning Systems for Subsonic Airplanes
- SAE ARP85G-2019 Air Conditioning Systems for Subsonic Airplanes
International Organization for Standardization (ISO), aircraft system
- ISO 24356:2022 General requirements for tethered unmanned aircraft systems
- ISO/DIS 23665 Unmanned aircraft systems — Training for personnel involved in UAS operations
- ISO 5110:2023 Test method for flight stability of a multi-copter unmanned aircraft system (UAS) under wind and rain conditions
- ISO 5015-2:2022 Unmanned aircraft systems — Part 2: Operation of vertiports for vertical take-off and landing (VTOL) unmanned aircraft (UA)
- ISO 1540:1977 Aerospace — Characteristics of aircraft electrical systems
- ISO/CD 1540 Aerospace — Characteristics of aircraft electrical systems
North Atlantic Treaty Organization Standards Agency, aircraft system
NATO - North Atlantic Treaty Organization, aircraft system
- STANAG 3614-1983 Electromagnetic Compatibility (EMC) of Aircraft Systems (ED 2 AMD 0; To obtain please contact your national Defense Standardization Office or the NATO Standardization Office website: http:/ so.nato.int so@ Phone: +32 (0)2 – 707 5556@ email: nso@nso.nato.i
- STANAG 3614-1989 Electromagnetic Compatibility (EMC) of Aircraft Systems (ED 3 AMD 0; To obtain please contact your national Defense Standardization Office or the NATO Standardization Office website: http:/ so.nato.int so@ Phone: +32 (0)2 – 707 5556@ email: nso@nso.nato.i
- STANAG 3614-2000 Electromagnetic Compatibility (EMC) of Aircraft Systems and Equipment (ED 4; To obtain please contact your national Defense Standardization Office or the NATO Standardization Office website: http:/ so.nato.int so@ Phone: +32 (0)2 – 707 5556@ email: nso@ns
- AAVSP-05-2018 ANALOGUE VIDEO STANDARD FOR AIRCRAFT SYSTEM APPLICATIONS (ED A@ Ver. 1)
- STANAG 3350-1989 Analogue Video Standard for Aircraft System Applications (ED 3 AMD 1; To obtain please contact your national Defense Standardization Office or the NATO Standardization Office website: http:/ so.nato.int so@ Phone: +32 (0)2 – 707 5556@ email: nso@nso.nato.
- ATP-3.3.7-2013 GUIDANCE FOR THE TRAINING OF UNMANNED AIRCRAFT SYSTEMS (UAS) OPERATORS (ED A@ Ver 1; To obtain please contact your national Defense Standardization Office or the NATO Standardization Office website: http:/ so.nato.int so@ Phone: +32 (0)2 – 707 5556@ email
- ATP-3.3.7-2014 GUIDANCE FOR THE TRAINING OF UNMANNED AIRCRAFT SYSTEMS (UAS) OPERATORS (ED B@ Ver 1; To obtain please contact your national Defense Standardization Office or the NATO Standardization Office website: http:/ so.nato.int so@ Phone: +32 (0)2 – 707 5556@ email
- STANAG 3659-1998 Electrical Bonding Requirements for Metallic Aircraft Systems (ED 3 AMD 1 Amendment 1 09/28/2000; To obtain please contact your national Defense Standardization Office or the NATO Standardization Office website: http:/ so.nato.int so@ Phone: +32 (0)2 – 70
- STANAG 3236-2000 Designation System for Aircraft and Designation of Role Codes of Aircraft (ED 9; To obtain please contact your national Defense Standardization Office or the NATO Standardization Office website: http:/ so.nato.int so@ Phone: +32 (0)2 – 707 5556@ email: ns
- STANAG 3659-1995 Electrical Bonding Requirements for Metallic Aircraft Systems (ED 2 AMD 1 Amendment 1@ 9/12/97; To obtain please contact your national Defense Standardization Office or the NATO Standardization Office website: http:/ so.nato.int so@ Phone: +32 (0)2 – 707
- AEP-101-2017 GUIDANCE ON SENSE AND AVOID FOR UNMANNED AIRCRAFT SYSTEMS (ED A@ Ver. 1; Agreement for NATO STANREC 4811)
- STANAG 3236-1991 Designation System for Aircraft and Designation of Role Codes of Aircraft (ED 8 AMD 0; To obtain please contact your national Defense Standardization Office or the NATO Standardization Office website: http:/ so.nato.int so@ Phone: +32 (0)2 – 707 5556@ ema
- STANAG 3697-1995 Airfield Aircraft Arresting Systems (ED 4 AMD 0; To obtain please contact your national Defense Standardization Office or the NATO Standardization Office website: http:/ so.nato.int so@ Phone: +32 (0)2 – 707 5556@ email: nso@nso.nato.int. For additional i
- STANAG 3456-1976 Aircraft Electrical System Characteristics (ED 4 AMD 4; To obtain please contact your national Defense Standardization Office or the NATO Standardization Office website: http:/ so.nato.int so@ Phone: +32 (0)2 – 707 5556@ email: nso@nso.nato.int. For addit
- STANAG 3456-1994 Aircraft Electrical Power System Characteristics (ED 5 AMD 0; To obtain please contact your national Defense Standardization Office or the NATO Standardization Office website: http:/ so.nato.int so@ Phone: +32 (0)2 – 707 5556@ email: nso@nso.nato.int. For
Institute of Electrical and Electronics Engineers (IEEE), aircraft system
Korean Agency for Technology and Standards (KATS), aircraft system
- KS W 0711-1997(2012) FLIGHT CONTROL SYSTEMS-DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
- KS W 0711-1979 FLIGHT CONTROL SYSTEMS-DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
- KS W 9001-2018 Unmanned aircraft systems — Part 1:Design and Testing for UAV
- KS W 9132-2018 Unmanned aircraft system components — Part 1: Design and Maintenance for Batteries
- KS W 9131-2018 Unmanned aircraft system compoments — Part 2: Design and Testing for Propeller
- KS W 2022-1977(2010) Aircraft flight inspection (Electric system)
- KS W 7213-1987(2012) Flight testing of electric systems in aircraft,general requirements for
- KS W 4020-2007(2012) Installation of aircraft propulsion system, general specification for
- KS W 4020-1987 Installation of aircraft propulsion system, general specification for
- KS W 7213-2014 Flight testing of electric systems in aircraft,general requirements for
- KS W 2023-2014 General of aircraft electric system inspection
- KS W 2023-1979(2012) General of aircraft electric system inspection
- KS W 2022-2014 Aircraft flight inspection (Electric system)
- KS W 7011-1993(2008) AEROSPACE-CHARACTERISTICS OF AIRCRAFT ELECTRICAL SYSTEMS
- KS W 7011-1983 AEROSPACE-CHARACTERISTICS OF AIRCRAFT ELECTRICAL SYSTEMS
- KS W 3211-2013 Aircraft Fuel System Components,General Specification for
- KS W 4020-2013 Installation of aircraft propulsion system, general specification for
- KS W 2923-2003(2008) HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT, GENERAL SPECIFICATIONS FOR
- KS W 3211-1984(2009) Aircraft Fuel System Components,General Specification for
British Standards Institution (BSI), aircraft system
- BS ISO 23665:2021 Unmanned aircraft systems. Training for personnel involved in UAS operations
- BS ISO 5015-2:2022 Unmanned aircraft systems - Operation of vertiports for vertical take-off and landing (VTOL) unmanned aircraft (UA)
- BS ISO 1540:2006 Aerospace - Characteristics of aircraft electrical systems
Standard Association of Australia (SAA), aircraft system
- AS 7460:2021 Railway networks – Remotely piloted aircraft systems (Drones) – Operational requirements
US-Unspecified Preparing Activity, aircraft system
US-RTCA, aircraft system
- RTCA DO-304-2007 Guidance Material and Considerations for Unmanned Aircraft Systems
GB-REG, aircraft system
- REG CAP 722-2010 Unmanned Aircraft System Operations in UK Airspace ?Guidance Fourth Edition
- REG NASA-LLIS-1239-2002 Lessons Learned - Space Shuttle Program/Shuttle System Upgrades/Cockpit Avionics Upgrade
Danish Standards Foundation, aircraft system
- DS/ISO 23665:2021 Unmanned aircraft systems – Training for personnel involved in UAS operations
- DS/EN 302480 V1.1.2:2008 Electromagnetic compatibility and Radio spectrum Matters (ERM); Harmonized EN for the GSM onboard aircraft system covering the essential requirementsof Article 3.2 of the R&TTE Directive
RO-ASRO, aircraft system
- STAS 9688-1986 AERGRAFTS Caracteristics of aircraft electrical , systems
SAE - SAE International, aircraft system
- SAE AIR4094A-2016 Aircraft Flight Control Systems Descriptions
- SAE AIR4061C-2016 Guidelines for Integrating Typical Engine Health Management Functions Within Aircraft Systems
- SAE ARP1088B-2010 Aircraft Indicating Systems
- SAE ARP1088-1970 Aircraft Indicating Systems
- SAE AIR4253-1989 Description of Actuation Systems for Aircraft with Fly-By-Wire Flight Control Systems
- SAE AIR1899-1985 Aircraft Hydraulic System Characteristics
- SAE AS1975E-2013 Hose Assembly@ Polytetrafluoroethylene@ Para-Aramid Reinforced@ 3000/4000 psi@ 275 °F@ Standard Duty@ Hydraulic@ Aircraft Systems
- SAE AS1975F-2015 Hose Assembly@ Polytetrafluoroethylene@ Para-Aramid Reinforced@ 3000/4000 psi@ 275 °F@ Standard Duty@ Hydraulic@ Aircraft Systems
- SAE AS1975B-1994 Hose Assemblies@ Polytetrafluoroethylene@ Aramid Reinforced@ 275 Degrees F@ Standard Duty@ 4000/3000 psi@ Hydraulic@ Aircraft Systems
- SAE AS1975D-2008 Hose Assembly@ Polytetrafluoroethylene@ Para-Aramid Reinforced@ 3000/4000 psi@ 275 °F@ Standard Duty@ Hydraulic@ Aircraft Systems
- SAE AS1975G-2016 Hose Assembly@ Polytetrafluoroethylene@ Para-Aramid Reinforced@ 3000/4000 psi@ 275 °F@ Standard Duty@ Hydraulic@ Aircraft Systems
- SAE AIR1223-1971 Installation of Liquid Oxygen Systems in Civil Aircraft
- SAE AIR1223A-1999 Installation of Liquid Oxygen Systems in Civil Aircraft
- SAE AIR860-1965 Aircraft Electrical Heating Systems
- SAE AS1975 SUP 1-2001 Hose Assembly@ Polytetrafluoroethylene@ Para-Aramid Reinforced@ 3000/4000 psi@ 275 °F@ Standard Duty@ Hydraulic@ Aircraft Systems (Supplement 1)
- SAE ARP217A-1960 TESTING OF PROTOTYPE AIRPLANE AIR CONDITIONING SYSTEMS
- SAE AS23A-2004 TESTS@ AIRCRAFT HYDRAULIC SYSTEMS & COMPONENTS
- SAE ARP945-1968 MINIMUM REQUIREMENTS FOR AIRPLANE CARGO SYSTEMS
- SAE AS6502-2015 Aircraft Propulsion System Performance Nomenclature
- SAE AIR1326-1974 Aircraft Fuel System Vapor-Liquid Ratio Parameter
- SAE AIR790A-1976 Considerations of Ice Formation in Aircraft Fuel Systems
- SAE PT-177-2014 Aircraft Thermal Management: Systems Architectures
- SAE ARP1401-1979 Aircraft Fuel System and Component Icing Test
- SAE AIR6326-2015 Aircraft Electrical Power Systems Modeling and Simulation Definitions
AT-ON, aircraft system
European Committee for Standardization (CEN), aircraft system
- prEN 4709-004-2020 Aerospace series - Unmanned Aircraft Systems - Part 004: Lighting requirements
- prEN 4709-002-2020 Aerospace series - Unmanned Aircraft Systems - Part 002: Direct Remote identification
- prEN 4709-003-2020 Aerospace series - Unmanned Aircraft Systems - Part 003: Geo-awareness requirements
- prEN 4709-001-2021 Aerospace series - Unmanned Aircraft Systems - Part 001: Product requirements and verification
- prEN 4709-001 Aerospace series - Unmanned Aircraft Systems - Part 001: Product requirements and verification
German Institute for Standardization, aircraft system
- DIN 5452-1:2018 Aerospace series - Unmanned aircraft systems (UAS) - Part 1: Terms and definitions; Text in German and English
- DIN EN 4709-004:2021 Aerospace series - Unmanned Aircraft Systems - Part 004: Lighting requirements; English version prEN 4709-004:2020
- DIN EN 4709-003:2021 Aerospace series - Unmanned Aircraft Systems - Part 003: Geo-awareness requirements; English version prEN 4709-003:2020
- DIN EN 4709-002:2021 Aerospace series - Unmanned Aircraft Systems - Part 002: Direct Remote Identification; English version prEN 4709-002:2020
- DIN 29576-2:1987 Aerospace; aircraft electrical systems; testing of electrical cables installed in aircraft
- DIN 29576-3:1991-11 Aerospace, aircaft electrical systems; bonding
- DIN 29576-3:1991 Aerospace, aircaft electrical systems; bonding
U.S. Military Regulations and Norms, aircraft system
ITU-R - International Telecommunication Union/ITU Radiocommunication Sector, aircraft system
- REPORT M.2204-2010 Characteristics and spectrum considerations for sense and avoid systems use on unmanned aircraft systems
- REPORT M.2171-2009 Characteristics of unmanned aircraft systems and spectrum requirements to support their safe operation in non-segregated airspace
CEN - European Committee for Standardization, aircraft system
- PREN 4709-001-2019 Aerospace series - Unmanned Aircraft Systems - Product requirements and verification for the Open category
General Administration of Quality Supervision, Inspection and Quarantine of the People‘s Republic of China, aircraft system
IEEE - The Institute of Electrical and Electronics Engineers@ Inc., aircraft system
Group Standards of the People's Republic of China, aircraft system
U.S. Air Force, aircraft system
- AIR FORCE QPL-7899-QPD-2012 Valve, Check, Aircraft Fuel System
- AIR FORCE QPL-7899-2012 Valve, Check, Aircraft Fuel System
- AIR FORCE MIL-DTL-32392 A-2013 AIRCRAFT ARRESTING SYSTEM - TEXTILE (TAAS)
- AIR FORCE QPL-7899-20-2005 VALVES, CHECK, AIRCRAFT FUEL SYSTEM
- AIR FORCE MIL-V-7899 C NOTICE 1-1996 VALVE, CHECK, AIRCRAFT FUEL SYSTEM
- AIR FORCE MIL-V-7899 C-1979 VALVE, CHECK, AIRCRAFT FUEL SYSTEM
- AIR FORCE MIL-DTL-32392-2011 AIRCRAFT ARRESTING SYSTEM - TEXTILE (TAAS)
- AIR FORCE MIL-STD-3035-2013 USAF AIRCRAFT ARRESTING SYSTEMS
- AIR FORCE MIL-PRF-7024 F-2012 CALIBRATING FLUIDS, AIRCRAFT FUEL SYSTEM COMPONENTS
RTCA - RTCA@ Inc., aircraft system
- RTCA DO-377-2019 Minimum Aviation System Performance Standards for C2 Link Systems Supporting Operations of Unmanned Aircraft Systems in U.S. Airspace
Military Standard of the People's Republic of China-Commission of Science,Technology and Industry for National Defence, aircraft system
- GJB 1476A-2006 General refit requirements of flight test instrumentation system for aircraft
AENOR, aircraft system
RU-GOST R, aircraft system
- GOST 22945-1978 Fuel systems for airplanes. Terms and definitions
- GOST 24898-1981 Electrical power system of aircraft and helicopters. Reliability factor design procedure
National Metrological Verification Regulations of the People's Republic of China, aircraft system
- JJG(民航) 0070-2004 TCAS-201 Traffic Alert and Collision Avoidance System Ramp Test Set
IN-BIS, aircraft system
US-FCR, aircraft system
ES-UNE, aircraft system
中华人民共和国国家质量监督检验检疫总局、中国国家标准化管理委员会, aircraft system
Japanese Industrial Standards Committee (JISC), aircraft system
- JIS W 2913:1982 Hydraulic system components, aircraft, general specification for
Lithuanian Standards Office , aircraft system
- LST EN 302 480 V1.1.2-2008 Electromagnetic compatibility and Radio spectrum Matters (ERM); Harmonized EN for the GSM onboard aircraft system covering the essential requirements of Article 3.2 of the R&TTE Directive
ETSI - European Telecommunications Standards Institute, aircraft system
- ETSI EN 302 480:2008 Electromagnetic compatibility and Radio spectrum Matters (ERM); Harmonized EN for the GSM onboard aircraft system covering the essential requirements of Article 3.2 of the R&TTE Directive (V1.1.2)
- ETSI EN 302 480:2007 Electromagnetic compatibility and Radio spectrum Matters (ERM); Harmonized EN for the GSM onboard aircraft system covering essential requirements of Article 3.2 of the R&TTE Directive (V1.1.1)