Filter :
Standard and/or project | Stage | TC |
---|---|---|
Withdrawal of ISO/R 103-1959 |
95.99 | ISO/TC 20 |
Withdrawal of ISO/R 130-1959 |
95.99 | ISO/TC 20 |
Standard form of declaration of performance of aircraft electrical equipment |
95.99 | ISO/TC 20/SC 1 |
Aircraft — Declaration of design and performance for aircraft equipment — Standard form |
95.99 | ISO/TC 20 |
Withdrawal of ISO/R 267-1962 |
95.99 | ISO/TC 20 |
Withdrawal of ISO/R 414-1965 |
95.99 | ISO/TC 20 |
Withdrawal of ISO/R 440-1969 |
95.99 | ISO/TC 20 |
Withdrawal of ISO/R 470-1966 |
95.99 | ISO/TC 20 |
Withdrawal of ISO/R 474-1966 |
95.99 | ISO/TC 20 |
Withdrawal of ISO/R 507-1970 |
95.99 | ISO/TC 43 |
Withdrawal of ISO/R 539-1967 |
95.99 | ISO/TC 20 |
Withdrawal of ISO/R 564-1967 |
95.99 | ISO/TC 20 |
Withdrawal of ISO/R 634-1964 |
95.99 | ISO/TC 20 |
Withdrawal of ISO/R 854-1968 |
95.99 | ISO/TC 20 |
Withdrawal of ISO/R 1075-1969 |
95.99 | ISO/TC 20 |
Withdrawal of ISO/R 1076-1969 |
95.99 | ISO/TC 20 |
Withdrawal of ISO/R 1077-1969 |
95.99 | ISO/TC 20 |
Withdrawal of ISO/R 1078-1969 |
95.99 | ISO/TC 20 |
Flight dynamics — Concepts, quantities and symbols — Part 1: Aircraft motion relative to the air |
95.99 | ISO/TC 20 |
Flight dynamics — Concepts, quantities and symbols — Part 1: Aircraft motion relative to the air |
90.60 | ISO/TC 20/SC 8 |
Terms and symbols for flight dynamics — Part 2: Motions of the aircraft and the atmosphere relative to the Earth |
95.99 | ISO/TC 20 |
Flight dynamics — Concepts, quantities and symbols — Part 2: Motions of the aircraft and the atmosphere relative to the Earth |
90.20 | ISO/TC 20/SC 8 |
Flight dynamics — Concepts, quantities and symbols — Part 2: Motions of the aircraft and the atmosphere relative to the Earth — Addendum 1 |
60.60 | ISO/TC 20/SC 8 |
Terms and symbols for flight dynamics — Part 3: Derivatives of forces, moments and their coefficients |
95.99 | ISO/TC 20 |
Flight dynamics — Concepts, quantities and symbols — Part 3: Derivatives of forces, moments and their coefficients |
90.60 | ISO/TC 20/SC 8 |
Flight dynamics — Concepts, quantities and symbols — Part 3: Derivatives of forces, moments and their coefficients — Technical Corrigendum 1 |
60.60 | ISO/TC 20/SC 8 |
Terms and symbols for flight dynamics — Part 4: Concepts, quantities and symbols used in the study of aircraft stability and control |
95.99 | ISO/TC 20 |
Terms and symbols for flight dynamics — Part 4: Concepts, quantities and symbols used in the study of aircraft stability and control — Addendum 1 |
95.99 | ISO/TC 20 |
Flight dynamics — Concepts, quantities, and symbols — Part 4: Concepts and quantities used in the study of aircraft stability and control |
90.60 | ISO/TC 20/SC 8 |
Terms and symbols for flight dynamics — Part 5: Quantities used in measurements |
95.99 | ISO/TC 20 |
Flight dynamics — Concepts, quantities and symbols — Part 5: Quantities used in measurements |
90.20 | ISO/TC 20/SC 8 |
Terms and symbols for flight dynamics — Part 6: Aircraft geometry |
90.20 | ISO/TC 20/SC 8 |
Terms and symbols for flight dynamics — Part 6: Aircraft geometry — Amendment 1 |
60.60 | ISO/TC 20/SC 8 |
Flight dynamics — Concepts, quantities and symbols — Part 7: Flight points and flight envelopes |
95.99 | ISO/TC 20/SC 8 |
Flight dynamics — Vocabulary — Part 7: Flight points and flight envelopes |
60.60 | ISO/TC 20/SC 8 |
Flight dynamics — Concepts, quantities and symbols — Part 8: Concepts and quantities used in the study of the dynamic behaviour of the aircraft |
95.99 | ISO/TC 20/SC 8 |
Flight dynamics — Vocabulary — Part 8: Dynamic behaviour of aircraft |
60.60 | ISO/TC 20/SC 8 |
Flight dynamics — Concepts, quantities and symbols — Part 9: Models of atmospheric motions along the trajectory of the aircraft |
90.20 | ISO/TC 20/SC 8 |
Flight dynamics — Concepts, quantities and symbols — Part 9: Models of atmospheric motions along the trajectory of the aircraft — Amendment 1: Turbulence |
60.60 | ISO/TC 20/SC 8 |
Flight dynamics — Vocabulary — Part 11: Control system |
60.00 | ISO/TC 20/SC 8 |
Withdrawal of ISO 1151-1975 |
95.99 | ISO/TC 20 |
Withdrawal of ISO 1152-1974 |
95.99 | ISO/TC 20 |
Withdrawal of ISO 1153-1972 |
95.99 | ISO/TC 20 |
Withdrawal of ISO/R 1220-1970 |
95.99 | ISO/TC 20 |
Withdrawal of ISO/R 1468-1970 |
95.99 | ISO/TC 20 |
Withdrawal of ISO/R 1490-1970 |
95.99 | ISO/TC 20 |
Withdrawal of ISO/R 1491-1970 |
95.99 | ISO/TC 20 |
Withdrawal of ISO/R 1761-1970 |
95.99 | ISO/TC 43 |
Withdrawal of ISO/R 1799-1971 |
95.99 | ISO/TC 20 |
Withdrawal of ISO/R 1800-1971 |
95.99 | ISO/TC 20 |
Withdrawal of ISO 1963-1973 |
95.99 | ISO/TC 20 |
Standard Atmosphere |
90.60 | ISO/TC 20/SC 6 |
Standard Atmosphere — Addendum 1: Hypsometrical tables |
60.60 | ISO/TC 20/SC 6 |
Standard Atmosphere — Addendum 2: Extension to - 5000 m and standard atmosphere as a function of altitude in feet |
60.60 | ISO/TC 20/SC 6 |
Withdrawal of ISO 2650-1974 |
95.99 | ISO/TC 20 |
Environmental tests for aircraft equipment — Part 1: Ice formation |
95.99 | ISO/TC 20 |
Withdrawal of ISO 2655-1975 |
95.99 | ISO/TC 20 |
Withdrawal of ISO 2657-1976 |
95.99 | ISO/TC 20 |
Withdrawal of ISO 2658-1975 |
95.99 | ISO/TC 20 |
Environmental tests for aircraft equipment — Part 1: Steady state acceleration |
95.99 | ISO/TC 20 |
Environmental tests for aircraft equipment — Steady-state acceleration |
90.20 | ISO/TC 20 |
Environmental tests for aircraft equipment — Part 3.4 : Acoustic vibration |
95.99 | ISO/TC 20 |
Withdrawal of ISO 2676-1975 |
95.99 | ISO/TC 20 |
Withdrawal of ISO 2684-1975 |
95.99 | ISO/TC 20 |
Aircraft — Environmental conditions and test procedures for airborne equipment — Resistance to fire in designated fire zones |
95.99 | ISO/TC 20 |
Aircraft — Environmental conditions and test procedures for airborne equipment — Resistance to fire in designated fire zones |
95.99 | ISO/TC 20 |
Aircraft — Environmental test procedure for airborne equipment — Resistance to fire in designated fire zones |
90.93 | ISO/TC 20 |
Withdrawal of ISO 2764-1974 |
95.99 | ISO/TC 20 |
Withdrawal of ISO 2765-1974 |
95.99 | ISO/TC 20 |
Acoustics — Procedure for describing aircraft noise heard on the ground |
95.99 | ISO/TC 43/SC 1 |
Telecommunications and information exchange between systems — Unmanned aircraft area network (UAAN) — Part 1: Communication model and requirements |
60.60 | ISO/IEC JTC 1/SC 6 |
Telecommunications and information exchange between systems — Unmanned aircraft area network (UAAN) — Part 2: Physical and data link protocols for shared communication |
60.60 | ISO/IEC JTC 1/SC 6 |
Telecommunications and information exchange between systems — Unmanned aircraft area network (UAAN) — Part 3: Physical and data link protocols for control communication |
60.60 | ISO/IEC JTC 1/SC 6 |
Telecommunications and information exchange between systems — Unmanned aircraft area network (UAAN) — Part 4: Physical and data link protocols for video communication |
60.60 | ISO/IEC JTC 1/SC 6 |
Test methods for civil multi-copter unmanned aircraft system |
60.60 | ISO/TC 20/SC 16 |
UA wind gust test |
30.98 | ISO/TC 20/SC 16 |
Unmanned aircraft systems — Part 2: Operation of vertiports for vertical take-off and landing (VTOL) unmanned aircraft (UA) |
60.60 | ISO/TC 20/SC 16 |
Evaluation method for the resonance frequency of the multi-copter UA (unmanned aircraft) by measurement of rotor and body frequencies |
60.60 | ISO/TC 20/SC 16 |
Test method for flight stability of a multi-copter unmanned aircraft system (UAS) under wind and rain conditions |
60.60 | ISO/TC 20/SC 16 |
Acoustics — Measurement of noise inside aircraft |
95.99 | ISO/TC 43 |
Acoustics — Measurement of noise inside aircraft |
95.99 | ISO/TC 43/SC 1 |
Acoustics — Measurement of sound pressure levels in the interior of aircraft during flight |
90.93 | ISO/TC 43/SC 1 |
Acoustics — Measurement of sound pressure levels in the interior of aircraft during flight — Amendment 1 |
60.60 | ISO/TC 43/SC 1 |
Rotorcrafts – Flight dynamics – Vocabulary |
60.60 | ISO/TC 20/SC 8 |
Flight performance of civil small and light fixed-wing unmanned aircraft systems (UAS) — Test methods |
60.60 | ISO/TC 20/SC 16 |
Noise measurements for UAS (unmanned aircraft systems) |
60.00 | ISO/TC 20/SC 16 |
Civil small and light unmanned aircraft systems (UAS) — Vibration test methods |
60.00 | ISO/TC 20/SC 16 |
Civil small and light unmanned aircraft (UA) — Sharp injury to human body by rotor blades — Evaluation and test method |
60.60 | ISO/TC 20/SC 16 |
Civil small and light unmanned aircraft systems (UAS) under low-pressure conditions — Test methods |
60.60 | ISO/TC 20/SC 16 |
Vertiports — Infrastructure and equipment for vertical take-off and landing (VTOL) of electrically powered cargo unmanned aircraft systems (UAS) |
60.60 | ISO/TC 20/SC 17 |
Aerospace — List of equivalent terms — Part 4: Flight dynamics |
95.99 | ISO/TC 20/SC 8 |
Aerospace — List of equivalent terms — Part 4: Flight dynamics |
90.60 | ISO/TC 20/SC 8 |
Aerospace — List of equivalent terms — Part 5: Environmental and operating conditions for aircraft equipment |
90.20 | ISO/TC 20/SC 8 |
Aerospace — List of equivalent terms — Part 6: Standard atmosphere |
90.60 | ISO/TC 20/SC 8 |
Aerospace — List of equivalent terms — Part 8: Aircraft reliability |
90.60 | ISO/TC 20/SC 8 |
Aerospace — List of equivalent terms — Part 9: Aircraft |
90.60 | ISO/TC 20/SC 8 |
Reference atmospheres for aerospace use |
95.99 | ISO/TC 20/SC 6 |
Reference atmospheres for aerospace use — Addendum 1: Wind supplement |
95.99 | ISO/TC 20/SC 6 |
Reference atmospheres for aerospace use — Amendment 1 |
95.99 | ISO/TC 20/SC 6 |
Reference atmospheres for aerospace use — Addendum 2: Air humidity in the Northern Hemisphere |
95.99 | ISO/TC 20/SC 6 |
Aircraft — Environmental conditions and test procedures for airborne equipment |
95.99 | ISO/TC 20 |
Aircraft — Environmental conditions and test procedures for airborne equipment |
95.99 | ISO/TC 20 |
Aircraft — Environmental conditions and test procedures for airborne equipment |
95.99 | ISO/TC 20 |
Aircraft — Environmental conditions and test procedures for airborne equipment |
90.20 | ISO/TC 20 |
Aircraft equipment — Environmental and operating conditions for airborne equipment — Humidity, temperature and pressure tests |
90.93 | ISO/TC 20/SC 6 |
Middle atmosphere — Global model at altitudes between 30 km and 120 km, and wind model at altitudes above 30 km |
95.99 | ISO/TC 20/SC 6 |
Detection and Avoidance System for Unmanned Aircraft Systems |
30.60 | ISO/TC 20/SC 16 |
Space systems — Experience gained in space projects (Lessons learned) — Principles and guidelines |
95.99 | ISO/TC 20/SC 14 |
Space systems — Experience gained in space projects (lessons learned) — Principles and guidelines |
90.92 | ISO/TC 20/SC 14 |
Space systems — Lessons learned — Principles and guidelines |
60.00 | ISO/TC 20/SC 14 |
Dosemetry for exposures to cosmic radiation in civilian aircraft — Part 1: Conceptual basis for measurements |
95.99 | ISO/TC 85/SC 2 |
Dosimetry for exposures to cosmic radiation in civilian aircraft — Part 1: Conceptual basis for measurements |
95.99 | ISO/TC 85/SC 2 |
Dosimetry for exposures to cosmic radiation in civilian aircraft — Part 1: Conceptual basis for measurements |
60.60 | ISO/TC 85/SC 2 |
Dosimetry for exposures to cosmic radiation in civilian aircraft — Part 2: Characterization of instrument response |
95.99 | ISO/TC 85/SC 2 |
Dosimetry for exposures to cosmic radiation in civilian aircraft — Part 2: Characterization of instrument response |
60.60 | ISO/TC 85/SC 2 |
Dosimetry for exposures to cosmic radiation in civilian aircraft — Part 3: Measurements at aviation altitudes |
95.99 | ISO/TC 85/SC 2 |
Dosimetry for exposures to cosmic radiation in civilian aircraft — Part 3: Measurements at aviation altitudes |
60.60 | ISO/TC 85/SC 2 |
Dosimetry for exposures to cosmic radiation in civilian aircraft — Part 4: Validation of codes |
60.60 | ISO/TC 85/SC 2 |
Unmanned aircraft systems — Part 2: UAS components |
60.60 | ISO/TC 20/SC 16 |
Unmanned aircraft systems — Part 3: Operational procedures |
95.99 | ISO/TC 20/SC 16 |
Unmanned aircraft systems — Part 3: Operational procedures |
60.60 | ISO/TC 20/SC 16 |
Unmanned aircraft systems — Part 4: Vocabulary |
90.92 | ISO/TC 20/SC 16 |
Unmanned aircraft systems — Part 4: Vocabulary |
40.60 | ISO/TC 20/SC 16 |
Aircraft and space — Industrial data — Product identification and traceability |
95.99 | ISO/TC 20 |
Aircraft — Integrated data processing materials management — Bar coding |
95.99 | ISO/TC 20 |
Aircraft and space — Industrial data — Product identification and traceability |
60.60 | ISO/TC 20 |
Categorization and classification of civil unmanned aircraft systems |
60.60 | ISO/TC 20/SC 16 |
Agricultural and forestry machinery — Unmanned aerial spraying systems — Part 1: Environmental requirements |
60.60 | ISO/TC 23/SC 6 |
Agricultural and forestry machinery — Unmanned aerial spraying systems — Part 2: Test methods to assess the horizontal transverse spray distribution |
30.99 | ISO/TC 23/SC 6 |
Experiment results on test methods for detection and avoidance (DAA) systems for unmanned aircraft systems |
50.00 | ISO/TC 20/SC 16 |
UAS traffic management (UTM) — Part 1: Survey results on UTM |
60.60 | ISO/TC 20/SC 16 |
UAS traffic management (UTM) — Part 5: UTM functional structure |
60.60 | ISO/TC 20/SC 16 |
UAS traffic management (UTM) — Part 7: Data model for spatial data |
60.60 | ISO/TC 20/SC 16 |
UAS traffic management (UTM) — Part 8: Remote identification |
60.60 | ISO/TC 20/SC 16 |
UAS traffic management (UTM) — Part 9: Interface between UTM service providers and users |
60.00 | ISO/TC 20/SC 16 |
UAS traffic management (UTM) — Part 12: Requirements for UTM service providers |
60.60 | ISO/TC 20/SC 16 |
Unmanned aircraft systems — Training for personnel involved in UAS operations |
95.99 | ISO/TC 20/SC 16 |
Unmanned aircraft systems — Training for personnel involved in UAS operations |
60.60 | ISO/TC 20/SC 16 |
Technical requirements for small unmanned aircraft electric energy systems |
60.60 | ISO/TC 20/SC 16 |
General requirements for the payload interface of civil unmanned aircraft systems |
60.60 | ISO/TC 20/SC 16 |
Flight control system for civil small and light multicopter unmanned aircraft system (UAS) — General requirements |
60.60 | ISO/TC 20/SC 16 |
General requirements for tethered unmanned aircraft systems |
60.60 | ISO/TC 20/SC 16 |
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