| Name |
Description |
Abstract |
Status |
Publication date |
Edition |
Number of pages |
Technical committee |
ICS |
| ISO 1151-2:1974 |
Terms and symbols for flight dynamics — Part 2: Motions of the aircraft and the atmosphere relative to the Earth |
|
Withdrawn |
1974-03 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
01.060
Quantities and units
;
49.020
Aircraft and space vehicles in general
|
| ISO 1151-2:1985 |
Flight dynamics — Concepts, quantities and symbols — Part 2: Motions of the aircraft and the atmosphere relative to the Earth |
Gives basic definitions and deals with motion of the aircraft and the atmosphere relative to the earth. The atmosphere is assumed to be at rest or in translational motion at constant velocity relative to the Earth. The aircraft is assumed to be rigid. However, most of the definitions can be applied to the case of a flexible aircraft. Describes axis system, velocities flight path angles and wind direction angles.
|
Published |
1985-09 |
Edition : 2 |
Number of pages : 5 |
Technical Committee |
01.060
Quantities and units
;
49.020
Aircraft and space vehicles in general
|
| ISO 1151-2:1985/Add 1:1987 |
Flight dynamics — Concepts, quantities and symbols — Part 2: Motions of the aircraft and the atmosphere relative to the Earth — Addendum 1 |
|
Published |
1987-08 |
Edition : 2 |
Number of pages : 2 |
Technical Committee |
01.060
Quantities and units
;
49.020
Aircraft and space vehicles in general
|
| ISO 1151-3:1972 |
Terms and symbols for flight dynamics — Part 3: Derivatives of forces, moments and their coefficients |
|
Withdrawn |
1972-12 |
Edition : 1 |
Number of pages : 10 |
Technical Committee |
01.060
Quantities and units
;
49.020
Aircraft and space vehicles in general
|
| ISO 1151-3:1989 |
Flight dynamics — Concepts, quantities and symbols — Part 3: Derivatives of forces, moments and their coefficients |
Deals with derivatives of forces, moments and of other quantities characterizing such forces and moments. The term "derivative" designates the partial derivative of a function with respect to an independent variable. These derivatives appear in the terms of the Taylor series representing the variations of functions with the independent variables. Is restricted to first-order terms. Terms of higher order would require additional definitions of higher order. The aircraft is assumed to be rigid. However, most of the definitions can be applied to the case of a flexible aircraft.
|
Published |
1989-04 |
Edition : 2 |
Number of pages : 10 |
Technical Committee |
01.060
Quantities and units
;
49.020
Aircraft and space vehicles in general
|
| ISO 1151-3:1989/Cor 1:1996 |
Flight dynamics — Concepts, quantities and symbols — Part 3: Derivatives of forces, moments and their coefficients — Technical Corrigendum 1 |
Corrigendum relates to a formula in subclause 3.3.2.4.
|
Published |
1996-03 |
Edition : 2 |
Number of pages : 1 |
Technical Committee |
01.060
Quantities and units
;
49.020
Aircraft and space vehicles in general
|
| ISO 1151-4:1974 |
Terms and symbols for flight dynamics — Part 4: Concepts, quantities and symbols used in the study of aircraft stability and control |
|
Withdrawn |
1974-02 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
01.060
Quantities and units
;
49.020
Aircraft and space vehicles in general
|
| ISO 1151-4:1974/Add 1:1986 |
Terms and symbols for flight dynamics — Part 4: Concepts, quantities and symbols used in the study of aircraft stability and control — Addendum 1 |
|
Withdrawn |
1986-10 |
Edition : 1 |
Number of pages : 2 |
Technical Committee |
01.060
Quantities and units
;
49.020
Aircraft and space vehicles in general
|
| ISO 1151-4:1994 |
Flight dynamics — Concepts, quantities, and symbols — Part 4: Concepts and quantities used in the study of aircraft stability and control |
Cancels and replaces the first edition (1974) and addendum 1 (1986). Deals with the concepts, quantities and symbols used in the study of aircraft stability and control.
|
Published |
1994-11 |
Edition : 2 |
Number of pages : 7 |
Technical Committee |
01.060
Quantities and units
;
49.020
Aircraft and space vehicles in general
|
| ISO 14193:1998 |
Aerospace — Airframe spherical roller bearings, single row, self-aligning, sealed, extended inner ring intermediate duty — Inch series |
|
Withdrawn |
1998-04 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 1151-5:1987 |
Flight dynamics — Concepts, quantities and symbols — Part 5: Quantities used in measurements |
Includes the quantities used in flight measurements. Defines fundamental characteristics of the atmosphere, geometric and geopotential altitudes, equivalent altitudes related to a standard atmosphere, physical quantities related to motion of the aircraft in the atmosphere, measurement of quantities related to motion of the aircraft in the atmosphere, speeds and indicated Mach number, on-board accelerometer indications and terms used for pressure differences in some countries.
|
Published |
1987-05 |
Edition : 2 |
Number of pages : 8 |
Technical Committee |
01.060
Quantities and units
;
49.020
Aircraft and space vehicles in general
|
| ISO 1151-6:1982 |
Terms and symbols for flight dynamics — Part 6: Aircraft geometry |
Defines certain notions used for the geometric description of an aircraft for the purpose of flight dynamic studies. Does not give all the definitions that permit the detailed description of the shape of the aircraft. The aircraft is considered to be made up of various components. Defines general characteristics, overall dimensions of the aircraft, ground limit angles, fuselage, aerodynamic surfaces, wing and empennages. Gives figures.
|
Published |
1982-04 |
Edition : 2 |
Number of pages : 26 |
Technical Committee |
01.060
Quantities and units
;
49.020
Aircraft and space vehicles in general
|
| ISO 1151-6:1982/Amd 1:1984 |
Terms and symbols for flight dynamics — Part 6: Aircraft geometry — Amendment 1 |
Gives note 2 in 6.7.2.13. Includes the delection of the last part of the sentence, i.e. the example given in parentheses, so that the sentence reads as follows: 2. It may be useful to define the fin area by projecting the fin chord surface on some other surface that shall be specified.
|
Published |
1984-07 |
Edition : 2 |
Number of pages : 1 |
Technical Committee |
01.060
Quantities and units
;
49.020
Aircraft and space vehicles in general
|
| ISO 1151-7:1985 |
Flight dynamics — Concepts, quantities and symbols — Part 7: Flight points and flight envelopes |
Is intended to give definitions specifying the terms: mission, controls, geometric configuration, situation of the systems, state of the aircraft, environment, flight points, effective flight points and flight envelopes, which are necessary for safety analyses, for qualification purposes.
|
Published |
1985-08 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
01.060
Quantities and units
;
49.020
Aircraft and space vehicles in general
|
| ISO/DIS 1151-7 |
Flight dynamics — Vocabulary — Part 7: Flight points and flight envelopes |
Is intended to give definitions specifying the terms: mission, controls, geometric configuration, situation of the systems, state of the aircraft, environment, flight points, effective flight points and flight envelopes, which are necessary for safety analyses, for qualification purposes.
|
Under development |
|
Edition : 2 |
Number of pages : 7 |
Technical Committee |
01.060
Quantities and units
;
49.020
Aircraft and space vehicles in general
|
| ISO 1151-8:1992 |
Flight dynamics — Concepts, quantities and symbols — Part 8: Concepts and quantities used in the study of the dynamic behaviour of the aircraft |
The aircraft is assumed to be rigid, of constant mass and of constant inertia. It is not equipped with systems modifying its natural dynamic behaviour. However, most of the definitions can be applied to the case of a flexible aircraft, of variable mass and of variable inertia. The general concepts defined are applicable to the atmospheric flight phase.
|
Withdrawn |
1992-06 |
Edition : 1 |
Number of pages : 8 |
Technical Committee |
01.060
Quantities and units
;
49.020
Aircraft and space vehicles in general
|
| ISO 1151-8:2022 |
Flight dynamics — Vocabulary — Part 8: Dynamic behaviour of aircraft |
This document defines terms related to the concepts and quantities characterizing some classes of aircraft motion and their fundamental dynamic characteristics.
The aircraft is assumed to be rigid, of constant mass and of constant inertia. It is not equipped with systems modifying its natural dynamic behaviour. However, most of the definitions can be applied to the case of a flexible aircraft, of variable mass and of variable inertia.
The general concepts defined in this document are applicable to the atmospheric flight phase.
|
Published |
2022-11 |
Edition : 2 |
Number of pages : 16 |
Technical Committee |
01.060
Quantities and units
;
49.020
Aircraft and space vehicles in general
|
| ISO 1151-9:1993 |
Flight dynamics — Concepts, quantities and symbols — Part 9: Models of atmospheric motions along the trajectory of the aircraft |
Deals with the concepts and quantities characterizing models of the air motions affecting the dynamic behaviour of the aircraft. The motion of the air with respect to the Earth is defined by the wind velocity in each point of the aircraft trajectory. In flight dynamic problems, it is usual to use mathematical models of the wind velocity field and its variation with time. The following models are defined: constant wind, wind gradients, discrete gusts, three-dimensional wind models, vortices. Other models can be defined by superposition of these models.
|
Published |
1993-09 |
Edition : 1 |
Number of pages : 5 |
Technical Committee |
01.060
Quantities and units
;
49.020
Aircraft and space vehicles in general
|
| ISO 1151-9:1993/Amd 1:1998 |
Flight dynamics — Concepts, quantities and symbols — Part 9: Models of atmospheric motions along the trajectory of the aircraft — Amendment 1: Turbulence |
|
Published |
1998-10 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
01.060
Quantities and units
;
49.020
Aircraft and space vehicles in general
|
| ISO/CD 1151-11 |
Flight dynamics — Vocabulary — Part 11: Control system: classification, terminology, notions and definitions |
This document defines terms used in the field of flight control system.
|
Under development |
|
Edition : 2 |
|
Technical Committee |
49.020
Aircraft and space vehicles in general
;
01.040.49
Aircraft and space vehicle engineering (Vocabularies)
|
| ISO 1151:1972 |
Withdrawal of ISO 1151-1975 |
|
Withdrawn |
1972-12 |
Edition : 1 |
Number of pages : 19 |
Technical Committee |
01.060
Quantities and units
;
49.020
Aircraft and space vehicles in general
|
| ISO 1152:1974 |
Withdrawal of ISO 1152-1974 |
|
Withdrawn |
1974-12 |
Edition : 1 |
Number of pages : 5 |
Technical Committee |
01.060
Quantities and units
;
49.020
Aircraft and space vehicles in general
|
| ISO 1153:1972 |
Withdrawal of ISO 1153-1972 |
|
Withdrawn |
1972-12 |
Edition : 1 |
Number of pages : 10 |
Technical Committee |
01.060
Quantities and units
;
49.020
Aircraft and space vehicles in general
|
| ISO/R 1220:1970 |
Withdrawal of ISO/R 1220-1970 |
|
Withdrawn |
1970-07 |
Edition : 1 |
Number of pages : 7 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO/R 1468:1970 |
Withdrawal of ISO/R 1468-1970 |
|
Withdrawn |
1970-07 |
Edition : 1 |
Number of pages : 8 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO/R 1490:1970 |
Withdrawal of ISO/R 1490-1970 |
|
Withdrawn |
1970-07 |
Edition : 1 |
Number of pages : 5 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO/R 1491:1970 |
Withdrawal of ISO/R 1491-1970 |
|
Withdrawn |
1970-07 |
Edition : 1 |
Number of pages : 5 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO/R 1761:1970 |
Withdrawal of ISO/R 1761-1970 |
|
Withdrawn |
1970-12 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
17.140.30
Noise emitted by means of transport
|
| ISO/R 1799:1971 |
Withdrawal of ISO/R 1799-1971 |
|
Withdrawn |
1971-01 |
Edition : 1 |
Number of pages : 2 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO/R 1800:1971 |
Withdrawal of ISO/R 1800-1971 |
|
Withdrawn |
1971-01 |
Edition : 1 |
Number of pages : 7 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 1963:1973 |
Withdrawal of ISO 1963-1973 |
|
Withdrawn |
1973-04 |
Edition : 1 |
|
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 2533:1975 |
Standard Atmosphere |
Specifies the characteristics of the Atmosphere Type ISO which is applicable to planning under identical conditions, to test results end elements. Permits the unification in the range of tests and calibration of instruments. Is recommended for treatment of results of observations of geophysics and meteorology.
|
Published |
1975-05 |
Edition : 1 |
Number of pages : 108 |
Technical Committee |
07.060
Geology. Meteorology. Hydrology
;
17.020
Metrology and measurement in general
;
19.020
Test conditions and procedures in general
;
49.020
Aircraft and space vehicles in general
|
| ISO 2533:1975/Add 1:1985 |
Standard Atmosphere — Addendum 1: Hypsometrical tables |
|
Published |
1985-02 |
Edition : 1 |
Number of pages : 76 |
Technical Committee |
07.060
Geology. Meteorology. Hydrology
;
17.020
Metrology and measurement in general
;
19.020
Test conditions and procedures in general
;
49.020
Aircraft and space vehicles in general
|
| ISO 5129:1981 |
Acoustics — Measurement of noise inside aircraft |
|
Withdrawn |
1981-04 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
17.140.30
Noise emitted by means of transport
|
| ISO 2533:1975/Add 2:1997 |
Standard Atmosphere — Addendum 2: Extension to - 5000 m and standard atmosphere as a function of altitude in feet |
|
Published |
1997-11 |
Edition : 1 |
Number of pages : 123 |
Technical Committee |
07.060
Geology. Meteorology. Hydrology
;
17.020
Metrology and measurement in general
;
19.020
Test conditions and procedures in general
;
49.020
Aircraft and space vehicles in general
|
| ISO 2650:1974 |
Withdrawal of ISO 2650-1974 |
|
Withdrawn |
1974-03 |
Edition : 1 |
Number of pages : 2 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 2653-1:1975 |
Environmental tests for aircraft equipment — Part 1: Ice formation |
|
Withdrawn |
1975-11 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 2655:1975 |
Withdrawal of ISO 2655-1975 |
|
Withdrawn |
1975-07 |
Edition : 1 |
Number of pages : 5 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 2657:1976 |
Withdrawal of ISO 2657-1976 |
|
Withdrawn |
1976-09 |
Edition : 1 |
Number of pages : 5 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 2658:1975 |
Withdrawal of ISO 2658-1975 |
|
Withdrawn |
1975-07 |
Edition : 1 |
Number of pages : 1 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 2669-1:1978 |
Environmental tests for aircraft equipment — Part 1: Steady state acceleration |
|
Withdrawn |
1978-09 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 2669:1995 |
Environmental tests for aircraft equipment — Steady-state acceleration |
Cancels and replaces the first edition (1978). Lays down two types of steady-state acceleration test and establishes five severity grades of acceleration forces used to simulate a gradually changing acceleration environment representative of that which civil aircraft equipment can encounter in operational use. Does not apply to emergency landing case.
|
Published |
1995-04 |
Edition : 2 |
Number of pages : 10 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 2671:1982 |
Environmental tests for aircraft equipment — Part 3.4 : Acoustic vibration |
Specifies laboratory conditions for testing the ability of equipment for subsonic and supersonic civil aircraft to withstand vibration. Two types of tests are specified: tests for the functioning of the equipment and tests for its acoustic endurance. The necessity of such tests, the use of the wide band noise method or harmonic sound method, and the applicable test sound pressure level shall be specified in the relevant equipment specifications.
|
Withdrawn |
1982-10 |
Edition : 1 |
Number of pages : 9 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
17.140.30
Noise emitted by means of transport
|
| ISO 2676:1975 |
Withdrawal of ISO 2676-1975 |
|
Withdrawn |
1975-08 |
Edition : 1 |
Number of pages : 2 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 2684:1975 |
Withdrawal of ISO 2684-1975 |
|
Withdrawn |
1975-11 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 2685:1992 |
Aircraft — Environmental conditions and test procedures for airborne equipment — Resistance to fire in designated fire zones |
|
Withdrawn |
1992-07 |
Edition : 1 |
Number of pages : 29 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO/TR 2685:1984 |
Aircraft — Environmental conditions and test procedures for airborne equipment — Resistance to fire in designated fire zones |
|
Withdrawn |
1984-06 |
Edition : 1 |
Number of pages : 36 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 2685:1998 |
Aircraft — Environmental test procedure for airborne equipment — Resistance to fire in designated fire zones |
This International Standard specifies the tests conditions applied to all components, equipments and structures located in zones designated as "fire zones" and built to satisfy the minimum specified level for resistance to fire.
Two grades of resistance to fire are applicable to components, equipments and structures.
Annexes A and B give details of the types of burners providing the standard flame and how they shall be used.
This International Standard does not relate to the resistance to fire outside designated fire zones, nor to flammability requirements, nor to those conditions induced by the flame coming from the combustion chamber.
|
Published |
1998-12 |
Edition : 2 |
Number of pages : 29 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 2764:1974 |
Withdrawal of ISO 2764-1974 |
|
Withdrawn |
1974-12 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 3891:1978 |
Acoustics — Procedure for describing aircraft noise heard on the ground |
Provides specifications for four steps to be followed when describing the noise from a single aircraft operation. Provides a method for determining a noise-exposure measure for a succession of operations in a given time-interval. Discusses furthermore specific purposes for which these methods might be used, including certification, monitoring of noise levels and of noise-exposure, and land-use planning.
|
Withdrawn |
1978-01 |
Edition : 1 |
Number of pages : 24 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
17.140.30
Noise emitted by means of transport
|
| ISO/IEC 4005-1:2023 |
Telecommunications and information exchange between systems — Unmanned aircraft area network (UAAN) — Part 1: Communication model and requirements |
This document describes a communication model and requirements for unmanned aircraft area network (UAAN), which is a wireless distributed communication network for units related with UA services in level II.
It describes:
— the communication structure and operation;
— the purpose of the three types of communication and related services;
— the interoperation of the three types of communication;
— the interworking with upper layers.
|
Published |
2023-03 |
Edition : 1 |
Number of pages : 19 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
35.100.05
Multilayer applications
|
| ISO/IEC 4005-2:2023 |
Telecommunications and information exchange between systems — Unmanned aircraft area network (UAAN) — Part 2: Physical and data link protocols for shared communication |
This document describes communication protocols for the physical and data link layer of shared communication, which is a wireless distributed communication network for units related with UAs in level II.
Physical layer includes frame structure, encoding procedure, physical layer procedure and coexistence operations. Data link layer includes channel and slot, resource management, broadcast and exchange of data, synchronization, security, and interface with upper layer and other communication layers.
|
Published |
2023-03 |
Edition : 1 |
Number of pages : 65 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
35.100.10
Physical layer
;
35.100.20
Data link layer
|
| ISO/IEC 4005-3:2023 |
Telecommunications and information exchange between systems — Unmanned aircraft area network (UAAN) — Part 3: Physical and data link protocols for control communication |
This document specifies communication protocols for the physical and data link layer for control communication, which is wireless distributed communication network for units related with unmanned aircrafts (UAs) in level II.
This document describes control communication, which is one-to-one communication between a UA and a controller.
|
Published |
2023-03 |
Edition : 1 |
Number of pages : 59 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
35.100.10
Physical layer
;
35.100.20
Data link layer
|
| ISO/IEC 4005-4:2023 |
Telecommunications and information exchange between systems — Unmanned aircraft area network (UAAN) — Part 4: Physical and data link protocols for video communication |
This document specifies communication protocols for the physical and data link layer of video communication, which is a wireless distributed communication network for units related with unmanned aircrafts (UAs) in level II.
This document describes video communication, which is one-to-one communication that transmits video from a UA to a video receiver. For the specific use of video communication, video can be transmitted from a UA to multiple receivers.
|
Published |
2023-03 |
Edition : 1 |
Number of pages : 57 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
35.100.10
Physical layer
;
35.100.20
Data link layer
|
| ISO 4358 |
Test methods for civil multi-copter unmanned aircraft system |
|
Under development |
2023-05 |
Edition : 1 |
|
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO/CD TR 4594 |
UA wind gust test |
|
Under development |
|
Edition : 1 |
|
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 5015-2:2022 |
Unmanned aircraft systems — Part 2: Operation of vertiports for vertical take-off and landing (VTOL) unmanned aircraft (UA) |
This document specifies the requirements for vertiport operations (e.g. removal of contaminants, noise) and interface with an unmanned aircraft system (UAS) or vertical take-off and landing (VTOL) aircraft operators and with UAS traffic management (UTM) service providers (SPs).
This document is applicable to operations of vertiports belonging to any type, supporting:
a) demonstration of compliance with applicable regulations of vertiport operations to aviation authorities or other public authorities, as a possible acceptable means of compliance (AMC), when applicable regulations require such involvement from the authority and when the authority considers this document acceptable;
b) attestation of compliance of vertiport operations by qualified entities or other accredited, competent and independent third parties, supporting the safety risk assessment of the UAS operations required by regulations, in particular when high level of assurance robustness is required;
c) attestation of compliance of vertiport operations by qualified entities or other accredited, competent and independent third parties even in the absence of any applicable regulation.
This document also covers safety of the vertiport operator and quality of data provided by the vertiport operator to other entities (e.g. UAS operators, service providers of aeronautical information, providers of UTM services).
Aspects that are not covered by this document are:
— requirements for operational procedures of UAS;
— requirements for physical characteristics and equipment for vertiports;
— requirements for UTM SPs.
|
Published |
2022-08 |
Edition : 1 |
Number of pages : 21 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 14216:1998 |
Aerospace — Airframe ball bearings, double-row, self-aligning, sealed, heavy duty — Inch series |
|
Withdrawn |
1998-05 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 5129:1987 |
Acoustics — Measurement of noise inside aircraft |
Specifies the instrumentation and procedures for obtaining reproducible and comparable data. The results can be used to determine the compliance with maximum noise goals, to assess the noise exposure for hearing conservation purposes and to assess the degree of speech interference.
|
Withdrawn |
1987-12 |
Edition : 2 |
Number of pages : 4 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
17.140.30
Noise emitted by means of transport
|
| ISO 5129:2001 |
Acoustics — Measurement of sound pressure levels in the interior of aircraft during flight |
1.1 This International Standard specifies requirements for instruments and test procedures for the measurement
and reporting of sound pressure levels at crew and passenger locations in the interior of aircraft under steady flight
conditions. The sound pressure levels may be used to determine various quantities for describing the acoustical
environment in the interior of the aircraft. The procedures are intended to ensure uniformity in test results and to
provide the basis for determination of measurement uncertainties.
1.2 This International Standard provides electroacoustical performance specifications for a complete measurement
system from a microphone to the readout device. Various individual components of a measurement system may be
selected so long as the total measurement system conforms to the specifications of this International Standard.
1.3 The preferred measurement procedure involves the recording of sound pressure signals with subsequent
analysis into one-third-octave band sound pressure levels. Direct measurements may be made of one-third-octaveband
sound pressure levels.
|
Published |
2001-10 |
Edition : 3 |
Number of pages : 10 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
17.140.30
Noise emitted by means of transport
|
| ISO 5129:2001/Amd 1:2013 |
Acoustics — Measurement of sound pressure levels in the interior of aircraft during flight — Amendment 1 |
|
Published |
2013-05 |
Edition : 3 |
Number of pages : 3 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
17.140.30
Noise emitted by means of transport
|
| ISO 5224:2021 |
Rotorcrafts – Flight dynamics – Vocabulary |
This document defines terms used in the field of rotorcrafts flight dynamics and aerodynamics, for example, rotorcraft design documents, with regard to rotorcrafts geometry and dynamic characteristics.
|
Published |
2021-11 |
Edition : 1 |
Number of pages : 23 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
01.040.49
Aircraft and space vehicle engineering (Vocabularies)
|
| ISO/DIS 5286 |
Test methods for flight performance of civil light weight and small fixed-wing UAS |
|
Under development |
|
Edition : 1 |
Number of pages : 7 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO/DIS 5305 |
Noise measurements for UAS (Unmanned aircraft systems) |
|
Under development |
|
Edition : 1 |
Number of pages : 43 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO/DIS 5309 |
Vibration test methods for lightweight and small civil UAS |
|
Under development |
|
Edition : 1 |
Number of pages : 13 |
Technical Committee |
17.160
Vibrations, shock and vibration measurements
;
49.020
Aircraft and space vehicles in general
|
| ISO/DIS 5312 |
Evaluation and test method of rotor blade sharp injury to human body for civil lightweight and small UA |
|
Under development |
|
Edition : 1 |
Number of pages : 7 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO/DIS 5332 |
Test methods for civil lightweight and small UAS under low pressure conditions |
|
Under development |
|
Edition : 1 |
Number of pages : 7 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO/FDIS 5491 |
Vertiports — Infrastructure and equipment for vertical take-off and landing (VTOL) of electrically powered cargo unmanned aircraft systems (UAS) |
|
Under development |
|
Edition : 1 |
Number of pages : 11 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 5843-4:1988 |
Aerospace — List of equivalent terms — Part 4: Flight dynamics |
|
Withdrawn |
1988-04 |
Edition : 1 |
|
Technical Committee |
49.020
Aircraft and space vehicles in general
;
01.040.49
Aircraft and space vehicle engineering (Vocabularies)
|
| ISO 5843-4:1990 |
Aerospace — List of equivalent terms — Part 4: Flight dynamics |
Establishes a list of terms in English, French, Russian and German. The list is given in English in alphabetical order. This list is the fourth part of equivalent terms used in the field of aerospace construction.
|
Published |
1990-10 |
Edition : 2 |
Number of pages : 29 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
01.040.49
Aircraft and space vehicle engineering (Vocabularies)
|
| ISO 5843-5:1990 |
Aerospace — List of equivalent terms — Part 5: Environmental and operating conditions for aircraft equipment |
|
Published |
1990-05 |
Edition : 1 |
Number of pages : 32 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
01.040.49
Aircraft and space vehicle engineering (Vocabularies)
|
| ISO 5843-6:1985 |
Aerospace — List of equivalent terms — Part 6: Standard atmosphere |
Gives a list of terms in English, French, Russian and German. The list is given in English in alphabetical order. This list is the sixth part of equivalent terms used in the field of aerospace construction.
|
Published |
1985-06 |
Edition : 1 |
Number of pages : 19 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
01.040.49
Aircraft and space vehicle engineering (Vocabularies)
|
| ISO 5843-8:1988 |
Aerospace — List of equivalent terms — Part 8: Aircraft reliability |
Gives a list of terms in English, French, Russian and German. The list is given in English in alphabetical order. This list is the eighth part of equivalent terms used in the field of aerospace construction.
|
Published |
1988-03 |
Edition : 1 |
Number of pages : 14 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
01.040.49
Aircraft and space vehicle engineering (Vocabularies)
|
| ISO 5843-9:1988 |
Aerospace — List of equivalent terms — Part 9: Aircraft |
Lays down a list of terms in English, French, Russian and German. The list is given in English in alphabetical order. This list is the ninth part of equivalent terms used in the field of aerospace construction.
|
Published |
1988-03 |
Edition : 1 |
Number of pages : 16 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
01.040.49
Aircraft and space vehicle engineering (Vocabularies)
|
| ISO 5878:1982 |
Reference atmospheres for aerospace use |
Presents information on the seasonal, latidudinal, longitudinal and day-to-day variability of atmospheric properties at levels between the surface and 80 km. The systematic variation of atmospheric properties is shown for altitudes up to 80 km by a family of models, comprising the reference atmospheres tropical, sub-tropical, mid-latidude, sub-arctic and arctic. Furthermore temporal and spatial variations and frequency distributions of observed temperatures and densities are given.
|
Withdrawn |
1982-04 |
Edition : 1 |
Number of pages : 39 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 5878:1982/Add 1:1983 |
Reference atmospheres for aerospace use — Addendum 1: Wind supplement |
|
Withdrawn |
1983-02 |
Edition : 1 |
Number of pages : 58 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 5878:1982/Amd 1:1990 |
Reference atmospheres for aerospace use — Amendment 1 |
Mainly amends numerical values in table 4 on page 7, table 10 on page 13, table 13 on page 16, table 16 on page 20, tables 17 and 18 on page 21, table 21 on pages 24 to 27, table 22 on page 28. Modifies curves in figures 1 and 3 on pages 34 and 36.
|
Withdrawn |
1990-12 |
Edition : 1 |
Number of pages : 1 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 5878:1982/Add 2:1983 |
Reference atmospheres for aerospace use — Addendum 2: Air humidity in the Northern Hemisphere |
|
Withdrawn |
1983-11 |
Edition : 1 |
Number of pages : 9 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 7137:1981 |
Aircraft — Environmental conditions and test procedures for airborne equipment |
|
Withdrawn |
1981-10 |
Edition : 1 |
Number of pages : 1 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 7137:1987 |
Aircraft — Environmental conditions and test procedures for airborne equipment |
|
Withdrawn |
1987-05 |
Edition : 2 |
Number of pages : 2 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 7137:1992 |
Aircraft — Environmental conditions and test procedures for airborne equipment |
|
Withdrawn |
1992-12 |
Edition : 3 |
Number of pages : 3 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 7137:1995 |
Aircraft — Environmental conditions and test procedures for airborne equipment |
Cancels and replaces the third edition (1992). Lists the different environmental conditions and test procedures for airborne equipment and is primarily intended for civil and/or transport aircraft applications.
|
Published |
1995-06 |
Edition : 4 |
Number of pages : 4 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 9662:1994 |
Aircraft equipment — Environmental and operating conditions for airborne equipment — Humidity, temperature and pressure tests |
Applies primarily to civil and transport aircraft and specifies the test requirements and various test procedures for aerospace equipment which could be subjected to moisture ingress, frosting and condensation, resulting from the passage through atmospheric conditions of high humidity, in combination with or induced by changing temperature and pressure.
|
Published |
1994-02 |
Edition : 1 |
Number of pages : 5 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO/TR 14618:1996 |
Middle atmosphere — Global model at altitudes between 30 km and 120 km, and wind model at altitudes above 30 km |
Establishes a global model monthly mean of temperature, pressure, density and wind. These data can be used as a function of geopotential/geometric height. The zone has a latitudinal coverage from 80° S to 80° N, extending from altitudes between 30 km and 120 km. Serves as basis for the design and operation of aircraft and space vehicles.
|
Withdrawn |
1996-03 |
Edition : 1 |
Number of pages : 104 |
Technical Committee |
07.040
Astronomy. Geodesy. Geography
;
49.020
Aircraft and space vehicles in general
|
| ISO/CD 15964 |
Detection and Avoidance System for Unmanned Aircraft Systems |
This standard specifies 'safety and quality' requirements for detection and avoidance (DAA) systems used between UAS and other objects including aircraft. The standard includes the requirements of radar and optical sensors used for DAA and was derived to meet the requirements for UAS operations involving DAA set out in ISO 21384-3.
|
Under development |
|
Edition : 1 |
|
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 16192:2010 |
Space systems — Experience gained in space projects (Lessons learned) — Principles and guidelines |
ISO 16192:2010 outlines lessons learned principles and guidelines that are applicable in all space project activities (management, technical, quality, cost and schedule).
The application of ISO 16192:2010 is intended to be included in the supplier quality management system, but can be tailored in individual contracts as agreed by the customer and supplier, depending on
the content of each project (size, technological level and novelty, particular organization, participants, etc.), and
the interest and usefulness of the related information.
The lessons learned information can result from any situations which might be encountered in similar contexts for future projects, i.e.
undesirable experiences that need to be avoided;
strategies, rules, principles of design, validation, tests and operations that proved to be successful or necessary.
ISO 16192:2010 neither endorses nor recommends the transmission of company proprietary information to external entities as part of a lessons learned process.
Implementing a formal lessons learned process as outlined in ISO 16192:2010 makes it possible to capture and benefit from this information.
The lessons learned activity is an important contribution to the processing of the preventive and corrective actions specified in ISO 9001 and ISO 17666.
ISO 16192:2010 also provides lessons learned processes and suggested lessons learned forms.
|
Withdrawn |
2010-06 |
Edition : 1 |
Number of pages : 12 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
49.140
Space systems and operations
|
| ISO 16192:2017 |
Space systems — Experience gained in space projects (lessons learned) — Principles and guidelines |
ISO 16192:2017 outlines lessons learned principles and guidelines that are applicable in all space project activities (management, technical, quality, cost and schedule).
The application of this document is intended to be included in the supplier quality management system, but can be tailored in individual contracts as agreed by the customer and supplier, depending on:
- the content of each project (size, technological level and novelty, particular organization, participants, etc.);
- the interest and usefulness of the related information.
The lessons learned information can result from any situation which might be encountered in similar contexts for future projects, i.e.:
- undesirable experiences that need to be avoided;
- strategies, rules, principles of design, validation, tests and operations that proved to be successful or necessary.
ISO 16192:2017 neither endorses nor recommends the transmission of company proprietary information to external entities as part of a lessons learned process.
Implementing a formal lessons learned process as outlined in this document makes it possible to capture and benefit from this information.
The lessons learned activity is an important contribution to the processing of the preventive and corrective actions specified in ISO 9001 and ISO 17666.
ISO 16192:2017 also provides lessons learned processes and suggested lessons learned forms.
|
Published |
2017-04 |
Edition : 2 |
Number of pages : 13 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
49.140
Space systems and operations
|
| ISO/DIS 16192 |
Space systems — Experience gained in space projects (lessons learned) — Principles and guidelines |
ISO 16192:2017 outlines lessons learned principles and guidelines that are applicable in all space project activities (management, technical, quality, cost and schedule).
The application of this document is intended to be included in the supplier quality management system, but can be tailored in individual contracts as agreed by the customer and supplier, depending on:
- the content of each project (size, technological level and novelty, particular organization, participants, etc.);
- the interest and usefulness of the related information.
The lessons learned information can result from any situation which might be encountered in similar contexts for future projects, i.e.:
- undesirable experiences that need to be avoided;
- strategies, rules, principles of design, validation, tests and operations that proved to be successful or necessary.
ISO 16192:2017 neither endorses nor recommends the transmission of company proprietary information to external entities as part of a lessons learned process.
Implementing a formal lessons learned process as outlined in this document makes it possible to capture and benefit from this information.
The lessons learned activity is an important contribution to the processing of the preventive and corrective actions specified in ISO 9001 and ISO 17666.
ISO 16192:2017 also provides lessons learned processes and suggested lessons learned forms.
|
Under development |
|
Edition : 3 |
Number of pages : 13 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
49.140
Space systems and operations
|
| ISO 2020:1984 |
Aerospace — Mechanical system parts — Preformed flexible steel wire rope for aircraft controls — Technical specification |
|
Withdrawn |
1984-11 |
Edition : 2 |
Number of pages : 8 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 20785-1:2006 |
Dosemetry for exposures to cosmic radiation in civilian aircraft — Part 1: Conceptual basis for measurements |
ISO 20785-1:2006 gives the conceptual basis for the determination of ambient dose equivalent for the evaluation of exposure to cosmic radiation in civilian aircraft and for the calibration of instruments used for this purpose.
|
Withdrawn |
2006-04 |
Edition : 1 |
Number of pages : 26 |
Technical Committee |
13.280
Radiation protection
;
49.020
Aircraft and space vehicles in general
|
| ISO 20785-1:2012 |
Dosimetry for exposures to cosmic radiation in civilian aircraft — Part 1: Conceptual basis for measurements |
ISO 20785:2012 gives the conceptual basis for the determination of ambient dose equivalent for the evaluation of exposure to cosmic radiation in civilian aircraft and for the calibration of instruments used for this purpose.
|
Withdrawn |
2012-12 |
Edition : 2 |
Number of pages : 28 |
Technical Committee |
13.280
Radiation protection
;
49.020
Aircraft and space vehicles in general
|
| ISO 20785-1:2020 |
Dosimetry for exposures to cosmic radiation in civilian aircraft — Part 1: Conceptual basis for measurements |
This document specifies the conceptual basis for the determination of ambient dose equivalent for the evaluation of exposure to cosmic radiation in civilian aircraft and for the calibration of instruments used for that purpose.
|
Published |
2020-07 |
Edition : 3 |
Number of pages : 27 |
Technical Committee |
13.280
Radiation protection
;
49.020
Aircraft and space vehicles in general
|
| ISO 20785-2:2011 |
Dosimetry for exposures to cosmic radiation in civilian aircraft — Part 2: Characterization of instrument response |
ISO 20785-1:2011 specifies methods and procedures for characterizing the responses of devices used for the determination of ambient dose equivalent for the evaluation of exposure to cosmic radiation in civilian aircraft. The methods and procedures are intended to be understood as minimum requirements.
|
Withdrawn |
2011-06 |
Edition : 1 |
Number of pages : 36 |
Technical Committee |
13.280
Radiation protection
;
49.020
Aircraft and space vehicles in general
|
| ISO 20785-2:2020 |
Dosimetry for exposures to cosmic radiation in civilian aircraft — Part 2: Characterization of instrument response |
This document specifies methods and procedures for characterizing the responses of devices used for the determination of ambient dose equivalent for the evaluation of exposure to cosmic radiation in civilian aircraft. The methods and procedures are intended to be understood as minimum requirements.
|
Published |
2020-07 |
Edition : 2 |
Number of pages : 36 |
Technical Committee |
13.280
Radiation protection
;
49.020
Aircraft and space vehicles in general
|
| ISO 20785-3:2015 |
Dosimetry for exposures to cosmic radiation in civilian aircraft — Part 3: Measurements at aviation altitudes |
The following documents, in whole or in part, are normatively referenced in ISO 20785-3:2015 and are indispensable for its application. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies.
ISO/IEC Guide 98‑1, Uncertainty of measurement ? Part 1: Introduction to the expression of uncertainty in measurement
ISO/IEC Guide 98‑3, Uncertainty of measurement ? Part 3: Guide to the expression of uncertainty in measurement (GUM:1995)
ISO 20785‑1, Dosimetry for exposures to cosmic radiation in civilian aircraft ? Part 1: Conceptual basis for measurements
ISO 20785‑2, Dosimetry for exposures to cosmic radiation in civilian aircraft ? Part 2: Characterization of instrument response
|
Published |
2015-11 |
Edition : 1 |
Number of pages : 16 |
Technical Committee |
13.280
Radiation protection
;
49.020
Aircraft and space vehicles in general
|
| ISO/FDIS 20785-3 |
Dosimetry for exposures to cosmic radiation in civilian aircraft — Part 3: Measurements at aviation altitudes |
The following documents, in whole or in part, are normatively referenced in ISO 20785-3:2015 and are indispensable for its application. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies.
ISO/IEC Guide 98‑1, Uncertainty of measurement ? Part 1: Introduction to the expression of uncertainty in measurement
ISO/IEC Guide 98‑3, Uncertainty of measurement ? Part 3: Guide to the expression of uncertainty in measurement (GUM:1995)
ISO 20785‑1, Dosimetry for exposures to cosmic radiation in civilian aircraft ? Part 1: Conceptual basis for measurements
ISO 20785‑2, Dosimetry for exposures to cosmic radiation in civilian aircraft ? Part 2: Characterization of instrument response
|
Under development |
|
Edition : 2 |
Number of pages : 18 |
Technical Committee |
13.280
Radiation protection
;
17.240
Radiation measurements
;
49.020
Aircraft and space vehicles in general
|
| ISO 20785-4:2019 |
Dosimetry for exposures to cosmic radiation in civilian aircraft — Part 4: Validation of codes |
This document is intended for the validation of codes used for the calculation of doses received by individuals on board aircraft. It gives guidance to radiation protection authorities and code developers on the basic functional requirements which the code fulfils.
Depending on any formal approval by a radiation protection authority, additional requirements concerning the software testing can apply.
|
Published |
2019-05 |
Edition : 1 |
Number of pages : 8 |
Technical Committee |
13.280
Radiation protection
;
49.020
Aircraft and space vehicles in general
|
| ISO 21384-2:2021 |
Unmanned aircraft systems — Part 2: UAS components |
This document specifies requirements for ensuring the quality and safety of the design and manufacture of unmanned aircraft systems (UAS) that include unmanned aircraft (UA), remote pilot stations (RPS), datalinks, payloads, and associated support equipment.
This document includes information regarding the unmanned aircraft, any associated remote pilot station (RPS)(s), the command and control links (C2 Link), any other required data links (e.g. payload, traffic management information, vehicle identification) and any other system elements as can be required. This document does not cover passenger carrying UAS or technical requirements for the design and manufacturing for UAS components.
This document does not include equipment considerations unique to compliance with UA traffic management systems.
The document is applicable to the reasonable expected use of a UAS.
This document is applicable:
a) to UAS designed for use where a State aviation authority has determined a Certificate of Airworthiness (C of A) is not required;
b) where a C of A is required, to complement technical standards published by the aviation authority for the purposes of building the certification basis; or
c) as an alternative means of compliance if acceptable to the aviation authority.
|
Published |
2021-12 |
Edition : 1 |
Number of pages : 38 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 21384-3:2019 |
Unmanned aircraft systems — Part 3: Operational procedures |
This document specifies the requirements for safe commercial UAS operations.
|
Published |
2019-11 |
Edition : 1 |
Number of pages : 18 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO/FDIS 21384-3 |
Unmanned aircraft systems — Part 3: Operational procedures |
|
Under development |
|
Edition : 2 |
|
Technical Committee |
49.020
Aircraft and space vehicles in general
|