| Name |
Description |
Abstract |
Status |
Publication date |
Edition |
Number of pages |
Technical committee |
ICS |
| ISO 21384-4:2020 |
Unmanned aircraft systems — Part 4: Vocabulary |
This document defines terms and definitions relating to unmanned aircraft systems that are widely used in science and technology.
|
Published |
2020-05 |
Edition : 1 |
Number of pages : 10 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
01.040.49
Aircraft and space vehicle engineering (Vocabularies)
|
| ISO/DIS 21384-4 |
Unmanned aircraft systems — Part 4: Vocabulary |
This document defines terms and definitions relating to unmanned aircraft systems that are widely used in science and technology.
|
Under development |
|
Edition : 2 |
Number of pages : 22 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
01.040.49
Aircraft and space vehicle engineering (Vocabularies)
|
| ISO 21849:2006 |
Aircraft and space — Industrial data — Product identification and traceability |
ISO 21849:2006 specifies the requirements for a product identification and traceability schema for life cycle management of aircraft and space products/parts. It specifies the minimum essential identification information needed for traceability of a product for its life cycle. It also provides the data structures for use with automatic identification technologies that support product/part life cycle data management activities.
ISO 21849:2006 defines a structure and rules for establishing a unique identifier for product/part identification and traceability. The rules and structure provide sufficient options to support various business practices. They provide the minimum amount of standardization required to support interoperability, improved business processes and efficiency across multiple users and applications of machine-readable media technologies.
ISO 21849:2006 also defines and establishes repeatable processes to allow efficient exchange of product data for life cycle product/part traceability, configuration, reliability, maintenance, and product performance management purposes.
It specifies the data carriers appropriate for representing the product data in a machine-readable form and associated dimensional and quality parameters.
Industries or trading partners will need to develop specific implementation guidelines to employ the principles defined in ISO 21849:2006.
Although primarily intended for aircraft and space products/parts, ISO 21849:2006 may be used for other products/parts where desired.
|
Withdrawn |
2006-12 |
Edition : 1 |
Number of pages : 58 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
35.240.60
IT applications in transport
|
| ISO/TS 21849:2003 |
Aircraft — Integrated data processing materials management — Bar coding |
ISO/TS 21849:2003 establishes the requirements for receipts and permanent bar code identification in the field of integrated data processing management for aircrafts.
|
Withdrawn |
2003-07 |
Edition : 1 |
Number of pages : 15 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
35.240.60
IT applications in transport
|
| ISO 21849:2022 |
Aircraft and space — Industrial data — Product identification and traceability |
This document specifies the requirements for a product identification and traceability schema for life cycle management of aircraft and space products/parts. It specifies the minimum essential identification information needed for traceability of a product for its life cycle. It also provides the data structures for use with automatic identification technologies that support product/part life cycle data management activities.
This document defines a structure and rules for establishing a unique identifier for product/part identification and traceability. The rules and structure provide sufficient options to support various business practices. They provide the minimum amount of standardization required to support interoperability, improved business processes and efficiency across multiple users and applications of machine-readable media technologies.
This document also defines and establishes repeatable processes to allow efficient exchange of product data for life cycle product/part traceability, configuration, reliability, maintenance, and product performance management purposes.
It specifies the data carriers appropriate for representing the product data in a machine-readable form and associated dimensional and quality parameters.
Specific implementation guidelines can be developed by industries or trading partners to employ the principles defined in this document.
Although primarily intended for aircraft and space products/parts, this document can be used for other products/parts where desired.
|
Published |
2022-01 |
Edition : 2 |
Number of pages : 46 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
35.240.60
IT applications in transport
|
| ISO 13414:1997 |
Aerospace — Airframe needle roller bearings, single-row, shielded — Inch series |
|
Withdrawn |
1997-12 |
Edition : 1 |
Number of pages : 5 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 21895:2020 |
Categorization and classification of civil unmanned aircraft systems |
This document specifies requirements for the classification and grading of civil unmanned aircraft system (UAS). This document applies to heavier than air aircraft as well as lighter than air aircraft of any possible architecture.
This document applies to the industrial conception, development, design, production and delivery of civil UAS. It also applies to modification, repair and maintenance of civil UAS.
The characteristics in this document can be used individually or in combination, to meet specific needs of the classification and grading of civil UAS.
Risk-based categorization of UAS operations is prerogative of the aviation authorities and it is hence out of scope of this document.
|
Published |
2020-02 |
Edition : 1 |
Number of pages : 7 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO/FDIS 23117-1 |
Agricultural and forestry machinery — Unmanned aerial spraying systems — Part 1: Environmental requirements |
|
Under development |
|
Edition : 1 |
Number of pages : 12 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
65.060.40
Plant care equipment
|
| ISO/CD 23117-2 |
Agricultural and forestry machinery — Unmanned aerial spraying systems — Part 2: Test methods to assess the horizontal transverse spray deposition |
|
Under development |
|
Edition : 1 |
|
Technical Committee |
49.020
Aircraft and space vehicles in general
;
65.060.40
Plant care equipment
|
| ISO/TR 23629-1:2020 |
UAS traffic management (UTM) — Part 1: Survey results on UTM |
This document provides results of a survey on UTM which indicates aggregated data from survey respondents. It does not cover detailed analysis of regions and organizations.
UTM is expected to reveal hundreds of commercial applications already in place, as well as social systems as their background conditions. The results can be used to analyze benefits and gaps for possible future standardization topics in consultation with authorities such as ICAO.
|
Published |
2020-04 |
Edition : 1 |
Number of pages : 15 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 23629-5 |
UAS traffic management (UTM) — Part 5: UTM functional structure |
|
Under development |
2023-04 |
Edition : 1 |
|
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 23629-7:2021 |
UAS traffic management (UTM) — Part 7: Data model for spatial data |
This document specifies the data model that is related to various spatial information for common use between the UAS service provider and the system for operation control, e.g. UTM. This document specifies the names of the items for the data model, while the communication architecture and responsibilities of actors to define the items are not included.
|
Published |
2021-09 |
Edition : 1 |
Number of pages : 26 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 23629-8 |
UAS Traffic Management (UTM) — Part 8: Remote identification |
|
Under development |
2023-04 |
Edition : 1 |
|
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO/DIS 23629-9 |
UAS traffic management (UTM) — Part 9: Interface between UTM service providers and users |
This document mainly specifies minimum requirements for elements of information exchange between UTM service providers(USP) and different users to support relevant UTM services between them, while the protocol requirements and transmission requirements of UTM actors at the operational level are not included.
|
Under development |
|
Edition : 1 |
Number of pages : 19 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
03.080.99
Other services
|
| ISO 23629-12:2022 |
UAS traffic management (UTM) — Part 12: Requirements for UTM service providers |
This document includes compliance monitoring, safety, security, privacy and other organisational requirements for providers in the context of UAS traffic management services.
|
Published |
2022-07 |
Edition : 1 |
Number of pages : 25 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
03.080.99
Other services
|
| ISO 23665:2021 |
Unmanned aircraft systems — Training for personnel involved in UAS operations |
This document describes the procedures for training personnel who will be involved in the operation of unmanned aircraft systems (UAS).
This document defines:
a) knowledge, skill, attitude and qualification criteria that are needed for UAS pilots and training organizations that provides training to trainees of UAS remote pilots and other personnel involved in UAS operations;
b) training curriculum and contents for specific learning courses;
c) qualification and confirmation criteria for the training organizations;
d) general procedures for providing training of UAS personnel. The requirements for a specific course as described in the annexes can be more restrictive in some cases.
|
Published |
2021-01 |
Edition : 1 |
Number of pages : 35 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
03.100.30
Management of human resources
|
| ISO 13415:1997 |
Aerospace — Airframe needle track roller, stud type, single-row, sealed — Inch series |
|
Withdrawn |
1997-12 |
Edition : 1 |
Number of pages : 11 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO/DIS 23665 |
Unmanned aircraft systems — Training for personnel involved in UAS operations |
This document describes the procedures for training personnel who will be involved in the operation of unmanned aircraft systems (UAS).
This document defines:
a) knowledge, skill, attitude and qualification criteria that are needed for UAS pilots and training organizations that provides training to trainees of UAS remote pilots and other personnel involved in UAS operations;
b) training curriculum and contents for specific learning courses;
c) qualification and confirmation criteria for the training organizations;
d) general procedures for providing training of UAS personnel. The requirements for a specific course as described in the annexes can be more restrictive in some cases.
|
Under development |
|
Edition : 2 |
Number of pages : 35 |
Technical Committee |
49.020
Aircraft and space vehicles in general
;
03.100.30
Management of human resources
|
| ISO 24352 |
Technical requirements for small unmanned aircraft electric energy systems |
|
Under development |
2023-05 |
Edition : 1 |
|
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO/FDIS 24354 |
General Requirements of Civil Small and Light Unmanned Aircraft System Payload Interface |
|
Under development |
|
Edition : 1 |
|
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 24355 |
Flight control system for civil small and light multicopter unmanned aircraft system (UAS) — General requirements |
|
Under development |
|
Edition : 1 |
|
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 24356:2022 |
General requirements for tethered unmanned aircraft systems |
This document specifies general and manufacturing requirements for tethered unmanned aircraft systems (tUAS), including heavier-than-air tethered unmanned aircraft (tUA), which are powered by equipment on the ground. The specifications are intended for tUAS where the purpose for the tether is to supply power to the tUA as well as to provide a mechanical restraint. Unmanned aircrafts (UAs) that are not receiving power from and only restrained by the tether are referred to ISO 21384-2; however, there are clauses in this document that apply to the tethering equipment (e.g. winches and cables).
This document is applicable to the development, manufacturing, industrial applications and delivery of tUAS.
|
Published |
2022-08 |
Edition : 1 |
Number of pages : 12 |
Technical Committee |
49.020
Aircraft and space vehicles in general
|
| ISO 3800-1:1977 |
Threaded fasteners — Axial load fatigue testing — Part 1: Test methods |
|
Withdrawn |
1977-05 |
Edition : 1 |
Number of pages : 7 |
Technical Committee |
21.060
Fasteners
|
| ISO 413:1974 |
Aircraft — Heads of lubricating nipples |
Specifies the envelope dimensions of axial type nipples and determines the clearance space which shall be provided in the region of the nipple to allow the lubricating gun to be connected, and the operating angle dimensions for the lubricating process. The tip design of the nipples is optional provided the profile remains within the envelope shown in figure 1.
|
Published |
1974-11 |
Edition : 1 |
Number of pages : 1 |
Technical Committee |
49.035
Components for aerospace construction
;
49.100
Ground service and maintenance equipment
|
| ISO 1002:1983 |
Rolling bearings — Airframe bearings — Characteristics, boundary dimensions, tolerances, static load ratings |
Applies to rolling bearings, other than tapered roller bearings. The term airframe is defined. Both metric and inch series bearings are included because of established usage in the aircraft industry. The bearings included in ISO 1002 are usually full complement bearings with basically cylindrical bore and outside surface and are sealed or shielded.
|
Published |
1983-06 |
Edition : 1 |
Number of pages : 18 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 1971:1975 |
Aircraft — Accessory drives and mounting pads |
Provides a design for quick-release couplings with involute spline drive, intended primarily for aircraft engine/gearbox accessories which require to be removed whilst the engine/gearbox is in service. Comprises design notes and recommendations, accessory flanges up to and above spigot reference 25O, engine/gearbox pads up to and above spigot reference 250, coupling clamps, selected involute splines.
|
Published |
1975-03 |
Edition : 1 |
Number of pages : 17 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 2020-1:1997 |
Aerospace — Preformed flexible steel wire rope for aircraft controls — Part 1: Dimensions and loads |
|
Published |
1997-08 |
Edition : 1 |
Number of pages : 5 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 2020-2:1997 |
Aerospace — Preformed flexible steel wire rope for aircraft controls — Part 2: Technical specification |
|
Published |
1997-08 |
Edition : 1 |
Number of pages : 9 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 2020:1973 |
Flexible steel wire rope for aircraft controls — Technical specification |
|
Withdrawn |
1973-02 |
Edition : 1 |
Number of pages : 5 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 7938:1986 |
Aircraft — Ball bearings for control cable pulleys — Dimensions and loads |
Specifies the requirements for sealed or shielded ball bearings for use in control cable pulleys conforming to ISO 7939 within the temperature range from -55 to +120 °C. Lays down materials, surface treatment, lubrication, designation and marking.
|
Withdrawn |
1986-02 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 7939:1988 |
Aircraft — Non-metallic pulleys with ball bearings for control cables — Dimensions and loads |
Includes the requirements for these pulleys and incorporating ball bearings conforming to ISO 7938. The pulleys shall only be used within the temperature range from -54 °C to + 100 °C. Gives the description, pulley body manufacture, designation, marking, technical specification.
|
Withdrawn |
1988-10 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 8399-1:1998 |
Aerospace — Accessory drives and mounting flanges (Metric series) — Part 1: Design criteria |
This part of ISO 8399 establishes the design criteria for accessory drives and mounting flanges with quick attach/detach provisions primarily intended for use in aircraft gearboxes or engine accessories.
NOTE — Some design criteria are subject to agreement between the engine/gearbox manufacturer and the accessory manufacturer (see clause 10).
|
Withdrawn |
1998-12 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 8399-2:1998 |
Aerospace — Accessory drives and mounting flanges (Metric series) — Part 2: Dimensions |
This part of ISO 8399 specifies the dimensions of couplings for accessory drives and mounting flanges with quick
attach/detach provisions primarily intended for use in aircraft gearboxes and engine accessories.
|
Published |
1998-12 |
Edition : 1 |
Number of pages : 11 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 9736:2000 |
Aerospace — Eye-ends, in steel, threaded, for aircraft control wire rope — Dimensions and loads |
This International Standard specifies the characteristics of eye-ends, in either low alloy steel or corrosion-resistant
steel, intended for the turnbarrels of aircraft control wire rope.
|
Published |
2000-12 |
Edition : 1 |
Number of pages : 5 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 9737:2000 |
Aerospace — Eye-ends, in corrosion-resistant steel, swaged on aircraft control wire rope — Dimensions and loads |
This International Standard specifies the characteristics of eye-ends in corrosion-resistant steel swaged on aircraft
control wire rope.
|
Published |
2000-12 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 9738:2000 |
Aerospace — Turnbarrels, for aircraft control wire rope — Dimensions and loads |
This International Standard specifies the characteristics of turnbarrels for aircraft control wire rope in either low alloy
steel, corrosion-resistant steel, copper-zinc alloy or aluminium alloy.
|
Published |
2000-12 |
Edition : 1 |
Number of pages : 5 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 9747:2000 |
Aerospace — Double-shank ball-ends, in corrosion-resistiant steel, swaged on aircraft control wire rope — Dimensions and loads |
This International Standard specifies the characteristics of double-shank ball-ends in corrosion-resistant steel swaged
on aircraft control wire rope.
|
Published |
2000-12 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 9748:2000 |
Aerospace — Ball-ends, in corrosion-resistant steel, swaged on aircraft control wire rope — Dimensions and loads |
This International Standard specifies the characteristics of ball-ends in corrosion-resistant steel swaged on aircraft
control wire rope.
|
Published |
2000-12 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 9749:2000 |
Aerospace — Stud-ends, in corrosion-resistant steel, swaged on aircraft control wire rope — Dimensions and loads |
This International Standard specifies the characteristics of stud-ends in corrosion-resistant steel swaged on aircraft
control wire rope.
|
Published |
2000-12 |
Edition : 1 |
Number of pages : 5 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 9757:2000 |
Aerospace — Fork-ends, in steel, threaded, for aircraft control wire rope turnbarrels — Dimensions and loads |
This International Standard specifies the characteristics of fork-ends, in either low alloy steel or corrosion-resistant
steel, for aircraft control cable turnbarrels.
|
Published |
2000-12 |
Edition : 1 |
Number of pages : 5 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 9758:2000 |
Aerospace — Fork-ends, in steel, threaded, for rolling bearings, for aircraft control wire rope — Dimensions and loads |
This International Standard specifies the characteristics of fork-ends for rolling bearings, in either low alloy steel or
corrosion-resistant steel, for aircraft control wire rope.
|
Published |
2000-12 |
Edition : 1 |
Number of pages : 5 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 9759:2000 |
Aerospace — Fork-ends, in corrosion-resistiant steel, swaged on aircraft control wire rope — Dimensions and loads |
This International Standard specifies the characteristics of fork-ends in corrosion-resistant steel swaged on aircraft
control wire rope.
|
Published |
2000-12 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 9760:2000 |
Aerospace — Fork-ends, in corrosion-resistant steel, swaged on aircraft control wire rope for rolling bearings — Dimensions and loads |
This International Standard specifies the characteristics of fork-ends for rolling bearings in corrosion-resistant steel
swaged on aircraft control wire rope.
|
Published |
2000-12 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 9761:2000 |
Aerospace — Locking clips, in corrosion-resistant steel, for aircraft control wire rope turnbuckles — Dimensions |
This International Standard specifies the characteristics of locking clips in corrosion-resistant steel for aircraft
control wire rope turnbuckles.
|
Published |
2000-12 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 9762:2000 |
Aerospace — Aircraft control wire rope assemblies — Dimensions and end-fitting combinations |
This International Standard specifies the possible combinations and lengths of preformed flexible steel wire ropes
for aircraft controls equipped with two end-fittings swaged on each end of the cable and the corresponding
designations.
|
Published |
2000-12 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 9763:1999 |
Aerospace — Aircraft control wire rope assemblies — Technical specification |
This International Standard specifies the characteristics, inspections and test methods as well as the quality
assurance requirements for aircraft control wire rope assemblies equipped with swaged end fittings. This
International Standard is applicable to control wire rope assemblies as defined in ISO 9762.
|
Published |
1999-08 |
Edition : 1 |
Number of pages : 8 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 10792-1:1995 |
Aerospace — Airframe spherical plain bearings in corrosion-resisting steel with self-lubricating liner — Part 1: Metric series |
Specifies the characteristics of spherical plain bearings of the metric series (without rolling elements) in corrosion-resisting steel with self-lubricating liner for elevated loads at ambient temperature, for use in fixed and moving parts of the aircraft structur and control mechanisms at temperatures of -55 °C to +163 °C.
|
Withdrawn |
1995-07 |
Edition : 1 |
Number of pages : 5 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 10792-2:1995 |
Aerospace — Airframe spherical plain bearings in corrosion-resisting steel with self-lubricating liner — Part 2: Inch series |
Specifies the characteristics of spherical plain bearings of the inch series (without rolling elements) in corrosion-resisting steel with self-lubricating liner for elevated loads at ambient temperature, for use in fixed and moving parts of the aircraft structure and control mechanisms at temperatures of -55 °C to +163 °C.
|
Published |
1995-07 |
Edition : 1 |
Number of pages : 10 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 10792-3:1995 |
Aerospace — Airframe spherical plain bearings in corrosion-resisting steel with self-lubricating liner — Part 3: Technical specification |
Contains a technical specification (characteristics, methods for checks and tests, quality assurance and acceptance conditions) for spherical plain bearings in corrosion-resisting steel with self-lubricating liner.
|
Withdrawn |
1995-07 |
Edition : 1 |
Number of pages : 20 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 10955:1999 |
Aerospace — End-fittings and turnbarrels for aircraft control wire rope — Technical specification |
This International Standard specifies the characteristics, the inspection and test methods as well as the quality
assurance requirements for:
end-fittings swaged on wire ropes, as specified in ISO 9737, ISO 9747, ISO 9748, ISO 9749, ISO 9759 and
ISO 9760,
wire rope turnbarrel parts, as specified in ISO 9736, ISO 9738, ISO 9757, ISO 9758 and ISO 9761, and
wire rope turnbarrel assemblies (as defined in 3.1),
used in aircraft controls.
This International Standard is applicable to the parts cited above providing that reference is made to it in the product
standard or the definition document.
|
Withdrawn |
1999-09 |
Edition : 1 |
Number of pages : 13 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 13411:1997 |
Aerospace — Airframe needle roller, cylindrical roller and track roller bearings — Technical specification |
|
Withdrawn |
1997-12 |
Edition : 1 |
Number of pages : 25 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 13412:1997 |
Aerospace — Airframe needle track roller, yoke type, single-row, sealed — Inch series |
|
Withdrawn |
1997-12 |
Edition : 1 |
Number of pages : 9 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 13413:1997 |
Aerospace — Airframe needle track roller, yoke type, double-row, sealed — Inch series |
|
Withdrawn |
1997-12 |
Edition : 1 |
Number of pages : 9 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 14194:1998 |
Aerospace — Airframe spherical roller bearings, double row, self-aligning, sealed, extended inner ring, heavy duty — Inch series |
|
Withdrawn |
1998-04 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 14195:1998 |
Aerospace — Airframe spherical roller bearings, double row, self-aligning, sealed, torque tube design, light duty — Inch series |
|
Withdrawn |
1998-04 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 14196:1998 |
Aerospace — Airframe spherical roller bearings, double row, self-aligning, sealed, plain inner ring, heavy duty — Inch series |
|
Withdrawn |
1998-04 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 14197:1998 |
Aerospace — Airframe spherical roller bearings, single row, self-aligning, sealed, intermediate duty — Inch series |
|
Withdrawn |
1998-04 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 14201:1998 |
Aerospace — Airframe ball bearings, double-row, self-aligning, diameter series 2 — Metric series |
|
Withdrawn |
1998-05 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 14202:1998 |
Aerospace — Airframe ball bearings, single-row, rigid, diameter series 0 and 2 — Metric series |
|
Withdrawn |
1998-05 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 14203:1998 |
Aerospace — Airframe ball bearings, single-row, rigid, diameter series 8 and 9 — Metric series |
|
Withdrawn |
1998-05 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 14204:1998 |
Aerospace — Airframe ball bearings, double-row, rigid, diameter series 0 — Metric series |
|
Withdrawn |
1998-04 |
Edition : 1 |
Number of pages : 5 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 14206:1998 |
Aerospace — Airframe ball bearings, single-row, rigid, sealed, light duty — Inch series |
|
Withdrawn |
1998-05 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 14207:1998 |
Aerospace — Airframe ball bearings, single-row, rigid, precision, sealed, light duty — Inch series |
|
Withdrawn |
1998-05 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 14208:1998 |
Aerospace — Airframe ball bearings, single-row, rigid, sealed, intermediate duty — Inch series |
|
Withdrawn |
1998-05 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 14209:1998 |
Aerospace — Airframe ball bearings, single-row, rigid, precision, sealed, intermediate duty — Inch series |
|
Withdrawn |
1998-05 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 14210:1998 |
Aerospace — Airframe ball bearings, single-row, rigid, sealed, torque tube design, light duty — Inch series |
|
Withdrawn |
1998-05 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 14211:1998 |
Aerospace — Airframe ball bearings, single-row, rigid, precision, sealed, torque tube design, light duty — Inch series |
|
Withdrawn |
1998-05 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 14212:1998 |
Aerospace — Airframe ball bearings, single-row, rigid, sealed, torque tube design, extra-light duty — Inch series |
|
Withdrawn |
1998-05 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 14213:1998 |
Aerospace — Airframe ball bearings, single-row, rigid, precision, sealed, torque tube design, extra-light duty — Inch series |
|
Withdrawn |
1998-05 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 14214:1998 |
Aerospace — Airframe ball bearings, double-row, rigid, sealed, heavy duty — Inch series |
|
Withdrawn |
1998-05 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 14215:1998 |
Aerospace — Airframe ball bearings, double-row, rigid, precision, sealed, heavy duty — Inch series |
|
Withdrawn |
1998-05 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.035
Components for aerospace construction
|
| ISO 3324-1:2013 |
Aircraft tyres and rims — Part 1: Specifications |
ISO 3324-1:2013 gives specifications for new and retread aircraft tyres and rims.
|
Withdrawn |
2013-07 |
Edition : 5 |
Number of pages : 30 |
Technical Committee |
83.160.20
Aircraft tyres
|
| ISO 3324-2:1979 |
Aircraft tyres and rims — Part 2: Test methods for tyres |
|
Withdrawn |
1979-05 |
Edition : 1 |
Number of pages : 11 |
Technical Committee |
83.160.20
Aircraft tyres
|
| ISO 3324-2:1998 |
Aircraft tyres and rims — Part 2: Test methods for tyres |
|
Withdrawn |
1998-02 |
Edition : 2 |
Number of pages : 14 |
Technical Committee |
83.160.20
Aircraft tyres
|
| ISO 3324-2:2013 |
Aircraft tyres and rims — Part 2: Test methods for tyres |
ISO 3324-2:2013 specifies test methods for new and retreaded aircraft tyres in the following categories:
a) low-speed tyres: for ground speeds up to and including 104 kn (120 mile/h);
b) high-speed tyres: for ground speeds above 104 kn (120 mile/h).
|
Withdrawn |
2013-07 |
Edition : 3 |
Number of pages : 15 |
Technical Committee |
83.160.20
Aircraft tyres
|
| ISO 7295:1982 |
Tyre valves — Aircraft — Interchangeability dimensions |
|
Withdrawn |
1982-11 |
Edition : 1 |
Number of pages : 8 |
Technical Committee |
83.160.20
Aircraft tyres
|
| ISO 7295:1988 |
Tyre valves for aircraft — Interchangeability dimensions |
|
Published |
1988-04 |
Edition : 2 |
Number of pages : 8 |
Technical Committee |
83.160.20
Aircraft tyres
|
| ISO 7295:1988/Amd 1:2014 |
Tyre valves for aircraft — Interchangeability dimensions — Amendment 1 |
|
Published |
2014-03 |
Edition : 2 |
Number of pages : 1 |
Technical Committee |
83.160.20
Aircraft tyres
|
| ISO 9475:1994 |
Aircraft inner tube and tubeless tyre valves — Cores and caps — Test methods |
Specifies the test methods used for valve cores and caps for aircraft tyres, with or without inner tubes, and minimum airtightness standards. Constitutes a detailed method allowing products to be evaluated on the same basis, and results to be compared.
|
Published |
1994-12 |
Edition : 1 |
Number of pages : 5 |
Technical Committee |
83.160.20
Aircraft tyres
|
| ISO 8074:1985 |
Aerospace — Surface treatment of austenitic stainless steel parts |
Gives the requirements to be met. Provides practical methods for removing contaminants and for obtaining suitable corrosion resistance. The surface treatments required during manufacture are mandatory for all surfaces. The final surface treatments are mandatory except when a surface coating is specified.
|
Published |
1985-08 |
Edition : 1 |
Number of pages : 5 |
Technical Committee |
49.040
Coatings and related processes used in aerospace industry
|
| ISO 8075:1985 |
Aerospace — Surface treatment of hardenable stainless steel parts |
Specifies the requirements for parts made from martensitic, precipitation hardening and maraging stainless steels. Provides practical methods for removing contaminants and for obtaining suitable corrosion resistance for aerospace applications. The final surface treatments are mandatory except when a surface coating is specified.
|
Published |
1985-08 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.040
Coatings and related processes used in aerospace industry
|
| ISO 8076:1984 |
Aerospace process — Anodic treatment of aluminium alloys — Chromic acid process 40 V DC, undyed coating |
Gives requirements for producing and testing. Sealed anodic coatings are applied to improve resistance to corrosion and as a pretreatment for painting. Unsealed anodic coatings provide a suitable surface for the application of structural adhesives and allow increased durability for paints. Gives information on technical requirements, quality assurance provisions, packaging and delivery.
|
Withdrawn |
1984-10 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.040
Coatings and related processes used in aerospace industry
|
| ISO 8077:1984 |
Aerospace process — Anodic treatment of aluminium alloys — Chromic acid process 20 V DC, undyed coating |
Includes requirements for producing and testing. Sealed anodic coatings are applied to improve resistance to corrosion and as a pretreatment for painting. Unsealed anodic coatings provide a suitable surface for the application of structural adhesives and allow increased durability for paints. Gives information on technical requirements, quality assurance provisions, packaging and delivery.
|
Withdrawn |
1984-10 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.040
Coatings and related processes used in aerospace industry
|
| ISO 8078:1984 |
Aerospace process — Anodic treatment of aluminium alloys — Sulfuric acid process, undyed coating |
Specifies requirements for producing and testing a coating on aluminium alloys. The anodizing process is applied in the manufacture of aerospace products to improve paint adhesion and resistance to corrosion. Gives technical requirements, quality assurance provisions, packaging and delivery.
|
Published |
1984-10 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.040
Coatings and related processes used in aerospace industry
|
| ISO 8079:1984 |
Aerospace process — Anodic treatment of aluminium alloys — Sulfuric acid process, dyed coating |
Includes requirements for producing and testing a coating on aluminium alloys where the coating is not required to withstand prolonged exposure to weathering and direct sunlight. The anodizing process is applied in the manufacture of aerospace products to improve resistance to corrosion, produce coloured surfaces for aesthetic reasons or to colour code parts for identification purposes.
|
Published |
1984-10 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.040
Coatings and related processes used in aerospace industry
|
| ISO 8080:1985 |
Aerospace — Anodic treatment of titanium and titanium alloys — Sulfuric acid process |
Specifies the requirements for producing and testing. The coating is used with solid film lubricants for protection of titanium fasteners against galling, for limited protection of less noble metals against galvanic corrosion when in contact with titanium or for other approved uses. Gives information on technical requirements, quality assurance provisions, packaging and delivery.
|
Withdrawn |
1985-05 |
Edition : 1 |
Number of pages : 2 |
Technical Committee |
49.040
Coatings and related processes used in aerospace industry
|
| ISO 8080:2021 |
Aerospace — Anodic treatment of titanium and titanium alloys — Sulfuric acid process |
This document specifies the requirements for producing and testing an unsealed anodic coating on titanium and titanium alloys. The anodic coating is produced by the sulfuric acid process.
The coating is used with solid film lubricants for protection of titanium fasteners against galling, for limited protection of less noble metals against galvanic corrosion when in contact with titanium or for other approved uses.
|
Published |
2021-05 |
Edition : 2 |
Number of pages : 3 |
Technical Committee |
49.040
Coatings and related processes used in aerospace industry
|
| ISO 8081:1985 |
Aerospace process — Chemical conversion coating for aluminium alloys — General purpose |
Describes the requirements for producing and testing. The coating specified is used in the manufacture of aerospace products in order to improve paint adhesion and resistance to corrosion. This process may also be used for touch-up of anodic coatings. Gives information on technical requirements, quality assurance provisions, packaging and delivery.
|
Withdrawn |
1985-02 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.040
Coatings and related processes used in aerospace industry
|
| ISO 8081:2021 |
Aerospace process — Chemical conversion coating for aluminium alloys — General purpose |
This document specifies the requirements for producing and testing a general purpose chemical conversion coating on aluminium alloys.
The chemical conversion coating is used in the manufacture of aerospace products in order to improve paint adhesion and resistance to corrosion.
This process can also be used for touch-up of anodic coatings.
|
Published |
2021-05 |
Edition : 2 |
Number of pages : 6 |
Technical Committee |
49.040
Coatings and related processes used in aerospace industry
|
| ISO 5843-10:1988 |
Aerospace — List of equivalent terms — Part 10: Aircraft structure |
Includes a list of terms in English, French, Russian and German. The list is given in English in alphabetical order. This list is the tenth part of equivalent terms used in the field of aerospace construction.
|
Published |
1988-10 |
Edition : 1 |
Number of pages : 26 |
Technical Committee |
49.045
Structure and structure elements
;
01.040.49
Aircraft and space vehicle engineering (Vocabularies)
|
| ISO 10046:1996 |
Aircraft — Methodology of calculating cargo compartment volumes |
Covers the methodology of calculating for the determination of the internal volumes of both the main deck and the lower deck aircraft cargo compartments. The minimum required clearance between the compartment envelope and the unit load devices (ULDs) is also stated in order to provide the maximum ULD external contour and the methodology to define the ULD internal volumes.
|
Published |
1996-12 |
Edition : 1 |
Number of pages : 7 |
Technical Committee |
49.045
Structure and structure elements
|
| ISO 45:1980 |
Aircraft — Pressure refuelling connections |
|
Withdrawn |
1980-05 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.050
Aerospace engines and propulsion systems
;
49.100
Ground service and maintenance equipment
|
| ISO 45:1990 |
Aircraft — Pressure refuelling connections |
Specifies the basic dimensions and access clearance. The basic dimensions shall be as specified in figure 1. The clearance allowed around the connector shall be in accordance with figure 2.
|
Published |
1990-12 |
Edition : 2 |
Number of pages : 4 |
Technical Committee |
49.050
Aerospace engines and propulsion systems
;
49.080
Aerospace fluid systems and components
;
49.100
Ground service and maintenance equipment
|
| ISO 493:1975 |
Aircraft — Dimensions for single-hole mounting (Class 1 and Class 2) lever-operated manual switches |
Gives the overall dimensions for switches having the characteristics specified in ISO 1466. The overall dimensions shall be accordance with those shown in figure 1 and the table, which are suitable for accomodating either terminal screws or integrated terminal on the face opposite the mounting bush. The holes in the mounting panel shall be as shown in figure 1a).
|
Published |
1975-05 |
Edition : 1 |
Number of pages : 1 |
Technical Committee |
49.060
Aerospace electric equipment and systems
|
| ISO 482:1977 |
Aircraft — Propulsion units and components — Methods of numbering and describing direction of rotation |
Specifies the methods of numbering aircraft engines, engine cylinders and combustion chambers, on drawings, for example, and the methods of describing the direction of rotation of main shafts and rotors and or propellers. The numbering of engines is given for horizontal thrust engines, vertical thrust engines and take-off booster engines. The numbering of cylinders in piston engines is given for in-line piston engines and radial piston engines. Furthermore the numbering of components in turbine engines and in rotorcraft engines is given.
|
Withdrawn |
1977-02 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.050
Aerospace engines and propulsion systems
|
| ISO 4153:1981 |
Aircraft — Pressure fuel dispensing system — Test procedure and limit value for shut-off surge pressure |
Includes a standard method for testing. The method specified and the limit value apply to all ground systems, fixed and mobile. Also, because these both are standardized, necessary knowledge is provided for aiding proper design of the aircraft fill control valve shut-off characteristics.
|
Published |
1981-11 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.050
Aerospace engines and propulsion systems
;
49.100
Ground service and maintenance equipment
|
| ISO 44:1975 |
Aerospace — Lever-operated, two-position, ON/OFF switches — Directions of operation |
Applies primarily to installations on the flight deck. The switches shall be mounted so that the operational direction is as specified in the table. Typical examples are demonstrated in the figure.
|
Withdrawn |
1975-04 |
Edition : 1 |
Number of pages : 1 |
Technical Committee |
49.060
Aerospace electric equipment and systems
|
| ISO/R 47:1957 |
Withdrawal of ISO/R 47-1957 |
|
Withdrawn |
1957-07 |
Edition : 1 |
Number of pages : 2 |
Technical Committee |
49.060
Aerospace electric equipment and systems
|
| ISO/R 222:1968 |
Withdrawal of ISO/R 222-1961 |
|
Withdrawn |
1968-12 |
Edition : 1 |
Number of pages : 2 |
Technical Committee |
49.060
Aerospace electric equipment and systems
|
| ISO 223:1975 |
Withdrawal of ISO 223-1975 |
|
Withdrawn |
1975-03 |
Edition : 1 |
Number of pages : 2 |
Technical Committee |
49.060
Aerospace electric equipment and systems
|