| Name |
Description |
Abstract |
Status |
Publication date |
Edition |
Number of pages |
Technical committee |
ICS |
| ISO 1023:1974 |
Aircraft — High pressure air charging valves |
Includes the coupling dimensions and access clearance. The basic dimensions of the valve and the access clearance to be provided shall conform to the requirements of figure 1. The valves shall be provided at the coupling end with a srew thread conforming to the requirements of figure 2. The valves are given in tables.
|
Withdrawn |
1974-07 |
Edition : 1 |
Number of pages : 2 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
49.100
Ground service and maintenance equipment
|
| ISO 1034:1973 |
Aircraft — Ground air-conditioning connections |
Gives the requirements for 127 mm and 203 mm connections for the purpose of air-conditioning from ground sources. The conncetions shall comply with the basic dimensional requirements shown in either figure 1 or figure 2 as appropriate. The ground unit must not project more than 14,O mm beyond the sealing plane except through defined openings.
|
Published |
1973-06 |
Edition : 1 |
Number of pages : 2 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
49.100
Ground service and maintenance equipment
|
| ISO 1465:1976 |
Aircraft — Liquid oxygen replenishment couplings — Mating dimensions |
|
Withdrawn |
1976-06 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
49.100
Ground service and maintenance equipment
|
| ISO 1465:1989 |
Aircraft — Liquid oxygen replenishment couplings — Mating dimensions |
Specifies the mating and clearance dimensions. The mating dimensions and characteristics of the ground half shall conform to those in figure 1 and table 1. The aircraft half shall mate with the ground half. The clearance envelope in the aircraft to accommodate the ground half for the purposes of coupling and uncoupling the hose unit shall be in accordance with figure 2 and table 2.
|
Published |
1989-09 |
Edition : 2 |
Number of pages : 3 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
49.100
Ground service and maintenance equipment
|
| ISO 1749:1973 |
Aircraft — Elastomeric sealing rings — Packaging and identification |
Specifies the requirements. It is essential that these rings be individually enclosed in sealed envelopes or in pockets in a multiple envelope provided that they can be removed without affecting the sealing of the remainder of the components in the package. The marking of package shall include the part number, material specification number, quarter and year of cure, compound number, acceptance batch number and manufacturer's identity.
|
Withdrawn |
1973-06 |
Edition : 1 |
Number of pages : 1 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
83.140.50
Seals
|
| ISO 2026:1974 |
Aircraft — Connections for starting engines by air |
Specifies the dimensions which are necessary to ensure international interchangeability of connectors with adaptors. Also gives the minimum clearances required on the aircraft to provide adequate access for the ground adaptor. The basic dimensions and tolerances for connections on aircraft and the minimum clearances around the connector, on the aircraft, are given in figure 1 and table 1 and figure 2 and table 2, respectively.
|
Withdrawn |
1974-11 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
49.100
Ground service and maintenance equipment
|
| ISO 2026:2020 |
Aircraft — Connections for starting engines by air |
This document specifies the dimensions of connections for starting aircraft engines by air, which are necessary to ensure international interchangeability of connectors with adaptors. lt also gives the minimum clearances required on the aircraft to provide adequate access for the ground adaptor.
|
Published |
2020-06 |
Edition : 2 |
Number of pages : 5 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
49.100
Ground service and maintenance equipment
|
| ISO 2563:1974 |
Aircraft ducting and piping — Profile dimensions for flanges of V-band couplings |
The profile dimensions of a mating pair of flanges shall comply with the figure given.
|
Withdrawn |
1974-11 |
Edition : 1 |
Number of pages : 1 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 2563:2009 |
Aircraft ducting and piping — Profile dimensions for flanges of V-band couplings |
ISO 2563:2009 gives the profile dimensions of V-band couplings, and the associated inch-based aircraft ducting and piping for the following external flange profiles:
lightweight solid profile;
medium-weight solid profile;
heavyweight solid profile;
narrow sheet metal profile;
wide sheet metal profile;
wide solid profile;
wide sheet metal to solid profile.
|
Published |
2009-09 |
Edition : 2 |
Number of pages : 9 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 2964:1974 |
Aircraft — Tubing outside diameters and thicknesses — Metric dimensions |
|
Withdrawn |
1974-02 |
Edition : 1 |
Number of pages : 2 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 2964:1985 |
Aerospace — Tubing — Outside diameters and thicknesses — Metric dimensions |
Includes the external diameters and thicknesses of tubes, for all metallic materials, to be selected for all uses in aircraft structural and system design. They shall be selected from those specified in the table. The tolerances shall be specified in the relevant standard appropriate to the material and intended application.
|
Published |
1985-04 |
Edition : 2 |
Number of pages : 2 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO/CD 2964 |
Aerospace — Tubing — Outside diameters and thicknesses — Metric dimensions |
Includes the external diameters and thicknesses of tubes, for all metallic materials, to be selected for all uses in aircraft structural and system design. They shall be selected from those specified in the table. The tolerances shall be specified in the relevant standard appropriate to the material and intended application.
|
Under development |
|
Edition : 3 |
|
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 3174:1981 |
Aircraft — Connections for checking hydraulic systems by ground appliances |
|
Withdrawn |
1981-10 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
49.100
Ground service and maintenance equipment
|
| ISO 3174:1994 |
Aircraft — Connections for checking hydraulic systems by ground appliances — Threaded type |
Cancels and replaces the first edition (1981). Specifies the requirements for connections installed in aircraft hydraulic system pressure and suction lines, intended for checking the systems by means of ground appliances.
|
Published |
1994-12 |
Edition : 2 |
Number of pages : 9 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
49.100
Ground service and maintenance equipment
|
| ISO 3323:1976 |
Aircraft — Hydraulic components — Marking to indicate fluid for which component is approved |
|
Withdrawn |
1976-09 |
Edition : 1 |
Number of pages : 2 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 3323:1987 |
Aircraft — Hydraulic components — Marking to indicate fluid for which component is approved |
Establishes a scheme for the marking, so that the correct type of fluid is readily apparent during any assembly or testing operations in workshops. The marking is not intended to serve any purpose when a component is installed in an aircraft. Describes the scheme, materials, design and manufacture and gives preferred dimensions of identifications plates.
|
Published |
1987-07 |
Edition : 2 |
Number of pages : 2 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO/FDIS 3323 |
Aircraft — Hydraulic components — Marking to indicate fluid for which component is approved |
|
Under development |
|
Edition : 3 |
Number of pages : 4 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 5859:1991 |
Aerospace — Graphic symbols for schematic drawings of hydraulic and pneumatic systems and components |
The requirements for the symbols are specified in SAE AS 1290A which is adopted as a de facto ISO International Standard. For the purposes of international standardization, the amendments listed in table 1 shall apply to the specific clauses of AS 1290A noted under "Reference".
|
Withdrawn |
1991-08 |
Edition : 1 |
Number of pages : 2 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
01.080.30
Graphical symbols for use on mechanical engineering and construction drawings, diagrams, plans, maps and in relevant technical product documentation
|
| ISO 5859:2014 |
Aerospace series — Graphic symbols for schematic drawings of hydraulic and pneumatic systems and components |
ISO 5859:2014 establishes a system of graphic symbols of hydraulic and pneumatic circuits and components for all types of aerospace systems.
|
Published |
2014-03 |
Edition : 2 |
Number of pages : 1 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
01.080.30
Graphical symbols for use on mechanical engineering and construction drawings, diagrams, plans, maps and in relevant technical product documentation
|
| ISO 7169:1993 |
Aerospace fluid systems — Separable tube fittings for 24 degrees cone — General specification |
|
Withdrawn |
1993-05 |
Edition : 2 |
Number of pages : 13 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO/FDIS 5859 |
Aerospace series — Graphic symbols for schematic drawings of hydraulic and pneumatic systems and components |
ISO 5859:2014 establishes a system of graphic symbols of hydraulic and pneumatic circuits and components for all types of aerospace systems.
|
Under development |
|
Edition : 3 |
|
Technical Committee |
49.080
Aerospace fluid systems and components
;
01.080.30
Graphical symbols for use on mechanical engineering and construction drawings, diagrams, plans, maps and in relevant technical product documentation
|
| ISO 5884:1987 |
Aerospace — Fluid systems and components — Methods for system sampling and measuring the solid particle contamination of hydraulic fluids |
Specifies procedures for determining the level of contamination. Three procedures are specified herein: microscopic method, automatic particle counting method and gravimetric method. In addition lays down the procedures for cleaning the apparatus and sample bottles, and specifies the solvents to be applied and how these solvents shall be prepared. Requirements as to the selection of the sampling point and to different sampling methods are also specified.
|
Withdrawn |
1987-08 |
Edition : 1 |
Number of pages : 14 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 5884:2018 |
Aerospace series — Fluid systems and components — Methods for system sampling and measuring the solid particle contamination in hydraulic fluids |
This document specifies best practice for sampling hydraulic fluid from aircraft hydraulic systems and other hydraulic systems associated with aerospace purposes.
|
Published |
2018-08 |
Edition : 2 |
Number of pages : 13 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 5887:1981 |
Aircraft — Joints for connecting crew members' regulator masks to oxygen sources |
Gives joint lock dimensions for connecting these masks to sources in aircraft and helicopters. Joint dimensions standardization provides interchangeability with masks of various types. The basic dimensions and tolerances are shown in figures 1 and 2. Dimensions without tolerances can correspond to national standards. The lock halves shall be installed as shown in figures 1 and 2.
|
Withdrawn |
1981-09 |
Edition : 1 |
Number of pages : 2 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 6771:1981 |
Aerospace construction — Fluid systems and components — Pressure and temperature classifications |
|
Withdrawn |
1981-07 |
Edition : 1 |
Number of pages : 1 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 6771:1987 |
Aerospace — Fluid systems and components — Pressure and temperature classifications |
Establishes the temperature types and pressure classes that are commonly used. System operating temperature ranges shall be classified as given in table 1. Nominal pressures shall be classified as given in table 2. The operating pressures listed are selected from ISO 2944 as far as practical.
|
Withdrawn |
1987-09 |
Edition : 2 |
Number of pages : 1 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 6771:2007 |
Aerospace — Fluid systems and components — Pressure and temperature classifications |
ISO 6771:2007 specifies the pressure classes and temperature types for the basic systems and component systems that are commonly used in aerospace fluid systems. Classes and types in the lower ranges represent systems in common use. Those in the higher ranges represent systems that are in less common use or that are used in developmental systems.
|
Published |
2007-08 |
Edition : 3 |
Number of pages : 4 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 6772:1981 |
Aerospace fluid systems — Impulse testing of hydraulic hose, tubing and fittings assemblies |
|
Withdrawn |
1981-12 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 6772:1988 |
Aerospace — Fluid systems — Impulse testing of hydraulic hose, tubing and fitting assemblies |
Specifies the requirements and the procedures. Requirements may apply, when appropriate, to components used in other areospace fluid systems. Against the first edition some technical details are revised. Includes the requirements for shape of impulse trace, rate of pressure rise, preparation of specimens, test fluid, principle of test, test method and intended use.
|
Withdrawn |
1988-10 |
Edition : 2 |
Number of pages : 3 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
83.140.40
Hoses
|
| ISO 6772:2012 |
Aerospace — Fluid systems — Impulse testing of hydraulic hose, tubing and fitting assemblies |
This International Standard specifies the requirements and the procedures for impulse testing of hose, tubing, and fitting assemblies for use in aerospace hydraulic systems. Requirements may apply, when appropriate, to components used in other aerospace fluid systems.
|
Published |
2012-10 |
Edition : 3 |
Number of pages : 6 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
83.140.40
Hoses
|
| ISO 6773:1982 |
Aerospace fluid systems — Thermal shock testing of piping and fittings |
|
Withdrawn |
1982-03 |
Edition : 1 |
Number of pages : 2 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 7169:2007 |
Aerospace — Separable tube fittings for fluid systems, for 24 degree cones, for pressures up to 3 000 psi or 21 000 kPa — Procurement specification, inch/metric |
ISO 7169:2007 specifies performance and quality requirements for the qualification and manufacture of standard 24° cone fittings and manufacture of 24° cone fittings to ensure reliable performance or equivalent inch-dimensioned fitting ends to ensure reliable performance in aircraft hydraulic systems.
ISO 7169:2007 specifies baseline criteria for the design and manufacture of system fittings that are qualification-tested on engines.
ISO 7169:2007 covers fittings of the temperature types and pressure classes specified in ISO 6771:1987.
|
Withdrawn |
2007-02 |
Edition : 4 |
Number of pages : 20 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 7169:2014 |
Aerospace — Separable tube fittings for fluid systems, for 24 degree cones, for pressures up to 3 000 psi or 21 000 kPa — Procurement specification, inch/metric |
ISO 7169:2014 specifies performance and quality requirements for the qualification and manufacture of standard 24° cone fittings and manufacture of 24° cone fittings to ensure reliable performance or equivalent inch-dimensioned fitting ends to ensure reliable performance in aircraft hydraulic systems.
This International Standard specifies baseline criteria for the design and manufacture of system fittings that are qualification-tested on engines.
This International Standard covers fittings of the temperature types and pressure classes specified in ISO 6771.
|
Published |
2014-11 |
Edition : 5 |
Number of pages : 20 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 7257:1983 |
Aircraft — Hydraulic tubing joints and fittings — Rotary flexure test |
Specifies procedures to determine and classify the fatigue strength of reconnectable or permanent hydraulic tube joints. The procedure is intended for conducting flexure tests of these parts with high strength tubes of various alloys such as corrosion resistant steel, Nimonic, titanium and aluminium alloy tube for use on commercial and military aircraft.
|
Withdrawn |
1983-07 |
Edition : 1 |
Number of pages : 9 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 7257:2016 |
Aircraft — Hydraulic tubing joints and fittings — Rotary flexure test |
ISO 7257:2016 specifies a flexure test procedure to determine and classify the fatigue strengths of reconnectable or permanent hydraulic tube joints.
The procedure is intended for conducting flexure tests of fittings and joints with high-strength hydraulic tubes of various alloys such as corrosion resistant steel, Nimonic?[1], titanium and aluminium alloy hydraulic tube for use on commercial and military aircraft.
A mean stress is applied by holding system pressure in the specimens and then flexing in a rotary bending test machine.
[1] Nimonic? is the trademark of a product supplied by Special Metals Corporation. This information is given for the convenience of users of this document and does not constitute an endorsement by ISO of the product named. Equivalent products can be used if they can be shown to lead to the same results.
|
Published |
2016-06 |
Edition : 2 |
Number of pages : 12 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 7258:1984 |
Polytetrafluoroethylene (PTFE) tubing for aerospace applications — Methods for the determination of the density and relative density |
Specifies three methods: Method A - density gradient column method without a preconditioning heating and cooling cycle; method B - displacement of water and determination of change of weight method; method C - density gradient column method with a preconditioning heating and cooling cycle.
|
Published |
1984-06 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
83.140.40
Hoses
|
| ISO 7313:1984 |
Aircraft — High temperature convoluted hose assemblies in polytetrafluoroethylene (PTFE) |
Gives characteristics of these assemblies for use in aircraft fluid systems at temperatures between -55 and +200 °C and at nominal pressures, depending on bore size, up to 6,8 MPa. Special approval from the proper national authority may be required it these hoses are to be part of a pressurized gas storage system. Two types of hose assembly are covered: Typ 1 - non-conductive inner tube and type 2 - conductive inner tube.
|
Withdrawn |
1984-03 |
Edition : 1 |
Number of pages : 8 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
83.140.40
Hoses
|
| ISO 7313:2020 |
Aircraft — High temperature convoluted hose assemblies in polytetrafluoroethylene (PTFE) |
This document specifies characteristics of hose assemblies with corrosion‑resistant metallic braid and convoluted polytetrafluoroethylene (PTFE) inner tube for use in aircraft fluid systems at temperatures between ‑55 °C and +200 °C and at nominal pressures, depending on bore size, up to 6,8 MPa. Special approval from the proper national authority can be required if these hoses are to be part of a pressurized gas storage system.
Two types of hose assembly are covered in this document:
— Type 1: Non‑conductive inner tube; and
— Type 2: Conductive inner tube.
|
Published |
2020-03 |
Edition : 2 |
Number of pages : 14 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
83.140.40
Hoses
|
| ISO 7314:1989 |
Aerospace — Fluid systems — Hose assembly, metal |
|
Withdrawn |
1989-11 |
Edition : 1 |
Number of pages : 12 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO/CD 7661 |
Aerospace — Fluid systems — Clamp blocks for tube lines having axial alignment — Design standard and qualification testing — Metric series |
|
Under development |
|
Edition : 2 |
|
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 7314:1994 |
Aerospace — Fluid systems — Hose assembly, metal |
Cancels and replaces the first edition (1989). Gives specifications for medium pressure, high temperature, flexible metal hose assemblies suitable for continuous operation in liquid and pneumatic systems from -55 °C to +400 °C, with short duration excursions up to +650 °C. Intended for use to convey air and gases in pneumatic systems, bleed air systems, heating and ventilating systems, and instrument air systems. Does not cover flow velocity in such assemblies exceeding 54 m/s.
|
Withdrawn |
1994-09 |
Edition : 2 |
Number of pages : 12 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 7314:2002 |
Aerospace — Fluid systems — Metal hose assemblies |
ISO 7314 gives specifications for medium pressure, high temperature, flexible metal hose assemblies suitable for continuous operation in liquid and pneumatic systems from - 55 °C to + 400 °C, with short duration excursions up to + 650 °C.
The hose assemblies covered by this International Standard are intended for use in aerospace applications for conveying air and other gases in pneumatic systems, bleed air systems, heating and ventilating systems and instrument air systems. ISO 7314 does not cover flow velocity in such assemblies exceeding 54 m/s; higher velocities require special vibration-dampening devices.
Hose assemblies supplied to the specifications laid down in this International Standard may be of two types:
Type 1: Convoluted inner tube - welded, of moderate mass and moderate flexibility.
Type 2: Convoluted inner tube - seamless or butt-welded and redrawn, of low mass and high flexibility.
|
Published |
2002-11 |
Edition : 3 |
Number of pages : 18 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 7315:1985 |
Aerospace — "P" clamps (loop clamps) for fluid tubing installations — Dimensions |
|
Withdrawn |
1985-11 |
Edition : 1 |
|
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 7315:1988 |
Aerospace — "P" clamps (loop clamps) for fluid systems — Envelope dimensions |
Specifies maximum and minimum dimensions for these clamps installed by means of a bolt with a nominal diameter of 5 mm. The specified dimensions define a dimensional envelope. Shall not be considered as an interchangeability standard. The tolerances for each type of clamp are to be defined in the parts standards drawings.
|
Published |
1988-02 |
Edition : 2 |
Number of pages : 3 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 7319:1982 |
Aerospace construction — Fluid systems — Interface of metric couplings |
|
Withdrawn |
1982-12 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 7319:1992 |
Aerospace — Fluid systems — Interface of 24 degree cone metric couplings |
Defines the geometry of the interface of couplings for fluid systems in aircrafts. Specifies the dimensions which allow the interchangeability of the male and female elements and of the nut used for the connection. The dimensions define the maximum volume of the male fitting.
|
Withdrawn |
1992-12 |
Edition : 2 |
Number of pages : 4 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 7319:2021 |
Aerospace — Fluid systems — Interface of 24° cone metric couplings |
This document defines the geometry of the interface of removable 24° cone couplings for fluid systems in aircraft. The connection with the pipe of each one of the connecting elements can be of different design.
This document specifies the dimensions which allow the interchangeability of the male and female elements and of the nut used for the connection.
The dimensions define the maximum volume of the male fitting.
|
Published |
2021-06 |
Edition : 3 |
Number of pages : 5 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 7320:1985 |
Aerospace — Fluid systems port connection, seal and fitting end — Dimensions |
|
Withdrawn |
1985-09 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 7320:1992 |
Aerospace — Couplings, threaded and sealed, for fluid systems — Dimensions |
Establishes a system for sealing the port connection of couplings. Specifies dimensions to achieve interchangeability of the port connection, the fitting end and a seal. The seal may be a standard O-ring or a special ring.
|
Withdrawn |
1992-12 |
Edition : 2 |
Number of pages : 7 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 7320:2021 |
Aerospace — Couplings, threaded and sealed, for fluid systems — Dimensions |
This document establishes a system for sealing the port connection of couplings used in the aerospace industry.
It specifies dimensions to achieve interchangeability of the port connection, the fitting end and a seal. The seal can be a standard O‑ring or a special ring.
|
Published |
2021-06 |
Edition : 3 |
Number of pages : 7 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 7661:1984 |
Aerospace — Fluid systems — Clamp blocks for tube lines having axial alignment — Design standard and qualification testing — Metric series |
Gives definitions for these clamps with or without electrical grounding, designed for a range of tube outside diameters from 4 to 32 mm selected from ISO 2964, and lays down the dimensions of clamp blocks and specifies the test methods for qualification testing. Furthermore gives classification and temperature conditions.
|
Published |
1984-12 |
Edition : 1 |
Number of pages : 8 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 8153-1:2009 |
Aerospace fluid systems and components — Vocabulary — Part 1: Hose assemblies |
ISO 8153-1:2009 defines terms used for all types of hose assemblies.
General terms can be made more precise through the addition of supplementary terminology relating to the design, range of application and/or the material of the hose/hose assembly.
Terms and definitions specific to metallic hose assemblies are given in ISO 7369.
|
Published |
2009-06 |
Edition : 1 |
Number of pages : 18 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
01.040.49
Aircraft and space vehicle engineering (Vocabularies)
;
01.040.83
Rubber and plastics industries (Vocabularies)
;
83.140.40
Hoses
|
| ISO 8153-2:2021 |
Aerospace fluid systems and components — Vocabulary — Part 2: Fittings and couplings |
This document defines terms which are used for all types of fittings and couplings.
NOTE - In addition to text written in the official ISO languages (English, French), this document gives text in German and Chinese. This text is published under the responsibility of the Member Body for Germany (DIN) and the Member Body for China (SAC) and is given for information only. Only the text given in the official languages can be considered as ISO text.
|
Published |
2021-09 |
Edition : 1 |
|
Technical Committee |
49.080
Aerospace fluid systems and components
;
01.040.49
Aircraft and space vehicle engineering (Vocabularies)
|
| ISO 8177:1985 |
Aerospace — Omega clamps (saddle clamps) for fluid tubing installations — Dimensions |
|
Withdrawn |
1985-11 |
Edition : 1 |
|
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 8177:1986 |
Aerospace — Omega clamps (saddle clamps) for fluid systems — Dimensions |
Includes maximum and minimum dimensions for clamps installed by means of two bolts with nominal diameters of 5 mm. The specified dimensions define a dimensional envelope. Shall not be considered as an interchangeability standard. The tolerances for each type of clamp are to be defined in the parts standards drawings. These clamps are intended for the installation, support and guiding of rigid tubing or hose assemblies.
|
Withdrawn |
1986-11 |
Edition : 2 |
Number of pages : 2 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 8177:2015 |
Aerospace — Omega clamps (saddle clamps) for fluid systems — Dimensions |
ISO 8177:2015 specifies maximum and minimum dimensions for omega clamps (saddle clamps) installed by means of two bolts with nominal diameters of 5 mm.
The specified dimensions define a dimensional envelope. This International Standard shall not be considered as an inter-changeability standard. The tolerances for each type of clamp are to be defined in the parts standards drawings.
|
Withdrawn |
2015-07 |
Edition : 3 |
Number of pages : 3 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 8177:2021 |
Aerospace — Omega clamps (saddle clamps) for fluid systems — Dimensions |
This document specifies maximum and minimum dimensions for omega clamps (saddle clamps) installed by means of two bolts with nominal diameters of 5 mm.
The specified dimensions define a dimensional envelope. This document is not an interchangeability standard. The tolerances for each type of clamp are defined in the drawings in the standards for parts.
|
Published |
2021-12 |
Edition : 4 |
Number of pages : 4 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 8278:1986 |
Aerospace — Hydraulic, pressure compensated, variable delivery pumps — General requirements |
Shall be used in conjunction with detail specifications concerning each pump model. Includes functional requirements, quality assurance provisions, qualification tests, acceptance tests, storage and packaging. A schematic summary is provided in the annex for easy reference to the contents of this International Standard.
|
Withdrawn |
1986-11 |
Edition : 1 |
Number of pages : 23 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 8278:2016 |
Aerospace series — Hydraulic, pressure compensated, variable delivery pumps — General requirements |
ISO 8278:2016 establishes the general requirements for pressure compensated, variable delivery hydraulic pumps, suitable for use in aircraft hydraulic systems at pressures up to 35 000 kPa (5 000 psi).
It is to be used in conjunction with detail specifications that is particular to each application.
|
Published |
2016-03 |
Edition : 2 |
Number of pages : 44 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 8479:1986 |
Aerospace — "Q" clamps (centre-mounted clamps) for fluid systems — Dimensions |
Gives maximum and minimum dimensions for clamps installed by means of a bolt with a nominal diameter of 5 mm. These clamps are intended for the installation, support and guiding of rigid tubing or hose assemblies. Clamps of sizes larger than DN 50 are not suitable for supporting tubing or hose assemblies; they may be used for other equipment, e. g. electrical cables or looms.
|
Published |
1986-12 |
Edition : 1 |
Number of pages : 2 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 12573:2010 |
Aircraft — Tubing tolerances — Inch series |
ISO 12573:2010 specifies the dimensional tolerances to be applied to round section inch series tubing used in aircraft.
|
Published |
2010-09 |
Edition : 1 |
Number of pages : 10 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 8574:1990 |
Aerospace — Hydraulic system tubing — Qualification tests |
Specifies flexure, pressure impulse and burst test procedures for determining and classifying the fatigue strengths for bent tubing. The procedures are intended for high and low pressure system tubing qualification purposes or for the evaluation of new materials. Describes test equipment, test specimens, stress determination, testing and requirements. Includes figures.
|
Withdrawn |
1990-11 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 8574:2004 |
Aerospace — Hydraulic system tubing — Qualification tests for bent tubes |
ISO 8574:2004 specifies pressure impulse and burst test procedures for determining and classifying the impulse fatigue strengths of bent tubes used in aerospace hydraulic systems. The procedures are intended for qualification purposes of high- and low-pressure system tubing or for the evaluation of new materials for hydraulic system tubing.
|
Published |
2004-05 |
Edition : 2 |
Number of pages : 5 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 8575:1990 |
Aerospace — Fluid systems — Hydraulic system tubing |
Gives the requirements relating to the sizes and material of tubing for use in hydraulic pressure and return systems. For pressure lines, the requirements apply to the pressure and temperature ranges covered by pressure classes D and E and temperature types II and III as specified in ISO 6771. Tubing materials are included in table 1, outside diameters, wall thicknesses and materials for hydraulic tubing pressure lines are given in table 2. Corresponding national standards for tubing materials are given in table A.1 of annex A.
|
Withdrawn |
1990-11 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 8575:2016 |
Aerospace — Fluid systems — Hydraulic system tubing |
ISO 8575:2016 provides information relating to the sizes and materials of tubing for use in aerospace hydraulic pressure and return and suction lines. For pressure lines, the requirements apply to the pressure and temperature ranges covered by pressure class D, E and J and temperature type 13 and type 20 as specified in ISO 6771.
|
Published |
2016-11 |
Edition : 2 |
Number of pages : 9 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO/DIS 8575 |
Aerospace series — Fluid systems — Hydraulic system tubing |
ISO 8575:2016 provides information relating to the sizes and materials of tubing for use in aerospace hydraulic pressure and return and suction lines. For pressure lines, the requirements apply to the pressure and temperature ranges covered by pressure class D, E and J and temperature type 13 and type 20 as specified in ISO 6771.
|
Under development |
|
Edition : 3 |
Number of pages : 9 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 8625-1:1993 |
Aerospace — Fluid systems — Vocabulary — Part 1: General terms and definitions related to pressure |
Gives 55 terms including their alphabetical index in English and French as well as a graphical presentation of an arbitrary pressure curve in annex A.
|
Withdrawn |
1993-01 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
01.040.49
Aircraft and space vehicle engineering (Vocabularies)
|
| ISO 8625-1:2018 |
Aerospace — Fluid systems — Vocabulary — Part 1: General terms and definitions related to pressure |
ISO 8625-1:2018 defines general terms relating to pressure in fluid systems used in aerospace construction.
|
Published |
2018-03 |
Edition : 2 |
Number of pages : 7 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
01.040.49
Aircraft and space vehicle engineering (Vocabularies)
|
| ISO 8625-2:1991 |
Aerospace — Fluid systems — Vocabulary — Part 2: General terms and definitions relating to flow |
Specifies 15 terms and definitions in English and French. Contains the alphabetical indexes in English and French.
|
Withdrawn |
1991-04 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
01.040.49
Aircraft and space vehicle engineering (Vocabularies)
|
| ISO 8625-2:2018 |
Aerospace — Fluid systems — Vocabulary — Part 2: General terms and definitions relating to flow |
ISO 8625-2:2018 defines general terms relating to flow in fluid systems used in aerospace construction.
|
Published |
2018-03 |
Edition : 2 |
Number of pages : 3 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
01.040.49
Aircraft and space vehicle engineering (Vocabularies)
|
| ISO 8625-3:1991 |
Aerospace — Fluid systems — Vocabulary — Part 3: General terms and definitions relating to temperature |
Specifies 18 terms and definitions in English and French. Contains the alphabetical indexes in English and French.
|
Withdrawn |
1991-04 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
01.040.49
Aircraft and space vehicle engineering (Vocabularies)
|
| ISO 8625-3:2018 |
Aerospace — Fluid systems — Vocabulary — Part 3: General terms and definitions relating to temperature |
ISO 8625-3:2018 defines general terms relating to temperature in fluid systems used in aerospace construction.
|
Published |
2018-03 |
Edition : 2 |
Number of pages : 3 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
01.040.49
Aircraft and space vehicle engineering (Vocabularies)
|
| ISO 8625-4:2011 |
Aerospace — Fluid systems — Vocabulary — Part 4: General terms and definitions relating to control/actuation systems |
ISO 8625-4:2011 defines general terms relating to control/actuation systems in the field of aerospace fluid systems and components.
|
Published |
2011-10 |
Edition : 1 |
Number of pages : 13 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
01.040.49
Aircraft and space vehicle engineering (Vocabularies)
|
| ISO 8775:1988 |
Aerospace — Gaseous oxygen replenishment connection for use in fluid systems (new type) — Dimensions (Inch series) |
Lays down the mating dimensions and access clearance for a replenishment coupling. Describes the requirements for the coupling mating dimensions, the thread and access clearance, which shall be in accordance with those given in figures and tables.
|
Published |
1988-02 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
49.100
Ground service and maintenance equipment
|
| ISO 8829-1:2009 |
Aerospace — Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies — Part 1: Metallic (stainless steel) braid |
ISO 8829-1:2009 specifies test methods for flexible polytetrafluoroethylene (PTFE) inner tubes with metallic (stainless steel) braided hose and hose assemblies used in aircraft fluid systems, in the pressure and temperature ranges covered by pressure classes and temperature types, as specified in ISO 6771.
If performance requirements are not defined in ISO 8829-1:2009, they are defined in the performance specification.
ISO 8829-1:2009 is applicable when reference is made to it in a procurement specification or other definition document.
|
Published |
2009-04 |
Edition : 1 |
Number of pages : 19 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
83.140.40
Hoses
|
| ISO 8829-2:2006 |
Aerospace — Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies — Part 2: Non-metallic braid |
ISO 8829-2:2006 specifies test methods for flexible polytetrafluoroethylene (PTFE) inner tubes with non-metallic braided hose and hose assemblies used in aircraft fluid systems, in the pressure and temperature ranges covered by pressure classes and temperature types, as specified in ISO 6771.
ISO 8829-2:2006 applies to the hose and the hose coupling. The tests and assembly requirements for the connecting end fittings are covered in the procurement specification.
ISO 8829-2:2006 is applicable when reference is made to it in a procurement specification or other definition document.
|
Published |
2006-09 |
Edition : 1 |
Number of pages : 21 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
83.140.40
Hoses
|
| ISO 8829:1990 |
Aerospace — Polytetrafluoroethylene (PTFE) hose assemblies — Test methods |
Specifies procedures for flexible hose and hose assemblies used in fluid systems in the pressure and temperature ranges covered by pressure classes B, D and E, and temperature types I, II and III as specified in ISO 6771. Applies to the hose and the hose coupling. The tests and assembly requirements for the connecting and fittings are covered in the procurement specification. Is applicable when reference is made to it in a procurement specification or other definition document.
|
Withdrawn |
1990-02 |
Edition : 1 |
Number of pages : 11 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
83.140.40
Hoses
|
| ISO 8913:1989 |
Aerospace — Lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 204 degrees C/21 000 kPa — Procurement specification |
|
Withdrawn |
1989-12 |
Edition : 1 |
Number of pages : 12 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
83.140
Rubber and plastics products
|
| ISO 8913:1989/Cor 1:1990 |
Aerospace — Lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 204 degrees C/21 000 kPa — Procurement specification — Technical Corrigendum 1 |
|
Withdrawn |
1990-09 |
Edition : 1 |
Number of pages : 2 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 8913:1994 |
Aerospace — Lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 204 degrees C/21 000 kPa — Procurement specification |
Cancels and replaces the first edition (1989). Specifies requirements for lightweight polytetrafluoroethylene hose assemblies for use in aircraft hydraulic systems at temperatures between -55 °C and +204 °C and at a nominal pressure up to 21 000 kPa. The hose assemblies are also suitable for use within the same temperature and pressure limitations in aircraft pneumatic systems where some gaseous diffusion through the wall of the PTFE liner may be tolerated. The use of these hose assemblies in high-pressure pneumatic storage systems is not recommended.
|
Withdrawn |
1994-12 |
Edition : 2 |
Number of pages : 15 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
83.140.40
Hoses
|
| ISO 8913:2006 |
Aerospace — Lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 400 degrees F/3 000 psi (204 degrees C/20 684 kPa) and 204 degrees C/21 000 kPa (400 degrees F/3 046 psi) — Procurement specification |
ISO 8913:2006 specifies requirements for lightweight polytetrafluoroethylene (PTFE) hose assemblies for use in aircraft hydraulic systems at temperatures between - 55 °C and 204 °C (- 65 °F and 400 °F), and at a nominal pressure up to 3 000 psi (20 684 kPa) or 21 000 kPa (3 046 psi). The hose assemblies are also suitable for use within the same temperature and pressure limitations in aircraft pneumatic systems where some gaseous diffusion through the wall on the PTFE liner may be tolerated.
The use of these hose assemblies in high-pressure pneumatic storage systems is not recommended. In addition, installations in which the limits specified in ISO 8913:2006 are exceeded, or in which the application is not covered specifically by ISO 8913:2006, for example for oxygen, are subject to the approval of the purchaser.
A listing of hose assembly procurement standards conforming to ISO 8913:2006 is given.
|
Published |
2006-11 |
Edition : 3 |
Number of pages : 27 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
83.140.40
Hoses
|
| ISO/CD 8913 |
Aerospace — Lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 400 degrees F/3 000 psi (204 degrees C/20 684 kPa) and 204 degrees C/21 000 kPa (400 degrees F/3 046 psi) — Procurement specification |
ISO 8913:2006 specifies requirements for lightweight polytetrafluoroethylene (PTFE) hose assemblies for use in aircraft hydraulic systems at temperatures between - 55 °C and 204 °C (- 65 °F and 400 °F), and at a nominal pressure up to 3 000 psi (20 684 kPa) or 21 000 kPa (3 046 psi). The hose assemblies are also suitable for use within the same temperature and pressure limitations in aircraft pneumatic systems where some gaseous diffusion through the wall on the PTFE liner may be tolerated.
The use of these hose assemblies in high-pressure pneumatic storage systems is not recommended. In addition, installations in which the limits specified in ISO 8913:2006 are exceeded, or in which the application is not covered specifically by ISO 8913:2006, for example for oxygen, are subject to the approval of the purchaser.
A listing of hose assembly procurement standards conforming to ISO 8913:2006 is given.
|
Under development |
|
Edition : 4 |
|
Technical Committee |
49.080
Aerospace fluid systems and components
;
83.140.40
Hoses
|
| ISO 9206:1990 |
Aerospace — Constant displacement hydraulic motors — General specifications |
Establishes informations for motors to be installed in aircraft, which transform hydraulic power into mechanical energy in the form of a rotational torque. Primary and secondary function motors are covered. Actuators with internal rotation angle limits and low-speed motors are not covered. Shall be used in conjunction with the detail specification particular to each application.
|
Withdrawn |
1990-02 |
Edition : 1 |
Number of pages : 18 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 9206:2016 |
Aerospace series — Constant displacement hydraulic motors — General specifications |
ISO 9206:2016 establishes the general requirements for constant displacement hydraulic motors, suitable for use in aircraft hydraulic systems at pressures up to 35 000 kPa (5 000 psi).
Primary and secondary function motors are covered in ISO 9206:2016; however, actuators with internal rotation angle limits and low-speed motors are not covered.
ISO 9206:2016 is to be used in conjunction with the detail specification that is particular to each application.
|
Withdrawn |
2016-03 |
Edition : 2 |
Number of pages : 34 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 9206:2018 |
Aerospace — Fixed displacement hydraulic motors — General specifications |
This document establishes the general requirements for constant displacement hydraulic motors, suitable for use in aircraft hydraulic systems at pressures up to 35 000 kPa (5 000 psi).
Primary and secondary function motors (see Clause 4) are covered in this document; however, actuators with internal rotation angle limits and low-speed motors are not covered.
This document is to be used in conjunction with the detail specification that is particular to each application.
|
Published |
2018-12 |
Edition : 3 |
Number of pages : 36 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 9528:1989 |
Aerospace — Standard-weight polytetrafluoroethylene (PTFE) hose assemblies, classification 204 degrees C/21 000 kPa — Procurement specification |
|
Withdrawn |
1989-12 |
Edition : 1 |
Number of pages : 12 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
83.140
Rubber and plastics products
|
| ISO 9528:1989/Cor 1:1990 |
Aerospace — Standard-weight polytetrafluoroethylene (PTFE) hose assemblies, classification 204 degrees C/21 000 kPa — Procurement specification — Technical Corrigendum 1 |
|
Withdrawn |
1990-09 |
Edition : 1 |
Number of pages : 2 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 9528:1994 |
Aerospace — Standard-weight polytetrafluoroethylene (PTFE) hose assemblies, classification 204 degrees C/21 000 kPa — Procurement specification |
Cancels and replaces the first edition (1989). Specifies requirements for standard-weight polytetrafluoroethylene hose assemblies for use in aircraft hydraulic systems at temperatures between -55 °C and +204 °C and at a nominal pressure up to 21 000 kPa. The hose assemblies are also suitable for use within the same temperature and pressure limitations in aircraft pneumatic systems where some gaseous diffusion through the wall of the PTFE liner may be tolerated. The use of these hose assemblies in high-pressure pneumatic storage systems is not recommended.
|
Withdrawn |
1994-12 |
Edition : 2 |
Number of pages : 14 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
83.140.40
Hoses
|
| ISO 9528:2022 |
Aerospace — Standard-weight polytetrafluoroethylene (PTFE) hose assemblies, classification 204 °C/21 000 kPa — Procurement specification |
This document specifies requirements for standard-weight polytetrafluoroethylene (PTFE) hose assemblies for use in aircraft hydraulic systems at temperatures between –55 °C and +204 °C and at a nominal pressure up to 21 000 kPa (210 bar). The hose assemblies are also suitable for use within the same temperature and pressure limitations in aircraft pneumatic systems where some gaseous diffusion through the wall of the PTFE liner can be tolerated.
|
Published |
2022-01 |
Edition : 3 |
Number of pages : 17 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
83.140.40
Hoses
|
| ISO 9538:1996 |
Aerospace — Hydraulic tubing joints and fittings — Planar flexure test |
Specifies a flexure test procedure for reconnectable and permanent hydraulik tube joints. This procedure is intended for conducting flexure tests on fittings with high-strength hydraulik tubes made of corrosion-resisting steel, nimonic, titanium and aluminium used on commercial and military aircraft.
|
Withdrawn |
1996-01 |
Edition : 1 |
Number of pages : 5 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 9538:2017 |
Aerospace series — Hydraulic tubing joints and fittings — Planar flexure test |
ISO 9538:2017 specifies a flexure test procedure for reconnectable and permanent hydraulic tube joints.
This procedure is intended for conducting flexure tests on fittings with high-strength hydraulic tubes made of corrosion-resisting steel, titanium and aluminium for use on commercial and military aircraft.
|
Published |
2017-04 |
Edition : 2 |
Number of pages : 6 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO/CD 9538 |
Aerospace series — Hydraulic tubing joints and fittings — Planar flexure test |
ISO 9538:2017 specifies a flexure test procedure for reconnectable and permanent hydraulic tube joints.
This procedure is intended for conducting flexure tests on fittings with high-strength hydraulic tubes made of corrosion-resisting steel, titanium and aluminium for use on commercial and military aircraft.
|
Under development |
|
Edition : 3 |
|
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 9634:1994 |
Aerospace — Fluid systems — Dimensions of plastic protective caps and plugs |
Defines the configuration and specifies the dimensions of various types of plastic caps and plugs used for the protection, during transit and storage, of openings in aerospace fluid system components.
|
Published |
1994-10 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 9679:2006 |
Aerospace — Clamps for fluid systems — Test methods |
ISO 9679:2006 specifies the test methods and procedures to be used for the qualification and comparison of support or retention devices used in the installation of aerospace fluid systems.
It is applicable when reference is made to parts standards, procurement specifications, or other definition documents.
|
Published |
2006-08 |
Edition : 1 |
Number of pages : 7 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 9938:1990 |
Aerospace — Polytetrafluoroethylene (PTFE) hose assemblies, classification 204 degrees C/28 000 kPa — Procurement specification |
|
Withdrawn |
1990-12 |
Edition : 1 |
Number of pages : 13 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
83.140
Rubber and plastics products
|
| ISO 9938:1994 |
Aerospace — Polytetrafluoroethylene (PTFE) hose assemblies, classification 204 degrees C/28 000 kPa — Procurement specification |
Cancels and replaces the first edition (1990). Specifies requirements for polytetrafluoroethylene hose assemblies for use in aircraft hydraulic systems at temperatures between -55 °C and +204 °C and at a nominal pressure up to 28 000 kPa. The hose assemblies are also suitable for use within the same temperature and pressure limitations in aircraft pneumatic systems where some gaseous diffusion through the wall of the PTFE liner may be tolerated. The use of these hose assemblies in high-pressure pneumatic storage systems is not recommended.
|
Withdrawn |
1994-12 |
Edition : 2 |
Number of pages : 14 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
83.140.40
Hoses
|
| ISO 9938:2022 |
Aerospace — Polytetrafluoroethylene (PTFE) hose assemblies, classification 204 °C/28 000 kPa — Procurement specification |
This document specifies requirements for polytetrafluoroethylene (PTFE) hose assemblies for use in aircraft hydraulic systems at temperatures between –55 °C and +204 °C and at a nominal pressure up to 28 000 kPa (280 bar). The hose assemblies are also suitable for use within the same temperature and pressure limitations in aircraft pneumatic systems where some gaseous diffusion through the wall of the PTFE liner may be tolerated.
|
Published |
2022-01 |
Edition : 3 |
Number of pages : 17 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
83.140.40
Hoses
|
| ISO 9939:1994 |
Aerospace — Pressure re-oiling connection (new type) |
Specifies the basic dimensions of a pressure re-oiling connection for use with all oils for aircraft engines, and the clearance envelope to be provided.
|
Published |
1994-01 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
49.100
Ground service and maintenance equipment
|
| ISO 9940:2015 |
Aerospace series — Fluid, hydraulic, phosphate ester-base, fire resistant — Technical specification |
ISO 9940:2015 defines technical requirements, qualification and quality control conditions (product qualification, batch control, acceptance) test and measurement methods to be used by manufacturers for qualification of fire-resistant phosphate-ester-base fluids used for hydraulic transmissions in aircrafts.
|
Published |
2015-08 |
Edition : 1 |
Number of pages : 28 |
Technical Committee |
49.080
Aerospace fluid systems and components
|
| ISO 10502:1992 |
Aerospace — Hose assemblies in polytetrafluoroethylene (PTFE) for use up to 232 degrees C and 10 500 kPa — Procurement specification |
Covers Class I fitting assemblies of corrosion-resistant steel or titanium parts (- 55 °C to + 232 °C) and Class II fitting assemblies of corrosion-resistant steel and aluminium parts, DN 12 and larger (- 55 °C to + 135 °C) for use in aircraft hydraulic, fuel and lubricating oil systems and in aerospace pneumatic systems where some gaseous diffusion through the wall may be tolerated. Annex A gives equivalent materials and components for information only.
|
Withdrawn |
1992-06 |
Edition : 1 |
Number of pages : 14 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
83.140.40
Hoses
|