49.080 – Aerospace fluid systems and components – PDF Standards Store ?u= Wed, 06 Nov 2024 00:31:49 +0000 en-US hourly 1 https://wordpress.org/?v=6.7.1 ?u=/wp-content/uploads/2024/11/cropped-icon-150x150.png 49.080 – Aerospace fluid systems and components – PDF Standards Store ?u= 32 32 ISO 9940:2015 ?u=/product/publishers/iso/iso-99402015/ Wed, 06 Nov 2024 00:31:49 +0000 Aerospace series — Fluid, hydraulic, phosphate ester-base, fire resistant — Technical specification
Published By Publication Date Number of Pages
ISO 2015-08 36
]]> 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.

]]> ISO 9939:1994 ?u=/product/publishers/iso/iso-99391994/ Wed, 06 Nov 2024 00:31:48 +0000 Aerospace — Pressure re-oiling connection (new type)
Published By Publication Date Number of Pages
ISO 1994-01 6
]]> 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.

]]> ISO 9938:2022 ?u=/product/publishers/iso/iso-99382022/ Wed, 06 Nov 2024 00:31:48 +0000 Aerospace - Polytetrafluoroethylene (PTFE) hose assemblies, classification 204 °C/28 000 kPa - Procurement specification
Published By Publication Date Number of Pages
ISO 2022-01 24
]]> 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.

]]> ISO 9938:1994 ?u=/product/publishers/iso/iso-99381994/ Wed, 06 Nov 2024 00:31:47 +0000 Aerospace — Polytetrafluoroethylene (PTFE) hose assemblies, classification 204 degrees C/28 000 kPa — Procurement specification
Published By Publication Date Number of Pages
ISO 1994-12 18
]]> 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.

]]> ISO 9679:2006 ?u=/product/publishers/iso/iso-96792006/ Wed, 06 Nov 2024 00:28:52 +0000 Aerospace — Clamps for fluid systems — Test methods
Published By Publication Date Number of Pages
ISO 2006-08 12
]]> 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.

]]> ISO 9634:1994 ?u=/product/publishers/iso/iso-96341994/ Wed, 06 Nov 2024 00:28:20 +0000 Aerospace — Fluid systems — Dimensions of plastic protective caps and plugs
Published By Publication Date Number of Pages
ISO 1994-10 12
]]> 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.

]]> ISO 9538:1996 ?u=/product/publishers/iso/iso-95381996/ Wed, 06 Nov 2024 00:27:28 +0000 Aerospace — Hydraulic tubing joints and fittings — Planar flexure test
Published By Publication Date Number of Pages
ISO 1996-01 12
]]> 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.

]]> ISO 9538:2017 ?u=/product/publishers/iso/iso-95382017/ Wed, 06 Nov 2024 00:27:28 +0000 Aerospace series — Hydraulic tubing joints and fittings — Planar flexure test
Published By Publication Date Number of Pages
ISO 2017-04 14
]]> 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.

]]> ISO 9528:2022 ?u=/product/publishers/iso/iso-95282022/ Wed, 06 Nov 2024 00:27:27 +0000 Aerospace - Standard-weight polytetrafluoroethylene (PTFE) hose assemblies, classification 204 °C/21 000 kPa - Procurement specification
Published By Publication Date Number of Pages
ISO 2022-01 24
]]> 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.

]]> ISO 9528:1994 ?u=/product/publishers/iso/iso-95281994/ Wed, 06 Nov 2024 00:27:26 +0000 Aerospace — Standard-weight polytetrafluoroethylene (PTFE) hose assemblies, classification 204 degrees C/21 000 kPa — Procurement specification
Published By Publication Date Number of Pages
ISO 1994-12 20
]]> 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.

]]>