Aerospace. Test Methods for Polytetraflouroethylene (PTFE) Inner-Tube Hose Assemblies. Metallic (Stainless Steel) Braid PDF Download
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Author: British Standards Institute Staff
Publisher:
ISBN: 9780580550645
Category :
Languages : en
Pages : 28
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Book Description
Aircraft components, Flexible pipes, Pipes, Plastics, Polytetrafluoroethylene, Fluid equipment components, Braid, Metals, Stainless steels, Mechanical testing, Pressure testing, Leak tests
Author: British Standards Institute Staff
Publisher:
ISBN: 9780580550645
Category :
Languages : en
Pages : 28
Get Book Here
Book Description
Aircraft components, Flexible pipes, Pipes, Plastics, Polytetrafluoroethylene, Fluid equipment components, Braid, Metals, Stainless steels, Mechanical testing, Pressure testing, Leak tests
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
This SAE Aerospace Standard (AS) describes the test methods for flexible PTFE hose and hose assemblies used in aircraft fluid systems in the pressure and temperature ranges defined in specific procurement specifications. It applies to the hose and the hose coupling. The tests and assembly requirements for the connecting end fitting are covered in the procurement specification.This document applies each time that it is referred to in a procurement specification or other definition document. This standard is being revised to reflect the current requirements as Section 3 - PTFE Inner Tube Test Methods, Section 4 - Metallic Braided Hose Assembly Test Methods, the addition of Section 5 - Non-Metallic Braided Hose Assembly Test Methods, and the addition of SI equivalent units as applicable.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
This SAE Aerospace Standard describes the test methods for flexible PTFE hose and hose assemblies used in aircraft fluid systems in the pressure and temperature ranges defined in MA2001 (ISO 6771). It applies to the hose and the hose coupling. The tests and assembly requirements for the connecting end fitting are covered in the procurement specification.This document applies each time that it is referred to in a procurement specification or other definition document.Fluids and materials used for the tests are listed in Appendix A.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
This document defines the requirements for polytetrafluoroethylene (PTFE) lined, metallic braid reinforced, hose assembly suitable for use in 400 °F (204 °C), 5080 psi (35 000 kPa) aircraft hydraulic systems.NOTE: The SI metric units defined herein are soft conversion units. Revised to reflect the current mating fitting standards, flareless fitting torques, and impulse test requirements.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
This Aerospace Standard (AS) defines the requirements for a heavy braid polytetrafluoroethylene (PTFE) lined, metallic reinforced, hose assembly suitable for use in high temperature, 400 °F, high pressure, 3000 psi, aircraft hydraulic fluid systems, also for use in pneumatic systems which allow some gaseous diffusion through the PTFE wall. The -20 size operating temperature is limited to 275 °F maximum. Added periodic testing requirements for fire resistant hose assemblies. Relocated fire test qualification requirements from NOTES paragraph 6.1.1 to qualification testing paragraphs 3.5.2.14 and 4.6.16, and revised Tables 4A and 4B to reflect applicable fire test paragraph.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
This document defines the requirements for polytetrafluoroethylene (PTFE) lined, metallic braid reinforced, hose assembly suitable for use in 400 °F (204 °C), 5080 psi (35000 kPa) aircraft hydraulic systems. Revised spherical ball size requirements to eliminate the straight fittings ball size.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
AS4006 HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE FIVE-YEAR REVIEW POLICY.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
AS4007 HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE FIVE-YEAR REVIEW POLICY.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
This SAE Aerospace Standard (AS) defines the requirements for a convoluted polytetrafluoroethylene (PTFE) lined, metallic reinforced, hose assembly suitable for use in aircraft fluid systems at temperatures of -65 to 400 °F and at operating pressures per Table 1. This document has been reaffirmed to comply with the SAE 5-year Review policy.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
