Download or read book Specification for Separable Tube Fittings for Fluid Systems written by British Standards Institution and published by . This book was released on 1986 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Separable Tube Fittings for Fluid Systems 24 0D Cone General Specification written by British Standards Institute Staff and published by . This book was released on 1998-12-01 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: Fluid equipment components, Aircraft components, Space technology components, Fluid equipment, Pipe fittings, Hydraulic equipment, Threads, Defects, Surface defects, Pressure, Grades (quality), Dimensions, Colour codes, Marking, Performance, Finishes, Classification systems, Test pressure, Bend testing, Test specimens, Inspection, Leak tests, Stress corrosion, Corrosion tests, Mechanical testing, Pressure testing, Sampling methods, Quality assurance, Approval testing, Quality control, Statistical quality control, Packaging, Specimen preparation, Angles (geometry)

Download or read book Tube Fittings Aerospace Fluid Systems Separable For 24 Cone General Specification Metric ISO 7169 written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2015 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This document specifies performance and quality requirements for the qualification and manufacture of 24° cone fittings to ensure reliable performance in aircraft hydraulic systems.This document specifies baseline criteria for the design and manufacture of system fittings that are qualification tested on engines.This document covers fittings of temperature types and pressure classes specified in MA2001. MA2005B has been reaffirmed to comply with the SAE five-year review policy.

Download or read book Tube Fittings Aerospace Fluid Systems Separable for 24 Degree Cone General Specification Metric ISO 7169 written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2021 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This document specifies performance and quality requirements for the qualification and manufacture of 24 degree cone fittings to ensure reliable performance in aircraft hydraulic systems.This document specifies baseline criteria for the design and manufacture of system fittings that are qualification tested on engines.This document covers fittings of temperature types and pressure classes specified in MA2001. Quality conformance inspection requirements revised to correct AQL levels in 4.2.2.1.2. Replace tubing specification MA2016 with ISO 8575 in 3.2.2.

Download or read book TUBE FITTINGS METRIC AEROSPACE FLUID SYSTEMS SEPARABLE GENERAL SPECIFICATION FOR written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 1983 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This standard establishes the basic performance and quality criteria for screw-together tube fitting assemblies and port connectors. It was prepared to standardize on the qualification test and procurement requirements for ISO standard tube fittings. The test requirements are intended to satisfy the most strenuous demands encountered in a high performance aircraft hydraulic system. The procurement requirements are intended to assure that fittings which are bought to this specification are of the same quality as the fittings used during the original qualification testing. Compliance with these test and procurement requirements is necessary for fittings which are used in control systems where a malfunction could affect the safety of flight.

Download or read book TUBE FITTINGS FLUID SYSTEMS SEPARABLE GENERAL SPECIFICATION FOR written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 1981 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This document establishes the basic performance and quality criteria for screw-together tube fitting assemblies and port connectors used in aircraft fluid systems.

Download or read book Aerospace Separable Tube Fittings for Fluid Systems for 24 0D Cones for Pressures Up to 3000 PSI Or 21000 KPa Procurement Specification Inch Metric written by British Standards Institute Staff and published by . This book was released on 2007-05-31 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aircraft components, Hydraulic equipment, Fluid equipment components, Fluid equipment, Pipe fittings, Threads, Defects, Surface defects, Pressure, Grades (quality), Performance, Dimensions, Angles (geometry), Colour codes, Marking, Finishes, Classification systems, Test pressure, Bend testing, Leak tests, Stress corrosion, Corrosion tests, Mechanical testing, Pressure testing, Sampling methods, Quality assurance, Inspection, Approval testing, Quality control, Statistical quality control, Packaging, Test specimens

Download or read book Aerospace Separable Tube Fittings for Fluid Systems for 24 0D Cones for Pressures Up to 3 000 Psi Or 21 000 KPa Procurement Specification Inch metric written by British Standards Institute Staff and published by . This book was released on 1914-11-30 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aircraft components, Hydraulic equipment, Fluid equipment components, Fluid equipment, Pipe fittings, Threads, Defects, Surface defects, Pressure, Grades (quality), Performance, Dimensions, Angles (geometry), Colour codes, Marking, Finishes, Classification systems, Test pressure, Bend testing, Leak tests, Stress corrosion, Corrosion tests, Mechanical testing, Pressure testing, Sampling methods, Quality assurance, Inspection, Approval testing, Quality control, Statistical quality control, Packaging, Test specimens

Download or read book Fittings Tube Fluid Systems Separable Beam Seal 3000 4000 Psi General Specification For Supplement 1 written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2013 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This supplement forms a part of SAE Aerospace Specification AS85421. It shall be used to identify fitting standards citing this procurement specification. AS85421SUP1 has been reaffirmed to comply with the SAE five-year review policy.

Download or read book Fittings Axially Swaged Tube with Flareless Separable Fluid System 5080 Psi 35 000 KPa Specification for written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2006 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This SAE Aerospace Standard (AS) establishes the requirements for externally swaged titanium tube fittings on titanium tubing with flareless separable fitting for use in hydraulic supply and return aerospace fluid systems up to operating pressure of 5080 psig (35,000 kPa) maximum and an operating temperature range of -65 to +275 °F (-54 to +135 °C). This specification was prepared to provide the performance requirements for axially swaged, field attachable, 5080 psi, tube fittings.

Download or read book Tube Fittings Metric Aerospace Fluid Systems Separable written by American National Standards Institute and published by . This book was released on 1983 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Fittings Tube Fluid Systems Separable High Pressure Dynamic Beam Seal General Specification For written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2004 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification covers the basic test and design requirements for one style separable high pressure beam seal fittings including boss or port seal connectors for use in 5000/8000 psi aerospace fluid systems. Definitions of fitting and related terms are included in 6.4.

Download or read book Fittings Axially Swaged Tube with Flareless Separable Fluid System for Operating Pressures Up to and Including 5080 Psi 35 000 KPa Specification for written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2009 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This SAE Aerospace Standard (AS) establishes the requirements for externally swaged titanium tube fittings on titanium and CRES tubing with flareless separable fitting for use in hydraulic supply and return aerospace fluid systems up to a maximum operating pressure of 5080 psig (35 000 kPa) and a maximum operating temperature range of -65 to +275 °F (-54 to +135 °C).This specification covers a common 5080 psi pressure titanium fitting that may be used for a range of operating pressures up to 5080 psi with different tubing materials and tubing wall thicknesses, and is assembled with the same tooling in accordance with AS5959. The fitting operating pressure is based on the fitting thread pitch. Extra fine pitch for 5080 psi operating pressure and fine pitch for operating pressures 3000 psi and less. Table 12 shows applicable fitting number and tubing materials and operating pressures. Add performance requirements for additional tube materials, tube thicknesses and pressures.

Download or read book Fittings Tube Fluid Systems Separable Beam Seal 3000 4000 Psi General Specification For written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 1998 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification covers the design requirements and test procedures for separable beam seal fittings which includes end fittings (see 6.10.3), fitting bodies (see 6.10.6), and boss fittings (see 6.10.1) for use in aerospace fluid systems. Design requirements are for class 3000 in corrosion resistant steel (CRES) only and for class 4000 in titanium alloy (Ti) only. Definition of fittings and related terms are defined in 6.10. This document has been reaffirmed to comply with the SAE 5-year Review policy.

Download or read book Fittings Tube Fluid Systems Separable High Pressure Beam Seal 5000 8000 Psi General Specification for written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2022 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification covers the design requirements and test procedures for separable beam seal fittings which include end fittings (see 2.4.2), connectors (see 2.4.3), and boss fittings for use in aerospace fluid systems. Design requirements are for Class 5000 and 8000 in titanium, and corrosion resistant steel (CRES). Definition of fittings and related terms are defined in 2.4. Modified periodic control testing procedures/tests (4.4.3); clarified flexure Tables 2A, 2B, and 2C; and added new tubing material options to Table 1.

Download or read book Fittings Tube Fluid Systems Separable High Pressure Dynamic Beam Seal 5000 8000 Psi General Specification For written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2015 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification covers the design requirements and test procedures for separable beam seal fittings which include end fittings (see 2.4.2), connectors (see 2.4.3), and boss fittings for use in aerospace fluid systems. Design requirements are for Class 5000 and 8000 in titanium, and corrosion resistant steel (CRES). Definition of fittings and related terms are defined in 2.4. This standard is revised to correct minor errors and to provide for PRI-QPL requirements and to establish PRI-QPL-AS85720.

Download or read book Fittings Axially Swaged Tube with Flareless Separable Fluid System for Operating Pressures Up to and Including 5080 Psi 35000 KPa Specification for written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2017 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This SAE Aerospace Standard (AS) establishes the requirements for axially swaged titanium fittings on titanium, CRES, and aluminum tubing with flareless separable fitting ends for use in hydraulic supply and return aerospace fluid systems up to operating pressure of 5080 psig (35000 kPa) maximum. The operating temperature range for titanium tubing and CRES tubing is 65 to +275 °F (54 to +135 °C) and the operating temperature range for aluminum return system tubing is 65 to +225 °F (54 to +107 °C).This specification covers a common 5080 psi pressure titanium fitting that may be used for a range of operating pressures up to 5080 psi with different tubing materials and tubing wall thicknesses, and is assembled with the same tooling in accordance with AS5959. The flareless fitting operating pressure is based on the fitting thread pitch. Extra fine pitch is used for 5080 psi operating pressure and fine pitch for operating pressures 3000 psi and less. Table 14 shows applicable aerospace fitting part number standard and tubing materials and operating pressures. Add performance requirements for aluminum tubing, class designation for tubing, update and correct existing text and figures.