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Book TUBE FITTINGS  METRIC  AEROSPACE FLUID SYSTEMS  SEPARABLE GENERAL SPECIFICATION FOR

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.

Book Tube Fittings  Aerospace Fluid Systems  Separable  For 24   Cone  General Specification  Metric  ISO 7169

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.

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

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

Book Tube Fittings  Metric  Aerospace Fluid Systems  Separable

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:

Book Tube Fittings  Aerospace Fluid Systems  Separable  for 24 Degree Cone  General Specification  Metric  ISO 7169

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.

Book TUBE FITTINGS  FLUID SYSTEMS  SEPARABLE  GENERAL SPECIFICATION FOR

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.

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

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

Book Separable Tube Fittings for Fluid Systems  24 0D Cone  General Specification

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)

Book Fittings  Axially Swaged Tube with Flareless Separable  Fluid System 5080 Psi  35 000 KPa   Specification for

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 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 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). AS5958 Rev. C is an exact duplication of AS5958 Rev. A. AS5958 Rev. B had been issued prematurely and has been removed from circulation.Rationale from Rev. A: Added -20 size and requirements and corrected errors.

Book Separable Fittings  Permanent Fittings  Tubing  Fluid Systems 8000 Psi Qualification Test Standard For

Download or read book Separable Fittings Permanent Fittings Tubing Fluid Systems 8000 Psi Qualification Test Standard For 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 Performance Standard covers the Qualification Test Requirements for separable fittings, permanent fittings, and tubing suitable for use in 8000 psi aerospace fluid power systems. The standard treats each of these elements as part of a "system" in which each element has a specific critical relationship one to the other This document is applicable to both the pressure (8000 psi) and the return (4000 psi) portions of an 8000 psi rated system. Rationale for tests, testing philosophy, and key words are covered in Sections 5 and 6. AS4401 has been reaffirmed to comply with the SAE five-year review policy.

Book Fittings  Axially Swaged Tube with Flareless Separable  Fluid System For Operating Pressures Up to and Including 5080 Psi  35 000 KPa   Specification for

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 2013 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 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 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 aerospace fitting part number standard and tubing materials and operating pressures. Add Blue Anodize and Ink-Jet Options as Identification and Marking methods to 3.4.2.3 and 3.5.2, and correct the joint strength conversion values to Newton in Tables 3A and 3B.

Book Fittings  Axially Swaged Tube with Flareless Separable  Fluid System for Operating Pressures Up to and Including 5080 Psi  35000 KPa   Specification for

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.

Book Aluminum Fittings  Axially Swaged Tube with Flareless Separable  Fluid System Up to 1500 Psi  10 340 KPa  Maximum  Specification for

Download or read book Aluminum Fittings Axially Swaged Tube with Flareless Separable Fluid System Up to 1500 Psi 10 340 KPa Maximum Specification for written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2011 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This SAE Aerospace Standard (AS) establishes the requirements for externally swaged aluminum tube fittings on aluminum tubing with flareless separable fitting ends for use in hydraulic supply and return aerospace fluid systems including pneumatic, coolants, and fire extinguishers up to a maximum operating pressure of 1500 psig (10 340 kPa) and a maximum operating temperature range of 65 to +225 °F (54 to +107 °C).This specification covers a common aluminum fitting that may be used for a range of operating pressures up to 1500 psi with different tubing materials and tubing wall thicknesses, and is assembled with the same tooling in accordance with AS6124. Table 12 shows applicable aerospace fitting part number standard and tubing materials and operating pressures. This specification is being prepared to provide the performance requirements for aluminum axially swaged, field attachable, 1500 psi, tube fittings.

Book Fittings  Tube  Fluid Systems  Separable  Beam Seal  3000 4000 Psi  General Specification For  Supplement 1

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.

Book Fittings  Tube  Fluid Systems  Separable  High Pressure  Dynamic Beam Seal  General Specification For

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.

Book Aluminum Fittings  Axially Swaged Tube with Flareless Separable  Fluid System Up to 1500 Psi  10340 KPa  Maximum  Specification for

Download or read book Aluminum Fittings Axially Swaged Tube with Flareless Separable Fluid System Up to 1500 Psi 10340 KPa Maximum Specification for written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2016 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This SAE Aerospace Standard (AS) establishes the requirements for externally swaged aluminum tube fittings on aluminum tubing with flareless separable fitting ends for use in hydraulic supply and return aerospace fluid systems including pneumatic, coolants, and fire extinguishers up to a maximum operating pressure of 1500 psig (10340 kPa) and a maximum operating temperature range of -65 to +225 °F (-54 to +107 °C).This specification covers a common aluminum fitting that may be used for a range of operating pressures up to 1500 psi with different tubing materials and tubing wall thicknesses, and is assembled with the same tooling in accordance with AS6124. Table 12 shows applicable aerospace fitting part number standard and tubing materials and operating pressures. Change operating pressure requirements of size 24 from 500 to 600 psi (including proof and burst pressures), add vibration curves requirements to Tables 10 and 11 for size 24, add the new configuration part number AS6323 to Table 12, and add size 24 dimensions to some of the standards configurations.

Book FITTINGS  TUBE  FLUID SYSTEMS  SEPARABLE  HIGH PRESSURE  DYNAMIC BEAM SEAL  DESIGN STANDARD FOR MALE END

Download or read book FITTINGS TUBE FLUID SYSTEMS SEPARABLE HIGH PRESSURE DYNAMIC BEAM SEAL DESIGN STANDARD FOR MALE END 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: