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 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 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 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 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 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 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 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 ISO Catalogue written by International Organization for Standardization and published by . This book was released on 2007 with total page 946 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Fitting Plug in Union Ring Locked 24 Degree Cone Fluid Connection 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 2010 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This SAE Aerospace Standard (AS) establishes the requirements for 24 degree cone AS5827 or EN 6123 flareless Ring locked fitting assemblies per AS5550 and AS5865, for use in aircraft fluid systems at nominal operating pressure of 5080 psi (35 000 kPa) maximum and operating temperature range of -65 to +275 °F (-54 to +135 °C).The general requirements shall be for, but not limited to, commercial aircraft hydraulic components per AS4941, using port configuration as specified in AS5551. Include SI Metric equivalents for ISO recognition of this document.
Download or read book Fittings 24 Degree Cone Flareless Fluid Connection 3000 Psi 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 SAE Aerospace Standard (AS) establishes the requirements for 24 degree cone flareless fluid connection fittings and nuts, internally or externally swaged, preset, or welded sleeves for use in aircraft fluid systems at nominal operating pressures up to and including 3000 psi. Note 3.3.2, sub-note 4 added to address acceptance of excessive roughness of thread crests due to thread rolling process. NAS1760 added to note 3.7.5. Specification number typo corrected in Table 12.
Download or read book Catalogue written by International Organization for Standardization and published by . This book was released on 2008 with total page 988 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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.
Download or read book Fittings 24 Cone Flareless Fluid Connection 3000 Psi written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2008 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This SAE Aerospace Standard (AS) establishes the requirements for 24 degree cone flareless fluid connection fittings and nuts, internally or externally swaged, preset, or welded sleeves for use in aircraft fluid systems at nominal operating pressures up to and including 3000 psi. To correct material specification numbers in Table 1, to clarify fluorescent inspection for aluminum forgings, to add a thread requirement for ISO 3161, and periodic control test requirements under 4.5.3 have been clarified and simplified.
Download or read book Fittings 37 Degree Internal Flare Fluid Connection Procurement Specification written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2020 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This SAE Aerospace Standard (AS) establishes the requirements for 37 degree flared tube fittings or machined internal cone fluid connection fittings for use with 37 degree external cone, spherical nose, and seal ring fittings in all types of aerospace fluid systems (see Section 6). Note 4.5.1.2 revised to remove the statement that destructive testing is required to retain QML status. This requirement is regulated by AC7112.
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 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.
