Fittings, 24 Degree Cone Flareless, Fluid Connection, 3000 Psi PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Fittings, 24 Degree Cone Flareless, Fluid Connection, 3000 Psi PDF full book. Access full book title Fittings, 24 Degree Cone Flareless, Fluid Connection, 3000 Psi by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies. Download full books in PDF and EPUB format.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Get Book Here
Book Description
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.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Get Book Here
Book Description
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.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Get Book Here
Book Description
This supplement forms a part of the Aerospace Standard AS18280 Fittings, 24° Cone, Flareless, Fluid Connection, 3000 psi, and shall be used to identify fitting standards citing this procurement specification. AS18280SUP1A 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
Get Book Here
Book Description
This SAE Aerospace Standard (AS) establishes the requirements for 24° 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. Revision G clarifies: defect descriptions for aluminum material finishes and test requirements for high purity aluminum (HPA) coating to eliminate redundancy with reference documents; qualification approval between 4130 and 15-5PH materials; equivalent materials for PRI QPL lists; pressure rating for size 16 aluminum tubing; provided reference for defect limits on unmachined surfaces. Lists of flareless fitting end standards is made consistent throughout. Adds single point machining requirement on flareless ends. Adds 12 month periodic test interval. Provides lubrication allowance for pneumatic test of similar materials.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Get Book Here
Book Description
This SAE Aerospace Standard (AS) establishes the requirements for 24° cone flareless fluid connection fittings and nuts and bite type flareless sleeves (see Section 6) for use in aircraft fluid systems at an operating pressure of 5000 psi for the fittings and nuts and 3000 psi for the bite type sleeves. AS4444 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
Get Book Here
Book Description
This SAE Aerospace Standard (AS) establishes the requirements for fluid fittings that combine both 24° cone flareless and 37° flared connections for use in all types of fluid systems. AS4444/2 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
Get Book Here
Book Description
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.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Get Book Here
Book Description
This SAE Metric Aerospace Standard (MA) establishes the requirements for fluid fittings that combine both weld fitting end and 24° cone flareless fitting end connections for use in all types of metric fluid systems. MA4510/1 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
Get Book Here
Book Description
This SAE Aerospace Standard (AS) establishes the requirements for fluid fittings that combine both straight thread port or flanged connections and 24° cone flareless connections for use in all types of fluid systems. AS4875/3 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
Get Book Here
Book Description
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 (35000 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. Updated 4.5.3 Periodic Control Tests to a 12-month interval.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Get Book Here
Book Description
This SAE Aerospace Standard (AS) establishes the requirements for fluid fittings that combine both weld fitting end and 24° cone flareless fitting end connections for use in all types of fluid systems. AS4510/1 has been reaffirmed to comply with the SAE five-year review policy.
