SAE AS5958F - Online Standart

SAE AS5958F

Fittings, Axially Swaged Tube with Flareless Separable, Fluid System for Operating Pressures up to and Including 5080 psi (35000 kPa), Specification for

Historical
Standard by SAE International, 2017-09-11

SKU: 3605afd78d01 Category:

View all product details

Quick Links

Norma
Get answers for your technical

Standart Library 
Find standards for your sector

Standart Chek
Verify updates for your standards

AS5958F.pdf

Secure PDF

Immediate Download

English
AS5958F.pdf

Online Access

Request Quote

English

About This Item

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.

Please request information about the document. Contact Page

Standard Details

  • Publication Date: 2017-09-11
  • Standard Status: historical
  • Publisher: SAE International
  • Document Type: Aerospace Standard
  • Subject: Assembling, Titanium alloys, Hydraulic fluids, Coatings, colorants, and finishes, Aluminum alloys, Fixed-wing aircraft, Jet fuel, Fittings, Identification numbers
  • Official SAE: Doi link

Document History

  • New Version Available: AS5958G (2019-06-10)
  • This Version: AS5958F (2017-09-11)
  • Previous Version: AS5958E (2013-10-20)
  • Previous Version: AS5958D (2011-01-12)
  • Previous Version: AS5958C (2009-07-06)
  • Previous Version: AS5958B (2009-06-01)
  • Previous Version: AS5958A (2007-11-05)
  • Previous Version: AS5958 (2006-01-11)

Please request information about the document. Contact Page