SAE AS4510-1996 PDF

Scope: This SAE Aerospace Standard (AS) establishes the requirements for weld fluid connection fittings and rings to be orbital arc welded to tubing for use in aircraft fluid systems at a maximum operating pressure of 5000 psi.

SAE AS4510-1996 Referenced Document

ISO 10012-1:1992 Quality assurance requirements for measuring equipment; part 1: metrological confirmation system for measuring equipment
SAE AMS2759 HEAT TREATMENT OF STEEL PARTS General Requirements
SAE AMS4928N-1993 Titanium Alloy Bars@ Wire@ Forgings@ and Rings 6Al - 4V Annealed (UNS R56400)
SAE AMS4944E-1995 Titanium Alloy@ Seamless@ Hydraulic Tubing 3.0Al - 2.5V Cold Worked@ Stress Relieved (UNS R56320)
SAE AMS4945A-1992 Titanium Alloy Tubing@ Seamless@ Hydraulic 3Al - 2.5V@ Texture Controlled 105 ksi (724 MPa) Yield Strength Cold Worked@ Stress Relieved
SAE AMS5561C-1992 Steel Tubing@ Welded and Drawn@ Corrosion and Heat Resistant 9.0Mn - 20Cr - 6.5Ni - 0.28N High-Pressure Hydraulic
SAE AMS5659 STEEL BARS@ FORGINGS AND RINGS@ CORROSION RESISTANT 15Cr - 5Ni - 4Cu Consumable Electrode Melted
SAE ARP1185 FLEXURE TESTING OF HYDRAULIC TUBING JOINTS AND FITTINGS
SAE ARP1185B-1993 Flexure Testing of Hydraulic Tubing Joints and Fittings
SAE ARP4784-1993 Performance and Evaluation Criteria@ Surface Defects@ Requirements for
SAE ARP603F-1985 Impulse Testing of Hydraulic Hose, Tubing, and Fitting Assemblies
SAE AS478 AS478 Bobbin. Anti-Spin Parachute. Jettison Slip