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SAE International, 08/12/2021
Publisher: SAE
File Format: PDF
$53.00$106.00
Published:12/08/2021
File Size:1 file , 280 KB
Note:This product is unavailable in Ukraine, Russia, Belarus
This procurement specification covers aircraft quality studs made from a low alloy steel of the type identified under the Unified Numbering System as UNS G87400, and of a series of room temperature tensile strengths ranging from 125000 to 185000 psi.
Titanium Alloy, Cold Rolled Sheet and Strip 15V - 3Al - 3Cr - 3Sn Solution Heat Treated
$35.00 $71.00
Aluminum Alloy, Drawn, Round, Seamless Hydraulic Tubing 4.4Cu - 1.5Mg - 0.60Mn (2024-T3) Solution Heat Treated, Cold Worked, and Naturally Aged
Aluminum Alloy, Plate (2.7 Cu - 1.8 Li - 0.7 Zn) 2099-T86 Solution Heat Treated, Cold Worked, and Artificially Aged
$33.00 $66.00
Contamination Classification for Hydraulic Fluids
$44.00 $88.00
