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SAE International, 11/01/2021
Publisher: SAE
File Format: PDF
$60.00$120.00
Published:01/11/2021
File Size:1 file , 390 KB
Note:This product is unavailable in Ukraine, Russia, Belarus
This document discusses the history and development of endurance requirements, provides an analysis of test contaminant material and includes a discussion of future requirements.
This document provides the reader with a background of aircraft turbine engine fuel system component endurance test requirements needed by engineers working on component design evaluation.
BOLT, MACHINE - HEXAGON HEAD, DRILLED 1 HOLE, PD SHANK, NICKEL ALLOY (UNS N07001), .3125-24 UNJF-3A
$24.00 $48.00
BOLT, MACHINE - HEXAGON HEAD, FULL SHANK, CORROSION RESISTANT STEEL (UNS S17400), 140 KSI MIN UTS, .5000-20 UNJF-3A
$20.00 $40.00
BOLT, MACHINE - HEXAGON HEAD, DRILLED 1 HOLE, PD SHANK, NICKEL ALLOY (UNS N07001), .3750-24 UNJF-3A
“D” RING SEAL FOR SHOCK STRUTS MOLDED FROM MIL-P-25732 ACRYLONITRILE BUTADIENE (NBR) MATERIAL
$27.00 $54.00
