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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.
NUT, PLAIN, HEXAGON, UNS S66286
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NUT, SELF-LOCKING, DOUBLE HEXAGON, REDUCED ENVELOPE, UNS S66286, COUNTERBORED SILVER PLATED THREADS ONLY
$24.00 $48.00
CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE, COAXIAL, SIZE 12 (FOR MIL-DTL-38999 SERIES I, II, III, AND IV CONNECTORS)
$33.00 $66.00
CAP ASSEMBLY, PRESSURE SEAL, FLARED TUBE FITTING
$30.00 $60.00
