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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.
T-BOLT, A-286, 1000 °F BUSHING HEAD
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WIRE, ELECTRICAL, FLUOROPOLYMER-INSULATED, CROSSLINKED MODIFIED ETFE, LOW FLUORIDE, NORMAL WEIGHT, 80 MICROINCH SILVER-COATED COPPER 200 °C, 600 VOLT, ROHS (Stabilized: Aug 2021)
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Unsettled Issues Concerning eVTOL for Rapid-response, On-demand Firefighting
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TERMINALS, LUG AND SPLICES, CONDUCTOR, CRIMP STYLE, COPPER, INSULATED, RECTANGULAR TONGUE, FOR THIN WALL WIRE, TYPE III, CLASS 1, FOR 105 °C TOTAL CONDUCTOR TEMPERATURE (Stabilized: Aug 2021)
