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SAE International, 04/08/2021
Publisher: SAE
File Format: PDF
$35.00$71.00
Published:08/04/2021
File Size:1 file , 280 KB
Note:This product is unavailable in Ukraine, Russia, Belarus
The purpose of this document is to present general considerations for the design and use of aircraft wheel chocks. The design and use of aircraft wheel chocks is a good deal more complicated than it may appear at first glance.
FITTING, UNION, STANDARD AND REDUCER, BULKHEAD, FLARELESS, PRECISION TYPE
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Heat Treatment of Carbon and Low-Alloy Steel Parts Minimum Tensile Strength Below 220 ksi (1517 MPa)
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INSTALLING AND REMOVAL TOOLS, CONNECTOR ELECTRICAL CONTACT, TYPE I & II, CLASS 2, COMPOSITION A
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CONNECTOR, PLUG, ELECTRIC, CRIMP TYPE, RACK AND PANEL, SERIES 3 (CLASS L AND E)