Your shopping cart is empty!
SAE International, 09/30/2021
Publisher: SAE
File Format: PDF
$48.00$97.00
Published:30/09/2021
File Size:1 file , 340 KB
Note:This product is unavailable in Ukraine, Russia, Belarus
This document covers the general requirements for hydraulic aircraft jacks. It can be applied to tripod, unipod, and axle jacks that may be used on open ramp areas as well as in the aircraft hangar.
Throughout this Aerospace Standard, the minimum essential criteria are identified by the key word "shall". Recommended criteria are identified by use of the key word "should". Deviation from recommended criteria should only occur after careful consideration and thorough service evaluation have shown alternate methods to provide an equivalent level of safety.
The term "vertical load" throughout this Aerospace Standard is defined as the force imposed on the aircraft jack at the airframe jack point.
Motorcycle Bank Angle Measurement Procedure
$27.00 $54.00
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, FULL SHANK, STEEL UNS G87400 CADMIUM PLATED, .5625-18 UNJF-3A
$24.00 $48.00
Battery Electric Vehicle Energy Consumption and Range Test Procedure
$73.00 $146.00
Nickel-Copper Alloy Wire and Ribbon, Corrosion-Resistant 67Ni - 31Cu Annealed
$33.00 $66.00