SAE AS36100C PDF

This SAE Aerospace Standard (AS) defines the minimum performance requirements and test parameters for air cargo unit load devices requiring approval of airworthiness for installation in an approved aircraft cargo compartment and restraint system that complies with the cargo restraint requirements of Title 14 CFR Part 25, except for the 9.0-g forward ultimate inertia force of ¿¿ 25.561 (b)(3)(ii).

File Size :	1 file , 1000 KB
Note :	This product is unavailable in Ukraine, Russia, Belarus
Number of Pages :	40
Published :	09/29/2020