Light
Dark
System
Log In
Loading...
Compare / EASA/
Incorporated Amendments
/
Compare & Highlight Differences
CS 22.597 Loads from single masses
Available versions for ERULES-1963177438-5378
ED Decision 2003/13/RM
found in: Sailplane Rule Book - Part-SAO Part-SFCL CS-22 (Nov 2022)
Version
Sailplane Rule Boo... (Nov 2022)
Section
Share
Version
Show details
Hide details
Version
CS 22.597 Loads from single masses ED Decision 2003/13/RM The attachment means for all single masses, which are part of the equipment of the sailplane, must be designed to withstand loads corresponding to the maximum design load factors to be expected from the established flight and ground loads.