Light
Dark
System
Log In
Loading...
Compare / EASA/
Incorporated Amendments
/
Compare & Highlight Differences
CS 31HB.23 Load factors
Available versions for ERULES-1963177438-4965
ED Decision 2009/005/R
found in: CS-31HB Amdt 1 - Hot Air Balloons (Dec 2011)
Version
CS-31HB Amdt 1 - H... (Dec 2011)
Section
Share
Version
Show details
Hide details
Version
CS 31HB.23 Load factors ED Decision 2009/005/R (a) Flight load factor. In determining limit loads, the limit load factor must be at least 1·4, except for (b). (b) Landing load factor. For all parts belonging to the balloon’s suspension system, including the envelope to suspension system pick up points, limit load must be determined using a limit load factor of at least 3·0.