Light
Dark
System
Log In
Loading...
Compare / EASA/
Incorporated Amendments
/
Compare & Highlight Differences
CS 22.955 Fuel flow
Available versions for ERULES-1963177438-5116
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 22.955 Fuel flow ED Decision 2003/13/RM (a) *Gravity systems.* The fuel flow rate for gravity systems (main and reserve supply) must be 150% of the take-off fuel consumption of the engine. (b) *Pump systems.* The fuel flow rate for each pump system (main and reserve supply) must be 125% of the take-off fuel consumption of the engine at the maximum power established for take-off .