Light
Dark
System
Log In
Loading...
Compare / EASA/
Incorporated Amendments
/
Compare & Highlight Differences
CS 27.961 Fuel system hot weather operation
Available versions for ERULES-1963177438-4748
ED Decision 2003/15/RM
found in: CS-27 Amdt 10 - Small Rotorcraft (Feb 2023)
From
CS-27 Amdt 10 - Sm... (Feb 2023)
CS-27 Amdt 9 - Sma... (Dec 2021)
From section
To
CS-27 Amdt 10 - Sm... (Feb 2023)
CS-27 Amdt 9 - Sma... (Dec 2021)
To section
No visible text changes
0 removals
0 additions
View
Rich
Plain
Sync scrolling
Share
From
Show details
Hide details
To
Show details
Hide details
Version
Show side by side
CS 27.961 Fuel system hot weather operation ED Decision 2003/15/RM Each suction lift fuel system and other fuel systems with features conducive to vapour formation must be shown by test to operate satisfactorily (within certification limits) when using fuel at a temperature of 43°C (110°F) under critical operating conditions including, if applicable, the engine operating conditions defined by [CS 27.927(b)(1) and (b)(2)](#_DxCrossRefBm8893843).
CS 27.961 Fuel system hot weather operation ED Decision 2003/15/RM Each suction lift fuel system and other fuel systems with features conducive to vapour formation must be shown by test to operate satisfactorily (within certification limits) when using fuel at a temperature of 43°C (110°F) under critical operating conditions including, if applicable, the engine operating conditions defined by [CS 27.927(b)(1) and (b)(2)](#_DxCrossRefBm472493277).