Light
Dark
System
Log In
Loading...
Compare / EASA/
Incorporated Amendments
/
Compare & Highlight Differences
CS 27.977 Fuel tank outlet
Available versions for ERULES-1963177438-4757
ED Decision 2003/15/RM
found in: CS-27 Amdt 9 - Small Rotorcraft (Dec 2021)
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 27.977 Fuel tank outlet ED Decision 2003/15/RM (a) There must be a fuel strainer for the fuel tank outlet or for the booster pump. This strainer must: (1) For reciprocating engine-powered rotorcraft have 3 to 6 meshes per cm (8 to 16 meshes per inch); and (2) For turbine engine-powered rotorcraft, prevent the passage of any object that could restrict fuel flow or damage any fuel system component. (b) The clear area of each fuel tank outlet strainer must be at least 5 times the area of the outlet line. (c) The diameter of each strainer must be at least that of the fuel tank outlet. (d) Each finger strainer must be accessible for inspection and cleaning.
CS 27.977 Fuel tank outlet ED Decision 2003/15/RM (a) There must be a fuel strainer for the fuel tank outlet or for the booster pump. This strainer must: (1) For reciprocating engine-powered rotorcraft have 3 to 6 meshes per cm (8 to 16 meshes per inch); and (2) For turbine engine-powered rotorcraft, prevent the passage of any object that could restrict fuel flow or damage any fuel system component. (b) The clear area of each fuel tank outlet strainer must be at least 5 times the area of the outlet line. (c) The diameter of each strainer must be at least that of the fuel tank outlet. (d) Each finger strainer must be accessible for inspection and cleaning.