Light
Dark
System
Log In
Loading...
Compare / EASA/
Incorporated Amendments
/
Compare & Highlight Differences
CS 27.1143 Engine controls
Available versions for ERULES-1963177438-4780
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 27.1143 Engine controls ED Decision 2003/15/RM (a) There must be a separate power control for each engine. (b) Power controls must be grouped and arranged to allow: (1) Separate control of each engine; and (2) Simultaneous control of all engines. (c) Each power control must provide a positive and immediately responsive means of controlling its engine. (d) If a power control incorporates a fuel shut-off feature, the control must have a means to prevent the inadvertent movement of the control into the shut-off position. The means must: (1) Have a positive lock or stop at the idle position; and (2) Require a separate and distinct operation to place the control in the shut-off position. (e) For rotorcraft to be certificated for a 30-second OEI power rating, a means must be provided to automatically activate and control the 30-second OEI power and prevent any engine from exceeding the installed engine limits associated with the 30-second OEI power rating approved for the rotorcraft.
CS 27.1143 Engine controls ED Decision 2003/15/RM (a) There must be a separate power control for each engine. (b) Power controls must be grouped and arranged to allow: (1) Separate control of each engine; and (2) Simultaneous control of all engines. (c) Each power control must provide a positive and immediately responsive means of controlling its engine. (d) If a power control incorporates a fuel shut-off feature, the control must have a means to prevent the inadvertent movement of the control into the shut-off position. The means must: (1) Have a positive lock or stop at the idle position; and (2) Require a separate and distinct operation to place the control in the shut-off position. (e) For rotorcraft to be certificated for a 30-second OEI power rating, a means must be provided to automatically activate and control the 30-second OEI power and prevent any engine from exceeding the installed engine limits associated with the 30-second OEI power rating approved for the rotorcraft.