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CS 27.1141 Powerplant controls: general
Available versions for ERULES-1963177438-4779
ED Decision 2003/15/RM
found in: CS-27 Amdt 9 - Small Rotorcraft (Dec 2021)
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CS-27 Amdt 10 - Sm... (Feb 2023)
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CS 27.1141 Powerplant controls: general ED Decision 2003/15/RM (a) Powerplant controls must be located and arranged under [CS 27.777](#_DxCrossRefBm472493360) and marked under [CS 27.1555](#_DxCrossRefBm472493381). (b) Each flexible powerplant control must be approved. (c) Each control must be able to maintain any set position without: (1) Constant attention; or (2) Tendency to creep due to control loads or vibration. (d) Controls of powerplant valves required for safety must have: (1) For manual valves, positive stops or in the case of fuel valves suitable index provisions, in the open and closed position; and (2) For power-assisted valves, a means to indicate to the flight crew when the valve: (i) Is in the fully open or fully closed position; or (ii) Is moving between the fully open and fully closed position. (e) For turbine-engine-powered rotorcraft, no single failure or malfunction, or probable combination thereof, in any powerplant control system may cause the failure of any powerplant function necessary for safety.
CS 27.1141 Powerplant controls: general ED Decision 2003/15/RM (a) Powerplant controls must be located and arranged under [CS 27.777](#_DxCrossRefBm8893933) and marked under [CS 27.1555](#_DxCrossRefBm8893955). (b) Each flexible powerplant control must be approved. (c) Each control must be able to maintain any set position without: (1) Constant attention; or (2) Tendency to creep due to control loads or vibration. (d) Controls of powerplant valves required for safety must have: (1) For manual valves, positive stops or in the case of fuel valves suitable index provisions, in the open and closed position; and (2) For power-assisted valves, a means to indicate to the flight crew when the valve: (i) Is in the fully open or fully closed position; or (ii) Is moving between the fully open and fully closed position. (e) For turbine-engine-powered rotorcraft, no single failure or malfunction, or probable combination thereof, in any powerplant control system may cause the failure of any powerplant function necessary for safety.