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CS 27.939 Turbine engine operating characteristics
Available versions for ERULES-1963177438-4741
ED Decision 2003/15/RM
found in: CS-27 Amdt 10 - Small Rotorcraft (Feb 2023)
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CS-27 Amdt 10 - Sm... (Feb 2023)
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CS 27.939 Turbine engine operating characteristics ED Decision 2003/15/RM (a) Turbine engine operating characteristics must be investigated in flight to determine that no adverse characteristics (such as stall, surge, or flameout) are present, to a hazardous degree, during normal and emergency operation within the range of operating limitations of the rotorcraft and of the engine. (b) The turbine engine air inlet system may not, as a result of airflow distortion during normal operation, cause vibration harmful to the engine. (c) For governor-controlled engines, it must be shown that there exists no hazardous torsional instability of the drive system associated with critical combinations of power, rotational speed, and control displacement.
CS 27.939 Turbine engine operating characteristics ED Decision 2003/15/RM (a) Turbine engine operating characteristics must be investigated in flight to determine that no adverse characteristics (such as stall, surge, or flameout) are present, to a hazardous degree, during normal and emergency operation within the range of operating limitations of the rotorcraft and of the engine. (b) The turbine engine air inlet system may not, as a result of airflow distortion during normal operation, cause vibration harmful to the engine. (c) For governor-controlled engines, it must be shown that there exists no hazardous torsional instability of the drive system associated with critical combinations of power, rotational speed, and control displacement.