EASA Module 14 Practice Questions - EASA Part-66 Module 14 - Propulsion (B2) Exam

In a turboshaft engine, the energy of the gas stream is used primarily to:

Produce reactive jet thrust at the exhaust nozzle Drive a free (power) turbine that delivers shaft power to a rotor or load Drive only the engine's own compressor with no useful output Generate electrical power directly without any rotating turbine

Correct Answer:

Drive a free (power) turbine that delivers shaft power to a rotor or load

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