Simulating zero thrust
Posted: Thu Jan 10, 2013 11:11 pm
Maybe I missed it in the DA42 POH, but I'm looking for help with simulation of "zero thrust" for practicing one engine inoperative (OEI) procedures.
Rather than setting one of the Engine Master switches to OFF to actually shut down and feather a DA42 engine (which must be restarted within 2 minutes below 10,000 feet), it's possible to simulate an engine failure and feathering by pulling the throttle back to a small percentage of power. The small amount of engine power should exactly offset the drag produced by a windmilling propeller, resulting in zero thrust from that engine.
My question specifically is what percentage engine power to use for this? I've been given conflicting advice by different instructors: some say 11% power, some say 20% power. This makes a HUGE difference in the amount of rudder required to counter the asymmetrical thrust, especially when the other engine is producing 100% power (such as during simulated critical engine failure after takeoff when a positive rate of climb is required).
I'm guessing the answer might be different for Thielert vs. Austro engines, but I'd like to hear what % power people have been using for the simulated feathered engine.
- Dave
Rather than setting one of the Engine Master switches to OFF to actually shut down and feather a DA42 engine (which must be restarted within 2 minutes below 10,000 feet), it's possible to simulate an engine failure and feathering by pulling the throttle back to a small percentage of power. The small amount of engine power should exactly offset the drag produced by a windmilling propeller, resulting in zero thrust from that engine.
My question specifically is what percentage engine power to use for this? I've been given conflicting advice by different instructors: some say 11% power, some say 20% power. This makes a HUGE difference in the amount of rudder required to counter the asymmetrical thrust, especially when the other engine is producing 100% power (such as during simulated critical engine failure after takeoff when a positive rate of climb is required).
I'm guessing the answer might be different for Thielert vs. Austro engines, but I'd like to hear what % power people have been using for the simulated feathered engine.
- Dave