Thanks Dave and Henrik for the correctionCFIDave wrote:My understanding is that constant-speed propellers are designed quite differently for single-engine vs. twin-engine piston aircraft applications, purposely built with different failure characteristics:Henrik wrote:From the questionnaire:Ouch, there goes our twin engine safety argument against Cirrus' chute!If the oil pressure to the propeller dome is lost, does the propeller go into
coarse or fine pitch? Fine pitch
On a DA40, loss of oil would cause the prop to go into fine pitch, for safe flight at the lower speeds required for landing or a go-around climb.
On a DA42, loss of oil would cause the prop to go into coarse pitch, all the way to feather. As multi-engine pilots know, it's extremely difficult to fly a twin with the asymmetric drag of a windmilling prop.
So I'd still take a DA42 twin over a Cirrus 'chute anytime. :-D
I have spend too much time flying singles lately....
From the DA 42 NG AFM page 7-27 Prop Control
Pitch is set by the ECU control of the governor. To change blade pitch angle gearbox oil is pumped into the propeller hub. Increasing the oil pressure leads to a decrease of pitch (fine) and a higher RPM. Decreasing the oil pressure leads to higher (Coarse) pitch and lower RPM.
Then on the next page under Feathering
To feather the propeller the engine must be shut down with the appropriate ENG MASTER switch. This will open the electric governor valve. All oil will flow back from the propeller hub, allowing blades to move into the feathered pitch position.
Thanks for the correction once again...
I shall give PIREPs during the next week.
Safe flying
Robin