Hello dev Team. I saw gladly, that the propeller switch you tried to correct it. Is the file not put very far?
Somebody would exchange the increase and decrease directions? The translation did not succeed unfortunately:
http://www.cockpitinstrumente.de/ins.../Fl18502-2.gif
Größer - "greater"
RPM!!* Reduce the angle of attack of the propeller (to the rotatory plane**), the wind resistance of a propeller decreases, the rev of an engine accelerates. The Prop pitch gauge move to 12:00.
Drehzahl - "rev/min"
Kleiner - "lesser" RPM: increase the AoA of propeller.
Segelstllg (Segelstellung) - "Glide-standing" increase to maximum AoA of Propeller**, because this causes the smallest wind resistance, if the engine stopped. This now totally wrong (on the switch).
*
http://www.cockpitinstrumente.de/Flu...ung/Bilder.htm
**What they measure the position angle of the propeller against in the Russian technical literature? Strange, that it was counted turned over in the il-2 already. I wrote the position angle of the propeller compared to the
rotatory plane.
ps. Did it not manage to convince it that water radiator flap indicator is bad? Ehh
