What is the technique for adjusting the C-47 v3 attitude indicator so it indicates correct pitch? According to the aircraft.cfg file, the static pitch of the aircraft is 11.1 degrees, but since there is no scale on the attitude indicator, I don't see how to make good use of this value. You could adjust the attitude indicator to indicate zero pitch when in level flight according to the altimeter, but the aircraft pitch may not be zero given the flight conditions ( speed, flaps, etc). So what technique did C-47 aircrews use? Was there a specified procedure, or was setting the pitch to zero in level flight 'close enough'?
Thx,
Al
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