TWIN COMANCHE C/R
I
4.
EMERGENCY PROCEDURES
a.
In the event of a malfunction in the AutoControl, push the ON/OFF button to “OFF”
position. This disengages the AutoControl from the control system.
111
b. AutoControl may be overpowered manually by exertion of 12(+ 3) pounds force on
the control wheel.
C.
In cruise configuration AutoControl malfunction with a 3 second recovery delay
resulted in a 35 degree bank and 30 foot altitude loss.
I
d. In approach configuration AutoControl malfunction with a 1 second recovery delay
resulted in a 25 degree bank and 40 foot altitude loss.
REPORT: 1605 PART I PAGE 24
MODEL: PA-39
FAA APPROVED November 28.1969
REISSUED: June 1,197O
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