AFMS N°D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
This table is a quick access table that provide additional information regarding residual A/P capa-
bilities in case of loss of PFD or MFD.
A/P reverts to PIT & ROLL (from any mode select-
ed) No aurals from A/P (both A/P DISC & USP)
A/P stays in the selected mode
A/P control keyboard unavail-
able
A/P can be disconnected with A/P DISC button on con-
trol wheel
FD command bars cannot be eliminat-
ed ESP Off on alert window on PFD
A/P automatically disconnects after ~ 4 to 5 se-
conds
A/P disconnection tone plays endlessly until A/P DISC
button is pressed