Daher TBM 930 - Autopilot or Electric Pitch Trim Malfunction

Pilot's Operating Handbook
Section 3
Emergency procedures
EASA Approved
Edition 1 - January 15, 2018
Rev. 0
Page 3.12.20
Autopilot or electric pitch trim malfunction
▲ CAUTION ▲
When disconnecting the autopilot after a pitch trim malfunction, hold the
control wheel firmly. Up to 30 pounds of force on the control wheel may
be necessary to hold the airplane level.
▲
1 - AP / TRIM DISC push-button Press and hold. . . . . . . . . . . . . . . . . . . . . . . . . . .
2 - AP / TRIMS switch OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
3 - AP / TRIM DISC push-button Release. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
If necessary :
4 - Control wheel Retrim. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
End of procedure.
PIM - DO NOT USE FOR FLIGHT OPERATIONS