Tecnam P2010 - Page 223

AFMS N°D01 FOR GARMIN GFC700 AUTOPILOT INSTALLATION AND
RNAV/RNP NAVIGATION ELIGIBILITY
Page 3A-31
Section 3 – Emergency procedures
AUTOPILOT EMERGENCY PROCEDURES
Ed. 1, Rev. 0
AUTOPILOT EMERGENCY PROCEDURES 12
In the event of autopilot malfunction, or when the system is not per-
forming as expected or commanded, take immediately the aircraft
control disconnecting the autopilot which must be set inoperative
until the failure has been identified and corrected.
12.1 AUTOPILOT HARDOVER OR FAILURE TO HOLD THE SELECTED
HEADING
In case of A/P hardover or failure to hold selected heading, apply following pro-
cedure:
Accomplish items 1 and 2 simultaneously:
1. Airplane control wheel
GRASP FIRMLY and OVERPOWER if
necessary to regain aircraft control
2. AP DISC/TRIM INTR switch
PRESS
3. AP MASTER SWITCH
OFF
4. AP Circuit Breaker
PULL
WARNING
Following an A/P or MET system malfunction, do not engage
the autopilot until the cause of the malfunction has been cor-
rected.
When Autopilot is disconnected, it may be necessary operate the
pitch trim through either the Manual Electric Trim Switch or the
Trim Wheel.
NOTE
NOTE