Tecnam P2006T, Aircraft Flight Manual

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Page G2-6
Section 9 - Supplements
Supplement no. G2 – S-TEC Fifty Five X Autopilot for Garmin G950
3
rd
Edition, Rev. 0
Autopilot hardover or failure to hold the selected heading
In case of Autopilot hardover or failure to hold the selected heading, apply follow-
ing procedure:
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
CAUTION
When Autopilot is disconnected as a consequence of a malfunc-
tion, hold the control wheel firmly: it may be necessary up to
35 pounds (15.8 daN) of force on the control wheel to hold the
airplane level.
When Autopilot is disconnected, it may be necessary operate
the pitch trim through either the Manual Electric Trim Switch
or the Trim Wheel.
NOTE