Tecnam P2006T, Aircraft Flight Manual

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Page G2-7
Section 9 - Supplements
Supplement no. G2 – S-TEC Fifty Five X Autopilot for Garmin G950
3
rd
Edition, Rev. 0
Electric trim malfunction
In case of Electric Trim malfunction (either in AP Autotrim mode or when manu-
ally operated through the Manual Electric Trim Switch), apply following proce-
dure:
1. AP DISC/TRIM INTR switch
PRESS and HOLD
2. TRIM MASTER SWITCH
OFF
3. TRIM Circuit Breaker
PULL
4. AP DISC/TRIM INTR switch
RELEASE
CAUTION
When Autopilot is disconnected because of a pitch trim mal-
function, hold the control wheel firmly: it could be necessary
up to 35 pounds (15.8 daN) of force on the control wheel to
hold the airplane level.
When electric trim is disconnected, it may be necessary operate
the pitch trim through the Trim Wheel.
When electric trim is disconnected, Autopilot system can be operated
both in pitch and roll modes; nevertheless, when a pitch mode (ALT
HOLD, VS, GS) is engaged, the Autopilot will provide an annuncia-
tion whenever it is necessary to manually trim the aircraft about the
pitch axis using the Trim Wheel. Make reference to S-TEC “Pilot’s
Operating Handbook Fifty Five X”(4
th
Edition – First Revision dated
March 01, 2008 or a more updated version).
NOTE
NOTE