Tecnam P2010 - Page 224

AFMS N°D01 FOR GARMIN GFC700 AUTOPILOT INSTALLATION AND
RNAV/RNP NAVIGATION ELIGIBILITY
Page 3A-32
Section 3 – Emergency procedures
AUTOPILOT EMERGENCY PROCEDURES
Ed. 1, Rev. 0
12.2 ALTITUDE LOST DURING A PITCH AXIS AUTOPILOT MALFUNC-
TION AND RECOVERY
Following table addresses the altitude lost during a pitch axis malfunction and re-
covery for each reported flight phase:
Flight phase
Altitude loss
Climb
90 ft
Cruise
200 ft
Descent
170 ft
Maneuvering
210 ft
Approach
70 ft
12.3 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 malfunction,
hold the control wheel firmly.
When electric trim is disconnected, it is 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 “Garmin G1000
Integrated Avionic System Pilot’s Guide”for Tecnam P2010 (Part No.
190-01830-00 Revision A dated September 25, 2014 or a more updat-
ed version).
NOTE
NOTE