Tecnam P2010, Flight Manual, Page: 216 / 587

AFMS
N°D01 FOR GARMIN GFC700 AUTOPILOT INSTALLATION AND
RNAV/RNP NAVIGATION ELIGIBILITY
Page 2A-17
Section 2 – Limitations
AUTOPILOT LIMITATIONS
Ed. 1, Rev. 1
Approved
AUTOPILOT LIMITATIONS 20
The “Garmin G1000 Pilot’s Guide for the Tecnam P2010” (Part No.
190-01830-00 Revision A dated September 25, 2014 or a more up-
dated version) must be carried in the aircraft and made available to
the pilot at all time.
Following operating limitations shall apply when the aircraft is equipped with
Garmin GFC700 Autopilot:

The Autopilot is certified for Category I – ILS Approaches [with a deci-
sion height not lower than 200 ft AGL (61 m)]

During Autopilot operation, a pilot with seat belt fastened must be seated
at the left pilot position

Maximum speed for Autopilot operation is 150 KIAS

Do not use autopilot for airspeed below 70 KIAS

Minimum approach speed is 70 KIAS

The autopilot must be OFF during takeoff and landing

Minimum altitude AGL for Autopilot operation is:
b. Cruise and Descent: 800 ft (244 m) AGL
c. Climb after Take-off: 400 ft (122 m) AGL
d. ILS CAT I precision approach: 200 ft (61 m) AGL

Use of the autopilot or manual electric trim system is prohibited before the
satisfactory completion of the Pre-flight procedure.

Autopilot USP function requires flaps indicators lights in the cockpit to be
efficient for correct operation. If one flap indicator light gets inoperative
during flight, USP function is not assured.
NOTE