AFMS
N"D07
FOR
GARMIN
GFC700
AUTOPILOT
AND
VARIABLE
PITCH
PROPELLER
EQUIPPED
AEROPLANES
~TEcNAM
[p~@'l]@
c
&r!IT'@~
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[1'1J&)!Ji)(!!]&)0
Page APV2-17
20
AUTOPILOT
LIMITATIONS
The
"Garmin
GlOOO
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 a/I time.
Following operating limitations shall apply when the aircraft
is
equipped
with Garmin GFC700 Autopilot:
Approved
The Autopilot is certified for Category I -
ILS
Approaches [with a
decision 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-night procedure.
Autopilot USP function requires flaps indicators lights in the cockpit to
be efficient for correct operation.
If
one flap indicator light gets in-
operative during flight, USP function
is
not assured.
Section
2 -
Limitations
AUTOPILOT
LIMITATIONS
Ed
2,
Rev. 0
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