Piper ARCHER II - Section 2 - Limitations

SECTION 2 — LIMITATIONS
The
Garmin
G5
Electronic
Flight
Instrument
Pilot’s
Guide
for
Certified
Aircraft,
part
number
190-01112-12
Rev
B
(or
later
approved
revisions),
must
be
immediately
available
to
the
flight
crew
(when
G5
is
installed).
The
Garmin
G3X
Touch
Pilot’s
Guide
for
Certified
Aircraft,
part
number
190-02472-00,
Rev
A
(or
later
approved
revisions)
must
be
immediately
available
to
(he
flight
crew
(when
G3X
EFIS
system
is
installed).
This AFMS is applicable to the software versions shown below:
Software Version
Software Item (or later FAA Approved version for this STC)
G5 Software Version 5.70
G3X Software Version 8.00
A
pilot
must
be
seated
in
the
left
pilot's
seat, with
seatbell
fastened,
during
all
autopilot
operations
Do
not
use
autopilot
during
takeoff
and
landing.
The
GFC
500
AFCS
preflight
test
must
complete
successfully
prior
to
use
of
the
autopilot,
flight
director
or
manual
electric
trim.
The maximum fuel imbalance with the autopilot engaged is 10 gallons.
The
autopilot
must
be
disengaged
below
200
feet
AGL
during
approach
operations
and
below
800
feet
AGL
during
all
other
operations.
The
GFC
500
autopilot
is
approved
for
Category
1
precision
approaches
and
non-precision
approaches
only.
Autopilot
Engagement
Speed
Minimum 65 KIAS (75 MPH)
Maximum
140
KIAS
(160
MPH)
190-02291-07
Rev.
5
7
AFMS
—
GFC
500
Autopilot
in
Piper
PA-28
Series
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