Autoflite Iiib Autopilot - Piper PA-28-181 Archer II Pilot Operating Handbook

PIPER
AIRCRAFT CORPORATION
PA-28-181,
ARCHER
II
SECTION
9
SUPPLEMENTS
SUPPLEMENT
2
AUTOFLITE
II
AUTOPILOT INSTALLATION
SECTION
1.
GENERAL
This
supplernent supplies
information
necessary
for
the operation
of
the
airplane when the optional
AutoFlite
II
Autopilot is
installed. The informa-
tion
contained
within this
supplement
is to
be
used
"as
described"
in
con-
junction with
the
complete
handbook.
This
supplement has
been
"FAA
Approved"
as
a permanent part
of
this
handbook and
must remain
in
this
handbook
at
all
times when the optional
AutoFlite
II
Autopilot is installed.
SECTION
2.
LIMITATIONS
(a)
Autopilot
use
prohibited
above 149
KIAS.
(b)
Autopilot OFF during takeoff and
landing.
SECTION
3
-
EMERGENCY
PROCEDURES
(a) In
case
of
malfunction DEPRESS and
hold Disconnect
switch
on
pilot's
control wheel.
(b)
Rocker switch on
instrument panel OFF.
(c)
Unit
rnay
be
overpowered
manually.
(d) In
climb,
cruise
or
descer,t
configuration
a
nal{unction with a
3
second
delay
in
recovery
initiation may result
in 45
bank and
180'
altitude loss.
Maximum altitude loss
measured
at
149
KIAS in
a
descent.
(e)
In
approach
conliguration
a
malfunction witlr
a
I
second
delay in
recovery
initiation
results
in
18
bank
and 10' altituds
loss.
REPORT:
VB-11.20
9-7
ISSUED: IULY 2,L979