Autoflite Ii Autopilot Installation - Piper Turbo Saratoga PA-32-301T Pilot's Manual

PIPER
AIRCRAFT CORPORATION
SECTION 9
PA-32-301T, TURBO SARATOGA SUPPLEMENTS
SUPPLEMENT 8
AUTOFLITE II AUTOPILOT INSTALLATION
SECTION 1
-
GENERAL
This supplement must be used in conjunction with
the
FAA Approved
Airplane Flight Manual, dated
1-9-80,
when Piper AutoFlite II Autopilot,
Model
AK304 is installed in
accordance
with
STC
SA3167SW-D. The
information
contained herein supplements
the information
of the basic
Airplane
Flight
Manual;
for limitations, procedures and performance
information
not contained
in this
supplement, consult the basic Airplane
Flight
Manual.
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 operation prohibited
above 175 KIAS.
(b)
Autopilot
must be OFF
for
takeoff and landing.
SECTION 3
-
EMERGENCY PROCEDURES
(a)
In
case of malfunction,
depress interrupt
switch on pilot's control
wheel, or overpower autopilot at either control wheel.
(b)
AutoFlite II
master switch
-
OFF.
(c)
In climb, cruise or descent configuration a malfunction with a
3
second delay in recovery initiation
may
result in a 58° bank and a
300 foot
altitude loss.
(d)
In approach configuration, coupled or uncoupled; a malfunction
with
a
1 second delay in
recovery
initiation may result in a 15° bank
and a 60 foot
altitude
loss.
ISSUED: APRIL 4, 1980 REPORT: VB-1070
REVISED: MAY 16, 1980 9-27