Piper Turbo Saratoga PA-32-301T Pilot's Manual page 308

SECTION 9 PIPER AIRCRAFT CORPORATION
SUPPLEMENTS
PA-32-301T, TURBO SARATOGA
SECTION
1
-
GENERAL
This supplement supplies information necessary for
the
operation of
the
airplane
when
the
optional King KAP/KFC 150 Series Flight Control
System is installed. The Flight Control System must be operated within
the
limitations herein specified. The information
contained
within this supple-
ment
is to be
used
in conjunction 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
King
KAP/KFC 150 Series
Flight Control System is installed.
SECTION 2
-
LIMITATIONS
(a)
During autopilot
operation,
a pilot with seat belt fastened must be
seated at
the
left pilot position.
(b)
The autopilot must be OFF during takeoff and landing.
(c)
The system is approved for Category I operation only (Approach
mode selected).
(d)
Maximum
fuel imbalance
-
12 gallons.
(e)
Autopilot airspeed limitation: Maximum 180
KIAS.
NOTE
In accordance
with FAA recommendation,
use
of
"altitude
hold" mode is not recommended
during operation in
severe
turbulence.
SECTION 3
-
EMERGENCY PROCEDURES
(a)
In
case
of
Autopilot
malfunction:
(accomplish
items 1. and 2.
simultaneously)
(1)
Airplane
Control
Wheel
-
GRASP
FIRMLY and regain
aircraft control.
(2)
AP DISC/ TRIM
INTER Switch
-
PRESS
and HOLD.
(3)
AP
DISC/ TRIM
INTER Switch
-
RELEASE
while observing
pitch
trim
wheel. If pitch
trim wheel is in motion, follow the
Electric
Trim
Malfunction
Procedure.
REPORT: VB-1070
ISSUED: AUGUST 6, 1982
9-84