Piper Turbo Saratoga PA-32-301T Pilot's Manual page 317

PIPER
AIRCRAFT CORPORATION
SECTION 9
PA-32-301T, TURBO SARATOGA SUPPLEMENTS
(1l)Before Landing
AP DISC TRIM INTER Switch
-
PRESS
to
disengage AP.
(c)
FLlGHT
DlRECTOR OPERATlON
(KFC 150 SYSTEMS
ONLY)
NOTE
The flight director
modes of operation
are the
same
as those used for autopilot
operations
except
the autopilot
is not engaged and the
pilot must maneuver the aircraft to satisfy the
flight director commands.
SECTION 5
-
PERFORMANCE
No change.
SECTION 6
-
WEIGHT AND BALANCE
Factory installed optional
equipment
is included in the licensed weight
and balance data in Section 6 of the basic Pilot's Operating
Handbook.
SECTION
7
-
DESCRIPTION AND OPERATION
The 150
Series AFCS is certified in this airplane with
2
axis control,
pitch and roll. The
various instruments and the controls
for the operation of
the 150 System
are described in Figures 7-1 thru 7-15.
The 150 Series AFCS has an electric pitch trim system which provides
autotrim during autopilot operation and manual electric trim for the pilot.
The trim
system
is designed to withstand
any
single inflight malfunction.
Trim faults are visually and aurally annunciated.
A lockout
device
prevents autopilot
engagement
until the system has
been
successfully preflight tested.
ISSUED:
AUGUST 6, 1982
REPORT:
VB-1070
9-93