Piper Arrow PA-28R-201 Pilot Operating Handbook page 329

PILOT'S
AIRPLANE
Piper models PA-28R-201
CONTROL WHEEL
The left grip of the pilot's control wheel will normally contain the following
autopilot switches:
•
Manual
•
Trim Interrupt/A/P Disconnect Switch
Control Wheel
If the optional co-pilot switch arrangement
switches with the same functions will be installed in the right grip of the copilot's
control wheel.
copilot's
ELECTRIC TRIM
The S-TEC
ElectricTrim System
either mechanical
during operations in the Manual
the system
is designed to limit the effect of any
operation. hi order to assure proper operation of these safeguards, it is
necessary to conduct a simple pre-flight testof the system. Following is a
brief description and a preflight test procedure for the trim system.
FAA/DAS APPROVED
P/N: 892033
DATE: 5-16-00
HB-PQY, Page: 9-76-(6)
S-TEC CORPORATION
MINERAL
WELLS,
FAAIDAS APPROVED
OPERATING HANDBOOK
FLIGHT MANUAL
FOR
SWITCHES
ElectricTrim
Steering (CWS)
SYSTEM
is designed to accept any single failure,
or electrical, without uncontrolled operation resulting
ElectricTrim Mode.
Page 6 of 11
TEXAS 76067
AND/OR
SUPPLEMENT
and PA-28R-201T
is installed, the same
During autotrim mode
failure causing trim
Issued: MAY 16, 2000
three
S_TEC 6 of 11