Piper PA-28-161 Pilot Operating Handbook page 181

SECTION 9
SUPPLEMENT 1
SECTION 1 • GENERAL
PIPER AIRCRAFT CORPORATION
PA-28-161, WARRIOR.II
This supplement supplies information necessary for the operation of the
airplane when the optional Piper Electric Pitch Trim is installed. The
information contained within this supplement is to
be
used in conjunction
with the complete handbook.
SECTION 2 ·LIMITATIONS
No change.
SECTION 3- EMERGENCY PROCEDURES
(a) In case of malfunction, disconnect electric pitch trim by activating
pitch trim switch on instrument panel to OFF position.
(b) In an emergency, electric pitch trim may be overpowered using
manual pitch trim. .
(c) In cruise configuration, malfunction results in 10° pitch change
and 200 ft altitude variation.
(d) In approach configuration, a malfunction can result in a 5° pitch
change and 50 ft altitude loss.
SECTION 4 • NORMAL PROCEDURES
The electric trim system may be turned ON and OFF by a switch located
above the ignition switch: The pitch trim may be changed when tQe electric
trim system is turned on either by moving the manual pitch trim control
wheel or by operating the trim control switch on the pilot's control yoke.
SECTION 5 • PERFORMANCE
No change.
REPORT: VB-1180
ISSUED: AUGUST 13, 1982
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