Arrow PA-28R-201 Pilot's Operating Handbook And Faa Approved Airplane Flight Manual page 216

SECTION 9
SUPPLEMENT 2
SECTION 1 • GENERAL
PIPER AIRCRAFT CORPORATION
PA·28R·201, ARROW
This supplement supplies infonnation necessary for the operation of the
airplane when the optional Piper Electric Pitch Trim is installed. The (
infonnation contained within this supplement is to be used in conjunction
with the complete handbook.
SECTION 2 • LIMITATIONS
No changes of the basic limitations provided by Section 2 of this Pilot's
Operating Handbook are necessary for this supplement.
SECTION 3 • EMERGENCY PROCEDURES
The following infonnation applies in case of electric trim malfunction:
(a) In case of malfunction, disconnect electric pitch trim by
activating pitch trim switch on pilot's control yoke to OFF
position.
(b) In case of emergency, electric pitch trim may be overpowered using
manual pitch trim, and/or control wheel pressure.
(c) In cruise configuration, a malfunction can result in a 20° pitch
change and 500 ft. altitude variation.
(d) In approach configuration, a malfunction can result in a 20° pitch
change and a 500 ft. altitude variation.
SECTION
4· NORMAL PROCEDURES
The electric pitch trim may be turned ON or OFF by a switch located
on the left horn of the pilot's control yoke adjacent to the trim control switch.
The pitch trim may be changed when the 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.
I
REPORT: VB·1365
9·8 2of4
ISSUED: SEPTEMBER 15, 1988
REVISED: APRIL 9, 1990
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