Piper Arrow PA-28R-201 Pilot Operating Handbook page 330

PILOT'S
AIRPLANE
Piper models PA-28R-201
TRIM
TRIM
INTRPT
UP A/P ti':
SYSTEM DESCRIPTION
The trim monitor system consistsof the components
is designed to alertthe pilot of a trim failure or trim in motion.
The system is activated by pushing the trim master switch on. A green On
light, a yellow Trim light and a red Fail light will illuminatein the switch
and the trim audio horn will activatefor one second, as a test.A trim fault
will cause the Trim and Fail lights to illuminate along with continuous horn
operation. The pilot should press and hold the red Trim Interrupt button and
conduct the emergency
PREFLIGHT TRIM
MANUAL ELECTRIC
Check trim circuit breaker
1.
Trim master switch
2.
completion of test cycle.
APPROVED
FAA/DAS
P/N:
892033
DATE: 5-16-00
HB-PQY, Page: 9-76-(7)
S-TEC CORPORATION
MINERAL
WELLS,
FAAJDAS APPROVED
OPERATING HANDBOOK
FLIGHT
MANUAL
FOR
SYSTEM WITH
ELEV.
ILPIMfi
PUSH
O ON/OFF
FIGURE
procedures listed in Section IIIof thisAFMS.
CHECK (With Trim Monitor)
Test Prior To Each Flight
TRIM
IN
Push ON
Page 7 of 11
TEXAS 76067
AND/OR
SUPPLEMENT
and PA-28R-201T
TRIM MONITOR
TRIM
TRIM
a
HORN
1
pictured in Figure 1 and
confirm green light ON
Issued: MAY 16, 2000
TRIM
C.B.
after
S_TEC 6 of 11