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

SECTION 7
DESCR/OPERATION
PIPER AIRCRAFf CORPORATION
PA.28R.201, ARROW
EMERGENCY GEAR
EXTENSION LEVER
FLIGHT CONTROL CONSOLE
Figure 7-9
7.13 FLIGHT CONTROLS
Dual flight controls are provided as standard equipment. A cable system
provides actuation of the control surfaces when the flight controls are moved
in their respective directions.
The horizontal surface (stabilator) features a trim tab/servo mounted
on the trailing edge. This tab serves the dual function of providing trim
control and pitch control forces. The trim function is controlled by a trim
control wheel located on the control console between the two front seats
(Figure 7-9). Rotating the wheel forward gives nose down trim and rotation
aft gives nose up trim.
The rudder is conventional in design and incorporates a rudder trim.
The trim mechanism is a spring-loaded recentering device. The trim control
(
(
is located on the right side of the pedestal below the throttle quadrant (
(Figure 7-1), Turning the trim control clockwise results in nose right trim
and counterclockwise rotation results in nose left trim.
I
REPORT: VB·136S
'·10
ISSUED: SEPTEMBER 15, 1988
REVISED: APRIL 9, 1990