ARROW II
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) is of the flying tail design with 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. Rotating the wheel forward gives nose down trim and
rotation aft gives nose up trim. The stabilator provides extra stability and controllability with
less area, drag and weight than conventional tail surfaces.
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 quadr
a
nt. Turning the trim control clockwise gives nose right trim and
counterclockwise rotation gives nose left trim.
Ailerons are provided with differential deflection. This feature reduces adverse yaw in
turning maneuvers, and thus reducing the amount of coordination required.
Manually controlled flaps are provided. They are extended by a control cable and are
spring-loaded to the retracted (up) position. The control is located between the two front seats
on the control console. To extend the flaps pull the handle up to the desired flap setting of 10,
25 or 40 degrees. To retract, depress the button on the end of the handle and lower the control.
A balanced control system is used for light operating forces.
When extending or retracting flaps, there is a pitch change in the aircraft. This pitch change
can be corrected either by stabilator trim or increased control wheel force. When the flaps are in
the retracted position the right flap, provided with a over-center lock mechanism, acts as a step.
NOTE
The right flap will support a load only in the fully retracted (up)
position. When loading and unloading passengers make sure the
flaps are in the retracted (up) position.
AIRPLANE AND SYSTEMS
ISSUED: November 15, 1971
N16422 POH
Содержание Cherokee Arrow II
Страница 34: ...ARROW II OVERRIDE LATCH 2 4 Throttle Quadrant Console AIRPLANE AND SYSTEMS REVISED August 30 1973 N16422 POH...
Страница 37: ...AIRPLANE AND SYSTEMS ISSUED Novemoer 15 1971 Main Wheel Assembly ARROWil BRAKE HOUSING 2 7 N16422 POH...
Страница 47: ...AIRPLANE AND SYSTEMS ISSUED November 1s 1971 Static System ARROW IT 2 17 _ I N16422 POH...
Страница 52: ...ARROW II 2 22 THIS PAGE INTENTIONALLY LEFT BLANK AIRPLANE AND SYSTEMS ISSUED November 15 1971 N16422 POH...
Страница 100: ...ARROW TIDS PAGE INTENTIONALLY LEFT BLANK REPORT VB 334 PAGE S 30 MODEL PA 28R 200 l UED October 14 1971 N16422 POH...
Страница 112: ...ARROW II 6 8 THIS PAGE INTENTIONALLY LEFT BLANK OPERATING INSTRUCTIONS ISSUED November 15 1971 N16422 POH...
Страница 113: ...THJS PAGE INTENTIONALLY LEFT BLANK OPERATING INSTRUCTIONS ISSUED February 4 1972 ARROW 11 6 9 N16422 POH...
Страница 114: ...ARROWD 6 10 Tms PAGE INTENTIONALLY LEFT BLANK OPERATING INSTRUCTIONS ISSUED February 4 1972 N16422 POH...
Страница 138: ...ARROW II 9 10 THIS PAGE INTENTIONALLY LEFT BLANK a I l j I HANDLING AND SERVICING ISSUED November 15 1971 u J N16422 POH...