Piper ARROW III Service Manual

NOTE
In the event of wing heaviness during flight, the flap on the side of the
heavy wing can be adjusted down from neutral to remedy this condition by
lengthening the control rod. Check the inspection hole in each rod end to
ascertain that there are sufficient threads remaining and a wire cannot be
inserted through these holes. Rod ends without check holes, maintain a
minimum of .375 of an inch thread engagement. Do not raise the flap of the
other wing above neutral.
Figure 5-18. Fabricated Aileron Bellcrank Rigging Tool
Revised: 2/13/89
1G16
* CHEROKEE ARROW III SERVICE MANUAL
SURFACE CONTROLS

Piper ARROW III Specifications

General

Manufacturer	Piper Aircraft
Model	ARROW III
Engine	Lycoming IO-360-C1C6
Horsepower	200 hp
Maximum Takeoff Weight	2, 750 lb (1, 247 kg)
Seating Capacity	4
Propeller	2-blade, constant speed
Length	24 ft 7 in (7.49 m)