Piper TURBO ARROW III User 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 TURBO ARROW III Specifications

General

Manufacturer	Piper Aircraft
Model	Turbo Arrow III
Horsepower	200 hp
Max Takeoff Weight	2, 900 lbs
Fuel Capacity	72 gallons
Service Ceiling	20, 000 ft
Seating Capacity	4
Type	Single-engine piston
Propeller	Constant-speed
Landing Distance	1, 200 ft