Piper TURBO ARROW III User Manual

NOTES
1. IT MAY HAVE BEEN NECESSARY TO USE SPECIAL LANDING GEAR ATTACHMENT
HARDWARE DURING ASSEMBLY OF THE AIRCRAFT DUE TO MANUFACTURING
TOLERANCES. THEREFORE, SPECIAL ATTENTION SHOULD BE GIVEN WHEN
REMOVING HARDWARE TO INSPECT AND ENSURE THE SAME DIAMETER
HARDWARE IS USED UPON REASSEMBLY. STANDARD AN4 OR AN5 BOLTS ARE
REPLACED BY ALTERNATE OVERSIZED BOLTS NAS3004 OR NAS3005
RESPECTIVELY, WHEN OVERSIZED HARDWARE IS REQUIRED.
2. WHEN NEW BUSHINGS, P/N 14843-16, ARE INSTALLED, LINE BEAM l.D. TO .376/.375.
BUSHINGS TO BE PRESS FIT AND IF LOOSE ON INSTALLATION, INSTALL WITH
LOCTITE 601.
Figure 7-10. Main Gear Installation
Revised: 2/13/89
1J17
* CHEROKEE ARROW III SERVICE MANUAL
LANDING GEAR AND BRAKE SYSTEM

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