Piper ARROW III Service Manual

TABLE II-I. LEADING PARTICULARS AND PRINCIPAL DIMENSIONS (cont.)
MODEL PA-28R-201 PA-28R-201T
ENGINE (cont.)
Starter - Prestolite (12-volt) MZ4206 MCL-6501
Alternator:
Chrysler (60 AMP) 2642997
Prestolite (60 AMP) ALY-6422
Prestolite (65 AMP) ALX-9425A
Alternator Voltage Regulator, WICO X16300B X16300B
Alternator Overvoltage Relay, WICO X16799B X16799B
PROPELLER - Constant Speed
Manufacturer McCauley or Hartzell Hartzell
Hub, Model B2D34C213 HC-C2YK-1( ) F BHC C2YF-1-BF
Blade, Model 90DHA-16 F7666A-2R F8459A-8R
Diameter (in.) 74.0 74.0 76.0
Diameter, Minimum (in.) 73.0 72.5 75.0
Blade Angle, Low Pitch* 12.5° ± 0.2° 14.0° ± 0.2° 14.4° ± 0.2°
Blade Angle, High Pitch* 29.8° ± 0.5° 29° ± 2° 29° ± 1.0°
Governor Control and Model Hartzell F-2-7 (AZ) Hartzell E-5 or
Woodward G210681
*Measured at 30 inch station.
LANDING GEAR
Type Hydraulically Hydraulically
Retractable Retractable
Shock Strut Type Combination Air-Oil Combination Air-Oil
Fluid Required (Struts, Hydraulic
System and Brakes) MIL-H-5606A MIL-H-5606 A
Strut Exposure (Exposure under
Static Load):
Nose 2.75 ± .25 in. 2.75 ± .25 in.
Main 2.00 ± .25 in. 2.00 ± .25 in.
Wheel Tread 10 ft. 5.72 in. 10 ft. 5.72 in.
Wheel Base 7 ft. 10.38 in. 7 ft.10.38 in.
Nose Wheel Travel 30° ± 2° left and right 30° ± 2° left and right
Revised: 12/11/78
1B1
*CHEROKEE ARROW III SERVICE MANUAL
HANDLING AND SERVICING

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)