Piper ARROW III Service Manual

TABLE II-I. LEADING PARTICULARS AND PRINCIPAL DIMENSIONS (cont.)
MODEL PA-28R-201 PA-28R-201T
LANDING GEAR (cont.)
Turning Radius (Min):
Nose Wheel 15 ft. 8.4 in. 15 ft. 8.4 in.
Wing Tip 29 ft. 9.6 in. 29 ft. 9.6 in.
Wheel Nose Cleveland 40-77B or Cleveland 40-77B or
McCauley D-30500, 5:00 x 5 McCauley D-30S00, 5:00 x 5
Wheel Main Cleveland 40-84, Cleveland 40-84,
6:00 x 6 6:00 x 6
Brake Type Cleveland 30-55 Cleveland 30-55
Tires, Nose 5 :00 x 5, 4 ply rating 5 :00 x 5, 4 ply
rating
Tires, Main 6:00 x 6, 6 ply 6:00 x 6, 6 ply
rating rating
Tire Pressure, Nose 27 PSI 27 PSI
Tire Pressure, Main 30 PSI 30 PSI
FUEL SYSTEM
Fuel Tanks:
Capacity (each) 38.5 gal. 38.5 gal.
Unusable Fuel (each) 2.5 gal. 2.5 gal.
Total Capacity 77 gal. 77 gal.
Total Unusable Fuel (Refer to Owner’s
Handbook, Pilot’s Information
Manual or Flight Manual for
Particular Airplane) 5 gal. 5 gal.
OVERALL
Gross Weight (lbs.) 2750 2900
Wing Loading (lbs/sq. ft.) 16.2 17.0
Length Ft. 24 ft. 8.25 in. 25 ft. 0.23 in.
Width (Span) (Wing Tip to Wing Tip) 35 ft. 5.11 in. 35 ft. 5.11 in.
Height (Static Ground Line) 7 ft. l 0.22 in. 7 ft. l 0.22 in.
Height, Propeller Hub, Thrust
Line Level 47.64 in. 46.64 in.
Clearance, Propeller Tips, Norrnal
Static Load 10.40 in. 8.20 in.
Clearance, Propeller Tips, Nose
Strut and Tire Flat 5.47 in. 3.15 in.
Revised 12/11/78
1B2
*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)