Piper ARROW III Service Manual

Figure 8-4. Propeller Blade Minor Repair
TABLE VIII-I. PROPELLER SPECIFICATIONS
Blade Angle
(l)
Low Pitch (High RPM) 14.4° ± 0.2°
High Pitch (Low RPM) 29° ± 1.0°
Propeller RPM Setting Engine Static High RPM 2575 RPM max.
Propeller Torque Limits Description Required Torque (Dry)
Spinner Bulkhead (Aft) 20-22 foot-pounds
Propeller Mounting 60-70 foot-pounds
Spinner Attachment Screws 35-40 inch-pounds
(1) MEASURED AT 30 INCH STATION.
Revised: 8/31/77
2A16
CHEROKEE ARROW III SERVICE MANUAL
POWER PLANT - CONTINENTAL

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)