Piper Arrow IV Turbo User Manual

Figure 61-6. Propeller Blade Minor Repair
CHART 6102. PROPELLER SPECIFICATIONS
Hartzell McCauley
Blade Angles
1
Low Pitch (High RPM) 14.0° ± 0.2° 12.5° ± 0.2°
High Pitch (Low RPM) 29.0° ± 2° 27.5° ± 0.5°
1
Measured at 30 inch station.
Propeller RPM Setting Engine Static High RPM 2700 RPM Max.
Propeller Torque Limits Description Required Torque (Dry)
Propeller Mounting Nuts 60-70 foot-pounds (Hartzell)
55-65 foot-pounds (McCauley)
Forward Bulkhead Attach-
ment Bolts 30-35 inch-pounds (Hartzell)
Aft Bulkhead Attachment
Bolts 50-70 inch-pounds
Spinner Attachment Screws 20-25 inch-pounds
Effectivity 61-10-02
PA-28RT-201 Page 61-10
Revised: February 23, 1979
3B5
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL

Piper Arrow IV Turbo Specifications

General

Manufacturer	Piper Aircraft
Model	Arrow IV Turbo
Horsepower	200 hp
Seating Capacity	4
Landing Gear	Retractable tricycle
Range	773 nautical miles
Service Ceiling	20, 000 ft
Fuel Capacity	72 gallons
Propeller	2-blade constant speed
Max Takeoff Weight	2, 900 lb (1, 315 kg)
Stall Speed (Flaps Down)	55 knots
Rate of Climb	1, 000 ft/min