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Piper Arrow IV Turbo User Manual

Piper Arrow IV Turbo
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Figure 74-4. Impulse Coupling Figure 74-5. Flyweight Clearance of Impulse
Coupling
Figure 74-6. Rotor Holding Tool Installed Figure 74-7. Timing Kit Installed
Effectivity 74-11-01
PA-28RT-201T Page 74-06
December 1, 1978
3D15
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL

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Piper Arrow IV Turbo Specifications

General IconGeneral
ManufacturerPiper Aircraft
ModelArrow IV Turbo
Horsepower200 hp
Seating Capacity4
Landing GearRetractable tricycle
Range773 nautical miles
Service Ceiling20, 000 ft
Fuel Capacity72 gallons
Propeller2-blade constant speed
Max Takeoff Weight2, 900 lb (1, 315 kg)
Stall Speed (Flaps Down)55 knots
Rate of Climb1, 000 ft/min

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