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Piper Arrow IV Turbo User Manual

Piper Arrow IV Turbo
752 pages
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Figure 80-2. Turning Starting Figure 80-3. Testing Motor Armature
Motor Commutator for Shorts
Figure 80-4. Testing Motor Fields for Grounds
80-10-05
Page 80-06
December 1, 1978
3G17
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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