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Piper Arrow IV Turbo User Manual

Piper Arrow IV Turbo
752 pages
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Figure 24-12. Testing Stator Figure 24-13. Removal of Pulley
Figure 24-14. Removal of Bearing Figure 24-15. Removal of Rectifier
End Shield Bearing
24-32-11
EFFECTIVITY: Page 24-21
CHRYSLER ALTERNATOR Revised: July 13, 1983
1I16
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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