Piper Arrow IV Turbo User Manual

Figure 24-2. Exploded View of Alternator (Chrysler)
Figure 24-3. Checking Field Coil Current Draw Figure 24-4. Testing Field Circuit
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EFFECTIVITY: Page 24-15
CHRYSLER ALTERNATOR Revised: July 13, 1983
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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