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Piper Arrow IV Turbo User Manual

Piper Arrow IV Turbo
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Figure 61-4. Propeller Controls
4. With the high RPM adjustment complete, the control system should be adjusted so that the governor
control arm will contact the high RPM stop when the cockpit control knob is .032 to .047 of an inch from its
full forward stop. To adjust the control knob travel, disconnect the control cable end from the control arm;
loosen the cable end jam nut and rotate the end to obtain the desired level clearance. Reconnect the cable end
and tighten jam nut. (Lower cowl must be removed to accomplish this adjustment.)
5. It is usually only necessary to adjust the high RPM (low pitch) setting of the governor control system,
as the action automatically takes care of the positive low RPM (high pitch) setting.
Effectivity 61-20-03
PA-28RT-201T Page 61-07
Revised: December 6, 1979
3B2
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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