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Piper Arrow IV Turbo User Manual

Piper Arrow IV Turbo
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2. The mixture may be adjusted as follows:
A. At the fuel injector, disconnect the clevis end of the mixture control cable from the control arm.
Loosen the jam nut that secures the clevis end.
B. Adjust the linkage by rotating the clevis end on the cable to obtain 0.010 to 0.030 of an inch spring
back on the instrument panel stop when in full rich position.
C. Reconnect the clevis end to the control arm and safety.
3. Check security of cable casing attachments.
4. Pull the throttle and mixture levers in the cockpit full aft to ascertain that the idle screw contacts its
stop and the mixture control arm contacts its lean position. A mixture control lock is incorporated in the
quadrant cover which prevents the mixture control from being moved to the idle cutoff position inadvertently.
The lock must be depressed before the control can be moved completely aft. Ascertain that the lock operates
freely without any tendency to bind or hang up.
—END—
Effectivity 73-20-01
PA-28RT-201 Page 73-16
December 1, 1978
3D5
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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