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Piper Arrow IV Turbo User Manual

Piper Arrow IV Turbo
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GENERAL. (PA-28RT-201)
DESCRIPTION AND OPERATION.
The S-1200 series magneto used on this engine is a completely self-contained unit featuring a rotating
magnet and a two lobe cam which operates the main breaker points. This magneto uses an impulse coupling to
provide reliable ignition at engine cranking speed. At low engine cranking speeds the impulse coupling
automatically retards the magneto until the engine is also at its retarded firing position. The spring action of the
impulse coupling is then released to spin the rotating magnet and produce the spark required to fire the engine.
When the engine is running, the impulse coupling acts as a drive coupling for the magneto.
TROUBLESHOOTING.
CHART 7402. TROUBLESHOOTING (MAGNETO)
Trouble Cause Remedy
Failure of engine to start. Defective spark plugs. Clean and adjust or replace
spark plugs.
Defective ignition wire. Check with electric tester and
replace defective wires.
Defective battery. Replace with charged battery.
Improper operation of Check points. Check internal
magneto breaker. timing of magnetos.
Failure of engine to idle Faulty ignition system. Check entire ignition system.
properly.
Low power and uneven run- Defective spark plugs. Clean and gap or replace
ning. spark plugs.
Magneto breaker points not Clean points. Check internal
working properly. timing of magnetos.
Defective ignition wire. Check wire with electric
tester. Replace defective wire.
Defective spark plug termi- Replace connectors on spark
nals connectors. plug wire.
Failure of engine to develop Faulty ignition. Tighten all connections.
full power. Check system with tester.
Check ignition timing.
Effectivity 74-02-00
PA-28RT-201 Page 74-22
December 1, 1978
3E7
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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