DIMENSIONS.
The principal airplane dimensions are shown in Figures 6-1 and 6-2 and are listed in Chart 601.
CHART 601. LEADING PARTICULARS AND PRINCIPAL DIMENSIONS
MODEL PA-28RT-201 PA-28RT-201T
ENGINE
Manufacturer Lycoming Continental
Model IO-360-CIC6 TSIO-360-FB
FAA Type Certificate
Rated Horsepower 200 200
Rated Speed:
Full Throttle 2700 RPM 2575 RPM @ 41.0 in. Hg.
Manifold Pressure
Propeller Drive Ratio 1:1 1:1
Propeller Shaft Rotation Clockwise Clockwise
Bore 5.125 in. 4.438 in.
Stroke 4.375 in. 3.875 in.
Displacement 361 cu. in. 360 cu. in.
Compression Ratio 8.7:1 7.5:1
Weight (with starter and alt.) 328 lbs. 393 lbs.
Dimensions:
Height 19.48 in.
Width 34.25 in. 31.38 in.
Length 33.65 in. 57.08 in.
Oil Sump Capacity 8 U.S. quarts 8 U.S. quarts
Oil Consumption, Maximum .010 lb/bhp/hr .009 above 75% power
Fuel, Aviation Grade, Minimum
and Specified Octane 100/130 or 100LL 100/130 or 100LL
Fuel Injector Bendix Continental
Magnetos, Bendix:
Left S4LN-1227 10-79020-18L
1
Right S4LN-1209 10-79020-19L
1
Magneto Drive, Ratio to Crankshaft 1:1 1.5:1
Magneto Drive, Rotation Clockwise Clockwise
Magneto Timing 20° BTC 20° BTC
Magneto Point Clearance .016 .018
FOOTNOTE:
1 A pressurized magneto retrofit kit is
available. Installation of this kit
(764921v) will provide pressurized air
to the magneto, improving ignition
system operation at higher altitudes and
reducing the frequency of ignition
system maintenance.
6-10-00
Page 6-01
Revised: July 13, 1983
1B18
PIPER AIRCRAFT
PA-28RT-201 / 201T
* MAINTENANCE MANUAL
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