Piper ARROW III Service Manual

TABLE II-I. LEADING PARTICULARS AND PRINCIPAL DIMENSIONS
MODEL PA-28R-201 PA-28R-201T
ENGINE
Manufacturer Lycoming Continental
Model IO-360-CIC6 TSIO-360-F
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, SAE Number See Table II-III See Table II-III
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
Right S4LN-1209 10-79020-19L
Magneto Drive, Ratio to Crankshaft 1:1 1.5:1
Magneto Drive, Rotation Clockwise Clockwise
Magneto Timing 25° BTC 20° BTC
Magneto Point Clearance .016 .018
Spark Plugs (Shielded): Refer to latest Refer to latest
Lycoming Service Continental Service
Instruction 1042 Bulletin M77-10
Spark Plug Gap Setting 0.015 to 0.021 .015 to .019
Firing Order 1-3-2-4 1-6-3-2-5-4
Revised 12/11/78
1A24
*CHEROKEE ARROW III SERVICE MANUAL
HANDLING AND SERVICING

Piper ARROW III Specifications

General

Manufacturer	Piper Aircraft
Model	ARROW III
Engine	Lycoming IO-360-C1C6
Horsepower	200 hp
Maximum Takeoff Weight	2, 750 lb (1, 247 kg)
Seating Capacity	4
Propeller	2-blade, constant speed
Length	24 ft 7 in (7.49 m)