Piper ARROW III Service Manual

TABLE VIII-II. ENGINE DATA
Model (Teledyne Continental) TSIO-360F or TSIO-360FB
Type Certificate Number E9CE
Number of Cylinders 6 Horizontally Opposed
Bore (Inches) 4.44
Stroke (Inches) 3.88
Displacement (Cubic Inches) 360
Compression Ratio 7.5:1.
Type of Propeller Drive, Flanged Direct
Rated Horsepower at Sea Lever, 2575 rpm 200
Fuel, Minimum Octane 100/130 or 100LL
Oil Sump Capacity 8 quarts
Oil Pressure (PSI): @ Max. Continuous Horsepower
Minimum 30
Normal 30-60
Maximum *80
Oil Temperature (°F): @ Max. Continuous Horsepower
Minimum 100
Normal (Desired) 160-200
Maximum 240
Probe Location Above Oil Filter Element
Cylinder Head Temperature (°F)
No. 2 cyl.: @ Max. Continuous Horsepower
Minimum 240
Normal (Desired) 300-400
Maximum 460
Magnetos Bendix 25 Series
Left Bank Fires 20° BTC Lower Right, Upper Left
Right Bank Fires 20° BTC Lower Left, Upper Right
Firing Order:
TSIO-360F and TSIO-360FB 1-6-3-2-5-4
Spark Plugs (Shielded) AC, SR86, S86R, HSR86
Auto Lt. PH26, PH260
Champ. REM38W, RHM38W, PHM38EP
RHM38E, REM38E, REM38P
Red Seal. SE270, SE270P
SJ270, SJ270P
Torque 360 to 420 inch-pounds
Alternator 12-volt, 65 ampere
Starter 12-volt, Prestolite
Engine Dry Weight With Accessories (Approx.) 393 pounds
Turbocharger
*WARNING - OPERATION OF ENGINE AT TOO HIGH AN RPM BEFORE REACHING OIL TEMPERATURE MAY CAUSE LOSS
OF OIL PRESSURE.
Revised: 2/13/89
2A21
CHEROKEE ARROW III SERVICE MANUAL
POWER PLANT - CONTINENTAL

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)