Leading Particulars And Principal Dimensions - Piper ARROW III Service Manual

TABLE II-I. LEADING PARTICULARS AND PRINCIPAL DIMENSIONS
MODEL
ENGINE
Manufacturer
Model
FAA Type Certificate
Rated Horsepower
Rated Speed:
Full Throttle
Propeller Drive Ratio
Propeller Shaft Rotation
Bore
Stroke
Displacement
Compression Ratio
Weight (with starter and alt.)
Dimensions:
Height
Width
Length
Oil, SAE Number
Oil Sump Capacity
Oil Consumption, Maximum
Fuel, Aviation Grade, Minimum
and Specified Octane
Fuel Injector
Magnetos, Bendix:
Left
Right
Magneto Drive, Ratio to Crankshaft
Magneto Drive, Rotation
Magneto Timing
Magneto Point Clearance
Spark Plugs (Shielded):
Spark Plug Gap Setting
Firing Order
Revised 12/11/78
*CHEROKEE ARROW III SERVICE MANUAL
PA-28R-201
Lycoming
IO-360-CIC6
200
2700 RPM
1:1
Clockwise
5.125 in.
4.375 in.
361 cu. in.
8.7:1
328 lbs.
19.48 in.
34.25 in.
33.65 in.
See Table II-III
8 U.S. quarts
.010 lb/bhp/hr
100/130 or 100LL
Bendix
S4LN-1227
S4LN-1209
1:1
Clockwise
25° BTC
.016
Refer to latest
Lycoming Service
Instruction 1042
0.015 to 0.021
1-3-2-4
1A24
PA-28R-201T
Continental
TSIO-360-F
200
2575 RPM @ 41.0 in. Hg
Manifold Pressure
1:1
Clockwise
4.438 in.
3.875 in.
360 cu. in.
7.5:1
393 lbs.
31.38 in.
57.08 in.
See Table II-III
8 U.S. quarts
.009 above 75% power
100/ 130 or 100LL
Continental
10-79020-18L
10-79020-19L
1.5:1
Clockwise
20° BTC
.018
Refer to latest
Continental Service
Bulletin M77-10
.015 to .019
1-6-3-2-5-4
HANDLING AND SERVICING