Engines; Propellers; Fuel; Oil - Piper CHEROKEE TURBO ARROW III 1976 Pilot Operating Handbook

PIPER AIRCRAFT CORPORATION
SECTION 1
PA-28R-201T,
CHEROKEE
TURBO ARROW HI
GENERAL
1.3 ENGINES
(a) Number of Engines
I
(b) Engine Manufacturer
Teledyne Continental
(c)
Engine Model
Number
TSIO-360-F
(d)
Rated Horsepower
200 Sea Level
to
12,000 Ft. Density Altitude
(e)
Rated Speed
(rpm)
2575
(f) Maximum Manifold Pressure (inches
mercury) 41
(g) Bore
(inches) 4.438
(h) Stroke (inches)
3.875
(i)
Displacement
(cubic
inches) 360
(j)
Compression Ratio 7.5:1
(k)
Engine
Type Six Cylinder, Direct Drive,
Horizontally Opposed, Air Cooled,
Turbosupercharged and Fuel Injected
1.5 PROPELLERS
(a)
Number of Propellers
1
(b)
Propeller Manufacturer
Hartzell
(c) Blade
Model
F8459A-8R
(d) Number
of
Blades
2
(e)
Hub Model
BHC-C2YF-lBF
(f) Propeller Diameter
(inches)
(1)
Maximum
76
(2)
Minimum
75
(g)
Propeller Type
Constant Speed,
Hydraulically Actuated
1.7 FUEL
(a)
Fuel Capacity (U.S. gal)
(total)
77
(b) Usable Fuel (U.S. gal)
(total) 72
(c)
Fuel Grade, Aviation
(1)
Minimum
Octane
100 LL
-
Blue
or
100/130
-
Green
(2)
Specified Octane
100
LL
-
Blue
or
100/130
-
Green
(3)
Alternate Fuels
Refer
to
latest revision of Continental
Service Bulletin "Fuel and Oil Grades"
1.9 OIL
(a) Oil Capacity (U.S. quarts)
8
(b)
Oil Specification
MHS-24A
(c) Oil Viscosity
SINGLE
MULTI
(1)
Above 40°F
Ambient Air (Sea Level) SAE
50
See
Teledyne
Continental
(2)
Below 40°F Ambient Air
(Sea Level)
SAE 30
TSIO-360-F Operator's
Manual
ISSUED: DECEMBER 20, 1976
REPORT:
VB-800
1-3