1.3
ENGINES
(a)
Number of Engines
1
(b)
Engine Manufacturer
Lycoming
(c)
Engine Model Number
0-320-D2A or 0-320-D3G
(d)
Rated Horsepower
160
(e)
Rated Speed (rpm)
2700
(f)
Bore (inches)
5.125
(g)
Stroke (inches)
3.875
(h)
Displacement (cubic inches)
319.8
(i)
Compression Ratio
8.5:1
(h)
Engine Type
Four Cylinder, Direct Drive,
Horizontally Opposed, Air Cooled
1.5
PROPELLERS
(a)
Number of Propellers
1
(b)
Propeller Manufacturer
Sensenich
(c)
Model
74DM6-0-60 or
74DM6-0-58
(d)
Number of Blades
2
(e)
Propeller Diameter (inches)
(1)
Maximum
74
(2)
Minimum
72
(f)
Propeller Type
Fixed Pitch
1.7
FUEL
(a)
Fuel Capacity (U.S. gal) (total)-
50
(b)
Usable Fuel (U.S. gal) (total)
48
(c)
Fuel
(1)
Minimum Octane
100 - Green or 100 LL - Blue
Aviation Grade
(2)
Alternate Fuel
Refer to Fuel Requirements,
Section 8 - Handling, Servicing and
Maintenance - paragraph 8.1, item (b).
1.9
OIL
(a)
Oil Capacity (U.S. quarts)
8
(b)
Oil Specification
Refer to latest issue of
Lycoming Service Instruction 1014.
(c)
Oil Viscosity per Average Ambient Temp. for Starting
SINGLE
MULTI
(1)
Above 60°F
S.A.E. 50
S.A.E. 40 or 50
(2)
30°F to 90°F
S.A.E. 40
S.A.E. 40
(3)
0°F to 70°F
S.A.E. 30
S.A.E. 40 or 20W-30
(4)
Below 10°F
S.A.E. 20
S.A.E. 20W-30
ISSUED: DECEMBER 16, 1976
REPORT: VB-880
REVISED: SEPTEMBER 13, 1990
1-3
PIPER AIRCRAFT CORPORATION
SECTION 1
PA-28-161, CHEROKEE WARRIOR II
GENERAL
Summary of Contents for CHEROKEE WARRIOR II
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