Engine; Propeller; Fuel - Piper ARCHER III Pilot Operating Handbook

PA-28-181
ARCHER
III
SECTION
1
GENERAL
1.5 ENGINE
(a)
Number of
Engines
I
(b)
Engine
Manufacturer
Lycoming
(c)
Engine
Model
Number
(1)
Fuel
Injected
10-360-84,{
(d)
Takeoff
Power
(BHP)
180
(e)
Takeoff
Power
Engine
Speed
(RPM)
ZIOO
(0
Bore
(inches)
S.LZS
(g)
Stroke
(inches)
4.315
(h)
Displacement (cubic
inches)
361,0
(i)
Compression
Ratio
8.5:1
0)
Engine
Type
Four
Cylinder, Direct
Drive,
Horizontally
Opposed
with
Fuel Injection
1.7 PROPELLER
(a)
Number of
Propellers
(b)
PropellerManufacturer
(c)
Model
(d)
Number of
Blades
(e)
Propeller Diameter (inches)
(1)
Maximum
(2)
Minimum
(0
Propeller Type
1..9
FUEL
AVGAS ONLY
(a)
Fuel Capacity (U.S.
gal.)
(total)
(b)
Usable
Fuel (U.S. gal.) (total)
(c)
Fuel
(1)
Minimum
Octane
ISSUED:
December 22, 2Ol7
REVISED: March 27,2020
1
Sensenich
76EM8S14-0-62
2
76
76
Fixed Pitch
100 Green
or
100LL Blue
Aviation
Grade
REPORT:
VB-2749
1_5
50
48