Piper ARCHER III Pilot Operating Handbook page 19

PA-28-181, ARCHER ill
•
1.5 ENGINE
(a) Number of Engines
Engine Manufacturer
(b)
(c) Engine Model Number
(I) Fuel Injected
(d) Takeoff Power (BHP)
(e) Takeoff Power Engine
Speed (RPM)
(f) Bore (inches)
Stroke (inches)
(g)
Displacement (cubic inches)
(h)
(i) Compression Ratio
(i) Engine Type
•
1.7 PROPELLER
(a) Number of Propellers
Propeller Manufacturer
(b)
Model
(c)
Number of Blades
(d)
(e) Propeller Diameter (inches)
(I) Maximum
(2) Minimum
Propeller Type
( f)
1.9 FUEL
AVGAS ONLY
(a) Fuel Capacity (U.S. gal.) (total)
•
Usable Fuel (U.S. gal.) (total)
(b)
(c) Fuel
(1) Minimum Octane
ISSUED: December 22, 2017
REVISED: March 27, 2020
Four Cylinder, Direct Drive,
Horizontally Opposed with Fuel lnjection
100 Green or lOOLL Blue
SECTION 1
GENERAL
1
Lycoming
IO-360-B4A
180
2700
5.125
4.375
361.0
8.5: I
1
Sensenich
76EM8S14-0-62
2
76
76
Fixed Pitch
50
48
Aviation Grade
REPORT: VB-2749
1-5