Engine; Propeller; Fuel - Piper Archer III PA-28-181 Handbook

PA-28-181, ARCHER III

1.5 ENGINE

(a) Number of Engines
(b) Engine Manufacturer
(c) Engine Model Number
(1) Fuel Injected
(d) Takeoff Power (BHP)
(e) Takeoff Power Engine
Speed (RPM)
(f) Bore (inches)
(g) Stroke (inches)
(h) Displacement (cubic inches)
(i) Compression Ratio
(j) Engine Type

1.7 PROPELLER

(a) Number of Propellers
(b) Propeller Manufacturer
(c) Model
(d) Number of Blades
(e) Propeller Diameter (inches)
(1) Maximum
(2) Minimum
(f) 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, 2017
Four Cylinder, Direct Drive,
Horizontally Opposed with Fuel Injection
100 Green or 100LL Blue
SECTION 1
GENERAL
Lycoming
IO-360-B4A
180
2700
5.125
4.375
361.0
8.5:1
Sensenich
76EM8S14-0-62
Fixed Pitch
Aviation Grade
REPORT: VB-2749
1
1
2
76
76
50
48
1-5