Piper ARCHER III - Engines; Propellers; Fuel

1.3 ENGINES
(a) Number of Engines 1
(b) Engine Manufacturer Lycoming
(c) Engine Model Number O-360-A4M
(d) Takeoff Power (BHP) 180
(e) Takeoff Power Engine
Speed (RPM) 2700
(f) Bore (inches) 5.125
(g) Stroke (inches) 4.375
(h) Displacement (cubic inches) 361.0
(i) Compression Ratio 8.5:1
(j) Engine Type Four Cylinder, Direct
Drive, Horizontally
Opposed, Air Cooled
1.5 PROPELLERS
(a) Number of Propellers 1
(b) Propeller Manufacturer Sensenich
(c) Model 76EM8S14-0-62
(d) Number of Blades 2
(e) Propeller Diameter (inches)
(1) Maximum 76
(2) Minimum 76
(f) Propeller Type Fixed Pitch
1.7 FUEL
AVGAS ONLY
(a) Fuel Capacity (U.S. gal.) (total) 50
(b) Usable Fuel (U.S. gal.) (total) 48
(c) Fuel
(1) Minimum Octane 100 Green or 100LL Blue
Aviation Grade
(2) Alternate Fuel Refer to latest issue of
Lycoming Instruction No. 1070.
1.3 ENGINES
(a) Number of Engines 1
(b) Engine Manufacturer Lycoming
(c) Engine Model Number O-360-A4M
(d) Takeoff Power (BHP) 180
(e) Takeoff Power Engine
Speed (RPM) 2700
(f) Bore (inches) 5.125
(g) Stroke (inches) 4.375
(h) Displacement (cubic inches) 361.0
(i) Compression Ratio 8.5:1
(j) Engine Type Four Cylinder, Direct
Drive, Horizontally
Opposed, Air Cooled
1.5 PROPELLERS
(a) Number of Propellers 1
(b) Propeller Manufacturer Sensenich
(c) Model 76EM8S14-0-62
(d) Number of Blades 2
(e) Propeller Diameter (inches)
(1) Maximum 76
(2) Minimum 76
(f) Propeller Type Fixed Pitch
1.7 FUEL
AVGAS ONLY
(a) Fuel Capacity (U.S. gal.) (total) 50
(b) Usable Fuel (U.S. gal.) (total) 48
(c) Fuel
(1) Minimum Octane 100 Green or 100LL Blue
Aviation Grade
(2) Alternate Fuel Refer to latest issue of
Lycoming Instruction No. 1070.
SECTION 1
PA-28-181, ARCHER III GENERAL
SECTION 1
PA-28-181, ARCHER III GENERAL
ISSUED: JULY 12, 1995 REPORT: VB-1611
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ISSUED: JULY 12, 1995 REPORT: VB-1611
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