- Source: Franklin O-200
The Franklin O-200 (company designation 4AC-199) was an American air-cooled aircraft engine of the early 1940s. The engine was of four-cylinder, horizontally-opposed layout and displaced 200 cu in (3 L). The power output ranged between 65 hp (48 kW) and 100 hp (75 kW) depending on variant. The O-200-5 (4ACG-199) featured a geared propeller drive.
Variants
4AC-199
O-200-1
O-200-3
O-200-7
O-200-9
4ACG-199
O-200-5
Applications
= Direct drive
=CAP-1 Planalto
CAP-5 Carioca
Aeronca Arrow
Babcock LC-11
Culver Cadet
LAR-90
XPQ-8
TDC-1 target drone
Interstate Cadet
Langley Twin
Monocoupe 90
Piasecki PV-2
Rearwin Skyranger
Sackett Jeanie
Stinson 10
Stinson L-9
Stout Skycar
= Geared drive
=Convair (Stinson) Model 103
Spratt Tilt-Wing
Goodyear Duck
Interstate Cadet
Interstate L-6
Piper PA-7 Skycoupe
Specifications (O-200-5/4ACG-199)
Data from
= General characteristics
=Type: 4-cylinder air-cooled horizontally opposed aircraft piston engine
Bore: 4.25 in (108 mm)
Stroke: 3.5 in (88.9 mm)
Displacement: 198.6 in³ (3.25 L)
Dry weight: 224 lb (102 kg)
= Components
=Cooling system: Air-cooled
= Performance
=Power output: 102 hp (76 kW) at 3,500 rpm
See also
Comparable engines
Continental O-200
Related lists
List of aircraft engines
References
Notes
Bibliography
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- Julius Robert Oppenheimer
- Kapal penjelajah kelas Alaska
- Franklin O-200
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- Benjamin Franklin
- Franklin D. Roosevelt
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