Fahlin SF-2 Plymocoupe

Length
5.1816 m
Flat Wing Span
9.7536 m
Flat Wing Area
16.5367 m²
Cruise Speed
167.3718 km/h
Max Speed
193.1213 km/h
Max Ceiling
4876.8 m
Number of Engines
1
First Flight
1935-01-01
Entry Into service
1935-01-01
Number Built
1
Total Fuel Capacity
64.352

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Aircraft Weight Variants

Aircraft Total Fuel Capacity
Fahlin SF-2 Plymocoupe 64.352

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All data (21 fields)
Name
Fahlin SF-2 Plymocoupe
Manufacturer
Swanson Aircraft Company Inc.
Description
The Fahlin SF-2 Plymocoupe was a high-wing, cantilever type, prototype experimental airplane produced in 1935.
First Flight
1935-01-01
Entry Into service
1935-01-01
Designer
Swen Swanson
Length (m)
5.1816
Max Speed (km/h)
193.1213
Cruise Speed (km/h)
167.3718
Max Ceiling (m)
4876.8
Rate of Climb (m/s)
5.08
Capacity Description
one passenger or 536 lb useful load
Endurance (h)
5
Number Built
1
Powerplant Description
1 × Plymouth 6-cyl water-cooled in-line piston engine, 60 kW (80 hp) each
Primary Users
Fahlin Aircraft Company, Russel Owen
Status
Single prototype destroyed in hangar fire in 1938
Wikipedia Article (URL)
en.wikipedia.org/wiki/Fahlin_SF-2_Plymocoupe
Flat Wing Span (m)
9.7536
Flat Wing Area (m²)
16.5367
Number of Engines
1