Fokker Super Universal
Fokker · United States · first flew 1928 · transport aircraft
The Fokker Super Universal was an improved single-engine high-wing transport built by the Atlantic Aircraft Corporation (Fokker's American subsidiary) from 1927, designed for airline and bush operations across North America.
Recognition (WEFT)
| W — Wings | High-mounted, straight |
|---|---|
| E — Engines | 1 × piston, nose-mounted |
| F — Fuselage | 11.25 m fuselage |
| T — Tail | Conventional |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- Late 1920s high-wing American-built Fokker transport
- Single radial engine, thick cantilever wing
- Enclosed cabin for 6-8 passengers on fixed undercarriage
Classic high-wing Fokker layout: thick cantilever wooden wing above a fabric-covered steel-tube fuselage, single radial engine, fixed spatted undercarriage, and an enclosed passenger cabin.
Specifications
- The Fokker Super Universal has a length of 11.25 m (37 ft).
- It has a wingspan of 15.44 m (51 ft).
- Its maximum speed is 222 km/h (138 mph).
- Typical crew: 1 pilot + 6-8 passengers.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
Atlantic Aircraft built the Super Universal as a development of the Fokker Universal, featuring a more powerful Pratt & Whitney Wasp engine and enlarged cabin. It was used by airlines including Canadian and US regional carriers, and served extensively as a bush aircraft in northern Canada and Alaska. The type was widely operated through the late 1920s and early 1930s.
Variants
The Super Universal was an enlarged development of the Universal; some aircraft were fitted with floats or skis for northern operations.
Where you'll see it
Operated by numerous North American airlines and bush operators; some examples served in the Canadian North well into the 1930s.
Related aircraft
- Fokker C.VII-W
- Fokker C.VIII
- Fokker D.XVI
- Fokker F.IX
- Beardmore Inflexible
- BFW M.20
- Boeing Model 95
- CAMS 53
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