Fokker F.II
Fokker · Netherlands · first flew 1919 · airliner
The Fokker F.II was Anthony Fokker's first airliner, and one of the earliest clean cantilever high-wing monoplane designs to enter commercial service.
Recognition (WEFT)
| W — Wings | High-mounted, straight |
|---|---|
| E — Engines | 1 × piston, nose-mounted |
| F — Fuselage | Welded steel-tube fuselage under fabric covering |
| T — Tail | Conventional |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- High-wing cantilever monoplane with a thick, strut-free wood wing
- Cramped four-seat cabin behind a single tractor engine
- Welded steel-tube fuselage under fabric covering
Spot the thick, strut-free wood wing sitting directly on the fuselage roof, with only a single engine and a tiny four-seat cabin, unlike the later trimotor F.VII.
Specifications
- The Fokker F.II has a length of 11.65 m (38 ft).
- It has a wingspan of 16.1 m (53 ft).
- Its maximum speed is 150 km/h (93 mph).
- Typical crew: 1.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
First flown in 1919, the F.II grew out of Reinhold Platz's wartime Fokker fighter designs, translating their thick cantilever wooden wing and steel-tube fuselage into a small four-passenger transport. Most of the roughly 23 built were assembled by Deutsche Aero Lloyd in Berlin using wings supplied by Albatros.
Variants
The related F.III followed almost immediately with a slightly larger cabin, and the type set the high-wing, strut-free layout Fokker would use through the F.VII series.
Where you'll see it
KLM and other early European airlines flew the F.II on pioneering scheduled routes in the early 1920s; no complete original airframe survives today.
Related aircraft
- Fokker A.300
- Fokker S.I
- Fokker V.40
- Fokker C.I
- de Havilland DH.16
- Farman F.60 Goliath
- Farman F.61 Goliath
- Farman F.68 Goliath
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