Junkers K 53
AB Flygindustri (Junkers licence) · Sweden · first flew 1926 · light aircraft
The Junkers K 53 was a single-engine military trainer and light utility aircraft built under Junkers licence by AB Flygindustri in Sweden, featuring the characteristic Junkers all-metal corrugated construction.
Recognition (WEFT)
| W — Wings | Low-mounted, straight |
|---|---|
| E — Engines | 1 × piston, nose-mounted |
| F — Fuselage | 9.2 m fuselage |
| T — Tail | Conventional |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- Swedish-built Junkers licence design with corrugated metal skin
- Single-engine low cantilever wing trainer/light utility
- Part of Junkers' export and licence production strategy
Corrugated Junkers metal skin, thick low cantilever wing, and single engine cowling are consistent family identifiers shared with other Junkers types of the period.
Specifications
- The Junkers K 53 has a length of 9.2 m (30 ft).
- It has a wingspan of 13.3 m (44 ft).
- Its maximum speed is 170 km/h (106 mph).
- Typical crew: 2.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
Produced in Sweden to circumvent the post-WWI restrictions placed on German aviation production under the Versailles Treaty, the K 53 was part of Junkers' strategy of establishing foreign licensed production facilities.
Variants
Variant designations are unclear given the licence production context.
Where you'll see it
Supplied to small export customers; details of operator nations are not well documented.
Related aircraft
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