LKL IV
Lubelski Klub Lotniczy · Poland · first flew 1932 · light aircraft
A Polish parasol-wing two-seat club aircraft built in the early 1930s.
Recognition (WEFT)
| W — Wings | High-mounted, straight |
|---|---|
| E — Engines | 1 × piston, nose-mounted |
| F — Fuselage | Parasol wing above the fuselage |
| T — Tail | Conventional |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- Parasol wing above the fuselage
- Two-seat club aircraft
- Single tractor engine of 85 hp
A parasol-wing monoplane with the wing carried above the fuselage and a single tractor engine.
Specifications
- The LKL IV has a length of 7.12 m (23 ft).
- It has a wingspan of 11.6 m (38 ft).
- Its maximum speed is 158 km/h (98 mph).
- Typical crew: 1.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
The LKL IV first flew in autumn 1932 and was built by the Lubelski Klub Lotnitczy.
Variants
It was very similar to the LKL V, differing primarily in the engine. Only one LKL IV was built.
Where you'll see it
It was a two-seat club aircraft.
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