Puneet Varma (Editor)

Letov Š 6

Updated on
Edit
Like
Comment
Share on FacebookTweet on TwitterShare on LinkedInShare on Reddit
Top speed
  
186 km/h

Length
  
8.85 m

Manufacturer
  
Letov Kbely

Wingspan
  
16 m

First flight
  
1923

The Letov Š-6 was a bomber aircraft produced in Czechoslovakia during the 1920s. Derived from the Š-2, it was a large biplane of conventional design. The wing cellule was an all-new design with a thicker profile, and while it had been intended to build them with a metal structure, wood was used instead due to shortages. Performance during testing was so promising that in 1924 an Š-6 was used to set a new altitude record with a 500 kg payload, and (on another occasion) a national endurance record of 10 h 32 min.

The Š-6 enjoyed a long career in Czechoslovakian service, remaining in use until 1934. One example was given a civil registration (L-BORA) and evaluated as an airliner for the Prague-Gothenburg route, but nothing came of this.

Specifications

General characteristics

  • Crew: Two
  • Length: 8.85 m (29 ft 0 in)
  • Wingspan: 15.69 m (51 ft 6 in)
  • Wing area: 43.0 m2 (462 ft2)
  • Empty weight: 1,152 kg (2,534 lb)
  • Gross weight: 2,008 kg (4,417 lb)
  • Powerplant: 1 × Maybach Mb.IV, 190 kW (260 hp)
  • Performance

  • Maximum speed: 186 km/h (116 mph)
  • Range: 780 km (490 miles)
  • Service ceiling: 6,250 m (20,500 ft)
  • Rate of climb: 2.6 m/s (520 ft/min)
  • References

    Letov Š-6 Wikipedia