Letov Sh 4


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Letov Sh 4

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Letov Sh 4A three-view drawing (1603 x 1167)

 ENGINE1 x 220hp Hispano-Suiza 8Ba
  Take-off weight980 kg2161 lb
  Empty weight673 kg1484 lb
  Wingspan8.00 m26 ft 3 in
  Length6.58 m22 ft 7 in
  Height2.62 m9 ft 7 in
  Wing area16.43 m2176.85 sq ft
  Max. speed232 km/h144 mph
  Cruise speed200 km/h124 mph
  Rate of climb323 m/min1050 ft/min
  Range500 km311 miles
 ARMAMENT2 x 7.7mm

Barry, 11.12.2015 18:34

Developed as a replacement for the Spad S.VII and S XIII, the Sh 4 was ordered by the Czechoslovak Air Force in 1922 with deliveries of all 20 models starting in 1923. However, in 1927 the poor build quality resulted in various problems so the Sh 4 became the Sh 4 trainer. All aircraft were retired in 1928.


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