Military Wiki
Levente I - II; Strucc
Role trainer and liaison aircraft
Manufacturer Repülőgépgyár Rt.
Designer András Fábián
First flight October 1940
Introduction 1943 (II)
Retired 1950s
Primary user Hungarian Air Force
Produced 1942-1943 (II)
Number built 100

The Levente series was a Hungarian two-seat trainer and liaison aircraft from World War II.

Design and development

Two prototypes, designed by András Fábián, (Fábián András) were built in Magyar Waggon - és Gépgyár Rt. (Hungarian Wagon and Machine Factory; one of the few big corporates of the time) in Győr. However, a tender was placed by the air forces with the profile change of the MWG, and production rights were eventually given to the Uhry brothers' factory (originally a small private vehicle body manufacturer, which later expanded rapidly and become a very successful competitor of elder corporations). The parasol-wing, two-seat primary trainer Levente I prototype flew in October 1940. A slightly modified military version of the aircraft was named the Levente II. In 1942, the Uhri Testvérek Autókarosszéria - és Járműgyár Kft. (Uhry Brothers Car-body and Vehicle factory Ltd.) launched a new company, Repülőgépgyár Rt. (roughly meaning Aeroplane factory jsc.) at Csepel island off the Danube, south of Budapest; renting the airfield and factory halls form Weiss Manféd Rt. The Levente II was being series produced, but the plant also repaired Bü 131s, and built prototype aircraft.

Operational history

Levente II was supplied to the Hungarian Air Force between 1941 and 1943. 100 Levente IIs were built as trainers, but as it was war, they also served in the communications/liaison roles until the end of the war. After 1945 the type was redesignated to the name Strucc (ostrich), because of the political connotations of the former name (see Levente (disambiguation))



Specifications (Levente II)

Data from Axis Aircraft of World War II

General characteristics

  • Crew: 1
  • Capacity: 1
  • Length: 6.08 m (19 ft 11 in)
  • Wingspan: 9.45 m (31 ft 00 in)
  • Height: 2.53 m (8 ft 3½ in)
  • Wing area: 13.50 m² (145.32 ft²)
  • Empty weight: 470 kg (1,036 lb)
  • Loaded weight: kg (lb)
  • Useful load: kg (kg)
  • Max. takeoff weight: 750 kg (1,654 lb)
  • Powerplant: 1 × Hirth HM 504A-2 4-cylinder inverted inline piston, 78 kW (105 hp)105 PS


  • Never exceed speed: km/h (knots, mph)
  • Maximum speed: 160 km/h (knots, 99 mph)
  • Cruise speed: km/h (knots, mph)
  • Stall speed: km/h (knots, mph)
  • Range: 650 km (nm, 404 mi)
  • Service ceiling: 4,500 m (14,765 ft)
  • Rate of climb: m/s (ft/min)
  • Wing loading: kg/m² (lb/ft²)
  • Power/mass: W/kg (hp/lb)

See also


Mondey, David (1984, reprinted 1987). The Consise Guide to Axis Aircraft of World War II. Aerospace Publishing Ltd. ISBN 1-85152-966-7. (In Hungarian language.)

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