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Hanriot H.35

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Top speed
  
185 km/h

Length
  
7.6 m

Wingspan
  
11 m

Manufacturer
  
Hanriot

The Hanriot H.35 was a 1920s French intermediate training monoplane designed and built by Avions Hanriot.

Contents

Design and development

The H.35 was developed from the earlier H.34 basic trainer and was a two-seat strut-braced parasol monoplane. The H.35 was powered by a 180 hp (134 kW) Hispano-Suiza 8Ab piston engine. Twelve aircraft were built for use with the Hanriot flying school and also the Societe Francaise d'Aviation at Orly.

A 1925 development of the H.35 was the H.36 which was a twin-float equipped version powered by a 120 hp (89 kW) Salmson 9Ac piston engine. An order for 50 H.36s was placed by Yugoslavia but it is not known if any were delivered.

Specifications (H.35)

Data from Illustrated Encyclopedia of Aircraft

General characteristics

  • Crew: 2
  • Length: 7.60 m (24 ft 11¼ in)
  • Wingspan: 11.39 m (37 ft 4½ in)
  • Height: 2.70 m (8 ft 10¼ in)
  • Wing area: 22.00 m2 (236.81 ft2)
  • Empty weight: 680 kg (1499 lb)
  • Gross weight: 945 kg (2083 lb)
  • Powerplant: 1 × Hispano-Suiza 8Ab water-cooled eight-cylinder Vee piston engine, 134 kW (180 hp)

    • Performance

  • Maximum speed: 185 km/h (115 mph)
  • Range: 320 km (199 miles)
  • Service ceiling: 5000 m (16405 ft)

    • References

    Hanriot H.35 Wikipedia
    (Text) CC BY-SA