Hanriot H.35

Hanriot H.35
General information
Type	Intermediate training monoplane
National origin	France
Manufacturer	Avions Hanriot
Number built	12+

The Hanriot H.35 was a 1920s French intermediate training monoplane designed and built by Avions Hanriot. ^{[1] [2]}

Design and development

Hanriot H.36 photo from L'Aéronautique January,1926

The H.35 was developed from the earlier H.34 basic trainer and was a two-seat strut-braced parasol monoplane. ^[1] The H.35 was powered by a 180 hp (134 kW) Hispano-Suiza 8Ab piston engine. ^[2] Twelve aircraft were built for use with the Hanriot flying school and also the Societe Francaise d'Aviation at Orly. ^[2]

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. ^[2] An order for 50 H.36s was placed by Yugoslavia. ^[2]

another view of the H.35

Specifications (H.35)

Data from ^[2] Illustrated Encyclopedia of Aircraft

General characteristics

• Crew: 2
• Length: 7.60 m (24 ft 11.25 in)
• Wingspan: 11.39 m (37 ft 4.5 in)
• Height: 2.70 m (8 ft 10.25 in)
• Wing area: 22.00 m² (236.81 sq ft)
• Empty weight: 680 kg (1,499 lb)
• Gross weight: 945 kg (2,083 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, 100 kn)
• Range: 320 km (199 mi, 173 nmi)
• Service ceiling: 5,000 m (16,405 ft)

References

Notes

1. "Hanriot". Flight : 26–49. 2 December 1926.
2. Orbis 1985, p. 2080
3. note the mis identification in the title- from original caption in magazine

Bibliography

• The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.