|Role||Intermediate training monoplane|
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.
- 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)
- Maximum speed: 185 km/h (115 mph)
- Range: 320 km (199 miles)
- Service ceiling: 5000 m (16405 ft)
- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.