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From Wikipedia, the free encyclopedia

H.41
Hanriot H.41 L'Aéronautique January,1926.jpg
Role Trainer
National origin France
Manufacturer Hanriot
First flight 1925

The Hanriot H.41 was a military trainer aircraft produced in France in the 1920s. It was a further development in the family of aircraft that had commenced with the HD.14 in 1920, and incorporated a number of design features that had been developed for other members of that family. Like those other aircraft, however, it was a conventional, two-bay biplane with unstaggered wings of equal span.

The H.41 used the modern engine and mixed construction developed for the HD.40 air ambulance and used them in a new design for a military trainer. The design did not prove a success, however, and only eleven were built, with three different engine types. A floatplane variant based on the HD.17 was slightly more successful, with twelve examples exported to Greece and Portugal.

Variants

H.41
Two-seat training aircraft.
H.410
version with Lorraine 5Pa engine (5 built)
H.411
version with Salmson 7Ac engine (2 built)
LH.412
version with Lorraine 5Pb engine (4 built, plus 3 converted from H.410)
HD.41H
:(Hydro) - floatplane with Salmson 9Ac engine (12 built)+ (10 built in Yugoslav Aircraft factory "Zmaj" Zemun)

Operators

Yugoslavia HD.41H
Yugoslavia HD.41H
 Greece
 Portugal
 Yugoslavia

Specifications (variant)

Data from Jane's all the World's Aircraft 1928[1]

General characteristics

  • Crew: 2
  • Length: 7.25 m (23 ft 9 in)
  • Wingspan: 10.26 m (33 ft 8 in)
  • Height: 3.13 m (10 ft 3 in)
  • Wing area: 34.9 m2 (376 sq ft)
  • Empty weight: 625 kg (1,378 lb)
  • Gross weight: 900 kg (1,984 lb)
  • Powerplant: 1 × Lorraine 5P 5-cylinder air-cooled radial piston engine, 75 kW (100 hp)
  • Propellers: 2-bladed fixed pitch propeller

Performance

  • Maximum speed: 185 km/h (115 mph, 100 kn)
  • Landing speed: 50 km/h (31 mph; 27 kn)
  • Range: 400 km (250 mi, 220 nmi)
  • Service ceiling: 3,500 m (11,500 ft)
  • Time to altitude: 1,000 m (3,300 ft) in 13 minutes
  • Wing loading: 25.8 kg/m2 (5.3 lb/sq ft)
  • Power/mass: 0.0830 kW/kg (0.0505 hp/lb)

References

  1. ^ Grey, C.G., ed. (1928). Jane's all the World's Aircraft 1928. London: Sampson Low, Marston & company, ltd. p. 104c.

Further reading

  • Isaic, Vladimir (September 1999). "L'hydroaviation français Hanriot 41: un appareil d'entraînement construit sous licence en Yugoslavie" [The Hanriot 41 Seaplane: A Trainer Constructed Under License in Yugoslavia] (in French) (78): 30–35. ISSN 1243-8650. {{cite journal}}: Cite journal requires |journal= (help)
  • Janić, Čedomir; O. Petrović (2011). Short History of Aviation in Serbia. Beograd: Aerokomunikacije. ISBN 978-86-913973-2-6.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 470.
  • World Aircraft Information Files. London: Bright Star Publishing. pp. File 896 Sheet 11.
This page was last edited on 16 April 2021, at 20:37
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