Hanriot H.41

__NOTOC__ Infobox Aircraft
name=H.41


caption=
type=Trainer
national origin=France
manufacturer=Hanriot
designer=
first flight=avyear|1925
introduced=
retired=
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variants with their own articles=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)

Operators

;GRE;POR

pecifications (variant)

aerospecs
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met or eng?= met

crew=Two, pilot and instructor
capacity=
length m=8.46
length ft=27
length in=9
span m=10.26
span ft=33
span in=8
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rot dia m=
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height m=3.25
height ft=10
height in=8
wing area sqm=
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volume m3=
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aspect ratio=
empty weight kg=725
empty weight lb=1,600
gross weight kg=1,000
gross weight lb=2,200
lift kg=
lift lb=

eng1 number=1
eng1 type=Salmson 9Ac
eng1 kw= 90
eng1 hp= 120
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max speed kmh=130
max speed mph=80
max speed mach=
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range km=400
range miles=250
endurance h=
endurance min=
ceiling m=3,500
ceiling ft=11,500
glide ratio=
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armament6= aircontent
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References

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