Hanriot H.180

__NOTOC__ Infobox Aircraft
name=H.170, H,180, and H.190


caption=
type=Utility aircraft
national origin=France
manufacturer=Hanriot
designer=Montlaur
first flight=avyear|1934
introduced=
retired=
status=
primary user=
more users=
produced=
number built=392
variants with their own articles=The Hanriot H.170, H.180, and H.190 were a family of light utility aircraft produced in France in the 1930s. All introduced in 1934, they appeared side-by-side at the Paris Air Show that year, the model numbers distinguishing between versions powered by Salmson, Renault, and Régnier engines respectively. In basic construction, they were otherwise almost identical, as largely conventional monoplanes with high, strut-braced wings and fixed, tailskid undercarriage. The pilot and one or two passengers sat in an extensively-glazed, enclosed cabin. Although usually described as a monoplane, this family of aircraft all featured small, stub wings at the bottom of the fuselage. These carried the fuel tanks and served as a mounting point for the wing struts and undercarriage. An interesting feature was that the upper portion of the rear fuselage was a removable module, allowing it to be replaced with alternative modules for different roles, for example to carry a stretcher, or a second, open cockpit for pilot or gunnery training.

The H.182 was the major production version, accounting for 346 out of the total of 392 aircraft built. Most of these were produced as part of a government order for machines to equip the "Cercles Aériens Régionaux" reserve flying units, with 172 aircraft still operational at the Fall of France in 1940. Ten more were purchased by the Second Spanish Republic for use in the Spanish Civil War, and 50 aircraft originally ordered by the French government were diverted to Turkey as part of a military aid agreement.

Variants

H.170

* H.170 - two-seat military observation version with Salmson 6Te engine (1 built)
* H.171 - three-seat civil tourer version of H.170 (1 built)
* H.172
** H.172B - two-seat trainer (1 built)
** H.172N - three-seat tourer (7 built)
* H.173 - aerobatic trainer version (1 built)
* H.174 - three-seat trainer (1 built)
* H.175 - liaison aircraft for French Navy (10 built)

H.180

* H.180
** H.180T - three-seat tourer with Renault 4Pdi engine (1 built)
** H.180M - two-seat military observation version with Renault 4Pei engine (1 built)
* H.181 - air ambulance version of H.180T (1 built)
* H.182 - main production version as trainer aircraft for French reserve aviation units.
* H.183 - aerobatic trainer with Renault 438 engine (1 built)
* H.184 - trainer version with uprated version of Renault 4Pei engine (1 built)
* H.185 - two-seat liaison version for French navy (6 built)

H.190

* H.190
** H.190M - two-seat observation aircraft with Régnier 60-01 engine (1 built)
* H.191 - three-seat tourer (1 built)
* H.192
** H.192B - two-seat trainer (1 built)
** H.192N - two-seat civil trainer with Régnier 6Bo.1 engine (9 built)
* H.195 - two-seat liaison aircraft with Régnier 6Bo.1 engine (1 built)

Operators

;FRA
*French Navy;flag|Spain|1931;TUR

pecifications (H.182)

aerospecs
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met or eng?= met

crew=Two, pilot and instructor
capacity=
length m=7.22
length ft=23
length in=8
span m=12.00
span ft=39
span in=5
swept m=
swept ft=
swept in=
rot number=
rot dia m=
rot dia ft=
rot dia in=
dia m=
dia ft=
dia in=
width m=
width ft=
width in=
height m=3.15
height ft=10
height in=4
wing area sqm=19.0
wing area sqft=204
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=604
empty weight lb=1,331
gross weight kg=887
gross weight lb=1,955
lift kg=
lift lb=

eng1 number=1
eng1 type=Renault 4Pei
eng1 kw= 104
eng1 hp= 140
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
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eng2 kw=
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max speed kmh=190
max speed mph=120
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=600
range miles=370
endurance h=
endurance min=
ceiling m=5,500
ceiling ft=18,400
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
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armament6= aircontent
see also=
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References

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