After its return to Hanriot's Bourges factory, the H.110
was fitted with a redesigned fuselage nacelle and an
uprated Hispano-Suiza 12Xbrs engine offering 690hp.
A 33mm APX cannon was mounted in a bulged housing
beneath the central nacelle and a four-bladed propeller
supplanted the three-blader. With these modifications,
the fighter re-emerged as the H.115 and was
flown for the first time in April 1934. Further modifications
were undertaken by the factory from November
1934, and, in June 1935, the H.115 was submitted to
Villacoublay for official evaluation. Flight testing ended
on 16 August. At this time it was concluded that, in
view of its radical configuration, the H.115 was of no
more than academic interest.
| Take-off weight||1786 kg||3937 lb|
| Empty weight||1428 kg||3148 lb|
| Wingspan||13.50 m||44 ft 3 in|
| Length||7.60 m||25 ft 11 in|
| Height||2.69 m||9 ft 10 in|
| Wing area||24.00 m2||258.33 sq ft|
| Max. speed||390 km/h||242 mph|
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