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Abraham Iris

General Aviation

Abraham Iris — General Aviation
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The Abraham Iris was a two-seat touring airplane produced in France in the early 1930s in two slightly different versions, the Iris I with a 75 kW (100 hp) Hispano-Suiza piston engine, and the Iris II with a Renault engine. The Iris was a conventional parasol wing monoplane with a neatly faired-in engine.

Specifications

Category
Fixed Wing
Sub-Category
General Aviation
Domain
Civil
Engine
1× 4-cylinder air-cooled in-line piston engine
Thrust / Power
95 hp
Length (ft)
23
Wingspan (ft)
32
Empty Weight (lb)
1030
MTOW (lb)
1676
Range (mi)
249
Max Speed (mph)
112