<!-- This article is a part of Wikipedia:WikiProject Aircraft. Please see Wikipedia:WikiProject Aircraft/page content for recommended layout. -->
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.
|prime units?=met
<!--
General characteristics
-->
|crew=2
|capacity=
|length m=6.87
|length note6=
|span m=9.8
|span note=
|height m=2.5
|height note=
|wing area sqm=
|wing area note=
|aspect ratio=<!-- sailplanes -->
|airfoil=
|empty weight kg=467
|empty weight note=
|gross weight kg=760
|gross weight note=
|max takeoff weight kg=
|max takeoff weight note=
|fuel capacity=
|more general=
<!--
Powerplant
-->
|eng1 number=1
|eng1 name=Renault 4Pb
|eng1 type=4-cylinder air-cooled in-line piston engine
|eng1 hp=95
|eng1 note=
|prop blade number=2
|prop name=fixed-pitch propeller
|prop dia m=<!-- propeller aircraft -->
|prop dia note=
<!--
Performance
-->
|max speed kmh=180
|max speed note=
|cruise speed kmh=
|cruise speed note=
|stall speed kmh=
|stall speed note=
|never exceed speed kmh=
|never exceed speed note=
|range km=400
|range note=
|ferry range km=
|ferry range note=
|endurance=<!-- if range unknown -->
|ceiling m=
|ceiling note=
|climb rate ms=
|climb rate note=
|time to altitude=
|wing loading kg/m2=51
|wing loading note=
|fuel consumption kg/km=
|power/mass=
|more performance=
References
External links
<!--dead link*Aerofred - Abraham Iris-->