Jodel D.11

The Jodel D.11 is a French two-seat monoplane designed and developed by Société Avions Jodel in response to a French government request for a low-wing aircraft for use by the nation's many emerging flying clubs.Of conventional tailwheel configuration, the D11 featured a fixed, spatted undercarriage, and accommodated pilot and passenger side-by-side.The wing panels outboard of the landing gear struts had a marked dihedral.[2] D.11s were licence-built by a number of manufacturers in Europe and elsewhere, including Wassmer, Aero-Difusión, and Falconar Avia.[3] Data from Jane's All the World's Aircraft 1958-59 [9]General characteristics Performance
Original 1958 Uetz Jodel D-11 C/N 931-13 in midair.
A homebuilt Falconar F11-3 using plans from Falconar of Canada which were based on the Jodel D.11
Wassmer Jodel D.120A Paris-Nice
ManufacturerJean DélémontezJodel D9Falconar F11 SportymonoplaneSociété Avions JodelÉdouard JolyfuselagetailwheelspattedundercarriagedihedralSalmson 9Continental O-170Continental O-200WassmerAero-DifusiónFalconar Aviahome-builtMinié 4.DC.32Continental A65Société Aéronautique NormandeContinental C90Continental O-200-AMinié 4.DA.28Salmson 9ADrWalter Mikron IIContinental A75Salmson 5Ap.01Salmson 5Aq.01Continental C85Falconar F11Walter Uetz FlugzeugbauContinental A65-8FAirfoilNACA 23013.5Continental C90-14FDruine CondorTaylor, John W. R.DR.1050Spanish Armed ForcesEE.1 (I)EE.1 (II)E.18 (II)