Jodel D11

D.11
SAN Jodel D117
Role Trainer/tourer
Manufacturer Jodel and others
Designer Jean Délémontez
First flight 1950
Developed from Jodel D9

The Jodel D11 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.

Contents

History

Designers Édouard Joly and Jean Délémontez based the design on two of their earlier projects; they combined the wing of the D10 with a lengthened and widened version of the D9 fuselage. The first example flew on 4 April 1950. Of conventional taildragger configuration, the D11 featured fixed, spatted undercarriage, and accommodated pilot and passenger side-by-side. The wing panels outboard of the landing gear struts had a marked dihedral. Various powerplants were installed, typically Salmson 9, Continental A65 or Continental C90.

D11s were licence-built by a number of manufacturers in Europe and elsewhere, including Wassmer, Aero Difusión, and Falconar. Many examples were also home-built with plans provided by Falconar.[1]

Variants

by Aero Difusión

Specifications (typical D11 with Continental O-200 engine)

Data from {name of first source}

General characteristics

Performance

See also

Aircraft of comparable role, configuration and era

References

  1. ^ "Ceasarian Jodel". Sport Aviation. January 1971. 
  2. ^ Air Trails: 8. Winter 1971. 

External links