D18 & D19 | |
---|---|
Jodel D18 | |
Role | Ultralight aircraft |
National origin | France |
Manufacturer | Jodel |
Status | In production |
The Jodel D18 is a French ultralight aircraft, designed and produced by Jodel. [1] [2] [3]
The original amateur-built category D18 was adapted to comply with the Fédération Aéronautique Internationale microlight rules with the addition of larger flaps and renamed the D185. Both the D18 and D185 feature a cantilever low wing, two seats in a side-by-side enclosed cockpit configuration, fixed conventional landing gear and a single engine in tractor configuration. [1] [2]
A tricycle landing gear-equipped version is designated D19 for the amateur-built category and D195 for the microlight category. [1] [2]
All the aircraft in the series are all made with a wooden structure, covered in doped aircraft fabric. The 7.50 m (24.6 ft) span wing employs polyhedral configuration with the outer wing panels exhibiting much greater dihedral. Engines used include the 85 hp (63 kW) Jabiru 2200 four-stroke powerplant as well as Rotax, Limbach Flugmotoren and 58 hp (43 kW) Volkswagen 1600 automotive engines. [1] [2] [3]
Data from Bayerl [1]
General characteristics
Performance
D18 & D19 | |
---|---|
Jodel D18 | |
Role | Ultralight aircraft |
National origin | France |
Manufacturer | Jodel |
Status | In production |
The Jodel D18 is a French ultralight aircraft, designed and produced by Jodel. [1] [2] [3]
The original amateur-built category D18 was adapted to comply with the Fédération Aéronautique Internationale microlight rules with the addition of larger flaps and renamed the D185. Both the D18 and D185 feature a cantilever low wing, two seats in a side-by-side enclosed cockpit configuration, fixed conventional landing gear and a single engine in tractor configuration. [1] [2]
A tricycle landing gear-equipped version is designated D19 for the amateur-built category and D195 for the microlight category. [1] [2]
All the aircraft in the series are all made with a wooden structure, covered in doped aircraft fabric. The 7.50 m (24.6 ft) span wing employs polyhedral configuration with the outer wing panels exhibiting much greater dihedral. Engines used include the 85 hp (63 kW) Jabiru 2200 four-stroke powerplant as well as Rotax, Limbach Flugmotoren and 58 hp (43 kW) Volkswagen 1600 automotive engines. [1] [2] [3]
Data from Bayerl [1]
General characteristics
Performance