Jodel D112 (Continental A65, 530 kg)
Explore the Jodel D112 (Continental A65, 530 kg) in side view and top view to compare its silhouette and proportions.
6.2 m20.3 ft
8.2 m26.9 ft
From Wikipedia
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.
Summary of “Jodel D.11” from Wikipedia, the free encyclopedia, used under CC BY-SA 4.0. Retrieved 2026-10-11.
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Drawing of the Jodel D112 (Continental A65, 530 kg) by AirwayControl Aircraft Library (https://aircraft.intelsystems.ai/aircraft/D11/), CC BY 4.0Specifications
- Length
- 6.2 m20.3 ft
- Wingspan
- 8.2 m26.9 ft
- Max take-off weight
- 0.53 t1,200 lb
- Engines
- 1 × Continental A65-8 / A65-12F
- Power
- 66 cv at 2300 rpm (type certificate rating)
- First flight
- 1950
From the AirwayControl spec register, curated from Wikipedia and manufacturer pages. Figures vary by variant.