Single-engine piston1950 touring aircraft family by Jodel
D11
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. More than 3,000 examples have been built and flown.
Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.
- Manufacturer
- Jodel
- Category
- Single-engine piston
- Length
- 6.5 m
- Wingspan
- 8.22 m
Specifications
- Cruise speed
- 105 kt
- Max speed
- 112 kt
- Range
- 630 nm
- Service ceiling
- 16,000 ft
- Rate of climb
- 790 ft/min
- Max takeoff weight
- 1,323 lb
- Empty weight
- 761 lb
- Fuel capacity
- 30.6 US gal
- Powerplant
- Continental C90-14F
- Engines
- 1
- Seats
- 2
- Length
- 21.3 ft
- Wingspan
- 27 ft
- Height
- 6.8 ft
- Number built
- 3,000
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.