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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.
Designers
Édouard Joly and Jean Délémontez based the design on two of their earlier
projects; they combined the wing of the projected D.10 with a lengthened and
widened version of the D.9 fuselage.
The
first example flew on 4 April 1950.
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.
Various powerplants were installed, typically Salmson 9, Continental A65 or
Continental C90.
The aircraft uses all-wood construction with a single piece box-spar.[1]
D.11s 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.
Specifications (typical D.11 with Continental O-200 engine)
General characteristics
- Crew: one
- Capacity: one passenger or student pilot
- Length: 6.2 m (20 ft 4 in)
- Wingspan: 8.2 m (26 ft 11 in)
- Wing area: 12.7 m2 (137 sq ft)
- Empty weight: 340 kg (750 lb)
- Gross weight: 620 kg (1,367 lb)
- Powerplant: 1 × 4-cyl. air-cooled horizontally opposed piston engine, 75 kW (101 hp)
Performance
- Maximum speed: 210 km/h (130 mph; 113 kn)
- Range: 900 km (559 mi; 486 nmi)
- Rate of climb: 4.33 m/s (852 ft/min)
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