avia.wikisort.org - Aeroplane

The Délémontez-Desjardins D.01 'Ibis' is a French ultralight monoplane designed by Jean Délémontez for amateur construction, derived from the Jodel D.11.

D.01 Ibis
Role	Ultralight monoplane Type of aircraft
National origin	France
Manufacturer	Jacques Desjardins
Designer	Jean Délémontez
First flight	12 June 1985
Developed from	Jodel D.11

Specifications

Data from Les Avions Français de 1965 a 1990[1]

General characteristics

• Crew: 1 or 2
• Capacity: 1 or 2 pax
• Length: 6.3 m (20 ft 8 in)
• Wingspan: 8.22 m (27 ft 0 in)
• Wing area: 12.75 m² (137.2 sq ft)
• Empty weight: 357 kg (787 lb)
• Gross weight: 617 kg (1,360 lb)
• Powerplant: 1 × Lycoming O-235 4-cylinder air-cooled horizontally-opposed piston engine, 75 kW (100 hp)
• Propellers: 2-bladed variable-pitch propeller

Performance

• Maximum speed: 200 km/h (120 mph, 110 kn)
• Cruise speed: 185 km/h (115 mph, 100 kn)
• Endurance: 3 hours
• Service ceiling: 4,000 m (13,000 ft)

References

External links

• Parmentier, Bruno (8 December 2017). "Délémontez-Desjardins D.01 'Ibis'". Aviafrance (in French). Paris. Retrieved 8 March 2019.

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