Dobi-II

Dobi-II is a second plane from Dobi line of aircraft designed by Lithuanian aviator Jurgis Dobkevičius in 1922, tested in October 1923. After two landing accidents plans for mass production of Dobi-II were abandoned.

Specifications

General characteristics

• Crew: 2
• Length: 6.1 m (20 ft 0 in)
• Wingspan: 14 m (45 ft 11 in)
• Wing area: 22.44 m² (241.5 sq ft)
• Empty weight: 840 kg (1,852 lb)
• Gross weight: 1,240 kg (2,734 lb)
• Powerplant: 1 × Benz Bz.IV 6-cyl. water-cooled in-line piston engine, 150 kW (200 hp)

Performance

• Maximum speed: 248 km/h (154 mph; 134 kn)
• Cruising speed: 190 km/h (120 mph; 100 kn)
• Stall speed: 90 km/h (56 mph; 49 kn)
• Range: 1,000 km (621 mi; 540 nmi)
• Service ceiling: 9,000 m (29,528 ft)

See also

• Dobi-I
• Dobi-III