Mikoyan MiG-110

The Mikoyan-Gurevich MiG-110 (Russian: МиГ-110) was a proposed Russian passenger/cargo aircraft that began development in 1995 but was not built. It would have been a high-mounted cantilever monoplane with a pod-and-boom configuration with a beaver tail rear fuselage, to be powered by two Klimov TV7-117 turboprop engines.

Proposed Variants

• MiG-110N – dedicated passenger version
• MiG-110NP – paramilitary version
• MiG-110M – combination passenger/freight version with all-weather and STOL capability
• MiG-110A – version for joint project to produce in Austria.

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Specifications (MiG-110M, as designed)

General characteristics

• Crew: 2
• Capacity:
  
• Passengers: 49
• Cargo: 5,500 kg (12,000 lb)
• Length: 18.5 m (60 ft 8 in)
• Wingspan: 22.12 m (72 ft 7 in)
• Max takeoff weight: 15,300 kg (33,731 lb)
• Powerplant: 2 × Klimov TV7-117 turboprop engines, 1,864 kW (2,500 hp) each

Performance

• Cruising speed: 500 km/h (311 mph; 270 kn)
• Range: 4,050 km (2,517 mi; 2,187 nmi) with full fuel
• Service ceiling: 11,000 m (36,089 ft)

See also

• List of airliners