Mikoyan MiG-110

The Mikoyan-Gurevich MiG-110 (Russian: МиГ-110) is a Russian passenger/cargo aircraft that began development in 1995 but has not yet flown. It is of pod-and-boom configuration, to be powered by twin 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: 18.9 m (62 ft 0 in)
• Wingspan: 25.0 m (82 ft 0 in)
• Height: 5.4 m (18 ft)
• Wing area: m² (ft²)
• Empty weight: kg (lb)
• Loaded weight: kg (lb)
• Max. takeoff weight: 18,000 kg (40,000 lb)
• Powerplant: 2 × Pratt & Whitney Canada PW127C turboprops, 1,846 kW (2,475 hp) each

Performance

• Maximum speed: 500 km/h (270 kn, 308 mph)
• Range: 3,710 km (2,000 nmi, 2,310 mi)
• Service ceiling: m (ft)
• Rate of climb: m/s (ft/min)
• Wing loading: kg/m² (lb/ft²)
• Power/mass: W/kg (hp/lb)

See also

• List of airliners