Aero A.22

The Aero A.22 was a Czechoslovakian biplane civil utility aircraft based on the Aero A.11 reconnaissance-bomber. The observer's position was replaced by seating for two passengers.

Specifications (A.22)

General Characteristics

  • Crew: one, pilot
  • Capacity: two passengers
  • Length: 8.20 m (26 ft 11 in)
  • Wingspan: 12.30 m (40 ft 4 in)
  • Height: m ( ft in)
  • Wing area: 36.9 m² (397 ft²)
  • Empty: 1,105 kg (2,431 lb)
  • Loaded: 1,415 kg (3,113 lb)
  • Maximum takeoff: kg ( lb)
  • Powerplant: 1x Maybach Mb IV, 194 kW (260 hp)

Performance

  • Maximum speed: 201 km/h (126 mph)
  • Range: km ( miles)
  • Service ceiling: 7,000 m (22,960 ft)
  • Rate of climb: m/min ( ft/min)
  • Wing loading: 30 kg/m² (6.1 lb/ft²)
  • Power/Mass: 0.18 kW/kg (0.08 hp/lb)

Related content

Related development: A.11 - A.12 - A.21 - A.25 - A.29 Comparable aircraft: Designation sequence: A.19 - A.20 - A.21 - A.22 - A.23 - A.24 - A.25

 

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