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http://en.wikipedia.org/wiki/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: 1
• Capacity: 2
• Length: 8.2 m (27 ft)
• Wingspan: 12.3 m (40 ft 4 in)
• Height: m (ft in)
• Wing area: 36.9 m² (397 ft²)
• Empty weight: 1,105 kg (2,430 lb)
• Loaded weight: 1,415 kg (3,115 lb)
• Powerplant: 1×Maybach Mb IV, 260 hp (194 kW)

Performance

• Maximum speed: 201 km/h (109 knots, 126 mph)
• Range: km (nm, mi)
• Service ceiling: 7,000 m (23,000 ft)
• Wing loading: 30 kg/m² (6.1 lb/ft²)
• Power/mass: 180 W/kg (0.08 hp/lb)

See also

Related development

• Aero A.11
• Aero A.12
• Aero A.21
• Aero A.25
• Aero A.29
  

Related lists

• List of civil utility aircraft
  

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Published in July 2009.

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