Aero A.22

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Aero A.22
Role Utility aircraft
Manufacturer Aero Vodochody
Primary user Czechoslovakia

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)[edit]

General characteristics

  • Crew: 1
  • Capacity: 2 pax
  • Length: 8.2 m (26 ft 11 in)
  • Wingspan: 12.3 m (40 ft 4 in)
  • Wing area: 36.9 m2 (397 sq ft)
  • Empty weight: 1,105 kg (2,436 lb)
  • Gross weight: 1,415 kg (3,120 lb)
  • Powerplant: 1 × Maybach Mb.IV 6-cyl. water-cooled in-line piston engine, 190 kW (260 hp)

Performance

  • Maximum speed: 201 km/h (125 mph; 109 kn)
  • Service ceiling: 7,000 m (23,000 ft)
  • Wing loading: 30 kg/m2 (6.1 lb/sq ft)
  • Power/mass: 0.180 kW/kg (0.08 hp/lb)

See also[edit]

Related development