Aero A.22

Summary

The Aero A.22 was a Czechoslovakian biplane civil utility aircraft based on the Aero A.12 reconnaissance-bomber. The observer's position was replaced by seating for two passengers.

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

Specifications (A.22) edit

Data from European Transport Aircraft since 1910[1]

General characteristics

  • Crew: 1
  • Capacity: 2 passengers
  • Length: 8.3 m (27 ft 3 in)
  • Wingspan: 12.8 m (42 ft 0 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 × Walter 6-cylinder water-cooled in-line piston engine, 160 kW (220 hp)

Performance

  • Maximum speed: 200 km/h (120 mph, 110 kn)
  • Cruise speed: 175 km/h (109 mph, 94 kn)
  • Range: 750 km (470 mi, 400 nmi)
  • Service ceiling: 7,650 m (25,100 ft)

See also edit

Related development

References edit

  1. ^ Stroud 1966, pp. 32–33

Stroud, John (1966). European Transport Aircraft since 1910. London: Putnam.