Aero A.22

Aero A.22
General information
Type	Utility aircraft
Manufacturer	Aero Vodochody
Primary user	Czechoslovakia

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

Specifications (A.22)

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

Related development

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

References

1. Stroud 1966, pp. 32–33

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