This article needs additional citations for verification . Please help improve this article by adding citations to reliable sources. Unsourced material may be challenged and removed. Find sources:  "Aero A.22"  –  news · newspapers · books · scholar · JSTOR (January 2021) ( Learn how and when to remove this message )

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.

Contents

• Specifications (A.22)
• See also
• References

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

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

This article on an aircraft of the 1920s is a stub. You can help Wikipedia by expanding it.

• v
• t
• e