Aero A.22

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)

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)

Aircraft produced by Aero Vodochody
1919-1938	Ae 01 Ae 02 Ae 03 Ae 04 Ae 10 A.8 A.10 A.11 A.12 A.14 A.15 A.17 A.18 A.19 A.20 A.21 A.22 A.23 A.24 A.25 A.26 A.27 A.29 A.30 A.32 A.34 A.35 A.38 A.42 A.46 A.100 A.101 A.102 A.104 A.125 A.130 A.134 A.200 A.204 A.230 A.300 A.304 A.330 A.430
1945-1992	Ae 45 Ae 50 Ae 145 Ae 245 Ae 345 L-29 L-39 L-59 L-60
1993-present	L-39NG L-159 Ae 270
Under licence	C-3 C-103 D-44 MB.200

This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.

Aero A.22

Specifications (A.22)

See also