- Source: Aero A.21
The Aero A.21 was a biplane military trainer aircraft developed in Czechoslovakia from the Aero A.11 reconnaissance-bomber. The aircraft was developed specifically as a night-trainer, to teach Czech Air Force pilots instrument flying techniques.
Specifications (A.21)
Data from On "nocturne" tchéoslovaque: l'Aero A-21General characteristics
Crew: 2
Length: 8.10 m (26 ft 7 in)
Wingspan: 12.78 m (41 ft 11 in)
Height: 3.16 m (10 ft 4 in)
Wing area: 36.51 m2 (393.0 sq ft)
Empty weight: 950 kg (2,094 lb)
Gross weight: 1,240 kg (2,734 lb)
Powerplant: 1 × Breitfeld & Danek Perun I 6-cyl. water-cooled in-line piston engine, 130 kW (180 hp)
Performance
Maximum speed: 170 km/h (110 mph, 92 kn)
Cruise speed: 150 km/h (93 mph, 81 kn)
Range: 340 km (210 mi, 180 nmi)
Service ceiling: 6,500 m (21,300 ft)
Time to altitude: 21 min 3 s to 3,000 m (9,800 ft)
Wing loading: 36 kg/m2 (7.4 lb/sq ft)
Operators
Czechoslovakia.
See also
Related development
Aero A.11
Aero A.12
Aero A.22
Aero A.25
Aero A.29
Related lists
List of military trainer aircraft
Citations
Bibliography
Kudlicka, Bohumir (February 2002). "On "nocturne" tchéoslovaque: l'Aero A-21" [Czech Nightlife: The Aero A-21]. Avions: Toute l'Aéronautique et son histoire (in French) (107): 53–55. ISSN 1243-8650.
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