Suomen ilmavoimat hankkivat kahdeksan Aero A-11HS-konetta korvaamaan Breguet-tiedustelukoneita vuonna 1927.
Halpa kone ohitti valinnassa kalliimman ja paremman Fokker C.V. harjoitus-koneen.
Koneiden tunnukset olivat AE-41 - 48. Konetyyppi oli käytössä vuoteen 1939, lopussa koulukoneena. Ensimmäinen käyttäjä oli Maalentoeskaaderi Utissa.
The Aero A.11 was a biplane light bomber and reconnaissance aircraft built in Czechoslovakia between the First and Second World Wars.
It formed the basis for a large number of other Czechoslovakian military aircraft of the inter-war period.
Around 250 were built, with some remaining in service at the outbreak of World War II.
Designed by Antonin Husnik, it was a development of the Aero A.12 (despite what the numbering of the designs might suggest).
A Hispano-Suiza 8Fb-powered version, the A.11H-s was built for the Finnish Air Force, the only foreign operator of the type.
The Finns had eight aircraft of this type and used them between 1927-39.
Specifications (A.11)
Crew: 2
Length: 8.2 m (27 ft)
Wingspan: 12.8 m (43 ft 0 in)
Height: 3.1 m (10 ft)
Wing area: 36.5 m² (393 ft²)
Empty weight: 1,080 kg (2,380 lb)
Loaded weight: 1,537 kg (3,381 lb)
Powerplant: 1 × Walter W IV, 180 kW (240 hp)
Performance
Maximum speed: 240 km/h (130 knots, 150 mph)
Range: 750 km (400 nm, 470 mi)
Service ceiling: 7,600 m (25,000 ft)
Rate of climb: 3.82 m/s (751 ft/min)
Wing loading: 42 kg/m² (8.6 lb/ft²)
Power/mass: 120 W/kg (0.071 hp/lb)
Armament
Guns:
1× forward firing .303 in (7.7 mm) Vickers machine gun
2× .303 in (7.7 mm) Lewis machine gun in flexible mount for observer
Bombs: 200 kg (441 lb)
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