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 8 Fb-powered version, the A.11H-s was built for the Finnish Air Force, the only foreign operator of the type.

Contents

1 Specifications (A.11) 1.1 General Characteristics 1.2 Performance 1.3 Armament 2 Related content

Specifications (A.11)

General Characteristics

• Crew: two, pilot and observer
• Length: 8.20 m (26 ft 11 in)
• Wingspan: 12.80 m (43 ft 0 in)
• Height: 3.10 m (10 ft 2 in)
• Wing area: 36.5 m² (393 ft²)
• Empty: 1,080 kg (2,376 lb)
• Loaded: 1,537 kg (3,381 lb)
• Maximum takeoff: kg ( lb)
• Powerplant: 1x Walter W IV, 179 kW (240 hp)

Performance

• Maximum speed: 240 km/h (150 mph)
• Range: 750 km (469 miles)
• Service ceiling: 7,600 m (25,000 ft)
• Rate of climb: 229 m/min (751 ft/min)
• Wing loading: 42 kg/m² (8.6 lb/ft²)
• Power/Mass: 0.12 kW/kg (0.07 hp/lb)

Armament

• 1x forward firing .303 Vickers machine gun
• 2x .303 Lewis machine gun in flexible mount for observer
• bombs

Related content

Related development: A.12 - A.21 - A.22 - A.25 - A.29

Comparable aircraft:

Designation sequence: A.10 - A.11 - A.12 - A.14 - A.15