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==Specifications== |
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Revision as of 04:29, 10 January 2014
{|class="infobox " style="float: right; clear: right; width: 315px; border-spacing: 2px; text-align: left; font-size: 90%;" ! colspan="2" style="text-align: center; font-size: large; padding-bottom: 0.3em;" | A.26 |-
! Role
| reconnaissance
|-
! National origin
| Czechoslovakia
|-
! Manufacturer
| Aero Vodochody
|-
! First flight | 1923 |-
! Developed from | Hansa-Brandenburg B.I |- |}
The Aero A.26 was a Czechoslovakian military reconnaissance biplane aircraft built by Aero Vodochody in the 1920s. It was Aero's last design to be based on the Hansa-Brandenburg B.I aircraft that the company had been building under licence during World War I as the Ae.10.
It first flew in 1923 and a small series was built. They were later used in the Czechoslovak civilian aviation.
Specifications
Data from {name of first source}
General characteristics
- Crew: two, pilot and observer
- Length: 8.30 m (27 ft 4 in)
- Wingspan: 12.30 m (40 ft 4 in)
- Height: ()
- Wing area: 38.5 m² (414 ft²)
- Empty weight: 882 kg (1,940 lb)
- Loaded weight: 1,196 kg (2,631 lb)
- Powerplant: 1 × BMW IIIa 6-cylinder, water-cooled inline engine, 138 kW (185 hp)
Performance
- Maximum speed: 158 km/h (knots, 99 mph)
- Cruise speed: 120 km/h
- Service ceiling: 6,000 m (19,680 ft)
- Rate of climb: 135 m/min (443 ft/min)
- Wing loading: 31 kg/m² (6.3 lb/ft²)
- Power/mass: 120 W/kg (0.07 hp/lb)
Armament
Operators
Czechoslovakia
See also
- Related development
External links
 |
Wikimedia Commons has media related to Aero Vodochody aircraft. |
Template:Aero Vodochody aircraft Template:Aviation lists
The original article can be found at Aero A.26 and the edit history here.