Ansaldo A.300
A.300 | |
---|---|
Role | Reconnaissance aircraft |
Manufacturer | Gio. Ansaldo & C. |
First flight | 1919 |
Number built | ~850 |
The Ansaldo A.300 was an Italian general-purpose biplane aircraft built by the Ansaldo company (now part of FIAT) of Turin from 1920 to 1929. It also served as a light bomber, transport, fighter and reconnaissance aircraft, and finally as an advanced trainer, with examples in service as late as 1940. 50 examples were also license-built in Poland at ZM E. Plage & T. Laśkiewicz, but were not a success due to poor quality.
Development
Based on Ansaldo's highly successful World War I Balilla and S.V.A scouts, the A.300 was a conventional single-engined two-bay open cockpit biplane of mixed metal and wood-and-fabric construction, powered usually by a water-cooled Fiat A.12bis V12 engine. Most variants had two fixed Vickers guns and one mobile gun mounted in the rear cockpit. It first flew in 1919.
Early examples were two seaters, but the A.300/3 was a three-seater intended for reconnaissance use, of which around 90 were delivered. The most significant variant was the A.300/4, again mostly three-seaters, which started full production in 1923, just as Ansaldo was absorbed into FIAT. This became the standard multi-role aircraft in the newly formed Regia Aeronautica and served in Italy, Sicily, Sardinia, Corfu, Libya and Eritrea.
Operational history
The A.300 was one of the most numerous aircraft of its time, with the production run of the A.300/4 alone, at 700 units, exceeding the total production of any other type of the 1920s except the Breguet XIX and Potez 25. Despite this, and possibly because it was Italian rather than French or British, it remains one of the least documented contemporary types, certainly the most obscure produced in anything like these numbers.
Variants
- A.300/2
- initial production version
- A.300/3
- three-seat version, also exported to Spain, Belgium, and Poland
- A.300/4
- definitive production version with improved cooling
- A.300/5
- prototype with Lorraine engine
- A.300/6
- improved A.300/4, also in service
- A.300C
- Four passenger airliner. Several built 1921-'26 and operated by the Belgian airline SNETA, French airlines SABENA and 1925 operated by the Romanian airlines SNNA, as regular flights with 5 aircraft. [1][2]
- A.300T
- Eight passenger airliner. At least one built 1921.[3][4]
- A.400
- prototype
Operators
Belgium
- Belgian Air Force
Kingdom of Italy
- Corpo Aeronautico Militare
Soviet Union
- Soviet Air Force
Turkey
Türk Hava Kurumu (THK)
Specifications (A.300/4)
General characteristics
Crew: two, pilot and observer
Length: 8.75 m (28 ft 9 in)
Wingspan: 11.24 m (36 ft 11 in)
Height: 2.97 m (9 ft 9 in)
Wing area: 39.5 m2 (425 ft2)
Empty weight: 1,200 kg (2,650 lb)
Gross weight: 1,700 kg (3,750 lb)
Powerplant: 1 × Fiat A.12bis piston engine, 170 kW (230 hp)
Performance
Maximum speed: 200 km/h (120 mph)
Endurance: 3 hours 30 min
Service ceiling: 5,500 m (18,000 ft)
Rate of climb: 2.5 m/s (490 ft/min)
Armament
Notes
^ Stroud 1964, pp. 392–393.
^ "The Ansaldo A-300 C Commercial Biplane" Flight, June 30, 1921
^ Stroud 1964, p. 393.
^ "1921 Paris Air Salon: Ansaldo Aéronautique A.330 T" Flight, November 17, 1921
References
Wikimedia Commons has media related to Ansaldo A.300. |
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Stroud, John (1966). European Transport Aircraft since 1910. London: Putnam..mw-parser-output cite.citation{font-style:inherit}.mw-parser-output q{quotes:"""""""'""'"}.mw-parser-output code.cs1-code{color:inherit;background:inherit;border:inherit;padding:inherit}.mw-parser-output .cs1-lock-free a{background:url("//upload.wikimedia.org/wikipedia/commons/thumb/6/65/Lock-green.svg/9px-Lock-green.svg.png")no-repeat;background-position:right .1em center}.mw-parser-output .cs1-lock-limited a,.mw-parser-output .cs1-lock-registration a{background:url("//upload.wikimedia.org/wikipedia/commons/thumb/d/d6/Lock-gray-alt-2.svg/9px-Lock-gray-alt-2.svg.png")no-repeat;background-position:right .1em center}.mw-parser-output .cs1-lock-subscription a{background:url("//upload.wikimedia.org/wikipedia/commons/thumb/a/aa/Lock-red-alt-2.svg/9px-Lock-red-alt-2.svg.png")no-repeat;background-position:right .1em center}.mw-parser-output .cs1-subscription,.mw-parser-output .cs1-registration{color:#555}.mw-parser-output .cs1-subscription span,.mw-parser-output .cs1-registration span{border-bottom:1px dotted;cursor:help}.mw-parser-output .cs1-hidden-error{display:none;font-size:100%}.mw-parser-output .cs1-visible-error{font-size:100%}.mw-parser-output .cs1-subscription,.mw-parser-output .cs1-registration,.mw-parser-output .cs1-format{font-size:95%}.mw-parser-output .cs1-kern-left,.mw-parser-output .cs1-kern-wl-left{padding-left:0.2em}.mw-parser-output .cs1-kern-right,.mw-parser-output .cs1-kern-wl-right{padding-right:0.2em}
Taylor, John W. R. (1969). Combat Aircraft of the World: from 1909 to the present. New York: Parragon Books.
Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
Hirschauer, Louis; Dollfus, Charles, eds. (1920). L'Année Aéronautique: 1919-1920. Paris: Dunod. p. 43.
Hirschauer, Louis; Dollfus, Charles, eds. (1921). L'Année Aéronautique: 1920-1921. Paris: Dunod. (p. 53 for 300/3, p. 55 for 300C)