Breda A.7
The Breda A.7 was a reconnaissance aircraft developed in Italy for use by the Regia Aeronautica in 1929. It was a braced parasol monoplane of conventional configuration with tailskid undercarriage. The pilot and observer sat in tandem, open cockpits. A single prototype of a long-range example, originally designated A.7 Raid and later A.16 (or Ba.16) was also constructed, but the air force showed no interest in it.
Variants
- A.7LD prototypes - Two prototypes, powered by a 298 kW (400 hp) Lorraine-Dietrich piston engine. (2 built).
- A.7 - Production version. Two-seat reconnaissance aircraft, powered by a 380 kW (510 hp) Isotta Fraschini Asso 500 piston engine, and fitted with a revised cooling system and empennage (12 built).
- A.7 Raid (later A.16 or Ba.16) - Long-range version, powered by Isotta Fraschini Asso 500 AQ engine. Engine later changed to a Bristol Jupiter VII and an extra seat added.
Operators
- Kingdom of Italy
Specifications (A.7)
General characteristics
- Crew: 2, pilot and observer
- Length: 9.22 m (30 ft 3 in)
- Wingspan: 15.18 m (49 ft 10 in)
- Height: 3.14 m (10 ft 4 in)
- Wing area: 43.0 m2 (463 ft2)
- Empty weight: 1,500 kg (3,307 lb)
- Gross weight: 2,500 kg (5,511 lb)
- Powerplant: 1 × Isotta Fraschini Asso 500 piston engine, 380 kW (510 hp)
Performance
- Maximum speed: 235 km/h (146 mph)
- Range: 1,200 km (746 miles)
- Service ceiling: 6,500 m (21,325 ft)
- Rate of climb: 4.6 m/s (905 ft/min)
Armament
- 1 × rearward-firing, trainable .303 Lewis Gun for observer
See also
- Related lists
References
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Wikimedia Commons has media related to Breda A.7. |
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 195.
- World Aircraft Information Files. London: Bright Star Publishing. pp. File 890 Sheet 77.
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