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Breda A.9
 
 Breda-A9-01
A.9
 
The Breda A.9 was a biplane trainer produced in Italy in 1928 for the Regia Aeronautica. Conventional in design, it featured a single-bay, unstaggered wing cellule and fixed tailskid undercarriage. The student and instructor sat in tandem, open cockpits.
 
A.9 I-BAZP was registered in 1927, before flying in 1928.
 
A slightly smaller version, designated A.9-bis was developed for use in Italy's aeroclubs. The A.9 bis of 1930 was a reduced span (8.72 m) single-seat aerobatics trainer.
 
 Breda-A9-02
A.9bis
 
 
A.9
Engine: 1 x Isotta-Fraschini Asso 250, 250 hp / 190 kW
Propeller: 2-bladed fixed pitch propeller
Wingspan: 9.32m (30 ft 7 in)
Wing area: 27 m2 (290 sq ft)
Length: 7.95 m (26 ft 1 in)
Height: 2.97 m (9 ft 9 in)
Empty weight: 770 kg (1,698 lb)
Gross weight: 1,050 kg (2,315 lb)
Wing loading: 39 kg/m2 (8.0 lb/sq ft)
Maximum speed: 185 km/h (115 mph; 100 kn)
Cruising speed: 152 km / h
Stall speed: 75 km/h (47 mph; 40 kn)
Range: 800 km (497 mi; 432 nmi)
Endurance: 3 hours
Service ceiling: 6,000 m (20,000 ft)
Power/mass: 0.196 kW/kg (0.119 hp/lb)
Seats: 2
No built: 36
 
A.9 bis
Engine: 1 x Isotta-Fraschini Asso 250, 250 hp / 190 kW
Wingspan: 8.72 m
Empty weight: 720 kg
MAUW: 940 kg
Seats: 2
 
 
 
 


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