The Breda Ba.32 was a low-wing trimotor monoplane with fixed, spatted main landing gear. It was powered by three Pratt & Whitney R-985 Wasp Junior nine-cylinder air-cooled radial engines. It had a crew of two, and its cabin could accommodate up to 10 passengers.^[1]

The Ba.32 prototype first flew in 1931, but despite displaying good flight characteristics, no production orders ensued and no further examples were built.^[1]

  Kingdom of Italy

Data from Italian Civil and Military aircraft 1930–1945 ^[1]

General characteristics

• Crew: 2
• Capacity: 8–11
• Length: 16.749 m (54 ft 11.4 in)
• Wingspan: 26.67 m (87 ft 6 in)
• Height: 4.153 m (13 ft 7.5 in)
• Wing area: 84.97 m² (914.6 sq ft)
• Empty weight: 3,792 kg (8,360 lb)
• Gross weight: 6,441 kg (14,200 lb)
• Powerplant: 3 × Pratt & Whitney Wasp Junior 9-cyl. air-cooled radial piston engine, 240 kW (320 hp) each

Performance

• Maximum speed: 237 km/h (147 mph, 128 kn)
• Cruise speed: 211 km/h (131 mph, 114 kn)
• Stall speed: 93 km/h (58 mph, 50 kn)
• Range: 1,350 km (840 mi, 730 nmi)
• Endurance: 8hrs
• Service ceiling: 5,300 m (17,400 ft)
• Rate of climb: 1.6 m/s (310 ft/min)
• Time to altitude: 16,400 in 52 minutes

Aircraft of comparable role, configuration, and era

• Fokker F.VII
• Junkers Ju 52