Breda-Zappata BZ.308

Airplanes

Length

33.52 m

Flat Wing Span

42.1 m

Height

7.15 m

Flat Wing Area

208 m²

Flat Wing Aspect Ratio

8.55

Max Seating

Cruise Speed

441 km/h

Max Speed

573 km/h

Max Ceiling

8000 m

Number of Engines

Aircraft Engine

First Flight

1948-08-27

Entry Into service

1949-01-01

Number Built

Maximum Take-Off Weight

46.5 t (paragliders: kg)

Total Fuel Capacity

18000

Maximum Range

7700 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Breda-Zappata BZ.308	46.5	18000	7700

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Boeing Y1B-20		33.3	47.8		Compare
Junkers Ju 290	BMW 801	28.64	42		Compare
Martin XB-16		35	42.672		Compare
Breguet 763 Deux-Ponts		28.94	42.96	107	Compare
Armstrong Whitworth AW.681	Rolls-Royce Medway	31.6992	40.8432		Compare
Lockheed XB-30	Wright R-3350 Duplex-Cyclone	31.91	37.5		Compare

All data (24 fields)

Name: Breda-Zappata BZ.308
Manufacturer: Società Italiana Ernesto Breda
Description: The Breda-Zappata B.Z.308 was an Italian four-engined airliner produced by Breda.
First Flight: 1948-08-27
Entry Into service: 1949-01-01
Designer: Filippo Zappata
Type: Four-engined airliner
Length (m): 33.52
Height (m): 7.15
Max Seating: 54
Max Speed (km/h): 573
Cruise Speed (km/h): 441
Min Speed (km/h): 135
Max Ceiling (m): 8000
Capacity Description: 54 passengers
Number Built: 1
Powerplant Description: 4 × Bristol Centaurus 568 18-cylinder air-cooled radial engines, 1864 kW (2500 hp) each
Primary Users: Italian Air Force
Wikipedia Article (URL): en.wikipedia.org/wiki/Breda-Zappata_BZ.308
Flat Wing Span (m): 42.1
Flat Wing Area (m²): 208
Flat Wing Aspect Ratio: 8.55
Aircraft Engine: Bristol Centaurus
Number of Engines: 4