Bréguet 19

Length
9.61 m
Flat Wing Span
14.83 m
Height
3.69 m
Flat Wing Area
50 m²
Max Speed
214 km/h
Max Ceiling
7200 m
Number of Engines
1
First Flight
1922-03-01
Number Built
2700
Maximum Take-Off Weight
2.5 t (paragliders: kg)
Total Fuel Capacity
365
Maximum Range
800 km

Pictures

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Total Fuel Capacity Maximum Range (km)
Bréguet 19 2.5 365 800

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All data (20 fields)
Name
Bréguet 19
Manufacturer
Bréguet Aviation
Description
The Breguet 19 (Breguet XIX, Br.19 or Bre.19) was a sesquiplane bomber and reconnaissance aircraft which was also used for long-distance flights and was designed by the French Breguet company and produced from 1924.
First Flight
1922-03-01
Designer
Marcel Vuillerme
Type
Light bomber/reconnaissance aircraft
Length (m)
9.61
Height (m)
3.69
Cockpit Crew
2
Max Speed (km/h)
214
Max Ceiling (m)
7200
Armament
1 × fixed, forward-firing 7.7 mm Vickers machine gun, and two flexible, rearward-firing 7.7 mm Lewis Guns.; Provision for light bombs.
Number Built
2700
Powerplant Description
1 × Lorraine 12Ed Courlis W-12 liquid-cooled piston engine, 336 kW (450 hp) each
Primary Users
French Air Force
Status
retired
Wikipedia Article (URL)
en.wikipedia.org/wiki/Br%C3%A9guet_19
Flat Wing Span (m)
14.83
Flat Wing Area (m²)
50
Number of Engines
1