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Brochet MB-80 / MB-81 / MB-83 / MB-84
 
 Broch-MB80-01
Brochet MB.84
 
The MB.80 was a derivative of the Brochet MB.70, using essentially the same airframe, but with a redesigned wider fuselage and revised undercarriage.
 
The MB.80 No.1 F-BGLA first flew on 4 October 1951with André Deschamps at controls.
 
 Broch-MB80-02
 
The Service de l'Aviation Légère et Sportive purchased ten examples for distribution to French aeroclubs. Most examples were operated in France, but one example was later sold privately to the United Kingdom.
 
MB.80
Engine: Minie 4DC-32B, 56 kW (75 hp
Wingspan: 10.45 m (34 ft 3 in)
Wing area: 14.2 m2 (153 ft2)
Length: 6.58 m (21 ft 7 in)
Height: 2.55 m (8 ft 4 in)
Empty weight: 385 kg (849 lb)
Gross weight: 615 kg (1,356 lb)
Maximum speed: 158 km/h (99 mph)
Range: 500 km (310 miles)
Rate of climb: 3.5 m/s (690 ft/min)
Crew: One pilot
Capacity: 1 passenger
10 built
 
MB.81
Engine: Hirth HM 500B-2
1 built
 
MB.83
Engine: Continental C90
1 converted from MB.80
 
MB.84
Engine: Continental A65
1 converted from MB.80 F-BGLI
 
 
 
 


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