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Jurca MJ-5 Sirocco

jurcamj5-1


The prototype MJ.5 Sirocco tandem two-seat aerobatic monoplane, built in France, was first flown in 1962. The Sirocco, an all-wood, fiberglass or fabric-covered low-wing design, can be identified by its rooster tail. The Sirocco sports retractable landing gear.

 

JurcaMJ5-03

 

The original prototype was still flying after 30 years.

jurcamj5-2

 

Gallery


Engine: Lycoming, 160 hp.
HP range: 125-200.
Weight empty: 1260 lbs.
Gross: 1860 lbs.
Height: 8.5 ft.
Wing area: 107.6 sq.ft.
Speed max: 196 mph.
Cruise 162 mph.
Stall: 64 mph.
ROC: 1850 fpm.
Service ceiling: 16,400 ft.
Seats: 2.
Landing gear: nose or tail wheel.
Takeoff run 820 ft.
Landing roll 750 ft.
Range 570 sm.

Engine: Lycoming, 150 hp.
Cruise: 115 kts.
Wing span: 23ft 4in.
Length: 21 ft.
MAUW: 1500 lbs.
Fuel cap: 25.5 Imp Gal.

 

Engine: Lycoming O-320, 160 hp
Wing span: 7.02 m
Wing area: 11 sq.m
MAUW: 840 kg
Empty weight: 560 kg
Fuel capacity: 170 lt
Max speed: 300 kph
Cruise speed: 240 kph
Minimum speed: 100 kph
Climb rate: 11 m/s
Seats: 2
Fuel consumption: 45 lt/hr
Plan price (1998): US$500

 

 

 

 

 


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