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Alisport Srl Yuma

alisportyuma


Alisport initiated development of the STOL YUMA in 1994. A single engine, two-seater side-by-side, high-wing monoplane with a metal structure, all aircraft structural parts are heat-treated and corrosion inhibiting coatings are used throughout. All aluminum skins are bonded to the underlying structure prior to final riveting.

The cockpit structure is a welded tubular steel frame, and aluminum is used for the wings, tail-cone, and empennage. The control surfaces are fabric-covered.
The flight characteristics of the YUMA are enhanced by an optimized wing profile and carbon-fiber leading edge slats (Handley-Page type) that directly address the requirements of S.T.O.L. flight. The large flaps permit steep final approaches to facilitate descent over tall obstacles.

The fuel system is two wing tanks and a header tank at the firewall providing a total endurance of up to five hours.

Engine: Rotax 912 UL (80 HP)        
Wing span: 9,75 m
Cabin width: 1,18 m                
Length: 6,45 m    
Height: 2,45 m                
Wheelbase: 2,00 m    
Wing area:  13,4 m2                
Aspect ratio: 6,6
Empty weight: 282 kg                
Max takeoff weight: 450 kg    
Wing loading: 33,5 kg/m2            
Maximum speed: 175 kph
Cruise speed 75%: 150 Km/h            
Stall (without flaps): 55 Km/h
Stall speed (with flaps): 50 Km/h            
VNE: 105 kt / 121 mph / 195 kmh
Rate of climb: 6 m/s
TO dist (with 1 pob): 40 m                
TO dist (full load): 45 m
Landing distance:    55 m                
Max ceiling: 5000 m
Fuel capacity: 85 lt            
Endurance max payload at cruise speed 75%(5000 rpm): 5,2 hr

Engine: Rotax 912 ULS (100 HP)    
Wing span: 9,75 m
Cabin width: 1,18 m                
Length: 6,45 m    
Height: 2,45 m                
Wheelbase: 2,00 m    
Wing area: 13,4 m2                
Aspect ratio: 6,6
Empty weight: 282 kg                
Max takeoff weight: 450 kg    
Wing loading: 33,5 kg/m2            
Maximum speed:    185 Km/h
Cruise speed 75%: 160 Km/h            
Stall (without flaps): 55 Km/h
Stall speed (with flaps): 50 Km/h            
VNE: 105 kt / 121 mph / 195 kmh
Rate of climb: 8 m/s
TO dist (with 1 pob): 30 m                
TO dist (full load): 40 m
Landing distance:    55 m                
Max ceiling: 5000 m
Fuel capacity: 85 lt
Endurance with max payload at cruise speed 75%(5000 rpm): 4,5 hr

Engine: Rotax 914 UL (115 HP)        
Wing span: 9,75 m
Cabin width: 1,18 m                
Length: 6,45 m    
Height: 2,45 m            
Wheelbase: 2,00 m    
Wing area:  13,4 m2                
Aspect ratio: 6,6
Empty weight: 282 kg                
Max takeoff weight: 450 kg    
Wing loading: 33,5 kg/m2            
Maximum speed:    195 Km/h
Cruise speed 75%: 170 Km/h            
Stall (without flaps): 55 Km/h
Stall speed (with flaps): 50 Km/h            
Rate of climb: 10 m/s
TO dist (with 1 pob): 30 m                
TO dist (full load): 40 m
Landing distance:    55 m                
Max ceiling: 7000 m
Fuel capacity: 85 lt                
Endurance with max payload at cruise speed 75%(5000 rpm): 4,1 hr

 

 


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