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BAaer BA-5 Gur

baaerba-5gur


The design goal for the Gurí was for a versatile ultralight and also an airplane kit that is easy to build. The Gurí design uses metalic and composites where it made the most sense from an engineering and a construction standpoint. The Gurí constant-chord wings are aluminum and fabric, with slotted ailerons and flaps.


For the compound curves of the cockpit, fiberglass composites are used. Fiberglass fabrics and epoxy-vinylester resin factory molding cockpit, landing gear and several parts insures a smooth finish and a simple assembly project. Rear fuselage is a 6 inch diameter aluminum tail boom with aluminum tube and fabric tail surfaces.
The main goal of the kit is the assembly of parts supplied, covering the flight surfaces, install system and engine, ulphostery and painting.  It does not include a engine, prop, paint and instruments.


Optional equipment includes wheel pants, instruments, floats, and ballistic chute. This aircraft can have 50 HP to 80 HP engine. Price 2009: 18000 USD

BA-5 Gurí

Engine: Rotax 503 50 HP    
Cruise speed @ 75%: 110 km/h (70 mph)     
Stall speed: 55 km/h (35 mph)     
Rate of Climb: 3 m/s (600 ft/m)     
Never exceded speed (VNE): 190 km/h (120 mph)     
Range: 500 km.(313 m.)     
Takeoff Distance: 150 m.(500 ft.)     
Landing Distance: 150 m.(500 ft.)     
Glide ratio: 12:1     
G Loading: +6  -4gs     
Fuel Consumption: 15 lts/hr    
Fuel capacity: 70 lts.     
Span: 10 m.(33 ft.)
Length: 6 m.(20 ft.)
Wing area: 14 sq.m (150 sq.ft)
Chord: 1.4 m.(55 in)
Empty weight: 225 kg.(495 lb.)
Gross weight: 450 kg.(1000 lb.)
Cockpit width: 1.05 m.(42 in)
Baggage capacity: 15 kg.(33 lb.)
Seats: 2

BA-5 Gurí
Engine: HKS 700E 60HP    
Cruise speed @ 75%: 120 km/h (75 mph)     
Stall speed: 55 km/h (35 mph)     
Rate of Climb: 3.5 m/s (700 ft/m)     
Never exceded speed (VNE): 190 km/h (120 mph)     
Range: 840 km.(525 m.)     
Takeoff Distance: 150 m.(500 ft.)     
Landing Distance: 150 m.(500 ft.)     
Glide ratio: 12:1     
G Loading: +6  -4gs
Fuel Consumption: 10 lts/hora     
Fuel capacity: 70 lts.     
Span: 10 m.(33 ft.)
Length: 6 m.(20 ft.)
Wing area: 14 sq.m (150 sq.ft)
Chord: 1.4 m.(55 in)
Empty weight: 225 kg.(495 lb.)
Gross weight: 450 kg.(1000 lb.)
Cockpit width: 1.05 m.(42 in)
Baggage capacity: 15 kg.(33 lb.)
Seats: 2

BA-5 Gurí
Engine: Rotax 582 64HP    
Cruise speed @ 75%: 130 km/h (80 mph)     
Stall speed: 55 km/h (35 mph)     
Rate of Climb: 4 m/s (800 ft/m)     
Never exceded speed (VNE): 190 km/h (120 mph)
Range: 500 km.(313 m.)     
Takeoff Distance: 100 m.(330 ft.)     
Landing Distance: 150 m.(500 ft.)     
Glide ratio: 12:1     
G Loading: -4gs     +6
Fuel Consumption: 18 lts/hr     
Fuel capacity: 70 lts.     
Stall: 32 kt / 37 mph / 60 kmh
Cruise: 70 kt / 81 mph / 130 kmh
VNE: 103 kt / 118 mph / 190 kmh
Empty Weight: 230 kg / 507 lbs
MTOW Weight: 450 kg / 992 lbs
Climb Ratio: 800 ft/min / 4 m/s
Glide Ratio: 10
Span: 10 m.(33 ft.)
Length: 6 m.(20 ft.)
Wing area: 14 sq.m (150 sq.ft)
Chord: 1.4 m.(55 in)
Empty weight: 225 kg.(495 lb.)
Gross weight: 450 kg.(1000 lb.)
Cockpit width: 1.05 m.(42 in)
Baggage capacity: 15 kg.(33 lb.)
Seats: 2

BA-5 Gurí

Engine: Rotax 912 80 HP
Cruise speed @ 75%: 150 km/h (90 mph)
Stall speed: 60 km/h (38 mph)
Rate of Climb: 5m/s (1000 ft/m)
Never exceded speed (VNE): 190 km/h (120 mph)
Range: 800 km.(500 m.)
Takeoff Distance: 80 m.(260 ft.)
Landing Distance: 150 m.(500 ft.)
Glide ratio: 12:1
G Loading: +6  -4gs
Fuel Consumption: 12 lts/hr
Fuel capacity: 70 lts.
Span: 10 m (33 ft.)
Length: 6 m (20 ft.)
Wing area: 14 sq.m (150 sq.ft)
Chord: 1.4 m.(55 in)
Empty weight: 225 kg.(495 lb.)
Gross weight: 450 kg.(1000 lb.)
Cockpit width: 1.05 m.(42 in)
Baggage capacity: 15 kg.(33 lb.)
Seats: 2

 

 


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