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Lancair International Evolution

lanceevo


The Lancair Evolution was developed entirely through Computer Aided Design, created by Computer Numeric Code machining and evaluated by Finite Element Analyses.
The Evolution is designed to FAR part 23 compliancy, the same standard that certified aircraft follow. It’s safety innovations include the BRS Ballistic Recovery Parachutes, AmSafe Aviation airbag seatbelts and energy absorbing seats.
The Fastbuild Kit did cost US$250,000 with a finished piston plane estimate of US$600,000, and turbine cost of US$650,000 - $1,000,000.

Lancair Evolution
Engine: Lycoming Piston
Length: 30 ft
Height: 10 ft
Wingspan: 37 ft
Seating: 4
Cargo Volume: 39 cu ft
Baggage Capacity: 225 lbs
Payload (full fuel): 1,074 lbs
Time to climb (FL 240): 13 min
Rate of climb: 2000 fpm
Mmo: .64
Vne: 255 kt
Vfe: 135 kt
Vfe 10 deg: 160 kt
Vlo: 180 kt
Vs1: 75 kt
Vso: 61 kt
T/O Distance: 1,200 ft
Landing Distance: 1,400 ft
Cruise Speed (max): 270 kt
Range: 1300 nm
Fuel Flow: 22 USgph
Cruise Speed (economy): 240 KTAS
Range: 1700 nm
Fuel Flow: 17.5 gph
Max Operating Altitude: 28,000 ft

Lancair Evolution
Engine: Pratt & Whitney PT6A-135A Turbine, 750 shp
Propeller type: Sensenich
Length: 30 ft
Height: 10 ft
Wingspan: 37 ft
Gross weight: 4300 lb
Seating: 4
Cargo Volume: 39 cu ft
Baggage Capacity: 225 lbs
Payload (full fuel): 957 lbs
Useful Load, Std: 1950 lb
Usable Fuel, Std: 146 US gal
Time to climb (FL 240): 8 min
Rate of climb: 4000 fpm
Mmo: .59
Vne: 255
Vfe: 135
Vfe 10 deg: 160
Vlo: 180 kt
Vs1: 75 kt
Vso: 61 kt
T/O Distance: 1,000 ft
Landing Distance: 1,000 ft
Cruise Speed (max): 330 KTAS
Range, Max Cruise: 886 nm
Max range: 1314 nm
Fuel Flow max cruise: 39 gph
Cruise Speed (economy): 270 KTAS
Fuel Flow econ cruise: 23 US gph
Max Operating Altitude: 28,000 ft

 

 

 


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