Aircraft L 410 UVP-E20 > L 410 aircraft characteristics > Performance & Power Unit
Aircraft L 410 UVP-E20

>> Performance & Power Unit

Performance parameters

 

Max. Cruise Speed 405 km/hr TAS 219 kTAS
Max. Range (ISA, reserves for 45 min) 1 520 km 820 NM

 

Cruise Altitude 4 200 m 14 000 ft
Technical Ceiling 6 096 m 20 000 ft

 

Take-off Distance to 35 ft / 10,7 m    
ISA, SL, MTOW 510 m 1 673 ft
ISA+15°C, SL, MTOW 547 m 1 795 ft

 

Landing Distance from 50 ft    
ISA, SL, MLDW 500 m 1 640 ft
ISA+15°C, SL, MLDW 520 m 1 706 ft

 

Single Engine Service Ceiling
(ISA, 95% MTOW, climb rate 50 fpm)
4 755 m 15 600 ft

 

Rate of Climb at S/L Both Engines 8,5 m/s 1 673 fpm
Rate of Climb at S/L One Engine 1,8 m/s 354 fpm

 

Take-off Rating 597 kW 800 SHP 
Max. Continuous Rating 522 kW 700 SHP

 

Crew 2 pilots  

 

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Engines

 

Manufacturer                                                                                     GE Aviation Czech s.r.o.
Model GE H80-200
Max. Take-off Performance 597 kW / 800 SHP
Max. Continuous Performance 522 kW / 700 SHP
TBO 3 600 flight hours

 

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Propellers

 

Manufacturer                                                                                     Avia Propeller
Model AV 725
Number of Blades 5
TBO 3 600 flight hours