EVEKTOR SPORTSTAR

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Evektor SportStar LSA

Technical Data

Dimensions	Rotax 912 ULS (100 HP)		Rotax 914 UL2 Turbo (115 HP)
Length	19 ft 7 1/2"	5.98 m	19 ft 7 1/2"	5.98 m
Height	8 ft 2"	2.48 m	8 ft 2"	2.48 m
Wing span	28 ft 5"	8.65 m	28 ft 5"	8.65 m
Cabin width	46 1/2"	1.18 m	46 1/2"	1.18 m
Baggage compartment volume	10.1 cu.ft	285 l	10.1 cu.ft	285 l
Weight & Quantities
Useful load	640 lb	292 kg	621 lb	283 kg
Max take-off weight	1 320 lb*	600 kg*	1 320 lb*	600 kg*
Empty weight (standard a/c)	680 lb	308 kg	699 lb	317 kg
Max. baggage	55 lb	25 kg	55 lb	25 kg
Design load factors	+6 / -3 g	+6 / - 3 g	+6 / -3 g	+6 / -3 g
Operation load factors	+4 / -2 g	+4 / - 2 g	+4 / -2 g	+4 / -2 g
Wing tank capacity	31.7 USgal	120 l	31.7 USgal	120 l
Flight performance
Never exceed speed	146 kts	270 km/h	146 kts	270 km/h
Maximum level speed	115 kts	213 km/h	128 kts	240 km/h
Cruising speed	110 kts	204 km/h	124 kts	230 km/h
Stall speed VS1	45 kts	83 km/h	45 kts	83 km/h
Stall speed VS0 (full flaps)	40 kts	74 km/h	40 kts	74 km/h
Rate of climb	1 020 ft / min	5.2 m/s	1.320 ft / min	6.7 m/s
Maximum ceiling	15 500 ft	4 720 m	27 000 ft	8 230 m
Take-off run (concrete RWY)	620 ft	190 m	560 ft	170 m
Landing run (concrete RWY)	590 ft	180 m	590 ft	180 m
Range	700 nm	1 300 km	600 nm	1 110 km
* For US market with VG´s.
Under ISA conditions. Performances at MTOW. All information can change without prior notice. Please check Evektor's Website for the latest details related to the Evektor SportStar.

Engine	Bombardier Rotax 912 ULS	Bombardier Rotax 914 ULS Turbo
Number of cylinders	4	4
Maximum power	100 hp	115 hp
TBO	2000 hrs	2000 hrs
Fuel consumption	4.0 US gal / hr 15 l / hr	5.3 US gal / hr 20 l / hr
Unleaded automotive gasoline RON95 / AKI91 / ASTM D4814 or AVGAS 100LL
Propeller	Fixed, on-ground or in-flight adjustable

*Red Circle = SportStar Turbo

AB Flight
Queen City Airport
1730 Vultee St.
Allentown, PA 18103
(610) 762-9909