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  Aircraft History, Specification and Information
Evektor Harmony LSA
 
2011 Evektor Harmony LSA (sn 2011 1413)
with a Rotax 912ULS (100hp) engine
Photo taken Jul. 22, 2015
Brennand Airport, Neenah, WI - USA (79C)
Photo © Marcel Siegenthaler

The Harmony LSA is the latest FAA approved S-LSA aircraft produced by Evektor and represents the next generation of the first FAA approved light sport aircraft- the SportStar. The Harmony LSA is the Ultimate Cross Country Touring & Training S-LSA. The new tapered wing, enlarged rudder & ailerons, more cockpit space and other innovations bring further comfort and performance enhancements.

Airframe

The Harmony LSA has an anodized advanced metal airframe. It is the only LSA with all construction joints riveted and adhesively bonded for enhanced durability. The outstanding durability of the Harmony LSA airframe has been proven in intensive flight operations of leading schools in the USA, Australia and other countries.

Engine Choices

  • Rotax 912 iS/S2 Sport Fuel Injected - for cost-effective operation
  • Rotax 914 Turbo Charged - for High Altitude Performance in mountainous & hot areas
  • Rotax 912 ULS Normally Aspirated – standard performance and minimized weight

Specification

Dimensions

Length: 20 ft / 6.11 m
Height: 8ft 2 in / 2.48 m
Wing span: 30 ft 4 in / 9.25 m
Cabin width: 46.5 in / 1.18 m
Baggage compartment volume: 10.1 cu.ft / 285 l

Weight & Quantities

Useful load: 634 lb / 289 kg
Max. take-off weight: 1 320 lb / 600 kg
Empty weight (standard a/c): 686 lb / 311 kg
Max. baggage: 55 lb / 25 kg
Design load factors: +6 / -3g
Operation load factors: +4 / -2g
Wing tank capacity: 31.7 U.S. gal / 120 l

Performance

Engine: Rotax 912ULS (100 hp) | Rotax 914 UL (115 hp)
Never exceed speed: 146 kts 270 km/h | 146 kts 270 km/h
Max. level speed: 120 kts 222 km/h | 128 kts 240 km/h
Cruising speed (75% power): 110 kts 204 km/h | 118 kts 219 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 fpm 5.2 m/s | 1 320 fpm 6.7 m/s
Service 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
Average fuel consumption: 4.0 U.S.gal 15 l/h | 5.3 U.S.gal 20 l/h
Range: 700 nm 1 300 km | 600 nm 1 120 km

Last updated January 26, 2016  
This article is licensed under the GNU Free Documentation License. Source: Evektor, spol. s r.o..
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