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This version of our Ellipse Spirit is equipped with a fixed landing gear and an 8.6m span wing and can be equipped only with a ground adjustable propeller.

The main undercarriage consists of a composite spring and a steerable nose wheel.Wing may be equipped by optional air brakes. This version allows the pilot seat position to be adjusted more upright.

  • LSA - Technical data

    Aircraft model LSA (8,6)

    Wing Span

    8.6 m (28.22 ft)

    Length

    6.55 m (21.49 ft)

    Height

    2,02 m (6.63 ft)

    Wing surfaces

    10.34  m2 (111.30 ft²)

    Specific empty weight (with BRS and safety fuel cells) *1

    324 kg (714 lbs)

    Maximum take-off Weight *2

    600 kg (1323 lbs)

    Maximum luggage weight

    25 kg (55 lbs)

    Standard Fuel Capacity *3 *4

    120 l (32 US gal

  • Performance

    Performance

    Stall speed VS0 (in landing configuration)

    62 km/hr (33 kts)

    Minimum approach speed

    78 km/hr (42 kts)

    Maximum cruise speed VH * 5

    250 km/hr (135 kts)

    Maximum Speed VNE

    315 km/hr (170 kts)

    Max. climb rate at MTOW *5

    6,4 m/s (1260 fpm)

    Max Cruise Range and Endurance (economy speed) *9*10

    1060 km (572 nm)/ 5,3 hrs

  • Explanatory notes:
    1. Passive crew safety is our priority, that is why Ellipse Spirit includes the rescue system already in the basic version together with the anti-crash fuel cells and a fixed slot in the leading edge (weight aprox. 25 kg).
    2. All versions are designed for maximum take off weight of 600 kg.
    3. Depends on used fuel tank - all information apply for anti crash fuel cells from production of Merin (Italy).
    4. On request of a customer, it is possible to install additional fuselage fuel tank for long flights, ranging from 20 l (5 US gal) to 60 l (16 US gal).
    5. Values for UL version with Rotax 912 ULS / LSA with UL Power 350iS.
    6. Performance shown with 45 minutes reserves and standard fuel cells.
    7. Cruise Range and Endurance of version S-LSA RG may be extended up to 2700 km (1450 nm / 14,24 hrs) by using the additional fuselage fuel tank with volume of 60l (16 US gal).
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