ED Decision 2013/015/R
This Certification Specification is applicable to Light Sport Aeroplanes to be approved for day-VFR only that meet all of the following criteria:
(a)Â Â Â Â A Maximum Take-Off Mass of not more than 600 kg for aeroplanes not intended to be operated on water or 650 kg for aeroplanes intended to be operated on water.
(b)    A maximum stalling speed in the landing configuration (VS0) of not more than 83 km/h (45 knots) CAS at the aircraft’s maximum certificated Take-Off Mass and most critical centre of gravity.
(c)Â Â Â Â Â A maximum seating capacity of no more than two persons, including the pilot.
(d)Â Â Â Â A single, non-turbine engine or electric propulsion unit fitted with a propeller.
(e)Â Â Â Â A non-pressurised cabin.
[Amdt LSA/1]
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