CS-LSA.5 Applicability

• ED Decision 2013/015/R found in: CS-LSA Amdt 1 - Light Sport Aeroplanes (Nov 2018)

CS-LSA.5 Applicability 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) 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) A maximum seating capacity of no more than two persons, including the pilot. (d) A single, non-turbine engine or electric propulsion unit fitted with a propeller. (e) A non-pressurised cabin. [Amdt LSA/1]