(e)
aeroplanes having measurable stall speed or the minimum steady flight speed in landing configuration not exceeding 35 knots calibrated air speed (CAS), helicopters, powered parachutes, sailplanes and powered sailplanes, having no more than two seats and a maximum take-off mass (MTOM), as recorded by the Member States, of no more than: Aeroplane/Helicopter/Powered parachute/powered sailplanes Sailplanes Amphibian or floatplane/helicopter Airframe mounted total recovery parachute Single-seater 300 kg MTOM 250 kg MTOM Additional 30 kg MTOM Additional 15 kg MTOM Two-seater 450 kg MTOM 400 kg MTOM Additional 45 kg MTOM Additional 25 kg MTOM When an amphibian or a floatplane/helicopter is operating both as a floatplane/helicopter and as a land plane/helicopter, it must fall below the applicable MTOM limit.
← anx_I__cpt_1__point_1__point_d__text_1 · All articles · anx_I__cpt_1__point_1__point_e__text_1 →
Source: EUR-Lex (Cellar) · retrieved 2026-10-12 · Text as adopted (Official Journal); later amendments are not incorporated in this text.