ED Decision 2003/18/RM
(a) VS0 is the stalling speed, if obtainable, or the minimum steady speed, in km/h (knots) (CAS), at which the aeroplane is controllable, with the -
(1) Power condition set forth in subparagraph (c);
(2) Propeller in the take-off position;
(3) Landing gear extended;
(4) Wing flaps in the landing position;
(5) Cowl flaps closed;
(6) Centre of gravity in the most unfavourable position within the allowable range; and
(7) Maximum weight.
(b) VS0 may not exceed 83 km/h (45 knots) (CAS).
(c) VS1 is the stalling speed, if obtainable, or the minimum steady speed, in km/h (knots), (CAS) at which the aeroplane is controllable with -
(1) Engine idling, throttle closed;
(2) Propeller in the take-off position;
(3) Aeroplane in the condition existing in the test in which VS1 is being used; and
(4) Maximum weight.
(d) VS0 and VS1 must be determined by flight tests, using the procedure specified in CS-VLA 201.
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