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The
CARS 101.01 - an "ultra-light aeroplane" - means an
advanced ultra-light aeroplane or a basic ultra-light aeroplane; (avion
ultra-léger)
A basic ultra-light aeroplane
is defined as either:
basic ultra-light aeroplane" means an aeroplane having no more than two
seats, designed and manufactured to have
(a) a maximum
take-off weight not exceeding 544 kg, and
(b) a stall speed in
the landing configuration (Vso) of 39 knots (45 mph) indicated
airspeed, or less, at the maximum take-off weight;
Note : When registering a basic
ultra-light aeroplane, you must demonstrate that the useful load of your
aeroplane (the difference between the maximum gross weight specified by the
manufacturer and the actual empty weight of your aircraft) is at least the
amount specified (Mu or Wu) below:
For a single place aeroplane
Mu = 80 + 0.3P, in kg; where P is the rated engine power in kilowatts
(Wu) = 175 + 0.5P, in lb.; where P is the rated engine power in Brake Horse
Power
or
For a two place aeroplane
Mu = 160 + 0.3P, in kg; where P is the rated engine power in kilowatts
(Wu) = 350 + 0.5P, in lb. ; where P is the rated engine power
in Brake Horse Power
Aircraft that do not provide at least the minimum useful
load specified
above cannot be registered as basic ultra-light aeroplanes.
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