Ultralight aircraft (Canada)
The Canadian Aviation Regulations define two types of ultralight aircraft: basic ultra-light aeroplane, and advanced ultra-light aeroplane.
Definition
Regulation of ultra-light aircraft in Canada is covered by the Canadian Aviation Regulations. An earlier definition of "ultra-light aeroplane", effective October 10, 1996, meant:- a single-seat aeroplane that has a launch weight of 165 kg or less, and a wing area, expressed in square metres, of not less than the launch weight in kilograms minus 15, divided by 10, and in no case less than,
- a two-seat instructional aeroplane that has a launch weight of 195 kg or less, and a wing area, expressed in square metres, of not less than 10 m2 and a wing loading of not more than 25 kg/m2, the wing loading being calculated using the launch weight plus the occupant weight of 80 kg per person, or
- an advanced ultra-light aeroplane;
Basic
On July 6, 1956 the Department of Transport first issued new requirements for ultralight aircraft, a category that was eventually renamed "Amateur-built aircraft", leaving Canada without an ultralight category. The basic ultralight category was established as a new category in 1982 to fill this gap. Regulation of ultralight aircraft in Canada is covered by the Canadian Aviation Regulations, which defines a "basic ultra-light aeroplane" as:an aeroplane having no more than two seats, designed and manufactured to have:
- a maximum take-off weight not exceeding 544 kg, and
- a stall speed in the landing configuration of 39 knots indicated airspeed, or less, at the maximum take-off weight;
Advanced
An advanced ultra-light aeroplane is an aeroplane which:
- Is propeller driven;
- Is designed to carry a maximum of two persons, including the pilot;
- Has a maximum take-off mass, MTOmax or WTOmax, of:
- # 350 kg for a single place aeroplane, or
- # 560.0 kg for a two place aeroplane;
- A maximum stalling speed in the landing configuration, VS0, at manufacturer's recommended maximum take-off mass not exceeding 72 km/h ; and
- Is limited to non-aerobatic operations. Non-aerobatic operations include:
- # manoeuvres incident to normal flying
- # stalls and spins ;
- # lazy eights, chandelles; and
- # steep turns, in which the angle of bank is not more than 60°
Minimum useful load
Advanced ultra-light aeroplanes shall have a minimum useful load, MU or WU computed as follows:- For a single place aeroplane:
- For a two place aeroplane:
Maximum empty mass (weight)
The registration marks for an advanced ultra-light aeroplane after 1997 begin with "C-Ixxx". Prior to that date they were C-Fxxx or C-Gxxx.
Operations
An ultra-light pilot permit, recreational pilot permit, Pilot licensing in Canada#Private [pilot licence.E2.80.94aeroplane|private], commercial or airline transport aeroplane licence issued by Transport Canada, is required in order for a person to operate an ultra-light aeroplane in Canada. Pilots holding a Recreational or higher license may carry a passenger in a two-seat advanced ultra-light aeroplane. Pilots with only an ultra-light permit may not carry a passenger in an advanced ultralight unless they have received a passenger carrying endorsement. Basic ultralights cannot carry passengers unless the passenger is another pilot. Student pilots undergoing training may be carried in basic ultralights.Canadian Basic and Advanced Ultralights may be flown in the USA if the pilot holds a Recreational Pilot Permit or higher designation. Pilots holding an Ultralight Pilot Permit with instructor rating and who have at least 2 hours of cross country experience may also fly to the US.
Any Canadian Ultralight flying to the US also requires a Special Flight Operations Certificate from the FAA. This is a form the pilot completes which is then valid for 180 days.