Abstract:
A buoyancy system (10) for an aircraft (1), said buoyancy system (10) comprises an inflatable float (15) and a cover (20). Said buoyancy system (10) includes at least one extensible connection means (25) fastened to the cover (20) to connect the cover (20) to a compartment (3) of an aircraft (1), while enabling the cover (20) to be retained and to be moved transversely during inflation of the float (15).