Patent ID: 8894012

Claim:
An aircraft nacelle, comprising: an outside surface with at least one opening that is blocked by at least one movable first part ( 16 ) and a second part ( 16 ′), said first and second parts ( 16 , 16 ′) configured to be connected in a closed position by at least one locking mechanism ( 20 ) that connects said first part ( 16 ) to said second part ( 16 ′); and a closure device ( 30 ), comprising an anchoring point ( 32 ) on one of the first and second parts to be connected, and a detachable link ( 34 ) that is detachably connectable to a traction means ( 36 ) that is integral with the other of the first and second parts, wherein the detachable link ( 34 ) comprises a strap ( 42 ), a first end ( 44 ) of the strap being attached to the traction means ( 36 ), and a second end ( 46 ) of the strap connectable in a detachable manner to the traction means ( 36 ) via a hooking means located at the second end, whereby the strap ( 42 ), when connected via the hooking means to the traction means, forms a loop in which the anchoring point ( 32 ) can be arranged.