Locking device for an aircraft door, with double c-shaped latch

A door assembly comprising:

• an aircraft door comprising:
• a male part;
• and
• a female part,
• wherein the male part comprises a rod having an intermediate region between two ends and extending along a longitudinal axis of the male part, the female part extending along a longitudinal axis of the female part,
• wherein the female part comprises a housing for receiving the male part, and a first lock and a second lock for locking the male part, the first and second locks being C-shaped locks, each comprising an open ring, the female part being mounted so as to pivot around the male part between an unlocking position of the aircraft door, in which the rod is free to be removed from the housing of the female part, and a locking position of the aircraft door, in which the rod is held by each of the C-shaped locks in the housing for receiving the male part, the longitudinal axis of the male part and the longitudinal axis of the female part coinciding in the locking position, the C-shaped locks being positioned on either side of the intermediate region of the rod in the locking position, the aircraft door being fitted with one out of the female part and the male part of the locking device, and a fixed part being fitted with the other out of the male part and the female part of the locking device.