| CPC E05C 17/32 (2013.01) [E05C 17/08 (2013.01); E05C 17/30 (2013.01)] | 13 Claims |

|
1. A door stop mechanism for use with an aircraft door, the door stop mechanism comprising:
a first link configured to be rotatably coupled to the aircraft door, the first link rotatable about a first pivot point;
a second link configured to be rotatably coupled to a floor, the first link rotatable about a second pivot point;
a third pivot point, wherein the first link is rotatably coupled to the second link via the third pivot point;
wherein the first link and the second link are configured to rotate to a hold-open position in which ends of the first and second links abut one another to hold the aircraft door open; and
wherein the first link nests within the second link to form a nested arrangement when the door is closed.
|