A system configured for installing or removing a door (104) from an aircraft, comprises: a pin (108), a hinge (202) comprising a slot (208) that forms a cavity for rotatively coupling the hinge (202) and the pin (108), a clamp (210) coupled to the pin (108), and a retaining mechanism (216) on the clamp (210) that selectively bears against the hinge (202) to maintain the pin (108) in the cavity when the retaining mechanism (216) is engaged and releases the hinge (202) when the retaining mechanism (216) is disengaged.
HINGE STRUCTURE
SCHARNIERSTRUKTUR
STRUCTURE DE CHARNIERE
2020-09-02
Patent
Electronic Resource
English