Patent ID: 9623961
Date: 2017-04-18
CPC Classifications: B64C,E05B,E05C

Claim:
1. An aircraft landing gear lock assembly comprising: a first part, wherein the first part comprises an airframe; a second part that is movably mounted relative to the first part so as to be movable between a first condition and a second condition, wherein the second part comprises a main fitting; and a lock assembly comprising: a pin elongated along a longitudinal axis and coupled to a first one of the first part and the second part; and wherein the pin includes: a prominent portion which defines a contact face; and one or more outer portions axially spaced from the prominent portion and defining one or more respective recessed faces, the contact face of the prominent portion being radially spaced further from the longitudinal axis of the pin in comparison to the one or more respective recessed faces.