CPC B64C 25/20 (2013.01) [B64C 25/001 (2013.01); B64C 2025/003 (2013.01)] | 17 Claims |
1. A landing gear main fitting for an aircraft landing gear assembly, the main fitting comprising:
a main barrel;
a cross beam fixedly positioned relative to the main barrel and extending radially from the main barrel; and
a drag arm comprising a first end pivotally coupled to the cross beam by a first pivotal connection and a second end pivotally coupled to the main barrel by a second pivotal connection, the second pivotal connection comprising a spherical bearing engaging the main barrel and the second end of the drag arm.
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