Aircraft engine assembly stand

An aircraft engine stand for supporting a variety of aircraft engines, comprising:

• a mount rotatably securable to a support, the mount extending around a central axis from a first end to a second end, the mount surrounding an engine-receiving space having an opening between the first end and the second end, the opening sized for allowing a selected one of the aircraft engines to be positioned into and removed from the engine-receiving space, the mount rotatable relative to the support about the central axis and about a transverse axis intersecting the central axis;
• and
• a set of adaptors selectively removably securable to the mount, the set of adaptors including a first adaptor and a second adaptor, the first adaptor configured to uniquely mate with a first configuration of the variety of aircraft engines, the second adaptor customized to uniquely mate with a second configuration of the variety of aircraft engines.