Aircraft load cell shoring

An aircraft load cell shoring for placing a wing in an unloaded condition, an aircraft engine being attached to said wing, the aircraft load cell shoring for use with a load cell, said load cell mounted on an aircraft jack, the aircraft load cell shoring comprising of:

• (a.) a load cell adapter, the load cell adapter being able to be disposed above and attachable to said load cell;
• and
• (b) a shoring contour assembly for supporting said aircraft engine at two specific locations, the shoring contour assembly having a shoring contour assembly bottom portion, a first cradle assembly for supporting said aircraft engine at a first location, a second cradle assembly for supporting said aircraft engine at a second location, a shoring shaft portion wherein the first cradle assembly and the second cradle assembly being located at opposite ends of the shoring shaft portion, the second cradle assembly having a cradle cut out, the shoring contour assembly having a fixed receptacle located at the shoring contour assembly bottom portion, the load cell adapter communicating with the fixed receptacle, said aircraft engine and enclosed part of the wing having a center of gravity, the fixed receptacle being located such that said aircraft jack is aligned with the center of gravity of said aircraft engine and enclosed part of said wing.