The structural component 1, wherein said structural component is {TAIL ~ an sircraft body component} having a vaulted configuration relative to {HEAD ~ a longitudinal central axis} of said aircraft body 
The structural component 1 , wherein said structural component is { TAIL ~ an sircraft body component } having a vaulted configuration relative to { HEAD ~ a longitudinal central axis } of said aircraft body
OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH TAIL TAIL TAIL TAIL TAIL TAIL TAIL TAIL OTH OTH OTH OTH OTH OTH HEAD HEAD HEAD HEAD HEAD HEAD HEAD HEAD OTH OTH OTH OTH