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