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