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