What was found
VERTICAL STABILIZER STRINGER EXTENSION SPLICE IS BENT JUST AFT OF MID SPAR 43.75 ON THE UPPER EDGE OF THE FUSELAGE SKIN. REPAIRED IAW SRM 51-42-06.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
VERTICAL STABILIZER STRINGER EXTENSION SPLICE IS BENT JUST AFT OF MID SPAR 43.75 ON THE UPPER EDGE OF THE FUSELAGE SKIN. REPAIRED IAW SRM 51-42-06.