What was found
CRACKED VERTICAL STABILIZER TO FUSELAGE LT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO 67.5% REAR SPAR DATUM. THE VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS REPAIRED IAW SRM 55-31-00-201-001-A01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED VERTICAL STABILIZER TO FUSELAGE LT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO 67.5% REAR SPAR DATUM. THE VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS REPAIRED IAW SRM 55-31-00-201-001-A01.