What was found
CRACK ON VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT LH DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) DRAG ANGLE WAS REPAIRED PER SRM 55-31-00-201-001-A01
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT LH DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) DRAG ANGLE WAS REPAIRED PER SRM 55-31-00-201-001-A01