What was found
DURING C2 INSPECTION IN CWA, LEFT HAND VERTICAL STAB TO FUSELAGE CLOSING ANGLE CRACKED 1 INCH LENGTH. MAINTENANCE REPAIRED IAW EO A55013.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C2 INSPECTION IN CWA, LEFT HAND VERTICAL STAB TO FUSELAGE CLOSING ANGLE CRACKED 1 INCH LENGTH. MAINTENANCE REPAIRED IAW EO A55013.