What was found
LEFT VERTICAL STAB TO FUSELAGE ATTACH ANGLE HAS AN APPROX. 1" CRACK EXTENDING FROM UNDER PREVIOUS REPAIR DOUBLER. REPAIRED LEFT VERTICAL STAB TO FUSEALGE ATTACH ANGLE IAW SRM 55-31-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT VERTICAL STAB TO FUSELAGE ATTACH ANGLE HAS AN APPROX. 1" CRACK EXTENDING FROM UNDER PREVIOUS REPAIR DOUBLER. REPAIRED LEFT VERTICAL STAB TO FUSEALGE ATTACH ANGLE IAW SRM 55-31-00.