What was found
DURING HEAVY CHECK, TAIL FUSELAGE LT CROWN PANEL INTERIOR SURFACE WAS CORRODED, FRAMES 43-44, STRINGERS 1L-2L. REPAIRED IAW SRM 530000-300-862-A01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HEAVY CHECK, TAIL FUSELAGE LT CROWN PANEL INTERIOR SURFACE WAS CORRODED, FRAMES 43-44, STRINGERS 1L-2L. REPAIRED IAW SRM 530000-300-862-A01.