What was found
FUSELAGE INTERNAL STRUCTURE FRAME IS DENTED AT FRAME 54.2, STRINGER 13L. REPAIRED FRAME AS REQUIRED IAW EA 6-5310-123550.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE INTERNAL STRUCTURE FRAME IS DENTED AT FRAME 54.2, STRINGER 13L. REPAIRED FRAME AS REQUIRED IAW EA 6-5310-123550.