What was found
FUSELAGE FRAME CORRODED AT BS 500D, BETWEEN STRINGERS 27 - 28L. REPAIRED THE FRAME IAW SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME CORRODED AT BS 500D, BETWEEN STRINGERS 27 - 28L. REPAIRED THE FRAME IAW SRM.