What was found
CORROSION AT THE ACFT JACKING POINT BL 0 STRINGER 27, BS 280. REMOVED AND REPLACED THE LT AND RT NLG JACK POINT SUPPORT IAW SRM 51-42-13.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION AT THE ACFT JACKING POINT BL 0 STRINGER 27, BS 280. REMOVED AND REPLACED THE LT AND RT NLG JACK POINT SUPPORT IAW SRM 51-42-13.