What was found
FOUND VERTICAL FIN ACCESS PANEL PUNCTURED. REPAIRED IAW SRM 51-40-06 AND REINSTALLED IAW MM 53-30-10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND VERTICAL FIN ACCESS PANEL PUNCTURED. REPAIRED IAW SRM 51-40-06 AND REINSTALLED IAW MM 53-30-10.