What was found
ELONGATED HOLES OF ACCESS PANEL 192AL FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL 192AL IAW SRM 51-70-05-2R-10, REPAIR 10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ELONGATED HOLES OF ACCESS PANEL 192AL FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL 192AL IAW SRM 51-70-05-2R-10, REPAIR 10.