What was found
SCREW HOLE ELONGATED AT FWD END OF FUSELAGE ACCESS PANEL 192AL / REPAIRED ELONGATED HOLE ON FUSELAGE ACCESS PANEL 192AL I-A-W SRM 53-40-70-2R-1; I.A.W SRM 51-70-04-2R-9.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SCREW HOLE ELONGATED AT FWD END OF FUSELAGE ACCESS PANEL 192AL / REPAIRED ELONGATED HOLE ON FUSELAGE ACCESS PANEL 192AL I-A-W SRM 53-40-70-2R-1; I.A.W SRM 51-70-04-2R-9.