What was found
INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT AFT LOWER CORNER OF R-1 DOOR CUTOUT, STA 328-344, S16R TO S17R. THE SKIN WAS REPAIRED IAW SRM 53-10-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT AFT LOWER CORNER OF R-1 DOOR CUTOUT, STA 328-344, S16R TO S17R. THE SKIN WAS REPAIRED IAW SRM 53-10-01.