What was found
INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN AT THE AFT LOWER CORNER OF THE R-1 DOOR CUTOUT, STA 328, S18R. REPAIRED IAW SRM 53-10-01. A DIP WAS ISSUED TO INSPECT THE REPAIR WITHIN 60,000 FLIGHT HOURS AFTER REPAIR ACCOMPLISHMENT.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN AT THE AFT LOWER CORNER OF THE R-1 DOOR CUTOUT, STA 328, S18R. REPAIRED IAW SRM 53-10-01. A DIP WAS ISSUED TO INSPECT THE REPAIR WITHIN 60,000 FLIGHT HOURS AFTER REPAIR ACCOMPLISHMENT.