What was found
4 INCH CRACK IN FUSELAGE SKIN AT FS 384 2 .5 INCH ABOVE STR 25R AND .25 INCH CRACK IN FUSE SKIN 2 INCH AFT OF ABOVE CRACK. REPAIR PER SRM 53-30-3 TIME LIMITED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
4 INCH CRACK IN FUSELAGE SKIN AT FS 384 2 .5 INCH ABOVE STR 25R AND .25 INCH CRACK IN FUSE SKIN 2 INCH AFT OF ABOVE CRACK. REPAIR PER SRM 53-30-3 TIME LIMITED.