What was found
USING HFEC .25 INCH CRACK FOUND AT DOOR 2L UPPER HINGE CUTOUT. CRACK REMOVED IAW SRM 52-00-2 FIG 6 (BEYOND LIMIT); NDT CHECKED. CRACK REMOVED IAW NDT PT.6 51-00-00; CRACK REPAIRED IAW ER 15-5210-01072-JS4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
USING HFEC .25 INCH CRACK FOUND AT DOOR 2L UPPER HINGE CUTOUT. CRACK REMOVED IAW SRM 52-00-2 FIG 6 (BEYOND LIMIT); NDT CHECKED. CRACK REMOVED IAW NDT PT.6 51-00-00; CRACK REPAIRED IAW ER 15-5210-01072-JS4.