What was found
AT C CHECK, EVIDENCE OF CORROSION AND SMALL CRACK AT BS 950C FRAME UPPER FLANGE BETWEEN S-26 L AND STR 27 L. CUT OUT DAMAGED AREA AT UPPER FLANGE, HFEC, INSTALLED FRAME REPAIR AT BS 950C PER SRM 51-40-3, N/R 3360.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C CHECK, EVIDENCE OF CORROSION AND SMALL CRACK AT BS 950C FRAME UPPER FLANGE BETWEEN S-26 L AND STR 27 L. CUT OUT DAMAGED AREA AT UPPER FLANGE, HFEC, INSTALLED FRAME REPAIR AT BS 950C PER SRM 51-40-3, N/R 3360.