What was found
AT C-CHECK, FOUND EXFOLIATION CORROSIION AT STR 20L LAP SEAM, BETWEEN BS 950E AND BS 950F. CUT OUT DAMAGED AREA 4 INCHES BY 2 INCHES 5 INCHES. INSTALLED DOUBLER 11 INCHES BY 7 INCHES AND FILLER 4 INCHES BY 3 INCHES PER SRM 53-30-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, FOUND EXFOLIATION CORROSIION AT STR 20L LAP SEAM, BETWEEN BS 950E AND BS 950F. CUT OUT DAMAGED AREA 4 INCHES BY 2 INCHES 5 INCHES. INSTALLED DOUBLER 11 INCHES BY 7 INCHES AND FILLER 4 INCHES BY 3 INCHES PER SRM 53-30-3.