What was found
AT C-CHECK, BUTT JOINT BS 259 AFT PANEL INDICATES OVER 10 PERCENT MATERIAL LOSS BETWEEN STRINGER 21R TO 23R. CUT OUT DAMAGED SECTION, INSTALLED REPAIR PER S/B 53-0084. N/R 3043
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, BUTT JOINT BS 259 AFT PANEL INDICATES OVER 10 PERCENT MATERIAL LOSS BETWEEN STRINGER 21R TO 23R. CUT OUT DAMAGED SECTION, INSTALLED REPAIR PER S/B 53-0084. N/R 3043