What was found
DURING REMOVAL OF STRINGER 26 LT DRILLING MARK EXISTS BETWEEN C38.2-39. REPAIR PERFORMED BY BUSH INSTALLATION IAW SRM 53-10-12 FIG 221.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING REMOVAL OF STRINGER 26 LT DRILLING MARK EXISTS BETWEEN C38.2-39. REPAIR PERFORMED BY BUSH INSTALLATION IAW SRM 53-10-12 FIG 221.