What was found
STIFFENER CORRODED, STAB T/E INNER UPPER SURFACE, HSS 118.9 . REWORKED THE FITTING AREA AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 55-20-09-1A-1, DETAIL III, REV 101. OPS CHECKED GOOD.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
STIFFENER CORRODED, STAB T/E INNER UPPER SURFACE, HSS 118.9 . REWORKED THE FITTING AREA AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 55-20-09-1A-1, DETAIL III, REV 101. OPS CHECKED GOOD.