What was found
FOUND CRACK IN VERTICAL STIFFENER STA 92.7 APPROX 24" AFT OF REAR SPAR. FABRICATED NEW STIFFENER AND INSTALLED IAW SRM 51-10-02, DEFECT SIZE: .500".
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND CRACK IN VERTICAL STIFFENER STA 92.7 APPROX 24" AFT OF REAR SPAR. FABRICATED NEW STIFFENER AND INSTALLED IAW SRM 51-10-02, DEFECT SIZE: .500".