What was found
CRACK ON UPPER/AFT WINDOW RING PAN STA 851. DAMAGE WAS REPAIRED IAW SRM 56-20-02. REPAIR 1, 51-41-02, 51-41-05, 51-20-09, AND 51-10-04 PAR 15 AND 21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON UPPER/AFT WINDOW RING PAN STA 851. DAMAGE WAS REPAIRED IAW SRM 56-20-02. REPAIR 1, 51-41-02, 51-41-05, 51-20-09, AND 51-10-04 PAR 15 AND 21.