What was found
CRACK ON UPPER AFT RING PAN STA Y=832 LH AT PAX, CABIN. UPPER AFT RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK L =0.510". HFEC WAS PERFORMED ON TRIMMED AREA AND NO CRACKS WERE FOUND AT TIME OF INSPECTION.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON UPPER AFT RING PAN STA Y=832 LH AT PAX, CABIN. UPPER AFT RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK L =0.510". HFEC WAS PERFORMED ON TRIMMED AREA AND NO CRACKS WERE FOUND AT TIME OF INSPECTION.