What was found
CRACKED RING PAN ON UPPER CORNER FWD OF FRAME BS 889. THE AREA WAS REPAIRED IAW SRM 56-20-02-2R1, FIG 202. HFEC INSPECTION WAS ACCOMPLISHED, NO CRACKS WERE FOUND IAW SPM 06-10-01.001.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED RING PAN ON UPPER CORNER FWD OF FRAME BS 889. THE AREA WAS REPAIRED IAW SRM 56-20-02-2R1, FIG 202. HFEC INSPECTION WAS ACCOMPLISHED, NO CRACKS WERE FOUND IAW SPM 06-10-01.001.