What was found
CRACK ON PAN AFT EDGE BETWEEN BEAMS NR 1 AND NR 2 MID CARGO COMPARTMENT DOOR. STOPPED CRACK IAW SRM 52-30-02, FIG 63. FABRICATED AND INSTALLED DOUBLER IAW SRM 52-30-06. AND 51-30-05.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON PAN AFT EDGE BETWEEN BEAMS NR 1 AND NR 2 MID CARGO COMPARTMENT DOOR. STOPPED CRACK IAW SRM 52-30-02, FIG 63. FABRICATED AND INSTALLED DOUBLER IAW SRM 52-30-06. AND 51-30-05.