What was found
CRACK ON INTERNAL PAN AT FWD CARGO COMPARTMENT DOOR UPPER FWD CORNER. CRACK WAS STOP DRILLED. INSTALLED REPAIR IAW SRM 52-03D, FIG 8, 51-10-2, 51-30-5 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON INTERNAL PAN AT FWD CARGO COMPARTMENT DOOR UPPER FWD CORNER. CRACK WAS STOP DRILLED. INSTALLED REPAIR IAW SRM 52-03D, FIG 8, 51-10-2, 51-30-5 AND 51-30-2.