What was found
INSPECTION FOUND A 0.7 CRACK AT FORWARD END OF BEAM NR 2 FASTENER LOCATION OF FORWARD CARGO COMPARTMENT DOOR OUTER PAN. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-03, FIGURE 8.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 0.7 CRACK AT FORWARD END OF BEAM NR 2 FASTENER LOCATION OF FORWARD CARGO COMPARTMENT DOOR OUTER PAN. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-03, FIGURE 8.