What was found
DURING D-CHECK, FOUND CRACK IN STRAP ALONG FWD EDGE OF MAIN CABIN ENTRY DOOR OUTER PAN BELOW NR 2 STOP FITTING. FABRICATED AND INSTALLED REPAIR IAW SRM 52-01 FIG 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING D-CHECK, FOUND CRACK IN STRAP ALONG FWD EDGE OF MAIN CABIN ENTRY DOOR OUTER PAN BELOW NR 2 STOP FITTING. FABRICATED AND INSTALLED REPAIR IAW SRM 52-01 FIG 2.