What was found
DURING D-CK, LT MLG DOOR PAN RADIUS UP FWD CORNER HAS CRACK AT PREV DOUBLR. MAINT REPAIRED IAW SRM 51-30-2, 52-05 FIG 15.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING D-CK, LT MLG DOOR PAN RADIUS UP FWD CORNER HAS CRACK AT PREV DOUBLR. MAINT REPAIRED IAW SRM 51-30-2, 52-05 FIG 15.