What was found
CRACK ON DOUBLER FWD/AFT END AT BEAM NR 1 L1 DOOR. FWD/AFT END AT BEAM NR 1 WERE REPIRED IAW SRM 52-10-02, FIG 201, REPAIR 7. CRACKS LONG .656 AND .468".
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON DOUBLER FWD/AFT END AT BEAM NR 1 L1 DOOR. FWD/AFT END AT BEAM NR 1 WERE REPIRED IAW SRM 52-10-02, FIG 201, REPAIR 7. CRACKS LONG .656 AND .468".