What was found
L1 DOOR TOP HINGE ARM FUSELAGE ATTACH POINT TOO LONG AND EXTERNAL SKIN DAMAGED TWO PLACES. REPAIRED BOLT BY ADDING WASHER IAW BOEING SRM 51-30-02 AND BLENDED DAMAGED SKIN IAW BOEING SRM 51-10-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
L1 DOOR TOP HINGE ARM FUSELAGE ATTACH POINT TOO LONG AND EXTERNAL SKIN DAMAGED TWO PLACES. REPAIRED BOLT BY ADDING WASHER IAW BOEING SRM 51-30-02 AND BLENDED DAMAGED SKIN IAW BOEING SRM 51-10-01.