What was found
AFT FUSELAGE BS 1508 FRAME TO SKIN ATTACH ANGLE CRACKED BETWEEN L1 AND L2R. REMOVED AND REPLACED CRACKED ANGLE AT STA 1508 IAW SRM 51-30-02 PG 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT FUSELAGE BS 1508 FRAME TO SKIN ATTACH ANGLE CRACKED BETWEEN L1 AND L2R. REMOVED AND REPLACED CRACKED ANGLE AT STA 1508 IAW SRM 51-30-02 PG 1.