What was found
RIGHT SIDE FUSELAGE SKIN DAMAGED BETWEEN STA 228.5 AND 236.5. REMOVED DAMAGE BY BLENDING IAW SRM 53-00-01-1A-1. HFEC, NO CRACK. C/W EO 767-5330-49395A INTERIM REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT SIDE FUSELAGE SKIN DAMAGED BETWEEN STA 228.5 AND 236.5. REMOVED DAMAGE BY BLENDING IAW SRM 53-00-01-1A-1. HFEC, NO CRACK. C/W EO 767-5330-49395A INTERIM REPAIR.