What was found
FUSELAGE SKIN DAMAGED AT FS 605 BETWEEN STRINGERS 24L TO 25L. RECONTOURED SKIN, PERFORMED EDY CURRENT INSPECTION AND RETURNED EXTERIOR FINISH TO THE ORIGINAL OPERATING CONFIGURATION IAW WVAC EO 601R-53-435OA. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN DAMAGED AT FS 605 BETWEEN STRINGERS 24L TO 25L. RECONTOURED SKIN, PERFORMED EDY CURRENT INSPECTION AND RETURNED EXTERIOR FINISH TO THE ORIGINAL OPERATING CONFIGURATION IAW WVAC EO 601R-53-435OA. (M)