What was found
FUSELAGE SKIN DAMAGED AT FS 621 BETWEEN STRINGERS 22L AND 25L. RE-CONTOURED SKIN, PERFORMED EDDY CURRENT INSPECTION AND RETURNED EXTERIOR FINISH TO THE ORIGINAL OPERATING CONFIGURATION IAW WVAC EO 601R-53-4350A. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN DAMAGED AT FS 621 BETWEEN STRINGERS 22L AND 25L. RE-CONTOURED SKIN, PERFORMED EDDY CURRENT INSPECTION AND RETURNED EXTERIOR FINISH TO THE ORIGINAL OPERATING CONFIGURATION IAW WVAC EO 601R-53-4350A. (M)