What was found
SURFACE CORROSION ON FUSELAGE SKIN BETWEEN BS 1060-1079 LONGERONS 28L - 29R. CORROSION REMOVED IAW SRM 51-30-2, 51-10-3 PARR. 26. AREA WAS TREATED AND PAINTED IAW SRM 51-10-3 PARR/ 14 AND 21, WITHIN LIMITS IAW SRM 53-04-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SURFACE CORROSION ON FUSELAGE SKIN BETWEEN BS 1060-1079 LONGERONS 28L - 29R. CORROSION REMOVED IAW SRM 51-30-2, 51-10-3 PARR. 26. AREA WAS TREATED AND PAINTED IAW SRM 51-10-3 PARR/ 14 AND 21, WITHIN LIMITS IAW SRM 53-04-02.