What was found
FUSELAGE SKIN AT BS 1016 BETWEEN S21 - 22L IS CORRODED IN PREVIOUSLY BLENDED AREA. REPAIRED THE SKIN IAW SRM 51-10-01 FIGURE 2 DETAIL A AND EA 265041.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN AT BS 1016 BETWEEN S21 - 22L IS CORRODED IN PREVIOUSLY BLENDED AREA. REPAIRED THE SKIN IAW SRM 51-10-01 FIGURE 2 DETAIL A AND EA 265041.