What was found
EVIDENCE OF CORROSION AT BS 351 STRINGER 26R EXTERIOR. INSTALLED FUSEALGE EXTERIOR SKIN REPAIR AT BS 351, STRINGER 26R. MATERIAL USED, 2024-T3, .063 INCH , 19 INCH BY 11 INCH. REPAIR ACCOMPLISHED IAW SRM 53-30-3 FIG 1. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
EVIDENCE OF CORROSION AT BS 351 STRINGER 26R EXTERIOR. INSTALLED FUSEALGE EXTERIOR SKIN REPAIR AT BS 351, STRINGER 26R. MATERIAL USED, 2024-T3, .063 INCH , 19 INCH BY 11 INCH. REPAIR ACCOMPLISHED IAW SRM 53-30-3 FIG 1. (M)