What was found
FUSELAGE UPPER LOBE INTERIOR STRUCTURE, CORROSION ON GILL LINER SUPPORT AT STA 1180, RBL68, AT STRINGER R9. REMOVED CORROSION AND INSTALLED REPAR DOUBLER AND FILLER REF SRM 1-40-23 FIG 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE UPPER LOBE INTERIOR STRUCTURE, CORROSION ON GILL LINER SUPPORT AT STA 1180, RBL68, AT STRINGER R9. REMOVED CORROSION AND INSTALLED REPAR DOUBLER AND FILLER REF SRM 1-40-23 FIG 1.