What was found
CF III INTERNAL SIDE FUSELAGE SKIN CORROSION ON SHEAR CLIPS AT FR 88 STRINGER 27R/28R. (C-CHECK RO 2/27/2025) REMOVED AND REPLACEDSHEAR CLIPS AT FR 88 STRINGER 27R/28R REF SRM 51-40-08. NO CHANGE IN WEIGHT CAUSED BY REPAIRS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CF III INTERNAL SIDE FUSELAGE SKIN CORROSION ON SHEAR CLIPS AT FR 88 STRINGER 27R/28R. (C-CHECK RO 2/27/2025) REMOVED AND REPLACEDSHEAR CLIPS AT FR 88 STRINGER 27R/28R REF SRM 51-40-08. NO CHANGE IN WEIGHT CAUSED BY REPAIRS.