What was found
CENTER FUSELAGE 3 STINGER20R HAS CORROSION AROUND 2 RIVET HEAD AT FRAME 88-89. PERFORMED PERMANENT REINFORCING REPAIR REF. ETD2026-170-016500 REV. B
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CENTER FUSELAGE 3 STINGER20R HAS CORROSION AROUND 2 RIVET HEAD AT FRAME 88-89. PERFORMED PERMANENT REINFORCING REPAIR REF. ETD2026-170-016500 REV. B