What was found
DURING SCHEDULED C2 CHECK, FOUND CORROSION VERTICAL FIN STA 87.00 TRAILING EDGE CHORD LT AND RT SKIN ATTACH ANGLES. CORROSION BEYOND LIMIT. REPAIRED EXTRUDED PARTS IAW SRM 51-40-4, 51-30-2 & 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED C2 CHECK, FOUND CORROSION VERTICAL FIN STA 87.00 TRAILING EDGE CHORD LT AND RT SKIN ATTACH ANGLES. CORROSION BEYOND LIMIT. REPAIRED EXTRUDED PARTS IAW SRM 51-40-4, 51-30-2 & 3.