What was found
LEVEL 1 CORROSION ON BODY LANDING GEAR STRUT AFT SIDE BELOW UPPER TORQUE LINK. CORROSION BLENDED OUT PER OHM 20-10-01 WITHIN LIMITS PER 32-13-38.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEVEL 1 CORROSION ON BODY LANDING GEAR STRUT AFT SIDE BELOW UPPER TORQUE LINK. CORROSION BLENDED OUT PER OHM 20-10-01 WITHIN LIMITS PER 32-13-38.