What was found
UPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE CENTER FWD BUTT PLATE WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 1671-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE CENTER FWD BUTT PLATE WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 1671-1.