What was found
UPON COMPLIANCE OF 2C INSPECTION TASK 161/162-01Z, THE FRAME 43 CHANNEL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 3674-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPON COMPLIANCE OF 2C INSPECTION TASK 161/162-01Z, THE FRAME 43 CHANNEL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 3674-2.