What was found
UPON COMPLIANCE 2C INSPECTION TASK 141/142 - 01Z THE FRAME 23 SKIN SUPPORT WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPON COMPLIANCE 2C INSPECTION TASK 141/142 - 01Z THE FRAME 23 SKIN SUPPORT WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.