What was found
UPON COMPLIANCE 2C INSPECTION TASK 163/164 - 01Z THE HALF FRAME 46A WAS FOUND TO BE CRACKED.THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 2400-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPON COMPLIANCE 2C INSPECTION TASK 163/164 - 01Z THE HALF FRAME 46A WAS FOUND TO BE CRACKED.THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 2400-3.