What was found
UPON COMPLIANCE 2C INSPECTION TASK 191/192 01Z THE LOWER FUSELAGE SKIN WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR SST-3431/00
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPON COMPLIANCE 2C INSPECTION TASK 191/192 01Z THE LOWER FUSELAGE SKIN WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR SST-3431/00