What was found
UPON COMPLIANCE 2C INSPECTION TASK 811-02Z THE PAX DOOR INNER SKIN WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 3840-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPON COMPLIANCE 2C INSPECTION TASK 811-02Z THE PAX DOOR INNER SKIN WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 3840-1.