What was found
UPON COMPLIANCE 2C INSPECTION TASK 5720-651-01I THE RIGHT WING SKIN SUPPORT ON RIB 20 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPPLACED 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 5720-651-01I THE RIGHT WING SKIN SUPPORT ON RIB 20 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.