What was found
UPON COMPLIANCE OF 2C INSPECTION TASK 261/262-01Z, THE FRAME 40 SKIN SUPPORT WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW 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 OF 2C INSPECTION TASK 261/262-01Z, THE FRAME 40 SKIN SUPPORT WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.