What was found
APU ENCLOSURE BOTH INTERNAL UPPER STIFFENERS WELDS ARE CRACKED AT AFT FLANGE FORWARD SIDE. REPAIRED APU ENCLOSURE INTERNAL UPPER STIFFENERS IAW SUP: 16-168 AND EA CRJ249-00441 AND SUP: 16-206.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
APU ENCLOSURE BOTH INTERNAL UPPER STIFFENERS WELDS ARE CRACKED AT AFT FLANGE FORWARD SIDE. REPAIRED APU ENCLOSURE INTERNAL UPPER STIFFENERS IAW SUP: 16-168 AND EA CRJ249-00441 AND SUP: 16-206.