What was found
INSIDE SKIN CRACKED AT RIVET IN APU INLET DUCT FOR I/B Z-ANGLE STIFFENER TOP END. REPAIRED PART BY WELDING PER BAC 5975 IAW ENGINEERING RESPONSE; HFEC INSPECTED - NO CRACKS NOTED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSIDE SKIN CRACKED AT RIVET IN APU INLET DUCT FOR I/B Z-ANGLE STIFFENER TOP END. REPAIRED PART BY WELDING PER BAC 5975 IAW ENGINEERING RESPONSE; HFEC INSPECTED - NO CRACKS NOTED.