What was found
LEFT FORWARD MAIN FRAME AT FUSELAGE STA 699 WAS CRACKED BEYOND LIMITS OF DC-9 S/B 53-131. CRACK RAN BETWEEN POINTS G - J. REPLACED FRAME IAW ABX EA 53400321-001-4, WO 600204273.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT FORWARD MAIN FRAME AT FUSELAGE STA 699 WAS CRACKED BEYOND LIMITS OF DC-9 S/B 53-131. CRACK RAN BETWEEN POINTS G - J. REPLACED FRAME IAW ABX EA 53400321-001-4, WO 600204273.