What was found
LOWER FUSELAGE LOBE INTERIOR, EXFOLATION ON FAIL SAFE CHORD AFT FRAME WEB AT STA 1562 BL 0.(<P>FAIL-SAFE LOWER CHORD WAS REPLACED PER DWG 146T1223. NO FURTHER DEFECTS NOTED</P>)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LOWER FUSELAGE LOBE INTERIOR, EXFOLATION ON FAIL SAFE CHORD AFT FRAME WEB AT STA 1562 BL 0.(<P>FAIL-SAFE LOWER CHORD WAS REPLACED PER DWG 146T1223. NO FURTHER DEFECTS NOTED</P>)