What was found
NR 1 ENGINE HAS TIP CURL ON ONE BLADE. .250" ON L/E THRU .100 ON OUTER EDGE TIP OF BLADE. REMOVED DAMAGED AREA REF AMM 72-31-02. PERFORMED FPI AND EDDY CURRENT IAW AMM 72-31-02, NO FAULTS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 1 ENGINE HAS TIP CURL ON ONE BLADE. .250" ON L/E THRU .100 ON OUTER EDGE TIP OF BLADE. REMOVED DAMAGED AREA REF AMM 72-31-02. PERFORMED FPI AND EDDY CURRENT IAW AMM 72-31-02, NO FAULTS.