What was found
NR 1 ENGINE, 1ST STAGE COMPRESSOR BLADE NR 34 HAS NICK 2.6250 INCHES FROM TIP AREA A. BLENDED 1ST STAGE BLADE AIRFOIL IAW AMM 72-31-02. REPAIR WITHIN LIMITS. EDDY CURRENT INSPECTION OK.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 1 ENGINE, 1ST STAGE COMPRESSOR BLADE NR 34 HAS NICK 2.6250 INCHES FROM TIP AREA A. BLENDED 1ST STAGE BLADE AIRFOIL IAW AMM 72-31-02. REPAIR WITHIN LIMITS. EDDY CURRENT INSPECTION OK.