What was found
#1 ENGINE BLADE #38 HAS .48 INCH NICK ON LEADING EDGE TIP OF AREA A. BLENDED #1 ENG BLADE 38 AREA A TO REPAIRABLE LIMIT PER AMM 72-21-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
#1 ENGINE BLADE #38 HAS .48 INCH NICK ON LEADING EDGE TIP OF AREA A. BLENDED #1 ENG BLADE 38 AREA A TO REPAIRABLE LIMIT PER AMM 72-21-02.