What was found
NR 1 ENGINE BLADE 25 HAS LEADING EDGE DAMAGE. BLENDED NICK OF BLADE 25 NR 1 ENG (AREA 2). INSPECTED BLENDING PROCESS AND ACCOMPLISHED HFEC PER NDT MM. NO CRACKS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 1 ENGINE BLADE 25 HAS LEADING EDGE DAMAGE. BLENDED NICK OF BLADE 25 NR 1 ENG (AREA 2). INSPECTED BLENDING PROCESS AND ACCOMPLISHED HFEC PER NDT MM. NO CRACKS.