What was found
ETOPS SIGNIFICANT SYSTEM - NR 2 ENG CIRCUMFERENTIAL & AXIAL CRACKS ON 1ST STAGE HPT BLADE DUCT SEGMENT AFT FACE. CRACK LENGTH APPROX 3/4 OF THE DISTANCE BETWEEN TWO TURBINE VANES. ACCOMPLISHED PER HAL M105 583082. OK FOR SERVICE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ETOPS SIGNIFICANT SYSTEM - NR 2 ENG CIRCUMFERENTIAL & AXIAL CRACKS ON 1ST STAGE HPT BLADE DUCT SEGMENT AFT FACE. CRACK LENGTH APPROX 3/4 OF THE DISTANCE BETWEEN TWO TURBINE VANES. ACCOMPLISHED PER HAL M105 583082. OK FOR SERVICE.