What was found
ENGINE HAS ONE EACH T2 BLADE WITH AXIAL CRACK IN AREA 'B' ON LEADING EDGE. WASHED T2 BLADE AND REINSPECTED AND CONFIRMED CRACK. AXIAL CRACKS AREA 'B' NOT PERMITTED. REMOVED ENGINE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ENGINE HAS ONE EACH T2 BLADE WITH AXIAL CRACK IN AREA 'B' ON LEADING EDGE. WASHED T2 BLADE AND REINSPECTED AND CONFIRMED CRACK. AXIAL CRACKS AREA 'B' NOT PERMITTED. REMOVED ENGINE.