What was found
HPT 2ND STG BLADE HAS AN AXIAL CRACK IN AREA B, FROM THE T/E COOLING SLOTS IN TOWARDS MIDDLE OF BLADE. REPLACE NR 1 ENGINE REF EG3710-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
HPT 2ND STG BLADE HAS AN AXIAL CRACK IN AREA B, FROM THE T/E COOLING SLOTS IN TOWARDS MIDDLE OF BLADE. REPLACE NR 1 ENGINE REF EG3710-1.