What was found
RIGHT ENGINE HAS 1 FAN BLADE WITH EVIDENCE OF SHINGLING. REMOVED 2 BLADE SETS WITH EVIDENCE OF SHINGLING. INSTALLED THE 2 BLADE SETS ON THE 1ST STAGE COMPRESSOR IAW MD80 MM 73-33-21 PAGE 401. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT ENGINE HAS 1 FAN BLADE WITH EVIDENCE OF SHINGLING. REMOVED 2 BLADE SETS WITH EVIDENCE OF SHINGLING. INSTALLED THE 2 BLADE SETS ON THE 1ST STAGE COMPRESSOR IAW MD80 MM 73-33-21 PAGE 401. (M)