What was found
RIGHT PYLON INTERNAL NACELLE AREA ANGLE CRACKED AT STA 200.00. R & R ANGLE IAW SRM & DWG.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT PYLON INTERNAL NACELLE AREA ANGLE CRACKED AT STA 200.00. R & R ANGLE IAW SRM & DWG.