What was found
LEFT ENGINE NACELLE AFT OUTBOARD SUPPORT ANGLE CRACKED APPROX 1.5 INCHES LENGTH AND EMANATING INTO ANGLE RADIUS / R & R'D #1 ENG. AFT O/B SUPPORT ANGLE IAW SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT ENGINE NACELLE AFT OUTBOARD SUPPORT ANGLE CRACKED APPROX 1.5 INCHES LENGTH AND EMANATING INTO ANGLE RADIUS / R & R'D #1 ENG. AFT O/B SUPPORT ANGLE IAW SRM 51-40-02.