What was found
LEFT ENGINE SPLINE COWL HAS A CRACKED ANGLE BY THE FORWARD HINGE FOR PANEL 412AL AND A POSSIBLE CRACK ON THE ANGLE BY THE FORWARD HINGE FOR PANEL 412AR. REPLACED ANGLES IAW SRM 51-41-00-00-01, AND 51-42-05-02-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT ENGINE SPLINE COWL HAS A CRACKED ANGLE BY THE FORWARD HINGE FOR PANEL 412AL AND A POSSIBLE CRACK ON THE ANGLE BY THE FORWARD HINGE FOR PANEL 412AR. REPLACED ANGLES IAW SRM 51-41-00-00-01, AND 51-42-05-02-01.