What was found
A 1 INCH CRACK WAS LOCATED AT BS 4010 AFT OF FORWARD LOWER ENGINE COWLING LATCH. CRACK ORIGINATED AT THE 90 DEGREE BEND OF THE BASE TO THE EDGE OF THE MATERIAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A 1 INCH CRACK WAS LOCATED AT BS 4010 AFT OF FORWARD LOWER ENGINE COWLING LATCH. CRACK ORIGINATED AT THE 90 DEGREE BEND OF THE BASE TO THE EDGE OF THE MATERIAL.