What was found
COVER IS CRACKED ACROSS EXTERIOR SURFACE FROM THE SHAFT HOLE OUTWARD. POSSIBLE CAUSE, STRESS, FATIGUE AND/OR WEAK POINT IN DESIGN OF COVER. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
COVER IS CRACKED ACROSS EXTERIOR SURFACE FROM THE SHAFT HOLE OUTWARD. POSSIBLE CAUSE, STRESS, FATIGUE AND/OR WEAK POINT IN DESIGN OF COVER. (X)