As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A REPETITIVE HFEC INSPECTION ON NLG LT TRUNNION FITTING, CRACK WAS FOUND PROPAGATING FROM THE PREVIOUSLY TRIM OUT AREA APPROXIMATELY 0.25 INCH LENGTH. CARRIED OUT STOP DRILL IAW SRM 53-10-14 FIGURE 203 REPAIR 2 REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 120.