What was found
LEFT VERTICAL STABILIZER CHINE ANGLE IS CRACKED .250 INCH BY .010 AND HAS WORKING RIVETS. SUBMITTER SUGGESTED CAUSE AS FATIGUE/VIBRATION AND RECOMMENDED A DETAILED INSPECTION BE CALLED OUT DURING C-CHECK INSPECTION.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT VERTICAL STABILIZER CHINE ANGLE IS CRACKED .250 INCH BY .010 AND HAS WORKING RIVETS. SUBMITTER SUGGESTED CAUSE AS FATIGUE/VIBRATION AND RECOMMENDED A DETAILED INSPECTION BE CALLED OUT DURING C-CHECK INSPECTION.