What was found
(CAN) VERTICAL STAB LEADING EDGE PANEL 322B1 CRACKED APPROXIMATELY 5 INCHES UP FROM LOWER EDGE. LT SIDE. THE DAMAGE IS WITHIN REPAIR LIMITS WILL BE REPAIRED AS PER SRM 55-30-00, PA 200, OR REPLACED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) VERTICAL STAB LEADING EDGE PANEL 322B1 CRACKED APPROXIMATELY 5 INCHES UP FROM LOWER EDGE. LT SIDE. THE DAMAGE IS WITHIN REPAIR LIMITS WILL BE REPAIRED AS PER SRM 55-30-00, PA 200, OR REPLACED.