What was found
CRACKED INNER ANGLE ON DORSAL FIN, REF BS 1427 BETWEEN LONGERONS 1 AND 2 RT. ANGLES WERE REPLACED IAW DWG 5912188 AND SRM 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED INNER ANGLE ON DORSAL FIN, REF BS 1427 BETWEEN LONGERONS 1 AND 2 RT. ANGLES WERE REPLACED IAW DWG 5912188 AND SRM 51-30-5.