What was found
CRACKS ON DORSAL FIN ATTACH ANGLE OF BS 1406 - 1435 LONGERONS 1- 2L. ATTACH ANGLE WAS REPLACED IAW DWG 591288, REV BD AND SRM 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKS ON DORSAL FIN ATTACH ANGLE OF BS 1406 - 1435 LONGERONS 1- 2L. ATTACH ANGLE WAS REPLACED IAW DWG 591288, REV BD AND SRM 51-30-5.