What was found
DURING CHECK-C MAINT, FOUND TAIL TO FUSELAGE ANGLE IN DORSAL FIN CRACKED FROM SCREW HOLE TO EDGE, ON RT SIDE AT STA 1081. REMOVED CRACKED ANGLE AND REPLACED WITH NEW ANGLE (P/N SR09530162-4), PER SB 53-223 REV 2, AND ARA 15725.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CHECK-C MAINT, FOUND TAIL TO FUSELAGE ANGLE IN DORSAL FIN CRACKED FROM SCREW HOLE TO EDGE, ON RT SIDE AT STA 1081. REMOVED CRACKED ANGLE AND REPLACED WITH NEW ANGLE (P/N SR09530162-4), PER SB 53-223 REV 2, AND ARA 15725.