What was found
DURING CHECK-C MAINT, THE ATTACH ANGLE ON BOTTOM OF DORSAL FIN CRACKED THROUGH THE SCREW HOLE, LT SIDE APROX STA 1420. INSTALLED REPAIR ANGLE PER SRM 53-01 PAGE 0 WITH FASTENERS PER SRM 51-10-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CHECK-C MAINT, THE ATTACH ANGLE ON BOTTOM OF DORSAL FIN CRACKED THROUGH THE SCREW HOLE, LT SIDE APROX STA 1420. INSTALLED REPAIR ANGLE PER SRM 53-01 PAGE 0 WITH FASTENERS PER SRM 51-10-3.