What was found
DURING C- CHECK INSPECTION WHILE ACCOMPLISHING A.D. 89-08-10; S.B.'S A53-154 AND A53-223, FOUND THE RIGHT DORSAL FIN ATTACH ANGLE CRACKED. REPLACED THE ANGLE IAW DC-9 SRM 53-05-23.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C- CHECK INSPECTION WHILE ACCOMPLISHING A.D. 89-08-10; S.B.'S A53-154 AND A53-223, FOUND THE RIGHT DORSAL FIN ATTACH ANGLE CRACKED. REPLACED THE ANGLE IAW DC-9 SRM 53-05-23.