As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON BS 947 LOWER TRANSITION ANGLE LBL 12; WL 156. CORROSION ON SUPPORT FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS AGE GIVEN THE SRM. REMOVED TRANSITION ANGLE IAW SRM 51-40-02-0G-0, LOCATED AND DRILLED A NEW TRANSITION ANGLE IAW SRM 51-40-05-0G-0 & DGW 149A8110 DWG 149A8117. INSTALLED ANGLE IAW SRM 51-40-05-0G-0 AND DGW 149A8110 DWG 149A8117.