As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
C-CHECK - FORE RUDDER CTR HINGE COVER, SKIN SUPPORT ANGLE IS CRACKED. REMOVED CRACKED SUPPORT ANGLE RIB, FABRICATED, LOCATED AND DRILLED UP NEW ANGLE RIB USING 2024T3 .025" MATERIAL IAW SRM 55-41-10 PG 2 ITEM 25 AND B DIRECT DWG NR 85547208. PERFORMED HFEC INSP OF FABRICATED BRACKET IAW 1-84-7A PT-6, 51-00-01, NO CRACKS NOTED. ALODINED AND PRIMED ANGLE RIB IAW SRM 51-20-00. INSTALLED ANGLE RIB IAW SRM 51-42-05. ALL WORK PERFORMED IAW EC 6-55-207.