What was found
DURING C-CHECK, FOUND RUDDER SKIN CRACKED .875 INCH AT TOP CLOSEOUT RIB MIDPOINT OF RUDDER. INSTALLED FLUSH REPAIR IAW SRM 55-03 FIG 8A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK, FOUND RUDDER SKIN CRACKED .875 INCH AT TOP CLOSEOUT RIB MIDPOINT OF RUDDER. INSTALLED FLUSH REPAIR IAW SRM 55-03 FIG 8A.