What was found
RUDDER INTERNAL STRUCTURE STIFFENER CRACKED 1.500 INCH STA ZR 162.000. REMOVED CRACKED STIFFENER IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW STIFFENER IAW SRM 51-1-21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RUDDER INTERNAL STRUCTURE STIFFENER CRACKED 1.500 INCH STA ZR 162.000. REMOVED CRACKED STIFFENER IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW STIFFENER IAW SRM 51-1-21.