What was found
FORWARD END OF RIGHT FOD PANEL ABOVE RIGHT MAIN LANDING GEAR, INBOARD END VERTICAL STIFFENER CRACKED. INSTALLED NEW VERTICAL STIFFENER PER SRM 51-10-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FORWARD END OF RIGHT FOD PANEL ABOVE RIGHT MAIN LANDING GEAR, INBOARD END VERTICAL STIFFENER CRACKED. INSTALLED NEW VERTICAL STIFFENER PER SRM 51-10-01.