What was found
CRACK IN THE SUPPORT OF THE LH ENG PANEL NACELLE(<P>CRACK ON SKATE ANGLE WAS REPAIRED PER CMA TLS 24-0209. NO FURTHER DEFECTS NOTED</P>)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK IN THE SUPPORT OF THE LH ENG PANEL NACELLE(<P>CRACK ON SKATE ANGLE WAS REPAIRED PER CMA TLS 24-0209. NO FURTHER DEFECTS NOTED</P>)