What was found
NR 1 SLAT HAS DAMAGE 41" FROM THE OB END ON THE UPPER SKIN. REPAIRED IAW ENGINEERING REPAIR 06-3471.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 1 SLAT HAS DAMAGE 41" FROM THE OB END ON THE UPPER SKIN. REPAIRED IAW ENGINEERING REPAIR 06-3471.