What was found
RIGHT WING, NR 7 SLAT HAS A CRACK AT ACTUATOR ATTACH POINT. VERIFIED WITH HFEC PART 6 51-00-00, PROCEDURE 23. C/W SLAT INSPECTION NO FOD FOUND. R & R NR 6 L/E SLAT AND TORQUED IAW AMM 27-81-21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT WING, NR 7 SLAT HAS A CRACK AT ACTUATOR ATTACH POINT. VERIFIED WITH HFEC PART 6 51-00-00, PROCEDURE 23. C/W SLAT INSPECTION NO FOD FOUND. R & R NR 6 L/E SLAT AND TORQUED IAW AMM 27-81-21.