What was found
INSPECTION FOUND A 1.5 INCH CRACK IN LT WING INBOARD FLAP INNER SKIN AT AFT END OF OPENING FOR UPPER ACCESS PANEL NR 8443. A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.5 INCH CRACK IN LT WING INBOARD FLAP INNER SKIN AT AFT END OF OPENING FOR UPPER ACCESS PANEL NR 8443. A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.