What was found
INSPECTION FOUND A 1 INCH CRACK IN PLATE AT RT INBOARD MIDFLAP ABOVE AFT END OF NR 5 SPINDLE. THE PLATE WAS REMOVED IAW SRM 51-30-2, PAGE 4. A NEW PLATE WAS INSTALLED IAW SRM 51-10-1 AND 51-10-2, PAGE 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN PLATE AT RT INBOARD MIDFLAP ABOVE AFT END OF NR 5 SPINDLE. THE PLATE WAS REMOVED IAW SRM 51-30-2, PAGE 4. A NEW PLATE WAS INSTALLED IAW SRM 51-10-1 AND 51-10-2, PAGE 1.