What was found
THE LT WING INBOARD T.E. FLAP HAD AN 8 INCH CRACK, 20 INCHES FROM THE INBD END, FROM A TIRE RECAP FAILURE. INSTALLED PERMANENT REPAIR TO LT INBOARD T.E. FLAP WEDGE PER SRM 51-70-17 AND ARA 16874. CHECK-C 816-00 LAX.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE LT WING INBOARD T.E. FLAP HAD AN 8 INCH CRACK, 20 INCHES FROM THE INBD END, FROM A TIRE RECAP FAILURE. INSTALLED PERMANENT REPAIR TO LT INBOARD T.E. FLAP WEDGE PER SRM 51-70-17 AND ARA 16874. CHECK-C 816-00 LAX.