What was found
INSPECTION FOUND STIFFENER CRACKED AT LT WING TRAILING EDGE FALSE SPAR WHERE FLAP TRACK NR 3 IS LOCATED. THE STIFFENER WAS REMOVED IAW SRM 51-30-2. A NEW STIFFENER WAS FABRICATED AND INSTALLED IAW SRM 51-20-1, 51-10-2, AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND STIFFENER CRACKED AT LT WING TRAILING EDGE FALSE SPAR WHERE FLAP TRACK NR 3 IS LOCATED. THE STIFFENER WAS REMOVED IAW SRM 51-30-2. A NEW STIFFENER WAS FABRICATED AND INSTALLED IAW SRM 51-20-1, 51-10-2, AND 51-30-2.