What was found
INSPECTION FOUND A 5.5 INCH CRACK IN LT WING INBOARD ATTACH ANGLE AT WS XCW 118. THE ANGLE WAS REMOVED IAW SRM 51-33-01. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 57-20-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 5.5 INCH CRACK IN LT WING INBOARD ATTACH ANGLE AT WS XCW 118. THE ANGLE WAS REMOVED IAW SRM 51-33-01. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 57-20-00.