What was found
INSPECTION FOUND A 1.125 INCH CRACK IN STRINGER 18A OUTBOARD FLANGE AT LT SIDE AFT OF BS 940 FRAME. THE CRACK WAS STOP DRILLED, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW ECRA 5310-03340, SRM 51-10-00 AND BOEING DRAWING 65C27166.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.125 INCH CRACK IN STRINGER 18A OUTBOARD FLANGE AT LT SIDE AFT OF BS 940 FRAME. THE CRACK WAS STOP DRILLED, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW ECRA 5310-03340, SRM 51-10-00 AND BOEING DRAWING 65C27166.