What was found
INSPECTION FOUND A 1.5 INCH CRACK IN STIFFENER INSIDE VERTICAL FIN ABOVE S DUCT AREA AT BS 1303-1323, BL 0. A NEW STIFFENER WAS INSTALLED IAW SRM 51-10-1, PAGE 2 AND 51-30-2, PAGE 4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.5 INCH CRACK IN STIFFENER INSIDE VERTICAL FIN ABOVE S DUCT AREA AT BS 1303-1323, BL 0. A NEW STIFFENER WAS INSTALLED IAW SRM 51-10-1, PAGE 2 AND 51-30-2, PAGE 4.