What was found
INSPECTION FOUND A 1 INCH CRACK AT EACH END OF LT PYLON PANEL NR 8111C ATTACH SUPPORT ANGLE. THE SUPPORT ANGLE WAS REMOVED AND A NEW SUPPORT ANGLE WAS INSTALLED IAW SRM 51-10-3 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK AT EACH END OF LT PYLON PANEL NR 8111C ATTACH SUPPORT ANGLE. THE SUPPORT ANGLE WAS REMOVED AND A NEW SUPPORT ANGLE WAS INSTALLED IAW SRM 51-10-3 AND 51-30-2.