What was found
INSPECTION FOUND A 1 INCH CRACK IN LT PYLON TOP SKIN TO FUSELAGE L-ANGLE AT STA 1019. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 54-04.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN LT PYLON TOP SKIN TO FUSELAGE L-ANGLE AT STA 1019. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 54-04.