What was found
INSPECTION FOUND A 1 INCH CRACK IN LT PYLON NAC STA 285 AREA I/B STIFFENER AFTER FRAME CHORD REMOVAL. THE STIFFENER WAS REPLACED IAW ECRA 5420-01445.
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 NAC STA 285 AREA I/B STIFFENER AFTER FRAME CHORD REMOVAL. THE STIFFENER WAS REPLACED IAW ECRA 5420-01445.