What was found
CABIN INTERIOR, FS 1176 REINFORCEMENT CHORD ANGLE HAS HEAVY TO SEVERE CORROSION. FLOOR LEVEL BETWEEN BL 44 TO 46 LT. REMOVED DAMAGED PORTION OF CHORD ANGLE, INSTALLED NEW SECTION AND SPLICE DOUBLER PER E/A NR 7531028817.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CABIN INTERIOR, FS 1176 REINFORCEMENT CHORD ANGLE HAS HEAVY TO SEVERE CORROSION. FLOOR LEVEL BETWEEN BL 44 TO 46 LT. REMOVED DAMAGED PORTION OF CHORD ANGLE, INSTALLED NEW SECTION AND SPLICE DOUBLER PER E/A NR 7531028817.