What was found
LEFT OTBD FLAP UPPER SURFACE 2 CRACKS ON THE SKIN .120 TO .250 INCHES IN LENGTH APPROX XOF 560. REMOVED DAMAGE & INSTALLED DOUBLER IAW SRM 57-00-01 FIG 4 SHEET 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT OTBD FLAP UPPER SURFACE 2 CRACKS ON THE SKIN .120 TO .250 INCHES IN LENGTH APPROX XOF 560. REMOVED DAMAGE & INSTALLED DOUBLER IAW SRM 57-00-01 FIG 4 SHEET 2.