What was found
LEFT OTBD FLAP UPPER SKIN HAS A 2.875 INCH CRACK AND A .4 INCH CRACK AT XOF 569. 8 INCHES FWD OF TRAILING EDGE. REPAIR IAW SRM 57-00-01, FIG 4, SHT 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT OTBD FLAP UPPER SKIN HAS A 2.875 INCH CRACK AND A .4 INCH CRACK AT XOF 569. 8 INCHES FWD OF TRAILING EDGE. REPAIR IAW SRM 57-00-01, FIG 4, SHT 2.