What was found
REPAIRED OIL-CANNED AREA OF 3.9" BY 1.6" OF THE UPPER INBOARD AFT WIN SKIN TRAILING EDGE, AT THE FLAP CUTOUT, BY INSTALLING .040" THICK 2024-T3 REINFORCING DOUBLER PER ENGINEERING ORDER.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
REPAIRED OIL-CANNED AREA OF 3.9" BY 1.6" OF THE UPPER INBOARD AFT WIN SKIN TRAILING EDGE, AT THE FLAP CUTOUT, BY INSTALLING .040" THICK 2024-T3 REINFORCING DOUBLER PER ENGINEERING ORDER.