As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
2 INCH CRACK ON R4 DOOR INNER SKIN 10 INCHES FROM FWD EDGE & 31 INCHES FROM TOP EDGE. CUTOUT DAMAGE AREA ON R4 DOOR INNER SKIN 10 INCHES FROM FWD EDGE & 31" FROM TOP EDGE. FABRICATED DOUBLER & SHIM, INSTALLED IAW SRM 20-41-02 & 51-70-13 FIG 1.