As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
REMOVED DAMAGED INBOARD DORR FRAME AREA, VERIFIED CRACK FREE USING HFEC. FABRICATED AN ANGLE DOUBLER FROM .063 INCH 2024-T3 CLAD MATERIAL. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED ANGLED DOUBLER PER FIGURE B. VERIFIED 8110-3 RECEIVED. REPAIR COMPLETED IAW ECO 1763, DEVIATION A. (M)