As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TRIMMED OUT BODY FRAME AND REMOVED DAMAGED PART OF FRAME. FABRICATED REPAIR CHANNELS AND FILLER PER TABLE 1 FROM .063 INCH THICK 7075-T6 CLAD. ALODINED AND PRIMED REPAIR PART. INSTALLED THE REPAIR PARTS MAKING A FRAYING SEAL WITH BMS 5-95 SEALANT IAW SRM 53-10-4, FIGURE 6. (M)