As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TRIMMED OUT DAMAGE STRINGER SECTION. FABRICATED A .090 INCH THICK J AND U-CHANNEL FROM 7075-T6. ALODINED AND APPLIED TWO COATS PRIMER TO ALL BARE ALUMINUM. INSTALLED REPAIR PARTS USING FASTENERS IDENTIFIED IN FIGURE 2. SEALED FAYING SURFACE WITH BMS 5-95 SEALANT. APPLIED CORROSION INHIBITING COMPOUND TO REPAIR AREA. VERIFIED 8110-3 RECEIVED. REPAIR SPLICE COMPLETED IAW ECO 2599, FIGURE 2. (M)