As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-CK, FOUND UPPER SECTION OF LT MAIN LANDING GEAR WHEEL WELL HAS A CRACK IN INNER SKIN NEAR ATTACH ANGLE ON O/B SIDE AT WL 200 STA 507. CRACK MEASURED 2 INCH LENGTH. FOUND CRACK OUT OF LIMITS, CUT OUT AREA FABRICATED AND INSTALLED FILLER TO EXISTING DOUBLER IAW LAC SRM 51-70-01, 53-60,02 AND 51-140-02.