As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING L-CHECK, FUSELAGE SKIN CRACKING WAS FOUND ON THE NOSE WHEEL WELL AFT CORNERS. ACCOMPLISHED SECT II INSP WITHIN 6000 CYCLES AFTER SECTION I. REPEAT SECTION II INSPECTIONS AT 1500 CYCLE INTERVALS. PERFORMED FUSELAGE EXTERIOR SKIN REPAIR IAW ER/A 488626-14AD.