As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C LOWER FUSELAGE SKIN BULGING AT L36, STA 380 TO 400. REMOVED SPLICE FITTING AT L36, STA 380 TO 400. REMOVED CORROSION ON L36 PER SRM 51-1-8. NO CORROSION FOUND ON SKIN. NDT REVEALED CRACK ON L36 FROM STA 390-394. FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION PER SRM 53-4-1 FIG 28. INSTALLED NEW SPLICE FITTING.