As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND SEVERAL POPPED RIVETS AND THE FUSELAGE SKIN CRACKED IN 2 AREAS. ONE CRACK WAS .375 INCH AND THE SECOND WAS .3125 INCH, WITH CORROSION AT LAP SEAM STA 490, STRINGER 18. REPAIRED FUSELAGE LAP SEAM SPLICE PER 727 SRM 53-30-3, FIG 5 SHEET 5. CHECK-C 9-7-99 MCI.