What was found
DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT FOUND FUSELAGE UPPER SKIN DRILLED WITH EXCESS DOUBLER HOLES FS436, WL257, RBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, CHAPTER 51-60 & 51-70.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT FOUND FUSELAGE UPPER SKIN DRILLED WITH EXCESS DOUBLER HOLES FS436, WL257, RBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, CHAPTER 51-60 & 51-70.