As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TOP AFT LT CORNER OF THE CTR WING SKIN AT S-1C AND S-2C AT LBBL 60 TO 65 HAS CORROSION ON (3) SPOTS THAT ARE OUT OF THE LIMITS (0.080, 0.070, AND 0.050) OF THE MFG SRM. INSTALLED INTERNAL AND EXTERNAL DOUBLERS IAW AEROTECH STRUCTURES INC" 8110-3 APPROVED DWG R09-010-01 (INITIAL RELEASE) DATED APRIL 20, 2009. (K)