As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFT WET AREA AT STA. 1006 UNDER PANEL 242VF HAS CORROSION ON FRAME. REMOVED CORROSION IAW SRM 51-10-02-0G-0. UT THICKNESS INSP. IAW NDT PART 4 51-00-00 PROCEDURE 3. MIN. THICKNESS 0.079'. ORIGINAL MAT. 0.080''. MAT REMOVED 0.001' MAT REMAINING 0.079' FOUND WITHIN LIMITS IAW SRM 53-70-51-1A-1, & DWG 147A5733. TREATED AND PRIMED AREA IAW AMM 51-21-72-37-804 AND AMM 51-21-41-370-802.