As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON THE FUSELAGE SKIN AT S-43L BETWEEN STA 1700 - STA 1720(<P>1) REMOVED EXISTING REPAIR PARTS IAW SRM 51-40-02-0G-0 REV 97. 2) PERFORM EI T2023A53M-870 SEQUENCE A REV 0. 3) ACCOMPLISHED EI T2023A53M-870 REV 1 AND CONDITION CHECK NORMAL. 4) RECORD THE REPAIR DOUBLER IS CONFIGURATION 2 REFER TO EO 4453B088 PART 2 STEP 4 REV 11 AND JOB COMPLETED</P>)