What was found
MAIN DECK COMPARMENT, FLOOR SUPPORT STRUCTURE, CLS AT PANEL 251LG CORRODED. DOT 28-13. ACCOMPLISHED STEP 3, EA#:300-5316-27-A3814, PRELIMINARY 1." FABRICATE A REPLACEMENT CLS ADAPTER (P/N:A53275451200) PER AIRBUS DRAWING A53275451 FROM MAXIMUM 2.00 INCH THICK 7050-T7451 PLATE PER AMS4050. ALL DIMENSIONS ARE TO BE PER AIRBUS DRAWING A53275451 AND A53275402. ACCOMPLISHED STEP 11, EA#:300-5316-27-A3814, PRELIMINARY 2. "INSTALL CLS ADAPTER PER AIRBUS DRAWING A53275474". USING EXISTING FASTENERS(HI-LOK). COLLAR. P/N: NSA5075-6 BATCH: 0004291986 SEALANT P/N: 04-001-0109 B/N 0004355128. ACCOMPLISHED REPAIR IN ACCORDANCE WITH UPS E0-92965-REQ1 AND VT-MAE EA 300-5316-27-A3814 REV.- NO FURTHER ACTION REQUIRED.