What was found
REMOVED PREVIOUS REPAIR STRAP THAT WAS INBD OF CRACKED SKIN AT RIVET HOLE & FABRICATED NEW EXTENDED REPAIR STRAP TO INCORPORATE THREE EXTRA RIVET HOLES. THE NEW REPAIR STRIP IS MADE USING 0.050 INCH THICK 2024-T3 ALUMINUM. THE REPAIR STRIP & LE SKIN WERE PREPARED FOR BONDING & ATTACHED USING EA9394 ADHESIVE & NAS1097AD5 SOLID RIVETS. REFERENCE REPAIR IAW DERT-635514-NM ON FAA FORM 8110-3 & SKETCH BB-289-2014-001, DATED SEPTEMBER 25, 2014.