What was found
ON THE NR 2 ENGINE, J10 HARNESS ABOVE RT THRUST LINK ATTACH BRACKET WORN THROUGH OUTER AND METAL BRAID. GROUNDED-YES. REPLACED NR 2 ENGINE HARNESS ASSEMBLY, REF B737-900 AMM 73-21-06-802-F00 PARAGRAPH 5E. POWER RE-APPLIED, ACCOMPLISHED ALL J10 HARNESS INSTALLATION TESTS. ALL TESTS PASS, REF AMM 73-21-06, 73-21-00.