What was found
FLIGHT CONTROL FLAP LOCKED ALIGNMENT FAULT. ACCOMPLISHED FAULT ISOLATION IAW TSM 27-51-08-810-818A, FOUND INTERCONNECT STRUT OUT OF ADJUSTMENT. ADJUSTED THE STRUT IAW AMM 27-51-44-820-001. PERFORMED BITE TEST OF SFCC 1 AND 2, NO FAULTS INDICATED AND OPS TESTED OK IAW AMM 27-54-00-710-001.