As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SPOILER CABLE S-23 BROKEN IN LT WHEEL WELL. REPLACED CABLES S-23 AND S-24. COMPLIED WITH SPOILER ADJ/TEST IAW WORK PACK 60172912. PERFORMED VISUAL INSPECTION OF SPOILER HYDRAULIC CONTROL LIMIT SWITCH CONNECTOR, P1-1036. FOUND CONNECTOR AND WIRING NEAR CONNECTOR DEGRADED. REPLACED P1-1036 AND SPLICED IN NEW SECTION OF WIRING IAW DC-8 WDM 27-62-01. OPS CHECKED ON ADJ/TEST.