If anyone is interested in technical aspects of an APU:
Each auxiliary power unit consists of a fuel tank, a fuel feed system, a system controller, an exhaust duct, lube oil cooling system, and fuel/lube oil vents and drains. Redundant electrical heater systems and insulation thermally control the system above 45 F to prevent fuel from freezing and to maintain required lube oil viscosity. Insulation is used on components containing hydrazine, lube oil or water to minimize electrical heater power requirements and to keep high surface temperatures within safe limits on the turbine and exhaust ducts. "
There may have been a short in a Load Control Assembly which affected one of two heaters in APU 1, which could have led to hydraulic failure in control surfaces of the orbitor. Therefore, a minimum of a 72 hour turnaround is necessary to troubleshoot the problem, according to the launch director.