Maintenance personnel’s improper installation of the pitch servo bridle cable clamp, which led to binding in the elevator control system that restricted aft yoke movement during the landing approach.

IMPROPER USE OF THE FUEL TANK SELECTOR BY THE PILOT AND HIS IMPROPER USE OF EMERGENCY PROCEDURES, WHICH RESULTED IN FUEL STARVATION AFTER A FUEL TANK HAD EMPTIED. CONTRIBUTING FACTORS WERE: INOPERATIVE FUEL QUANTITY GAUGES, PILOT'S OPERATION WITH KNOWN DEFICIENCIES IN THE AIRCRAFT, DARK NIGHT, TOTAL LOSS OF ELECTRICAL POWER, AND LACK OF SUITABLE TERRAIN FOR A FORCED LANDING.