FAILURE OF THE ENGINE-DRIVEN FUEL PUMP, WHICH RESULTED IN THE LOSS OF POWER, AND THE LACK OF AIRCRAFT FLOTATION EQUIPMENT. FACTORS RELATED TO THE ACCIDENT WERE: FLIGHT OVER WATER ADJACENT TO TERRAIN THAT AFFORDED NO SUITABLE FORCED LANDING SITE, AND THE LACK OF A PASSENGER BRIEFING BY THE OPERATOR ON THE LOCATION AND OPERATION OF LIFE PRESERVERS.