Alaska Airlines Flight 779

The DC-6A was chartered by the Military Air Transport Service to carry cargo from Travis Air Force Base to Tachikawa, Japan with refueling stopovers in Anchorage and Shemya. On July 20, the flight departed Everett without cargo en route to Travis Air Force Base. Upon arrival in Travis military personnel loaded 25,999 pounds (11,793 kg) of cargo onto the aircraft under the supervision of the flight engineer. The flight then departed Travis en route to Alaska, for the purpose of refueling and picking up the navigator from Anchorage. It took 8 hours and 59 minutes for the flight to arrive at Anchorage from Travis. The aircraft was at Anchorage Airport for an hour and 8 minutes. The time from takeoff in Anchorage to the crash was 6 hours and 30 minutes. In Anchorage, the crew was given weather information for the route to Shemya but were not notified of the approach and field lighting deficiencies. Wind at speeds of 20 knots were present at an altitude of approximately 500 feet. At 02:12, when the observer of the U. S. Weather Bureau was notified, the weather conditions as follows were recorded: Indefinite 200-foot variable ceiling; visibility 3/4 mile variable, fog; temperature 45°; dewpoint 45°, wind south-southeast 8 knots; altimeter setting 29.84; ceiling 100 feet variable to 300 feet, visibility 1/2 mile variable to one mile. == Aircraft ==

The aircraft involved was a Douglas DC-6A equipped with four Pratt & Whitney R2800 CB17 engines with registration number N6118C. It was manufactured in a cargo configuration for Alaska Airlines on 20 October 1957 with serial number 45243. At the time of the accident, it had accumulated 10,600 air frame hours and had undergone a major inspection 146 hours prior to the accident. == Investigation ==

The investigation revealed that the aircraft was in full working order when it crashed, in line with federal regulations and company procedures. All four engines were running when it crashed. Fuel management logs and main tank gauges showed that there was adequate supply of fuel to the engines prior to the crash. Control surfaces and aircraft structures were shown to be functional prior to the crash with no evidence of mechanical malfunction. == Causes ==

The investigation revealed that the approach lights for the runway were not lit on the night of the crash. The pilot could not have known that only one strobe light was lit because the air traffic controller failed to adequately inform of the status of the runway lights. == References ==