United States of America

The wind direction shifted from east to south while the crew were preparing to land at runway 08. The captain decided to initiate a landing on runway 26. The sink rate during the approach became unsatisfactory and a go around was attempted. The aircraft was in a right turn at 150 feet when the plane settled and crashed in the Chuckchi Sea, some 300 yards from the runway. Both pilots survived the impact, but one of them drowned in the 27° F water. Downdrafts in the area north of the runway probably caused the plane to settle. Downdrafts were known to exist when the wind is southerly. The phenomena is caused by high terrain surrounding the strip on all sides except the north.

The crew was engaged in a training flight out from Westover AFB. While cruising at low height, control was lost. Three crew members were able to bail out before the aircraft crashed in the Elephant Mountain Range located near Greenville. Seven crew members were killed while two survived.
Crew (99th BS):
Lt Col Dante Bulli, pilot,
Maj Robert J. Morrison, copilot, †
Cpt Gerald Adler, navigator,
Lt Col Joe R. Simpson Jr., †
Maj William W. Gabriel, †
Maj Robert J. Hill, †
Cpt Herbert L. Hansen, †
T/Sgt Michael F. O'Keefe, †
Cpt Charles G. Leuchter. †

This flight was designated by West Coast Airlines, Inc., (WCA) as Pilot Training Flight No. 703. It was for the purpose of rating a company DC-3 captain for F-27 aircraft. N 2703 arrived at Salt Lake City Municipal Airport January 17, 1963, at 1431 1 as West Coast Flight 752 from Seattle, Washington, with stops at Yakima, Pasco, Walla Walla, all in Washington; Lewiston, Montana; and Boise and Twin Falls, both in Idaho. The flight had been uneventful and there were no carryover discrepancies entered in the aircraft's flight log. After completion of turnaround servicing, N 2703 departed the West Coast Airlines ramp at approximately 1506 with Company Cheek Pilot Instructor William Harvey Lockwood, Trainee Captain Elmer J. Cook, and FAA Carrier Inspector Buell Z. Davis aboard. A flight plan was prepared and signed by Captain Lockwood. It listed Elmer J. Cook as the first officer, FAA Inspector Buell Z. Davis as a crew member, and specified that the flight would be in the local area, under VFR conditions, and of 1 hour and 30 minutes duration. At departure Captain Cook occupied the left pilot seat, Captain Lockwood the right pilot seat, and Inspector Davis the observer's (jump) seat. The aircraft carried approximately 3,500 pounds of fuel which was ample for the intended flight. The aircraft's computed gross weight was 28,310 pounds, approximately 7,000 pounds less than maximum allowable for takeoff, and the center of gravity was within prescribed limit. Flight 703 took of f at 1510 and remained in the traffic pattern for a practice landing which was made at 1517. At 1522, Flight 703 made a second takeoff and was last observed three miles south of the airport by the local controller in the tower. The tower clearance for this takeoff was the last radio contact with the flight. The next known sighting of Flight 703 was from the air by the crew of Western Airlines Flight No. 38. At 1531 they observed it at an estimated altitude of 8,000 feet mean sea level (m.s.l.) descending to an estimated altitude of 7,000 feet m.s.l. with the left propeller feathered. It was headed southeasterly, and in the vicinity of the southern tip of Antelope Island in Great Salt Lake, some 10 miles west-northwest of the airport. Several minutes later, the ground controller in the Salt Lake City Tower observed Flight 703 for a few minutes. He saw it approaching the airport from the west at an estimated altitude of 8,000 feet above the ground. It appeared to be flying level as it came approximately over him, continuing a few miles to the east and over Salt Lake City. It then made a right turn to a west-northwesterly heading and continued in that direction until the controller discontinued watching it at a point approximately five miles west of the airport. He did not notice anything unusual about the aircraft's appearance or performance. The next observation of Flight 703 was by a motorist near the southeastern shore of the Great Salt Lake who saw it at an estimated 3,000 feet above the ground descending. He estimated the time of his initial observation to be 1550. The aircraft appeared to be on a northwesterly heading making a normal descent considerate west of the Salt Lake City Airport and continued descent until it appeared "to actually go into the lake itself." He did not see any splash; his position was about six miles from where the wreckage was later found. The official U.S. Weather Bureau observation at Salt Lake City Municipal Airport at 1555 on the day of the accident was: Ceiling estimated 12,000 feet broken, high overcast, visibility 12 miles, temperature 34 degrees F., dewpoint 2 degrees F., wind from south-southwest at 5 knots, altimeter setting 30.05, smoky, snow showers of unknown intensity east. Weather conditions were not appreciably different an hour earlier nor an hour later. At 1700, the Salt Lake City Flight Service Station (FSS) received a request from the Salt Lake City Air Route Traffic Control Center (ARTCC) to initiate a call to Flight 703 on all available frequencies. There was no reply from Flight 703 to these calls. At 1758 the Salt Lake City FSS received information from the Salt Lake City ARTCC that West Coast Flight 703 was overdue and unreported. On January 18, 1963, at approximately 1140, one body and aircraft debris was seen floating in Great Salt Lake. This floating debris was 10.4 nautical miles to the Salt Lake City Very High Frequency Omni Directional Range (VOR) or the 248 de radial. Early next morning the other two bodies were sighted and all three were recovered from the lake.

On approach to Kaktovik Airport completed by night, the pilot encountered poor weather conditions with fog. Descending under VFR, the twin engine aircraft struck the ground few km short of runway. A passenger was seriously injured while all five other occupants were killed.

While approaching Kodiak Airport following a maritime patrol flight over the North Pacific, the crew encountered poor weather conditions and low visibility. The airplane struck the north face of the Mt Old Womens located few miles short of runway. Five crew members were rescued while seven others were killed.
Those killed were:
Lt William M. Carter,
John Anthony Cole,
Lt Paul W. Dannell,
Russel S. Feldmann,
Merlin J. Haas,
Lt Richard T. Healy,
Charles A. Treat.

Shortly after takeoff from Alameda NAS, the port auxiliary jet engine caught fire. The crew attempted to return but the airplane became uncontrollable and crashed into the San Francisco Bay. The crew was rescued while the aircraft was lost.

The first officer, who was flying, started the approach to runway 17 which does not have approach lights nor Instrument landing System. At the time the aircraft was northbound in the holding pattern of the Grand Island VOR. A 90 degree left turn, then a 270 degree right turn was accomplished which aligned the aircraft, with the runway. The following sequence of events was described by the captain and substantiated by the first officer. The captain stated “. . . We completed the approach checklist and made a turn north of the low frequency range (8391 feet from the threshold of runway 17) which was visible as we went over it. The area around the range and the south half of the distance to the airport was absolutely clear. Our path was one which had the runway lights clearly aligned. (The runway lights were on at position 3 which is medium intensity.) The approach was a normal gradual descent. The radios were tuned to the low frequency range and the Omni. Since we were not ready to land our checklist was complete with the exception of approach flaps and landing flaps and ADI on. There were no ground witnesses to the approach or crash which was in a large level open field. There was no moonlight and the captain testified that except for the lights on the range station, there were no ground lights seen under the approach path. Both he and the first officer testified that they did not observe the runway light appear to "spread," which amounts to a visual warning of being very low - nearly at the level of the lights upon approaching the runway. A weather observation at 2037. seven minutes after the accident was: special, clear, visibility 7 miles, temperature 26 degrees F, dewpoint 26 degrees F, wind south 10 knots, altimeter setting 29.80 inches (aircraft accident) (observation recorded but not transmitted via teletype). The initial point of contact of the nosewheel was about three feet to the right of the extended centerline of runway 17 and approximately 4,061 feet short of the threshold of that runway. Additional marks indicate that the aircraft struck while nearly level longitudinally, in a yaw of about six degrees to the right, and in a shallow left bank. Upon initial impact, the left main landing gear collapsed and was torn free. Both propellers struck the ground and were also torn off with the nose cones of their respective engines. The left wing became detached as the aircraft rolled to the left onto its back and slid, inverted, swerving to the left and coming to rest on a heading of about 045 degrees at a distance of 1,275 feet from the place of first contact. Fire developed in the detached left wing, but not in the fuselage. Consequently all 43 occupants were able to evacuate the aircraft quickly, with the majority going out through the galley service door, which the stewardess opened and the others leaving via the emergency exit at seat 8D. The captain left through a cockpit window; the first officer and one passenger through a hole in the fuselage. Injuries were sustained by both pilots and three passengers. The aircraft was destroyed by a post crash fire.

On December 14, 1962, at 2212 P.s.t., a Flying Tiger Line Inc., Super Constellation, N6913C, crashed about 1-1/4 miles west of the Lockheed Air Terminal, Burbank California, during an ILS approach to runway 7. All five persons on board the aircraft and three persons on the ground sustained fatal injuries. The last radio communication with N6913C was the flight's acknowledgement of its radar-observed position two miles from the end of the runway on the localizer course. Twenty seconds later the aircraft crashed Into a fog-shrouded residential/industrial area.

Eastern Air Lines Flight 512, a Douglas DD-7B, N815D, crashed during an attempted go-around following an instrument approach to runway 4R at New York International Airport, at 2145 e.s.t., on November 30, 1962 Of the 51 persons aboard, 21 passengers, 3 crew members and an additional crew member occupying the jump seat did not survive. Flight 512, regularly scheduled from Charlotte, North Carolina, non-stop to New York International Airport, entered a fog condition near the threshold of runway 4R. A go-around was initiated; however, the aircraft struck the ground in a slightly nose-high attitude and was virtually destroyed by impact and subsequent fire.

The crew was involved in a local training mission at Smyrna-Sewart AFB, Tennessee. Shortly after takeoff, while in initial climb, the airplane banked left, lost height and crashed near the runway end. All five crew members were killed.