All World

Trip 845/26, a scheduled flight from Seattle-Tacoma, Washington, to Sydney, Australia, departed Seattle-Tacoma Airport at 0815LT for Portland, Oregon, the first intermediate stop. There were 13 passengers and a crew of 8 consisting of Captain H. S. Joslyn, First Officer A. G. Kendrick, a Navigator N. F. Kerwick, Flight Engineer D. R. Fowler, Assistant Flight Engineer S. Bachman, Purser Natalie B. Parker, Stewardess Elizabeth M. Thompson, and Steward J. D. Peppin. The flight to Portland was normal in all respects with arrival at 0910. There the aircraft was serviced and two additional passengers boarded. Only inspections and service were accomplished. The flight left the ramp at 1010 and took off for Honolulu, Territory of Hawaii, at 1021 on an IFR clearance. Weather conditions at time of takeoff were VFR. There were 15 passengers and the saw crew of 8. Takeoff gross weight was 139,494 (maximum allowable was 145,800 pounds) and the center of gravity was located within limits. The flight plan was via Newberg and Newport, Oregon, and thence to Honolulu to Cruise at 10,000 feet. Estimated flight time was 11 hours and 3 minutes. The flight reported over Newberg at 1031 at 7,000 feet climbing., reached 10,000 feet at approximately 1039, and reported over Newport at 1048 at cruising altitude. The aircraft was then headed to make good the initial track or 221 degrees . Forty-two minutes after takeoff, severe vibration occurred while cruising era at 10,000 feet under VIM conditions. This lasted for five to eight seconds following which No. 3 engine and propeller tore free and fell from the aircraft. The captain immediately disconnected the autopilot. Severe buffeting ensued, the nose want down and the aircraft swung to the right sharply. At this point, the emergency "Mayday" signal was broadcast on both VHF and HF. Direct return to Portland was authorized by Seattle Air Route Traffic Control. The captain, in the left seat, tried to get the airplane under control. Airspeed was about 220 knots and going higher, so he closed the throttles to keep the airspeed down. He still could not get the nose up; it felt to him as though the elevators were still on automatic pilot. He tried the elevator trim tab and could not turn it. After rapid loss of altitude to about 5,000 feet, the captain directed the first officer to assist him with the controls. Their combined efforts finally brought the nose up very rapidly but the aircraft then went into a steep climb. It turned sharply to the right about 180 degrees and, according to the captain, appeared to be on "the verge of a spin." Level attitude was regained by pushing the yoke forward, and by use of the rudder and aileron trim the turn was stopped. At an airspeed of 150 knots, flaps extended 25 degrees, buffeting decreased immediately, however., the aircraft continued to descend rapidly. Attempts to get rated power were futile and a message was broadcast that ditching was imminent. This message was sent at approximately 1106. The aircraft was then at an altitude of 500-1,000 feet. Ditching was imminent. Cabin attendants, realizing the emergency, assumed their respective stations for ditching. All passengers had been seated in the upper desk of the cabin with seat belts fastened and life jackets donned. The aircraft touched down under near ideal sea conditions with little swall. Contact with the water we severe and the impact dislodged life rafts from their storage bins and some seats were torn loose. The aft portion of the fuselage and empennage broke off at impact. Evacuation was orderly and the three rafts, although dislodged from their stowage receptacles, were launched without undue delay. The lanyards of all three life rafts were temporarily held at the cabin door by crow members. However, when one of the rafts was endangered by sharp metal of the broken fuselage its lanyard was released. Another was released by a crew member who then swam to that raft to right it. The lanyard of the third raft was released for unknown reasons. Consequently the rafts were carried away by the light surface wind. Passengers and crew left by both the main cabin door and escape hatches on both sides of the fuselage over each wing. Some crew members and passengers ware able to swim to and board the rafts. Three of the four fatalities, including the copilot and first engineer, were unable to do so and were lost. Members of the crew and passengers tried in vain to paddle to these persons. One other passenger later died in a raft from awe and shock. The purser, a woman, although suffering from shock swam and towed the only seriously injured passenger to the nearest raft, some 200 feet distant. The time of ditching was determined as 1112 and the position at lat. 43 degrees 48'15" N., long. 125 degrees 12'40" W., approximately 35 miles off the Oregon coast. The U.S.S. Bayfield, en route to Seattle, changed course toward the site and by add of search aircraft reached the life rafts some two hours later.

The crew was engaged in a transatlantic flight from Lajes to Hamilton, Bermuda. Enroute, the captain informed ground that he was short of fuel and was unable to reach Hamilton. He reduced his altitude and ditched the airplane near the Echo weather station. A USCG crew was able to evacuate all eight crew members while the aircraft sank and was lost.

The aircraft left RAF St Eval at 1020LT for a 15 hours training mission, preceded by six minutes from a first RAF Avro 696 Shackleton MR.2 registered WG531 and carrying nine crew members as well. The last radio contact was recorded at 2058LT and two minutes later, both aircraft disappeared simultaneously. SAR operations were conducted but all operations were suspended few days later as no trace of both aircraft nor the 18 crew members was found. More than eleven years later, a fisherman found in is fishnet the engine number four from the Shackleton registered WL743 about 75 miles north of the assumed collision point.
Crew (42nd Squadron):
P/O L. W. Wood, pilot,
Sgt H. Davies, pilot,
F/O N. Horrocks, navigator,
F/O G. Molyneux, navigator,
Sgt D. Male, flight engineer,
Mst I. O. Cathcart, air signaler,
Sgt C. W. Scott, air signaler,
Sgt R. E. Ridgers, air signaler,
Sgt L. W. Cooper, air signaler.

The aircraft left RAF St Eval at 1014LT for a 15 hours training mission, followed six minutes later by a second RAF Avro 696 Shackleton MR.2 registered WL743 and carrying nine crew members as well. The last radio contact was recorded at 2058LT and two minutes later, both aircraft disappeared simultaneously. SAR operations were conducted but all operations were suspended few days later as no trace of both aircraft nor the 18 crew members was found. More than eleven years later, a fisherman found in is fishnet the engine number four from the Shackleton registered WL743 about 75 miles north of the assumed collision point.
Crew (42nd Squadron):
F/O G. Board, pilot,
F/O K. G. Richards, pilot,
F/O G. Rogers, navigator,
F/O B. H. Webb, navigator,
F/Sgt M. G. Rae, air signaler,
Sgt L. R. Swann, air signaler,
Sgt J. T. Goodwin, air signaler,
Sgt E. J. Morgan, air signaler,
Sgt G. Thompson, air signaler.

The crew left RAF Saint Eval to conduct a training mission consisting of a submarine attack. In unknown circumstances, the aircraft crashed into the Celtic Sea off the Cornwall coast. All seven crew members were killed.

The aircraft was performing a flight from Patuxent River NAS to Port Lyautey, Morocco, with an intermediate stop at Lajes, carrying 21 crew members and 21 passengers, among them civilians and children. At 2330LT, the crew informed ATC about his position 400 miles east of Baltimore (Maryland), this was the last radio transmission. About an hour and a half later, while cruising at an altitude of 17,000 feet, the aircraft went out of control and crashed into the Atlantic Ocean without any distress call on part of the crew. SAR operations were conducted on a large area but were suspended six days later due to poor weather conditions. No trace of the aircraft nor the 42 occupants was found. It was reported by the board that the aircraft was also carrying 111 life vests, 46 exposure suits, 660 paper cups and 5 life rafts. All elements supposed to float. However, no trace of them was ever found.

The Lockheed P2V-5 Neptune was shot down by Soviet fighter airplanes. The aircraft operated on a routine patrol mission over the Sea of Japan. At 1758LT while the airplane was flying on a course of 090 degrees magnetic, over the high seas of the Sea of Japan, its position was approximately 41 degrees 51 minutes north and 132 degrees 47 minutes east. At 1807LT, the course was changed to 067 degrees magnetic. The ground speed of the aircraft at the time continued at approximately 180 knots and its altitude was approximately 8,000 feet. The course of 067 degrees had been continued for approximately five minutes, when at least two Soviet MiG fighter aircraft came up behind the Neptune aircraft, and opened fire. The pilot of the Neptune turned sharply to the right and went simultaneously into a steep dive at a rate of descent of approximately 2,000 to 3,000 feet per minute, attempting to fly farther and farther away from the Soviet land mass and seeking the protective cover of a cloud bank approximately ten miles farther away. The MiG aircraft again opened fire. The Neptune continued its steep dive and made evasive maneuvers to the right and left. The left wing was hit and a fire erupted. The fire continued to spread quickly through the wing to the fuselage, and when the Neptune had reached an altitude of 400 feet over water, the pilot determined that it was necessary to abandon the aircraft in the. The Neptune was landed on the sea and came to a complete stop within 50 to 70 yards after the initial impact. Of the ten members of the crew on board the Neptune aircraft, nine succeeded in making their way out of the aircraft to the surface of the sea and entered a survival raft which had been carried aboard. The United States claimed that the point of the first attack was over the high seas to the southeast of Cape Ostrovnoi, in the neighborhood of 42 degrees 22 minutes north and 134 degrees and 11 minutes east, or further to the south and east of that position, approximately 33 to 40 nautical miles from Soviet territory. All survivors were rescued by the crew of a USN SA-16 Albatross.
Crew:
Roger H. Reid, †
John B. Wayne,
John C. Fischer,
William A. Bedard,
Frank E. Petty,
Anthony P. Granera,
Texas R. Stone,
Paul R. Mulmollem,
Ernest L. Pinkevich,
David A. Atwell.

The crew was completing a training mission over the Ionian Sea when an engine failed in flight. The pilot lost control of the airplane that crashed into the sea about 72 km east of Punta Stilo, Calabria. The aircraft was destroyed and all seven crew members were killed.

While cruising about 400 miles east of Hawaii, the crew informed ground about a dual engine failure and the captain attempted to ditch the aircraft. Six crew members were rescued while four others were killed. The aircraft sank and was lost.

The crew was performing a supply mission to the Arctic expedition 'Sever' located on a drifting ice floe near the North Pole (at N89.1500 W90.0000). On approach, while at a height of 15 meters, the aircraft pitched down and crashed in flames on the ice. All five occupants were able to evacuate the cabin and were slightly injured. The aircraft was quickly destroyed by fire.