Positioning

Crashed in flames for unknown reason, killing the pilote, sole on board.

En route from the Isle of Man to RAF Abbotsinch, the twin engine aircraft encountered heavy turbulences, went out of control and crashed on the slope of a mountain. The pilot F/Lt Barney Barclay was injured and the aircraft was destroyed.

Shortly after takeoff from Travis AFB, while climbing to a height of 3,000 feet, the aircraft banked left, dove into the ground and crashed in a huge explosion. Six crew members were killed while two others were seriously injured. The airplane was returning to Tachikawa, Japan, after a major overhaul at the Douglas Aircraft plant in Long Beach.
Crew:
Maj Henderson Cagle, †
Cpt Robert E. Rogers, †
1st Lt Curtis A. Guild, †
2nd Lt Robert Distefano, †
T/Sgt Carroll D. Coziah, †
S/Sgt Raymond L. Hart, †
S/Sgt Ivan J. Wiebold,
A2c Charles R. Vance.

The accident occurred at 2208 hours during an unscheduled flight from London to Prestwick where the aircraft mas to pick up passengers for BOAC under a charter arrangement and fly them to London. The aircraft took off at 2042 hours GMT from London Airport, cruised on the Airways at 18 500 ft and then commenced the descent to Prestwick with an initial clearance to 8 500 ft. Within a few minutes the clearance was amended to cross the Prestwick radio beacon at 4 000 ft. The descent appeared to the pilots to be normal until the aircraft struck the ground close to the site of the beacon very shortly after the captain had reported passing 11 000 ft in the holding pattern. The aircraft slid along the ground for 400 yards, and fire broke out in the starboard wing, Of the five crew aboard the aircraft, three were seriously injured. The airplane was totally destroyed by fire.

The flight was to be from Dusseldorf, Germany, to New York via Reykjavik. One crew was to pilot the first leg of the trip to Reykjavik and the relief crew was to complete the flight to New York. Of the ten aboard the aircraft, seven were crew and three were passengers. Take-off from Dusseldorf at 0700 hours was normal until the aircraft became airborne. Immediately after becoming airborne and following retraction of the gear No. 1 engine was cut off and its propeller feathered. Then the No. 2 engine was also cut off and its propeller feathered. During this process the flaps were immediately and fully retracted. The aircraft, having attained an altitude of 50 metres, dropped sharply, lost altitude and crashed (0703 hours) into buildings within the city limits killing six of the occupants instantly and seriously injuring the other four. In addition, one person on the ground was killed and two others seriously injured. The wreckage was completely destroyed by fire.

The aircraft departed London Airport at 1516LT hours GMT on a flight to Belfast in pursuance of a special charter, carrying 5 crew and 2 company employees. At 1645 the aircraft was taken over by the Precision Approach Controller for a GCA talkdown on runway 28 (276°) in weather conditions which the captain thought would allow him to become visual at or above his critical height of 500 ft. Soon after '3/4 of a mile from touchdown' the aircraft was to the right of the centerline and shortly afterwards was 'well right of centerline', Just after '1/2 a mile from touchdown' the Precision Approach Controller said 'if you're overshooting turn left left 5° on overshoot over' to which the reply came '...overshooting'. At about this time a number of witnesses heard the aircraft "rev-up". Shortly thereafter (at 1651 hours) the aircraft crashed within the boundary of the airport approximately 1,000 ft to the south of the western end of runway 28, killing all occupants.

On final approach to Panagarh, the airplane crashed in a field located 5 km short of runway. Both pilots were injured while the aircraft was written off.

The aircraft arrived at Ciudad Trujillo on the morning of 16 August with No, 2 engine inoperative. It was decided to disembark the passengers there and continue the flight to New York via Miami, using only three engines, in order that the defective engine could be changed in New York. The aircraft, therefore, carrying only the crew, took off from General Andrews Airport, Ciudad Trujillo at 1516 hours with No. 2 propeller feathered. About 50 minutes after take-off, No. 4 engine propeller oversped and proved to be impossible to control or feather. It then tore free from the engine, damaging No. 3 engine propeller as it parted; No. 3 propeller was, therefore, feathered. In the meantime, No. 4 engine caught fire, and only No. 1 engine remained operative. As it was not possible to reach Ciudad Trujillo, an attempt was made to land on the road or the beach, but this failed owing to the large number of trees and the narrowness of the beach. Under these circumstances the aircraft was ditched parallel to the coast about 500 metres from it. It was considered that in carrying out the three-engined ferry flight without passengers, the operator acted in accordance with para. 6.2. 2, Part II of the ICAO International Standards and Recommended Practices, Annex 8 to the Convention, "when the State of Registry considers that the damage sustained is of a nature such that the aircraft is no longer airworthy, it shall prohibit the aircraft from resuming flight until it is restored to an airworthy condition; the State of Registry may, however, in exceptional circumstances, prescribe particular limiting conditions to permit the aircraft to fly without fare-paying passengers to an aerodrome at which it can be restored to an airworthy condition". After ditching, the aircraft sank to a depth of about 40 feet. On a second attempt the weather permitted a diving operation to be carried out, and inspection of the wreckage revealed the following in- formation: All six flap sections of the port wing were entirely separated from the aircraft. No. 1 engine propeller tore free at the time of impact, splitting the propeller shaft next to the propeller thrust bearing. No. 2 power plant was wrenched free from its nacelle and remained attached to it only by pipes and control cables. This propeller was feathered. The two inner flap sections of the starboard wing were fractured and partially detached from the aircraft. The No. 3 engine propeller also was feathered and the tip of one of its blades was broken a point 18 inches from the leading edge to 12 inches from the trailing edge. The trailing edge of the same blade also had two deep dents. Marks, apparently made by a propeller blade, were found on the right side of the No. 3 engine cowling, No. 4 engine propeller was missing but only a small part of the nose section of the No. 4 engine was broken. The diaphragm and the pitch reducing mechanism were in their original places. The fuselage was fractured and the crack extended diagonally across the main part from the front towards the right rear wall.

While cruising under VFR at an altitude of 2,100 meters, the right engine failed and caught fire. The crew elected to extinguish the fire but without success. Shortly later, the engine detached and struck the right tail, causing the aircraft to enter a spin and to crash in a steppe located about 55 km west of Mys Kamenny. The aircraft was destroyed upon impact and all 6 crew members were killed.

Struck a submerged obstacle while landing on Kikori River. The aircraft quickly sank and was lost. Both crew members were rescued.