Douglas C-54 Skymaster

On the leg from Barranquilla to Gamarra, the four engine aircraft hit the slope of a mountain located between the cities of El Banco and Curumaní, about 80 km north of Gamarra Airport. Both pilots, Cpt Santiago Paris (captain) and Cpt Guillermo Acevedo (copilot) were killed.

The four engine aircraft left Travis AFB at 2220LT on March 26 on a cargo flight to Honolulu, carrying one passenger and a crew of three. At 0155LT on March 27, while cruising at an altitude of 8,000 feet, the engine number four suffered a loss of hydraulic pressure and was shut down and its propeller was feathered. In such conditions, the captain decided to divert to San Francisco for a precautionary landing when, about an hour later, the manifold pressure of the engine number three dropped. This engine was also shut down and its propeller was feathered as well. Unable to maintain a safe altitude, the crew decided to ditch the aircraft into the Pacific Ocean few miles off San Francisco. All four occupants were rescued while the aircraft sank five hours later.

Transocean Air Lines’ Flight 942 of March 20, 1953, departed Roswell, New Mexico, at 1211 for Oakland, California. On board were 30 military passengers and a crew consisting of Captain H. E. Hum, First Officer F. W. Patchett, Chief Pilot H. W. Rodgers and Stewardesses V. Sandridge and L. Chapman. The flight was for the purpose of transporting military personnel in accordance with the company’s contract with the United States Department of Defense. Prior to departure a DVFR (Defense Visual Flight Rules) flight plan was filed with ARTC (Air Route Traffic Control), indicating a flight to be flown at an altitude of at least 500 feet on top of clouds via Red Airway 88 to Albuquerque, New Mexico; Green Airway 4 to Palmdale, California; Blue Airway 14 and Amber Airway 1 to Bakersfield, California; Amber Airway 1 to Fresno, California; and Blue Airway 10 to Oakland, California. There was sufficient fuel on board for 10 hours and the flying time to Oakland was estimated to be six hours and 35 minutes. According to the company’s records the gross weight of the aircraft at the time of takeoff was 63,817 pounds, which was within the allowable gross weight of 73,000 pounds; the load was properly distributed. After departing Roswell the flight progressed in a routine manner and at 1451, when in the vicinity of Winslow, Arizona, the DVFR flight plan was changed to IFR (Instrument Flight Rules), still at least 500 feet on top of clouds. At 1732 the flight reported that it was over Fresno, California, at 1730, that it was cruising at 8,000 feet (at least 500 feet on top of clouds), estimating Los Banos, California, at 1740 and requested further clearance, At 1744 Flight 942 called the Fresno radio communications station and asked that the requested clearance be expedited, stating that it was now at 7,000 feet, at least 500 feet on top. At 1747, the following clearance was issued the flight: “ARTC clears Transocean 942 to the Newark radio beacon, maintain 8,000, contact Oakland Approach Control after passing Evergreen, no delay expected, report reaching 8,000.” Approaching Evergreen at 1809, the flight was advised to maintain 8,000 feet to Newark. One minute later, at 1810, Flight 942 reported over Evergreen at 8,000 and requested a lower altitude. This request was denied because of traffic at the 7,000-foot level. At 1819 the flight reported over the Newark, California, compass locator and fan marker (radio beacon) at 8,000 feet where it held for 11 minutes. At 1827, Oakland Approach Control cleared Flight 942 for a straight-in range approach, to descend in the holding pattern to cross the Newark compass locator at 3,500 feet and to report leaving each 1,000-foot level. Three minutes later, at 1830, the flight reported leaving 8,000 feet, and subsequently reported leaving each 1,000-foot level. At 1836, it reported being at 3,500 feet leaving the Newark compass locator inbound. This was the last known radio contact with the flight. At approximately 1838 the aircraft crashed in a barley field. Impact and fire destroyed the aircraft. There were no survivors. The Oakland weather reported at the time was: Measured ceiling 1300 feet broken, 1800 feet overcast, light rain, fog, visibility two and one-half miles, wind south-southwest 17 miles per hour, altimeter setting 30.09.

The final approach to Bordeaux-Mérignac was performed in foggy conditions. Due to low visibility, the flying crew did not realize that his altitude was insufficient when the four engine aircraft hit the top of pine trees, stalled and crashed in flames in a wooded area located in Eysines, north of the airfield. The aircraft was destroyed by a post crash fire and nine occupants were killed, six crew members and three passengers.

On final approach to Stephenville Airport by night, the four engine aircraft hit the ground and crashed 1,5 km short of runway threshold. A passenger was rescued while 13 other occupants were killed. For unknown reason, the crew was completing the approach at an insufficient altitude.

Flying Tiger's Flight 841 of January 7, 1953, a ferry flight from Burbank, California, to Seattle, to pick up military personnel, was made in accordance with the company's contract with the Department of National Defense. Departure from Burbank was at 1437, with Captain C. Greber, pilot in command, Captain B. Merrill, and Copilot W. Lowe comprising the crew. Captain H. Wall, chief pilot of the company's Burbank Division, was on board as an observer. The weight of the aircraft at takeoff was 57,520 pounds which was within the maximum allowable gross weight; there was no revenue load. Throughout the segment of the flight to San Francisco, California, Captain Merrill and Captain Lowe flew the aircraft; with the exception of a false fire warning signal from the No. 3 engine nacelle observed in the cockpit shortly after takeoff, the flight to San Francisco was routine. Upon arrival there mechanics checked the fire warning system and found no evidence of a fire having occurred. Captain Merrill told the mechanics that he was satisfied from their inspection there was no danger of fire and that he would not delay the flight further. The malfunctioning fire waning system was not repaired at this time. Captain Wall terminated his flight at San Francisco and a company stewardess, together with a woman passenger and her two children (the wife and children of a company pilot), boarded the aircraft at this point to fly as non-revenue passengers. No fuel or cargo was added at San Francisco. Flight 841 departed San Francisco at 1737 with Captain Greber in command occupying the left pilot's seat and Captain Merrill occupying the copilot's seat. The flight was cleared by ARTC (Air Route Traffic Control) to fly VFR via Amber Airway No. 1 to Williams, California, and IFR from Williams to Boeing Field, Seattle, at an altitude of 11,000 feet MSL. The estimated time en route was three hours and 39 minutes with 1,500 gallons of fuel on board and the Seattle-Tacoma Airport was designated as the alternate. Normal en route position reports were made by the flight and at 1947 it reported being over Eugene, Oregon, at 11,000 feet. Seattle ARTC then cleared the flight to descend to and maintain 9,000 feet until passing Portland, Oregon, and from this point, to descend to and maintain 7,000 feet. At 2036 Flight 841 reported over the McChord radio range station and requested further clearance. Accordingly, ARTC cleared the flight to maintain 7,000 feet, to contact Seattle Approach Control immediately and advised that no delay was expected. Contact was immediately made with approach control; the flight was then cleared to make a standard range approach to Boeing Field and requested to report leaving each 1,000-foot level during the descent. The following weather information was given the flight at this time: "Boeing Field - 1800 scattered, 2200 overcast, 8 miles, wind south-southeast 22, gusts to 30, altimeter 2925; Seattle-Tacoma - measured 1900 broken with 3100 over-cast." Flight 841 acknowledged this clearance and reported leaving 7,000 feet at 2040. Two minutes later, at 2042, it reported being over the outer marker and leaving the 6,000-foot level. No report of leaving the 5,000-foot level was made and at 2045 the flight advised it was leaving 4,000 feet. When the latter was acknowledged by approach control the flight was further advised as follows: "If you're not VFR by the tine you reach the range you can shuttle on the northwest course at 2,000 feet, it's possible you'll break out in the vicinity of Boeing Field for a south landing." The flight acknowledged at 2050 and said it was leaving 3,000 feet. At the time N 86574 was making the approach to Boeing Field, a Pan American DC-4 aircraft was also approaching this airport from the northwest. The latter aircraft had been advised by approach control that it was No. 2 to land behind the Flying Tiger aircraft in the traffic pattern. The Pan American aircraft its making a routine let-down on the northwest leg on the Seattle range and at 2054 reported being at the 3,000-foot level and VFR. Immediately after receiving this altitude report approach control called N 86574 and advised: "You're clear to contact Boeing Tower on 118.3 for landing instructions." This was acknowledged by "Roger" and was the last known contact with the Flying Tiger aircraft. At approximately 2055, N 86574 crashed about 11 miles east of the Seattle range station at the base of Squak Mountain. All seven occupants were killed and the aircraft was demolished by impact and the ensuing fire.

The C-54G, assigned to the Military Air Transport Service (MATS), 1701st Air Transport Wing at Malmstrom Air Force Base (AFB), Great Falls, Montana, was inbound from Ladd AFB, Fairbanks, Alaska, carrying 32 American servicemen and their dependents, and a crew of seven. At 0030LT, the pilot, Captain Albert J. Fenton, radioed the McChord air traffic control tower for field conditions and was informed that visibility was approximately three-quarters of a mile. Captain Fenton was directed to execute a wide left-hand turn and descend for a ground-controlled landing from the south. As the aircraft neared the field, a thick fog bank, rising 300 feet high, suddenly developed, reducing visibility to near zero. At 0048LT, Captain Fenton, now on final approach, decided to abort the landing and radioed the control tower that he was proceeding to Malmstrom AFB instead. Minutes later, witnesses telephoned the control tower and the Pierce County Sheriff’s Department to report a downed aircraft. The Skymaster crashed into an open field (now Wards Lake Park) approximately one mile north of McChord AFB and one-half mile east of S Tacoma Way between S 84th and S 88th Streets in the unincorporated community of Lakewood. It barely missed the Edgewood Park apartments, 35 four-family units built to ease the military’s housing shortage during the Korean War (1950-1953), and other nearby homes. Several people who saw the accident said the Skymaster was on fire before it crashed. Upon impact, the aircraft broke in two and exploded into flames. Bodies, personal belongings, packages and luggage were scattered around the crash scene for 200 yards. Most of the fire was in the forward section of the fuselage, the tail and aft section remaining almost intact. Some witnesses said they could hear the cries of people caught in the burning wreckage, but were helpless to render assistance. Meanwhile, fire and rescue teams from McChord AFB, Lakewood, and Tacoma rushed to the crash site and extinguished the fires in the fuselage and scattered debris. Using magnesium flares and flashlights, police and sheriff’s officers, firemen, and military personnel searched the smoldering, twisted wreckage, looking for victims. Of the 39 people aboard the C-54G, they found only three survivors: Airman Bobby R. Wilson, age 20, a member of the plane’s crew, Airman Curtis Redd, age 23, and Joseph M. Iacovitti, age 8, both passengers. Wilson, who had third-degree burns, internal injuries, and multiple skull fractures, died at Pierce County Hospital on Saturday, November 29. Redd was taken to St. Joseph Hospital in Tacoma in critical conditions with third-degree burns, but survived. Iacovitti was taken to Pierce County Hospital in serious condition with burns, broken legs and a fractured neck. He lived through the ordeal, but his parents, two brothers, and a sister died in the mishap, leaving him an orphan and the only surviving member of his family. Three other families were wiped out entirely.
Crew:
Benedict, John H., 20, Airman Second Class
Bentley, Patricia, 24, Airman Third Class
Bokinsky, Joseph H., 24, Staff Sergeant
Childers, Wilber C., 21, Airman Second Class
Fenton, Albert J., 29, Captain, pilot
Harvey, James D., 27, First Lieutenant, copilot
Wilson, Bobby R., 20, Airman Third Class.
Passengers:
U.S. Army:
Coons, Robert F., 22, Corporal
Galloway, Calvin, 18, Private First Class
Hockenberry, Denny L., 22, Sergeant
Hockenberry, Elda M., 21, spouse
Hockenberry, Susan E., 2, daughter
Hockenberry, Denise M., 1, daughter
Lebonitte, Joseph T., 23, Private First Class
Zeravich,Christoph, 24, Corporal
U.S. Air Force
Alsbury, Jack R., 21, Airman Third Class
Cook, Robert H., 20, Airman First Class
Farley, Donna L., 20, (spouse of Farley, Glen D., Staff Sergeant)
Iacovitti, Anthony R., First Lieutenant
Iacovitti, Dorothy E., 31, spouse
Iacovitti, Anthony F., 6, son
Iacovitti, John A., 4, son
Iacovitti, Barbara, 2, daughter
Johnson, Dwight P., 23, Airman Second Class
Morris, George E., 33, Master Sergeant
Morris, Anna D., 28, spouse
Morris, George E., Jr., 3, son
Morris, Geraldine A., 5, daughter
Niemi, Edwin, 35, Staff Sergeant
Parlett, Frederick D., 18, Basic Airman
Pickerel, Robert L., 22, Airman First Class
Smith, Raymond D., 24, Staff Sergeant
Swang, Marion E., 41, Major [incorrectly listed as Swann]
Weikum, Elmer, 23, Airman Second Class
Wells, Samuel R., 35, Master Sergeant
Wells, Margaret A., 33, spouse
Wells, Samuel R. III, 3, son
Survivors
Iacovitti, Joseph M., 8, (son of Dorothy and Anthony Iacovitti)
Redd, Curtis, 23, Airman Second Class.
Source:
http://www.koreanwar-educator.org/topics/airplane_crashes/c54_tacoma_19521128/p_c54_tacoma_11_28_52.htm

The four engine aircraft went out of control and crashed in unknown circumstances into Lake Chad. A pilot was rescued while five other occupants were killed. The crew was performing a cargo flight from Fort Lamy to Beirut.

Braniff Airways' Flight 65 departed Denver, Colorado, at 1535 on March 26, 1952, for Dallas, Texas, with intermediate stops scheduled at Colorado Springs, Colorado, and Oklahoma City, Oklahoma. The crew consisted of Captain J. W. Stanford, First Officer J. P. Beakley, and Hostesses Dorothy Currey and Betty Murphy. The flight arrived at Colorado Springs after a routine trip and departed there at 1620. On departure it was cleared IFR (Instrument Flight Rules) direct to LaJunta, Colorado, and then by Red Airway 35 to Garden City, Kansas, and Red Airway 59 to Oklahoma City; to cruise at 8,000 feet to LaJunta, and to descend and maintain 7,000 feet from LaJunta to Oklahoma City. According to company records, the gross weight of the aircraft was within approved limits and the load was properly distributed. At 1653 the flight reported over LaJunta at 8,000 feet, descending to 7,000. Four minutes later, at 1657, the flight canceled its IFR flight plan and advised that it was proceeding VFR (Visual Flight Rules) direct to Oklahoma City via Liberal, Kansas. When in the vicinity of Hugoton, Kansas, at approximately 6,000 feet MSL, (3000 feet above the ground), one of the hostesses advised the crew that the right wing was on fire. This was the first indication the crew had that anything was wrong, as the fire-warning signal devices had not functioned and all engines appeared to be operating in a normal manner. The captain immediately looked through the small window in the forward cargo loading door on the right and saw a brilliant red reflection on the inboard surface of the No. 4 engine nacelle. Because of the brilliance of the reflection and the fact that it covered the entire visible portion of this nacelle, he believed the fire was of considerable proportion. He immediately asked the copilot where the fire was and was advised that he thought it was No. 3. The captain then decided to land as quickly as possible on a small airport near Hugoton which he had seen only a few seconds before the hostess came to the cockpit. Accordingly, the hostess was told to advise the passengers that an emergency landing was to be made, and the "Fasten seat belt" and "No smoking" signs were turned on. The captain then disengaged the autopilot, closed the throttle of the No. 3 engine, put the mixture control at idle cutoff, closed the fuel selector valve, and set the propeller control at the full high pitch position. Following this, he dived the aircraft in an attempt to extinguish the fire and to lose altitude. At this time the copilot asked the captain if he wanted the No. 3 engine's propeller feathered, and the captain said, "No." When an air speed of approximately 230 miles per hour was reached, power was reduced on the remaining three engines. During the dive the aircraft was heading in a southeasterly direction, and after a short time the dive was decreased and a steep left turn was made to a westerly heading. When the air speed decreased to approximately 200 miles per hour, the captain pulled the No. 3 fire extinguisher selector valve control handle (this also operates the fire wall shutoff valves), and then pulled the discharge handle of the left CO 2 bottle. When this bottle was discharged, the reflection on the No. 4 engine nacelle was observed to diminish appreciably. The captain said that at this time he thought he asked the copilot to discharge the right CO 2 bottle; however, this bottle was not discharged. The landing gear was lowered, and power was resumed on the three remaining engines. About this time the fire warning light in the cockpit came on, and the bell rang. These warning signals continued to operate intermittently. As soon as the gear was down, the descent was steepened and a series of steep slipping "S" turns were made toward the north while approaching the airport. At an altitude of approximately 200 to 300 feet above the ground, a pronounced buffeting (similar to that which accompanies a near stalling attitude) was experienced. This buffeting was so pronounced it was difficult to control the aircraft; however, it soon stopped and normal control was again resumed. When the buffeting occurred, the indicated air speed was approximately 150 mph. It is believed that the No. 3 engine fell from the aircraft at this time. The captain next called for full flaps. Although the copilot immediately executed this command, no apparent effect of the flaps being lowered was noticed by the crew, and a few seconds later, the aircraft touched down in the middle of the airport. The captain applied brake pressure immediately, but the aircraft did not decelerate. Approaching the north boundary of the field, the captain tried to turn left to avoid crossing a road which was adjacent to the airport, but the nose steering wheel was inoperative. Left rudder was immediately applied; however, the aircraft responded so quickly to this action that right rudder had to be applied at once to keep the aircraft from ground looping. After the aircraft was gain rolling straight, the captain pulled back on the wheel, causing the nose wheel to life from the ground, and the aircraft rolled beyond the airport boundary across a highway, through two fences and a ditch, and came to rest in a wheat field. All of the occupants were evacuated in an orderly manner, some through the forward compartment and main cabin doors by using descent ropes and a few by means of an emergency exit located on the left side of the aircraft.

The four engine aircraft christened 'Helka' was performing a cargo flight, carrying 50 cows. After touchdown at Pisa-San Giusto Airport, the airplane encountered difficulties to stop within the remaining distance. It overran and came to rest in flames in a ditch. All four crew members were evacuated safely while only three cows were rescued, 47 others being killed.