Crash of a Douglas C-54A-5-DO Skymaster off São Sebastião

Date & Time: Nov 4, 1957 at 1350 LT
Type of aircraft:
Operator:
Registration:
PP-AXS
Flight Phase:
Survivors:
Yes
Schedule:
São Paulo – Rio de Janeiro
MSN:
7467
YOM:
1944
Country:
Crew on board:
4
Crew fatalities:
Pax on board:
30
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
While cruising at an altitude of 3,000 meters, the engine number two fuel pressure dropped to zero. The crew feathered the propeller when the oil pressure on both left engines rose and smoke spread from the battery and generator compartment. The engine number two caught fire and the crew declared an emergency. Shortly later, the engine number two detached and the crew attempted to ditch the aircraft into the Praia de Balaia off São Sebastião. All 34 occupants were evacuated safely while the aircraft was damaged beyond repair.
Probable cause:
Failure of a pipe on the engine number two fuel supply system.

Crash of a Douglas C-54A-1-DO Skymaster in Düsseldorf: 7 killed

Date & Time: Nov 3, 1957 at 0703 LT
Type of aircraft:
Operator:
Registration:
D-ALAF
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Düsseldorf – Reykjavik – New York
MSN:
7459
YOM:
1944
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
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.
Probable cause:
The accident was caused by the intentional creation of an emergency situation on take-off for a long distance flight: first No. 1 engine was cut off and its propeller feathered, then No. 2 engine was also stopped and its propeller feathered. In addition, the flaps were immediately and fully retracted at low altitude. Such action by the pilot-in-command during take-off immediately after the aircraft became airborne, with a view to testing a crew member, caused the aircraft to crash. The piloting technique was not consistent with the safety requirements and operating instructions as prescribed by the Directorate of Civil Aviation.
Final Report:

Ground fire of a Douglas C-54-DO Skymaster at Toulouse

Date & Time: Nov 2, 1957
Type of aircraft:
Operator:
Registration:
F-BHKY
Flight Phase:
Survivors:
Yes
MSN:
3055
YOM:
1943
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Caught fire while parked at Toulouse-Blagnac Airport. There were no injuries but the aircraft was destroyed.

Crash of a Douglas C-54A-1-DO Skymaster in Greenland: 2 killed

Date & Time: May 13, 1957 at 0335 LT
Type of aircraft:
Operator:
Registration:
N68736
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Qikiqtarjuaq – Narsarsuaq
MSN:
7449
YOM:
1943
Flight number:
UO736
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
12929
Captain / Total hours on type:
5150.00
Copilot / Total flying hours:
5675
Copilot / Total hours on type:
3550
Circumstances:
The aircraft carried a crew of three and no passengers. It was one of several Company aircraft under contract to transport diesel oil from Narsarsuaq, Greenland, to various DEW Line sites (Distant Early Warning Radar Line). The flight was returning from DEW site 39 when it crashed during a VFR descent on the Greenland ice cap at approximately 0335LT. After impact, the airplane skidded about 4,500 feet before coming to rest. The copilot survived while two other occupants were killed.
Final Report:

Crash of a Douglas C-54B-20-DO Skymaster near Blyn: 5 killed

Date & Time: Mar 2, 1957 at 1719 LT
Type of aircraft:
Operator:
Registration:
N90449
Flight Phase:
Survivors:
No
Site:
Schedule:
Fairbanks – Seattle
MSN:
27239
YOM:
1944
Flight number:
AS100
Location:
Crew on board:
3
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
12033
Captain / Total hours on type:
8023.00
Copilot / Total flying hours:
10791
Copilot / Total hours on type:
4532
Aircraft flight hours:
28835
Circumstances:
Alaska Airlines, Inc., is an air carrier certificated to conduct scheduled operations within the Territory of Alaska and between Alaska and the continental United States. Flight 100 of March 2 originated at Fairbanks, Alaska, as a regularly scheduled nonstop flight to Seattle, Washington. The aircraft, N 90449, had arrived from Seattle at 0717 March 2 as Trip 101/1. Two minor discrepancies reported by the inbound crew were corrected during a turnaround inspection and by 0930 that morning the aircraft was ready for the return flight to Seattle. The crew assigned to Flight 100, Captain Lawrence F. Currie, Copilot Lyle O. Edwards, and Stewardess Elizabeth Goods, arrived at operations and made the normal routine preparations for the flight. The pilots discussed the flight with the station agent and all necessary flight papers were completed. Weather for the route was given to the pilots. The weight and balance were determined and both were well within allowable limits. The aircraft was serviced with 2,380 gallons of fuel. The following IFR flight plan was filed with Fairbanks ARTC (Air Route Traffic Control): Alaska 100, a DC-4, departing 10,000 feet Amber 2 Snag, 12,000 Blue 79 Haines, 10,000 Blue 79 Annette, 9,500 direct Port Hardy, 10,000 Amber 1 Seattle; airspeed 185; estimating 7 hours, 44 minutes en route; proposing 0955. At 0940 the two passengers and crew boarded the aircraft. Takeoff was made in VFR weather conditions at 0958. Shortly thereafter Fairbanks center called N 90449 and relayed the ATC clearance, approving the flight plan as filed. The weather conditions at Fairbanks and en route were forecast to be generally good and the flight proceeded in the clear as planned, making routine position reports as it progressed. At 1240, when over Haines, Alaska, at 12,000 feet, Flight 100 canceled its instrument flight plan and informed ARTC that they would proceed VFR to Annette and would file DVFR 2 (Defense Visual Flight Rule) after Annette and before entering the CADIZ (Canadian Air Defense Identification Zone). Thereafter the flight proceeded, reporting its position as DVFR at 1,000 feet. The flight was observed at Patricia Bay, British Columbia, at an estimated 3,000 feet m. s. l. by a tower operator. It was also observed leaving the CADIZ. At 1717 the Alaska Airlines Seattle dispatch office received the following position report by radio from Flight 100: "Dungeness at 16 VFR estimating Seattle at 34." This was the last contact with the flight, which crashed shortly thereafter. All five occupants were killed. N 90449 crashed in heavily timbered mountainous terrain March 2 and was not located until March 3, 1957. The crash occurred approximately in the center of the "on course" zone of the northwest leg of the Seattle low frequency radio range, about 11 nautical miles southeast of the Dungeness fan marker. This leg of the Seattle range defines the center of Amber Airway 1 between the Dungeness intersection and the range station. The minimum instrument en route altitude for this segment is 5,000 feet. Because of adverse weather and inaccessibility of the location, CAB investigators were unable to reach the scene until March 6. The investigators noted that the wreckage had been disturbed prior to their arrival; some components were missing, presumably carried away by persons unknown. The path of the aircraft during the final seconds of flight was clearly defined in the heavy timber growing on the steep slope against the aircraft smashed. The aircraft’s first contact with the trees was at a point 650 feet from the wreckage. From this point it cut a level swath on a heading of 106 degrees magnetic, the width of its wing span, into the steeply rising wooded slope at an elevation of approximately 1,500 feet m. s. l. The terrain immediately ahead of the aircraft‘s path rose to an altitude of 2,000. 2,100 feet MSL.
Probable cause:
The Board determines that the probable cause of this accident was a navigational error and poor judgment exhibited by the pilot in entering an overcast in a mountainous area at a dangerously low altitude. The following findings were reported:
- No malfunction or emergency existed and the aircraft was intact prior to its initial contact with the mountain,
- Several errors and omissions in the course of the flight Indicate the crew was lax and not giving proper attention to their duties,
- A navigational error resulted in the aircraft being three to four miles west of the flight path assumed by the crew,
- The pilot flew into instrument weather without obtaining a proper clearance,
- The aircraft crashed in terrain obscured by clouds.
Final Report:

Crash of a Douglas C-54A-10-DC Skymaster near Puerto Somoza: 25 killed

Date & Time: Nov 15, 1956 at 1515 LT
Type of aircraft:
Operator:
Registration:
XA-HEG
Flight Phase:
Survivors:
No
Schedule:
Panama City – Guatemala City – Mexico City
MSN:
10324
YOM:
1944
Country:
Crew on board:
5
Crew fatalities:
Pax on board:
20
Pax fatalities:
Other fatalities:
Total fatalities:
25
Circumstances:
The aircraft was on a flight from Tocumen Airport, Panama, to Central Airport, Mexico City, with a stop at La Aurora Airport, Guatemala City. The flight reported "all well'' Over Managua, Nicaragua, at 2053 hours GMT (1453 hours local time). Somewhere between Managua and the eastern part of León Department an unknown trouble originated. Fire in flight resulted and the aircraft crashed in a wooded area located 13 km northwest of Puerto Somoza. All 25 persons aboard, 20 passengers and 5 crew members, including one supernumerary pilot, were killed. The aircraft disintegrated on impact.
Probable cause:
It was not possible to determine the origin of the fire in the-main section of the hydraulic and fuel distribution systems; this determination will depend upon the results of laboratory tests and maintenance reports; when these are in, a reasonable conclusion can be reached regarding the probable cause of fire in flight. This may have been occasioned by a number of causes, for example, breaking of a hydraulic pressure line, short circuits in the electrical wiring or leakage of fuel lines or tanks, etc.
Final Report:

Crash of a Douglas C-54A-5-DC Skymaster in Ushuaia

Date & Time: Feb 29, 1956
Type of aircraft:
Operator:
Registration:
4-T-2
Flight Type:
Survivors:
Yes
MSN:
10301
YOM:
1944
Country:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crash landed at Ushuaia Airport, lost its right wing and came to rest in flames. There were no casualties but the aircraft registered 4-T-2 (ex 0277/CTA-5) was destroyed.

Crash of a Douglas R5D-2 on Mt Sunol Ridge: 40 killed

Date & Time: Feb 17, 1956 at 1342 LT
Type of aircraft:
Operator:
Registration:
39116
Flight Type:
Survivors:
No
Site:
Schedule:
Camp Pendleton – El Toro – Alameda – Hickam
MSN:
18331
YOM:
1944
Crew on board:
5
Crew fatalities:
Pax on board:
35
Pax fatalities:
Other fatalities:
Total fatalities:
40
Circumstances:
The aircraft departed El Toro Airbase at 1030LT Bound for Alameda NAS on behalf of the Marine Transport Squadron 152. On board were United States Marines from Camp Pendleton en route to Hickam Field, and five crew members. While approaching his destination, the captain was instructed to follow a 30 minutes holding circuit. At 1342LT, while descending at an altitude of 3,500 feet in marginal weather conditions, the pilot started the approach when the aircraft hit the slope of Mt Sunol Ridge located about 21 miles southeast of Alameda Airbase. The aircraft was destroyed upon impact and all 40 occupants have been killed. It was reported that the airplane hit the mountain about 200 feet below the summit.
Crew:
Maj Alexander Watson, pilot,
1st Lt Thomas E. Straughan, copilot,
M/Sgt Donald J. Down, navigator,
S/Sgt Terrell M. Young, flight engineer,
S/Sgt Harry E. Knight, radio operator.
Probable cause:
It was determined that the collision with the mountain was the consequence of several errors and omissions on part of the flying crew who neglected approach procedures and wrongly interpreted some signals transmitted by local beacons. This caused the crew to start the descent prematurely and the aircraft to drift off course by six miles to the northeast at the time of the accident. Low visibility due to clouds was considered as a contributing factor.

Crash of a Douglas C-54M Skymaster near Ketama: 8 killed

Date & Time: Dec 11, 1955
Type of aircraft:
Operator:
Registration:
44-9094
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Tripoli – Kenitra
MSN:
27320
YOM:
1945
Country:
Region:
Crew on board:
8
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
8
Circumstances:
While cruising in poor weather conditions, the four engine aircraft hit the slope of a mountain located 8 km southeast of Ketama. All eight crew members were killed.

Crash of a Douglas C-54-DO Skymaster in Seattle: 28 killed

Date & Time: Nov 17, 1955 at 2359 LT
Type of aircraft:
Registration:
N88852
Flight Phase:
Survivors:
Yes
Site:
Schedule:
Seattle – Newark
MSN:
3123
YOM:
1942
Flight number:
PNS17K
Crew on board:
4
Crew fatalities:
Pax on board:
70
Pax fatalities:
Other fatalities:
Total fatalities:
28
Captain / Total flying hours:
5920
Captain / Total hours on type:
1000.00
Copilot / Total flying hours:
5778
Copilot / Total hours on type:
531
Aircraft flight hours:
19630
Circumstances:
Peninsular Air Transport Common Carriage Flight 17K was scheduled to originate at Boeing Field and terminate at Newark, New Jersey, with intermediate refueling stops. The assigned crew consisted of Captain W. J. McDougall, First Officer F. C. Hall, and Steward J. O. Adams. The third pilot, Edward, McGrath, deadheading to Miami, Florida, occupied the jump seat with no crew duties. The flight, scheduled to depart at 2030, was delayed because of a heavy snowfall during the afternoon and early evening of November 17 which delayed passenger arrivals and necessitated removal of snow from the aircraft before departure. At 2332 the flight taxied to runway 13, holding off the runway waiting its turn behind other flights to take off, During this time the crew completed pre-takeoff cheeks and received an IFR (Instrument Flight Rules) clearance. This, in part, instructed them to turn right after takeoff and climb on the northwest course of the Seattle Range to 5,000 feet m. s. 1. (mean sea level). The takeoff was started at 2358 and appeared normal as the landing gear retracted and right turn was begun. When approximately 300-400 feet above the ground the first reduction of power, from takeoff to normal rated power, was made and about five of the 15 degrees of flaps extended, were retracted. At this time the No. 4 propeller surged and engine r. p. m. increased to about 2,800. Unable to reduce the r. p. m. of No. 4 by reducing its power an attempt was made to feather the propeller; this also was unsuccessful. As the aircraft then began to descend takeoff power was reapplied to Nos. 1, 2, and 3 engines and the power from No. 4 was further reduced. This action did not reduce the r. p. m. of No. 4 which surged again and increased to more than 3,000. The aircraft veered to the right and continued to descend. Realising that a crash-landing was imminent Captain McDougall reduced the airspeed until the aircraft was nearly stalled and applied full power to all four engines. The aircraft continued to settle. It then struck a telephone pole and several trees before crash-landing in a nose-high attitude. Fire and rescue equipment was dispatched to the scene from both the Seattle Fire Department and the Seattle-Tacoma Airport. The units arrived promptly and gave first aid to the survivors. Fire which followed the crash was quickly extinguished but not before extensive property was burned and the aircraft was nearly consumed. One crew member and 27 passengers were killed.
Probable cause:
The Board determines that the probable cause of this accident was the excessively high drag resulting from the improperly indexed propeller blades and inability to feather. These conditions were the result of a series of maintenance errors and omissions. The following findings were reported:
- Weather conditions at takeoff were above minim with respect to ceiling and visibility,
- There was no snow or ice on the aircraft when it took off,
- During the first power reduction the No. 4 engine r. p. m. fluctuated, became uncontrollable, and shortly thereafter increased to more than 3,000,
- Efforts to reduce the r. p. m. and feather the malfunctioning propeller were unsuccessful,
- The propeller dome retaining nut was not tightened sufficiently permitting oil to leak around the dome seal,
- The leaking oil resulted in a lack of oil for reducing the r. p. m. or feathering the No. 4 propeller,
- Poor maintenance procedures, omissions during maintenance, and lack of proper inspection were evident in the maintenance work performed by Seattle Aircraft Repair, Inc,
- Improper indexing of the No. 4 propeller blades occurred during the work at Seattle,
- Propeller drag from the overspeeding No. 4 propeller greatly increased by the incorrect indexing of the blades made continued flight difficult if not impossible,
- The aircraft was unairworthy following the Seattle maintenance work.
Final Report: