Crash of a Douglas DC-6A on Mt Rainier: 5 killed

Date & Time: Apr 23, 1965 at 1423 LT
Type of aircraft:
Operator:
Registration:
N6541C
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Seattle – Ogden-Hill
MSN:
45369/984
YOM:
1958
Flight number:
AAX1422A
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
6861
Captain / Total hours on type:
4088.00
Copilot / Total flying hours:
17310
Copilot / Total hours on type:
5214
Aircraft flight hours:
18315
Circumstances:
On April 23, 1965, at 1423 P.s.t., an AAXICO Airlines, Inc., Douglas DC-6A, N6541C, crashed on the west slope of Mt. Rainier, Washington. The accident site was 40.2 nautical miles southeast of the Seattle ‘VORTAC, on the 125° radial, at an elevation of 10,200 feet m.s.l. The aircraft was being operated as Logair Flight 1422A, on a Visual Flight Rules (VFR) flight from Boeing Field, Seattle, Washington, to Hill Air Force Base (AFB), Utah. All five crew members received fatal injuries as a result of the crash. The flight was attempting to obtain an Instrument Flight Rules (IFR) clearance when it struck the snow covered glacier. The aircraft was destroyed by impact. There was no fire.
Probable cause:
The Board determines that the probable cause of this accident was the improper correlation of the aircraft position with respect to obstructing terrain while continuing the flight on a VFR flight plan in instrument weather conditions.
Final Report:

Crash of a Douglas DC-6B on Mt San José: 87 killed

Date & Time: Feb 6, 1965 at 0836 LT
Type of aircraft:
Operator:
Registration:
CC-CCG
Flight Phase:
Survivors:
No
Site:
Schedule:
Santiago – Buenos Aires – Montevideo
MSN:
45513/1004
YOM:
1958
Flight number:
LA107
Country:
Crew on board:
7
Crew fatalities:
Pax on board:
80
Pax fatalities:
Other fatalities:
Total fatalities:
87
Aircraft flight hours:
17085
Circumstances:
Flight 107 was a scheduled international fiight from Los Cerrillos Airport, Santiago (Chile) to Montevideo, Uruguay, with a scheduled stop at Buenos Aires, Argentina. The flight plan was as follows:
(a) VMC - Santiago - Melipilla - Cerro Maipo climbing to 19 000 feet,
(b) VMC - Cerro Maipo - San Rafael - Huinca Renanco - Junin - Suipacha - Buenos Aires (Ezeiza) in level flight at 19 800 feet.
The aircraft took off at 0806 hours from south to north in the direction of the city of Santiago. It flew low over the city in the Cerro San Cristobal area and later between 0810 and 0812 hours in the vicinity of Cerro Marquehue. At 0817 hours, it made radio contact with Panagra Control to request a change of route via Amarillo - Tumuyan Viejo - Reynolds 5,700 m. Mendoza Control authorized the change of route and asked for the estimated time over Amarillo. The flight replied that it estimated reaching Amarillo at 0336 hours. At 0822 the radio contact came to an end. The aircraft continued inland at low altitude in relation to the surrounding terrain, via Farellones, Lagunillas, Planta Queltehue and Lo Valdés. At 0836 hours, several witnesses saw the aircraft crash into the ridge joining the Catedral and Corona peaks. The aircraft disintegrated on impact and all 87 occupants have been killed.
Probable cause:
The accident was caused by lack of discipline on the part of the pilot-in- command of the aircraft who did not follow the instructions of the flight plan or those relating to crossing the mountains.
Final Report:

Crash of a Douglas DC-6B on Mt Alcazaba: 80 killed

Date & Time: Oct 2, 1964 at 0545 LT
Type of aircraft:
Operator:
Registration:
F-BHMS
Flight Phase:
Survivors:
No
Site:
Schedule:
Paris – Marseille – Palma de Majorque – Nouadhibou – Nouakchott
MSN:
44062
YOM:
1953
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
73
Pax fatalities:
Other fatalities:
Total fatalities:
80
Captain / Total flying hours:
10964
Aircraft flight hours:
29620
Circumstances:
The aircraft was flying a scheduled international passenger flight from Paris to Marseilles, Palma de Mallorca and Port-Etienne. The trip to Palma was uneventful and, following receipt of the latest meteorological information available, the aircraft took off from runway 27 for Port-Etienne at 0314 hours GMT. According to its flight plan the air- craft was to check with the following while en route: area control centres at Barcelona, Seville, Casablanca and Dakar and the control tower at Port-Etienne. At 0339 hours, it advised Palma control tower that it was over Ibiza. It reported to Barcelona FIR that it had crossed the FIR boundary at 0401 hours at flight level 100. At 0353 hours, it reported to Seville FIR that it was estimating the FIR boundary at 0401 at flight level 100 and Los Alcazares at 0415 hours. At 0420 hours, it reported having passed Los Alcazares in clear skies at 0415 hours, estimating abeam Malaga at 0500 hours, overhead Tanger at 0524, and Port-Etienne at 1020 hours. This was the last communication from the flight. Seville FIR tried subsequently, without success, to contact the aircraft. The aircraft hit a mountain at 0445 hours.
Probable cause:
At the time of last contact with the aircraft it was flying in clear skies. The aircraft deviated from the flight plan but flew at altitudes within the established safety margin, then struck a mountain. The reason for the deviation from the planned route could not be determined. It is believed that after Los Alcazares (0415 hours), the aircraft headed for Tanger, deviating slightly from the planned route which was 25 km away from the scene of the accident and at altitudes which were within the established safety margin. The difference between the Los Alcazares - Tanger route and the Los Alcazares - site of the accident route, exceeds 5°. Since the automatic pilot error is plus or minus 1°, the remaining 4° may have been caused by wind or some other undiscovered error.
Final Report:

Crash of a Douglas DC-6B on Mt Cameroon: 55 killed

Date & Time: May 3, 1963 at 1427 LT
Type of aircraft:
Operator:
Registration:
F-BIAO
Flight Phase:
Survivors:
No
Site:
Schedule:
Douala – Lagos
MSN:
45479
YOM:
1958
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
48
Pax fatalities:
Other fatalities:
Total fatalities:
55
Captain / Total hours on type:
6561.00
Copilot / Total flying hours:
4811
Copilot / Total hours on type:
3435
Circumstances:
The four engine aircraft departed Douala Airport at 1416LT bound for Lagos. While climbing to an altitude of 6,500 feet, the airplane struck the slope of Mt Cameroon located 63 km northwest of Douala Airport. The wreckage was located few hours later 800 meters below the summit. Two passengers were seriously injured while 53 other occupants were killed. Three days after the crash, on May 6, one of the survivor died from his injuries and on May 9, the second survivor died as well.
Probable cause:
The accident was caused by a lack of caution on the part of the pilot-in-command who deliberately selected a route which led the aircraft into a dangerous and even prohibited sector at too low an altitude. Also, he neglected his navigation and transferred to instrument flight when approaching the mountain range.
Final Report:

Crash of a Douglas DC-6B in Copenhagen

Date & Time: Apr 13, 1963 at 0404 LT
Type of aircraft:
Operator:
Registration:
OY-EAP
Flight Type:
Survivors:
Yes
Schedule:
Las Palmas – Barcelona – Copenhagen
MSN:
43750
YOM:
1952
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
9617
Captain / Total hours on type:
768.00
Copilot / Total flying hours:
1770
Copilot / Total hours on type:
171
Aircraft flight hours:
33819
Circumstances:
On 12 April 1963, at 1521 hours GMT, Sterling Airways' DC-6B, OY-EAP, took off from Las Palmas Airport in the Canary Islands on a three-engine ferry flight bound for Copenhagen. After an intermediate refuelling stop at Barcelona, the aircraft departed again at 2224 GMT for Copenhagen. It contacted Copenhagen ATC when passing Michelsdorf on 13 April, at 0238 GMT. It was then at FL110 which was maintained until the aircraft, when over ROBBY NDD, was cleared to descend to FL45. At 0253 GMT, when passing PRESTO NDB at FL60, the aircraft reported that Copenhagen Airport was in sight, whereafter the flight mas performed with visual contact to this airport's runway 04. When passing marker beacon CODAN on the north coast of Stevns, the aircraft descended to 3,500-4,000 feet, the speed being normal, i. e. 170 kt. About 1 - 1/2 minutes later flaps were set to 20°, whereafter the speed in the course of the next few minutes was slowly reduced to 145 kt at which rate the undercarriage was extended and the flap angle was increased to 300. The altitude was then approximately 1 500 ft and the approach towards the clearly visible runway was continued in a shallow glide. The approach was rather low, for which reason the engine power had to be increased several times in order to reach the runway. On short final - probably immediately before passing the first approach lights - the pilot-in-command ordered full flaps. The speed was then 110-130 kt and the height still rather low. Shortly after the flaps were fully extended the aircraft showed a tendency to bank which the pilot-in-command tried to counteract by applying aileron control. When the aircraft was 100-200 m from the runway threshold, the pilot-in-command realizing that he no longer had sufficient control to make as the landing decided to abandon the landing. He ordered "pulling-up, full power, gear up, flaps twenty". The speed was then around 100 kt. The flight engineer immediately pushed the propeller pitch selector lever forward to full RPM position and thereafter advanced the throttles, at the same time moving the landing gear lever to the "up" position. When power was applied the aircraft immediately made a violent bank and an uncontrollable right-hand turn. About 10 seconds later the starboard wing tip hit the ground about 200 m beyond the threshold of runway 04 and 80 m to the right of the centre line. This caused the disintegration of the outer portion of the starboard wing whereupon the aircraft crashed. The aircraft came to a stop 220 m further on with its nose pointing roughly to 240°. The accident occurred at 0304 GMT, i. e. one hour before sunrise. The aircraft was destroyed by impact forces and a post crash fire. All three crew members were injured.
Probable cause:
During the approach to runway 04 with the starboard outer engine inoperative, the speed of the aircraft decreased to a value critical for safe manoeuvring. Because of this the pilot-in-command attempted an overshoot. In the course thereof he lost control of the aircraft which, in a heavy bank, went into an uncontrolled right-hand turn, its starboard wing hit the ground, and the aircraft crashed. That the aircraft got into the above-mentioned critical situation must,to an essential degree, be attributed to the fact that the pilot-in-command selected full flaps at a time when the altitude and speed of the aircraft in relation to the distance from the runway threshold did not justify such disposition.
Final Report:

Crash of a Douglas DC-6B in Hamāh: 1 killed

Date & Time: Apr 7, 1963
Type of aircraft:
Operator:
Registration:
YK-AEB
Flight Phase:
Survivors:
Yes
Schedule:
Aleppo – Hamāh – Damascus
MSN:
43749
YOM:
1953
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
26
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
While taking off from Hamāh Airport, the four engine airplane went out of control, veered off runway and came to rest in flames. A passenger died while 29 other occupants were evacuated. The aircraft was destroyed.

Crash of a Douglas DC-6B on Mt Chachacomani: 39 killed

Date & Time: Mar 15, 1963 at 1355 LT
Type of aircraft:
Operator:
Registration:
CP-707
Flight Phase:
Survivors:
No
Site:
Schedule:
Arica – La Paz – Cochabamba
MSN:
43547
YOM:
1951
Flight number:
LB915
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
36
Pax fatalities:
Other fatalities:
Total fatalities:
39
Captain / Total flying hours:
10069
Captain / Total hours on type:
1319.00
Copilot / Total flying hours:
4034
Copilot / Total hours on type:
910
Circumstances:
The airplane departed Arica on the return flight at approximately 1327 hours Bolivian time. It was to be an eight-hour, VFR flight, and the aircraft was to cruise at 17,000 feet. Eight minutes after take-off the crew advised ATC at Cochabamba of the departure time, the number of passengers on board, the aircraft's weight and the amount of fuel being carried. Between 1347 and 1348 the air traffic controller at La Paz advised that Panagra flights 701 and 393, flying at 22,000 and 21,000 feet were estimating Charaña at 1355 and Arica at 1351 respectively. Flight 915 acknowledged the message. ATC at La Paz called the flight at approximately 1400 hours, and several times thereafter, to report on the new positions of the two Panagra aircraft, which were in the Arica zone but received no reply. It was determined subsequently that the aircraft crashed into Chachacomani Peak (latitude 17°49'00'', longitude 69°50'00''W) in Peruvian territory near the Chilean border at an altitude of 14,250 feet, sometime between 1351 and 1355. The wreckage was spotted by the crew of a reconnaissance aircraft few hours later and the first rescuers arrived on scene later to confirm that all 39 occupants have been killed.
Probable cause:
A flight under visual flight rules was attempted below the minimum altitude indicated in the flight plan in weather conditions that were marginal for this type of operation and were associated with the severe turbulence which usually exists in that region (western area).
Final Report:

Crash of a Douglas DC-6B on Mt Velino: 5 killed

Date & Time: Mar 8, 1962 at 2300 LT
Type of aircraft:
Operator:
Registration:
I-DIMO
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Khartoum – Rome
MSN:
44254
YOM:
1954
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
The crew was completing a cargo flight from Khartoum to Rome-Ciampino Airport and started the approach by night from the east. At an altitude of 7,700 feet, the four engine aircraft struck the slope of Mt Velino located 14 km north of Avezzano. The wreckage was found 125 meters below the summit and all five crew members were killed.
Crew:
Salvatore Di Gaetano 4.
Probable cause:
It is believed the accident was caused by a premature descent on part of the crew.

Crash of a Douglas DC-6B in Boston

Date & Time: Nov 15, 1961 at 1710 LT
Type of aircraft:
Operator:
Registration:
N8228H
Flight Phase:
Survivors:
Yes
Schedule:
Boston – New York – Norfolk
MSN:
43821
YOM:
1953
Flight number:
NA429
Crew on board:
5
Crew fatalities:
Pax on board:
25
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
8000
Captain / Total hours on type:
1445.00
Copilot / Total flying hours:
6000
Copilot / Total hours on type:
1459
Aircraft flight hours:
26849
Circumstances:
On November 15, 1961, at approximately 1710LT, 47 minutes after sunset, a ground collision occurred at Logan International Airport, Boston, Massachusetts, between a National Airlines DC-6B, N8228H, attempting a takeoff on runway 09 and a Northeast Airlines Viscount N6592C, during its landing roll on runway 04R. National Airlines Flight 429 originated at Boston. Its destination was Norfolk, Virginia, with five intermediate stops. Northeast Airlines Flight 120 originated at Washington, D. C. Its destination was Boston, Massachusetts, with an intermediate stop at LaGuardia Airport, New York. There were no serious injuries to either the crew or passengers of the DC-6; however, four passengers of the Viscount received minor cuts and abrasions while deplaning. There was major damage to both aircraft. As a result of this accident the Board recommended to the Federal Aviation Agency that consideration be given to requiring that all restrictive clearances or instructions issued by air traffic control be acknowledged by pilot repetition.
Probable cause:
The Board finds that this ground collision accident occurred as the result of commencement of takeoff by National 429 without clearance. Contributing factors were the failure of tower personnel to provide adequate surveillance of the active runways and to issue an appropriate warning message to the pilot of National 429 alerting him to the impending traffic confliction.

Crash of a Douglas DC-6 in Ndola: 16 killed

Date & Time: Sep 17, 1961 at 2213 LT
Type of aircraft:
Operator:
Registration:
SE-BDY
Flight Type:
Survivors:
No
Schedule:
Léopoldville - Ndola
MSN:
43559
YOM:
1952
Flight number:
UNO001
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
11
Pax fatalities:
Other fatalities:
Total fatalities:
16
Captain / Total flying hours:
8000
Captain / Total hours on type:
1350.00
Copilot / Total flying hours:
2700
Copilot / Total hours on type:
720
Circumstances:
The airplane was conducting a special flight (UNO001) from Léopoldville to Ndola on behalf of the United Nations Organizations, carrying five crew members and a 11 passengers, among them Dag Hammarskjöld, United Nations General Secretary. During the final approach to Ndola by night, the four engine aircraft was too low, struck trees and crashed in flames in a wooded area located 15 km short of runway. The aircraft was totally destroyed and all 16 occupants have been killed.
Probable cause:
It was strongly urged that the Commission should not conclude that the accident was due to pilot error. Reasons have been given for saying that other suggested causes were not really possible. Reasons have also been given for concluding that the approach was made by a visual descent procedure in which the aircraft was brought too low. It could not be said whether that came about as a result of inattention to the altimeters or misreading of them. The Commission felt it must conclude that the aircraft was allowed, by the pilots, to descend too low. In so doing it struck trees and crashed.
COMMENTS FROM THE UNITED NATIONS:
The Commission has carefully examined all possible causes of the accident. It has considered the possibility of sabotage or of attack and the material or human failures which could have resulted in an accident. It has found no evidence to support any of the particular theories that have been advanced nor has it been able to exclude the possible causes which it has considered. In this connexion it notes that the United Nations and the Swedish Observers who participated in the work of the Rhodesian Board of Investigation also expressed the opinion that it was impossible to exclude any of the possible causes which they considered or to establish an order of priority among them. With respect to sabotage it has noted that the aircraft was without special guard while it was at N'Djili Airport in Léopoldville and access to it was not impossible. The Commission is aware that there are many possible methods of sabotage. No evidence of sabotage has come to its attention but the possibility cannot be excluded. The possibility of attack from either the air or the ground has also been fully examined. The Commission has found no evidence that an attack of any kind occurred It has also noted the opinion of experts that it is improbable that the plane would have been in the apparently normal approach position indicated by the crash path and wreckage analysis had it been under attack. Nevertheless, it cannot exclude attack as a possible cause of the crash. The Commission has also considered various possibilities of material failure, including technical or structural defects, altimeter failure or fire in flight. A thorough analysis of that part of the wreckage capable of being examined was made by technical experts, including members of the Rhodesian Board of Investigation and United Nations and Swedish observers. The altimeters were examined in the United States by the Civil Aeronautics Board and the manufacturer. No evidence of material failure of the aircraft was found, but this possibility cannot be excluded, mainly because of the destruction of a major part of the aircraft by fire. The Commission also considered various possibilities of human failure. It found no evidence that any of the pilots had been incapacitated. It cannot, however, completely exclude this possibility as some forms of incapacity might not be revealed by a post-mortem examination, It also considered various possibilities of pilot error, including the use of a wrong instrument approach chart or a misreading of altimeters. It noted that the Rhodesian inquiry, by eliminating to its satisfaction other possible causes, had reached the conclusion that the probable cause of the crash was pilot error. The Commission, while it cannot exclude this possibility, has found no indication that this was the probable cause of the crash. The Commission considered the possibility that during the course of a visual or semi-visual approach or through the use of an instrument procedure involving a descending turn, the aircraft might have come below the accepted safety margin of 1 000 ft above ground level. On some landing charts, information concerning exact elevations in the approach area is not provided and should the aircraft have descended below the accepted margin a momentary distraction, either from inside or outside the aircraft, might have caused the pilot to lose the remainder of his margin of safety. The Commission however, has found no evidence that this could have been a possible cause of the crash. The Commission considers it its duty to record that it has examined the various rumors that have come to it, attention concerning the cause of the crash and has found no evidence in their support.
Final Report: