Crash of a Tupolev TU-124 in Minsk

Date & Time: Jun 13, 1966
Type of aircraft:
Operator:
Registration:
CCCP-45017
Survivors:
Yes
Schedule:
Moscow - Minsk
MSN:
1 35 05 02
YOM:
1961
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Following an uneventful flight from Moscow, the pilot-in-command completed the landing at Minsk-Loshitsa Airport (Minsk-1). After touchdown, the airplane was unable to stop within the remaining distance, overran and came to a halt. While there were no injuries among the occupants, the airplane was damaged beyond repair.

Crash of a Noorduyn Norseman at Pekogaming Lake

Date & Time: May 25, 1966
Type of aircraft:
Registration:
CF-IRI
Flight Phase:
Survivors:
Yes
MSN:
672
YOM:
1944
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Shorty after takeoff from Pekogaming Lake, while climbing, the engine failed. The aircraft stalled, hit trees and crashed in a dense wooded area. All six occupants were injured while the aircraft was destroyed.
Probable cause:
Engine failure during initial climb.

Crash of a Lockheed L-749A Constellation near Tomas: 49 killed

Date & Time: Apr 27, 1966 at 0805 LT
Operator:
Registration:
OB-R-771
Flight Phase:
Survivors:
No
Site:
Schedule:
Lima - Cuzco
MSN:
2521
YOM:
1947
Flight number:
LP501
Location:
Country:
Crew on board:
6
Crew fatalities:
Pax on board:
43
Pax fatalities:
Other fatalities:
Total fatalities:
49
Captain / Total flying hours:
14684
Captain / Total hours on type:
1692.00
Copilot / Total flying hours:
963
Copilot / Total hours on type:
875
Aircraft flight hours:
47899
Circumstances:
Flight 501 was a scheduled domestic flight from Lima to Cuzco. It was instructed to take-off from runway 15 and to climb in accordance with No. 2 standard climb procedure, described as follows in the airline's route guide: climb on a heading of 190° until 9 NM southwest of the airport, then on a heading of 120°. The flight took off from Lima-Callao-Jorge Chavez International Airport at 0740LT, 10 minutes after the take-off time indicated on the flight plan. At 0757 hours it contacted Lima radio on the route frequency, 126.9 MCIS, and reported: "Departed Lima- Callao at 1240Z, climbing, estimating Ayacucho at 1337Z. It This was the last message from the aircraft, although Lima and Cuzco repeatedly called the aircraft around 0840 hours. One witness from "Tres Cruces" and two witnesses from the village of San Pedro de Pilas testified that their attention was attracted between 0800 and 0805 hours by an aircraft flying unusually low over San Pedro de Pilas or Tamard; one of the witnesses stated that he had been able to read the "LANSA" inscription on the aircraft. They had heard on several occasions aircraft flying over the area, but these were always seen at much higher altitudes. They all concurred that the aircraft was following the gap between San Pedro de Pilas and Tamard and was flying toward the mountain range below the level of the peaks. The two witnesses from San Pedro de Pilas pointed out positions on the Huamantanga peak where they observed the aircraft evading the mountain by a slight turn to .the left and entering the gap towards the east. They did not see any smoke or signs of fire and one indicated that he was positive that all four engines were operating at the time. The wreckage of the aircraft was located on 28 April on the southeast slopes of Mount Talaula at an elevation of 12 600 ft, 61 NM from Lima-Callao Airport and 29 NM north of the normal route. All 49 occupants have been killed.
Probable cause:
The Commission considered that the probable cause of the accident was pilot error in that he:
a) Incorrectly selected the route to be flown in violation of the provisions established by the Airline for operation of flight 501;
b) Incorrectly calculated the climb performance of the aircraft in relation to its total weight of takeoff. This aircraft type, with a gross takeoff weight of 90,572 lb can't within the 25 minutes of flight after takeoff attain the altitude required to fly over the peaks of the Cordillera which are encountered over the distance that can be covered in the above-indicated time along the route followed by the aircraft. Under such conditions the operation can be performed only by flying the aircraft. Under such conditions the operation can be performed only by flying the aircraft at lower levels between the mountains, in violation of the most elementary principles of flight safety;
c) Erroneously estimated the elevation of the nearby peaks he had to clear along the route. The Commission considered that the critical moment of decision came in the area of the towns of Tamara and Pilas which are separated by a gap running into the Cordillera and joining in the same area another wide gap into which flows the Rio Omas and which leads to the coastal town of Asia. At this point the pilot could still have flown out to the east but this would have entailed continuing on this course, then turning to avoid Mount Huamantanga (12 600 feet), since he was flying below the elevation of the mountain so as to enter the gap and follow it up to the Cordillera even though it would have been flying below the elevation of surrounding peaks. The Tamara and Pilas gap, the entrance to which is in the area of the above mentioned villages, at a rather low elevation, is about 5 nm wide along its entire length up to the Cordillera, rises very steeply until it reaches elevations of more than 14 000 feet, which could not be cleared by the subject aircraft, considering its weight, the climb characteristics of the aircraft, the time to fly the 5nm length of the gap and the altitude of the aircraft when it entered the gap;
d) In view of the flight experience of the pilot in command, who had completed 112 flights on the 501-502 route, one can only surmise that his judgment was affected by insufficient rest and his particular state of mind as a result of his assignment to perform the flight for which he was not rostered. He may have been further influenced in the selection of the direct route by the perfect weather conditions obtaining at the time;
e) Finally, although there was no evidence of any mechanical failure the Commission could not definitely rule out the possibility of some 'undetermined' factor during the two minutes if flight from San Pedro de Pilas to the point of impact inside the gap. If such was the case, this would have only aggravated the situation, since it was considered that after having entered the Tamara-Pilas gap, the aircraft could not have been cleared the peaks along the route nor come back. In view of this circumstance, it was considered that an 'undetermined factor did not necessarily cause the accident.
Final Report:

Crash of an Ilyushin II-14P off Baku: 33 killed

Date & Time: Apr 23, 1966 at 0803 LT
Type of aircraft:
Operator:
Registration:
CCCP-61772
Flight Phase:
Survivors:
No
Schedule:
Baku – Makhatchkala – Saratov
MSN:
1460 003 10
YOM:
1956
Flight number:
SU2723
Location:
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
28
Pax fatalities:
Other fatalities:
Total fatalities:
33
Aircraft flight hours:
16257
Circumstances:
Twelve minutes after takeoff, while climbing in stormy weather, both engines started to run intermittently, maybe due to a technical problem with the sparking plugs while in contact with water. In such conditions, the captain decided to return to Baku-Bina Airport but due to poor visibility, he was unable to locate the airfield. Five minutes later, both engines temperature dropped and four minutes later, out of control, the airplane crashed into the sea off Baku. SAR operations were quickly conducted but eventually suspended few days later as no trace of the aircraft nor the 33 occupants was found. On May 13, 1966, the wreckage was found at a depth of 23 meters some 19 km south of the Nargen Island.
Probable cause:
Investigations were unable to determine with certainty the cause of the engine problems.

Crash of a Douglas C-47B-45-DK in Porto Nacional

Date & Time: Apr 20, 1966
Operator:
Registration:
PP-VAY
Survivors:
Yes
MSN:
17013/34276
YOM:
1945
Country:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Suffered an accident at Porto Nacional Airport. No casualties.

Crash of a Douglas DC-3C in Skopje

Date & Time: Apr 16, 1966
Type of aircraft:
Operator:
Registration:
YU-ABG
Flight Phase:
Survivors:
Yes
MSN:
14035/25480
YOM:
1944
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed in unknown circumstances while taking off from Skopje Airport. There were no casualties.

Crash of an Antonov AN-24B in Cairo: 30 killed

Date & Time: Mar 18, 1966 at 1658 LT
Type of aircraft:
Operator:
Registration:
SU-AOA
Survivors:
No
Schedule:
Berlin – Nicosia – Cairo
MSN:
57302009
YOM:
1965
Flight number:
MS749
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
25
Pax fatalities:
Other fatalities:
Total fatalities:
30
Circumstances:
Flight 749 took off from Nicosia at 15:49 for a flight to Cairo. Bad weather existed along the route and weather at destination Cairo was also worsening. The crew contacted Misrair Operations and requested information about possible airports for a diversion. The crew also reported they where flying in a thunderstorm with turbulent and icing conditions. One altimeter read 24000 feet while the other read 25000 feet, the magnetic compass was unserviceable and there was a crack in a cockpit window panel due to the thunderstorm. Possible like Alexandria, Port Said and El Arish were discussed, but the flight continued to Cairo. The flight was cleared for a runway 23 approach and landing, but nothing more was heard from the flight. The aircraft had crashed and caught fire 5 km from the runway.
Probable cause:
The accident arose from the descent of the aircraft below the safe flight altitude in the final approach and the impact of the port wing against the sand dunes lying to the northeast of the aerodrome. As a result the pilot lost control of his aircraft and hit the ground. It is probable that the cause of descent of the aircraft below the safe level was due to the change from IFR to VFR, taking into consideration that considerable time would have been needed for the pilot to have adapted to this change in the prevailing weather conditions.

Crash of a Grumman G-21A Goose off Reef Island: 6 killed

Date & Time: Mar 10, 1966 at 1714 LT
Type of aircraft:
Operator:
Registration:
CF-MSK
Survivors:
Yes
MSN:
B032
YOM:
1943
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
6
Captain / Total flying hours:
12719
Captain / Total hours on type:
246.00
Circumstances:
The descent to Reef Island was completed in marginal weather. On approach, the aircraft struck power cables, stalled and crashed into the Portland Canal. The wreckage was located a day later and the pilot was evacuated while all six passengers were killed. The aircraft sank and was lost. At the time of the accident, weather conditions were poor with snow falls reducing the visibility to half a mile and a wind up to 35 knots.
Probable cause:
It was determined that the pilot continued the descent under VFR mode in adverse weather conditions and misjudged the altitude and clearance. Low ceiling, snow, unfavorable wind conditions and downdrafts/updrafts were considered as contributing factors.
Final Report:

Crash of a Pilatus PC-6/340-H2 Porter in Genjem

Date & Time: Mar 8, 1966
Operator:
Registration:
PK-NPY
Flight Phase:
Survivors:
Yes
MSN:
538
YOM:
1964
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed in unknown circumstances in Genjem. There were no casualties but the aircraft was written off.

Crash of a Boeing 707-436 on Mt Fuji: 124 killed

Date & Time: Mar 5, 1966 at 1415 LT
Type of aircraft:
Operator:
Registration:
G-APFE
Flight Phase:
Survivors:
No
Site:
Schedule:
San Francisco – Honolulu – Tokyo – Hong Kong – London
MSN:
17706
YOM:
1960
Flight number:
BA911
Location:
Country:
Region:
Crew on board:
11
Crew fatalities:
Pax on board:
113
Pax fatalities:
Other fatalities:
Total fatalities:
124
Captain / Total flying hours:
14724
Captain / Total hours on type:
2155.00
Copilot / Total flying hours:
3663
Copilot / Total hours on type:
2073
Aircraft flight hours:
19523
Aircraft flight cycles:
6744
Circumstances:
BOAC Flight 911 was a scheduled service from San Francisco (SFO) to Hong Kong (HKG) via Honolulu (HNL) and Tokyo (HND). The Boeing 707 was expected to arrive at Tokyo Airport at 16:45 on 4 March. However, due to poor meteorological conditions at Tokyo and because the precision approach radar (PAR) of the GCA was out of service, it diverted to Fukuoka (FUK) and landed there at 18:00. After staying overnight at Fukuoka, Flight 911 left for Tokyo at 11:25 and landed there at 12:43. The aircraft was prepared for the next leg to Hong Kong and a flight plan was filed for a flight in accordance with the instrument flight rules via Oshima on airway JG6 to Hong Kong at FL310. At 13:42 hours the crew contacted ATC requesting permission to start the engines and clearance for a VMC climb via Fuji-Rebel-Kushimoto. The aircraft left the ramp at 13:50. It was instructed to make "a right turn after take off", and departed Tokyo Airport at 13:58. After takeoff the aircraft flew over Gotemba City on a heading of approximately 298 deg at an altitude of approximately 4900 m and indicated airspeed of 320 to 370 knots. The aircraft, trailing white vapor, then suddenly lost altitude over the Takigahara area, and parts of the aircraft began to break away over Tsuchiyadai and Ichirimatsu. Finally over Tarobo at an altitude of approx. 2000 m, the forward fuselage broke away. The mid-aft fuselage together with the wing, making a slow flat spin to the right, crashed into a forest at the foot of Mount Fuji. The forward fuselage crashed into the forest approx. 300 m to the west of the above site and caught fire. All 124 occupants were killed.
Probable cause:
The aircraft suddenly encountered abnormally severe turbulence over Gotemba City which imposed a gust load considerably in excess of the design limit.
Final Report: