Crash of a Vickers 833 Viscount in Tel Aviv

Date & Time: Oct 26, 1969
Type of aircraft:
Operator:
Registration:
4X-AVC
Flight Type:
Survivors:
Yes
Schedule:
Tel Aviv - Tel Aviv
MSN:
425
YOM:
1959
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was completing a night training mission at Tel Aviv Airport, consisting of touch-and-go manoeuvres. After landing, control was lost and the airplane veered off runway before coming to rest. All three pilots were slightly injured while the aircraft was damaged beyond repair.

Ground accident of a Vickers 754D Viscount in Honolulu

Date & Time: Jun 27, 1969 at 0702 LT
Type of aircraft:
Operator:
Registration:
N7410
Flight Phase:
Survivors:
Yes
Schedule:
Honolulu – Molokai
MSN:
242
YOM:
1957
Location:
Crew on board:
3
Crew fatalities:
Pax on board:
11
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
7000
Captain / Total hours on type:
3000.00
Circumstances:
While taxiing at Honolulu Airport, on a flight to Molokai, the pilot-in-command lost control of the airplane that collided with a parked Hawaii Air DC-9 registered N906H. While the DC-9 was slightly damaged, the Viscount was damaged beyond repair and the 14 occupants were uninjured.
Probable cause:
Loss of control during taxi due to the failure of the landing gear braking system. It was determined that the crew lost brakes and steering as the hydraulic system was not bled of air. The following factors were considered as contributing:
- Improper maintenance and inspection on part of the maintenance personnel,
- Inadequate preflight preparation on part of the flying crew.
Final Report:

Crash of a Vickers 757 Viscount in Seven Islands: 1 killed

Date & Time: Apr 7, 1969
Type of aircraft:
Operator:
Registration:
CF-THK
Survivors:
Yes
Schedule:
Seven Islands - Montreal
MSN:
271
YOM:
1957
Country:
Crew on board:
4
Crew fatalities:
Pax on board:
16
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
Shortly after takeoff from Seven Islands Airport, while climbing, the crew reported a fire on engine number two and was cleared to return for a safe landing. After touchdown, the crew started an emergency braking procedure when control was lost due to fire in the left main gear wheel well. The airplane veered off runway to the right before coming to rest in flames. A passenger died during the evacuation and the aircraft was written off.
Probable cause:
Overheating of the starter selector relay during starting of no.1 and 2 engines. The proximity of a wire bundle to the relay provided a source of combustibles for the initial fire.

Crash of a Vickers 815 Viscount in Manchester: 3 killed

Date & Time: Mar 20, 1969
Type of aircraft:
Operator:
Registration:
G-AVJA
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Manchester - Edinburgh
MSN:
336
YOM:
1959
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The crew (two pilots and two flight attendants) was completing a positioning flight to Edinburgh-Turnhouse Airport. Both pilots took the opportunity to make some training and decided to simulate an engine failure at takeoff. Shortly after liftoff at Manchester-Ringway Airport, while in initial climb, the crew shut down the engine n°4 and feathered its propeller when the airplane started to yaw sharply to starboard. Control was lost then the aircraft crashed inverted and burst into flames. A flight attendant was injured while three other occupants were killed.
Crew:
I. Wallace, pilot, †
R. A. Weeks, copilot, †
S. Wallis, stewardess, †
Jane Timson, stewardess.

Crash of a Vickers 736 Viscount in East Midlands

Date & Time: Feb 20, 1969
Type of aircraft:
Operator:
Registration:
G-AODG
Survivors:
Yes
Schedule:
Glasgow – East Midlands
MSN:
77
YOM:
1955
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
48
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On approach to East Midlands Airport, the crew encountered poor weather conditions (snow falls) and the captain decided to go-around. During a second attempt to land on runway 10, the pilot-in-command failed to realize his exact position when the airplane struck the ground 1,000 feet prior to the touchdown zone. Upon impact, the nose gear was torn off and the aircraft came to rest in a snow covered field, broken in two. All 53 occupants escaped uninjured while the aircraft was written off.
Probable cause:
Wrong approach configuration in poor weather conditions.

Crash of a Vickers 794D Viscount in Ankara

Date & Time: Feb 2, 1969
Type of aircraft:
Operator:
Registration:
TC-SET
Survivors:
Yes
MSN:
432
YOM:
1958
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
22
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On final approach to Ankara-Esenboğa Airport, the crew encountered marginal weather conditions and failed to realize his altitude was too low. On final, the four engine airplane struck a concrete pole, stalled and crashed in a snow covered field. On impact, the airplane lost its undercarriage, broke in two and came to rest few hundred meters short of runway. All 26 occupants were evacuated safely while the aircraft was destroyed.

Crash of a Vickers 720 Viscount near Port Hedland: 26 killed

Date & Time: Dec 31, 1968 at 1135 LT
Type of aircraft:
Operator:
Registration:
VH-RMQ
Flight Phase:
Survivors:
No
Schedule:
Perth – Port Hedland
MSN:
45
YOM:
1954
Flight number:
MV1750
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
22
Pax fatalities:
Other fatalities:
Total fatalities:
26
Captain / Total flying hours:
19129
Captain / Total hours on type:
367.00
Copilot / Total flying hours:
2660
Copilot / Total hours on type:
143
Circumstances:
Flight 1750 was a scheduled domestic flight from Perth to Port Hedland in the State of Western Australia. Whilst taxiing for take-off on runway 02 at Perth Airport, the crew received and acknowledged an air traffic clearance communicated by Perth Tower. Of the alternative clearances offered, the pilot-in-command elected to proceed via the 030° radial of the Perth Very High Frequency Omni-Range (VOR), to Ballidu, whilst climbing to FL 170. Take-off was normal and the crew reported the departure time as 0836 hours Western Standard Time. At 0839 hours the pilot-in-command reported that he was climbing at an indicated airspeed of 155 kt, instead of the 175 kt proposed in the flight plan, because of turbulence which he first encountered at 1 500 ft. During this climb the co-pilot also advised Perth that the aircraft would continue its climb beyond the proposed FL 170 and cruise at FL 190. Apart from these minor changes to the flight plan the aircraft continued normally along the intended route with position reports being transmitted as scheduled to Perth Flight Service Centre, Meekatharra Flight Service Unit and Port Hedland Flight Service Centre. At 1114 hours the aircraft advised Port Hedland that it was abeam Wittenoom Gorge at FL 190 and that its estimated time of arrival at Port Hedland was 1142 hours. At 1120 hours the flight advised that it would be commencing its descent from FL 190 in three minutes and at 11-34 hours it reported that it was 30 miles by Distance Measuring Equipment south of Port Hedland-and had left 7 000 ft on descent. The flight service officer at Port Hedland acknowledged this message and transmitted the surface wind and temperature conditions and the altimeter setting for landing at Port Hedland. When this communication was not acknowledged further calls were made but no further communication from the aircraft was heard or recorded. At about the time that the aircraft failed to respond to the radio communication, two persons, each in different positions, saw the aircraft descending rapidly and steeply although these observations were made from distances of 44 and 64 miles respectively. Neither of these eyewitnesses was able to observe any impact with the ground because of intervening high terrain. At 1212 hours a Cessna 337 aircraft left Port Hedland to search along the route which the aircraft had been expected to follow and, eleven minutes later, the pilot of the search aircraft saw the burning wreckage of the Viscount aircraft, close to the intended route. Approximately one hour later a ground party from Port Hedland reached the scene of the accident. The location of the wreckage was later determined to be 28.1 miles on a bearing of 184' true from Port Hedland Airport. The aircraft was totally destroyed and none of the 26 occupants survived the crash.
Probable cause:
The cause of the accident was that the fatigue endurance of the starboard inner main spar lower boom was substantially reduced by the insertion of a flared bush at station 143 when the margin of safety associated with the retirement life specified for such booms did not ensure that this boom would achieve its retirement life in the presence of such a defect.
Final Report:

Crash of a Vickers 827 Viscount in São Paulo: 3 killed

Date & Time: Sep 15, 1968 at 2120 LT
Type of aircraft:
Operator:
Registration:
PP-SRE
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
São Paulo - São Paulo
MSN:
399
YOM:
1958
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The crew was engaged in a local training flight at São Paulo-Congonhas Airport and was completing touch-and-go manoeuvres. After takeoff, while in initial climb, the airplane went out of control and crashed in a district located 7,450 meters from the airport. The aircraft was totally destroyed and both pilots were killed as well as one people on the ground. At the time of the accident, the crew was climbing with one engine inoperative, maybe two.
Probable cause:
Loss of control due to insufficient speed while climbing with one or two engine inoperative. It is believed the crew may overestimated the aircraft capabilities and performances.

Crash of a Vickers 739A Viscount in Langenbruck: 48 killed

Date & Time: Aug 9, 1968 at 1304 LT
Type of aircraft:
Operator:
Registration:
G-ATFN
Flight Phase:
Survivors:
No
Schedule:
London-Heathrow - Innsbruck
MSN:
394
YOM:
1958
Flight number:
EG802
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
44
Pax fatalities:
Other fatalities:
Total fatalities:
48
Aircraft flight hours:
18658
Circumstances:
While cruising at an altitude of 21,000 feet south of Ingolstadt, the pilot informed ATC that a fire erupted on board, declared an emergency and requested the permission to divert to Munich Airport. The crew immediately started an emergency descent when control was lost. The airplane entered a dive, partially disintegrated in the air and eventually crashed in flames on a highway. Debris were found in an open field and the main wreckage on the Munich - Nuremberg highway. The tail was found about three km from the main wreckage. Rescue teams were hampered in their mission and it was really difficult to reach the crash site as the highway was totally jammed by cars from people living on holidays. None of the 48 occupants survived the crash. At the time of the accident, weather conditions were considered as good despite broken clouds from 800 feet till 15,000 feet.
Probable cause:
It was determined that the main generator failed in flight, causing a major power failure and probably an electrical short-circuit. This caused several systems and onboard instruments to fail such as the gyrocompas. While cruising in poor visibility due to clouds, the crew was unable to maintain a proper attitude and the aircraft went out of control. During the descent, aerodynamic forces exceeded the certification of the tail and the wings that were torn off. Then, the aircraft impacted ground at a speed of 310 knots. The accident was unsurvivable. The exact cause of the generator failure could not be determined with certainty.

Crash of a Vickers 812 Viscount in Southend

Date & Time: May 4, 1968
Type of aircraft:
Operator:
Registration:
G-APPU
Survivors:
Yes
Schedule:
Rotterdam - Southend
MSN:
364
YOM:
1958
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
79
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew completed the landing procedure on a wet runway 06 at a too high speed. After touchdown, the captain started the braking procedure but thought he was encountering aquaplaning situation when control was lost. The airplane veered to the right and went down an embankment before coming to rest, broken in several pieces. All 83 occupants were evacuated safely while the aircraft was destroyed.
Probable cause:
The accident was caused through landing at a too high speed for the landing distance available. A contributory factor was reduced braking effectiveness due to the main wheel being mechanically locked by the application of the hand-brake.