Crash of a PZL-Mielec AN-2 near Dnipropetrovsk

Date & Time: Nov 18, 1982
Type of aircraft:
Operator:
Registration:
CCCP-54883
Flight Phase:
MSN:
1G185-50
YOM:
1980
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed in unknown circumstances after the crew got distracted. Occupant's fate unknown.

Ground fire of a Swearingen SA226AT Merlin IV in Copenhagen

Date & Time: Nov 12, 1982 at 1811 LT
Operator:
Registration:
OY-AUI
Survivors:
Yes
Schedule:
Stauning - Copenhagen
MSN:
AT-015
YOM:
1974
Flight number:
DX386
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
13
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
2395
Circumstances:
The aircraft was completing flight DX386 from Stauning to Copenhagen. It departed Stauning at 1724LT with 13 passengers and a crew of two on board. During approach to runway 22L at Kastrup Airport, the captain noticed a faint smell of burnt insulation and asked the copilot if he could smell anything "hot". The copilot who could not confirm the smell was asked by the captain to turn the cabin temperature - which was operated in manual mode - towards cold. The captain checked indication and warning systems for generators, batteries, circuit breakers and continued the approach. After a normal approach and landing at 18:07 hours the aircraft was cleared to the parking area via taxiway two and to change frequency to Apron Tower when clear of the runway. After contact with Apron Tower instructions were received for taxi to parking via taxiway two and inner perimeter but one minute later new instructions were received to taxi via runway three zero. While taxiing the left engine was shut down as is normal company procedure and taxiing continued on the right engine. Suddenly the captain noticed a flash outside the aircraft. The captain's first thought was that fire had started in the left engine or in the brakes and he brought the aircraft to a halt to investigate. Very shortly after a flash fire erupted in the left hand cockpit side console aft of and close to the captain's left leg. The crew made no radio transmissions about the fire since all electrical power was immediately turned off, in accordance with emergency procedure, after the aircraft was brought to a stop. The captain shouted towards the cabin: "It is burning, out". The passengers and crew then vacated the aircraft. The accident occurred at or about 18:11 hours on runway 30 during darkness. All 15 occupants escaped uninjured.
Probable cause:
An intense fire had erupted in the aft end of the left hand cockpit side console/ originating from an electrical short to ground. Contributing to the intensity of the fire was escaping oxygen under 70 PSI pressure through a melted PVC oxygen tube.

Crash of a Piper PA-31T-620 Cheyenne II in Kirkland Lake

Date & Time: Oct 18, 1982
Type of aircraft:
Operator:
Registration:
C-GSID
Survivors:
Yes
MSN:
31-7520042
YOM:
1975
Country:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed in unknown circumstances upon landing at Kirkland Lake Airport. There were no casualties.

Crash of a Boeing 707-366C in Geneva

Date & Time: Oct 17, 1982 at 1220 LT
Type of aircraft:
Operator:
Registration:
SU-APE
Survivors:
Yes
Schedule:
Cairo - Geneva - Zurich
MSN:
20342
YOM:
1970
Flight number:
MS771
Country:
Region:
Crew on board:
10
Crew fatalities:
Pax on board:
174
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
12564
Captain / Total hours on type:
4239.00
Copilot / Total flying hours:
3000
Copilot / Total hours on type:
350
Aircraft flight hours:
39002
Circumstances:
The four engine aircraft was performing a schedule service MS771 from Cairo to Zurich with an intermediate stop in Geneva, carrying 174 passengers and a crew of 10. Following an uneventful flight from Cairo-Intl, the crew was cleared to descent for an ILS approach to Geneva-Cointrin Airport runway 23. On short final, the captain failed to realize his altitude was insufficient when the right main gear struck an ILS antenna. Few seconds later, the airplane landed 35 meters short of runway threshold. While contacting the concrete runway, all three landing gear were torn off. The airplane slid on its belly for about 900 meters then made a left turn and lost its right wing before coming to rest. A fire erupted on the right side of the airplane but was quickly extinguished. All 184 occupants were evacuated, two passengers were seriously injured during the evacuation. The aircraft was destroyed.
Probable cause:
The accident was the consequence of the followings:
- Lack of decision on part of the pilot-in-command (captain) who failed to initiate a go-around procedure following a wrong approach configuration after the aircraft passed below 1,000 feet or at least after passing over the outer marker,
- Insufficient work coordination in the cockpit, after the crew failed to follow the approach checklist and all instructions relative to approach and landing controls, lack of a clear distribution of tasks as well as surveillance and mutual assistance (doublecheck / crosscheck),
- Stubbornness to land once the ground in sight despite a wrong approach configuration (airbrakes deployed) with an excessive rate of descent.
The following contributing factors were reported:
- Omission of a correct approach and landing planing,
- Late increase of engine power during the last portion of the approach,
- A possible inadvertent deployment of the interior airbrakes shortly before impact.
Final Report:

Crash of a Vickers 828 Viscount in Cuenca

Date & Time: Oct 8, 1982
Type of aircraft:
Operator:
Registration:
HC-ATV
Survivors:
Yes
Schedule:
Guayaquil – Cuenca
MSN:
458
YOM:
1962
Country:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
For unknown reasons, the four engine airplane landed long on runway 23 with an excessive speed. After touchdown, the crew started the braking procedure but the captain realized he could not stop the aircraft on the remaining distance. Thus he elected to steer the aircraft to the right of the runway. The right main gear dug into soft ground, causing the right wing to struck the ground as well as both right engines n°3 and 4. There were considerable structural damages to the right wing and right engines so the aircraft was considered as damaged beyond repair. There were no injuries.

Crash of a Fokker F27 Friendship 200 in Merowe

Date & Time: Oct 5, 1982
Type of aircraft:
Operator:
Registration:
ST-AAS
Survivors:
Yes
Schedule:
Khartoum - Merowe
MSN:
10194
YOM:
1962
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
17
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
33950
Aircraft flight cycles:
23052
Circumstances:
Crashed upon landing at Merowe Airport in unknown circumstances. There were no injuries among the 20 occupants.

Crash of an Ilyushin II-62M in Luxembourg: 7 killed

Date & Time: Sep 29, 1982 at 1923 LT
Type of aircraft:
Operator:
Registration:
CCCP-86470
Survivors:
Yes
Schedule:
Moscow - Luxembourg - Havana - Lima
MSN:
72503
YOM:
1977
Flight number:
SU343
Country:
Region:
Crew on board:
11
Crew fatalities:
Pax on board:
66
Pax fatalities:
Other fatalities:
Total fatalities:
7
Aircraft flight hours:
10325
Circumstances:
Following an uneventful flight from Moscow-Shermetyevo Airport, the crew completed the approach to Luxembourg-Findel Airport. While passing over the runway 06 threshold at a height of 5 meters and a speed of 278 km/h, engine power was reduced to 40% and thrust reversers were activated on engine n°1 and 4. For unknown reasons, reversers on engine n°1 failed to deploy and the airplane banked right. At a speed of 265 km/h, the airplane landed five seconds later and after touchdown, the spoilers were activated and the engine power increased on engine n°1 and 4 to 86% and 80% respectively. The airplane veered off runway to the right, rolled for 1,300 meters then struck a water tower before coming to rest 900 meters further, bursting into flames. 38 occupants were injured and 32 others were unhurt. Unfortunately, seven passengers were killed in the accident.
Probable cause:
The accident may be attributed to a mechanical failure affecting the mechanism of controlling thrust which occurred during the most critical phase of landing. This failure, sudden and unpredictable, was identified by the crew and made the aircraft uncontrollable in direction during the execution of the normal landing procedure.

Crash of a PZL-Mielec AN-2 in Shimkent

Date & Time: Sep 28, 1982
Type of aircraft:
Operator:
Registration:
CCCP-44628
Survivors:
Yes
MSN:
1G87-05
YOM:
1967
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed on landing for unknown reasons. There were no casualties.