Crash of a Britten-Norman BN-2A-21 Islander in Ngau

Date & Time: Sep 23, 1996
Type of aircraft:
Registration:
DQ-FIF
Survivors:
Yes
Schedule:
Suva - Ngau
MSN:
417
YOM:
1974
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The approach and landing to Ngau Airport were completed in poor weather conditions with fog and rain falls. After landing on a wet grassy runway, the aircraft was unable to stop within the remaining distance (the runway is 760 metres long). It overran, lost its undercarriage and came to rest few dozen metres further. All five occupants escaped injured and the aircraft was damaged beyond repair.
Probable cause:
Wrong approach configuration on part of the crew who completed the landing at an excessive speed on a wet and short grassy runway.

Crash of a Tupolev TU-154M in Longyearbyen: 141 killed

Date & Time: Aug 29, 1996 at 1022 LT
Type of aircraft:
Operator:
Registration:
RA-85621
Survivors:
No
Site:
Schedule:
Moscow - Longyearbyen
MSN:
86A742
YOM:
1986
Flight number:
VKO2801
Country:
Region:
Crew on board:
11
Crew fatalities:
Pax on board:
130
Pax fatalities:
Other fatalities:
Total fatalities:
141
Captain / Total flying hours:
6232
Captain / Total hours on type:
1940.00
Copilot / Total flying hours:
19538
Copilot / Total hours on type:
10177
Circumstances:
Vnukovo Airlines flight VKO2801 departed Moscow-Vnukovo Airport at 04:44 UTC bound for Longyearbyen Airport on the Norwegian archipelago of Svalbard. It was a chartered flight with workers and their families to coal mining towns on Svalbard. The flight was uneventful until the start of the descent. Before radio contact with Longyear Information, the crew went through the detailed landing procedure for runway 10. At 09:56, the crew were cleared to start the descent. A little later, the crew received additional information consisting of runway in use 28, wind 230 degrees at 16 knots, visibility more than 10 km, rain showers, clouds: few at 1500 feet, scattered at 2000 feet and broken at 4000 feet, temperature +5°C, dewpoint -0°C and QNH 1005 hPa. (Later changed to 1006 hPa). The crew tried to request runway 10 for landing twice, but the request was not understood as such by Longyear Information due to language difficulties. When the flight was overhead the ADV beacon, at 10:15 hrs, the crew reported their position to Longyear Information and entered the base turn with a bank angle of 22 degrees. At 10:16 hrs, the aircraft came out of this turn on magnetic heading 160 degrees. During the right turn to the base turn, a malfunction occurred in the electric trimming mechanism, which was corrected by the crew. At 10:17, the crew started the turn to bring the aircraft out on the magnetic inbound course 300 degrees, as prescribed by the approach chart. The distance from the airport at this moment was 14 NM (25.9 km), as prescribed by the approach chart, but the lateral deviation from the outbound magnetic course 155 degrees from ADV was 2 NM (3.7 km) to the left. At 10:18, after the radio altimeter aural warning had been activated twice, the co-pilot took the controls and, after 6 seconds, turned the autopilot pitch channel off by 'overriding' it. From then on until the impact, the flight continued in autopilot mode in the roll channel, and in manual mode in the pitch channel. The aircraft passed through the localizer centerline and when the turn had been completed, the aircraft rolled out on a magnetic heading of 290 degrees. At this time, there was a discussion within the crew as to whether or not the final turn had been made at the correct time. The discussion led to the roll out of the turn to final approach and a corrective turn to the right to magnetic heading 306 degrees. At this point, the aircraft was 14.7 NM (27.4 km) from the airport, 2.8 km to the right of the approach centerline, maintaining an altitude of 5000 feet (1520 m ) and the crew increased the flap setting to 28 degrees. The airspeed was reduced to approx. 330 km/hr (180 kts). Instead of intercepting the centerline, the crew continued the flight on the right side, more or less paralleling the localizer course with minor heading changes. At 10:20 the flight made a corrective turn, resulting in a track close to 300 degrees. At this point, the lateral deviation from the approach centerline was 3.7 km to the right. During this corrective turn, the aircraft started descending. At 10:21, the crew made yet another corrective turn to the right. At 10:22:05, the aircraft started turning towards the left. The distance to the airport was 8 NM (14.8 km). On this part of the final approach, the aircraft apparently entered an area of strong turbulence created by the proximity to the mountains. The GPWS then activated 9 seconds before impact. The crew reacted to this by applying power and initiating a pitch-up. At 10:22:23, 7.7 NM (14.2 km) from the airport at an altitude of 2975 feet (907 m), the aircraft collided with the top of the mountain Operafjellet 3.7 km to the right of the approach centerline. All 141 occupants were killed, most of them employees of a local carbon mine and their family members.
Probable cause:
The following findings were reported:
1) There is no Russian procedure for offset localizer approaches modifying the required rule to set the landing course on the HSI.
2) The course selected on both HSIs was 283° even though the approach course is 300°. This setting does not affect the indication of the CDI. However, the CDI was pointing to 283° on the dial, which is 17° to the left of the approach course, giving a visual impression of wind drift to the left and therefore giving a possible reason for a heading correction to the right.
3) The navigator in a stressed and overloaded working situation most probably followed the rule setting the landing course 283° on the GPS in OBS mode instead of the approach course 300°.
4) The crew was not fully aware of the status of an AFIS officer in comparison with the authority of a Russian air traffic controller with the result that the crew accepted safety information from the AFIS officer as orders.
5) The crew had limited knowledge of the English language with the consequence that they had problems communicating their intentions to the AFIS officer.
6) The navigator was overloaded with tasks leaving little time for rechecking his work, thereby setting the scene for making mistakes.
7) The pilots did not monitor the work of the navigator sufficiently.
8) Leaving the communication with AFIS to the navigator during the approach was not according to the normative documents.
9) Due to the workload of the navigator, the decision of the co-pilot to transfer the responsibility of controlling the aircraft laterally to him, was inappropriate.
10) The crew resource management of the PIC was not satisfactory.
11) When the crew had made the decision to carry out the approach to runway 28, a new approach briefing was not accomplished.
12) The crew made the proper correction for the wind drift, but did not try to intercept the outbound track from ADV with the consequence that they overshot the approach centerline turning inbound.
13) Seemingly confusing indications on the HSIs in the base turn caused the crew to become uncertain of the aircraft position in relation to the LLZ 28 centerline. In this situation, the crew showed a lack of situational awareness.
14) The two pilots did not have the approach chart in front of them at all times during the approach making it difficult for them to maintain situational awareness.
15) The crew did not know of the possibility to check the position of the aircraft in relation to the localizer centerline by the VDF service available.
16) On final approach the crew probably put too much emphasis on the indications displayed on the GPS.
17) The crew started descent in a mountainous area without firm and positive control of the lateral navigation demonstrated by the disagreement within the crew as to whether to correct to the left or right.
18) In spite of the uncertainty within the crew as to whether they were approaching correctly or not, they continued instead of abandoning the approach and climbing to a safe altitude to solve the problem.
Final Report:

Crash of a Boeing 707-366C in Istanbul

Date & Time: Aug 21, 1996 at 1700 LT
Type of aircraft:
Operator:
Registration:
SU-AVX
Survivors:
Yes
Schedule:
Cairo - Istanbul
MSN:
20760
YOM:
1973
Flight number:
MS837
Country:
Region:
Crew on board:
11
Crew fatalities:
Pax on board:
120
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On final approach to Istanbul-Atatürk Airport, the crew encountered marginal weather conditions with rain falls. The visibility was estimated to be 8 km but on short final, the crew lost visual contact with the runway for few seconds while the aircraft encountered local strong showers. After touchdown on a wet runway 24, the aircraft was unable to stop within the remaining distance and overran. It lost its undercarriage, went through a fence, crossed a road and collided with various obstacles before coming to rest, broken in two. All 131 occupants were evacuated, among them 19 passengers were slightly injured.

Crash of a PZL-Mielec AN-2TP in Sovetskoye

Date & Time: Aug 17, 1996
Type of aircraft:
Operator:
Registration:
RA-01672
Flight Phase:
Survivors:
Yes
MSN:
1G83-13
YOM:
1967
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed in unknown circumstances. There were no casualties.

Crash of a Britten-Norman BN-2A Islander near Panama City

Date & Time: Aug 15, 1996 at 1200 LT
Type of aircraft:
Registration:
HP-839KN
Flight Phase:
Survivors:
Yes
MSN:
44
YOM:
1968
Country:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed in unknown circumstances near Panama City Airport. There were no casualties. The accident occurred somewhere in August 1996 (exact date unknown).

Crash of a Cessna 402B in Saint-Barthélemy

Date & Time: Aug 5, 1996 at 1335 LT
Type of aircraft:
Operator:
Registration:
N403N
Flight Phase:
Survivors:
Yes
Schedule:
Saint-Barthélemy – Charlotte Amalie
MSN:
402B-0900
YOM:
1975
Crew on board:
1
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On August 5, 1996, about 1335 Atlantic standard time, a Cessna 402B, N403N, registered to Virgin Air, Inc. dba Air St. Thomas, as flight 105, 14 CFR Part 135 scheduled international passenger service, from St. Barthelemy Island to St. Thomas, overran the runway during an aborted takeoff at St. Barthelemy Island. Visual meteorological conditions prevailed at the time and an instrument flight plan was filed. The aircraft received substantial damage and the airline transport-rated pilot and 6 passengers were not injured. One passenger received minor injuries. The flight was originating at the time of the accident. The pilot stated the elevator control jammed during the takeoff roll. He aborted the takeoff, but could not stop prior to over running the runway. The aircraft came to rest in about 3 feet of water.

Crash of a Boeing 737-2D6C in Tlemcen

Date & Time: Aug 2, 1996
Type of aircraft:
Operator:
Registration:
7T-VED
Flight Phase:
Survivors:
Yes
Schedule:
Tlemcen - Algiers
MSN:
20650
YOM:
1972
Location:
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
100
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
43293
Circumstances:
During the takeoff roll, the captain noted a difference in the engine N1 readings. He decided to abandon the takeoff procedure and initiated an emergency braking manoeuvre. Unable to stop within the remaining distance, the aircraft overran, lost its nose gear and came to rest 40 metres further. All 106 occupants escaped uninjured and the aircraft was damaged beyond repair.

Crash of a Yakovlev Yak-40 in Monrovia

Date & Time: Jul 25, 1996 at 1037 LT
Type of aircraft:
Operator:
Registration:
RA-87573
Survivors:
Yes
Schedule:
Freetown - Monrovia
MSN:
9 22 05 22
YOM:
1972
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Following an uneventful flight from Freetown, the three engine aircraft encountered windshear on final approach to Monrovia, lost height and struck the ground 5 metres before the runway threshold (0.8-1 meter below the runway elevation). The left main gear was torn off and the aircraft slid/rolled for about 300 metres before coming to rest. All 11 occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
Loss of control on short final after the aircraft encountered windshear.

Crash of a Fokker F27 Friendship 600 in Mergui: 8 killed

Date & Time: Jul 24, 1996
Type of aircraft:
Operator:
Registration:
XY-AET
Survivors:
Yes
Schedule:
Yangon - Mergui
MSN:
10433
YOM:
1970
Flight number:
UB309
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
45
Pax fatalities:
Other fatalities:
Total fatalities:
8
Circumstances:
While descending to Mergui Airport, the crew encountered poor weather conditions with heavy rain falls. On short final, the aircraft lost height and struck the ground about 250 metres short of runway 18. On impact, the undercarriage were torn off and the aircraft slid for few dozen metres before coming to rest in a 1,2 metre deep excavation located short of runway threshold. Eight passengers were killed while 16 others were seriously injured.
Probable cause:
It was reported that the crew initiated the approach while maintaining a visual contact with the runway. At an altitude of 1,500 feet, visual contact with the runway was lost due to heavy rain falls and the aircraft lost height and struck the ground in a relative flat attitude. The horizontal visibility at the time of the accident was estimated to be 1,500 metres and it is possible that the aircraft encountered windshear.

Crash of a Boeing 747-131 off East Moriches: 230 killed

Date & Time: Jul 17, 1996 at 2031 LT
Type of aircraft:
Operator:
Registration:
N93119
Flight Phase:
Survivors:
No
Schedule:
New York – Paris
MSN:
20083
YOM:
1971
Flight number:
TW800
Crew on board:
18
Crew fatalities:
Pax on board:
212
Pax fatalities:
Other fatalities:
Total fatalities:
230
Captain / Total flying hours:
18800
Captain / Total hours on type:
5490.00
Copilot / Total flying hours:
17000
Copilot / Total hours on type:
4700
Aircraft flight hours:
93303
Aircraft flight cycles:
16869
Circumstances:
On July 17, 1996, about 2031 eastern daylight time, Trans World Airlines, Inc. (TWA) flight 800, a Boeing 747-131, N93119, crashed in the Atlantic Ocean near East Moriches, New York. TWA flight 800 was operating under the provisions of 14 Code of Federal Regulations Part 121 as a scheduled international passenger flight from John F. Kennedy International Airport (JFK), New York, New York, to Charles De Gaulle International Airport, Paris, France. The flight departed JFK about 2019, with 2 pilots, 2 flight engineers, 14 flight attendants, and 212 passengers on board. All 230 people on board were killed, and the airplane was destroyed. Visual meteorological conditions prevailed for the flight, which operated on an instrument flight rules flight plan. The investigation revealed that the crash occurred as the result of a fuel/air explosion in the airplane's center wing fuel tank (CWT) and the subsequent in-flight breakup of the airplane. The investigation further revealed that the ignition energy for the CWT explosion most likely entered the CWT through the fuel quantity indication system wiring; neither the ignition energy release mechanism nor the location of the ignition inside the CWT could be determined from the available evidence. There was no evidence of a missile or bomb detonation.
Probable cause:
An explosion of the center wing fuel tank (CWT), resulting from ignition of the flammable fuel/air mixture in the tank. The source of ignition energy for the explosion could not be determined with certainty, but, of the sources evaluated by the investigation, the most likely was a short circuit outside of the CWT that allowed excessive voltage to enter it through electrical wiring associated with the fuel quantity indication system. Contributing factors to the accident were the design and certification concept that fuel tank explosions could be prevented solely by precluding all ignition sources and the design and certification of the Boeing 747 with heat sources located beneath the CWT with no means to reduce the heat transferred into the CWT or to render the fuel vapor in the tank non flammable.
Final Report: