Crash of a Cessna 402A in Stord: 9 killed

Date & Time: Oct 12, 1998 at 2325 LT
Type of aircraft:
Registration:
OY-BHE
Survivors:
No
Schedule:
Aalborg - Stord
MSN:
402A-0062
YOM:
1979
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
9
Circumstances:
On final approach to Stord-Sørstokken Airport by night, the twin engine aircraft stalled and crashed in a rocky area located 180 metres short of runway 33. The aircraft was destroyed and all nine occupants were killed, among them eight naval workers.
Probable cause:
It was determined that both engines failed simultaneously on final approach due to fuel exhaustion.

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 Cessna 208B Caravan I in Oslo: 1 killed

Date & Time: Dec 4, 1994 at 0502 LT
Type of aircraft:
Operator:
Registration:
LN-PBC
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Oslo - Bergen
MSN:
208B-0310
YOM:
1992
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
1676
Captain / Total hours on type:
327.00
Aircraft flight hours:
2193
Circumstances:
The aircraft was completing a cargo flight to Bergen, carrying one pilot and 1,389 kilos of newspapers. Following a night takeoff from runway 19, while climbing in poor weather conditions at an altitude of about 390 metres, the single engine aircraft stalled and crashed in a wooded area located 1,5 km from the airport. The pilot, sole on board, was killed.
Probable cause:
The accident was the consequence of a stall during initial climb to an excessive accumulation of ice on wings and tail as the aircraft had not been deiced prior to departure. The following contributing factors were reported:
- The plane was outdoors for an estimated time of 20 minutes under conditions in which ice could adhere on the surface of the plane's hull, wings and tail surfaces.
- The plane was not de-iced by the pilot prior to departure.
- The company had not developed adequate written instructions for de-icing. The company had no written instructions to prevent icing during ground stay.
- The company had no sufficient equipment available, or added conditions sufficiently organized so that icin accretion be prevented or removed before departure from Gardermoen.
- The plane took off with ice on the surface of the wings and tail surfaces
- Ice on the surface of the wings and tail surfaces reduced flight characteristics in such a degree that the pilot did not manage to gain height after departure and therefore crashed.
Final Report:

Crash of a De Havilland DHC-6 Twin Otter 300 in Namsos: 6 killed

Date & Time: Oct 27, 1993 at 1916 LT
Operator:
Registration:
LN-BNM
Survivors:
Yes
Schedule:
Trondheim - Namsos
MSN:
408
YOM:
1974
Flight number:
WF744
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
17
Pax fatalities:
Other fatalities:
Total fatalities:
6
Captain / Total flying hours:
4835
Captain / Total hours on type:
1998.00
Copilot / Total flying hours:
6354
Copilot / Total hours on type:
1365
Aircraft flight hours:
40453
Circumstances:
On approach to Namsos Airport by night, the crew encountered poor visibility due to rain falls. In below weather minima, the crew descended below the minimum safe altitude until the aircraft struck the ground and crashed in a swampy area located about 6 km short of runway. The aircraft was destroyed on impact and six occupants including both pilots were killed. All 13 other occupants were injured.
Probable cause:
The accident was the consequence of a controlled flight into terrain. The following findings were reported:
- The company had failed to implement a standardized concept of aircraft operation that the pilots fully respected and lived by;
- The approach briefing was not not fully implemented in accordance with the rules. There were deficiencies in:
- "Call outs" during the approach
- Descent rate (feet/min) during "FAF inbound"
- Timing "outbound" from the IAF and the time from FAF to MAPt;
- The crew did not execute the "base turn" at the scheduled time, with the consequence that the plane ended up about 14 NM from the airport;
- The Pilot Flying ended the approach with reference to aircraft instruments and continued on a visual approach in the dark without visual reference to the underlying terrain. During this part of the approach the aircraft's position was not positively checked using any available navigational aids;
- Both crew members had in all likelihood most of the attention out of the cockpit at the airport after the Pilot Not Flying announced that he had it in sight;
- The crew was never aware of how close they were the underlying terrain;
- The last part of the descent from about 500 feet indicated altitude to 392 feet can be caused by inattention to the fact that the plane may have been a little out of trim after the descent;
- Crew Cooperation during the approach was not in accordance with with the CRM concept and seems to have ceased completely after the Pilot Not Flying called "field in sight";
- Before the accident the company had not succeeded well enough with the introduction of standardization and internal control/quality assurance. This was essentially because the management had not placed enough emphasis on awareness and motivate employees;
- The self-control system described in the airline operations manual and the parts of the quality system, was not incorporated in the organization and served as poor safety governing elements;
- Neither the Norwegian CAA nor the company had defined what visual reference to terrain is, what sufficient visual references are and what the references must be in relation to a moving aircraft.
Final Report:

Crash of a Beechcraft 200 Super King Air in Dagali: 3 killed

Date & Time: Mar 19, 1993 at 2002 LT
Operator:
Registration:
LN-TSA
Survivors:
Yes
Schedule:
Bergen - Dagali
MSN:
BB-308
YOM:
1978
Location:
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
5058
Captain / Total hours on type:
1330.00
Copilot / Total flying hours:
686
Copilot / Total hours on type:
11
Aircraft flight hours:
4032
Aircraft flight cycles:
4787
Circumstances:
The twin engine aircraft was performing an on-demand taxi flight from Bergen to Dagali, carrying eight passengers and two pilots. The descent to Dagali Airport was completed visually by night and poor weather conditions with clouds down to 1,200 feet and a visibility near minima. On final approach, the crew failed to realize his altitude was too low when the aircraft crashed in a hilly and snowy terrain located 5 km short of runway 26. Both pilots and a passenger were killed while seven other occupants were injured.
Probable cause:
The crew failed to adhere to the published procedures and continued a visual approach in difficult conditions. The following contributing factors were reported:
- Poor weather conditions and limited visibility,
- The captain was also General Manager, Operations Manager, Instructor, flight manager and member of the board of the operator. Thus, he was reporting to himself in case of any safety issue,
- The crew was not sufficiently trained,
- Lack of crew coordination during the final stage of the flight.
Final Report:

Crash of a De Havilland DHC-6 Twin Otter 100 in Honningsvåg: 3 killed

Date & Time: Oct 29, 1990 at 1430 LT
Operator:
Registration:
67-063
Flight Type:
Survivors:
Yes
MSN:
63
YOM:
1967
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
12
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
On final approach to Honningsvåg-Valan in marginal weather conditions, the aircraft started to pitch up and down then stalled. The crew increased power and the aircraft was able to gain a little height when it stalled a second time and crashed 150 meters short of runway threshold. Both pilots and a passenger were killed while 12 other occupants were injured.
Probable cause:
It was determined that the crew completed the approach at a too low airspeed according to the wind component and force. At the time of the accident, atmospheric turbulences and relative strong winds were present in the approach path and the crew failed to adapt his speed according to these phenomenons. The relative low experience of the crew was considered as a contributing factor.

Crash of a De Havilland DHC-6 Twin Otter 300 off Værøy: 5 killed

Date & Time: Apr 12, 1990 at 1444 LT
Operator:
Registration:
LN-BNS
Flight Phase:
Survivors:
No
Schedule:
Værøy – Bodø
MSN:
536
YOM:
1977
Flight number:
WF839
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
5534
Captain / Total hours on type:
1269.00
Copilot / Total flying hours:
1370
Copilot / Total hours on type:
354
Aircraft flight hours:
27304
Aircraft flight cycles:
58709
Circumstances:
Less than two minutes after takeoff from Værøy Airport runway 25, while climbing in marginal weather conditions, the aircraft banked left then entered an uncontrolled descent and crashed in the sea in a near vertical attitude about 1,8 km from the airport. The aircraft was destroyed and all five occupants were killed. When the crew started to roll at the airport, the wind was gusting to 57 knots which was 7 knots above the maximum allowable limit for ground operations. After takeoff, the aircraft encountered wind gusting to 34 knots which was 14 knots above the maximum allowable limit for flight operations. Excessive wind component caused the stabilizers/elevator to fail, causing the aircraft to enter an uncontrolled descent and to crash in the sea.
Probable cause:
The cause of the accident was that the plane during departure came into the wind that exceeded the aircraft's design criteria. Thus there was a break in the horizontal stabilizer / elevator which meant that the plane could no longer be controlled.
Final Report:

Crash of a Cessna 551 Citation II/SP near Bardufoss: 4 killed

Date & Time: Nov 15, 1989 at 2302 LT
Type of aircraft:
Registration:
LN-AAE
Flight Type:
Survivors:
No
Site:
Schedule:
Tromsø - Bardufoss
MSN:
551-0245
YOM:
1980
Flight number:
AXP05
Location:
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
8920
Captain / Total hours on type:
460.00
Copilot / Total flying hours:
4067
Copilot / Total hours on type:
405
Aircraft flight hours:
3417
Aircraft flight cycles:
3389
Circumstances:
The aircraft departed Tromsø-Langnes Airport at 2248LT on an ambulance flight to Bardufoss, carrying one patient and three crew members. Four minutes later, at an altitude of 8,000 feet, the crew contacted Bardufoss control and obtained information for an ILS approach to runway 29. At 2254LT, the crew awas cleared to descend to 6,000 feet and was instructed by ATC to report once established on the ILS. At about 22:57:50 at a position about 8 NM north of the Målselv (MLV) NDB, the airspeed increased from 265 knots to 285 knots over a distance of about 5 NM. This speed was maintained up to the NDB. At 22:59:30 LN-AAE passed the MLV NDB. Instead of performing the left hand procedure turn from 174° to 122°, the crew continued a straight heading for about 30 seconds at an airspeed about 100 knots above the recommended approach speed. The aircraft was about 2 NM (4 km) south in relation to the established procedure pattern. The airplane should still have been at 6,000 feet until established on the ILS but it had descended 1,250 feet below the minimum altitude when it collided with a relatively flat mountain ridge just south of the summit of Langfjelltind (4,935 feet). The wreckage was found about 35 km east-southeast of the airport and all four occupants were killed.
Probable cause:
The accident resulted in a controlled flight into terrain after the crew failed to follow the ILS approach procedure to runway 29.
Final Report:

Crash of a Rockwell Grand Commander 680FP off Kristiansand

Date & Time: May 3, 1989
Operator:
Registration:
TF-AFM
Flight Type:
Survivors:
Yes
MSN:
680-1420-148
YOM:
1964
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was completing a flight from Sweden to Iceland when he encountered engine problems and decided to divert to Kristiansand Airport. On final approach, the aircraft crashed in the sea few km short of runway 04. Both pilots were rescued while the aircraft was damaged beyond repair.

Crash of a De Havilland Dash-7-102 in Brønnøysund: 36 killed

Date & Time: May 6, 1988 at 2030 LT
Operator:
Registration:
LN-WFN
Survivors:
No
Schedule:
Trondheim – Namsos – Brønnøysund – Sandnessjøen – Bodø
MSN:
28
YOM:
1980
Flight number:
WF710
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
33
Pax fatalities:
Other fatalities:
Total fatalities:
36
Captain / Total flying hours:
19886
Captain / Total hours on type:
2849.00
Copilot / Total flying hours:
6458
Copilot / Total hours on type:
9
Aircraft flight hours:
16934
Aircraft flight cycles:
32347
Circumstances:
Widerøe flight 710 took off from Trondheim (TRD), Norway, at 19:23 local time on a domestic light to Namsos (OSY), Brønnøysund (BNN), Sandnessjøen (SSJ) and Bodø Airport (BOO).
The flight to Namsos was uneventful. The aircraft took off from Namsos at 20:07 and contacted Trondheim ACC six minutes later, stating that they were climbing from FL70 to FL90. At 20:20 the crew began their descent for Brønnøysund and switched frequencies to Brønnøysund AFIS. Weather reported at Brønnøysund was: wind 220°/05 kts, visibility 9 km, 3/8 stratus at 600 feet and 6/8 at 1000 feet, temperature +6 C, QNH 1022 MB. The crew executed a VOR/DME approach to Brønnøysund's runway 04, followed by a circle for landing on runway 22. The crew left the prescribed altitude 4 NM early. The aircraft descended until it flew into the Torghatten hillside at 560 feet. A retired police officer reported in July 2013 that a passenger had taken a mobile phone on board. The police officer disembarked the plane at Namsos, a stop-over and reported that the passenger with the mobile phone was seated in the cockpits jump-seat. After the accident, he reported this fact to the Joint Rescue Coordination Centre (JRCC). After reading the investigation report during the 25th anniversary of the accident, he noticed that there was no mention of the mobile phone.
NMT 450 network-based mobiles at the time were fitted with a 15-watt transmitter and a powerful battery which could lead to disruption in electronic equipment. The Norwegian AIB conducted an investigation to determine if electronic interference from the mobile phone might have affected the flight instruments. The AIB concluded that there was no evidence to support the theory that there was any kind of interference.
Probable cause:
The cause of the accident was that the last part of the approach was started about 4 NM too soon. The aircraft therefore flew below the safe terrain clearance altitude and crashed into rising terrain. The Board cannot indicate any certain reason why the approach started so early.
Final Report: