Crash of a Beechcraft B200 Super King Air in Akureyri: 2 killed

Date & Time: Aug 5, 2013 at 1329 LT
Operator:
Registration:
TF-MYX
Flight Type:
Survivors:
Yes
Schedule:
Reykjavik - Akureyri
MSN:
BB-1136
YOM:
1983
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
2600
Captain / Total hours on type:
1700.00
Copilot / Total flying hours:
2200
Copilot / Total hours on type:
1100
Aircraft flight hours:
15247
Aircraft flight cycles:
18574
Circumstances:
On 4th of August 2013 the air ambulance operator Mýflug, received a request for an ambulance flight from Höfn (BIHN) to Reykjavík Airport (BIRK). This was a F4 priority request and the operator, in co-operation with the emergency services, planned the flight the next morning. The plan was for the flight crew and the paramedic to meet at the airport at 09:30 AM on the 5th of August. A flight plan was filed from Akureyri (BIAR) to BIHN (positioning flight), then from BIHN to BIRK (ambulance flight) and from BIRK back to BIAR (positioning flight). The planned departure from BIAR was at 10:20. The flight crew consisted of a commander and a co-pilot. In addition to the flight crew was a paramedic, who was listed as a passenger. Around 09:50 on the 5th of August, the flight crew and the paramedic met at the operator’s home base at BIAR. The flight crew prepared the flight and performed a standard pre-flight inspection. There were no findings to the aircraft during the pre-flight inspection. The pre-flight inspection was finished at approximately 10:10. The departure from BIAR was at 10:21 and the flight to BIHN was uneventful. The aircraft landed at BIHN at 11:01. The commander was the pilot flying from BIAR to BIHN. The operator’s common procedure is that the commander and the co-pilot switch every other flight, as the pilot flying. The co-pilot was the pilot flying from BIHN to BIRK and the commander was the pilot flying from BIRK to BIAR, i.e. during the accident flight. The aircraft departed BIHN at 11:18, for the ambulance flight and landed at BIRK at 12:12. At BIRK the aircraft was refueled and departed at 12:44. According to flight radar, the flight from BIRK to BIAR was flown at FL 170. Figure 4 shows the radar track of the aircraft as recorded by Reykjavík Control. There is no radar coverage by Reykjavík Control below 5000 feet, in the area around BIAR. During cruise, the flight crew discussed the commander’s wish to deviate from the planned route to BIAR, in order to fly over a racetrack area near the airport. At the racetrack, a race was about to start at that time. The commander had planned to visit the racetrack area after landing. The aircraft approached BIAR from the south and at 10.5 DME the flight crew cancelled IFR. When passing KN locator (KRISTNES), see Figure 6, the flight crew made a request to BIAR tower to overfly the town of Akureyri, before landing. The request was approved by the tower and the flight crew was informed that a Fokker 50 was ready for departure on RWY 01. The flight crew of TF-MYX responded and informed that they would keep west of the airfield. After passing KN, the altitude was approximately 800’ (MSL), according to the co-pilot’s statement. The co-pilot mentioned to the commander that they were a bit low and recommended a higher altitude. The altitude was then momentarily increased to 1000’. When approaching the racetrack area, the aircraft entered a steep left turn. During the turn, the altitude dropped until the aircraft hit the racetrack.
Probable cause:
The commander was familiar with the racetrack where a race event was going on and he wanted to perform a flyby over the area. The flyby was made at a low altitude. When approaching the racetrack area, the aircraft’s calculated track indicated that the commander’s intention of the flyby was to line up with the racetrack. In order to do that, the commander turned the aircraft to such a bank angle that it was not possible for the aircraft to maintain altitude. The ITSB believes that during the turn, the commander most probably pulled back on the controls instead of levelling the wings. This caused the aircraft to enter a spiral down and increased the loss of altitude. The investigation revealed that the manoeuvre was insufficiently planned and outside the scope of the operator manuals and handbooks. The low-pass was made at such a low altitude and steep bank that a correction was not possible in due time and the aircraft collided with the racetrack. The ITSB believes that human factor played a major role in this accident. Inadequate collaboration and planning of the flyover amongst the flight crew indicates a failure of CRM. This made the flight crew less able to make timely corrections. The commander’s focus was most likely on lining up with the racetrack, resulting in misjudging the approach for the low pass and performing an overly steep turn. The overly steep turn caused the aircraft to lose altitude and collide with the ground. The co-pilot was unable to effectively monitor the flyover/low-pass and react because of failure in CRM i.e. insufficient planning and communication. A contributing factor is considered to be that the flight path of the aircraft was made further west of the airfield, due to traffic, resulting in a steeper turn. The investigation revealed that flight crews were known to deviate occasionally from flight plans.
Causal factors:
- A breakdown in CRM occurred.
- A steep bank angle was needed to line up with the racetrack.
- The discussed flyby was executed as a low pass.
- The maximum calculated bank angle during last phase of flight was 72.9°, which is outside the aircraft manoeuvring limit.
- ITSB believes that the commander’s focus on a flyby that he had not planned thoroughly resulted in a low-pass with a steep bank, causing the aircraft to lose altitude and collide with the ground.
Contributory factors:
- The commander’s attention to the activity at the race club area, and his association with the club was most probably a source of distraction for him and most likely motivated him to execute an unsafe maneuver.
- Deviations from normal procedures were seen to be acceptable by some flight crews.
- A flyby was discussed between the pilots but not planned in details.
- The flight crew reacted to the departing traffic from BIAR by bringing their flight path further west of the airport.
- The approach to the low pass was misjudged.
- The steep turn was most probably made due to the commander’s intention to line up with the race track.
Final Report:

Crash of a Piper PA-31-425 Pressurized Navajo in Reykjavik

Date & Time: Apr 22, 1997
Type of aircraft:
Operator:
Registration:
OY-AUT
Flight Type:
Survivors:
Yes
Schedule:
Reykjavik – Sondreströmfjord
MSN:
31-7400183
YOM:
1974
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Few minutes after takeoff from Reykjavik Airport, while cruising over Eyjafjallajökull, the pilote declared an emergency following the failure of the left engine. He was cleared to return to Reykjavik and was vectored for an approach to runway 14. On final, he encountered strong winds when the aircraft banked left then stalled and crashed 200 metres short of runway. The aircraft was damaged beyond repair and the pilot escaped uninjured. At the time of the accident, the wind was gusting from 100°-130° up to 35 knots.
Probable cause:
Engine failure for unknown reasons.

Crash of a Britten-Norman BN-2A-21 Islander near Keflavik

Date & Time: Mar 17, 1996 at 1212 LT
Type of aircraft:
Registration:
N904WA
Flight Type:
Survivors:
Yes
Schedule:
Reykjavik - Narsarsuaq
MSN:
904
YOM:
1981
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The pilot, sole on board, was completing a delivery flight from Europe to the US via Iceland and Greenland. Eight minutes after her departure from Reykjavik Airport, outbound to Narsarsuaq, the pilot informed ATC that her portable GPS fell on the ground and was not able to locate it. It such conditions, she decided to divert to Keflavik Airport when less than five minutes later, while descending, the right engine failed. For unknown reasons, she did not feather the propeller and did not elected to restart the engine. Due to drag and a loss of speed, the aircraft lost altitude and crashed near the village of Njarðvík, about 5 km east of Keflavik Airport. The aircraft was destroyed and the pilot was seriously injured.
Probable cause:
It was determined that the loss of power on the right engine was caused by the pilot who probably inadvertently reduced the mix ratio of the right engine while trying to find the portable GPS. For unknown reasons, she did not feather the propeller which increased drag and reduced speed and lift. A the time of the accident, the total weight of the aircraft was 297 kilos above MTOW, which was considered as a contributing factor.

Crash of a Partenavia P.68C on Mt Geitarhilđ: 1 killed

Date & Time: Jun 30, 1995 at 1416 LT
Type of aircraft:
Operator:
Registration:
TF-VEN
Flight Phase:
Survivors:
No
Site:
Schedule:
Reykjavik - Selfoss
MSN:
284
YOM:
1983
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
800
Captain / Total hours on type:
15.00
Aircraft flight hours:
2824
Circumstances:
The twin engine aircraft departed Reykjavik Airport on a schedule flight to Selfoss, Southern Region. While flying under VFR mode in IMC conditions, the pilot failed to realize his altitude was too low when the aircraft struck the slope of Mt Geitarhilđ located near Lake Kleif, about 20 km south of Reykjavik. The aircraft was destroyed by impact forces and a post crash fire and the pilot, sole on board, was killed.
Probable cause:
Controlled flight into terrain.
Final Report:

Crash of a Dornier DO.28D Skyservant in Nuuk

Date & Time: Dec 5, 1994 at 1223 LT
Type of aircraft:
Operator:
Registration:
D-IDNG
Flight Type:
Survivors:
Yes
Schedule:
Reykjavik - Goose Bay
MSN:
4112
YOM:
1971
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The twin engine aircraft was on a delivery flight from Germany to Colombia via Iceland and Canada, carrying one passenger and one pilot. On the leg from Reykjavik to Goose Bay, about 20 minutes into the flight, the right engine failed. As the pilot was unable to restart it, he decided to divert to Nuuk for an emergency landing. On short final, at a height of about 100 metres, the aircraft entered a right turn and struck the ground. Upon impact, the undercarriage were torn off and the aircraft came to rest against an embankment. Both occupants were slightly injured and the aircraft was damaged beyond repair.
Probable cause:
The exact cause of the engine failure could not be determined. Except the fact that a hinge pin was missing in the injector air heating system, no technical malfunction was found. It was reported that the pilot was not certified to perform such flight and the passenger was not allowed to take part to such mission according to the provisional airworthiness certificate that was valid till the day of the occurrence. The possible presence of windshear on final approach was not ruled out and it was also reported that the approach was completed with a speed that was approximately 10 to 15 knots below the prescribed approach speed.

Crash of a Rockwell Shrike Commander 500S off Vestmannaeyjar: 2 killed

Date & Time: Sep 23, 1994 at 2102 LT
Registration:
N9082N
Flight Type:
Survivors:
No
Schedule:
Biggin Hill – Reykjavik
MSN:
500-3068
YOM:
1970
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The crew was repatriating the aircraft from Kinshasa, Zaire, to the US. On the leg from Biggin Hill to Reykjavik, while approaching the Icelandic coast, the left engine failed. The crew declared an emergency and was cleared to divert to Vestmannaeyjar Airport. While circling for landing, the right engine failed as well. The crew lost control of the airplane that crashed in the sea few km offshore. Both occupants were killed.
Probable cause:
It was determined that the cause of the dual engine failure was the presence of a foreign material in the airframe fuel filters, causing restriction of the fuel flow and fuel starvation to both engines.

Crash of a Boeing 727-247 in the Atlantic Ocean: 16 killed

Date & Time: Sep 11, 1990 at 1530 LT
Type of aircraft:
Operator:
Registration:
OB-1303
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Valetta – London – Reykjavik – Gander – Miami – Lima
MSN:
20266
YOM:
1969
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
10
Pax fatalities:
Other fatalities:
Total fatalities:
16
Circumstances:
After being leased to Air Malta for few months, the aircraft was repatriated to Peru via London, Reykjavik, Gander and Miami. On the leg from Reykjavik to Gander, while at cruising altitude, the crew declared an emergency and elected to ditch the aircraft when contact was lost. Apparently, the aircraft crashed in the Atlantic Ocean about 290 km southeast from the Newfoundland coast. SAR operations were initiated but eventually abandoned few days later as no trace of the aircraft was found.
Probable cause:
Due to lack of evidences, the exact cause of the accident could not be determined. However, it is believed that the crew reported a low fuel warning.

Crash of a Rockwell Turbo Commander 680V in Keflavik

Date & Time: Aug 5, 1990
Registration:
N444GB
Flight Type:
Survivors:
Yes
Schedule:
Frobisher Bay – Reykjavik
MSN:
680-1565-21
YOM:
1966
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total hours on type:
15.00
Circumstances:
While approaching Iceland on a ferry flight from Frobisher Bay, the crew declared an emergency due to fuel shortage and requested the permission to divert to Keflavik Airport. On final approach to runway 29, both engines failed simultaneously. The aircraft stalled and crashed on a road located 1,500 meters short of runway. Both pilots were injured and the aircraft was destroyed.
Probable cause:
The pilot's experience on this type of aircraft was limited to 15 hours and he failed to calculate the fuel consumption correctly prior to departure from Frobisher Bay. It was determined that he calculated the flight as being 7 hours and 15 minutes while the autonomy of this aircraft is 8 hours and 20 minutes. Investigations revealed that both engines failed after six hours and 15 minutes of flight. Poor flight planning and preparation were considered as contributing factors.

Crash of a Casa 212 Aviocar 200 in Reykjavik: 3 killed

Date & Time: Aug 2, 1988 at 1742 LT
Type of aircraft:
Operator:
Registration:
C-GILU
Flight Type:
Survivors:
No
Schedule:
Ottawa – Goose Bay – Narsarsuaq – Reykjavik – Nantes
MSN:
245
YOM:
1982
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Aircraft flight hours:
4049
Circumstances:
The CASA 212 was bought by Geoterrex in 1983 and registered in Canada in 1985. The plane had been extensively modified for aerial survey work. These modifications consisted of two probes mounted on the fuselage above the cockpit and extending 10 feet in front of the aircraft nose, a l6-foot tail boom, and two wing tip pylons. The probes, pylons, and tail boom served to support a wire loop antenna which ran around the aircraft. In July 1988 the plane was prepared for a ferry flight across the Atlantic to Nantes, France. For the purposes of this ferry trip, the survey loop antenna and the wing tip pylons had been removed and stowed in the main cabin area. For this configuration a special ferry permit was necessary, but the company did not apply for one. On July 31, 1988 the aircraft departed Ottawa and arrived at Goose Bay later that day. On 2 August 1988, the aircraft departed Goose Bay at 09:05 UTC and arrived at Narsarsuaq, Greenland at 12:50 UTC. The aircraft was refuelled and departed one hour later at 13:50 UTC for Reykjavik, Iceland, at a planned altitude of FL130. Although the pilot’s instrument rating had expired and the co-pilot did not possess one, the crew filed an IFR flight plan to Reykjavik. The weight of the aircraft was about 3,000 pounds above the maximum authorized takeoff weight on takeoff from Narsarsuaq. At Reykjavik, the crew flew an ILS approach to runway 20. During the approach, the flaps were set at approximately 25 degrees, 15 degrees above the approved maximum of 10 degrees. Approximately one-half mile from the runway threshold, the aircraft entered a steep turn to the right, and the nose of the aircraft dropped sharply. The aircraft continued to turn to the right through 270 degrees and descended rapidly until it struck the ground approximately 900 feet short of the runway threshold. The aircraft burst into flames shortly after impact.
Probable cause:
The crew lost control of the aircraft most probably because of large fluctuations in the power output of the right engine caused by the shift of an incorrectly installed speeder spring in the right propeller governor.

Crash of a Beechcraft A65-8200 Queen Air near Angmagssalik: 2 killed

Date & Time: Mar 17, 1978 at 2215 LT
Type of aircraft:
Registration:
N8431N
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Washington D.C. – Sondreströmfjord – Reykjavik – Liverpool
MSN:
LC-307
YOM:
1969
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The crew was completing a ferry flight from Washington DC to Liverpool, UK, with intermediate stops in Sondreströmfjord and Reykjavik. On the leg between Greenland and Iceland, the crew encountered icing conditions and declared an emergency after the right engine failed. He was vectored to Kulusuk Airport which is a VFR Airfield located on the southeast coast of Greenland, near the city of Angmagssalik (Tasiilaq) and open to traffic by day only. An hour later, the crew started the descent but due to a limited visibility caused by night and clouds, he was unable to locate the runway and initiated a go-around. About 45 minutes later, while descending to an altitude of 1,700 feet, the airplane struck the slope of a mountain located near Angmagssalik. The airplane was destroyed upon impact and both pilots were killed.
Probable cause:
Controlled flight into terrain while attempting an approach below weather minimums. At the time of the accident, the aircraft was descending to an altitude of 1,700 feet while the minimum safe altitude for that area was 3,500 feet.
Final Report: