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Crash of a Lockheed C-130J-30 Super Hercules near Kiruna: 5 killed

Date & Time: Mar 15, 2012 at 1457 LT
Type of aircraft:
Operator:
Registration:
5630
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Harstad - Kiruna
MSN:
5630
YOM:
2010
Flight number:
HAZE 01
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
6153
Captain / Total hours on type:
5937.00
Copilot / Total flying hours:
3285
Copilot / Total hours on type:
243
Aircraft flight hours:
856
Circumstances:
The accident occurred during a Norwegian military transport flight from Harstad/Narvik Airport (Evenes) in Norway to Kiruna Airport in Sweden. The flight was performed as a part of the Norwegian-led military exercise Cold Response. The aircraft, which was of the model C-130J-30 Super Hercules, had the call sign HAZE 01. HAZE 01 took off with a crew of four and one passenger on board. The aircraft climbed to Flight Level 130 and assumed a holding pattern south of Evenes. After one hour, the flight continued towards Kiruna Airport. The Norwegian air traffic control had radar contact and handed over the aircraft to the air traffic control on the Swedish side. Swedish air traffic control cleared HAZE 01 to descend to Flight Level 100 “when ready” and instructed the crew to contact Kiruna Tower. The crew acknowledged the clearance and directly thereafter, the aircraft left Flight Level 130 towards Flight Level 100. The lower limit of controlled airspace at the location in question is Flight Level 125. HAZE 01 informed Kiruna Tower that the aircraft was 50 nautical miles (NM) west of Kiruna and requested a visual approach when approaching. Kiruna Tower cleared HAZE 01, which was then in uncontrolled airspace, to Flight Level 70, and the aircraft continued to descend towards the cleared flight level. Neither ACC Stockholm nor Kiruna Tower had any radar contact with the aircraft during the sequence of events because the Swedish air navigation services do not have radar coverage at the altitudes at which HAZE 01 was situated. HAZE 01 levelled out at Flight Level 70 at 14.57 hrs. Half a minute later, the aircraft collided with the terrain between the north and south peaks on the west side of Kebnekaise. Data from the aircraft's recording equipment (CVR and DFDR) showed that HAZE 01 was flying in level flight at a ground speed of approximately 280 knots prior to the moment of collision and that the crew was not aware of the imminent danger of underlying terrain. The remaining distance to Kiruna Airport was 42 NM (77 km). Everyone on board received fatal injuries. Accidents in complex systems are rarely caused by a single factor, but there are often several circumstances that must coincide for an accident to occur. The analysis of the investigation deals with the circumstances which are deemed to have influenced the sequence of events and the barriers which are intended to prevent dangerous conditions from arising. In summary, the investigation indicates that latent weaknesses have existed both at the Norwegian Air Force and at LFV. It is these weaknesses and not the mistakes of individual persons that are assessed to be the root cause of the accident. On the part of flight operations, the investigation has found shortcomings with respect to procedures for planning and following up a flight. Together with a probably high confidence in air traffic control, this has led to the crew not noticing that the clearance entailed an altitude that did not allow for adequate terrain separation. In terms of the air traffic services, the investigation demonstrates that the aircraft was not issued clearances and flight information in accordance with applicable regulations. This is due to it not having been ensured that the air traffic controllers in question had sufficient experience and knowledge to guide air traffic from the west in towards Kiruna Airport in a safe manner under the present circumstances. The lack of radar coverage reduced the opportunities for air traffic control to monitor and guide air traffic. The aircraft's Ground Collision Avoidance System is the last barrier and is intended to be activated and provide warning upon the risk of obstacles in the aircraft's flight path. The investigation has shown that with the terrain profile in question and the settings in question, the criteria for a warning were not fulfilled. No technical malfunction on the aircraft has caused or contributed to the occurrence of the accident. The rescue operation was characterized by very good access to resources from both Sweden and abroad. The operations lasted for a relatively long time and were carried out under extreme weather conditions in difficult alpine terrain. The investigation of the rescue operation demonstrates the importance of further developing management, collaboration and training in several areas.
Probable cause:
The accident was caused by the crew on HAZE 01 not noticing to the shortcomings in the clearances issued by the air traffic controllers and to the risks of following these clearances, which resulted in the aircraft coming to leave controlled airspace and be flown at an altitude that was lower than the surrounding terrain.
The accident was rendered possible by the following organizational shortcomings in safety:
- The Norwegian Air Force has not ensured that the crews have had sufficiently safe working methods for preventing the aircraft from being flown below the minimum safe flight level on the route.
- LFV has not had sufficiently safe working methods for ensuring, partly, that clearances are only issued within controlled airspace during flight under IFR unless the pilot specifically requests otherwise and, partly, that relevant flight information is provided.
Final Report:

Crash of a De Havilland DHC-3 Otter in Rossfjordstraumen

Date & Time: Mar 28, 1968
Type of aircraft:
Operator:
Registration:
LN-FAE
Flight Phase:
Survivors:
Yes
Schedule:
Tromsø – Harstad
MSN:
18
YOM:
1953
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft on amphibious floats departed from Tromso at 1015 hours for a scheduled flight to Harstad. In addition to the pilot, a company mechanic was on board as an assistant and there were three passengers. The weather was not good, with low cloud, heavy snow showers and reduced visibility. Due to the conditions, the pilot elected to divert from the track laid out in the company's route manual. This change of route however was not reported to air traffic control because of poor radio coverage at low altitude. This is a very rugged coastal area with numerous fjords and inlets amidst mountains rising to four thousand feet. As the Otter flew in on the west side of Rossfjord, some 45 kilometres south-west of Tromso, visibility dropped and the pilot said to his assistant “We'll cut across here, I know this area” and started a right turn. Eye witness reports put the aircraft at this time at between 100 feet and 25 feet above the ice-covered fjord, although the pilot was later to claim he was flying at 500 feet. Immediately after starting the turn, the right wingtip and float made contact with the ground. The aircraft was thrown to the left at the first impact and crashed at a 35 degree angle to its direction of travel. It caught fire and was burnt to destruction. All five occupants survived the crash but one passenger and the pilot's assistant suffered severe burns and were flown by helicopter to hospital in Tromso.
Source: https://www.dhc-3archive.com
Probable cause:
The Accident investigation Board was not able to determine whether the pilot meant to make a 180 degree turn and fly back out of the fjord, or initiate a climb to get across a low mountain ridge and out into the next fjord to the west. The Board concluded that the accident was caused by the pilot’s decision to turn towards higher terrain. If the purpose was to exit the fjord, it should have been made to the left over the fjord. If it was to climb across the ridge, it would not have been possible to clear the terrain, given the aircraft’s weight and performance.

Crash of a Noorduyn Norseman IV in Harstad

Date & Time: Oct 3, 1953
Type of aircraft:
Operator:
Registration:
LN-SUW
Flight Phase:
MSN:
728
YOM:
1944
Location:
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Caught fire shortly after takeoff and crashed in flames. Occupant fate remains unknown. The aircraft was destroyed.

Crash of a Short S.25 Sandringham 6 off Harstad

Date & Time: May 15, 1950
Type of aircraft:
Operator:
Registration:
LN-IAU
Flight Phase:
Survivors:
Yes
Schedule:
Harstad – Tromsø
MSN:
SH.882
Location:
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
26
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Shortly after takeoff from the bay of Vagsfjorden off Harstad, while in initial climb, the seaplane stalled and crashed into the sea. All 33 occupants were quickly rescued and the airplane sank an hour later.

Crash of a Short S.25 Sandringham VI near Harstad: 35 killed

Date & Time: Aug 28, 1947 at 0905 LT
Type of aircraft:
Operator:
Registration:
LN-IAV
Flight Phase:
Survivors:
No
Site:
Schedule:
Tromsø – Harstad – Bodø – Hommelvik – Oslo
MSN:
SH.915
Location:
Country:
Region:
Crew on board:
8
Crew fatalities:
Pax on board:
27
Pax fatalities:
Other fatalities:
Total fatalities:
35
Circumstances:
While cruising at an altitude of 13,000 feet in poor weather conditions, the four engine seaplane hit the slope of a mountain located 31 km northeast of Harstad. The wreckage was found in a rocky are some 290 meters from the summit and all 35 occupants were killed. It is believed that the aircraft was slightly off course at the time of the accident.
Crew:
John Buer, pilot,
Karl Bengtsen, copilot,
Johannes Daae Risnes, navigator,
Paul Idland, radio operator,
Gunnar Michaelsen, mechanic,
Atle Fedje, steward,
Ester Mildrid Løsnes, stewardess.