Nordland

Kato Airline flight KAT603, an aircraft of the type Dornier 228-202 with registration LN-HTA, was to fly a regular scheduled flight from Røst airport (ENRS) to Bodø airport (ENBO). There were two passengers and two pilots on board. There was a strong westerly wind, and when the plane approached Bodø extensive lightning activity developed quickly. The aircraft was struck by a very powerful lightning. The lightning struck the aircraft’s nose area and passed to the tail. Boundings between the fuselage and tail surface and a wire between the tail surface and the elevator were burned off. A powerful electric energy passed through the elevator rod in the tail section. A rod end came loose, resulting in a breach in the control rod. Thus the only connection between the control column in the cockpit and the elevator was lost. This aircraft type has electric pitch trim which adjusts the tail surface angle of attack and after a period the pilots regained limited control of the aircraft’s nose position by using this. When the lightning struck the aircraft, the pilots were blinded for approximately 30 seconds. They lost control of the aircraft for a period and the aircraft came very close to stalling. The pilots declared an emergency. The aircraft’s remaining systems were intact and the pilots succeeded in bringing the plane in for landing. During the first landing attempt the airspeed was somewhat high. The aircraft hit the ground in an approximate three-point position and bounced into the air. The pilots concluded that the landing was uncontrollable because the elevator was not working. The landing was aborted and the aircraft circled for a new attempt. Wind conditions were difficult and the next attempt was also unstable in terms of height and speed. At short final the aircraft nosed down and the pilots barely managed to flare a little before the aircraft hit the ground. The point of impact was a few metres before the runway and the aircraft slid onto the runway. Emergency services quickly arrived at the scene. The two pilots were seriously injured while both passengers suffered only minor physical injuries. No fuel leakage or fire occurred. The aircraft was written off.

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.

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.

Upon landing on Lake Ornes near Bodø, the single engine airplane went out of control and sank. There were no casualties.

Crashed in unknown circumstances on Grønnøya Island. There were no casualties while the aircraft was damaged beyond repair.

Crashed in unknown circumstances into the sea few hundred meters off Bodø. While all occupants were rescued, the aircraft sank and was lost.

The crew started the approach to Bodø Airport in limited visibility when the twin engine aircraft struck the slope of a mountain located on the Fugløya Island, some 32 km southwest of runway 07 threshold. The aircraft was destroyed and both crew members were killed. Controlled flight into terrain is suspected.

Upon landing onto the bay off Novika, the single engine overturned and came to rest near the shore. The pilot and all passengers evacuated safely while the aircraft was written off.

Crashed in unknown circumstances in the harbor of Bodø. There were no casualties.

While landing in the Svolvær Bay, the seaplane went out of control and plunged into the water before coming to rest. There were no casualties among the 12 occupants while the aircraft was damaged beyond repair.