De Havilland DHC-6 Twin Otter

Few minutes after takeoff from Loja Airport, while climbing in poor weather conditions, the twin engine aircraft struck the slope of a mountain and crashed. All 14 occupants were killed. The aircraft had a dual registration: civil HC-BCG and military FAE446.

The Twin Otter departed Goose Bay on a medical evacuation flight to St. Anthony. The flight was uneventful and landed in St. Anthony at 15:24. At 16:02, the aircraft departed St. Anthony on a VFR flight back to Goose Bay. On board were the two pilots and the doctor and nurse. Approaching the Goose Bay Airport, weather became marginal, but the crew continued visual flight. The crew likely encountered near zero forward visibility in snow showers and fog; it is probable that they were able to maintain vertical contact with the ground and were confident they could continue flight with visual reference to the ground. The crew may not have been able to see terrain ahead and therefore may not have been able to determine if the aircraft would clear the hills, particularly, when steep hills were encountered. The plane struck a rock outcropping 100 feet below the summit of a 2,050-foot mountain. After bouncing twice, the Twin Otter had come to rest in a small, wooded gully, approximately 350 feet from the initial point of impact.

The aircraft departed Fort Norman at 16:51 and arrived overhead Fort Franklin at approximately 17:15. Because Fort Franklin was shrouded in fog, a local resident contacted the pilot on a portable VHF transceiver and advised him that there was little or no visibility. The pilot replied that he did not think he would be able to land. The resident drove to the airstrip and contacted the pilot again when he heard the aircraft returning. He advised the pilot that visibility was 200-300 feet. The pilot then asked if this was the vertical or horizontal visibility. At that moment the Twin Otter struck a 200-foot-high telecommunications tower while in controlled level fight. Part of the right wing broke off and the aircraft slowly rolled over before striking the ground. The decision of the pilot to continue the approach in foggy weather were possibly influenced by the effects of stress and a greater than usual personal need to complete the flight. The stress was probably caused by the fact that the pilot had been involved in four accidents since March 1984. Although he was a very experienced pilot, his previous employer terminated his employment on 31 August 1984. In their opinion, his ability to make operational decisions was in question. The pilot was hired by Nahanni Air Services one month later.

The aircraft crash landed after the pilot used flaps and power to semi control pitch after the elevator down control cable failed at about 300 feet agl on final approach. The left wing of the aircraft hit the terminal roof during the stall mush from 50 feet agl. The company is changing their aircraft control cables from steel to stainless steel to aid in the anti-corrosion and modifying their inspection period from 800 to 100 hours between inspections. The cable that separated failed from corrosion. No evidence of fatigue cracking or mechanical wear was found. Corrosion products were found within 2 inches of the serapation on both cable pieces.

Shortly after takeoff, while in initial climb, one of the engine failed. The crew reduced his altitude and completed an emergency landing past the runway end. There were no casualties while the aircraft was damaged beyond repair.

On approach to Córdoba-Pajas Blancas Airport, the crew encountered marginal weather conditions and was forced to initiate a go-around. During a second attempt to land, the aircraft was too low and crashed in a maize field, few km short of runway 18 threshold. All 15 occupants were rescued and the aircraft was damaged beyond repair.

On approach to Paulatuk Airport, the pilot encountered marginal weather conditions with strong cross winds and blowing snow. On short final, while making a transition from visual to instruments flight rules, the pilot decided to initiate a go-around when the left wing struck the ground. Out of control, the aircraft veered to the left and came to rest. The pilot and a passenger were killed while 10 other occupants were injured.

Crashed in unknown circumstances. Occupant fate unknown.

The Twin Otter was completing a schedule service from Sandy Lake to Thunder Bay with an intermediate stop in Landsdowne House, carrying five passengers and two pilots. On approach, the crew encountered marginal weather conditions and the captain decided to initiate a go-around procedure. A second circuit was completed without losing sight of the airfield. During the second attempt to land, the pilot-in-command reported 'runway in sight' and the copilot called for radioaltimer at 200 feet altitude. On short final, the captain reported he was encountering whiteout conditions when the airplane struck the snow-covered and icy surface of the lake about 1,200 feet short of runway threshold. Upon impact, the nose gear was torn off then the aircraft struck rocky terrain and eventually came to rest in flames about 600 feet short of runway. A passenger was seriously injured while both pilots escaped with minor injuries. Four passengers were killed in the accident.

After takeoff from Lonkin Airport, while in initial climb, the crew initiated a turn to the left when the left engine failed. The airplane lost height, struck trees and crashed few hundred meters from the runway end. Five passengers were seriously injured while nine other occupants were killed.