Swearingen SA226 Metro II

The aircraft was on a flight from Winnipeg, Manitoba, to Norway House, Manitoba, with two crew members and seven passengers on board. After touchdown on Runway 05, when propeller reverse was selected, the aircraft veered to the left. The crew attempted to regain directional control; however, the aircraft departed the left side of the runway surface, entered an area of loose snow, traversed a shallow ditch, climbed a rocky embankment, and came to rest on its belly with all three landing gears collapsed. The crew and passengers exited the aircraft through the main door stairway and the over-wing exits. There were no reported injuries. The accident occurred during daylight hours at 0834 central standard time.

While in cruise flight at 16,000 feet, the pilot requested from ATC and was cleared to make a 360-degree turn to the left. Shortly after this, the pilot requested a 360-degree turn to the right. The pilot then requested radar vectors to the closest airport and was given this. ATC asked the pilot if he had an emergency and the pilot reported he had an asymmetric fuel condition. The pilot then asked for a lower altitude and was cleared by ATC to 4,000 feet. About a minute later the pilot transmitted "Mayday" six times and shortly after this radar and radio contact with the flight was lost. Recorded radar data showed that at 1803:13 the accident airplane was proceeding on a southerly heading at 16,100 feet mean sea level (MSL). At 1803:53 the airplane turned left to a southeasterly heading. At 1804:13 the airplane turned right returning to its original southerly heading. At 1805:14 the accident airplane turned to the right on a southwesterly heading, and maintained that heading until 1809:04 at which time the airplane turned due west and was at an altitude of 15,400 feet. The last radar contact was at 1810:06 at an altitude of 13,800 feet. The airplane wreckage was located due north from this last recorded radar contact. Witnesses observed the airplane descend in a near vertical attitude, collide with the ground, and then explode. Components from all areas of the aircraft structure and flight control surfaces were located at the crash site along with components from both engines and propellers. Impact and post crash fire damage precluded the examination of the airplanes fuel system and components.

erimeter Aviation flight 914, a Metro II with 17 people on board, was on approach at Thompson, MB. The first officer flew the aircraft during the approach, and encountered turbulence and fluctuating airspeed. The captain took control at 200 feet agl. The aircraft was high and left of centreline. The captain added power, continued the approach and landed hard on runway 23 near the intersection with runway 32. After the aircraft arrived at the apron, a fuel leak was noted. The aircraft was inspected and damage was found in the wheel wells, wing leading edge, engine mounts and a wing-fuselage attachment point. No injuries were reported. Reported winds at 1400Z were 010 at 15-20 kts; 1500Z winds were 350 at 9 kts.

The crew was completing a positioning flight from Reus to Barcelona for maintenance purposes. During take off roll on runway 07, at a speed of 80 knots, the nose gear collapsed. The aircraft slid on its nose for few dozen metres before coming to rest on the runway. Both pilots escaped uninjured while the aircraft was damaged beyond repair.

The accident involved 2 Swearingen airplanes. The pilot of the first airplane reported that he had taxied north for departure. There were several company aircraft in front of him in line for departure so he came to a complete stop. The pilot of the second airplane reported that he was also taxiing north for departure. He had seen the lights from an aircraft holding short of runway 17R; however, he did not see the lights of the first airplane until it was too late. The pilot of the second airplane reported he applied full brakes and used reverse thrust but was unable to avoid hitting the first airplane. Both airplanes were substantially damaged.

According to the pilot, he was told to enter left base and was cleared to land. The pilot stated that, when he reduced the airspeed to lower the landing gear, he "heard the gear come down," and he verified "three green in the [landing] gear indicator." He landed the airplane on its "main [landing gear] wheels first" and slowly let the nose of the airplane drop. Although both main landing gear assemblies remained down and locked, the nose landing gear collapsed, allowing the nose of the airplane and both propellers to strike the runway. The airplane slid approximately 3,000 feet, coming to a stop on the right edge of the runway. Several fractured propeller pieces impacted the left and right sides of the fuselage substantially damaging two fuselage station bulkheads. The fuselage bulkhead, forward of the nose landing gear well, was also substantially damaged due to contact with the runway. The pilot said that, during the approach, from base to final, he did not hear a landing gear warning horn. An air traffic control specialist, stated that he told the pilot to enter a left base and that he was cleared to land. The specialist stated that he observed the airplane roll out on a 2-mile final "with the gear down." As the airplane was rolling down the runway the "nose wheel collapsed." An FAA inspector examined the airplane and noted that, according to the Fairchild SA226 Maintenance Manual, the nose landing gear's up-lock mechanism was not properly lubricated, a "critical clearance" measurement between the nose landing gear's bell crank roller and positioning cam was found to be out of tolerance, and when the throttles were retarded, the landing gear warning horn activated, but it was "barely audible." According to the Fairchild SA226 Maintenance Manual, the landing gear should be lubed every 200 hours. The FAA inspector stated that the approved maintenance inspection sheet for the operator, did not show the requirement for the main landing gear or nose landing gear to be lubed every 200 hours.

The twin engine aircraft departed Nairobi-Wilson Airport at 1558LT on a charter flight to Samburu, carrying 12 passengers (all US citizens) and two pilots. En route, the crew decided to make a tour over the Mt Kenya before continuing to Samburu. While cruising at an altitude of 16,500 feet in clouds, the aircraft struck the eastern slope of Mt Point Lenana (third highest peak of Mt Kenya). The wreckage was found 450 feet below the summit and all 14 occupants were killed.

The flight was following a heavy jet on landing approach. The crew agreed to fly the approach at a slightly higher altitude than normal to avoid any possible wake turbulence. The first officer, who was flying the airplane, called for the landing gear to be lowered. When the captain placed the gear handle in the DOWN position, he noted red IN-TRANSIT lights. He recycled the landing gear, but got the same result. He consulted the emergency checklist and thought he had manually extended the landing gear because he "heard the normal 'clunk feel' and airspeed started to decay." In addition, when power was reduced to FLIGHT IDLE, the GEAR UNSAFE warning horn did not sound. The first officer agreed, noting 2,000 pounds of hydraulic pressure. The airplane landed wheels up. Propeller blade fragments penetrated the fuselage, breaching the pressure vessel. Postaccident examination revealed the nose gear had been partially extended but the main landing gear was retracted. The crew said the GEAR UNSAFE indication had been a recurring problem with the airplane. The problem had previously been attributed to a frozen squat switch in the wheel well.