Landing (descent or approach)

After takeoff from Treviso-Istrana Airbase, the crew informed ATC about technical problems and was cleared to divert to Venice-Tessera Airport for an emergency landing. On final, the aircraft went out of control and crashed few hundred metres short of runway. All three crew members were killed.

Following an uneventful flight from Frankfurt, the crew started the descent to Warsaw-Okecie Airport in poor weather conditions with thunderstorm activity, wind shear, rain falls and CB's. After being cleared to land on runway 11, the wind component changed during the last seconds. The right main gear touched down 770 metres past the runway threshold (aircraft's speed was 170 knots). The left main gear touched down 9 seconds later, 1,525 metres past the runway threshold. On a wet runway, the crew started the braking procedure and activated the thrust reversers and spoilers but the remaining distance was insufficient. At a speed of 72 knots, the aircraft overran, went down an embankment, lost its left engine and came to rest 90 metres further, bursting into flames. A female passenger and the captain were killed while all other occupants were rescued, among them 51 were seriously injured. The aircraft was destroyed by a post crash fire.

On approach, the aircraft was too low and struck the ground short of runway. Upon impact, the undercarriage were torn off and the aircraft came to rest on its belly. All six occupants escaped uninjured and the aircraft was written off.

Cessna 208 Caravan aircraft VT-AAN operated by Andaman and Nicobar Administration was engaged in a flight from Port Blair - Dugong Creek - Hut Bay - Port Blair. There were four persons on board the aircraft including pilot-in-command. The flight from Dugong Creek to Hut Bay was uneventful. The aircraft took-off from Hut Bay for Port Blair where it was intended to land on sea
adjacent to Viper Island. Soon after touchdown on seawater, the aircraft flipped over its nose and sank thereafter. Three persons including the pilot evacuated the aircraft. However, one person died due to drowning, as he remained strapped in his seat. The aircraft sustained substantial damage. There was no fire.

During an approach to land, the pilot made S-turns to allow for proper spacing from a preceding airplane. On short final, he decided to go around because the runway was still not clear. However, he reported there was a lack of response concerning the power, so he decided to land as originally planned. The pilot tried to align the airplane with the runway centerline, but its right wing and landing gear struck the ground, and the right landing gear collapsed. The airplane skidded off the right side of the runway. During the accident sequence, the outward portion of the right wing was torn away from the airplane and a fuel line was ruptured. A ground fire erupted and burned through the right side of the airplane's structure and right wing. No preimpact part failure or malfunction was reported.

Twenty minutes after takeoff from San Juan-Luis Muñoz Marin Airport, while in cruising altitude, a steward noticed smoke in the lavatory and informed the crew accordingly. In the meantime, the crew noticed a fire alarm in the cockpit, declared an emergency and became number one for landing at Santo Domingo-Las Américas Airport. Following a normal approach and landing, the crew vacated the runway and parked the aircraft at gate A6. While the passengers was disemmarking, smoke spread in the cabin and fire erupted, destroying the airplane.

After landing at Buenos Aires-Aeroparque-Jorge Newbury Airport, the crew started the braking procedure and activated the reverse thrust that failed to deploy. The crew used the emergency brakes but the aircraft failed to stop within the remaining distance, overran and collided with a support vehicle (pick up) that was parked outside the safety zone. The aircraft lost its undercarriage and both wings and all four occupants were injured.

The approach to Tijuana-General Abelardo L. Rodríguez Airport was completed in poor weather conditions with clouds down to 180 metres. On short final, the captain realized his position was not correct and made several correction but inefficiently. The aircraft landed hard, right main gear first. On impact, both tires on the right main gear burst. The aircraft went out of control, veered to right and came to rest. All six occupants escaped uninjured while the aircraft was damaged beyond repair.

The aircraft was completing a cargo flight from San Felipe, Guainía, to Villavicencio, carrying three passengers, three crew members and a load of straw. En route, one of the engine failed and the crew decided to divert to Barranco Minas Airport. After touchdown on runway 27, the aircraft was unable to stop within the remaining distance, overran and plunged in the Río Guaviare. Four people were rescued while the bodies of the copilot and the flight engineer disappeared in the river.

The pilot reported the right engine failed, followed by the left engine approximately one minute later while he was in cruise at 25,000 feet. He said he initiated a steep descent to get below 18,000 feet, and attempts at restarting the left engine were unsuccessful. The pilot landed 500 feet down a 1,900 feet long runway and ran off the departure end, 300 feet, into a wooded area. Post accident investigation found 130 gallons of fuel onboard in the main tanks. The fuel was tested and found to be free of water. The fuel lines were free of obstructions and the fuel pumps worked. A failed torque sensor was found on the left engine which would disconnect the left engine driven fuel pump. The right engine was test run satisfactorily.