Airport (less than 10 km from airport)

Upon landing at Lokichoggio Airport, the airplane banked right, causing the right propeller and the right wing to struck the runway surface. The aircraft slid for few dozen metres before coming to rest. There were no injuries while the aircraft was damaged beyond repair.

While taxiing to runway 23, the aircraft suffered a right landing gear failure and came to rest. There were no injuries and the aircraft was damaged beyond repair.

The pilot of the multi engine airplane, operated by a regional airline, was conducting a positioning flight in night instrument meteorological conditions. After takeoff, the airplane made a slight left turn before making a right turn that continued until radar contact was lost. The airplane reached a maximum altitude of 700 feet before impacting terrain about 3 miles northwest of the departure airport. Post accident examination of the wreckage did not reveal any preimpact failures. The weather reported at the airport, about the time of the accident, included a visibility of 5 statute miles in light rain and mist and an overcast ceiling at 400 feet. Analysis of the radar and weather data indicated that, with the flight accelerating and turning just after having entered clouds, the pilot likely experienced spatial disorientation.

During the takeoff roll from runway 25 at Quito-Mariscal Sucre Airport, the crew noted a fire alarm connected to the forward cargo compartment. The captain decided to abandon the takeoff procedure and initiated an emergency braking manoeuvre. Unable to stop within the remaining distance, the aircraft overran, collided with the ILS antenna, went down an embankment then impacted a brick wall and came to rest 300 metres past the runway end. All 66 occupants were rescued, among them eight passengers were injured. The aircraft was damaged beyond repair.

On September 19, 2008, about 2353 eastern daylight time, a Bombardier Learjet Model 60, N999LJ, owned by Inter Travel and Services, Inc., and operated by Global Exec Aviation, overran runway 11 during a rejected takeoff at Columbia Metropolitan Airport, Columbia, South Carolina. The captain, the first officer, and two passengers were killed; two other passengers were seriously injured. Both pilots and two passengers were killed while two others were seriously injured. Both passengers who were admitted in a local hospital for high burns were DJ AM & Travis Barker of the Rock band called "Blink". They were travelling back to California after they gave a concert in South Carolina.

On approach to Tbilisi Airport by night, the aircraft's speed was excessive while passing over the inner marker at a height of 204 feet. Upon landing, the aircraft hit the ground with a positive aerodynamic force estimated between 1,81 and 1,97 G. The aircraft bounced several times and eventually hit the ground with a positive aerodynamic force of 4,82 G. The nose gear collapsed and punctured the cockpit floor. Then the aircraft slid for few dozen metres before coming to rest. There were no injuries while the aircraft was damaged beyond repair.

According to radar and Global Positioning System data, the pilot overflew the airport from the southwest and turned to the west to maneuver into position for landing on runway 9. Several witnesses observed the airplane to the west of the airport at a low altitude, appearing to enter a turn that was followed by a "rapid descent" and impact with the ground. The ground scars and
damage to the airplane were consistent with a near-vertical descent and impact. An examination of the airplane and its systems revealed no preaccident anomalies. The moon was obscured by an overcast sky and dark night conditions were prevalent.

The pilot was completing a local post maintenance test flight at Cooinda Airport. Shortly after takeoff, while in initial climb, the engine failed. The pilot attempted an emergency landing in the bush but the aircraft collided with a telephone pole and came to rest. The pilot escaped with minor injuries and the aircraft was damaged beyond repair.

Damaged beyond repair following structural failure due to fatigue upon landing at Efogi, PNG. There were no injuries but the aircraft was damaged beyond repair and dismantled.

Just after the airplane's landing gear was retracted during takeoff for a retardant drop mission, a ball of fire was observed coming out of the left jet engine before the airplane rolled steeply to the left and descended into the terrain. Prior to takeoff, the captain said he would make the takeoff and provided a takeoff briefing concerning the runway to be used and his intentions should an emergency develop. Shortly thereafter, the captain informed the co-pilot that this would actually be his (the co-pilot's) takeoff. On the cockpit voice recorder, the co-pilot stated "Same briefing (sound of laughter)". The co-pilot did not give an additional takeoff briefing beyond the one given by the captain and the captain did not ask the co-pilot to give one. During the initial climb, the captain said he detected a fire on the left side of the airplane and the copilot responded that he was holding full right aileron. At no point did either pilot call for the jettisoning of the retardant load as required by company standard operating procedures, or verbally enunciate the jet engine fire emergency checklist. Recorded data showed that the airplane's airspeed then decayed below the minimum air control speed, which resulted in an increased roll rate to the left and impact with terrain. The 11th stage compressor disc of the left jet engine failed in fatigue, which caused a catastrophic failure of the compressor section and the initiation of the engine fire. Metallurgical examination of the fracture identified several origin points at scratches in the surface finish of the disk. The scratches were too small to have been observed with the approved inspection procedures used by the company. A review of the FAA sanctioned Approved Aircraft Inspection Program, revealed no shortcomings or anomalies in the performance or documentation of the program. A post-accident examination of the airframe and three remaining engines revealed no anomalies that would have precluded normal operations.