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Svi udesi aviona Airbus Ovo je kompilacija svih zvanično registrovanih udesa aviona Airbus tokom poslednje dve decenije, zaključno sa, u ovom trenutku najnovijom, katastrofom "AA" Airbusa A300B4-605R, koja se dogodila 12. novembra 2001, neposredno nakon poletanja aviona za Santo Domingo sa njujorškog aerodroma JFK. Kompilacija udesa aviona tipa Airbus sačinjena je zahvaljujući bogatoj i ažurnoj bazi podataka i priloga na poznatom sajtu AirDisaster.Com.
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Avion pun putnika (mahom novinara i poslovnih partnera kompanije) srušio se dok je pred gledaocima demonstrirao niski prelet. Nakon što je prošao pistu, sa nepromenjenim režimom rada motora uleteo je u mladu šumu na obodu aerodroma, srušio se i zapalio. Službeno je optužena posada, ali postoji dokaz da je neispravan kompjuter onemogućio pilotima da dodaju snagu sve dok nije postalo prekasno. Putnika/poginulih: 136/3
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nema
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Avion je greškom oborila raketa ispaljena sa američkog razarača "USS Vincennes". Američki vojnici su poverovali da je u pitanju avion koji želi da ih napadne. Putnika/poginulih: 290/290
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Avion se tokom prilaza srušio nedaleko od piste. Posada je dozvolila da brzina aviona padne do kritične, na kojoj je nastupio stall. Naime, kopilotov flight director ostao je u open descent idle modu, umesto u vertical speed modu, propisanom za prilaženje i sletanje, tako da avion nije bio u stanju da zadrži korektnu putanju poniranja sa oduzetom snagom motora. Pilotska greška. Putnika/poginulih: 146/92
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nema
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Dok je prilazio aerodromu u Strazburu, avion je udario u planinsku ivicu. Utvrdjeno je da je udes izazvala pogrešna upotreba preklopnika za selekciju moda poniranja. Posada je omaškom selektovala rejt od 3.300 stopa u minuti umesto ugao od 3.3 stepena za putanju poniranja. Putnika/poginulih: 96/87
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After experiencing a flap problem while attempting to extend the flaps fully on a seven mile final, the crew requested a missed approach and it was approved. The radar at Kathmandu was inoperative due to maintenance work, and the aircraft turned toward the south toward rising terrain. The Captain ignored the ground proximity warning system thinking it was a false alarm. Crew error in not following the published missed approach procedure. Putnika/poginulih: 113/113
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The aircraft crashed on approach to Kathmandu in poor weather conditions. The crew failed to follow the proper approach course, which resulted in the collision with terrain. Crew desorientation. Putnika/poginulih: 167/167
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The aircraft skidded off the end of the runway during landing. The aircraft touched down with sink rate low enough that the onboard flight computers did not consider it to be "landing," which inhibited thrust reverse and brake application for nine seconds. The aircraft touched down soft enough that the flight computers did not recognize that the aircraft had landed, resulting in a delay in activation of thrust reverers and brakes. Putnika/poginulih: 70/2
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After the completion of an A-check the aircraft was pulled from the maintenance hangar to the terminal at Paris-Charles de Gaulle Airport. At that moment a fire broke out. The airport fire services were not able prevent the aircraft from being damaged beyond repair by the fire. PROBABLE CAUSE: Overheat and fire of the yellow hydraulic electric pump operating the aircraft cargo doors on ground with the engines off. Putnika/poginulih: 0/0
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nema
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The aircraft crashed after entering a zero G spin. The Captain was allowing his 15-year-old son to fly the airplane when the boy applied full deflection to the yoke, causing the autopilot to disengage and the aircraft to roll nearly 90°. The First Officer then pulled back on his yoke to attempt recovery, but the aircraft stalled and entered a spin from which recovery was not possible. Putnika/poginulih: 75/75
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The aircraft was on an ILS approach to land at Nagoya when the First Officer accidently pressed the TOGA (take-off go around) button located on the forward edge of the throttles. The F/O then attempted to correct the situation by disconnecting the auto-throttle and taking over speed control manually. The TOGA switch, however, also commands a pitch up attitude for a go-around, and as the crew pushed the yoke the autopilot trimmed the aircraft up to the maximum allowable. The aircraft stalled due to the severe nose high attitude and crashed. Crew error in not disconnecting the autopilot and manually landing the airplane. Putnika/poginulih: 271/264
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nema
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The aircraft crashed during a flight test in which the crew was simulating an engine failure on takeoff. Pilor error, misunderstanding of auto-flight systems. Putnika/poginulih: 7/7
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nema
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The aircraft overran the runway and caught fire after landing in a thunderstorm. Disagreement between the Captain and First Officer during the last seconds of the approach on whether to abandon the landing contributed to the delay in stopping the aircraft. Putnika/poginulih: 160/0
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nema
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The aircraft crashed shortly after takeoff due a malfunction in the auto-throttle system which led to an assymetric thrust situation and a loss of control. Putnika/poginulih: 60/60
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nema
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A flight control failure at V1 caused the crew to abandon the takeoff, with deceleration beginning at V1+8 knots. The aircraft overran the runway, causing the nosegear to collapse. The flight control problem was traced to a faulty microchip in the aircraft's Fly-By-Wire system. Putnika/poginulih: 115/0
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nema
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The aircraft crashed into terrain while on approach to Medan. Air Traffic Control mistakenly gave the crew a vector into high terrain. Putnika/poginulih: 234/234
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nema
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The aircraft crashed during a go-around attempt. The aircraft pitched up to 40° until a loss of airspeed caused a stall. Pilot error. Putnika/poginulih: 196/196
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The aircraft overran runway 4 while landing. A malfunction of the onboard flight computers prevented power from being reduced to idle, which inhibited thrust reverse and spoilers from being used. The offending engine was shut down, and brakes applied, but the aircraft was unable to stop before the end of the runway. Putnika/poginulih: 127/0
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The aircraft crashed while attempting its third non-precision approach to Surat Thani. The ILS was out of service for maintenance, which necessitated the use of the less accurate VOR approach by the crew. Crew fatigue having completed two previous approaches unsuccessfully. Putnika/poginulih: 146/101
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nema
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The aircraft crashed into the Atlantic Ocean shortly after takeoff from Abidjan. Numerous eyewitnesses who saw the airplane takeoff reported that it failed to gain altitude and struck the water around a mile from the runway. 10 survivors were pulled from the water by rescue boats. No cause has been determined. Putnika/poginulih: 179/169
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nema
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The aircraft was being towed across the airfield with a TUG when a C-130 on its takeoff roll collided with the Airbus. All eight crew members of the Hercules died in the collision in which both planes caught fire on the tarmac, and a worker towing the Airbus to a hangar for repairs was injured. Putnika/poginulih: 0/0, plus 8
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During taxi for takeoff, the aircraft's left landing gear collapsed, allowing the engine to strike the taxiway. A fuel line was ruptured, leading to an engine fire which spread to the wing, causing substantial damage. The aircraft was written off. Putnika/poginulih: 186/0
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Shortly after the aircraft departed Chania, Greece bound for Hanover, Germany, the flight crew realized that the landing gear could not be retracted. The decision was made to continue the flight to Hanover at a lower altitude and airspeed with the landing gear extended. As the aircraft neared the mid-point of its journey, the crew realized that the remaining fuel would be insufficient to continue the flight to Hanover, so a landing was planning at Vienna, Austria. As the aircraft descended through 10,000 feet, the left engine failed due to fuel exhaustion. By utilizing crossfeed fuel pumps, the crew was able to keep the right engine running, but was unable to restart the left. As the aircraft turned a six mile final, the right engine also failed due to fuel exhaustion. The plane touched down 600 feet short of runway 34, collapsing the main landing gear, and seriously damaging the left wing and engine. Putnika/poginulih: 150/0
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The aircraft was conducting a normal approach to Runway 12 at Bahrain International Airport. Approximately 1nm from touchdown and at about 600 feet above mean sea level the aircraft commenced a go-around. During the go-around the aircraft impacted the sea about 1nm north of the airport. Preliminary: The Captain reported that the aircraft was unable to slow on final approach, and a go around was executed. While attempting to return to land, the crew lost control of the aircraft, which crashed into shallow water several miles off the end of the runway. Putnika/poginulih: 143/143
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The aircraft was on a flight from Toronto, Ontario, Canada to Lisbon Portugal when a problem developed with the fuel system approximately 300nm northeast of Terciera Island, Azores Islands, Portugal. The crew elected to divert to Terciera Island for an emergency landing. The Captain reported that approximately 100nm from the airport, the left engine failed, and some ten minutes later, the right engine failed as well. The aircraft, using a minimal amount of hydraulic and electrical power supplied from its Ram Air Turbine, continued gliding toward Terciera Island in a gradual descent. The Captain reported that the flight arrived over Terciera Island at FL150 (15,000 feet), at dawn, and so he elected to make a visual approach to the airport with no engine power. The total flying time without engine power was in the neighborhood of 17 to 18 minutes. The aircraft sustained minor damage during the landing, including damage to the landing gear as twelve tires exploded upon touchdown. Initial reports indicate that a fuel line that had been replaced several days before became severed, leading to a fuel leak of approximately 37,000 gallons over the Atlantic Ocean. Putnika/poginulih: 298/0
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American Airlines Flight 587 departed Runway 31R at John F. Kennedy Airport in New York at 9:13am local time on a flight to Santo Domingo, Dominican Republic. Approximately four minutes later, while climbing through 2,700 feet, radar contact was lost with the aircraft. Witnesses reported seeing an engine fire develop on the aircraft's no.1 engine, followed by small pieces of debris breaking away from the left wing, and shortly afterward, a complete separation of the left engine from the aircraft's wing. The aircraft then reportedly entered a steep nose-down attitude and crashed into the borough of Queens near Rockaway Beach, destroying four residential structures, and severely damaging eight others. Putnika/poginulih: 260/260
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