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Advance Airlines Flight 4210 : ウィキペディア英語版 | Advance Airlines Flight 4210
Advance Airlines Flight DR4210 was a scheduled passenger flight which crashed at Sydney Airport on 21 February 1980, killing all 13 people on board the Beech Beechcraft King Air 200. After taking off on runway 25 for a scheduled flight the aircraft's left (port) engine failed and the pilot requested an emergency landing on runway 34. The plane crashed into the sea wall while attempting the emergency landing. The accident caused the greatest number of fatalities in a civil aircraft crash in Australia since MacRobertson Miller Airlines Flight 1750, a Vickers Viscount that crashed near Port Hedland in Western Australia on 31 December 1968 killing all 26 on board.〔(【引用サイトリンク】title=Ten Worst Air Crashes in Australia since 1968 )〕 ==Accident== King Air VH-AAV was operating as Advance Airlines flight DR4210 to Temora and Condobolin, New South Wales with a single pilot and 12 passengers on board. The aircraft commenced takeoff on runway 25 at 1908 hours and, after climbing to a height of no more than , the aircraft was observed to level off and enter a shallow bank to the left. The pilot contacted the control tower advising he had suffered failure of the left engine and requesting an immediate return to land on runway 34. Air Traffic Control acknowledged this request and cleared the King Air to make a visual approach to the runway behind an Ansett Airlines Boeing 727 on final approach. As VH-AAV continued to turn towards the runway, it descended to just a few feet above the water on a heading towards a sea wall enclosing the runway which stretches into Botany Bay. This manoeuvre prompted the tower controller to enquire if the approach and landing would proceed as normal. The reply from the pilot eight seconds later was "Alpha Alpha Victor negative". This was the final transmission from the aircraft. At 1909:08, the Sydney Airport crash alarm system was activated, and the preceding Ansett 727 was instructed to expedite its landing roll and vacate the runway. At 1909:20 VH-AAV was cleared to land but this clearance was not acknowledged. At 1909:22 the aircraft impacted the sea wall above the waterline. The total duration of the flight was 106 seconds from brakes release to impact. Five fire fighting appliances were dispatched to the accident site and crews extinguished the fire within 10 minutes of the crash. The initial impact caused the left wing to disintegrate while a section of the right wing, including its engine, separated from the aircraft and came to rest adjacent to the runway. The fuselage was engulfed in an explosion caused by fuel igniting as the wing structures separated. The main wreckage bounced over the sea wall and landed inverted on a taxiway, sliding along the ground for a distance of approximately . All 13 aboard the aircraft were killed in the accident which was ruled to be non-survivable.〔(【引用サイトリンク】title=Aircraft Accident Investigation – Beech 200 VH-AAV Sydney (Kingsford Smith) Airport 21 February 1980 )〕
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