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Thai Airways 261

105 ItzaePlanes  2 months ago
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Auto Credit Based on GalacticaAsia's A310-300[GE]

Thai Airways International flight 261, an Airbus A310, stalled and crashed while on approach to Surat Thani Airport, Thailand , killing 101 occupants; 45 survived the accident.Flight TG261 left Bangkok-Don Muang International Airport, Thailand at 17:54 hours local time for a domestic flight to Surat Thani.At 18:26 hours, the co-pilot first established contact with the Surat Thani approach controller while the aircraft was 70 nautical miles away from Surat Thani Airport. The controller radioed that the crew could expect a VOR/DME instrument approach to runway 22. At that time surface wind was calm with a visibility of 1500 meters, light rain and a cloud base of 1800 feet.At 18:39 hours the co-pilot contacted Surat Thani aerodrome controller and reported over the Intermediate Fix (IF). The controller informed him that the precision approach path indicators (PAPI) on the right side of runway 22 were unserviceable while the left lights were in use.At 18:41 hours, the co-pilot reported passing final approach fix (FAF). The controller informed the pilot that the aircraft was not in sight but it was cleared to land on runway 22. The surface wind was blowing from 310 degrees at a velocity of 5 knots so the pilots should be careful or the slippery runway.At 18:42 hours, the co-pilot reported that the runway was in sight and later on the controller also had the aircraft in sight. The pilot decided to go-around. The controller asked the pilot about the distance where the runway could be seen. The co-pilot reported that it could be seen at 3 nautical miles and requested for the second approach. The controller requested to report over FAF . When the co-pilot reported that the flight was over the FAF again, the controller cleared the flight to land although he again could not see the runway.When the flight crew failed to observe the runway lights, the captain decided to go around again.Again the controller instructed the flight to report over the FAF and reported that visibility

General Characteristics

  • Predecessor A310-300[GE]
  • Created On Android
  • Wingspan 144.0ft (43.9m)
  • Length 153.1ft (46.7m)
  • Height 53.9ft (16.4m)
  • Empty Weight N/A
  • Loaded Weight 89,132lbs (40,430kg)

Performance

  • Power/Weight Ratio 1.284
  • Horse Power/Weight Ratio 0.033
  • Wing Loading 26.9lbs/ft2 (131.4kg/m2)
  • Wing Area 3,311.1ft2 (307.6m2)
  • Drag Points 13388

Parts

  • Number of Parts 504
  • Control Surfaces 9
  • Performance Cost 3,160