Thai Airways International Flight 601

22°18′07″N 114°13′02″E / 22.3020°N 114.2173°E / 22.3020; 114.2173AircraftAircraft typeSud Aviation Caravelle IIIAircraft nameChiraprapaOperatorThai Airways InternationalRegistrationHS-TGIFlight originHaneda Airport, Japan1st stopoverSongshan Airport, TaiwanLast stopoverKai Tak Airport, Hong KongDestinationDon Mueang Airport, ThailandOccupants80Passengers73Crew7Fatalities24Injuries56Survivors56

Thai Airways International Flight 601 was a Sud Aviation Caravelle that crashed into the sea on landing at the former Kai Tak Airport, Hong Kong, in a typhoon on Friday, 30 June 1967.

Aircraft

The aircraft involved was a Sud Aviation SE-210 Caravelle III, MSN 25, registered as HS-TGI, which was manufactured by Sud Aviation in 1960. The aircraft had logged approximately 17350 airframe hours and was equipped with two Rolls-Royce Avon 527 engines.^[1][2]

Accident

Thai Airways International Flight 601 took off from Taipei Songshan Airport on an hour-long flight to Kai Tak Airport. The Sud Aviation Caravelle had 80 people aboard: 73 passengers and 7 crew. With the plane on ILS approach to runway 31 at Kai Tak, Captain Viggo Thorsen (age 43) and Co-pilot Sanit Khemanand (aged 50) became occupied trying to make visual contact with the ground, and failed to notice that the aircraft had descended below the decision height of 415 feet (126 m). The crew made an abrupt heading change (while already 80 feet (24 m) below the glide slope), and then entered a high-speed descent. The aircraft undershot runway 31 and crashed into the sea, killing 24 passengers.

Probable cause

The probable cause of the accident was pilot error, specifically not noticing that the aircraft had descended below the glide slope. The presence of strong wind shear and downdrafts as a result of then-present Typhoon Anita was a probable contributing factor. However, at the time of the accident there were no means of detecting such weather phenomena. Further factors included:

• The pilots did not adhere to Thai Airways procedure for a captain-monitored Instrument approach in bad visibility.
• The captain did not monitor the approach adequately.
• The abrupt heading change after the aircraft descended below minimum altitude may have exacerbated the high rate of descent.
• Downdrafts and wind shear may have contributed to the height loss which resulted from this mishandling.

References

• Accident description for HS-TGI at the Aviation Safety Network. Retrieved on 12 July 2013.
• [1] ^{[dead link]}