Hong Kong - Bangkok - Vienna

On May 26, 1991 at 11:17 PM, Hong Kong - Bangkok - Vienna experienced a crash involving Boeing 767-300, operated by Lauda Air, with the event recorded near Phu Toey Suphan Buri (<U+0E2A><U+0E38><U+0E1E><U+0E23><U+0E23><U+0E13><U+0E1A><U+0E38><U+0E23><U+0E35>).

The flight was categorized as scheduled revenue flight and the reported phase was flight at a plain, valley crash site.

223 people were known to be on board, 223 fatalities were recorded, 0 survivors were identified or estimated. This corresponds to an estimated fatality rate of 100.0%.

Crew on board: 10, crew fatalities: 10, passengers on board: 213, passenger fatalities: 213, other fatalities: 0.

The listed crash cause is technical failure. Lauda Air Flight 004 (NG004) was a scheduled passenger flight from Hong Kong to Vienna, Austria with an en route stop in Bangkok, Thailand. The flight departed Bangkok at 1602 hours on May 26, 1991 for the final flight sector to Vienna Austria. All pre-flight, ground, and flight operations appear routine until five minutes and forty five seconds after the cockpit voice recorder (CVR) recorded the sounds of engine power being advanced for takeoff. At this point a discussion ensued between the crew members regarding an event later identified as a crew alert associated with a thrust reverser isolation valve. The crew discussed this alert for some four and one half minutes. The Quick Reference Handbook (QRH) was consulted to determine appropriate crew actions in response to the alert. No actions were required, and none were identified as being taken. Ten minutes and twenty seconds into the flight the co-pilot advised the pilot-in-command of the need for rudder trim to the left. The pilot-in-command acknowledged the co-pilot's statement. Fifteen minutes and one second into the flight, the co-pilot stated "ah reverser's deployed." Sounds similar to airframe shuddering were then heard on the CVR. Twenty nine seconds later the CVR recording ended with multiple sounds thought to be structural breakup. Flight conditions were recovered from non-volatile memory in the left engine electronic engine control (EEC). At the suspected point of reverser deployment, the EEC readout indicated that the airplane was at an approximate altitude of 24,700 feet, a speed of Mach 0.78, and developing climb power. The airplane crashed in mountainous jungle terrain at 14 degrees 44 minutes North latitude and 99 degrees 27 minutes East longitude at approximately 1617 hours. Night time visual meteorological conditions prevailed. All 223 occupants were killed.

Aircraft reference details include registration OE-LAV, MSN 24628, year of manufacture 1989.