Lauda flight 
                                      004, service from Bangkok to Vienna, 
                                      departed Don Muang International Airport 
                                      at 11:02pm the night of May 26, 1991. 
                                      Along with Captain Tom Welsh and First 
                                      Officer Josef Thurner, eight cabin 
                                      attendants and 213 passengers were on 
                                      board the Boeing 767 that night. 004 
                                      climbed out normally from Bangkok, cleared 
                                      to FL310. After being handed off to 
                                      Bangkok Control, Thurner called the Lauda 
                                      Air company base, reporting it's estimated 
                                      arrival time in Vienna. 
                                      This would be 004's 
                                      last transmission. Some twelve minutes 
                                      later, while climbing through FL240, 004's 
                                      target disappeared from Bangkok Control's 
                                      radar screen. Further radio calls from 
                                      Bangkok went unanswered. Shortly 
                                      afterwards, Thailand's Department of 
                                      Aviation's Rescue Co-ordination Centre 
                                      received a call from from a remote police 
                                      outpost reporting that people from a 
                                      mountain village had reported hearing and 
                                      seeing an aircraft explode in the air and 
                                      fall into the jungle. The aircraft was 
                                      less than two years old at the time and 
                                      there was not forecast severe weather in 
                                      the area. Clearly, whatever had caused the 
                                      accident had struck swiftly, the crew 
                                      having no time to report and signs of 
                                      trouble.
                                      
                                      ......Investigators were unable to reach 
                                      the wreckage until the following morning 
                                      and it became immediately apparent that 
                                      there had been a catastrophic in-flight 
                                      failure. No impact crater was found and 
                                      aircraft wreckage and bodies strewn at 
                                      random across the jungle mountain slopes. 
                                      Eyewitness reports of fire or explosion 
                                      were substantiated by evidence of fire 
                                      damage in the wreckage. Further 
                                      investigation, however, showed that the 
                                      aircraft was not on fire until after 
                                      in-flight separation occurred. The reports 
                                      of an explosion also prompted 
                                      investigators to search for signs of 
                                      sabotage, though no traces of explosives 
                                      or shrapnel could be found. 
                                      Study of the engine 
                                      cowlings began to reveal a picture of the 
                                      accident. Inside the cowling of the Pratt 
                                      & Whitney 4000 engines are rub strips 
                                      which function as air seals for the fan 
                                      blades and during takeoff, when maximum 
                                      aerodynamic forces act on the cowling, the 
                                      blades lightly touch the strip, creating a 
                                      rub. Investigation of 004's engines showed 
                                      that there was a much deeper than normal 
                                      rub in the cowling and it was down from 
                                      the top of the cowl, indicating a nosedown 
                                      pitch moment sometime in flight. Most 
                                      astonishing however was the finding that 
                                      the port engine thrust reverser was in the 
                                      deployed position. 
                                      After collection of the 
                                      wreckage, it became clear that the 
                                      aircraft had broken up due to excessive 
                                      buffeting and excessive control forces. 
                                      The FDR had been destroyed in ground fire, 
                                      but the CVR was still readable and 
                                      confirmed the investigator's findings. 
                                      Just after calling Lauda's Bangkok 
                                      facility, Welsh said "That keeps...that's 
                                      come on again!" He then asks Thurner what 
                                      the aircraft's handbook says about the 
                                      indication that Welsh is seeing. Although 
                                      it's still unclear at this point what the 
                                      indication is, it quickly becomes clear. 
                                      Thurner, then reading from the handbook, 
                                      replied "Addition system failures may 
                                      cause inflight deployment. Expect normal 
                                      reverse operation after landing." Thurner 
                                      then asks Welsh if he should call the 
                                      ground facility to ask for advice. 
                                      Welsh replied "Ah...you 
                                      can tell 'm about it...it's just...ah 
                                      no...it's probably...ah water or moisture 
                                      or something because it's not just on, 
                                      it's coming on and off." Nothing more was 
                                      said about it for another five minutes 
                                      when Thurner suddenly said "Reverser's 
                                      deployed!" immediately after there are 
                                      sounds of buffeting and metallic snapping 
                                      until the CVR ends thirty seconds later. 
                                      The investigators were not able to 
                                      determine what caused the uncommanded 
                                      deployment of the thrust reversers, but 
                                      concluded that either the hydraulic or 
                                      electrical systems could have been at 
                                      fault. The destruction of the aircraft was 
                                      so extensive that no determination could 
                                      be made. Tunnel tests of the aircraft 
                                      after the accident showed that the 
                                      recovery window was as small as 4-6 
                                      seconds, the loss of lift on the effected 
                                      wing causing roll rates of up to 28 
                                      degrees/second