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             It was a nasty 
             afternoon in Miami the day of February 12, 1963. A Northwest 
             Airlines Boeing 720, designated flight 705, was scheduled to depart 
             at 1:30pm bound for Portland, Oregon. On the flight deck that day 
             was Captain Roy Almquist and First Officer Robert Feller. Along 
             with the flight engineer and five cabin attendants, only 
             thirty-five passengers boarded for the first leg to Chicago. A 
             squall line was lying to the northwest of the city, slowly moving 
             southeast. Associated with this line were thunderstorm cells up to 
             20 miles in diameter, some reaching as high as 40,000ft. A sigmet 
             had been issued for moderate to severe turbulence with a chance of 
             extreme turbulence inside the storms. The crew asked for a 
             southeast departure, hoping to go around or over the top of the 
             worst of the weather. After heading south east initially, the 
             aircraft was vectored back north at 5000ft. Feller called Miami, 
             asking for a higher altitude and reporting that "We're in the clear 
             now. We can see it out ahead...it looks pretty bad." 705 was then 
             cleared to climb to FL250 and said they would be turning 30 degrees 
             left, giving them and approximate heading of 270 degrees. Feller 
             then told Miami that turbulence was "moderate to heavy" and then 
             advised them "OK, you better run the rest of them off the other 
             way." After being handed off to Miami Centre, Feller reported that 
             they were climbing through 17,500ft. This transmission, thirteen 
             minutes after takeoff, was the last from 705. Shortly after, 
             several people located in the Everglades heard a loud explosion 
             followed by a ground tremor. One women reported seeing what looked 
             like "a ball of flame in the edge of a cloud."......Wreckage was strewn over some 
             fifteen miles, indicating an in-flight break-up of the aircraft. 
             While it was clear the weather was severe in the area, sabotage 
             could not be ruled out nor could some other sort of component 
             failure, the aircraft having been involved in a landing accident a 
             few months prior.
 
              Reconstructed 
             Wreckage of 705
 
             Collection of the 
             wreckage showed that the tail surfaces had broken off downward 
             while the forward fuselage separated upwards. All four engines had 
             separated upward as well. Readout of the FDR showed that showed 
             that the aircraft had encountered some heavy turbulence while 
             climbing to 15,000ft until it turned more westerly. It then turned 
             back northwest and began to climb again, at one point obtaining a 
             climb rate of 9000ft/min until reaching just over 19,000ft. At this 
             point, the vertical acceleration suddenly became negative 2gs, 
             increasing even further with fluctuations up to negative 2.8gs, the 
             airspeed continuing to increase as well. Vertical acceleration 
             abruptly went back to positive 1.5gs. During it's descent, the 
             airspeed increased until the FDR was no longer able to accurately 
             measure it, greater than 470kts. Analysis showed that the aircraft 
             would have reached some 22 degrees pitch up during it's dramatic 
             climb to beyond vertical in it's final descent. Structural tests of 
             the 720 showed that it could have withstood the initial excessive 
             forces brought on by the thunderstorm gusts. It appeared that the 
             aircraft did not break up until the crew apparently tried to 
             recover when passing through 10,000ft. The question then was what 
             caused the aircraft to get into such an unusual condition. The 
             answer came in the fact that the aircraft has an inherit tendency 
             to 'weathervane' into gusts. So, when the initial updraft caught 
             the aircraft, it would have an initial tendency to nose down into 
             the gust. This apparently prompted Almquist to give nose-up inputs, 
             which would actually worsen the overall situation. The same effect 
             worked in the downdraft which followed. It is also important to 
             note that, although it appears full up elevator was used in the 
             recovery attempt, full nose-down trim was still wound in from the 
             prior encounter with the updraft. Boeing tests showed that recovery 
             from the dive in this condition beyond 320kts is not possible.
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