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#26
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This is an interesting point, but I think incorrect. There was a very
interesting book about the DC-10 that came out a number of years ago. The Sioux City incident was not the first one where control was lost, albeit for different reasons. The locking mechanism on the cargo door of the DC-10 was electromechanical, not hydraulic like on others. An electric motor was used to pull toggles over center to lock the cargo door to the fuselage frame and floor. That meant that when the locking mechanism jammed (and the locking lever was capable of being jammed when forced to close), the fuselage underwent an explosive decompression when the locking toggles failed, rather than having the hydraulic mechanism gradually "overpowered" by pressure differential. The control cables for the empennage were routed on the underside of the floor, and when the fuselage underwent explosive decompression, the floor buckled and the cables jammed. I think the first incident happened over Windsor, Ontario. There was another in Ermenonville, France. After that the DC-10 pilots actually practiced, in the sim of course, flying the airplane by using differential thrust. So, I agree with the premise, but I think the detail is wrong. I recognize that in Sioux City the reason for the failure and the extent of control loss was different. Captain Haines is one of my heroes. The best example I can think of is United #232 (Sioux City, 1989). I doubt Al Haines was ever trained to control a DC-10 without hydraulic power to the flight control surfaces. Yet he managed to steer the jet with differential thrust to a (scary) landing without the loss of all aboard. There will never be a replacement for experience IMO. |
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