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Interestingly enough, the DC-10 fuselage structure was designed by General Dynamics, not McDonnell Douglas. And when GD ran the structural test of the fuselage, meant to show that the fuselage could withstand the effects of explosive decompression, it failed. They found that explosive decompression in the cargo compartments would result in the collapse of the passenger compartment floor - the floor that also served to hold the flight control routings. GD told McD that they would have to redesign the fuselage and McD replied that there was no time for that. Lockheed was building the L-1011, a similar sized widebody airliner, and the expectations were that the market would not support both of them. Lockheed was ahead of McD and both companies viewed who had the first airplane rollout to be crucial to determining program success. As it turned out, the DC-10 floor vulnerability proved to be a real problem, since it was combined with a flawed baggage compartment hatch design, which McD chose to make electrically powered rather that using hydraulics, with the result that it could be closed but not locked in place.Stress test of an airliner
Not exactly, but the logic is absolutely correct.Concorde?
"...next time, maybe drop your payload at a little higher altitude..."No problem! We'll have it back on the line tomorrow morning.
I flew on a DC-10 from San Fran up to Seattle, on the return leg of a trip I took to Japan when I was 13.Interestingly enough, the DC-10 fuselage structure was designed by General Dynamics, not McDonnell Douglas. And when GD ran the structural test of the fuselage, meant to show that the fuselage could withstand the effects of explosive decompression, it failed. They found that explosive decompression in the cargo compartments would result in the collapse of the passenger compartment floor - the floor that also served to hold the flight control routings. GD told McD that they would have to redesign the fuselage and McD replied that there was no time for that. Lockheed was building the L-1011, a similar sized widebody airliner, and the expectations were that the market would not support both of them. Lockheed was ahead of McD and both companies viewed who had the first airplane rollout to be crucial to determining program success. As it turned out, the DC-10 floor vulnerability proved to be a real problem, since it was combined with a flawed baggage compartment hatch design, which McD chose to make electrically powered rather that using hydraulics, with the result that it could be closed but not locked in place.
I worked with this guy in 1992 and the way he made it sound, I think he had worked there just a few years before, but for how long, I don't recall (if I ever knew).DC-8 series 50 for certain flew nose down to kill excessive lift, other series I am not sure.
Tempted maybe, but I bet you would take the ride.I hope that Shagbat can handle the speed of that tow!
I think if one of those came to pick me up while I was floating in my little dingy I'd be tempted to tell them I would catch the next ride.
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I read of a Spitfire Wingco in the Med seized a brand new bird for his personal use. On a patrol over Italy he found out too late that the drop tank would not feed. He ended up bailing out over the water. After what it seemed like an eternity a Shagbat came to pick him up but on the way there it had taken some ground fire and was in the process of sinking. They eventually got it off and returned him home.Tempted maybe, but I bet you would take the ride.
I believe a discussion on the Tu-144 is unlikely to be relevant within this thread, so I've decided to start a new thread here. Hopefully, I can explain there why the use of the nickname "Concordski" is inappropriate.That makes sense, I could not understand what the heating elements where for, I forgot about the 2 Mach 2 capable designs. Good photo! Now I would like to see the Soviet cooling solution in diagram for the Concordski. I understand the noise it transmitted to the passenger cabin was most unpleasant!