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Midwinter wrote:The first thing I thought of when I saw it was a Fed Ex plane that crashed was "Am I expecting anything in the mail?"... does that make me a bad person? Condolences to the families of the pilots though. Seriously, the work of your loved ones help to make living away from home that much more bearable. Thank you....
Midwinter wrote:The first thing I thought of when I saw it was a Fed Ex plane that crashed was "Am I expecting anything in the mail?"... does that make me a bad person?
Takechanpoo wrote:
Takechanpoo wrote:
Greatest danger: Takeoff and landing
Windshear poses the greatest danger to aircraft during takeoff and landing, when the plane is close to the ground and has little time or room to maneuver. During landing, the pilot has already reduced engine power and may not have time to increase speed enough to escape the downdraft. During takeoff, an aircraft is near stall speed and thus is very vulnerable to windshear.
The MD-11 has been involved in accidents in which it flipped while landing, and pilots have complained about the aircraft in the past. The plane is no longer used by carriers for passenger travel but is widely employed for moving cargo.
In 1999, an MD-11 flipped over and burst into flames, killing three people during a crash landing in a storm in Hong Kong. And in 1997 one of the planes landed hard, flipped and caught fire while landing in Newark, N.J.
Tomoki Kuwano, a former Japan Airlines pilot and aviation expert, said that although wind shear could not be ruled out, the MD-11 has a tendency to be unstable during landing.
"In the past, the MD-11 has a record of landing failure," he said. "And when that happens it often flips over."
Tsuru wrote:Mike is on the money. Well-designed planes DO NOT crash from an inflight upset such as windshear. The MD-11 has big problems coping with inflight upsets due to the way it is designed (being a trijet with one engine hanging over the back, being longer than a DC-10 while at the same time having a smaller tailplane for economic reasons), and to top it all off the wing on the side that receives the brunt of the impact of an extremely hard landing on a DC-10 or MD-11 will usually completely separate from the rest of the airframe, with the asymmetric lift from the remaining wing flipping the aircraft on its back as it slides across the ground.
They fitted the MD-11 with a system called LSAS to help the pilots control this design failure with wings, but as you can see it didn't really help them flying into a gusty Narita. Rest in peace.
Mike Oxlong wrote:The plane is no longer used by carriers for passenger travel but is widely employed for moving cargo.
Finnair and KLM still fly them with passengers, the latter is phasing them out in 2012. Lucky coincidence has me flying their MD-11 sim this friday, giving me a chance to see all of this for myself.Mock Cockpit wrote:I believe Finnair, for one, still flies MD11s, at least they were as recently as last August when I saw one at Kansai.
Tsuru, as I understand, the problem you described is basically what caused AA 191 to crash.
Tsuru wrote:The same flightnumber landing in similar conditions onto the other end of the same runway, as flown a month and a half ago:
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Behan wrote:That looked scary and really close to accident.
GuyJean wrote:Narita Drifting.. ]This might've been posted somewhere before, but...[/I]
GJ
Tsuru wrote:Finnair and KLM still fly them with passengers, the latter is phasing them out in 2012. Lucky coincidence has me flying their MD-11 sim this friday, giving me a chance to see all of this for myself.
AA191 is an oddball crash with a different cause altogether, improper maintenance (using a forklift instead of the special cradle to replace engines) caused hairline fractures in the no.1 engine mount and during takeoff in Chicago one day, the no.1 engine tore itself loose from the wing at full power, taking some of the plumbing for the hydraulics with it which in turn caused the leading edge high-lift devices called slats to retract on one side. The now slatless left wing stalled immediately and the lift differential between the handicapped left wing and the fully fuctioning right wing combined with the loss of thrust on the left side of the plane flipped the plane upside down in a split second, sending it into a trailerpark at 400mph. The only other crash it can be compared to is the 747 cargo crash that happened in Amsterdam in 1992, which is the big one that motivated me as a kid to become what I am today
Mock Cockpit wrote:I understood about the improper handling of the engine but not about the loss of hydraulic power. Makes sense. Again, as I understand it, the loss of an engine (functionally or actual physical separation) shouldn't necessarily cause a plane to crash. Would I be right in thinking that in today's planes the scenario you described above be almost impossible?
Greji wrote:Impossible is a big word, but with the advent of fan jet engines, you can lose a couple of engines and if you still have one good one, you have a good possibility of maintaining an airborne attitude and getting back on the ground safely even with some of the bigger birds. Even without engines your aerodynamics can keep control to bring it into a controlled landing of sorts, i.e. Sully's Hudson River splash down.
The biggest problems would probably be structural failures with wings and otherwise. You have a wing or stabilizer failures and you start getting control problems, especially if it is accompanied with other malfunctions. Loss of control at 3-400 knots can cause the pilot's pucker factor to start nipping washers out of the seat....
Mock Cockpit wrote:Would I be right in thinking that in today's planes the scenario you described above be almost impossible?
FG Lurker wrote:I would guess (and a guess it is) that if the hydraulic lines get ripped out of the wing then there isn't much that any control system can do.
A fly-by-wire system actually replaces manual control of the aircraft with an electronic interface. The movements of flight controls are converted to electronic signals, and flight control computers determine how to move the actuators at each control surface to provide the expected response. The actuators are usually hydraulic, but electric actuators have been used.
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