Posted on 11/16/2001 1:09:13 PM PST by Oldeconomybuyer
Edited on 04/13/2004 3:29:03 AM PDT by Jim Robinson. [history]
WASHINGTON -- Safety records show the American Airlines plane that crashed in New York was severely shaken by air turbulence seven years earlier in an episode that injured 47 people.
One possibility safety investigators are considering is that the Airbus A300 broke apart Monday after hitting turbulence from the plane taking off before it at Kennedy International Airport.
(Excerpt) Read more at bayarea.com ...
"Lets see, birds crashed it, turbine blades separated, engine pilons were weak and fell off, fuel system ignited accidentally, engine was on fire before it took off, engine fell off and caused a yaw, now turbulence seven years ago caused it........anyone smell BULL ??"
Nope! All of these things can bring down an aircraft. If they failed to find any stress fractures, and the vertical stab spar was not magnafluxed after the 1994 incident to inspect it ... the seven year scenario is perfectly plausible. You guys act like there is no shoddy maintenance that happens on major airlines.
In answer to your question of smelling BULL ... yeah, its coming from all of the tin foil hat types on this subject.
Add to that the fact that I'm, to a great degree, master of my own destiny while driving a car, not dependent on a pilot and an airline, and you can see why driving is looking better and better.
2. Separation of the wing.
3. Wing sheers off the "tail" (V/stabilizer).
Could we be seeing only the top part of the V/stabilizer after is had been sheered off by the departing wing?
Also, where did the turbulence come from? The departing flight before Fl. 587 was many miles ahead of it when Fl. 587 took off. You don't have "wake turbulence" for miles behind a plane.
Something is definitely fishy about this investigation. The more of these wacko "mechanical failure" scenarios they come up with, the more comfortable I get with wacko cover-up theories....
Add to this that there was a helicpoter in the vicinity of flight 587, a large source of turbulence.
Its possible that the airport security delays is putting pressure on allowing more lift-offs per hour and less time between lift-off.
Engines
Birds
Turbulence
Prior damage
What next, a loner pychopath right-wing extremist?
The turbulence from other planes on other runways can drift, its not static. Plus a helicopter was in area.
Actually you do, especially behind a large heavy airplane like a 747 headed to Japan. But generally, the vortices will sink to the ground. The 747 likely had a longer take off roll and a slower ascent, so the vortices, in theory, should have sunk lower to the ground than the normal flight path of the Airbus (unless they are such tugs that they climb poorly). Anyway, the point is simple: airliners hit wake turbulence all the time. It shakes and/or rolls the aircraft, the pilot corrects, and you keep going.
Yeah! And some still think the planes hitting the WTC was a terrorist act! They haven't shown one piece of plane to actually prove it!!
Also, Central-Scrutinizer is a handle that could mean you look at race cars real close. (Just curious)
I sure hope that the NTSB isn't going to try to fob us off with some turbulence bs. A plane that can't handle turbulence???? I have yet to be on a plane that didn't have some turbulence, and sometimes so bad that I could almost (gulp) "see" the nuts and bolts working themselves loose!
A terrorist threat wouldn't keep me from flying again. Planes that can't handle turbulence would!
The one I was on was flying in the Carribean about 20 years ago. - Tom
Something's Up!!
On the day this happend, just before making this post, I checked the FAA Incident Database for N14053, the airplane's registration, which was published by AOPA.
There was no report there, nothing...but there is today. Draw your own conclusions.
Here's another wacko theory: Is it possible that the control system failed (while trying to compensate for wake turbulence) which allowed uncontrolled movement by the rudder? If uncontrolled, a "flapping" rudder could exert substantial stress on the VS. Obviously, this scenario would also have to end with the rudder locked in a 10 degree left positon.
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