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American Flight 191 - Recovery Procedure



 
 
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  #11  
Old November 3rd 06, 04:43 PM posted to rec.aviation.piloting
Jim Macklin
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Posts: 2,070
Default American Flight 191 - Recovery Procedure

I was speaking about ANOTHER accident that had been asked
about. I was speaking about the Sioux City accident. I had
already addressed the 191 slat retract.



"Ron Wanttaja" wrote in message
...
| On Fri, 3 Nov 2006 00:24:54 -0600, "Jim Macklin"
| wrote:
|
| That accident was almost a successful landing, right up
to
| the point that they dropped the gear.
|
| Wrong accident...you're thinking of United 232 in Sioux
City. American 191 is
| the one in Chicago where the engine pod physically broke
free of the wing right
| after takeoff. 271 dead, no survivors.
|
| I have my own strange connection to the Chicago accident.
I was an on-duty
| operator for a USAF missile launch detection satellite
which operated in the IR
| spectrum. We detected the heat from the crash.
|
| Ron Wanttaja


  #12  
Old November 3rd 06, 09:15 PM posted to rec.aviation.piloting
Mxsmanic
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Posts: 9,169
Default American Flight 191 - Recovery Procedure

Ron Wanttaja writes:

I have my own strange connection to the Chicago accident. I was an on-duty
operator for a USAF missile launch detection satellite which operated in the IR
spectrum. We detected the heat from the crash.


Are you saying anything you shouldn't?

--
Transpose mxsmanic and gmail to reach me by e-mail.
  #13  
Old November 4th 06, 12:21 AM posted to rec.aviation.piloting
Robert M. Gary
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Posts: 2,767
Default American Flight 191 - Recovery Procedure


Jim Macklin wrote:
Yes, a DC-10 at Tulsa had both wing mounted engines fail
after sucking up about 10,000 sparrows. Came around on just
the tail engine.

The problem with flight 191 was that the crew did not know
the slat had retracted. Since lift varies by the sq.root of
the speed, the wing would not be stalled at V2, but with the
slat retracted, the effect was greater than the combined
effect of rudder and aileron anti-roll command. At 300 feet
they just wasn't time to figure it out.


Running both hydralic lines (allowing the slats to retract) within
inches of eash other was perhaps a questional decision.

-Robert

  #14  
Old November 4th 06, 02:07 AM posted to rec.aviation.piloting
Ron Wanttaja
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Posts: 756
Default American Flight 191 - Recovery Procedure

On Fri, 03 Nov 2006 22:15:41 +0100, Mxsmanic wrote:

Ron Wanttaja writes:

I have my own strange connection to the Chicago accident. I was an on-duty
operator for a USAF missile launch detection satellite which operated in the IR
spectrum. We detected the heat from the crash.


Are you saying anything you shouldn't?


All the time, why?

Ron Wanttaja
  #15  
Old November 4th 06, 07:25 AM posted to rec.aviation.piloting
Jim Macklin
external usenet poster
 
Posts: 2,070
Default American Flight 191 - Recovery Procedure

It was OK on the DC-9 and nobody considered the difference
on the DC-10. Yes it was a bad design as was not using
hydraulic fuses and not having essential power as is now
required on Part 25, perhaps because of what was learned
from 191.



"Robert M. Gary" wrote in message
oups.com...
|
| Jim Macklin wrote:
| Yes, a DC-10 at Tulsa had both wing mounted engines fail
| after sucking up about 10,000 sparrows. Came around on
just
| the tail engine.
|
| The problem with flight 191 was that the crew did not
know
| the slat had retracted. Since lift varies by the
sq.root of
| the speed, the wing would not be stalled at V2, but with
the
| slat retracted, the effect was greater than the combined
| effect of rudder and aileron anti-roll command. At 300
feet
| they just wasn't time to figure it out.
|
| Running both hydralic lines (allowing the slats to
retract) within
| inches of eash other was perhaps a questional decision.
|
| -Robert
|


  #16  
Old November 5th 06, 12:20 AM posted to rec.aviation.piloting
Blanche
external usenet poster
 
Posts: 346
Default American Flight 191 - Recovery Procedure

Mxsmanic wrote:
Ron Wanttaja writes:

I have my own strange connection to the Chicago accident. I was an on-duty
operator for a USAF missile launch detection satellite which operated

in the IR
spectrum. We detected the heat from the crash.


Are you saying anything you shouldn't?


It's common and public knowledge that one of NORAD's responsibilities
is to monitor missle launches.

www.norad.mil/about_us.htm
  #17  
Old November 5th 06, 02:17 AM posted to rec.aviation.piloting
Mxsmanic
external usenet poster
 
Posts: 9,169
Default American Flight 191 - Recovery Procedure

Blanche writes:

It's common and public knowledge that one of NORAD's responsibilities
is to monitor missle launches.


Yes, but the exact monitoring capabilities of satellites may not be
public knowledge (although they aren't necessarily always classified,
either).

--
Transpose mxsmanic and gmail to reach me by e-mail.
  #18  
Old November 5th 06, 03:35 AM posted to rec.aviation.piloting
Ron Wanttaja
external usenet poster
 
Posts: 756
Default American Flight 191 - Recovery Procedure

On Sun, 05 Nov 2006 03:17:21 +0100, Mxsmanic wrote:

Blanche writes:

It's common and public knowledge that one of NORAD's responsibilities
is to monitor missle launches.


Yes, but the exact monitoring capabilities of satellites may not be
public knowledge (although they aren't necessarily always classified,
either).


"In recent years, scientists have been developing methods to use DSP's infrared
sensor as part of an early warning system for natural disasters...."

http://spaceflightnow.com/titan/b39/040210dsp.html

Ron Wanttaja
 




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