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#1
February 26th 04, 05:03 PM
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"Tarver Engineering" wrote...
What is "an unmapped part of the A-320's flight control system" supposed to mean?!? Airbus hadn't programmed their A-320 to do what the operator commanded. Hmmm... I suspect that when the pilot added go-around power, he commanded the airplane to provide maximum lift/minimum sink while the engines spooled up. As far as we can tell, the flight control system responded properly, providing max lift without stalling. It is not the job of the flight control system to map trees, but the trees in the flight path interrupted the plan... I am quite certain that the A-320's certification included slow flight and approaches to stalls, and that its flight control system is well able to handle them. Then you have departed from reality. I see... Now you imply that either the A-320 certification did NOT include slow flight and approaches to stalls, or that it was certified despite its failure to demonstrate the required controllability in those regimes. Anyone have the coordinates of reality? I need to punch them into the FMS-CDU tomorrow... 
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#2
February 26th 04, 06:17 PM
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"John R Weiss" wrote in message news:AFp%b.402349$I06.4378804@attbi_s01... "Tarver Engineering" wrote... What is "an unmapped part of the A-320's flight control system" supposed to mean?!? Airbus hadn't programmed their A-320 to do what the operator commanded. Hmmm... I suspect that when the pilot added go-around power, he commanded the airplane to provide maximum lift/minimum sink while the engines spooled up. In what wy do you believe that stalling the wing is within the flight envelope?
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#3
February 26th 04, 09:41 PM
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"Tarver Engineering" wrote...
Airbus hadn't programmed their A-320 to do what the operator commanded. Hmmm... I suspect that when the pilot added go-around power, he commanded the airplane to provide maximum lift/minimum sink while the engines spooled up. In what wy do you believe that stalling the wing is within the flight envelope? In what way do you believe stalling the wing had anything to do with the late go-around attempt? What flight envelope?
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#4
February 27th 04, 12:40 AM
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"John R Weiss" wrote in message news:rKt%b.418959$na.808977@attbi_s04... "Tarver Engineering" wrote... Airbus hadn't programmed their A-320 to do what the operator commanded. Hmmm... I suspect that when the pilot added go-around power, he commanded the airplane to provide maximum lift/minimum sink while the engines spooled up. In what wy do you believe that stalling the wing is within the flight envelope? In what way do you believe stalling the wing had anything to do with the late go-around attempt? What?
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#5
February 28th 04, 06:11 PM
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"Tarver Engineering" wrote in message ...
"John R Weiss" wrote in message news:AFp%b.402349$I06.4378804@attbi_s01... "Tarver Engineering" wrote... What is "an unmapped part of the A-320's flight control system" supposed to mean?!? Airbus hadn't programmed their A-320 to do what the operator commanded. Hmmm... I suspect that when the pilot added go-around power, he commanded the airplane to provide maximum lift/minimum sink while the engines spooled up. In what wy do you believe that stalling the wing is within the flight envelope? how did it stall ?
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