Originally posted by ATLcrew
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Originally posted by ATLcrew View Post
The scenario you describe would require for both BMC lanes to malfunction as well, hence the "failure due to excessive demand". One of BMC's job is precisely to control that demand precisely to prevent what you're describing. So, it seems very unlikely that that's what happened here.
Here is a link to that article if it interests you:
This is a 2009 publication, so the problem may have been designed out since then, but perhaps not retrofitted to older planes.
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Originally posted by Evan View Post
The Airbus lit depicts the Bleed Monitoring Computer in the system description and schematic but makes no mention of a failure as part of the scenario.
Here is a link to that article if it interests you:
This is a 2009 publication, so the problem may have been designed out since then, but perhaps not retrofitted to older planes.
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Bobby, Berntie, ATLie: Something happened involving a lot of acronyms. We (see footnote) think pilots and procedure writers get many things wrong, like this incident.
We must make bold and wordy suggestions as to how you stupid insiders should fix it.
Footnote: We is actually referring to as individual outside, ass hat, parlour talker.
Bicycle, bicycle, bicycle, I want to ride my bicycle…
Les règles de l'aviation de base découragent de longues périodes de dur tirer vers le haut.
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Originally posted by ATLcrew View Post
Well...for one thing, that procedure is for a 320 which is not what was involved in the HiFly incident. For another thing, there are 2 BMC, each with 2 lanes, which this "lit" seems to fail to mention. Finally, our current dual bleed loss procedure is different from what is in the "lit", albeit not radically different.
Both serious incidents were caused by malfunctioning of the engines’ bleed regulated pressure transducers' (Pr). The malfunctioning was caused by freezing of water that had accumulated in the bleed regulated pressure transducers' pressure cell rooms, extremely confined by design. Due to malfunctioning the transducers provided faulty pressure information to bleed monitoring computers. Due to the erroneous information the computers closed both engines’ bleed air systems which resulted loss of pressurisation in cabin, i.e. an increase in cabin air pressure altitude.
The investigation commission issued four safety recommendations. The European Aviation Safety Agency (EASA) was recommended to: 1) require that Airbus S.A.S. replace the pressure transducers on both engines of A330 aircraft with such transducers that function in conditions approved for the A330 fleet and 2) require that Airbus S.A.S. also include Dual Bleed Loss abnormal procedures in the A330 electronic centralized aircraft monitor action.
As of 2012 (latest data I could find), about 30% of the A330 fleet were still not retrofitted with redesigned parts to contend with the threat.
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Originally posted by Evan View PostBut there are scenarios for the A330 that don't require BMC malfunction, but rather erroneous data sent to the BMC's. This is from a Finnish report of two Finnair incidents in which A330's suffered dual bleed air loss
--- Judge what is said by the merits of what is said, not by the credentials of who said it. ---
--- Defend what you say with arguments, not by imposing your credentials ---
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Originally posted by Gabriel View PostProhibiting dispatch with one PAC inop will not help avoid that. Just saying.
One of the downsides of using these planes would be a slightly increased ticket price.
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Originally posted by bstolle View PostExactly. I assume that evan wants only planes like the Do X, H-4 and B-52 to be used as airliners because history shows that all engines have failed even on four engined jet transports.
One of the downsides of using these planes would be a slightly increases ticket price.
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