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#24
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"sid" wrote in message om... "Tarver Engineering" wrote in message ... "Gord Beaman" wrote in message ... (sid) wrote: I should have framed the question this way: How far would either aircraft fly if there is trouble in the E&E bay that compromises the electrical system and you are down to DC power...And then you lose even that? Isn't that like saying "what would happen if the bloody wings were to fall off"?...pretty silly statement imo. I can't understand the obsession with DC power either. Airplanes mostly use AC power for controls. I have yet to see a synchro that runs on DC. Further assurance of maintaining proper attitude can come from dedicated power sources. In the last five minutes of the 1998 tragedy of Swissair Flight 111, with a raging electrically stoked fire spreading from the attic space in the cockpit, the two pilots had no attitude reference at all-not even a turn needle or turn coordinator to fall back on. They saw inky blackness on the outside and black primary flight displays [PDFs] inside the cockpit. The standby ADI, even if it had been working, was located near the bottom center of the instrument panel. It was poorly lit and even more difficult to see while wearing smoke masks. Yep, old Marky Ostendorf modified the airplane such that there was a half assed exension cord in the cieling carrying 55 Ampres of AC derived from the battery bus. The Swissair jet's standby was lost because it had been hooked to a vulnerable hot battery bus. When it failed, the powerless gyro started to spin down. Therein lies a vital object lesson in redundancy: Standby instruments need their own batteries, so that a loss of generated power doesn't take down the sole fallback attitude reference. None of that mattered when the magnetic contacter triped bac in and th arc tracing wire bundle burned an 18 feet long hole in the fuse; including cutting the doubler at dorr #1. Writing about a case of manslaughter by way of gross negligence is no reflection whatsover WRT Boeing, or AI airplanes. |
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