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#1
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I am not sure I would willingly fly around with this much life
endangering explosive products in the baggage compartment of my Warrior.... And in an aircraft that was not engineered to willingly assist the pilot to maintain, recover to, and sustain controlled flight.. Hmmmmmm... But, alas, I am also having difficulty in understanding why Garmin would install magnets in their remote GPS antenna that commonly is placed on the cowl/glareshield of of what is usually an ALUMINUM or COMPOSITE aircraft. Must be getting old, I'm having trouble understanding some things.. Dave ..On Sun, 18 Dec 2005 14:08:02 -0500, "Peter R." wrote: Ron Lee wrote: That is comforting. You crash in a Cirrus but sustain life-threatening injuries. So no one can assist until Cirrus is contacted. So they wait a safe distance from the aircraft until you die. I have a friend who is a sergeant with the NY State Police. Three and a half years ago he was the first responder to the fatal Cirrus spin crash here in Central NY. He told me was that the police and rescue squad were all warned to remain clear of the aircraft because of the explosive device used to launch the parachute. He also added that it was obvious from the state of the bodies that they were not there to save the pilots lives. |
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#2
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Dave wrote:
I am not sure I would willingly fly around with this much life endangering explosive products in the baggage compartment of my Warrior.... When fuel tanks are less than full, one may have an explosive air/fuel vapor mixture in them. And post-crash fires are sufficiently common that I'm not sure why a ballistic chute system is considered any more dangerous than many dozens of pounds of highly flammable liquid. Why would one consider an undeployed BRS more dangerous than a fuel system on a crashed plane? [...] Must be getting old, I'm having trouble understanding some things.. Me too. :-) |
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#3
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On Mon, 19 Dec 2005 03:56:14 -0000, Jim Logajan
wrote: Dave wrote: I am not sure I would willingly fly around with this much life endangering explosive products in the baggage compartment of my Warrior.... When fuel tanks are less than full, one may have an explosive air/fuel vapor mixture in them. And post-crash fires are sufficiently common that That's *may* have, but under normal circumstances I'd expect the mixture to be above the UEL. Post crash fires and particularly the spectacular ones are usually from ruptured tanks. I'm not sure why a ballistic chute system is considered any more dangerous than many dozens of pounds of highly flammable liquid. Why would one consider an undeployed BRS more dangerous than a fuel system on a crashed plane? The fuel can leak away and vaporize so if there is no immediate fire there is unlikely to be one. OTOH a primed BRS is primed until disabled. To me, it wouldn't make a bit of difference between the two. If the paths taken where the lanyards are in the fuselage and wings were marked out they could have avoid areas. As far as airbags, the system should be capable of being disarmed easily. If not, it needs fixing. OTOH It makes me no more nervous to fly planes with out a BRS than it does with.. Roger Halstead (K8RI & ARRL life member) (N833R, S# CD-2 Worlds oldest Debonair) www.rogerhalstead.com [...] Must be getting old, I'm having trouble understanding some things.. Me too. :-) |
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#4
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Jim,
Why would one consider an undeployed BRS more dangerous than a fuel system on a crashed plane? Because in the former case, it is much clearer who to sue in a frivolous law suit. -- Thomas Borchert (EDDH) |
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#5
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"Dave" wrote\ And in an aircraft that was not engineered to willingly assist the pilot to maintain, recover to, and sustain controlled flight.. ++++++++++++++++++ I'm not sure if that is the whole picture. The Cirrus was not certified for spin resistance and recovery because it would have been so expensive to do so, up to the FAA's standards. That is not to say that it would not meet them, if they tried to do so. +++++++++++++++++++ Simply put, they took the cheap way out, with the *added* benefit of another mode of recovery for other types of situations, such as pilot incompacitation, loss of flight controls, loss of power over inhospitable terrain... +++++++++++++++++++ But, alas, I am also having difficulty in understanding why Garmin would install magnets in their remote GPS antenna that commonly is placed on the cowl/glareshield of of what is usually an ALUMINUM or COMPOSITE aircraft. Must be getting old, I'm having trouble understanding some things.. +++++++++++++++++++ Nah, that is called wisdom... I think! g I predict that Garmin will finally give in and make a new type of antenna. (I hope) -- Jim in NC |
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#6
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Apparently the pressure is building...
It is an expensive unit, and some people are getting upset.. The magnets are very difficult to remove, Garmen has made it abundantly clear that this will void the warranty, and have no interest in exchanging it for one without magnets, which of course they don't make .. Or something like that... ![]() WHAT were they thinking? (or were they) Surprising from a company with long experience in aviation GPS units.... Dave On Sun, 18 Dec 2005 23:59:14 -0500, "Morgans" wrote: I predict that Garmin will finally give in and make a new type of antenna. (I hope) |
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#7
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"Dave" wrote WHAT were they thinking? (or were they) Surprising from a company with long experience in aviation GPS units.... Myself, I don't think it is too surprising. You have the hardware gurus with the aviation permanent mount receiver department. Then you have the hardware guys for the handheld units. Lots of difference in the hardware, most likely different people. The software is the most common thing between the two, but the software people don't care what is running it, as long as the unit is capable of running it, which is what the hardware guys can tell them. The aviation guys know what they have to have for permanent mount antennae on airplanes. No magnets, right? The handhelds have antennae in the units, with a few having the added capability of an added antenna. Who uses those? For one, the XM guys, and the car GPS receiver guys. People with steel car roofs, thus the magnets. The XM people say, "hey, why not use a basic design we already use." The left hand didn't anticipate the different needs of the right hand. So how long does it take to realize there is a big problem, design a different antenna, get it to manufacturing and distribute it? My guess is 6 months, minimum. Added to that the fact that they already have made a big production run of the wrong antennae, which they would no doubt like to sell; otherwise it takes directly away from the per unit profit. These people kill to save pennies per unit, but now they are going to have to take a hit for several tens of dollars per unit? Someone up top is *not* a happy camper, at Garmin, I'll bet. -- Jim in NC |
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#8
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Morgans wrote: "Dave" wrote\ And in an aircraft that was not engineered to willingly assist the pilot to maintain, recover to, and sustain controlled flight.. ++++++++++++++++++ I'm not sure if that is the whole picture. The Cirrus was not certified for spin resistance and recovery because it would have been so expensive to do so, up to the FAA's standards. That is not to say that it would not meet them, if they tried to do so. +++++++++++++++++++ Simply put, they took the cheap way out, with the *added* benefit of another mode of recovery for other types of situations, such as pilot incompacitation, loss of flight controls, loss of power over inhospitable terrain... It was cheaper to design, test and certify a BRS than it was to take the plane up and do a couple of spins? I think not. The CAPS tests themselves required the destruction of at least one airframe. Spin testing just has to show recovery after a couple times around. The reason the Cirrus was not spin tested is because it is very stall resistant. Any maneuver that could throw this plane into a spin might be so violent as to be unrecoverable. There have been accidents attributed to people trying deliberately to spin the Cirrus. There is no reason to attempt to spin the airplane anyway. It is unlikely to enter a spin accidentally, so it is not as if it is a needed emergency procedure. Some people claim the airplane will successfully recover from at least an initial spin. Fine. But why bother? Cirrus strongly discourages it. It is not really certified for it. There is no training advantage to it. If I want to do spins then give me an airplane where they will be fun; even Aerobat. Doing spins in a Cirrus would be like doing motocross in a Ferrari. |
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#9
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"cjcampbell" wrote\ It was cheaper to design, test and certify a BRS than it was to take the plane up and do a couple of spins? I think not. The CAPS tests themselves required the destruction of at least one airframe. Spin testing just has to show recovery after a couple times around. I wouldn't know for sure about the cost. It was my impression that it was very expensive and time consuming to spin certify , and spin resistance certify a new design. The reason the Cirrus was not spin tested is because it is very stall resistant. Any maneuver that could throw this plane into a spin might be so violent as to be unrecoverable. There have been accidents attributed to people trying deliberately to spin the Cirrus. There is no reason to attempt to spin the airplane anyway. It is unlikely to enter a spin accidentally, so it is not as if it is a needed emergency procedure. Granted about the spin resistance. I think the other thing that some people are overlooking is the brother's goals in a new GA airplane, which was to make it safer than all other GA craft, in giving an out in continued VFR into IMC, departures, loss of engine and a dozen other problems that sometimes come up. That was real important to them. Some people claim the airplane will successfully recover from at least an initial spin. Fine. But why bother? Cirrus strongly discourages it. It is not really certified for it. There is no training advantage to it. If I want to do spins then give me an airplane where they will be fun; even Aerobat. Doing spins in a Cirrus would be like doing motocross in a Ferrari. Chuckle How true! -- Jim in NC |
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#10
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On Sun, 18 Dec 2005 at 22:05:05 in message
, Dave wrote: But, alas, I am also having difficulty in understanding why Garmin would install magnets in their remote GPS antenna that commonly is placed on the cowl/glareshield of of what is usually an ALUMINUM or COMPOSITE aircraft. Perhaps because it is almost the same as the one I have had for some time that goes on the roof of my car? There it fits snug and never seems to move until I take it off. :-) -- David CL Francis |
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