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Hi,
Gentlemen, per JAR, an automatic ELT was mandatorily mounted on the aircraft. It activates automatically on crash-like G-forces and sends a short message on 406 MHZ. This message gets through COSPAS/SARSAT. So... What happened to it ? What is the means (safety matter) to have a bunch of emmitting emergency devices if those have to be manually triggered ?? (minus those of liferafts .. etc..) but I am pretty sure that there is no requirement to carry automatic activation ELTs. I think the primary rationale for ELTs is tracing of floating survivors (who will activate them), not automatic location of wreckage. Can someone give the price of such devices ? must be very costly certainly ? :) So .. now.. it's to spend tons of $ for search the plane .... |
jcjeant stridently says:
Yes .. I repeat .. what happened to it ? ?? It (the primary(?) ELT) went to the bottom of the Equtorial Atlantic with the rest of the wreckage. As it got to greater depths the bits that had airpockets were crushed. That's what happened to it. ELT's quite often fail to activate in serious crashes (though they sometimes activate on hard landings :rolleyes: ). Even it AF447's ELT activated on impact, the signal was - literally - drowned out as the wreckage sank. C2j |
Bearfoil,
How many dollars per minute can you afford? Can you obtain the necessary satellite orbital positions to make it work? What are the rules for sending the data? How much power are you willing to dedicate to the problem? How much hardware expense is justified? Can you get the frequency allocations for this service? It sounds like a good idea. It isn't, today. It may be someday. We've been over and over this "solution" here. So far it has come up as not feasible if it is provisioned for peak traffic times for a typical 15 degree horizon to 15 degree horizon satellite. {^_^} |
Bearfoil,
Ten feet, and I wrote ......second (s). {^_-} |
keitaidenwa, ADS-B sounds like an interesting solution. It has some potentially devastating problems associated with its general use. The chief problem is the ability to spoof the system by introducing transmissions for phantom aircraft among the ADS-B transmissions from legitimate aircraft. If that's solved AND the range is sufficient, this would be good for routes that have suitable traffic. For AF447 it might have worked. Some folks here have mentioned being the only plane out over portions of the South Pacific for most of his flight. I believe a Chile to Oz route would enjoy such levels of flight infrequency. Then what?
{^_^} |
KMD, the DC to 30kHz RF spectrum is pretty much the property of the USN simply because the USN spent the money to build the antennas required to operate in that region of the spectrum efficiently. There may be some other nations who have built transmitters in that region. I don't know if Canada has or not. Doing so reads to this USAian to be outside of typical Canadian character. I could be wrong.
These days those transmitters are deprecated in favor of satellite hops. (Outside of littoral waters hiding a submarine under water is close to impossible these days. Satellite photography reveals their locations with wonderful huge arrows painted on the water surface from their underwater wakes. The Navy REALLY does not like to talk about that, for fairly easy to understand reasons.) Note that at least for a while NIST maintained a time standards broadcast on 20kHz-26kHz FSK, WWVL. That service has terminated with WWVB at 60KHz being the VLF service today. So the USN clearly does not have a lock on everything below 500kHz. It may seem that way. People have mostly forgotten that those frequencies can be used with exceptional ranges if you devote enough wire to the antenna. For an extreme antenna example check out "Jim Creek". For a smaller example check out WWVB's antenna. For sonar - there is no way the USN could snarf up everything below 500kHz. There is no international allocation body to allow that. And it would effectively turn off two and a quarter bazillion fishing sonars, bottom obstruction avoidance sonars, and all the other private sonar uses. (I've babbled too much already - I'll be quiet for awhile unless specifically addressed.) |
Originally Posted by JD-EE
(Post 5826439)
KMD, the DC to 30kHz RF spectrum is pretty much the property of the USN....
CJ |
The final Report of the ICAO ELT Task Force of August 2005 can be found at
ICAO ELT Task Force Report and even though an Automatic Fixed ELT is mandatory, the report makes it quite clear that should an aircraft sink, the moment the antenna becomes submerged it is ineffective. So that's what happened to it. mm43 |
Hi,
It (the primary(?) ELT) went to the bottom of the Equtorial Atlantic with the rest of the wreckage. As it got to greater depths the bits that had airpockets were crushed. That's what happened to it. the moment the antenna becomes submerged it is ineffective. And if this floating device is inside the aircraft ... it's another utter non-sens ... For the Airbus ... better to put it on the exterior of the vertical stabilizer .. it's the only part of this aircraft who always float after a crash at sea ....... :eek: Otherwise .. it's plenty auto- release systems working by hydrostatic press ... maybe it's too much sophisticated for the aviation world ?? .. but it work great in the naval world ...... |
jcjeant wrote:- This not supposed to be a floating device ? mm43 |
JD-EE
Hi. I was merely comparing the need for a landslide of data on demand, and the presence of two black boxes that must be retrieved to be of any use. A setting of Mayday on the Tx, or a button push in concert with a distress call could rapidly send all the data needed for forensic reconstruction of flight, (accident). No perpetual transmission is needed, merely the pilot's sending, or the a/c sending a data dump at Law switch. The need for a concentrated "Loop" of pertinent flight data is far, far less expensive than a constant drone of completely unnecessary recordings. You don't like my idea? Tagged Air Computed Airspeed. TACA. It's proprietary, but it makes pitots completely ballast. The nano-nano came from a discussion I was having with my brother, the cosmologist. Plus a wager on who would take the time to compute the metrics. From a land where Light cannot get out of its own way, actually. Mois Aider = M'Aider, meaning "help (aid, or assist me)" pronounced "May Day". Apropos the etiology given we discuss a French tragedie. rgds, bear |
According to the following diagram :
http://i35.servimg.com/u/f35/11/75/17/84/af447_14.gif the ELT antenna could be this one : http://i35.servimg.com/u/f35/11/75/17/84/af447_13.gif Photos: Airbus A330-243 Aircraft Pictures | !!!!!!!!!!!!!! I am also a bit surprised by the following quote from the BEA report : An ELT distress beacon with manual tripping was also recovered. This had not been actuated. Its switch was found in the “OFF” position. On the A330s I know, there are 3 ELTs :
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jcjeant wrote:
This not supposed to be a floating device ? Not a pilot, eh? I've been around since ELT's were first required in the US. They have never been designed to float. As a matter of fact they are supposed to be installed securely in a section of the plane likely NOT to get crushed in an accident. Detachable, floating "rescue beacons" are a more recent boat derivations of the aircraft ELT. The ELT was originally designed to help find aircraft that crashed while NOT in radar contact OVER LAND i.e. "who knows where they crashed". As jet aircraft and airliners were assumed to always be on a flight plan / under radar observation, and as aircraft truly, rarely "fall out of the sky" the risk of not being able to find overwater flights was of minimal concern. Until recently US registered jet aircraft did not require ELT's to even be installed! Is it time to update "crash locator" abilities / requirements? That's for others to decide. Even if new and upgraded units with oceanic "survivability" You can bet that EVERY airline will dig in its heels at the expense and will only do it grudgeingly if mandated. C2j |
Type of portable ELT
Two type of paortable ELTs are installed on Air France fleet :
CEIS S06 : http://www.ceis.com/uk/fiches/03SO6/1SO6/f_1SO6.html or ADT 406S : http://www.elta.fr/uk/emergency-locator-transmitters-elt/1/emergency-locator-transmitters/9/survival-portable-type-adt406-s/8 Both ELTs need to be switched ON manually to begin transmission. The CEIS S06 has an ON/OFF switch that needs to be used. The ADT 406S has an ON/ARMED/OFF switch. The ARMED position is arming the hydraulic switch that allows the ELT to transmit once the switch is activated by some kind of liquid. So the ADT 406 can be water activated only after it has been put in the ARMED mode. This is video (french) showing the ADT406S : Dailymotion - Julie CFS - une vidéo Vie pratique |
CONF iture;
Thanks for the photo and ELT antenna location schematic. Realized after seeing it that I already had the same drawing! pgroell; The links to the Air France fitted ELT types are appreciated, though the most important link came up with "Page not found". The correct link is:- Emergency Locator Transmitters Scroll down to the bottom of the page and there are 6 links to the various ELTs available. The pop-up windows are also scrollable, and some include links to additional windows/pages. The Automatic Fixed type is fitted with a "g" switch, and though details of its operation are not included, the specification calls for the switch to operate when subject to an acceleration of 5g or greater for at least 11 milliseconds in any vector. The GEOSAR satellites covering the position of the AF447 crash are the Meteosat Second Generation geostationary satellites MSG-1 at 9.5° E, MSG-2 at 0° and GOES-12 at 75°W. http://i846.photobucket.com/albums/a...447/geosar.png Modified GEOSAR Coverage Map Once activated the ELT will transmit a 0.5 second data stream on 406.025MHz every 50 seconds, but in this case, I suspect the departing Vertical Stabilizer removed the ELT antenna before the first data burst was complete. EDIT:: Bearing in mind that following activation, no carrier is transmitted during the first 50 seconds, then the first 0.5sec data stream is sent to commence the normal 50 second cycles. So the antenna was by then either missing or submerged. mm43 |
Hi,
It's very frustrating that from the first ACAR message to the second after the AF447 touch water .. nothing on this plane (a nest of high technology) worked as expected ( or worked as expected ???) And to today all the explainations about the possibles reasons of the crash or the explainations about the failures to find the remains of the plane are at least foggiest. |
AF447 search
Finding things on the sea bottom is incredibly dificult, especially given the conditions where AF447 crashed. In fact even finding something on the sea's surface is very difficult. One is dealing with a totally alien environment (which does not seem to be the case at first glance). Paitence, gentlemen patience.
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Hi,
Finding things on the sea bottom is incredibly dificult, especially given the conditions where AF447 crashed. In fact even finding something on the sea's surface is very difficult So it's frustrating that all the (expensives) brains working for the devellopement for a "safest" aviation world had not yet (or want not) design a reliable device able to float and send his position when a plane crash at sea ... Remind me .. we .. humans .. were able to go and land on the Moon and return !!! ... Do we need to revamp the wheel ? .. or it's a "no will" ? |
Lessons learned
From AF447 and Adam Air 574 (and others) we have learned it can be many days before the wreckage of an aircraft traveling in an oceanic environment is localized. This uncertainty significantly increases the cost of recovery efforts and practically guarantees that there can be no survivors.
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Airbus software
I've been thinking about the programming for fly-by-wire aircraft and the software conditional branches to contend with flying close to coffin corner, encountering a major thunderstorm and possibly losing some real-time physical status input. When Windows encounters this kind of situation and gives me the blue screen of death, I can just hit the reset button and restart to a known condition, except on newer machines where you have to disconnect the battery because there is no reset button. Does fly-by-wire hardware have a reset button anywhere close to a human in the cockpit or is it necessary to find a circuit breaker somewhere? Perhaps some professional pilot could answer this.
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