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DaveReidUK
2025-06-17T20:00:00 permalink Post: 11904606 |
I was referring to CVR/FDRs in general being specialist equipment requiring specialist facilities to process. In any case, I would be very interested to find out where those from this accident are read. It appears from a post upthread there are new facilities in New Dehli that could be used. Having said that, for the EK 521 accident in Dubai the recorders were sent to the UK for analysis, despite a "flight data recorder centre" in Abu Dhabi being opened (again with much fanfare) by the UAE GCAA five years before the occurrence.
Subjects: AAIB (All) AAIB (IDGA) CVR EAFR FDR 3 users liked this post. |
DaveReidUK
2025-06-17T21:29:00 permalink Post: 11904679 |
the difference may lay in the content that was recorded and not so much the 2 identical EAFR's. Only the forward EAFR is connected to a dedicated backup battery (RIPS) which also provides backup power to the Cockpit Area Microphone. So in case of a major electrical power mishap, the forward - and likely (externally?) damaged - EAFR might be crucial for recovering all available CVRecordings. Hence the somewhat understandable split-up in news-reports, between FDR data (from the rear EAFR) and complete CVR recordings (from the forward).
If the aft EAFR ceased recording at the point (just short of the runway end) where the ADS-B and likely everything else went dark, then the extra 30 seconds of CVR recording from the forward recorder could well be crucial to the investigation. |
DaveReidUK
2025-06-17T21:46:00 permalink Post: 11904696 |
That's an interesting possibility. The independent power supply for the forward recorder also powers the cockpit area microphone, but not the individual crew mikes, so working out who said what could well be dependent on being able to recognise the voices.
Subjects: CVR 3 users liked this post. |
DaveReidUK
2025-06-20T08:54:00 permalink Post: 11906737 |
Do both EAFRs run on emergency power? Could it be possible that only ONE (if any) EAFR unit was recording after the supposed loss of thrust on both engines? If the other one is severely damaged we might as well end up with NO EAFR data from the critical last part of the flight. Perhaps both units are severely damaged? I\x92m not convinced your optimism is entirely warranted.
Subjects: EAFR 7 users liked this post. |
DaveReidUK
2025-06-20T09:07:00 permalink Post: 11906749 |
Subjects: FlightRadar24 3 users liked this post. |
DaveReidUK
2025-06-20T12:44:00 permalink Post: 11906939 |
IIRC, "real-time" means downloading batches of data every 30 minutes or so - which of course is fine for EHM, not so good for accident investigation. Subjects: None 5 users liked this post. |
DaveReidUK
2025-06-21T07:37:00 permalink Post: 11907550 |
FR24 graphic vs FR24 data
The figures being bandied around for the speed profile during the airborne segment of the TOD look a bit odd.
Firstly, because there isn't actually any speed data in the FlightRadar24 download (and even if there were, the aircraft doesn't send Airborne Velocity packets at the same time as Airborne Position ones). This is a longstanding issue with FR24, and it means that any graphic showing speed at a given position isn't necessarily 100% accurate: ![]() Secondly, and assuming that FR24 has calculated GS as a second-order parameter, rather than a transmitted value, the instantaneous values still don't quite match the data in the download. It's easy to see that by correlating how far the aircraft has progressed against the data timestamps. Charting the remaining distance to the end of the runway against an arbitrary timescale starting from the first of the 8 data points looks like this: ![]() Obviously the slope/gradient of the blue line represents the average GS between successive points. The yellow reference line corresponds to a GS of 180 kts (ignore the offset, just use the slope for comparison). Yes, the aircraft had clearly slowed down after rotation, but the final two data points appear to show that it had stopped decelerating by the time the transponder stopped sending. One wonders how FR24 arrived at its groundspeed values? Subjects: FlightRadar24 4 users liked this post. |
DaveReidUK
2025-06-21T14:58:00 permalink Post: 11907818 |
All are readily worked around, after which what's left is the same data that underpins many of today's ATC systems. Subjects: FlightRadar24 4 users liked this post. |
DaveReidUK
2025-06-21T18:21:00 permalink Post: 11907963 |
I have no idea if he actually knew how much fuel was on board, or whether he'd simply been told it was "full" and somebody had looked up the capacity (126k litres) and he then quoted that "full" number. Or whether, in fact, there was an excess of fuel. But since that seems so far the only public statement on fuel load, it shouldn't just be dismissed out of hand.
Subjects: None 3 users liked this post. |
DaveReidUK
2025-06-22T11:25:00 permalink Post: 11908461 |
Subjects: AAIB (All) AAIB (IDGA) CVR EAFR FDR 4 users liked this post. |
DaveReidUK
2025-06-22T13:14:00 permalink Post: 11908532 |
That aside, I think we're agreed that downloading an intact FDR/EAFR is probably several orders of magnitude easier than one that's been burnt, battered or bruised. |
DaveReidUK
2025-06-28T07:27:00 permalink Post: 11912371 |
I don't believe it's absolutely confirmed yet but earlier posts (thank you
V1... Ooops
et al
) indicated that the unit in question may be a GE Aviation Model 3254F,
the document here
gives some good detail, along with
another
doc from Skybrary that has some relevant information..
|
DaveReidUK
2025-06-28T19:10:00 permalink Post: 11912632 |
However you are correct in that the requirements only specify that the CVR functions and the CAM must continue to operate. |
DaveReidUK
2025-06-30T15:36:00 permalink Post: 11913705 |
Subjects: None 1 user liked this post. |
DaveReidUK
2025-06-30T16:31:00 permalink Post: 11913750 |
Subjects: Self Proclaimed Experts 9 users liked this post. |