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WholaLottaLove wrote:As per Bloomberg:
"U.K. engine maker’s initial analysis of Iberia A350 in-flight turbine shutdown was due to an issue with the engine’s control system; this is now being addressed, Rolls-Royce says in emailed statement.
- Inspections showed no damage to engine core, confirms no connection between incident on Iberia flight and Trent 1000 problems on 787 aircraft
- Rolls-Royce says it’s supporting plane’s return to service"
Hence, much ado about nothing.
lightsaber wrote:WholaLottaLove wrote:As per Bloomberg:
"U.K. engine maker’s initial analysis of Iberia A350 in-flight turbine shutdown was due to an issue with the engine’s control system; this is now being addressed, Rolls-Royce says in emailed statement.
- Inspections showed no damage to engine core, confirms no connection between incident on Iberia flight and Trent 1000 problems on 787 aircraft
- Rolls-Royce says it’s supporting plane’s return to service"
Hence, much ado about nothing.
Actually, still an issue. The engine control system is so vague it could be:
Actuator
Linkage
Valve
Software
Bad/damaged harness
FADAQ hardware failure
I listed from least to most concerning.
I like specific answers as they show a root cause finding. This reply is too vague.
Lightsaber
Dalmd88 wrote:As for the IB A350 in BOS. I heard it was a auto rollback shutdown. The Trent family has lots of built in protections. If the engine sees certain faults it will auto shutdown to prevent damage. A vibe problem is one possible example. Delta shipped up the engine change kit this week in the event of an engine change. As of Friday I had not heard any updated info.
lightsaber wrote:WholaLottaLove wrote:As per Bloomberg:
"U.K. engine maker’s initial analysis of Iberia A350 in-flight turbine shutdown was due to an issue with the engine’s control system; this is now being addressed, Rolls-Royce says in emailed statement.
- Inspections showed no damage to engine core, confirms no connection between incident on Iberia flight and Trent 1000 problems on 787 aircraft
- Rolls-Royce says it’s supporting plane’s return to service"
Hence, much ado about nothing.
Actually, still an issue. The engine control system is so vague it could be:
Actuator
Linkage
Valve
Software
Bad/damaged harness
FADAQ hardware failure
I listed from least to most concerning.
I like specific answers as they show a root cause finding. This reply is too vague.
Lightsaber
Peterwk146 wrote:lightsaber wrote:WholaLottaLove wrote:As per Bloomberg:
Lightsaber
Actually, Rolls-Royce doesn't have to provide any information to you. It's theirs, Airbus and Iberia's business, not your's so they don't have to supply you with a root cause.analysis.
Ruscoe wrote:Just a couple of AD's from EASA over the years relating to the XWB.
15/4/16 - ...Thrust Reverser Actuation system replacement...
30/5/17 - cracking on several intermediate pressure turbine stage 2 locking plates..
21/12/16 - .... a certain population of compressor case support pins and hollow dowels have insufficient material properties......
15/5/17 - incorrect assembly of LP compressor disc to the compressor shaft...
6/9/18 - this is the canecellation date of an AD regarding an error in the EEC software.. potentially limiting thrust control ....
Overall I expected more AD's from a new engine.
Ruscoe
Ruscoe wrote:I speculate that this is not a minor problem, because if it was it would be fixed on the wing.
a350lover wrote:Is there any schedule for that A350 to return to service?
zeke wrote:Ruscoe wrote:Just a couple of AD's from EASA over the years relating to the XWB.
15/4/16 - ...Thrust Reverser Actuation system replacement...
30/5/17 - cracking on several intermediate pressure turbine stage 2 locking plates..
21/12/16 - .... a certain population of compressor case support pins and hollow dowels have insufficient material properties......
15/5/17 - incorrect assembly of LP compressor disc to the compressor shaft...
6/9/18 - this is the canecellation date of an AD regarding an error in the EEC software.. potentially limiting thrust control ....
Overall I expected more AD's from a new engine.
Ruscoe
Being such a new engine I would expect none of those to be applicable. The fixes would have been incorporated during build. The reverse actuator AD for example as far as I am aware there is not a single engine in service that applies to as they have been updated.
cat3appr50 wrote:It’s a certainty that the vast majority of airline passengers don’t give a diddly squat about RR’s share price. They are interested in getting from point A to point B safely and without worry or inconvenience. That being said, what is the specific technical root cause of this XWB shutdown? Some assert its one thing, others assert it’s another thing. Others say (and LOL over this assertion) it is nobody’s business what it was, just RR’s and Airbus’s business, taking the paying passengers right out of the equation.
It’s preposterous to think that there aren’t passengers technically savvy enough to avoid airlines and/or aircraft flying trans-Atlantic or trans-Pacific routes with a knowledge from media reports, etc. of technical engine faults causing in flight diversions, without to-date root cause(s) identified and communicated regarding same, and not hearing what’s being done to make sure it doesn’t happen again. The lack of communication on the specific root cause of this diversion incident seems deafening.
RB211trent wrote:Lack of communication?? Deafening?? Since when do inflight shutdowns warrant public statement about root cause etc within a few days? They have stated it’s a control issue, what more do you want. Did EA when they lost a fan and fancase, do we all have a detailed account of the uncontained failure of the Delta PW 2000 from the 5th Sept........I don’t think so.
BOSAero wrote:Regardless of this being an engine (RR) issue continuing from the 787 engines or an auto roll back issue, both Airbus and RR are on the hook here. They both have to investigate and provide root cause analysis to the proper authorities (FAA/EASA). Some of these reports will become public record wether they like it or not, so it’s better for them to at least have their respective PR people realease some kind of statement on the issue. Auto roll back implies there is something going on with the airplane and it’s own software simply because the engine EEC has to interphase with the aircraft software and throttle controls. My guess is that the engine is being replaced due to the amount of time the engine was windmilling from the shutdown event to the time the airplane landed in BOS. Turbine engines don’t really like windmilling for prolonged periods of time at high speeds(relatively speaking). The internal bearings on that engine might be ground to dust. Anyone care to elaborate more on this?
chrisnh wrote:On the BOS Spotters FB Page there are photos of it in the DL hangar. They backed it in, and it just barely fits.
pabloeing wrote:chrisnh wrote:On the BOS Spotters FB Page there are photos of it in the DL hangar. They backed it in, and it just barely fits.
¿What is that Facebook page?
Peterwk146 wrote:BOSAero wrote:Regardless of this being an engine (RR) issue continuing from the 787 engines or an auto roll back issue, both Airbus and RR are on the hook here. They both have to investigate and provide root cause analysis to the proper authorities (FAA/EASA). Some of these reports will become public record wether they like it or not, so it’s better for them to at least have their respective PR people realease some kind of statement on the issue. Auto roll back implies there is something going on with the airplane and it’s own software simply because the engine EEC has to interphase with the aircraft software and throttle controls. My guess is that the engine is being replaced due to the amount of time the engine was windmilling from the shutdown event to the time the airplane landed in BOS. Turbine engines don’t really like windmilling for prolonged periods of time at high speeds(relatively speaking). The internal bearings on that engine might be ground to dust. Anyone care to elaborate more on this?
So who are these people clamouring for a PR statement apart from you? There's an engine shut down - OK - no different to an engine shut down on any other aircraft.
Revelation wrote:So, given https://flightaware.com/live/flight/ECMYX and ETOPS flight rules, why was BOS deemed "nearest adequate airport" rather than YHZ or elsewhere?
It would have sucked if the 2nd engine had an "auto roll back issue" over the Gulf of Maine.
Peterwk146 wrote:Revelation wrote:So, given https://flightaware.com/live/flight/ECMYX and ETOPS flight rules, why was BOS deemed "nearest adequate airport" rather than YHZ or elsewhere?
It would have sucked if the 2nd engine had an "auto roll back issue" over the Gulf of Maine.
I hadn't seen anything to say that the first engine shut down was due to an "auto roll back issue". Have I missed that or is it speculation?
Revelation wrote:So, given https://flightaware.com/live/flight/ECMYX and ETOPS flight rules, why was BOS deemed "nearest adequate airport" rather than YHZ or elsewhere?
It would have sucked if the 2nd engine had an "auto roll back issue" over the Gulf of Maine.
zeke wrote:Revelation wrote:So, given https://flightaware.com/live/flight/ECMYX and ETOPS flight rules, why was BOS deemed "nearest adequate airport" rather than YHZ or elsewhere?
It would have sucked if the 2nd engine had an "auto roll back issue" over the Gulf of Maine.
It’s nearest suitable, not nearest adequate.
What is deemed suitable is up to the crew on the day.
zeke wrote:And we do not even know for sure if it was shutdown or running at idle. Unless people here have more information....
Revelation wrote:Still would be interested in why YHZ would not be deemed suitable.
Revelation wrote:Still would be interested in why YHZ would not be deemed suitable.
AvHerald suggests they were 70nm southeast from YHX when engine was shut down. FlightAware trace looks further than that. It also said they were flying for 90 minutes from engine shutdown till landing. Maybe they knew they needed that much time to dump fuel and so BOS was more suitable than YHX. Maybe weather.
zeke wrote:The grown-ups that fly these aircraft are trained to know even an engine failure is not that big of a deal.
We do not rush the process of working out what is wrong, how to fix it, and then decide is a diversion is necessary.
A normal engine out driftdown takes the best part of an hour to go from cruise altitude down to one engine out altitude.
An airport 70 nm seems nice to you, but it really is too close. Normal top of descent would be 120 mn away, and then you would have 40 mn to set the approach up and brief it.
Add the additional items of engine out and overweight, there is no rush.
gatibosgru wrote:She flew out yesterday as far as I know