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CONSO
22nd Apr 2016, 23:25
FAA Orders ?Urgent? 787 Repair After Engine Fails at 20,000 Feet - Bloomberg (http://www.bloomberg.com/news/articles/2016-04-22/repairs-to-ge-engines-ordered-after-dreamliner-in-flight-damage)



FAA says pilots need updated instructions within seven days
New version of General Electric's GEnx-1B engines prone to ice


Airlines flying Boeing Co.’s 787 Dreamliner jets with the latest General Electric Co. engines were ordered to repair them, or swap out at least one with an older model, in an urgent safety directive issued after an in-flight failure.
A GEnx-1B PIP2, part of a family of engines plagued by issues related to icing, suffered “substantial damage” in the Jan. 29 incident, when ice on the fan blades broke loose, the U.S. Federal Aviation Administration said in an order published Friday in the Federal Register.
“The potential for common cause failure of both engines in flight is an urgent safety issue,” the FAA said in its order.
The GEnx, a high-efficiency engine developed for wide-body aircraft, has faced earlier issues with icing. In 2013, the FAA ordered (http://www.bloomberg.com/news/articles/2013-11-26/boeing-787-engines-ice-risk-spurs-faa-to-warn-airlines) airlines to avoid flying 787 and 747-8 planes equipped with the GE engines near thunderstorms in high-altitude cruise flight. Even in those sub-freezing temperatures, moisture from the storms could enter the engines and form dangerous ice, the FAA said.

G0ULI
23rd Apr 2016, 01:51
I can't decide which is more disturbing.

A modern engine design not being able to cope with ice, or the commercial pressures driving pilots to routinely fly through areas of known thunderstorm activity.

lomapaseo
23rd Apr 2016, 02:14
A modern engine design not being able to cope with ice, or the commercial pressures driving pilots to routinely fly through areas of known thunderstorm activity.

Where did you get this thunderstorm activity from? ... I couldn't read it having anything to do with the AD.

any 787 pilots care to comment?

G0ULI
23rd Apr 2016, 02:54
Iomapaseo
The Air Directive orders airlines to avoid flying near thunderstorms in high-altitude cruise flight, which rather suggests that this was/is a routine activity. Lines 10 and 11 of the originally posted extract. Just my interpretation based on two crashes that could be directly linked to airliners flying into thunderstorms in the ITCZ, neither of which were 787s or 747-8s though.

tdracer
23rd Apr 2016, 04:06
The specific issue in question has nothing to do with high altitude Ice Crystal Icing (which the GEnx has also had issues with).

Rather, this particular issue is related to the more conventional icing threat (i.e. super cooled droplets) that forms ice on the fan blades at low power. Based on what is currently known, it only applies to one 'version' of the GEnx-1B engine. No known impact on the GEnx-2B (747-8) or the earlier versions of the -1B on the 787.

CONSO
23rd Apr 2016, 04:42
A bit more on the FAA and the problem on GE Engines

FAA orders urgent fix to engines that could shut down on Boeing 787s | The Seattle Times (http://www.seattletimes.com/business/boeing-aerospace/faa-orders-engine-fix-on-176-boeing-787s/)

The FAA directive (http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgad.nsf/0/c72a6b102f851f2886257f9d0049d985/$FILE/2016-08-12.pdf), first reported Friday by The Wall Street Journal, states that the problem arises only in the latest upgraded model of the GEnx engine powering the Dreamliner, the GEnx-1B PIP2.
That upgrade, which was certified by the FAA and entered service in 2013, improved the fuel burn incrementally, in part by reducing the tiny gap between the tips of the engine’s large fan blades and the fan case.
In the January incident, ice had built up on the fan blades before the trouble occurred at an altitude of 20,000 feet as the plane descended.
When the ice abruptly shed, it caused the blades to move slightly forward and because of the contour of the fan case, this was enough to make the blade tips rub against the case.
The resultant heavy vibrations did so much damage that the engine shut down and could not be restarted.
Luckily, the GEnx engine on the other wing of the JAL Dreamliner was older and not the specific upgraded PIP2 design. The FAA directive says that second engine incurred only “minor damage during the icing event and continued to operate normally.”


A side note. Many many years ago when the 787 was just starting preliminary design and concepts, the management was beginning to look for the cheapest way to do things with minimum $$$$$ outof pocket. A very logical ' beancounter' power point ranger had prettty well sold the idea of a choice of a Single engine manufacturer via competition, yada yada. A very good friend of mine who was well respected in the company despite being a ' simple' Engineer albeit with many hours of military and commercial flight, delivery, and training hours going back to Kc-135 tankers made his views on that very well known- that it was to big a risk for a variety of reasons.
Suggested that two engines be chosen from the then 3 major manufacturers- and that a common interface/mounting be designed so it would be a near plug and play issue.



As a senior official later said about him -" We never had a problem diagramming his sentences "

And so it goes . . .

Mark in CA
23rd Apr 2016, 18:33
According to an AFP (news agency) report today:

GE recommended the repairs last month, the FAA statement Friday said, and Boeing and GE have been working on the issue for months, with more than 40 Dreamliner engines fixed so far, reports say.

The repairs -- involving grinding down engine casings -- can be done without removing the engines from planes.

The FAA order also requires that pilots be alerted to new operating procedures for coping with possible icing problems at low altitude.

zetec2
23rd Apr 2016, 20:27
Similar to the old "centre line closure" problem that we had with the Sapphire although now at the front as opposed to in the compressor.

Bond'll Do
23rd Apr 2016, 21:23
100 nm minimum avoidance around ITCZ -type weather has held me well over the last 40 yrs.

New engines are just being tested in-service. That will always be the case now.

Just avoid the weather.....what trainer ever told you to leave less than 100nm from severe weather? (in commercial pax a/c?). WTF?

Sqwak7700
23rd Apr 2016, 22:23
100 nm minimum avoidance around ITCZ -type weather has held me well over the last 40 yrs.

Wtf? 100 nm? Yeah, no. Never heard of that one. Never in over 20 years flying tubes have I heard anyone diverting 100nm around weather.

TURIN
23rd Apr 2016, 23:13
The specific issue in question has nothing to do with high altitude Ice Crystal Icing (which the GEnx has also had issues with).

Rather, this particular issue is related to the more conventional icing threat (i.e. super cooled droplets) that forms ice on the fan blades at low power. Based on what is currently known, it only applies to one 'version' of the GEnx-1B engine. No known impact on the GEnx-2B (747-8) or the earlier versions of the -1B on the 787.

What version is fitted to the 787-9?

olasek
24th Apr 2016, 01:30
A modern engine design not being able to cope with ice,
This is really a silly comment, ice has always been and will always remain a permanent challenge in aviation, regardless of how state of the art equipment is. Sometimes subtle changes to engine (pitot tubes, etc, etc.) design can introduce unwanted icing side effects, often it is impossible to predict it just based on theoretical modelling and ground or in-flight testing only covers most nominal scenarios.

qld330
24th Apr 2016, 02:12
100 nm minimum avoidance around ITCZ -type weather has held me well over the last 40 yrs.

New engines are just being tested in-service. That will always be the case now.

Just avoid the weather.....what trainer ever told you to leave less than 100nm from severe weather? (in commercial pax a/c?). WTF?
Try and get 100NM wx deviation in China

lomapaseo
24th Apr 2016, 02:19
A modern engine design not being able to cope with ice,

This is really a silly comment, ice has always been and will always remain a permanent challenge in aviation, regardless of how state of the art equipment is. Sometimes subtle changes to engine (pitot tubes, etc, etc.) design can introduce unwanted icing side effects, often it is impossible to predict it just based on theoretical modelling and ground or in-flight testing only covers most nominal scenarios.


This reads OK if the modifier is :"too much ice...."

After all we do have regulations, that if met, will provide a significant measure of protection. It would appear that this latest problem had to add a crutch fix to finally meet the desired level of safety. If the problem was too much ice, not anticipated in the development and certification, then all models of all engines would have to address the issue at the same time since they all fly at these altitudes 0-20000 ft

porterhouse
24th Apr 2016, 02:31
It isn't "too much ice", its is way more subtle then that, it is ice taking advantage of insufficient gaps in the modified engine to start to form.. and what was the reason for the engine modification - improved fuel economy so clearly we have trade-off here between engine fuel efficiency and its resistance to ice. We will have problems like that in the foreseeable future unless all aircraft engine development ceases.

tdracer
24th Apr 2016, 04:49
What version is fitted to the 787-9?
I don't work the 787, so I'm not as intimately familiar as I am with the 747, but the GEnx-1B "PIP 2" certified over 2 years ago. So I suspect most if not all GE 787's delivered in the last 2 years were delivered with PIP 2 engines. However GEnx-1B engines can be freely interchanged so what a 787 was delivered with and what it's flying with today may not be the same.

neila83
24th Apr 2016, 21:29
Wtf? 100 nm? Yeah, no. Never heard of that one. Never in over 20 years flying tubes have I heard anyone diverting 100nm around weather.

Indeed, I used to live in Fiji and that's more than the width of the main island! And for sure while a storm was raging on one side, it'd be heavy blue skies on the other half.

Weather avoidance is something that fascinates me, partly because turbulence turns me from a lover of flight to borderline panic attacks, and partly from a lifelong interest in meteorology. And I seem to read so many different mentalities regarding it. Personally I'd prefer the pilot stayed as far away as possible because any turbulence does cause a lot of fear at the back, and I feel if you're transporting passengers you shouldn't enter areas you're not comfortable with.

Sorry if this isba little off topic, but I'd be interested to hear your general strategies? And how much are you considering the commercial side i.e. do you fly in areas you'd rather not if the deviation would be 'too far'? And what is too far? Personally I'm inclined to think paying passengers have a right to think the pilot should be free to take all avoidance he deems necessary. Do you feel some colleagues are 'too brave'?

I also occasionally read here about poor radar technique being common, but I tell myself it can't be that bad or we'd be seeing a lot of incidents in SE Asia with the number of flights dodging around the monsters down there!

Metro man
24th Apr 2016, 23:28
Wasn't there something similar with the BAE 146 back in the 1990s ?

4runner
25th Apr 2016, 06:44
I can't decide which is more disturbing.

A modern engine design not being able to cope with ice, or the commercial pressures driving pilots to routinely fly through areas of known thunderstorm activity.

Evil companies making aircraft fly around where there might be storms....🙄. I heard that in some places, aircraft have to fly in snow and ice😦. And one time, I heard an aircraft was asked to fly with a deferred APU☹️.

TURIN
25th Apr 2016, 09:34
I don't work the 787, so I'm not as intimately familiar as I am with the 747, but the GEnx-1B "PIP 2" certified over 2 years ago. So I suspect most if not all GE 787's delivered in the last 2 years were delivered with PIP 2 engines. However GEnx-1B engines can be freely interchanged so what a 787 was delivered with and what it's flying with today may not be the same.

Fair point TDRacer.

I only ask because very recently I saw a brand new 787-9 with this exact problem. Not something i had seen on previous older -8 models.

WingNut60
26th Apr 2016, 00:04
Can anyone out there shed some insight into the implications for ETOPS certification while this sort of directive is in place?

lomapaseo
26th Apr 2016, 02:13
ETOPS shouldn't be at risk since this is a problem in the approach phase at low powers.

KRviator
26th Apr 2016, 08:45
Let's hope they don't have a depressurisation or other issue requiring an emergency descent then...

Basil
26th Apr 2016, 08:51
Try and get 100NM wx deviation in China
JDI!
When we did, the controller was going nuts esp since we crossed a national border in the process. When we changed freq there was a tacit understanding that least said soonest mended.

NWA SLF
26th Apr 2016, 14:39
GE is responsible for the engine - the problem is fan to cowl clearance, an engineering screw up as the information states that fuel efficiency will not be reduced - adequate blade tip clearance with the front edge insufficient. Engine installation - is that a Boeing task (I refer to the cowling design) or is that part of the engine package and totally GE's design? I presume increasing the clearance by grinding involves more than a crew of mechanics with Dremel grinders, which would really be cool watching from the window of your flight as you have loaded first in First Class and are able to look back at mechanics making the final touches before your plane is pushed back.

lomapaseo
26th Apr 2016, 17:53
That which is touched directly under the fan blades, belongs to GE under the FARs.

From my read of the AD I'm not aware of installation effects under other parts of the FARs

barit1
27th Apr 2016, 02:16
NWA SLF:the problem is fan to cowl clearance

No - the clearance in question is between blade tips and the engine casings, GE parts, which are quite different from, and housed within the external Boeing cowl. :hmm:

pattern_is_full
27th Apr 2016, 03:50
This is what GE delivers to Boeing - black and "green" casing already installed around the fan, by GE.

http://www.geaviation.com/engines/img/thumb-genx.jpg

oliver2002
29th Apr 2016, 15:38
100 nm minimum avoidance around ITCZ -type weather has held me well over the last 40 yrs.

New engines are just being tested in-service. That will always be the case now.

Just avoid the weather.....what trainer ever told you to leave less than 100nm from severe weather? (in commercial pax a/c?). WTF?

I see. That may be possible in cruise (in sparsely populated airspace), but please tell me how you accomplish that when leaving cruise and descending below 20000ft on your way to an airfield like Singapore?