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UPDATED: Boeing says wing box fix won't affect first flight

Boeing just issued the following statement about the center wing box problem on the 787.

It is a normal part of the development of a new airplane to discover
need for improvements, and that is what we are experiencing on the 787.
The robust test process in place on the 787 program has confirmed the
majority of our designs but we have found the need for some
improvements.

The center wing box issue has been addressed. The fix is being installed
on Airplanes 1-6 in the Everett factory. Installations have begun on the
four airplanes currently in Final Assembly. All airplanes after
Airplane 7 will have the solution incorporated from the beginning.

The fundamental technologies being used on the 787 are proving to be
reliable and effective. The material choices and manufacturing
techniques for the airplane are sound.

Boeing is working its normal processes for developing a new airplane.
The test process is working when issues are discovered and we are
reacting appropriately by implementing normal design validation and
fixes when we find issues.

Also, Jon Ostrower of Flight International, who posts under flightblogger, has a detailed account of the wing box problem, based on information from his sources.

He writes that there is the potential for premature buckling in the structural spars in the massive wing box, in part because of the 787 weight gains.
Stiffeners will be needed to fix the problem, he reports.

During the initial development phase of the center wing box, the structural spars were designed to the appropriate width to support the required structural loads.

The original design for the center wing box was changed when the weight of the Dreamliner began to increase. The structural spars, which are made of composite, were reduced in width as a weight saving measure.

Boeing and Fuji Heavy Industries manufactured composite test pieces to demonstrate the structural capabilities of the spars. Findings indicated that the composite spars were buckling prematurely compared to metal spars of the same width.

This is the story I filed Thursday about ILFC's Steven Udvar-Hazy's comments about problems with the center wing box and Boeing's response.

UPDATE: Boeing tells me the wing box issue WILL NOT affect power on or first flight, contradicting what Hazy said.

But that does not mean those major milestones will not be further delayed for other reasons.

Here is my report, which will be posted on the P-I Web site shortly:

By James Wallace
P-I aerospace reporter

In trying to shave pounds on the overweight 787 Dreamliner, The Boeing Co. ended up with a costly structural issue – but one it says is being fixed.

A day after published reports that a key 787 customer said the program faced more delays of as much as six months because of structural problems in a critical area of the wings, Boeing said the issue is being resolved.

The problem involves the center wing box, which is where the wings are attached to the fuselage. It also holds fuel.

Engineers have figured out a fix and it will be accomplished on six test flight planes by Boeing workers at the Everett plant, the company said.

Starting with the first planes that are delivered to customers, Boeing said, the redesign will be incorporated into the center wing box before that structure leaves the Fuji factory in Japan.

The wing box issue, Boeing said, will not affect two critical 787 milestones – "power on" and first flight.

But Boeing will not say if those two events may be delayed by production and supply chain issues that have slowed work on the first 787 at the Everett plant and resulted in delays that already stretch about nine months.

The wing box issue, sources confirmed, involves the spars that provide strength to the massive structure, which measures some 19 feet wide and 17.5 feet long. The skin and spars are composite.

Boeing's own 787 weight-saving efforts caused a potential problem, sources said.

Boeing has acknowledged before that the 787 is overweight. Parts have been redesigned to save weight, and different and lighter materials have been used in some cases, according to Boeing.

But in trying to shave weight from the huge wing box, the width of the spars was reduced. Subsequent testing showed the thinner spars could possible buckle under severe loads, the sources said, confirming what was first reported Thursday by Jon Ostrower of Flight International magazine, who posts as "Flightblogger.''

The spars must now be "beefed up'' the sources said.

Boeing would not comment on whether the wing box problems involved the spar. But the company did release a statement Thursday that said the center wing box issue is being fixed.

"It is a normal part of the development of a new airplane to discover need for improvements, and that is what we are experiencing on the 787,'' the statement said. "The robust test process in place on the 787 program has confirmed the majority of our designs but we have found the need for some improvements.

"The center wing box issue has been addressed. The fix is being installed on airplanes 1-6 in the Everett factory. Installations have begun on the four airplanes currently in final assembly. All airplanes after airplane 7 will have the solution incorporated from the beginning.''

The first two of six test flight planes are in final assembly at the Everett plant, as well as two planes that will be used for static and fatigue testing on the ground. It's not clear how much work is involved in making the necessary fixes to the center wing box in those planes in final assembly.

But Yvonne Leach, chief 787 spokeswoman, said the wing box issue "is not a pacing item'' for either power on or first flight.

Boeing is expected to update media and industry analysts about the status of the 787 program in early April, after it completes an on-going review with its partners. That overall program assessment includes the flight test and delivery schedules.

Boeing has already announced two delays for the 787 totaling about nine months. In its last program update in January, Boeing said it hoped to have "power on" around the end of the first quarter and first flight by the end of June or early July. Deliveries would begin in early 2009, Boeing said at the time.

First flight was to have originally occurred around the end of August 2007, with the first plane delivered to launch customer All Nippon Airways of Japan in May of this year.

Some industry analysts are expecting Boeing to announce yet another delay when executives give the 787 update next month.

Earlier this week, Steven Udvar-Hazy, chairman of International Lease Finance Corp. told a JPMorgan aviation conference in New York that he believes the 787 will be delayed as much as six more months. He cited the structural issue with the center wing box as driving the delay. Hazy told the conference "power on" and first flight are likely to be further delayed, with first deliveries slipping to the end of the third quarter of 2009.

Boeing has nearly 900 orders for the 787, which will be the first large commercial jetliner with a composite airframe.

In its statement Thursday, Boeing said the "fundamental technologies being used on the 787 are proving to be reliable and effective. The material choices and manufacturing techniques for the airplane are sound.''

ILFC has ordered 74 Dreamliners and Hazy has said he is in talks with Boeing for 26 more.

In an e-mailed statement Thursday to Commercial Aviation Online, Hazy said the 787 "will turn out to be a good aircraft.''

He added that "ILFC plans to keep its 74 orders firm
and we are having a careful review later this year to see if ILFC needs to order more 787s to meet airline customer lease demand.''

Posted by at March 20, 2008 10:56 a.m.
Categories: ,
Comments
#110041

Posted by unregistered user at 3/20/08 11:39 a.m.

Boeings inexperience of using composites has already started to show.

#110046

Posted by unregistered user at 3/20/08 11:49 a.m.

Normal teething problems of a new aircraft. The 747 had a much more serious problem with its wing and still became the great plane it is today.

#110047

Posted by captbob at 3/20/08 11:49 a.m.

And Airbus's inexperience with wings required the modifications to the A380 wing?

#110053

Posted by unregistered user at 3/20/08 11:58 a.m.

#110047 may sit back and drink his warm beers and spout nonsense.

Airbus has had a lot of issues with its aircraft. This can be called inexperience when you are producing something new. It happens to all plane makers. If there were no issues then you have simply built an existing design.

#110055

Posted by unregistered user at 3/20/08 12:00 p.m.

Unfortuntally, the center wing box is the structural centerstone of the A/C. A structural update of the wing box of an assembled A/C is extremely challenging at best since the fuselage and wings are already attached to it and it is hardly accessible.
Furthermore, the added weight will have a snowball effect on other components, making the whole A/C heavier. This obviously cuts into range and fuel efficiency, and the spec performance sold (not just promised) to the customer could be effected. So either the A/C spec had some serious back-up from the start (which is highly doubtful) or Boeing will not just have to explain the 3rd delay to the customer.
Never forget: an airline doesn't buy a specific A/C, it buys a promised commercial performance (payload/range).

#110058

Posted by unregistered user at 3/20/08 12:02 p.m.

Airbus's inexperience with wings? Since the B777 Airbus has built A321, A340-600, A380 and A400M wings, that's alot of inexperience.

#110063

Posted by captbob at 3/20/08 12:06 p.m.

But the thing is, the A380 was nothing new. It was just a bigger airplane. Basic things like wing loading should not be a surprise.

#110065

Posted by captbob at 3/20/08 12:08 p.m.

To #110058. What I am saying is that when the A380 wings went into fatigue testing, they failed a lower value then expected, thus requiring a modification.

#110066

Posted by unregistered user at 3/20/08 12:09 p.m.

The B747's problem wasn't found this early though. I find it difficult to believe that this requires strengthening before first flight, it must be pretty serious. These sorts of things are usually found during flight testing, fatigue testing and static load testing, guess those problems are yet to be found.Strengthening composites is sure going to cost in weight.

#110086

Posted by unregistered user at 3/20/08 12:45 p.m.

It's obvious you no nothing about Boeing and it's experience with composites! Nope, they don't use composites in military or commercial, do they. Back in the 60s they didn't have the software to find it early, that's why it took until flight test.

#110107

Posted by captbob at 3/20/08 1:10 p.m.

I guess my sarcastic remark was directed at #110041 where it was stated that Boeing experience with composites caused a problem. My statement was that even with years of exerience with wing design and construction, the A380 wing required modification.

#110108

Posted by captbob at 3/20/08 1:13 p.m.

And to #110053. I like my beer cold and served like the Germans do. But that does not mean I am German.

#110117

Posted by unregistered user at 3/20/08 1:30 p.m.

This is bad, very bad.
They are quickly becoming victims of the advanced composite technology.
The FAA/EASA Acceptable Means of Compliance is very clear on this; geometric changes means new physical testing.
No FEA is acceptable this time since there is no history of similar components that can demonstrate compliance.
The same goes for material changes.

#110139

Posted by unregistered user at 3/20/08 2:02 p.m.

Hey, the A380 was pretty much optimised for weight if it went just under the requied 1.5 limit loads, those guys at Airbus UK deserve credit for that.

#110162

Posted by unregistered user at 3/20/08 2:25 p.m.

Huh? The A380 max pax specs were reduced due to its obesity problem. The A380 is a big fat load.

#110167

Posted by unregistered user at 3/20/08 2:36 p.m.

Posted by captbob at 3/20/08 12:06 p.m.

But the thing is, the A380 was nothing new. It was just a bigger airplane. Basic things like wing loading should not be a surprise.

Both the A3456 and the A380 employ composite centre wingbox

#110207

Posted by unregistered user at 3/20/08 3:39 p.m.

This has nothing to do with composite unexperience. This has everything to do with the trust we - and the clients - can have in Boeing. AFAIK, this is not an issue they just discovered (THAT would be frightening). But they've been hiding it, using "fasteners/supply chain" excuses for months, until the minute it began to appear in unofficial sources . Now, we can raise a question about any single potential issue: wiring, wing box, horizontal stab, weight... Are they telling the truth ? No. As I client, I wouldn't cancel my order. But just like some airlines did for the A380, I would send my own technical experts to have a reliable assessment of what's going on in Everett.

#110260

Posted by unregistered user at 3/20/08 5:42 p.m.

I've said it before, and I'll say it again, by the time this 787 is flight tested. Airbus will only be six months behind on their own flight test. This 787 in its current iteration is not air-worthy. It will take another year or two for redesign before they can finally feel confident in one.

#110262

Posted by unregistered user at 3/20/08 5:46 p.m.

Boeing should be sued for Fraud. It is fraudulent to sell products with a promised delivery date, when they know for a fact they would not meet them. They were merely racking up orders, so that investors would pump in the money, so they can continue on this charade of lies.

#110318

Posted by unregistered user at 3/20/08 9:57 p.m.

Significant weight savings are possible.
For example, the fuselage sections did not fail at 250% of ultimate strength, although there were some fiber failures.
Aircraft structures must survive 150% of ultimate strength.
The A380 wing did not survive 150% of ultimate strength and needed to be strengthened.

#110335

Posted by unregistered user at 3/20/08 11:14 p.m.

The A380 max pax specs were reduced due to its obesity problem

Nonsense. The pax spec was reduced in exchange for 200 nm more range. The underlying payload range curve did not shift by one iota.

#110456

Posted by unregistered user at 3/21/08 10:55 a.m.

The DC8's wings were redesigned during development. They're still flying cargo.

As a passenger on Boeing's products I've always been disappointed by the flappy wings and mimimal lateral stability. Flew in a 747 across the pond that acted
more like a cross between a wallowing whale and a swan than an aeroplane.
I understand that it's a design choice that works for
longer life, but............are there more DC8's or more
707's flying today?

The most passenger friendly configuration, (717) didn't please Boeing and they discontinued it.

I was born with the wrong preferences.

Bob

#110755

Posted by unregistered user at 3/22/08 8:31 a.m.

Just to set the record staright, the 747 had major wing problems before it ever flew. This got corrected after much handwringing and accusations - like today on the 787. The wing box problem is not a big deal on the 787. It's being corrected as we speak.

#110764

Posted by unregistered user at 3/22/08 9:06 a.m.

I think that it is extremely unlikely that Airbus will have the A350 ready for it's first flight within a year of the 787's. That would be a superhuman effort-and what makes you think that Airbus may not have some problems in their development program? I think Boeing is much more likely to have troubles with their supply chain of subcontractors than this wing box issue. One final thing: if Boeing can pull off the 787, with it's revolutionary technology advances, they could then either concentrate on the single aisle class or the 380 class-would anybody buy a 380 if they could get a composite ac with 20% better efficiency and all the other benefits of the new tech? The 380 is the last of it's era-like the last big flying boat, or the last big ocean liner.

#110985

Posted by unregistered user at 3/24/08 2:13 a.m.

One of the reasons the 787 is overweight is that Boeing had to add a lot of metal into the wing join to avoid the possibility of catasrophic damage in the event of a lightning strike. My question is, will the metal spar that is being used to fix the problem in planes 1 to 6 focus an electric charge in a critical part of the wing or wing box.
But don't get me wrong here. I believe Airbus has just as many problems with the A380. They made all sorts of changes to save weight, such as very-high-pressure hydraulics systems.
Quite frankly I will not fly in either plane for at least a decade. In my view, the 777 is probably the safest plane around now because it is the newest and is made of metal. 747s are ageing and we know they have problems with ageing wiring. The A340 seems to be okay but I know it has a very high wing loading.

#110991

Posted by unregistered user at 3/24/08 3:59 a.m.

quote: #110985
"They [A380] made all sorts of changes to save weight, such as very-high-pressure hydraulics systems."

The A380 had 5000psi hydraulics from the outset - a design feature shared with the 787, by the way. In case of the A380, the decision was driven by aircraft size and its impact on hydraulic fluid volume and required mass flow. Using a more common 3000psi was not an option.

#110996

Posted by unregistered user at 3/24/08 4:05 a.m.

quote: #110985
"One of the reasons the 787 is overweight is that Boeing had to add a lot of metal into the wing join to avoid the possibility of catasrophic damage in the event of a lightning strike. My question is, will the metal spar that is being used to fix the problem in planes 1 to 6 focus an electric charge in a critical part of the wing or wing box."

A lot of metal is added not INTO but on ONTO the wing. Lightning strike protection relies on expanded metal foil covering the areas where the wing skin is fastened to the internal structure, namely spars and ribs. From pictures this foil is looking decidedly reddish suggesting some aluminum/copper alloy.

There is no such think as a metal spar.

#111129

Posted by unregistered user at 3/24/08 2:12 p.m.

I've seen some examples of wiring on the Boeing 777 under the SFAR 88 requirements and they're not pretty.
I'd put Airbus miles ahead of Boeing in safety standards and question the #110985 assumption the 777 is safest. I donot fly 777 or any Boeing aircraft after what I've seen.

#111162

Posted by unregistered user at 3/24/08 4:02 p.m.

"...very-high-pressure hydraulics systems..."
Concorde has 4000psi hydraulics.
So, forty years later, I would hardly call 5000psi "vey-high-pressure....

#111239

Posted by unregistered user at 3/25/08 3:11 a.m.

110985 here again. I just booked my next o/s trip with Singapore Airlines and asked for the 777.
A couple of years ago, the A380 was 5.5 tonnes overweight; would anyone care to explain how this was remedied!
Perhaps you would also like to look up the Mangan whistleblower case concerning a faulty microprocessor.
Also there is the matter of the use of aluminium rather than copper wiring. Aluminium is brittle and will not last. Anything to save weight!!!
Then there was the last minute need to reinforce section 19 - the aft cone of the fuselage (July 2006).
How much more don't we know about.
The aluminium wiring is the biggie. In a few short years it will develop fatigue cracks and will cost the airlines a fortune to replace. Considering how airlines treat problems they don't want to know about, if there is no FAA order to fix the problem, a lot of people will be at risk every time an A380 takes to the air.
When I booked my SIA flight I specifically asked for the 777 and specifically said that I did not want to fly the A380.

#111245

Posted by unregistered user at 3/25/08 4:08 a.m.

To #111239 "When I booked my SIA flight I specifically asked for the 777 and specifically said that I did not want to fly the A380." Book it if you prefer it but thinking about last 777 not clarifed accidents (Heathrow and Arabia) I would think twice before....

#111258

Posted by unregistered user at 3/25/08 5:47 a.m.

Boeing are useless at designing composites in a HCF environment.
B1 is basically worthless, airbus on the other hand has over 3 decades of composite airliner experience

#111259

Posted by unregistered user at 3/25/08 5:53 a.m.

Well I've seen wiring installations on the B777 for fuel pumps installed against sharp structure within the Fuel tanks. One trodden maintanence foot away from an ignition. Not good design.

#111317

Posted by unregistered user at 3/25/08 11:15 a.m.

#111259:
I don't know about the 777, but I just spent a couple of days staring at the inside of a 727 fuel tank-30 years older and I didn't see any "shocking" wiring installation problems. Also, I have trouble understanding why anyone would put aluminum wiring in an aircraft-I sure hope that it is a new space age type that doesn't have all the problems of older aluminum wiring. I wouldn't even put aluminum wiring in my house.

#111535

Posted by unregistered user at 3/26/08 3:18 a.m.

Aluminium wires are not allowed outside of pressurized area

#111729

Posted by unregistered user at 3/26/08 1:56 p.m.

727???? All that high voltage wiring running through the fuel tanks??? you're joking, definately wouldn't fly on that dinaoaur!

#113075

Posted by unregistered user at 3/30/08 3:32 p.m.

For all the folks that like playing down the A380; it contains more composites then the 787, among others, an enormous CRFP central wingbox that doesn't buckle.

#114815

Posted by unregistered user at 4/4/08 8:04 p.m.

captbob wrote: "But the thing is, the A380 was nothing new. It was just a bigger airplane."

I think we all should fly with just a bigger version of Orville and Wilbur Wrights airplane. Nothing new since then, right?

#122940

Posted by unregistered user at 4/29/08 2:33 a.m.

The A380 is a marvelous aircraft, performing better then promised, contains lots of innovations and composites. It burn less per passneger then anything and most worldwide flag carriers (re)ordered it. In future versions will dominate the skies above the oceans.

Stop the sour grapes, cool down & enjoy your flight.

www.youtube.com/watch?v=hxeKmiFudFg

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