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UPDATE 3-More cracks found in Airbus A380 wings

#1
User is offline   xUT 

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UPDATE 3-More cracks found in Airbus A380 wings

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PARIS, Jan 19 (Reuters) - Airbus insisted on Thursday that Europe's A380 superjumbo is safe to fly after another set of cracks was discovered in the wings of the world's largest jetliner.

It is the second time in as many weeks that hairline cracks have surfaced inside the mammoth double-decker jet, which entered service four years ago, and their discovery is expected to lead to expanded safety checks.


Quote

Airbus has dismissed calls to ground its superjumbo fleet over the cracks, which first came to light during repairs of a Qantas Airways Ltd A380 damaged by an engine blowout shortly after taking off from Singapore in November (Stuttgart: A0Z24E - news) 2010.

Two aviation industry officials said European safety inspectors would, however, order additional safety inspections.

A spokesman for the European Aviation Safety Agency confirmed it would issue an airworthiness directive on Friday.


Let's hope it's just growing pains for a new aircraft type.
B) xUT
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#2
User is offline   eolesen 

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The AD is out.

http://news.aviation...-wing-rib-feet/


I can't recall seeing this much AD activity with an aircraft fleet that hasn't even come due for their first MBVs yet.
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#3
User is online   BoeingBoy 

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I'm a little concerned that this might be the end result of computer design. Designers and engineers can now design airplanes with very little margin over that required for certification. Gone are the days of making the planes stronger if there was any doubt. There's a story about the DC-3, which had the wings bolted together outboard of the engines using a couple of hundred bolts on each side. Supposedly there were worries among some potential customers about the strength of using bolts instead of a continuous wing spar so Donald Douglass had mechanics remove all but 3 of the bolts and flew the airplane through a set of maneuvers, erasing all doubt about the strength of the wing. Nowadays, if the computer said the dc3 needed 2.985 bolts to be strong enough, only 3 would be used instead of the hundreds Douglas put in.

Jim
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#4
User is online   chris perry 

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View Posteolesen, on 20 January 2012 - 12:48 PM, said:

The AD is out.

http://news.aviation...-wing-rib-feet/


I can't recall seeing this much AD activity with an aircraft fleet that hasn't even come due for their first MBVs yet.


We are seeing these new generation aircraft with problems only seen in 20 year old aircraft.The skins on the new gen 737 are scary
Thin...parts are breaking way premature...I see job security,or throw away aircraft.Don,t see them lasting 20 years without major maint.
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#5
User is online   tech2101 

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View PostBoeingBoy, on 20 January 2012 - 05:31 PM, said:

I'm a little concerned that this might be the end result of computer design. Designers and engineers can now design airplanes with very little margin over that required for certification. Gone are the days of making the planes stronger if there was any doubt. There's a story about the DC-3, which had the wings bolted together outboard of the engines using a couple of hundred bolts on each side. Supposedly there were worries among some potential customers about the strength of using bolts instead of a continuous wing spar so Donald Douglass had mechanics remove all but 3 of the bolts and flew the airplane through a set of maneuvers, erasing all doubt about the strength of the wing. Nowadays, if the computer said the dc3 needed 2.985 bolts to be strong enough, only 3 would be used instead of the hundreds Douglas put in.

Jim

That Douglas philosophy is what ended their business (although I agreed with the philosophy).

The DC aircraft were/are workhorses.
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#6
User is offline   delldude 

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Our old 9 fleet were always near HEAVY on check.......lotta beer cans on them fuselages....
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#7
User is offline   TWU informer 

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Makes one wonder which is more important, Fuel Economy/Light Weight or Aircraft Safety/Strength

Pushing the envelope appears to be risky.
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#8
User is offline   2ndGENAMT 

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After working the A300 for a couple of years I always thought that their aluminum was of inferior quality compared to Douglas/Boeing.. Jims point about computer design makes perfect sense in my view as well as CP's throw away aircraft..

What better way to make profits than selling customers parts for 10-15 years and at lease end a new aircraft..
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