Qantas keeps A380s grounded over engine 'anomalies'
google.com
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Or is this just a bug to work out with a new aircraft and engine design? Or is it just random chance?
(Also, it's odd to blame Rolls-Royce for the failures, when the engines are both owned and maintained by Qantas in Singapore.)
I'd say it's much more likely that there's some bug in the A380 RR engine than Qantas doing a maintenance job crappy enough to cause a 2 year old engine suffer such a catastrophic failure. You should be able to do the shoddiest maintenance job in the world and not have an engine fail in a way that causes the wing to be pierced.
I think this is the bit that is more worrisome than any possible maintenance issues. Jet engines have lots of turbine blades spinning at hellacious rpms. The one catastrophic failure that modern engines are supposed to be designed to prevent is having the blades leave the cowling; this is the sort of failure mode that can result in the failure of a single engine taking an entire plane down (c.f. UAL 232). This is not supposed to happen on modern engines. Ever
With engines this young, you would have to look at design factors to at least check there is no problem. That's why Qantas has grounded the fleet. Remember, Qantas is the oldest airline to have never suffered a fatality. It's part of their brand equity, and I don't think they want to change that anytime soon.
One Qantas flight was even shot down by the Japanese in 1942!
(Apologies for the pedantry)
[1] http://en.wikipedia.org/wiki/List_of_Qantas_fatal_accidents
"This is an engine issue and the engines have been maintained by Rolls-Royce since they were installed on the aircraft..."[1]
[1] http://www.adelaidenow.com.au/plane-reportedly-qantas-sheds-...
[2] http://www.abc.net.au/news/stories/2010/11/05/3057785.htm
I'm making a mental note to only fly on planes with GE engines from now on :)
"3) The FOHE, although compliant with the applicable certification requirements, was shown to be susceptible to restriction when presented with soft ice in a high concentration, with a fuel temperature that is below -10°C and a fuel flow above flight idle.
4) Certification requirements, with which the aircraft and engine fuel systems had to comply, did not take account of this phenomenon as the risk was unrecognised at that time."
Well, yeah, that's why they blew up!
:)