It looks like you're using an Ad Blocker.
Please white-list or disable AboveTopSecret.com in your ad-blocking tool.
Thank you.
Some features of ATS will be disabled while you continue to use an ad-blocker.
Zaphod58
reply to post by luxordelphi
Boeing has worked with composites for years prior to the 787. The military has used composites in stealth aircraft without any problems for decades.
But suddenly they have no idea what they're doing. It's amazing how that eureka
ownbestenemy
luxordelphi
Unbelievable. So you're telling this person that if the rudder falls off, the engines will too? My question is legit because I didn't know about the engine falling till the other poster said it. Is it like "hip bone connected to the thigh bone"? or...are you saying there was a vortex? Please explain.
How is that unbelievable? The stress applied to the engine mounts is tested for "normal" flight; take-off, level flight, and landing; not abnormal flight such as an aircraft losing a vertical stabilizer (the tail fin) and going into a flat-spin.
They may or may not come off in the event that an aircraft loses its complete vertical stabilizer, but it isn't a stretch that the mounts would fail under such stress.
The FAA proposes to adopt a new airworthiness directive (AD) for GE CF6-80C2 series turbofan engines. This proposed AD would require replacing certain installed part number (P/N) and serial number (SN) cast titanium weld-repaired forward engine mount platforms and cast titanium forward mount yokes, with a forged titanium or a non-welded cast titanium part. This proposed AD results from the discovery of cracks, in a weld-repaired area on a forward engine mount platform and a forward engine mount yoke, found during a fluorescent penetrant inspection (FPI). These parts were weld-repaired during manufacture. We are proposing this AD to prevent cracks in the forward engine mount platform and forward engine mount yoke that could result in possible separation of the engine from the airplane.
You acknowledge that you have no experience, and then sit there and basically act like an expert going on about things you don't know about. So yes, I'm going to respond like that to someone that says that, and acts like that.
As for the tail delamination, delamination would have no relation to the tail separating. The tail separated due to the bolt holes (which were made out of aluminum, not composites) failing, due to stress applied to the tail.
Zaphod58
reply to post by Mikeultra
There was one battery fire. Nothing is hidden. It was Japan in Boston.
With the reliability, and efficiency of new engines, it doesn't make sense to build four engine aircraft anymore. The -135 in question would have landed on one engine, had it been a twin engined aircraft, with modern engines.
Zaphod58
reply to post by Mikeultra
And you're an expert now? The tail was ALWAYS going to have to be removed, because of how close to the leading edge the damage was.
Zaphod58
reply to post by Mikeultra
I didn't see anything that said they didn't plan on removing the tail. There is no way to put any kind of repair in place with it on. The repair will have to go right up to the leading edge of the tail.