Kev3188
Veteran
These last couple of posts have been really informative. Thanks for putting that info out there!
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In the scheme of things, does that information have any relevance to the accident investigation? The use of stolen or fake passports are a pretty common occurrence in southeast Asia.700UW said:Also being reported the two stolen passports were used by two Iranians.
700UW said:Iran=Terrorism link, possible.
cltrat said:Knot just as an example if this A/C lost total control and started to fall would sheer force rip it apart before impact or would it stay intact?
I would think it would break into several large pieces but idkdelldude said:
Depends what kind of G forces were exerted on the airframe. Every A/C has limits.
cltrat said:I would think it would break into several large pieces but idk
.The men were scheduled to connect in Beijing for flights to Europe. The police in Pattaya said the tickets were bought not by the passengers themselves but by an Iranian man known to the police only as Mr Ali
There are far to many factors involved to make that determination. No one knows if the structural integrity of the airframe was compromised during the initial upset or if a catastrophic system/s failure lead to loss of control. I would surmise that if there were no primary load bearing surface structural failures, the aircraft would remain intact during the descent until the aircraft impacted the water or land, as the case may be.cltrat said:Knot just as an example if this A/C lost total control and started to fall would sheer force rip it apart before impact or would it stay intact?
Thanks Knot.Knotbuyinit said:There are far to many factors involved to make that determination. No one knows if the structural integrity of the airframe was compromised during the initial upset or if a catastrophic system/s failure lead to loss of control. I would surmise that if there were no primary load bearing surface structural failures, the aircraft would remain intact during the descent until the aircraft impacted the water or land, as the case may be.
On the other hand, if the structural integrity of the airframe were compromised from the onset, there is a high probability that the high dynamic loads (wing loading) on surfaces like the horizontal and vertical stabilizers (as an example) would liberate them during the high speed descent. Control surface flutter at high speeds would easily liberate those surfaces in short order. The wings and wing box structure would, IMO, remain relatively intact.
Again, there are too many variables involved to accurately determine the exact failure mode at this point.