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On Sat, 17 Apr 2010 01:10:49 -0800, "Dave D"
wrote: "Bob (not my real pseudonym)" wrote in message .. . On Wed, 14 Apr 2010 19:57:46 +0930, "Dave Kearton" wrote: "Salamanda" wrote in message ... Anyone know what happened? "guido" wrote in message . .. How can a plane fly in this conditions? http://www.talkingproud.us/HistoryB52NoTail.html Boeings ~usually~ make it home after the tail falls off. http://www.seattlepi.com/archives/1989/8901260265.asp Of course, the KC-135/707 was designed with a folding tail, for back in the days when it were the big'n in the hangar. Bob ^,,^ In fact, none of the 135s upon which I flew had folding tails. BTW and FWIW, the 135 is not a 707. It is, per Boeing, a 717..... DaveD With about 10k hours in RC135 aircraft. I'm not an expert on this stuff, but thought I had read that at least the KC-135 had this feature. Could it have either been removed, or just never used? When I look at my own and other's photos of KC-135s from before the re-engining projects, they all have what appears to be a walkway outlined in black (looked like a big check mark) on the port side of the vertical stabilizer - which would have been the topside when folded. http://aviation-safety.net/photos/ai...-P-d-1-500.jpg Also, wasn't part of the reason the USAF scarfed up so many used 707 and 720 airframes back in the '80s was for replacement vertical stabs for the KC-135s? Or was the folding stab only implemented on the 367-80? Sorry - limited vision and blood flow to the brain inhibit further research on my part at this time. Bob ^,,^ |
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