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#11
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"Buzzer" wrote in message ... On Fri, 19 Mar 2004 09:15:45 -0500, "Kevin Brooks" wrote: In 1961 there were some 571 B-52's in service ( http://www.nrdc.org/nuclear/nudb/datab7.asp ), and by the following year that had climbed to some 673; I doubt that any major program such as the addition of a TA radar was completed in a period of less than three or four years at best for a force of that size (just based upon the '61 size); doing it in two years would have required a modification rate of nearly one aircraft per day, sevven days a week, fifty-two weeks a year. IF E forward came out with TA then the D is the only one that needed the mod, and maybe the C... Most sources seem to indicate the C's, or some of them, did get them. As to E. I don't know--neither source I checked (Baugher and IAPR) specifically indicated they were in the aircrraft as they were delivered. Both of those sources are hardly infallible (as you pointed out with Baugher earlier, and I noted in IAPR that they mistakenly indicated that the Hound Dog brought the first thermonuclear warhead to the B-52 warload, when in fact they had already been carrying freefall TN devices). But I find Baugher's indication that there were some development/integration problems with the TA radar at least believable (that would have been sort of cutting edge stuff during that period), so whether or not the E's had them on delivery is a valid question. There was also an airframe modification program initiated to strengthen the structure so that it could absorb the increasedfatigue loads of low altitude work--I have not seen any indication of when that effort was completed, either, or whether it ever addressed either the C or E models. Some of our D models at Glasgow 64 or so had the stress gauges on them for the study of the structure mod. Only reason I knew about them at the time was they were obvious on the inside skin in the tail section when we loaded chaff. I think the B-52 that crashed in 65 during low level had them because the Boeing engineers were "reading the tapes" from a recorder on the aircraft in our maintenance office. I always figured the recorder was the one that monitored the stress gauges and other aircraft data. Not positive but the structure mod was probably during Big Belly. Or not done at all on the Vietnam birds since they would only be flying high? I believe your last sentence is the correct one, from what I have been reading. I am not sure that either the C's or D's ever got those mods; I think the E's and F's already had them "factory installed", so to speak. In a maintenance debriefing once there was a discussion about the 2000 hr design life of the B-52D and our planes were at something like 1500/1600 hrs. I'm about 19 years old and a flunky two striper thinking what a waste of money designing an aircraft for only 2000 hrs. Click and the clock hits 2000 and off to the junkyard. And then along comes Vietnam... I wish the Army had designed their trucks that way...in 1993, when I gave up company command, we still had some of the old "multi-fuel" series five ton trucks in hand, and they were still wheezing along five or six years later when the Army announced they were no longer going to carry the repair parts lines for them. They were not as old as the Buff's, but they were beat all to hell. How many commercial operators plan to use the same trucks for twenty-five years or so? Brooks |
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