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Gord Beaman wrote:
What goes around comes around? ![]() acquired an ASW aircraft called the Argus...it was a much modified Bristol Britannia and had 'floating controls'. They were free floating and were controlled by 'tabs' on their trailing edges. When at rest the ailerons hung down (both of them!) at about 45 degrees and when the 'gust locks' were on they both reared up about the same. The elevators both hung down 30 0r 40 degrees when unlocked and were straight back when locked, the rudder was straight back when locked and was 'where-ever it damned well wanted' when unlocked...quite weird...got many tower controllers (and airline pilots) in a knot. ![]() Doesn't the DC-9 work this way too? I have a vague recollection of talking to a DC-9 pilot who explained the system to me -- mechanical interconnections to servo tabs, with the main surfaces floating free. Or is my memory faulty? |
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Bob Moore wrote:
(Roy Smith) wrote Doesn't the DC-9 work this way too? I have a vague recollection of talking to a DC-9 pilot who explained the system to me -- mechanical interconnections to servo tabs, with the main surfaces floating free. Don't know about the DC-9, but the B-707 worked that way. Bob Moore PanAm(retired) Really?, I'd have thought that the 707 (and maybe DC-9 too) would have had powered controls?... -- -Gord. (use gordon in email) |
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Gord Beaman wrote
Really?, I'd have thought that the 707 (and maybe DC-9 too) would have had powered controls?... Rudder...yes, Ailerons and Elevator...no. In fact, the two elevators were not connected to each other. It was not unusual to see a taxing 707 with one elevator up and the other one down. Each positioned by a control tab, the left one by the left yoke and the right one by the right yoke. The two yokes were connected under the cockpit by a coupler that would slip if forced. Airflow would cause the tabs to "fly" the elevators to the commanded position. The ailerons operated in a somewhat similiar fashion. Bob Moore ATP B-707 B-727 PanAm (retired) |
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