Elevator (aeronautics)

Definition and stakes

Portal:Civil Aeronautics Board,  Aviation Accident Report: Eastern Air Lines Flight 304 (1966)

“ The larger size of the stabilizer makes it approximately three times as powerful as the elevator, and therefore, about six degrees of up elevator is required to counteract the effect of an unwanted 2-degree AND stabilizer position. This amount of elevator deflection is lost insofar as recovery is concerned. Also, as speed increases, the ability to get any recovery action from the elevator diminishes, and disappears completely at about 470 knots. Other factors could also prolong the dive. ”
Source: Wikisource

Portal:Civil Aeronautics Board,  Aviation Accident Report: Eastern Air Lines Flight 304 (1966)

“ Data developed by an independent research agency, under government contract, revealed that the rate of response to elevator deflection has a profound effect on the behavior of the aircraft from the pilot viewpoint. This mode of motion, the longitudinal short period mode, has a one to five second period and is involved in the maneuvering of the aircraft. As the short-period frequency decreases, a slower response is experienced, and the initial motion is not a good indicator of what the final response will be. ”
Source: Wikisource

Portal:Civil Aeronautics Board,  Aviation Accident Report: Eastern Air Lines Flight 304 (1966)

“ In other words, the pilot, finding his aircraft in an excessively nose-high attitude, pushes the column forward and, when the aircraft does not respond to his satisfaction, he also actuates the trim switch. He then suddenly finds the aircraft responding more rapidly than he anticipated, and thus motion could also have been aggravated by a gust reversal which becomes additive to the elevator and stabilizer inputs. At this point, in all probability, the PIO conditions have ended for all practical purposes, and the aircraft is in a dive. ”
Source: Wikisource

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