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Topic: Horizontal stabilizer

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	Parts of Airplane
		At the rear of the wings and stabilizers are small moving sections that are attached to the fixed sections by hinges.
		The hinged part of the vertical stabilizer is called the rudder; it is used to deflect the tail to the left and right as viewed from the front of the fuselage.
		The hinged part of the horizontal stabilizer is called the elevator; it is used to deflect the tail up and down.
	www.grc.nasa.gov /WWW/K-12/airplane/airplane.html (688 words)

	Aircraft horizontal stabilizer drive - Patent 4273006
		a horizontal stabilizer may be actuated by a single actuator although it may employ a torque tube and multiple linkages.
		Particularly acute is a horizontal stabilizer drive system wherein the entire stabilizer is rotated to provide trim.
		The driven structure (in this case the horizontal stabilizer) must be designed to withstand a worse case division of load forces equal to one half the maximum driving force, plus the braking force, plus the fixed pin shear force acting on one actuator with the balance on the other actuator.
	www.freepatentsonline.com /4273006.html (4302 words)

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	NTSB - Alaska Airlines Flight 261 Board Meeting Presentations
		Subsequent airplane nose down stabilizer trim motion from 7.0 degress ANU to 2.0 degrees ANU was due to the use of primary trim.
		Stabilizer motion from 2.0 degrees ANU to 0.4 degrees AND was commanded by the autopilot.
		The horizontal stabilizer jammed at 0.4 degrees AND and remained jammed until the Acme nut threads failed.
	www.ntsb.gov /events/2000/aka261/presentations/presentations.htm (502 words)

	Airdisaster.Com Forums - View Single Post - Stabilizer Position...
		FDR data indicated that the horizontal stabilizer’s last movement during the climbout was to 0.4º airplane nose down at 1349:51 as the airplane was climbing through 23,400 feet at 331 knots indicated airspeed (KIAS).
		After this, no horizontal stabilizer movement was recorded on the FDR until the airplane’s initial dive 2 hours and 20 minutes later.
		FDR and airplane performance data indicated that during the 3 to 4 seconds following the autopilot disconnect, the horizontal stabilizer traveled from its jammed position of 0.4º airplane nose down to beyond the maximum airplane-nose-down position that could be recorded by the FDR and remained beyond this position for the remainder of the flight.
	www.airdisaster.com /forums/showpost.php?p=379599&postcount=3 (761 words)

	ASN Aircraft accident description Embraer 120RT Brasilia N33701 - Eagle Lake, TX
		Although planned for the third shift, the 47 screws from the top of the left leading edge assembly for the horizontal stabilizer were already removed by the second shift.
		The cruise portion of the flight was uneventful and at 10:03 the aircraft was descending through 11800 feet to 9000 feet when the air loads caused the left horizontal stabilizer leading edge to bend downward and separate.
		PROBABLE CAUSE: "The failure of Continental Express maintenance and inspection personnel to adhere to proper maintenance and quality assurance procedures for the airplane's horizontal stabilizer deice boots that led to the sudden in-flight loss of the partially secured left horizontal stabilizer leading edge and the immediate severe nose-down pitchover and breakup of the airplane.
	www.aviation-safety.net /database/record.php?id=19910911-0&lang=en (489 words)

	horizontal stabilizer - OneLook Dictionary Search
		Horizontal stabilizer, Horizontal stabilizer, Horizontal stabilizer : InfoVisual Visual Dictionary [home, info]
		horizontal stabilizer : Hickok Sports Glossaries [home, info]
		noun: the horizontal airfoil of an aircraft's tail assembly that is fixed and to which the elevator is hinged
	www.onelook.com /?loc=rescb&w=horizontal+stabilizer (143 words)

	Skytronics, Inc.
		Overhaul: T/E Flapscrews; T/E Flap Transmissions; Horizontal Stabilizer Actuators; Horizontal Stabilizer Actuator Jackscrews.
		Overhaul: T/E Flapscrews; T/E Flap Transmissions; Horizontal Stabilizer Actuator Jackscrews; L/E Rotary and Kruger Actuators.
		Overhaul: T/E Flapscrews; T/E Flap Transmissions; Horizontal Stabilizer Actuator Jackscrews.
	www.skytronicsinc.com /Boeing_applications.htm (163 words)

	X-Plane, by Austin Meyer
		Ten elements per side per wing or stabilizer is the maximum, and studies have shown that this provides roll rates and accelerations that are very close to the values that would be found with a much larger number of elements.
		The aircraft linear and angular velocities, along with the longitudinal, lateral, and vertical arms of each element are considered to find the velocity vector of each element.
		The airfoil data entered in Part-Maker is 2-dimensional, so X-Plane applies finite wing lift-slope reduction, finite-wing CLmax reduction, finite-wing induced drag, and finite-wing moment reduction appropriate to the aspect ratio, taper ratio, and sweep of the wing, horizontal stabilizer, vertical stabilizer, or propeller blade in question.
	www.x-plane.com /about.html (860 words)

	Building the Super Six!
		04/18/03 - Install compression ribs in horizontal stabilizers, install hardware on elevators and attach all to tail group.
		08/30/03 - Cover right horizontal stabilizer, cut fabric for elevators, rudder and one flap.
		04/09 - 04/17/04 - Pick up remaining painted items at shop, hang horizontal stabilizers, run trim cable, hang elevators, install elevator horn and reattach to elevator yoke, install fuel scuppers, attach aft baggage compartment door, attach rudder stops, install rudder cable pulleys and keepers, readjust steering chains to half-compression.
	www.s6s.org /BuildingS6S.htm (2430 words)

	DJ'S Hobby Inc. Helicopters
		T-REX VERTICAL & HORIZONTAL STABILIZER - SILVER (3K CAR
		Vertical stabilizer x 1 Horizontal stabilizer x 1 Br...
		Metal Tail boom stiffener(L) x 1 Metal Tail boom sti...
	www.copterfreak.com /category/ajp (635 words)

	Fracture of an Aircraft Horizontal Stabilizer
		Click here to download the complete source publication for $73 PDF (8.8M)
		The paper shows how fracture mechanics can be used on data given in the accident report of the crash of a Boeing 707 at Lusaka to predict the fracture toughness of the material from which the cracked component was made, and to estimate the load transferred within the stabilizer by the arrest of this crack.
		ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA, 19428-2959 USA
	www.astm.org /DIGITAL_LIBRARY/STP/PAGES/STP19337S.htm (99 words)

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