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Typical trim tabs on aileron, rudder and elevator. Trim tabs are small surfaces connected to the trailing edge of a larger control surface on a boat or aircraft, used to control the trim of the controls, i.e. to counteract hydro- or aerodynamic forces and stabilise the boat or aircraft in a particular desired attitude without the need for the operator to constantly apply a control force.
An anti-servo tab on the elevator of an American Aviation AA-1 Yankee. An anti-servo tab, or anti-balance tab, works in the opposite way to a servo tab. It deploys in the same direction as the control surface, making the movement of the control surface more difficult and requires more force applied to the controls by the pilot.
A Piper PA-48 Enforcer, N202PE, c/n PE2-1001, crashed after structural failure due to flutter caused by a Piper-modified elevator trim-tab, off Vero Beach, Florida. [80] Four of the heavily modified, turbine-powered TF-51 derivatives were built for the counter-insurgency role with two tested at Eglin AFB , Florida in 1983–1984, but no orders ...
Most fixed-wing aircraft have a trimming control surface on the elevator, but larger aircraft also have a trim control for the rudder, and another for the ailerons. The rudder trim is to counter any asymmetric thrust from the engines. Aileron trim is to counter the effects of the centre of gravity being displaced from the aircraft centerline ...
In these incidents, there was a failure of control system components themselves (e.g. cables, hydraulics, flaps, slats, ailerons, rudder, stabilizer, trim tabs, auto-pilot). (Control system fatigue failures are here, but improperly installed or incorrectly adjusted controls in the next section.) United Airlines Flight 585, Boeing 737, March 3 ...
Cockpit controls and instrument panel of a Cessna 182D Skylane. Generally, the primary cockpit flight controls are arranged as follows: [2] A control yoke (also known as a control column), centre stick or side-stick (the latter two also colloquially known as a control or joystick), governs the aircraft's roll and pitch by moving the ailerons (or activating wing warping on some very early ...
The MACS3 Loading Computer System is a computer controlled loading system for commercial vessels, developed by Navis Carrier & Vessel Solutions. [1] Prior to October, 2017 it was offered by Interschalt maritime systems GmbH, and before 2007 - by Seacos Computersysteme & Software GmbH.
The Il-62 is the only airliner in its class with unpowered, all-manual flight controls, using steel cables, rods, pulleys, aerodynamic and weight balances, and aerodynamic trim tabs. [4] The Il-62 also has a forward-mounted tank serving as a water ballast. This may be used when the aircraft flies empty or lightly loaded.
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