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  2. Vertical stabilizer - Wikipedia

    en.wikipedia.org/wiki/Vertical_stabilizer

    The vertical stabilizer is the fixed vertical surface of the empennage. A vertical stabilizer or tail fin [1] [2] is the static part of the vertical tail of an aircraft. [1] The term is commonly applied to the assembly of both this fixed surface and one or more movable rudders hinged to it. Their role is to provide control, stability and trim ...

  3. Flight with disabled controls - Wikipedia

    en.wikipedia.org/wiki/Flight_with_disabled_controls

    According to the NTSB, the aggressive use of the rudder controls by the first officer stressed the composite vertical stabilizer until it separated from the aircraft. The complete loss of the vertical stabilizer meant the loss of all rudder control. As the pilots struggled to control the aircraft, it entered a flat spin. The resultant forces ...

  4. Flight control surfaces - Wikipedia

    en.wikipedia.org/wiki/Flight_control_surfaces

    The rudder is typically mounted on the trailing edge of the vertical stabilizer, part of the empennage. When the pilot pushes the left pedal, the rudder deflects left. Pushing the right pedal causes the rudder to deflect right. Deflecting the rudder right pushes the tail left and causes the nose to yaw to the right.

  5. Wingtip device - Wikipedia

    en.wikipedia.org/wiki/Wingtip_device

    The Rutan combined winglets-vertical stabilizer appeared on his Beechcraft Starship business aircraft design that first flew in 1986. Winglets are also applied to other business aircraft, reducing take-off distance to operate from smaller airports, and allowing higher cruise altitudes.

  6. Tailless aircraft - Wikipedia

    en.wikipedia.org/wiki/Tailless_aircraft

    It may still have a fuselage, vertical tail fin (vertical stabilizer), and/or vertical rudder. Theoretical advantages of the tailless configuration include low parasitic drag as on the Horten H.IV soaring glider and good stealth characteristics as on the Northrop B-2 Spirit bomber. Disadvantages include a potential sensitivity to trim.

  7. Vought F6U Pirate - Wikipedia

    en.wikipedia.org/wiki/Vought_F6U_Pirate

    The Vought F6U Pirate was the Vought company's first jet fighter, designed for the United States Navy during the mid-1940s. Although pioneering the use of turbojet power as the first naval fighter with an afterburner and composite material construction, the aircraft proved to be underpowered and was judged unsuitable for combat.

  8. Trailing cone - Wikipedia

    en.wikipedia.org/wiki/Trailing_Cone

    Download QR code; Print/export Download as PDF; Printable version; ... A Boeing 787-8 during a test flight with a trailing cone attached to the vertical stabilizer.

  9. McDonnell Douglas AV-8B Harrier II - Wikipedia

    en.wikipedia.org/wiki/McDonnell_Douglas_AV-8B...

    To compensate for the slight loss of directional stability, the vertical stabilizer's area was enlarged through increases in chord (length of the stabilizer's root) and height. [ 32 ] [ 33 ] USMC TAV-8Bs feature the AV-8B's digital cockpit and new systems but have only two hardpoints and are not combat capable. [ 33 ]