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  2. Position error - Wikipedia

    en.wikipedia.org/wiki/Position_error

    This static port and the conduit constitute the aircraft's static system. The objective of the static system is to sense the pressure of the air at the altitude at which the aircraft is flying. In an ideal static system the air pressure fed to the altimeter and airspeed indicator is equal to the pressure of the air at the altitude at which the ...

  3. Pitot–static system - Wikipedia

    en.wikipedia.org/wiki/Pitotstatic_system

    A pitot–static system is a system of pressure-sensitive instruments that is most often used in aviation to determine an aircraft's airspeed, Mach number, altitude, and altitude trend. [1] A pitot–static system generally consists of a pitot tube, a static port, and the pitot–static instruments. [2]

  4. Pitot tube - Wikipedia

    en.wikipedia.org/wiki/Pitot_tube

    A pitot-static system generally consists of a pitot tube, a static port, and the pitot-static instruments. [5] Errors in pitot-static system readings can be extremely dangerous as the information obtained from the pitot static system, such as airspeed, is potentially safety-critical. Several commercial airline incidents and accidents have been ...

  5. Trailing cone - Wikipedia

    en.wikipedia.org/wiki/Trailing_Cone

    The trailing cone system trails at least one fuselage length behind the aircraft (SpaceAge Control) via a high-strength pressure tube. Static pressure is measured forward of the cone by several static ports. [3] The cone stabilizes and aligns the ports relative to the freestream airflow. [4]

  6. Aeroperú Flight 603 - Wikipedia

    en.wikipedia.org/wiki/Aeroperú_Flight_603

    The blockage of all of the static ports is one of the few common-failure modes resulting in total failure of multiple basic flight instruments and, as such, is regarded as one of the most serious faults that can occur in avionics systems. [12] The design of the aircraft did not incorporate a system of maintenance covers for the static ports.

  7. Indicated airspeed - Wikipedia

    en.wikipedia.org/wiki/Indicated_airspeed

    Indicated airspeed (IAS) is the airspeed of an aircraft as measured by its pitot-static system [1] and displayed by the airspeed indicator (ASI). [2] This is the pilots' primary airspeed reference.

  8. Airspeed - Wikipedia

    en.wikipedia.org/wiki/Airspeed

    The measurement and indication of airspeed is ordinarily accomplished on board an aircraft by an airspeed indicator (ASI) connected to a pitot-static system. The pitot-static system comprises one or more pitot probes (or tubes) facing the on-coming air flow to measure pitot pressure (also called stagnation, total or ram pressure) and one or ...

  9. Birgenair Flight 301 - Wikipedia

    en.wikipedia.org/wiki/Birgenair_Flight_301

    None of the pitot tubes were recovered so investigators were unable to determine for certain what caused the blockage. Investigators believe that the most likely culprit was the black and yellow mud dauber ( Sceliphron caementarium ), a type of solitary sphecid wasp well known to Dominican pilots, which makes a cylindrical nest out of mud and ...