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- Pitot-static_system abstract "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. A pitot-static system generally consists of a pitot tube, a static port, and the pitot-static instruments. This equipment is used to measure the forces acting on a vehicle as a function of the temperature, density, pressure and viscosity of the fluid in which it is operating. Other instruments that might be connected are air data computers, flight data recorders, altitude encoders, cabin pressurization controllers, and various airspeed switches. Errors in pitot-static system readings can be extremely dangerous as the information obtained from the pitot static system, such as altitude, is often critical to a successful flight. Several commercial airline disasters have been traced to a failure of the pitot-static system.".
- Pitot-static_system thumbnail Faa_pitot_static_system.JPG?width=300.
- Pitot-static_system wikiPageExternalLink AD-CalibrationOfAirDataSystemsAndFlowDirectionSensors.pdf.
- Pitot-static_system wikiPageExternalLink Learning_Pitot_Sim.aspx.
- Pitot-static_system wikiPageID "2097807".
- Pitot-static_system wikiPageRevisionID "603336742".
- Pitot-static_system hasPhotoCollection Pitot-static_system.
- Pitot-static_system subject Category:Aircraft_instruments.
- Pitot-static_system subject Category:Speed_sensors.
- Pitot-static_system type AircraftInstruments.
- Pitot-static_system type Artifact100021939.
- Pitot-static_system type Detector103180969.
- Pitot-static_system type Device103183080.
- Pitot-static_system type Instrument103574816.
- Pitot-static_system type Instrumentality103575240.
- Pitot-static_system type Object100002684.
- Pitot-static_system type PhysicalEntity100001930.
- Pitot-static_system type SpeedSensors.
- Pitot-static_system type Whole100003553.
- Pitot-static_system comment "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. A pitot-static system generally consists of a pitot tube, a static port, and the pitot-static instruments. This equipment is used to measure the forces acting on a vehicle as a function of the temperature, density, pressure and viscosity of the fluid in which it is operating.".
- Pitot-static_system label "Pitot-Statik-System".
- Pitot-static_system label "Pitot-static system".
- Pitot-static_system label "Sistema pitot-statico".
- Pitot-static_system label "Système pitot-statique".
- Pitot-static_system label "Приёмник воздушного давления".
- Pitot-static_system sameAs Pitot-Statik-System.
- Pitot-static_system sameAs Système_pitot-statique.
- Pitot-static_system sameAs Sistema_pitot-statico.
- Pitot-static_system sameAs m.06lznn.
- Pitot-static_system sameAs Q456431.
- Pitot-static_system sameAs Q456431.
- Pitot-static_system sameAs Pitot-static_system.
- Pitot-static_system wasDerivedFrom Pitot-static_system?oldid=603336742.
- Pitot-static_system depiction Faa_pitot_static_system.JPG.
- Pitot-static_system isPrimaryTopicOf Pitot-static_system.
