Airspeed-Altitude Computer
Item Name Code (INC) 00417
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A single component with the dual function of determining the rate of movement through the air and the vertical distance above a reference plane of the aircraft in which it is installed.
Additional Information for Airspeed-Altitude Computer
An Airspeed-Altitude Computer is a device used in aviation to calculate and display the aircraft's airspeed and altitude. It is a part of the Flight Instruments supply class, which includes various instruments used for navigation and control of an aircraft. The Airspeed-Altitude Computer is specifically designed to provide accurate and real-time information about the aircraft's speed and altitude, allowing pilots to make informed decisions during flight. It is an essential tool for maintaining safe and efficient operations in the aviation industry.
Related Item Names for INC 00417 Airspeed-Altitude Computer
Airspeed-Altitude Computer Present Position Computer Pressure Altimeter Venturi Tube Attitude Indicator Turn And Slip Indicator Pitot Tube Pitot-Static Tube Static Tube Mach And True Air Speed Indicator Vertical Velocity Indicator Machmeter Air Speed Computer Mechanical Accelerometer Aircraft Inclinometer Aircraft Instruments Manifold Position Transmitter Position Indicator Recorder Subassembly Recorder Group Altitude Computer Azimuth-Elevation Deviation Indicator Control Surfaces Trim Indicator Data Display Group Course Indicator Linear Electrical Accelerometer Optical Element Cell Dummy Static Tube Indicator Housing Angle Of Attack Transmitter Flight Director Computer Air Data Computer Mach Number Computer Magnetic Recording Tape Reel Airspeed And Direction Indicator Computer Subassembly Head-Up Display Unit Air Speed Indicator Angle Indicator Gyroscopic Heading Indicator Airport Runway Instrument Landing Indicator Instruments And Laboratory Equipment Modification Kit Wrist Instrument Strap Flight Data Recorder Collision Avoidance Computer Data Acquisition Unit Head-Up Display Symbol Generator Head-Up Display Monitor Pressure Altimeter Subassembly Automatic Pressure Standby Servo Controlled Altimeter Subassembly Preset Command Information Servo Controlled Altimeter Subassembly Air Speed Indicator Subassembly Flight Instruments Angle Indicator Subassembly Attitude Indicator Subassembly Flight Instruments Course Indicator Subassembly Gyroscopic Heading Indicator Subassembly Mach And True Air Speed Indicator Subassembly Flight Instruments Position Indicator Subassembly Control Surfaces Trim Indicator Subassembly Turn And Slip Indicator Subassembly Vertical Velocity Indicator Subassembly Flight Data Recorder Interface Subassembly Flight Data Recorder Memory Unit Electronic Air Inlet Controller Flight Information Processor Fuel Management Computer Flight Information Display Unit Fuel Management Panel Fuel Savings Advisory Computer Ground Speed Indicator Control-Display Unit Static Tube To Case Section Adapter Automatic Pressure Standby Servo Controlled Altimeter Preset Command Information Servo Controlled Altimeter Stabilization Data Indicator Static Tube Protector Static Tube Subassembly Static Tube Base Static Tube Mast Static Tube Probe Static Tube Vane Assembly Multiple Aircraft Parameters Display Computer Multiple Aircraft Parameters Display Attitude And Heading Reference Unit Aircraft Pitot Static Drain Bottle Special Purpose Computer System Special Purpose Computer Autopilot Control Unit Impact Pressure Transducer
NATO Stock Numbers with Item Name 00417 Airspeed-Altitude Computer Page 1 of 1
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