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Air Data Computer
Requirement of Air Data Computer
- Avoid multiple Pitot and Static lines
- Provide centralized source of static and pitot pressure
- Convert pressure data in an electric or electronic format
Advantage of Air Data Computer
- Provide pressure data to other equipments
- Flight data recorder
- Navigation computer
- Auto Pilot
Equipments dependent on Air Data Computer
- ADC provides pressure data to
- Flight Data Recorder
- Electronic Flight Information System
- Warning Systems
- ATC Transponder
- Inertial Reference System
- Flight Control Computer
- Flight Management System
Analogue ADC
- Analogue ADC
- E-I bar to convert pressure data to electrical inputs
- Pressure information is transmitted through Pressure Transducer
Digital ADC
- Digital ADC
- Analogue to digital interface units
- Pressure information is transmitted through Digital Bus Bar
Configuration Module
- Configuration module corrects for position error
- Built in test equipment called BITE test
- Power up Check Up on start up
- Continuous Monitoring every one second
- Maintenance Tests during servicing or post-mortem
System Redundancy
- Redundancy to cater for blockage or leaks
- Electrical change over to use alternate static source
- Captain’s pressure sensors can provide data to Co-pilot’s equipments
Failure Warning in ADC
- Failure warning by Comparison monitor
- Warning Flag in case of loss of valid data or internal failure
- Comparison of outputs of Left and Right ADC components
- Light on the Instrument warning panel
Advantages of Air Data Computer
- Advantages of ADC over conventional Pitot Static system
- Improved Displays like digital, moving tape and combined displays
- Reduced Instrument and Lag Errors using servo motors.
- Error Correction by comparison of multiple inputs
- Height and airspeed channel for additional equipments
- Central pressure data Source for Other Systems
- Clean Design and Better Maintenance
Inputs – Outputs of ADC
- Inputs
- Pitot pressure
- Static pressure
- Total air temperature
- Angle of attack
- Weight on wheels switch
- Main power source
- Backup power source
- Outputs
- Altitude
- Vertical speed
- IAS or CAS
- SAT
- TAS
- Mach number
- Angle of attack
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