Electronic Flight Display Flashcards
1
Q
ADC Air Data
A
provides typical Pitot-Static info
•Airspeed
•Altitude
•Vertical Speed
2
Q
Attitude Heading Reference System (AHRS)
A
Provides pitch, roll, yaw
3
Q
Attitude- heading reference system
A
- Gyros - angular velocities per each axis
- Newton’s 1st law : a body remains in motion unless the body is acted upon by an external force
- In this case, vibrating quartz tends to stay in vibrating plane
- Able to detect transition changes of roll, pitch & yaw
- Accelerometers - change of linear velocities per each axis
- Detects forces when roll and pitch are established
- Initial attitude reference (level)
- Inclinometer information
4
Q
Air Data/Attitude/Heading Reference System (ADAHRS)
A
- Air Data
- Uses digitized Ram & Static Air pressures with OAT
- Magnetometer
- Magnetic Heading information
- Three axis solid state gyro and accelerometer system
- Three Axis – Pitch, Bank, Roll
- Gyros - angular velocities per each axis
- Accelerometers – change of linear velocities per each axis
5
Q
Multifunction Displays (MFDs)
A
Provides in general •Moving maps •Checklists •System status •Flight plan information •Nearest functions Limitations •In general you can only use the MFD as a reference (not primary) •Refer to the aircrafts specific POH for more information