2.
The GPS NOTAM system.

3.
Failure annunciations.

4 . Oper ating lim it ations on the us age of GPS (e. g. , f ailu re of s ens or du ring GPS approaches , etc. ) .
3.5.5.1. Receiver Autonomous Integrity Monitoring
Receiver autonomous integrity monitoring (RAIM) is an onboard means of verifying GPS integrity.
Objectives that shall be understood:
1.
The concept and function of receiver
autonomous integrity monitoring.

2.
Current versus Predictive RAIM.

3.
Fault detection and exclusion (FDE)

4.
Failure annunciations associated with loss or exceedance of RAIM limits.

5. Operating limitations on the loss or
exceedance of RAIM (e.g., loss of RAIM
during GPS approaches, etc.).

3.6. Weather Radar
Weather radar is used to avoid hazardous weather.
Objectives that shall be understood:
1.
The operation and intended function of each button, knob and/or annunciation associated with the weather radar controller.

2.
How weather radar is integrated into the EDS and all display options available.

3.
Limitations on the operational use of the weather radar (e.g., turn off while refueling, do not use near ground personnel, etc.).

3.7. Ground Proximity Warning System /Terrain Awareness and Warning System
Ground proximity warning system (GPWS) is a reac-tive system that blends radio altimeter inputs with ILS glideslope and discrete signals from gear and flap systems in order to provide warnings of impending collision with terrain. Terrain awareness and warning system (TAWS) provides the functionality of GPWS with look ahead capability by displaying terrain on the EDS.
Objectives that shall be understood:
1.
Warnings and required response for safe flight (e.g.,“sink rate”,“pull up”, etc.). This includes call-outs that may occur during normal operations.

2.
How to perform an escape maneuver.

3.
How TAWS is integrated into the EDS and options that can be controlled by the pilot.

4.
Limitations on the operational use of
GPWS/TAWS (e.g., WGS 84,QFE, etc.).

3.8. Radio Altimeter
The radio altimeter measures height above ground.
Objectives that shall be understood:
1.
EDS symbology.

2.
How to test the radio altimeter if required.

3. Operating limitations associated with the loss of the radio altimeter (e.g.,unable to perform CAT II approaches,MEL, etc. ).

3.9. Traffic Alert and Collision Avoidance System
The tr af f ic alert and collision avoid ance system (TCAS) provides traffic advisories (TA) and resolu-tion advisories (RA).
Objectives that shall be understood:
1.
The operation and intended function of each button, knob and/or annunciation associated with the TCAS controller.

2.
Differences and significance of TCAS warn-ings (i.e., TA or RA).

3.
How to perform a RA maneuver and ATC issues with RA maneuver.

4.
Operating limitations associated with TCAS (e.g.,ILS PRM, RVSM, etc.)

3.10. Heads Up Display
The heads up display (HUD) displays flight guidance information onto a combiner glass mounted in front of the pilot.
Objectives that shall be understood:
1.
The operation and intended function of each button, knob and/or annunciation associated with the HUD controller.

2.
Special CRM issues associated with HUD operations.

3.
How to interpret what is displayed (i.e., sym-bology, etc.).

4.
Operating limitations associated with HUD (e.g.,CAT II/III, runway requirements, etc.).

3.11. Autothrottles
The autothrottle system provides speed or power control.
　
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