3.5.1. Air Data Computer
3.5.2. Vertical Gyro/Directional Gyro or Attitude and Heading Reference System
3.5.3. Inertial Reference System
3.5.4. Very High Frequency Omni Range/Distance Measuring Equipment
3.5.5. Global Positioning System
3.5.5.1. Receiver Autonomous Integrity Monitoring
3.6. Weather Radar
3.7. Ground Proximity Warning System /Terrain Awareness and Warning System ........................................13
3.8. Radio Altimeter ..............................................................................................................................................13
3.9. Traffic Alert and Collision Avoidance System ............................................................................................14
3.10. Heads Up Display ........................................................................................................................................14
3.11. Autothrottles ................................................................................................................................................14
3.12. Airborne Windshear Alerting System ........................................................................................................14
3.13. Radio/Audio Controllers ..............................................................................................................................14
4. Automation Tasks by Phase of Flight ......................................................................................15
4.1. Ground Operations ........................................................................................................................................15
4.2. Takeoff/Departure/Climb ..............................................................................................................................15
4.3. Cruise ..............................................................................................................................................................15
4.4.Descent ............................................................................................................................................................16
4.5. Approach/Landing ..........................................................................................................................................16
4.6. Missed Approach/Alternate Destination ......................................................................................................16
Acknowledgements
The National Business Aviation Association expresses gratitude to the members of the NBAA FMS/Charting Subcommittee for the creation of these guidelines.
Cover Photo: Honeywell Primus 2000 Integrated Avionics Flight Control System for the Citation X
1. Introduction
This document provides National Business Aviation Ass oc i ation , Inc. ( N BAA) recommended tr ain ing guidelines for aircraft with automated flight decks. The document presents a training outline that repre-sents the minimum curriculum necessary to satisfy an automated flight deck instructional program.
These tr ain ing guidelines do not mand ate how advanced flight deck training is to be implemented. Each training provider must determine the most effective and efficient method to meet the objectives presented in this document.
For the purposes of this document, an automated flight deck is defined as an integrated avionics system consisting of at least a flight management system (FMS), flight guidance control system (FGCS) and electronic display s ystem (EDS). Training g uidelines also are provided for other advanced avionics, such as autothrottle, terrain awareness and warning system (TAWS), heads up display (HUD), etc.
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