2.
Operating modes of the autothrottles and how the modes are annunciated on the EDS.
3.
Operating limitations on the use of autothrot-tles (e.g.,minimum engagement altitude, etc.).
4.
The interaction that exists between flight director/autopilot modes and the autothrottle (e.g., for airspeed descents the autothrottle sets the throttles to flight idle, etc.).
3.12. Airborne Windshear Alerting System
A device or system which identifies the presence of windshear once the windshear is encountered. Some systems also may provide guidance information to the pilot.
Objectives that shall be understood:
1.
Warnings and required response for safe flight (i.e., escape maneuver).
2.
How windshear is integrated into the EDS.
3.
Limitations on the operational use of
windshear.
3.13. Radio/Audio Controllers
Radio/audio controllers provide for control of radio and audio.
Objectives that shall be understood:
1. The operation and intended function of each button, knob and/or annunciation associated with the radio/audio controller.
4. Automation Tasks by Phase of Flight
This section provides automation tasks required to be u nderstood and demonstr ated for each phase of flight.The training program shall provide“hands-on” practice using the avionics systems in realistic opera-tional flight scenarios (operationally-oriented train-ing ) . Various procedu r al tasks will be performed using the automated systems during all normal phas-es of flight operations (i.e., pre-flight, takeoff, climb, cruise, descent,approach and landing).All the tasks will be performed to proficiency upon completion of initial training.
The level of automation used for each phase of flight will vary depending upon SOP, aircraft equipment, environmental conditions, operation to be performed and other factors . The tr ain ing progr am should include all these factors and allow the pilot to choose the appropriate level of automation. It also should allow pilots to perform normal and abnormal check-list procedures as they apply to avionics-related sys-tems. It is assumed CRM is employed for all phases of flight and thus is not specified for each phase of flight.
4.1. Ground Operations
This phase includes all operations from equipment power-up and self-test through the before-takeoff checklist procedures.All initialization and configura-tion for the initial phases of flight are included.
Objectives that shall be understood and demonstr ated :
1.
Configuration of flight guidance modes and displays (e.g.,selecting FD modes, navigation sources, TAWS,WX radar, TCAS,HUD, etc.).
2.
Initialization of the FMS and creation of an active flight plan for the route of flight. This includes:
a. Use of datalink (e.g.,AFISTM, ACARS, etc.) to obtain ATIS and clearance, as applicable.
b.
Selection of departure runway, departure procedure, route of flight (per clearance).
c.
Comparison of the electronic departure to the printed departure procedure (e.g., overfly waypoints, left or right turns, discontinuity, altitude constraints, speed restrictions, etc).
d.
Configuration and verification of takeoff data (e.g.Vspeeds, runway required, etc.).
3. Position sensor management.
a.
Tuning of departure navaids, if applicable.
b.
GPS RAIM check (e.g., destination, alter-nate) for GPS approaches.
c.
Quick download align procedures (if appli-cable).
4.
Crew briefings. This shall include automation plan for the takeoff and departure (e.g., later-al/vertical/autothrottle modes during the takeoff/departure phases, route of flight, altitude restrictions, speed limits, emergency return, etc.).
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