Intermediate CompanionRevision 3.1
FNX-FANTHE FLIGHT COMPANIONS
INTERMEDIATE / REVISION 3.1

DESCENT MODES AND ENERGY MANAGEMENT

Contents

Plan the descent around height, speed, clearance and route restrictions. A shortcut removes distance, wind changes progress over the ground and a speed restriction can require deceleration while height still needs to be lost. Assess the combined effect early enough to choose a workable path. [13, PDF pp. 141-146]

DES follows the computed managed profile. OP DES descends towards the selected altitude with a different relationship to flight-plan constraints. V/S commands vertical speed, requiring particular attention to the resulting speed and energy. Read the active mode, altitude target and actual speed together before deciding on the next intervention. [60, PDF pp. 3-4,10-12]

Monitor the plan as it develops and revise it when conditions change. Use speedbrakes within their applicable operating conditions, while allowing the distance and time needed for deceleration. One early, understood adjustment usually leaves a clearer picture than several large interventions made close to the airport. [13, PDF pp. 141-146]

Original Fenix V3 VNAV display detail. The FMA is outside this crop, so the active vertical mode cannot be identified from this image.

Original Fenix V3 VNAV display detail. The FMA is outside this crop, so the active vertical mode cannot be identified from this image. [2, Source illustration]

IN PRACTICE: Start the descent and watch the path stay believable

Before you begin: The arrival is prepared, the route and wind data are current, and ATC has cleared descent to a defined altitude or flight level.

1. Set the clearance before requesting a mode

Action. Turn the FCU altitude to the cleared level and read it back. At the cleared descent start, push the altitude knob for the planned managed descent along the route.

Check. DES is the requested managed mode and the FCU level remains the lower limit of the present clearance. [13, PDF pp. 141-146] [14, PDF pp. 1085-1090]

2. Read the aircraft response

Action. Check the FMA descent/thrust indications and the actual pitch, speed and vertical trend. Compare the vertical deviation with the computed profile.

Check. The aircraft has entered the expected descent and is moving towards the intended path; a button press alone has not been taken as confirmation. [13, PDF pp. 141-146]

3. Monitor constraints before they become urgent

Action. Look ahead at the next altitude and speed restrictions on F-PLN and the ND. Compare the predicted crossing with the chart and the active clearance.

Check. The next restriction remains achievable within the current path, speed and clearance. There is time to act if the prediction changes. [13, PDF pp. 141-146] [14, PDF pp. 1085-1090]

4. Manage excess energy while it is still manageable

Action. If the aircraft is high or fast, review the wind, speed and path picture early. Use permitted speedbrake as required, monitor the response, and retract it as the profile is recovered.

Check. The excess energy is reducing. The aircraft is not left applying additional thrust against forgotten speedbrake. [13, PDF pp. 141-146]

5. Treat vectors as a guidance change

Action. If ATC vectors the aircraft or a tactical descent is needed, set the cleared heading and level, select the appropriate vertical mode and read the FMA again. In OP DES, manually protect constraints that are no longer followed by the managed path.

Check. The selected guidance follows the new clearance, and the crew understands the change in automatic constraint handling. [13, PDF pp. 141-146]

6. Recheck after a shortcut or runway change

Action. After a direct clearance, route shortening or revised arrival, inspect the new distance, vertical deviation and next constraints. Update the route and prediction before relying on the old top-of-descent picture.

Check. The descent plan is based on the route now being flown, including the available distance to slow and configure. [13, PDF pp. 141-146] [14, PDF pp. 1085-1090]

Complete when: The descent remains within the clearance, its modes are understood, and the approach can be reached with a controllable energy state.

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