PRIMARY FLIGHT DISPLAY (PFD) - DESCRIPTION AND OPERATION

** ON A/C NOT FOR ALL

1. General
The Primary Flight Display (PFD) image is presented in front of each pilot on the outer display unit. It is transferred on the Navigation Display (ND) when the PFD is off or when PFD/ND transfer is requested.

** ON A/C NOT FOR ALL

2. Component Location

PFD - Component Location ** ON A/C NOT FOR ALL

FIN	FUNCTIONAL DESIGNATION	PANEL	ZONE	ATA REF
** ON A/C ALL
2CA	FCU	13VU	210	22-81-12
2WT1	PFD-CAPT	3VU	211	31-63-22
2WT2	PFD-F/O	5VU	212	31-63-22
1WT1	DMC-1	85VU	127	31-63-34
1WT2	DMC-2	86VU	128	31-63-34
1WT3	DMC-3	85VU	127	31-63-34

** ON A/C NOT FOR ALL

3. System Description
The PFD image is divided in 9 zones

PFD - Zones ** ON A/C NOT FOR ALL

The PFD image presents the main information necessary for the control of the A/C, arranged in the basic T configuration.

A grey background is permanently present on the screen.
If the SDAC detects AVIONICS VENT EXTRACT FAULT and AVIONICS VENT BLOWER FAULT conditions it sends a discrete signal to the DMCs which command the PFDs to suppress the grey background. This limits tube consumption and thus prevents them overheating. Tube operation is certified for 30 minutes without ventilation.

A. Attitude Data

PFD - Aircraft Attitude Display ** ON A/C NOT FOR ALL

The aircraft attitude (pitch and roll) is indicated in the center part of the image by a cut-sphere shaped window which features a conventional ADI.

(1) Aircraft symbol

PFD - Aircraft Attitude Display ** ON A/C NOT FOR ALL

The fixed symbol is in yellow color, it comprises 3 parts: two simplified wing/landing gear parts plus a center part.

(2) Aircraft symbol - Description
It provides the pilot with a quick glance attitude information, both in pitch and roll with respect to the attitude sphere. When the pilot selects the TRK FPA mode on the FCU instead of the HDG V/S mode, the A/C symbol is dimmed (except at take off).

(3) Aircraft symbol - Description
It provides the pilot with a quick glance attitude information, both in pitch and roll with respect to the attitude sphere.

(4) Pitch angle information

PFD - Aircraft Attitude Display ** ON A/C NOT FOR ALL

The A/C present pitch angle is given by the vertical displacements of the pitch attitude scale with respect to the center of the A/C symbol. The scale moves behind the cut-sphere shaped window, limited by the lines of an upper and a lower sector. The scale rotates around the center of the A/C symbol in accordance with the A/C present roll angle.
The pitch scale comprises white reference lines and associated pitch angle values. The lines are given every 2.5 degrees from 0 to 10 degrees, then for the 15 degrees, 20 degrees, 30 degrees, 50 degrees and 80 degrees values. Beyond 30 degrees, red large arrow heads (V-shaped) indicate an excessive attitude and the direction to follow in order to reduce it.

PFD - Pitch Scale ** ON A/C NOT FOR ALL

(5) Pitch angle information

PFD - Aircraft Attitude Display ** ON A/C NOT FOR ALL

The A/C present pitch angle is given by the vertical displacements of the pitch attitude scale with respect to the center of the A/C symbol. The scale moves behind the cut-sphere shaped window, limited by the lines of an upper and a lower sector. The scale rotates around the center of the A/C symbol in accordance with the A/C present roll angle.
The pitch scale comprises white reference lines and associated pitch angle values. The lines are given every 2.5 degrees from 0 to -10 degrees and from 0 to 30 degrees , then for the -15 degrees, -20 degrees, -30 degrees, +/- 50 degrees and +/- 80 degrees values. Beyond 30 degrees, red large arrow heads (V-shaped) indicate an excessive attitude and the direction to follow in order to reduce it.

(6) Roll angle information

PFD - Aircraft Attitude Display ** ON A/C NOT FOR ALL

A yellow triangle which remains on the line going through the center of the A/C symbol and which is perpendicular to the horizon line, moves against the fixed roll scale on the upper contour of the attitude sphere.
This fixed roll scale comprises white marks for the 10 degrees, 20 degrees, 30 degrees and 45 degrees significant values, on either side of the zero position (horizontal wings) which is indicated by a small fixed triangle. The 60 degrees roll indication corresponds to the limits of the upper contour of the cut-sphere shaped window.

(7) Upper sector

PFD - Attitude Zone Sectors ** ON A/C NOT FOR ALL

PFD - Sectors ** ON A/C NOT FOR ALL

This cyan sector masks the upper part of the pitch scale. It rotates around the A/C symbol center with the same angle as the A/C present roll angle.

(8) Lower sector

PFD - Sectors ** ON A/C NOT FOR ALL

The brown sector masks the lower part of the pitch scale. It rotates around the A/C symbol center like the upper sector.
In the final phase of an approach, the lower sector progressively climbs up as the A/C nears the ground; this is called rising runway.

PFD - Rising Runway,Lateral Acceleration and FD Bars Parameters ** ON A/C NOT FOR ALL

When the A/C is on the ground, the sector covers the full earth area up to horizon line.

ITEM LIST

PFD - Rising Runway,Lateral Acceleration and FD Bars Parameters ** ON A/C NOT FOR ALL

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ITEM PARAMETER EQUIPMENT LABEL COLOUR

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1 Rising runway/ground Radio alti 164 White

2 Lateral acceleration ADIRU IRS 332 Yellow

or estimated side slip FAC 226 Yellow

or target estimtd side slip FAC 077 Cyan

3 Roll FD FMGC 140 Green

4 Pitch FD FMGC 141 Green

(9) Lower sector

PFD - Attitude Zone Sectors ** ON A/C NOT FOR ALL

PFD - Rising Runway,Lateral Acceleration and FD Bars Parameters ** ON A/C NOT FOR ALL

When the A/C is on the ground, the sector covers the full earth area up to horizon line. Provided the optional rising runway is installed, the rising runway symbol replaces the rising ground.
In the final phase of an approach, the rising runway symbol rises from the bottom of the pitch scale to the aircraft reference. The rising runway symbol can be displayed either with the conventional crossed bar or with the optional V-bars.
ITEM LIST

PFD - Rising Runway,Lateral Acceleration and FD Bars Parameters ** ON A/C NOT FOR ALL

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ITEM PARAMETER EQUIPMENT LABEL COLOUR

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1 Rising runway/ground Radio alti 164 White

2 Lateral acceleration ADIRU IRS 332 Yellow

or estimated side slip FAC 226 Yellow

or target estimtd side slip FAC 077 Cyan

3 Roll FD FMGC 140 Green

4 Pitch FD FMGC 141 Green

(10) Heading marks

PFD - Attitude Zone Sectors ** ON A/C NOT FOR ALL

PFD - Sectors ** ON A/C NOT FOR ALL

Provided that the pitch angle, roll angle and magnetic heading information is valid, magnetic heading graduations are constantly displayed just under the horizon line every 10 degrees of heading.
For high attitude values, when the horizon line disappears behind the upper sector or the lower one, the magnetic heading graduations remain in view. They are displayed below the sector line.

(11) Attitude failure presentation

PFD - Attitude Failure Display ** ON A/C NOT FOR ALL

In case of detected failure of the ADIRU (IRS) concerning the pitch and/or roll angle information, the whole attitude and guidance display is replaced by the ATT red flag (flashing for 9 s then steady). This ATT red flag disappears when the PFD is supplied again with healthy pitch and roll data, from another source or from the same source.

(12) Lateral acceleration
A yellow trapezoidal index below the roll angle will represent the A/C lateral acceleration on the ground. It will be driven by the side slip information above 30 ft radio-altitude if this information is available.

PFD - Slip Indication ** ON A/C NOT FOR ALL

item (a).
If not, the index gives again an indication of A/C lateral acceleration.
In case of engine failure, at take off or go around the index changes to cyan color and becomes thicker.
It will then be animated by the difference:

(estimated side slip) minus (target side slip),

so that it will be centered if the pilot gives the proper rudder control necessary to compensate for the engine failure.

(13) Lateral acceleration
A yellow trapezoidal index below the roll angle will represent the A/C lateral acceleration on the ground. It will be driven by the side slip information above 30 ft radio-altitude if this information is available.

PFD - Slip Indication ** ON A/C NOT FOR ALL

item (a).
If not, the index gives again an indication of A/C lateral acceleration.
In case of engine failure, at take off or go around the index changes to cyan color.
It will then be animated by the difference:

(estimated side slip) minus (target side slip),

so that it will be centered if the pilot gives the proper rudder control necessary to compensate for the engine failure.

(14) SI flag
In case of failure a SI red flag is presented at the symbol location

PFD - Slip Indication ** ON A/C NOT FOR ALL

item (b).

NOTE: As a safety precaution the SI flag like other red flags is visible on the PFD, even in minimum brightness condition.

NOTE: A SI red flag is presented at the symbol location if any reverse is deployed in flight.

(15) Guidance
With the standard FD bars, either of these two modes of presentation of the Flight Director orders is available depending on the HDG V/S -TRK FPA choice

PFD - Guidance Selection ** ON A/C NOT FOR ALL

item (a) :

conventional crossed bars, pitch and roll (plus yaw bar for take off and land align and roll phases).
Flight Path Director symbols in relation with the Flight Path Vector, they give the orders in flight path and in track.

The guidance orders are presented on a given PFD provided that the FD pushbutton switch light on the respective EFIS control section of the FCU is on, the on condition corresponds to the FD ON selection

PFD - Guidance Selection ** ON A/C NOT FOR ALL

item (b).
Moreover, at least one FD must be engaged.
Provided that there is a value displayed in the FCU HDG/TRK counter and the FD is off, a cyan vertical bar on the horizon line indicates the selected heading or track.

(16) Guidance
With the standard FD bars, either of these two modes of presentation of the Flight Director orders is available depending on the HDG V/S -TRK FPA choice

PFD - Guidance Selection ** ON A/C NOT FOR ALL

item (a) :

conventional crossed bars, pitch and roll (plus yaw bar for take off and land align and roll phases).
Flight Path Director symbols in relation with the Flight Path Vector, they give the orders in flight path and in track.
With Vbar option pin program, the Vbar symbol is displayed depending on the HDG V/S - TRK FPA choice:
with the HDG V/S mode: Vbar symbol (plus yaw bar for TO and LAND ALIGN & ROLL OUT phases)
with the TRK FPA mode: Vbar symbol associated to the flight path vector.

PFD - Guidance Selection ** ON A/C NOT FOR ALL

(17) FD bars

PFD - FD Display ** ON A/C NOT FOR ALL

The pitch and roll bars automatically go out of view at touchdown in land mode.
In some cases, the FD bars flash for 10 s and then remain steady. For example in the following conditions :

reversion to the AFS basic modes (case of power supply transient),
change of selected flight level when the AFS was already engaged in ALT CAPT mode.
loss of LOC or G/S in land mode or loss of LAND mode.

(18) Flight Path Vector

PFD - Flight Path Presentation and Parameters ** ON A/C NOT FOR ALL

By means of the HDG V/S - TRK FPA pushbutton switch on the FCU, the crew can choose either set of basic modes for the AFS, and subsequent presentation on thePFD:

with the HDG V/S mode, the A/C attitude presentation is privileged,

with the TRK FPA mode, the A/C symbol is dimmed an the flight path vector symbol appears giving the A/C actual flight path angle and drift angle (track).
The flight path vector symbol provides the pilot with the A/C present flight path angle and the A/C present track information.
This symbol provides the pilot with the display of his actual flight path trajectory, in longitudinal and in vertical so that he sees no discontinuity when "switching" from this symbol on the PFD to the view of the outside world throught the windshield.
The Flight Path Vector lateral displacements are limited to 21 deg (21 deg) drift angle.
ITEM LIST

PFD - Flight Path Presentation and Parameters ** ON A/C NOT FOR ALL

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ITEM PARAMETER EQUIPMENT LABEL COLOUR

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1 Flight path vector longitudinal ADIRU IRS 322 Green

Flight path vector lateral ADIRU IRS 321 Green

2 Flight path director longit. FMGC 141 Green

Flight path director lateral FMGC 140 Green

(19) Flight Path Director

PFD - Flight Path Presentation and Parameters ** ON A/C NOT FOR ALL

This symbol (which consists of 2 triangles facing each other and linked by a thin line whose the middle is indicated by a small point) has 3 degrees of freedom:

lateral displacements (parallel to the horizon line),
longitudinal displacements (parallel to the pitch scale),
rotation around its middle.

It follows the lateral and longitudinal displacements of the FPV and gives the pitch and roll orders respectively through its longitudinal and rotation movements with respect to the Flight Path Vector symbol.
In case of failure of the guidance signals a red FD Flag is displayed (when FD pushbutton switch is pressed).

PFD - FD and FPV Failure Display ** ON A/C NOT FOR ALL

item (a).
If the track angle or flight path angle signal or both are wrong, the red FPV signal is displayed (when the TRK-FPA pushbutton switch mode is selected).

PFD - FD and FPV Failure Display ** ON A/C NOT FOR ALL

item (b).

(20) Flight Path Director

PFD - Flight Path Presentation and Parameters ** ON A/C NOT FOR ALL

Two green triangles opposite to each other are used for the flight-path director symbol. A thin green line connects these two triangles and a small point shows the middle of the line. This symbol can move as follows:

Laterally (parallel to the horizon line)
Longitudinally (parallel to the pitch scale)
In rotation around its middle.

The rotation and the translation of the flight path director have the same limits as the Flight Director (FD) bars.
The flight path director follows the lateral and longitudinal movements of the Flight Path Vector (FPV) and gives the related pitch and roll orders through its longitudinal (2.25 degress/mm) and rotation movements (1 shown for an order of 1.3 degrees) in relation to the FPV symbol.
If there is a failure of the guidance signals, a red FD flag shows (when you push the FD pushbutton switch).

PFD - FD and FPV Failure Display ** ON A/C NOT FOR ALL

item (a).
If the track angle and/or the Flight Path Angle (FPA) signals are incorrect, the red FPV signal shows (when you select the TRK-FPQ mode pushbutton-switch).

PFD - FD and FPV Failure Display ** ON A/C NOT FOR ALL

The FPD shows in green in the conditions that follow:

The attitude is correct.
The V-bars option is not installed.
The FD pushbutton switch is pushed on the Flight Control Unit (FCU).
On PFDs 1 and 2, the flight-director engagement status-message 1 FD 1 or 2 FD 2 is shown.
The FD roll angle is correct.
The FD pitch angle is correct.
The Drift Angle (DA) is correct.
The FPA is correct.
The FPV symbol is not shown or incorrect.
The harmonized PFD option is not on.

When the harmonized PFD option is on, the usual flight path director is replaced by a new one (in magenta with a radius of 1.7 MM (0.1 IN.) and with a priority higher than the upper and the lower sector) in the conditions that follow:

FPD Shape for HPFD when not Dashed ** ON A/C NOT FOR ALL

The harmonized PFD is shown.
The FD is engaged.
The FD pushbutton switch is pushed on the FCU.
The attitude is correct.
The delta pitch order (related to the FPV position) is valid.
The delta roll order (related to the FPV position) is valid.

When the harmonized PFD option is on, the limit of the flight-path director movement is a circular zone with a radius of 31.4 mm (1.2 in.), The center of the circular zone is the aircraft reference. When the flight path director is out of the approved zone, it is necessary to make a projection on the zone border and use a dash.
When the harmonized PFD option is on, for the flight-path director lateral and longitudinal movements in relation to the FPV, it is necessary to apply a gain equal to three to:

The filtered pitch-differential order
The filtered roll-differential order.

When the harmonized PFD option is on, the flight path director must flash if the pitch bar flashing-order is detected or if the FD roll-bar flashing-order is detected.

(21) Yaw Bar

PFD - Yaw, FD, Radio Alt, Roll and Pitch Angle Parameters ** ON A/C NOT FOR ALL

This symbol provides the pilot with flight director yaw orders.
When in RWY mode, during take off, this symbol remains presented until the A/C reaches the altitude of 30 ft.
When in ROLL OUT mode this symbol appears, when in descent the A/C reaches 30 ft. just before landing.

(22) Selected Flight Path Angle (FPA)

Selected FPA for the HPFD Option ** ON A/C NOT FOR ALL

This symbol gives the pilot a slope reference to prevent cluttering. No final approach FPA value is shown on the right side of the line opposite to Head-Up Display (HUD).
When the harmonized PFD option is on, the selected FPA is shown in cyan, with an empty space between the two lines in the conditions that follow:

The attitude is correct.
The aircraft is in the approach phase (the speed delta is correct with a Sign Status Matrix (SSM), not at No Computed Data (NCD)).
The aircraft is not in the flare mode.
The selected FPA value is correct with an SSM, not at NCD.
The selected FPA value is negative.
The automatic pilot is not on.
The FD pushbutton switch is not pushed or the FD is not on.

The position of the selected FPA must be in relation to the PFD pitch scale:

Laterally, in the center position
In a longitudinal position, to show on the pitch scale the FPA value selected on the Flight Control Unit (FCU)
After the roll movements.

(23) Tailstrike indication

PFD - Tailstrike indication ** ON A/C NOT FOR ALL

The tailstrike indication is an amber "V", it is submitted to the roll angle, it is positioned on the pitch scale according to the following principle: the tailstrike angle is reached when the lower tip of the "V" contacts to the aircraft reference.

(24) ITEM LIST

PFD - Yaw, FD, Radio Alt, Roll and Pitch Angle Parameters ** ON A/C NOT FOR ALL

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ITEM PARAMETER EQUIPMENT LABEL COLOUR

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1 YAW FD FMGC 143 Green

2 RADIO ALTITUDE RADIO ALTI 164 Green

or amber

3 ROLL ANGLE ADIRU IRS 325 YELLOW

4 PITCH ANGLE ADIRU IRS 324 YELLOW

(25) Excessive Attitude Presentation

PFD - Yaw, FD, Radio Alt, Roll and Pitch Angle Parameters ** ON A/C NOT FOR ALL

PFD - Excessive Attitude Display ** ON A/C NOT FOR ALL

In case of excessive attitude:

pitch angle more than +25 degrees or less than -13 degrees or
absolute value of roll angle more than 45 degrees

The display of several zones is cleared from the PFD for better legibility: FMA, guidance symbols (FD or FPD).
The affected information is back on display when the pitch angle and roll angle become "normal" again:

pitch angle less than 22 degrees or more than -10 degrees
absolute value of roll angle less than 40 degrees.

(26) Check ATT Message

PFD - Yaw, FD, Radio Alt, Roll and Pitch Angle Parameters ** ON A/C NOT FOR ALL

PFD - Attitude Discrepancy ** ON A/C NOT FOR ALL

In case of discrepancy between the pitch or roll attitude information presented on the CAPT and F/O PFDs, a CHECK ATT amber message flashes for 9 s on both PFDs, then remains steady.
In this case, it is up to the pilots to remove ambiguity by cross checking the PFD attitude displays with the standby horizon indicator display, in order to detect the ADIRU (IRS) source which is drifting away, then to make the appropriate transfer switching by means of the ATT/HDG selector switch.

(27) WINDSHEAR Message

PFD - W/S Ahead Message ** ON A/C NOT FOR ALL

PFD - Reactive windshear alert ** ON A/C NOT FOR ALL

In approach or in take-off phase, when the altitude is comprised between 50 and 1300 ft, a red WINDSHEAR message is displayed for at least 15s on the PFDs if a reactive windshear condition is detected by the FAC.
In case of windshear detection the pilot must follow a safe trajectory using the TAKEOFF or GO AROUND mode.

(28) WINDSHEAR Message
In approach or in take-off phase, when the altitude is comprised between 50 and 1300 ft, a red WINDSHEAR message is displayed for at least 15s on the PFDs if a reactive windshear condition is detected by the FAC.
In case of windshear detection the pilot must follow a safe trajectory using the TAKEOFF or GO AROUND mode.

(29) Radio Altitude Indication
When below 2500 ft the A/C present radio altitude value is presented on the lower sector, in digits which size depends on the A/C proximity with respect to the ground.

3 mm high green digits if 2500 ft. > Height Radio Altitude (HRA) > 400 ft.
PFD - Radio Altitude Indication ** ON A/C NOT FOR ALL
item (a),
4 mm high green digits if DH+100 < HRA < 400 ft.
PFD - Radio Altitude Indication ** ON A/C NOT FOR ALL
item (b),
4 mm high amber digits if HRA < DH+100.

Below DH+100 the HRA value is indicated every 10 ft. if the A/C is above 50 ft. then every 5 ft. if 5 ft. < HRA < 50 ft and at last every foot below 5 ft. HRA.
The DH letters are displayed in large size and in amber color just above the line of the lower sector when the A/C reaches the selected DH and below

PFD - Radio Altitude Indication ** ON A/C NOT FOR ALL

item (c).
In case of radio altitude failure a red RA message is displayed in large size in the lower sector

PFD - Radio Altitude Indication ** ON A/C NOT FOR ALL

item (d).

(30) Side Stick Controller Order
On the ground with one engine running, a white cross indicates the resulting side stick controller order from the Captain and the First Officer: up and rightfor an order controlling on A/C nose up and right movement. Four white corners show the limits of this cross in pitch (plus or minus 15°) and in roll (plus or minus 19°).

(31) Attitude Protection Indication
Two small green dashes on each side of the cut-sphere show that the roll protections are available (plus or minus 65°).
Other green dashes on the pitch scale (on each side of the +30° and -15° graduations) show that the pitch protections are available: +30°, -15°. If not (for pitch or roll, independently), the dashes are replaced by amber crosses.

(32) Radio altitude indication
When the A/C is flying below 2500 ft, its radio altitude value is shown on the lower sector and the size of digits depends on the A/C proximity with respect to the ground.
The size is 3 mm high green digits, if 2500 ft. > Hra > 400 ft.

PFD - Radio Altitude Indication ** ON A/C NOT FOR ALL

item (a).
The size is 4 mm high green digits, if DH+100 < Hra < 400 ft.

PFD - Radio Altitude Indication ** ON A/C NOT FOR ALL

item (b).
The size is 4 mm high amber digits, if Hra < DH+100.

For 50 < Hra < 100 ft, the Hra value is indicated every 10 ft.
For 5 < Hra < 50 ft, the Hra value is indicated every 5 ft.
For 1 < Hra < 5 ft, the Hra value is indicated every foot.

The DH letters are displayed in large size and in amber color just above the line of the lower sector when the A/C reaches the selected DH and below.

PFD - Radio Altitude Indication ** ON A/C NOT FOR ALL

item (c).
In case of radio altitude failure, a red RA message is displayed in large size in the lower sector.

PFD - Radio Altitude Indication ** ON A/C NOT FOR ALL

item (d).

(33) Side stick controller order
On the ground with one engine running, a white cross indicates the resulting side stick controller order from the Captain and the First Officer. For a side stick controller order, when the A/C is nose up and moving to the right, the cross indicates 'up' and 'right' on the PFD. Four white corners show the limits of this cross in pitch (plus or minus 15°) and in roll (plus or minus 19°). Side stick order indication is removed when the nose landing gear is not compressed.

Side Stick Controller Order ** ON A/C NOT FOR ALL

(34) Attitude protection indication
Two small green dashes on each side of the cut-sphere show that the roll protections are available (plus or minus 65°).
Other green dashes on the pitch scale (on each side of the +30° and -15° graduations) show that the pitch protections are available (+30°, -15°). If not (for pitch or roll, independently), the dashes are replaced by amber crosses.

(35) IF WET : RWY TOO SHORT message

PFD - IF WET : RWY TOO SHORT message ** ON A/C NOT FOR ALL

In flight, during approach, the amber IF WET : RWY TOO SHORT message comes into view when the FMGC predicts that a runway overrun will occur if the runway is wet. If the runway is dry, the message can be disregarded and the approach continued.

(36) RWY TOO SHORT message

PFD - RWY TOO SHORT message ** ON A/C NOT FOR ALL

In flight, during approach, the red RWY TOO SHORT message comes into view if the FMGC predicts that a runway overrun will occur. In this case, the pilot must follow the safe trajectory by using the TAKE OFF or GO AROUND mode.

(37) MAX BRAKING message

PFD - MAX BRAKING message ** ON A/C NOT FOR ALL

On the ground, the red MAX BRAKING message comes into view if the FMGC measures that the current braking deceleration does not allow to stop before the runway end. In this case, the pilot must apply full braking power.

(38) MAX REVERSE message

PFD - MAX REVERSE message ** ON A/C NOT FOR ALL

On the ground, the red MAX REVERSE message comes into view if the FMGC measures that the current braking deceleration does not allow to stop before the runway end and no failure is detected on reverse by the FWC. In this case, the pilot must put the levers on reverse. Both MAX BRAKING and MAX REVERSE can be displayed at the same time.

(39) STALL message

PFD - STALL Message ** ON A/C NOT FOR ALL

In flight, the red STALL STALL message comes into view on the PFD in case of stall warning and an aural alert comes from the FWS. In this case the pilot must correct the angle of attack.

(40) W/S AHEAD message

PFD - W/S Ahead Message ** ON A/C NOT FOR ALL

This message is displayed, when the predictive windshear system has detected windshear ahead of the aircraft.
The message is in amber or red, depending on the alert level.

(41) RWY AHEAD message
On ground, a yellow pulsing RWY AHEAD message is displayed in PFD center in case of runway proximity detected by the OANS.

(42) STOP RUDDER INPUT message

STOP RUDDER INPUT message ** ON A/C NOT FOR ALL

The message "STOP RUDDER INPUT" is displayed in steady red and maintained at least for 4.5s when:

Stop rudder input condition is detected.
"STALL STALL", "RWY TOO SHORT", "IF WET: RWY TOO SHORT" messages are not displayed.
Aircraft is in flight phase 6.

(43) IF WET : RWY TOO SHORT message

PFD - IF WET : RWY TOO SHORT message ** ON A/C NOT FOR ALL

In flight, during the approach, the amber IF WET : RWY TOO SHORT message comes into view when the Flight Management and Guidance Computer (FMGC) tells that a runway overrun will occur if the runway is wet. If the runway is dry, you can ignore the message and continue the approach.

(44) RWY TOO SHORT message

PFD - RWY TOO SHORT Message ** ON A/C NOT FOR ALL

In flight, during the approach, the RWY TOO SHORT message comes into view if the FMGC tells that a runway overrun will occur. In this condition, the pilot must follow the safe trajectory and use the TAKE OFF or GO AROUND mode. Below 400 ft and above 200 ft, on the PFD, in the sky altitude zone, the RWY TOO SHORT message is shown in amber. The message flashes for nine seconds and then stays stable. There is no audio alert. Below 200 ft, on the PFD, in the sky altitude zone, the RWY TOO SHORT message is shown in red and flashes for nine seconds, then stays stable. The related audio alert operates again and again.

(45) MAX BRAKING message

PFD - MAX BRAKING message ** ON A/C NOT FOR ALL

On the ground, the red MAX BRAKING message comes into view if the FMGC measures that the braking deceleration does not let the aircraft stop before the runway end. In this condition, the pilot must apply the full braking power.

(46) MAX REVERSE message

PFD - MAX REVERSE message ** ON A/C NOT FOR ALL

On the ground, the red MAX REVERSE message comes into view if the FMGC measures that the braking deceleration does not let the aircraft stop before the runway end. The Flight Warning Computer (FWC) detects no reverse failure. In this condition, the pilot must put the levers in the reverse position. The MAX BRAKING message and the MAX REVERSE message can come into view in the same time.

(47) STALL message

PFD - STALL Message ** ON A/C NOT FOR ALL

In flight, the red STALL STALL message comes into view on the PFD when the stall warning and an aural alert comes from the Flight Warning System (FWS). In this condition the pilot must correct the Angle Of Attack (AOA).

(48) W/S AHEAD message

PFD - W/S Ahead Message ** ON A/C NOT FOR ALL

This message is shown when the predictive windshear system detected windshear in front of the aircraft.
The message is shown in amber or red, in relation to the alert level.

(49) RWY AHEAD message
On the ground, in the center of the PFD, the RWY AHEAD message is shown when the Onboard Airport Navigation System (OANS) detects that the runway is near. The message is shown in yellow and flashes.

(50) STOP RUDDER INPUT message

STOP RUDDER INPUT message ** ON A/C NOT FOR ALL

The STOP RUDDER INPUT message is shown for a minimum of 4.5 seconds in (stable) red when:

The stop rudder input-condition is detected.
The "STALL STALL", "RWY TOO SHORT", "IF WET: RWY TOO SHORT" messages are not shown.
The aircraft is in flight phase 6.

(50) BANK BANK message

BANK BANK Message ** ON A/C NOT FOR ALL

The BANK BANK message is shown on the PFD in (stable) red when a too large bank angle is detected and the aircraft is in flight phase 5, 6 or 7.

(51) System messages (feedback monitoring)

PFD - System Messages ** ON A/C NOT FOR ALL

A safety function is implemented in the EIS to monitor the critical parameters displayed on the PFD,such as PITCH, ROLL. When a discrepancy occurs between an incoming parameter (at the DMC input) and the same parameter ready to be drawn on the relevant DU (inside the DU), then a feedback message is generated on the DUs which monitor the faulty DU.

(a) Some of the feedback messages are displayed above the attitude zone:
CHECK PFD CAPT (amber)
CHECK PFD FO (amber)
CHECK EWD (amber)
DISPLAY SYSTEM VERSION INCONSISTENCY (amber)
DU NOT MONITORED (amber)

(b) Some of the feedback messages are displayed above the heading scale:
CHECK ND CAPT (amber)
CHECK ND FO (amber)
CHECK SD (amber)

B. Attitude Data - Condition of Display
The table below gives the conditions of display of the attitude information:

-------------------------------------------------------------------------------

! PARAMETERS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! A/C symbol ! - Valid attitude. !

! ! - Yellow (normal brightness) : take-off or heading/V/S !

! ! mode. !

! ! - Yellow (dimmed) : TRK-FPA mode. !

!--------------------!--------------------------------------------------------!

! Scale ! - Valid attitude. !

!--------------------!--------------------------------------------------------!

! Lateral ! - Yellow if attitude information is valid. !

! acceleration ! - On the ground : presents valid acceleration. !

! ! - In flight : presents estimated side slip, if valid, !

! ! otherwise, presents lateral acceleration. !

!--------------------!--------------------------------------------------------!

! Rising runway ! - Valid attitude. !

! ! - Valid radio altitude. !

! ! - Radio altitude above 50ft. !

!--------------------!--------------------------------------------------------!

! FD bars ! - Valid and not excessive attitude. !

! ! - Heading / V/S mode. !

! ! - FD engaged (green light on). !

! ! - Roll FD and pitch FD from FMGC valid. !

!--------------------!--------------------------------------------------------!

! Flight path vector ! - Valid atttude. !

! ! - Valid drift angle and flight path angle. !

! ! - TRK-FPA mode selected on FCU. !

!--------------------!--------------------------------------------------------!

! Flight path ! - Valid and not excessive attitude. !

! director ! - FD1 or FD2 engaged. !

! ! - Roll FD and pitch FD from FMGC valid. !

!--------------------!--------------------------------------------------------!

! Heading marks ! - Valid attitude. !

! ! - Valid magnetic heading. !

!--------------------!--------------------------------------------------------!

! Selected HDG/track ! - FD off. !

! ! - Valid attitude and magnetic heading. !

! ! - Selected track in TRK/FPA mode, selected heading in !

! ! HDG/V/S mode. !

!--------------------!--------------------------------------------------------!

! Radio altitude ! - Green, size 3mm : radio altitude between 400 and !

! ! 2500ft. !

! ! - Green, size 4mm : under 400ft., above DH+100ft. !

! ! - Amber, size 4mm : either RA under DH+100ft., either !

! ! invalid DH and RA under 400ft. !

! ! - Not excessive attitude condition. !

!--------------------!--------------------------------------------------------!

! Decision height ! - DH amber flashing when radio altitude goes under !

! (DH) ! decision then steady. !

!--------------------!--------------------------------------------------------!

! Yaw bar ! - On the ground, at least one engine running. !

! ! - Roll and pitch command position valid. !

!--------------------!--------------------------------------------------------!

! Protection marks ! - Only if valid attitude. !

! ! - Green dashes when roll protection in normal law. !

!--------------------!--------------------------------------------------------!

! Target side slip ! - Cyan trapezo??dal index below the roll angle in case !

! ! of engine failure, presenting the difference between !

! ! estimated side slip and target side slip. !

The table below gives the conditions of display of the attitude information:

-------------------------------------------------------------------------------

! PARAMETERS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! A/C symbol ! - Valid attitude. !

! ! - Yellow !

!--------------------!--------------------------------------------------------!

! Scale ! - Valid attitude. !

!--------------------!--------------------------------------------------------!

! Lateral ! - Yellow if attitude information is valid. !

! acceleration ! - On the ground : presents valid acceleration. !

! ! - In flight : presents estimated side slip, if valid, !

! ! otherwise, presents lateral acceleration. !

!--------------------!--------------------------------------------------------!

! Rising runway/ ! - Valid attitude. !

! ground ! - Valid radio altitude. !

!--------------------!--------------------------------------------------------!

! FD bars ! - Valid and not excessive attitude. !

! ! - Heading / V/S mode. !

! ! - FD engaged (green light on). !

! ! - Roll FD and pitch FD from FMGC valid. !

!--------------------!--------------------------------------------------------!

! Flight path vector ! - Valid atttude. !

! ! - Valid drift angle and flight path angle. !

! ! - TRK-FPA mode selected on FCU. !

!--------------------!--------------------------------------------------------!

! Flight path ! - Valid and not excessive attitude. !

! director ! - FD1 or FD2 engaged. !

! ! - Roll FD and pitch FD from FMGC valid. !

!--------------------!--------------------------------------------------------!

! Heading marks ! - Valid attitude. !

! ! - Valid magnetic heading. !

!--------------------!--------------------------------------------------------!

! Selected HDG/track ! - FD off. !

! ! - Valid attitude and magnetic heading. !

! ! - Selected track in TRK/FPA mode, selected heading in !

! ! HDG/V/S mode. !

!--------------------!--------------------------------------------------------!

! Radio altitude ! - Green, size 3mm : radio altitude between 400 and !

! ! 2500ft. !

! ! - Green, size 4mm : under 400ft., above DH+100ft. !

! ! - Amber, size 4mm : either RA under DH+100ft., either !

! ! invalid DH and RA under 400ft. !

! ! - Not excessive attitude condition. !

!--------------------!--------------------------------------------------------!

! Decision height ! - DH amber flashing when radio altitude goes under !

! (DH) ! decision then steady. !

!--------------------!--------------------------------------------------------!

! Side Stick Order ! - On the ground, at least one engine running. !

! ! - Roll and pitch command position valid. !

!--------------------!--------------------------------------------------------!

! Protection marks ! - Only if valid attitude. !

! ! - Green dashes when roll protection in normal law. !

!--------------------!--------------------------------------------------------!

! Target side slip ! - Cyan trapezo??dal index below the roll angle in case !

! ! of engine failure, presenting the difference between !

! ! estimated side slip and target side slip. !

!-----------------------------------------------------------------------------!

! Yaw Bar ! - valid attitude (and not excessive) !

! ! - FD1 and FD2 engaged !

! ! - Yaw FD from FMGC valid !

! ! - RWY or ROLL OUT modes !

The table below gives the conditions of display of the attitude information:

-------------------------------------------------------------------------------

! PARAMETERS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! A/C symbol ! - Valid attitude. !

! ! - Yellow !

!--------------------!--------------------------------------------------------!

! Scale ! - Valid attitude. !

!--------------------!--------------------------------------------------------!

! Lateral ! - Yellow if attitude information is valid. !

! acceleration ! - On the ground : presents valid acceleration. !

! ! - In flight : presents estimated side slip, if valid, !

! ! otherwise, presents lateral acceleration. !

!--------------------!--------------------------------------------------------!

! Rising runway/ ! - Valid attitude. !

! ground ! - Valid radio altitude. !

!--------------------!--------------------------------------------------------!

! FD bars ! - Valid and not excessive attitude. !

! ! - Heading / V/S mode. !

! ! - FD engaged (green light on). !

! ! - Roll FD and pitch FD from FMGC valid. !

!--------------------!--------------------------------------------------------!

! Flight path vector ! - Valid attitude. !

! ! - Valid drift angle and flight path angle. !

! ! - TRK-FPA mode selected on FCU. !

!--------------------!--------------------------------------------------------!

! Flight path ! - Valid and not excessive attitude. !

! director ! - FD1 or FD2 engaged. !

! ! - Roll FD and pitch FD from FMGC valid. !

!--------------------!--------------------------------------------------------!

! Heading marks ! - Valid attitude. !

! ! - Valid magnetic heading. !

!--------------------!--------------------------------------------------------!

! Selected HDG/track ! - FD off. !

! ! - Valid attitude and magnetic heading. !

! ! - Selected track in TRK/FPA mode, selected heading in !

! ! HDG/V/S mode. !

!--------------------!--------------------------------------------------------!

! Radio altitude ! - Green, size 3mm : radio altitude between 400 and !

! ! 2500ft. !

! ! - Green, size 4mm : under 400ft., above DH+100ft. !

! ! - Amber, size 4mm : either RA under DH+100ft., or !

! ! invalid DH and RA under 400ft. !

! ! - Not excessive attitude condition. !

!--------------------!--------------------------------------------------------!

! Decision height ! - DH amber flashing when radio altitude goes under !

! (DH) ! decision then steady. !

!--------------------!--------------------------------------------------------!

! Side Stick Order ! - On the ground, at least one engine running. !

! ! - Roll and pitch command position valid. !

! ! - NLG compressed. !

!--------------------!--------------------------------------------------------!

! Protection marks ! - Only if valid attitude. !

! ! - Green dashes when roll protection in normal law. !

!--------------------!--------------------------------------------------------!

! Target side slip ! - Cyan trapezo??dal index below the roll angle in case !

! ! of engine failure, presenting the difference between !

! ! estimated side slip and target side slip. !

!-----------------------------------------------------------------------------!

! Yaw Bar ! - valid attitude (and not excessive) !

! ! - FD1 and FD2 engaged !

! ! - Yaw FD from FMGC valid !

! ! - RWY or ROLL OUT modes !

The table below gives the conditions of display of the attitude flags:

-------------------------------------------------------------------------------

! FLAGS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! ATT ! Red flag replacing the whole attitude display when !

! ! attitude is invalid, flashing during 2s then steady. !

! ! This flag disappears when DMC is supplied again with !

! ! healthy pitch and roll data. !

!--------------------!--------------------------------------------------------!

! FPV ! Red flag under initial position of horizon line (has a !

! ! steady position and does not follow pitch and roll !

! ! variations). It is displayed in TRK/FPA mode when !

! ! attitude is valid but drift angle or flight path angle !

! ! are not valid. !

!--------------------!--------------------------------------------------------!

! FD ! Red flag in left upper corner of upper sector of pitch !

! ! scale. It is displayed when FD pushbutton switch light !

! ! is on on FCU, attitude is valid and not excessive, and !

! ! besides, both FMGC are seen invalid or both FD are !

! ! disengaged. !

! ! This flag flashes during 9s then is steady. !

!--------------------!--------------------------------------------------------!

! CHECK ATT ! Amber message under upper limit of upper sector of !

! ! pitch scale. It is displayed when there is attitude !

! ! discrepancy between CAPT and F/O PFD or discrepancy !

! ! between input and displayed pitch or roll. !

! ! This flag flashes during 9s then is steady. !

!--------------------!--------------------------------------------------------!

! SI ! Red flag instead of lateral acceleration index when !

! ! lateral acceleration is invalid on the ground or !

! ! estimated side slip and lateral acceleration are !

! ! invalid in flight. !

!--------------------!--------------------------------------------------------!

! RA ! Red flag on the lower sector when both radio altimeters!

! ! are invalid, altitude is not excessive and the aircraft!

! ! is in clean configuration. !

!--------------------!--------------------------------------------------------!

! DH ! Amber message in lower part of attitude scale when !

! ! attitude is not excessive, DH and RA are both valid !

! ! and DH>RA. !

! ! This flag flashes during 3s then is steady. !

The table below gives the conditions of display of the attitude flags:

-------------------------------------------------------------------------------

! FLAGS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! ATT ! Red flag replacing the whole attitude display when !

! ! attitude is invalid, flashing during 9s then steady. !

! ! This flag disappears when DMC is supplied again with !

! ! healthy pitch and roll data. !

!--------------------!--------------------------------------------------------!

! FPV ! Red flag under initial position of horizon line (has a !

! ! steady position and does not follow pitch and roll !

! ! variations). It is displayed in TRK/FPA mode when !

! ! attitude is valid but drift angle or flight path angle !

! ! are not valid. !

! ! This flag flashes 9s then steady. !

!--------------------!--------------------------------------------------------!

! FD ! Red flag in left upper corner of upper sector of pitch !

! ! scale. It is displayed when FD pushbutton switch light !

! ! is on on FCU, attitude is valid and not excessive, and !

! ! besides, both FMGC are seen invalid or both FD are !

! ! disengaged. !

! ! This flag flashes during 9s then is steady. !

!--------------------!--------------------------------------------------------!

! CHECK ATT ! Amber message under upper limit of upper sector of !

! ! pitch scale. It is displayed when there is attitude !

! ! discrepancy between CAPT and F/O PFD or discrepancy !

! ! between input and displayed pitch or roll. !

! ! This flag flashes during 9s then is steady. !

!--------------------!--------------------------------------------------------!

! SI ! Red flag instead of lateral acceleration index when !

! ! lateral acceleration is invalid on the ground or !

! ! estimated side slip and lateral acceleration are !

! ! invalid in flight. !

! ! This flag flashes 9s then steady. !

!--------------------!--------------------------------------------------------!

! RA ! Red flag on the lower sector when both radio altimeters!

! ! are invalid, altitude is not excessive !

! ! This flag flashes 9s then steady. !

!--------------------!--------------------------------------------------------!

! DH ! Amber message in lower part of attitude scale when !

! ! attitude is not excessive, DH and RA are both valid !

! ! and DH>RA. !

! ! This flag flashes during 9s then is steady. !

!--------------------!--------------------------------------------------------!

! CHECK PFD CAPT ! Amber message above the attitude zone or above the !

! ! heading scale. !

! CHECK ND CAPT ! It is displayed when there is a discrepancy between !

! CHECK PFD FO ! what is computed by the DMC and what is displayed on !

! CHECK ND FO ! the related PFD (ND,EWD,SD). !

! CHECK EWD ! This message flashes for 9s then is steady. !

-------------------------------------------------------------------------------

! FLAGS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! WINDSHEAR ! Red message above the A/C symbol (left part). !

! ! It is displayed when a windshear condition is detected !

! ! It appears for at least 15 s. !

-------------------------------------------------------------------------------

! FLAGS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! W/S AHEAD ! Red message above the A/C symbol (left part) displayed !

! ! when a predictive W/S level 3 alert is computed. !

! ! The message is amber if the alert is of level 2. !

-------------------------------------------------------------------------------

! FLAGS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! WINDSHEAR ! Red message above the A/C symbol (left part). !

! ! It is displayed when a windshear condition is detected !

! ! This message flashes 9s then steady. !

! ! It appears for at least 15 s. !

-------------------------------------------------------------------------------

! FLAGS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! W/S AHEAD ! The message above the A/C symbol (left part) flashes !

! ! for 9s then steady if a predictive windshear condition !

! ! is detected, and in the following main conditions: !

! ! - WXR unit with winndshear function installed !

! ! - windshear P/B SW on (AUTO/OFF P/B SW on WXR control !

! ! unit) !

! ! - valid WXR !

! ! - no reactive windshear condition. !

! ! The message is : !

! ! - amber for a level 2 alert !

! ! - red for a level 3 alert. !

C. Heading

PFD - Heading Presentation ** ON A/C NOT FOR ALL

item (a)
The heading scale presents the aircraft actual magnetic heading in analog form.

PFD - Heading Presentation ** ON A/C NOT FOR ALL

item (a)
The heading scale presents the aircraft actual magnetic heading in analog form.

(1) Scale description

PFD - Heading Presentation ** ON A/C NOT FOR ALL

item (b)
The scale comprises white reference bars and associated heading values for each 10 degrees, written in small size. Each value which is multiple of 30 degrees is written with larger size characters.
The displayed portion of the heading scale represents plus or minus 24 degrees with respect to the aircraft present magnetic heading values.
True heading

PFD - Heading Presentation ** ON A/C NOT FOR ALL

Above 73° North and 60° South, the TRU indication comes on white above and on the right hand of the heading scale.

(2) Scale description

PFD - Heading Presentation ** ON A/C NOT FOR ALL

Above 73° North and 60° South, the TRUE indication comes on white above and at the centre of the heading scale. Depending on the PP-POLARNAV pin program, this is performed either manually by the crew (NORTH REF P/BSW on the TRUE position) or automatically by the ADIRUs when the aircraft reaches the polar zone. In such a case, a cyan TRUE message appears in a cyan box above the heading reference line (the LOC scale being displayed or not). In automatic or manual true heading configuration, at slats extension, the TRUE message and its box flashe for 10s then remain steady.

(3) Selections and figurations

(a) Heading - V/S Mode

PFD - Selections and Figurations ** ON A/C NOT FOR ALL

items (a)
A green diamond shaped symbol represents the aircraft actual track. A cyan triangular symbol indicates the selected heading or track provided that a heading or track value is displayed in the FCU dedicated counter. This symbol is replaced by digits on the right hand or the left hand of the heading scale when the selected value is outside the displayed portion of the heading.

(b) ILS Approach

PFD - Selections and Figurations ** ON A/C NOT FOR ALL

item (b)
In ILS approach, when the ILS pushbutton switch is pressed (pushbutton switch light on), the ILS course or QFU is displayed on the heading scale by means of a magenta dagger shaped symbol.
The QFU symbol is replaced by digits on the right hand or the left hand of the heading scale when the ILS course value is outside the displayed range of the heading.

PFD - Selections and Figurations ** ON A/C NOT FOR ALL

item (c)
In case of failure of the magnetic heading, a red flag flashing for 9s then
steady is displayed at the location of the heading scale.
ITEM LIST

PFD - Selections and Figurations ** ON A/C NOT FOR ALL

-----------------------------------------------------------------------------

ITEM PARAMETER EQUIPMENT LABEL COLOUR

-----------------------------------------------------------------------------

REFERENCE LINE FCU 274 YELLOW

SELECTED HEADING FCU 101 CYAN

QFU ILS 105 MAGENTA

TRACK ADIRU IRS 317 GREEN

SELECTED TRACK FCU 114 CYAN

HEADING SCALE ADIRU IRS 320 WHITE

(4) The table below gives the conditions of display of the heading information:

-------------------------------------------------------------------------------

! PARAMETERS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! Heading reference ! - Yellow. !

! line ! - Magnetic heading valid. !

!--------------------!--------------------------------------------------------!

! Actual track ! - Green. !

! ! - Magnetic heading and magnetic track angle valid. !

!--------------------!--------------------------------------------------------!

! Selected track or ! - If magnetic heading valid : !

! heading ! - selected heading when in HDG/V/S mode !

! ! - selected track when in TRK/FPA mode. !

! ! - Cyan triangle if the difference between selected !

! ! heading/track and actual heading is between -24° and !

! ! +24° (these values excluded). !

! ! - If the difference is above +24°, cyan digits on the !

! ! right side of the heading scale. !

! ! - If the difference is below -24°, cyan digits on the !

! ! left side of the heading scale. !

!--------------------!--------------------------------------------------------!

! QFU index ! - ILS P/B switch pressed on FCU. !

! ! - Magnetic heading valid. !

! ! - If runway heading is memorized, ILS course if ILS !

! ! frequency is valid, otherwise memorized ILS course. !

! ! - Magenta dagger-shaped symbol if the difference !

! ! between QFU and actual magnetic heading is between !

! ! -24° and +24° (these values excluded). !

! ! - If the difference is above +24°, magenta digits on !

! ! the right side of the heading scale. !

! ! - If the difference is below -24°, magenta digits on !

! ! the left side of the heading scale !

(5) The table below gives the conditions of display of the heading flags:

-------------------------------------------------------------------------------

! FLAGS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! CHECK HDG ! - Amber message at the center of the heading scale !

! ! when magnetic heading is valid and when there is a !

! ! discrepancy between CAPT and F/O heading indications.!

!--------------------!--------------------------------------------------------!

! HDG ! - Red flag replacing the whole heading scale when !

! ! magnetic heading is not valid. !

! ! This flag flashes during 9s then is steady. !

(6) The table below gives the conditions of display of the heading flags:

-------------------------------------------------------------------------------

! FLAGS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! CHECK HDG ! - Amber message at the center of the heading scale !

! ! when magnetic heading is valid and when there is a !

! ! discrepancy between CAPT and F/O heading indications.!

! ! This message flashes 9s then steady. !

!--------------------!--------------------------------------------------------!

! HDG ! - Red flag replacing the whole heading scale when !

! ! magnetic heading is not valid. !

! ! This flag flashes during 9s then is steady. !

!--------------------!--------------------------------------------------------!

! PFD 1 (2 or 3) ! - Magenta message showing above the heading scale !

! ! which DMC drives the DU displaying the message, !

! ! in the test mode on ground. !

D. Altitude

PFD - Altitude Presentation ** ON A/C NOT FOR ALL

PFD - Altitude Indications Display ** ON A/C NOT FOR ALL

The altitude scale presents the aircraft actual altitude according to a baro setting reference. Different displays are presented depending on this reference (standard or baro corrected).
The altitude value is transmitted by the ADIRU on label 203 (standard altitude) and on label 204 (baro altitude) on CAPT side or on label 220 (baro altitude) on F/O side.

(1) Scale Description

PFD - Altitude Presentation ** ON A/C NOT FOR ALL

PFD - Altitude Indications Display ** ON A/C NOT FOR ALL

Item (a)
The altitude indication is provided by means of a tape moving up and down with respect to a window within which the aircraft actual altitude is displayed.
The tape of the scale is graduated every 100 ft. and digital values are displayed every 500 ft. in hundreds.
The aircraft actual altitude is provided by a counter located at the middle of the scale in which the actual value is displayed in green digits.
The hundreds of feet are written in a large size whereas the tens and units are displayed by a drum operating as a classical mechanical altimeter.
Small white marks are positioned in front of every number on the tape.

(2) Negative Altitude

PFD - Altitude Presentation ** ON A/C NOT FOR ALL

Item (b)
If the altitude is negative, a NEG white message is added at the left side of the digital value (instead of the 10 thousand digit). The digital value is limited to minus 15000 ft.
When the altitude is negative, the classical mechanical altimeter moves in the same way but all the scale are opposite (without sign).

(3) Altitude Alerts
When the A/C approaches a selected altitude or flight level, the altitude counter window pulses as long as the A/C is within the boundaries : (sel alt -750 ft., sel alt -250 ft.) or (sel alt +250 ft., sel alt +750 ft).
If the A/C diverts from the altitude which is selected on the FCU as the difference (sel alt - actual altitude) exceeds 250 feet, the altitude counter window (box) constantly flashes in amber color.

(4) Non Precision Approach
If the pilot performs a non precision approach and reaches or goes below the MDA (Minimum Descent Altitude), the altitude digits change from green to amber.

(5) Selected Altitude

PFD - Altitude Selected Display ** ON A/C NOT FOR ALL

The selected altitude value is displayed by means of a dedicated symbol in cyan transmitted by the FCU on label 102

PFD - Altitude Selected Display ** ON A/C NOT FOR ALL

item (b).
When the selected value is outside the displayed portion of the scale it is displayed either above or below the scale. This value is indicated either in feet when the baro setting is the corrected one or in hundreds of feet when the setting is the standard one
The selected altitude value is set by the pilot by means of a dedicated selector knob located on the FCU

PFD - Altitude Selected Display ** ON A/C NOT FOR ALL

item (a).
When the A/C reaches a selected altitude, the selected altitude symbol and the associated digital value go behind the window of the altitude counter.
When the FMGC operates in vertical auto control, if altitude constraints are included in the flight plan, they replace the FCU altitude selection. The FMGC sends the value for the dedicated symbol on the label 164. The selected altitude value and the associated symbol change from cyan to magenta.

(6) Selected Altitude

PFD - Altitude Selected Display ** ON A/C NOT FOR ALL

The selected altitude value is displayed by means of a dedicated symbol in cyan transmitted by the FCU on label 102

PFD - Altitude Selected Display ** ON A/C NOT FOR ALL

PFD - METRIC ALTITUDE ** ON A/C NOT FOR ALL

PFD - Other Altitude Indications ** ON A/C NOT FOR ALL

(7) Selected Altitude

PFD - Altitude Selected Display ** ON A/C NOT FOR ALL

The selected altitude value is displayed by means of a dedicated symbol in cyan transmitted by the FCU on label 102

PFD - Altitude Selected Display ** ON A/C NOT FOR ALL

(8) Altitude Setting Reference
Two different possibilities are offered to the pilot regarding the baro setting reference. The selection is performed on the FCU thanks to a baro reference selector knob

PFD - Altitude Setting Reference ** ON A/C NOT FOR ALL

item (a).
By pulling the knob, the pilot selects the standard baro setting i.e 1013 hpa. A yellow box surrounding a STD message is displayed below the scale

PFD - Altitude Setting Reference ** ON A/C NOT FOR ALL

item (b).
By pressing the baro reference selector knob the pilot selects baro setting whose value can be adjusted by turning the knob. This pressure is a QNH reference. Regarding this baro corrected reference, the unit can be Hpa or inches of mercury (In.Hg)

PFD - Altitude Setting Reference ** ON A/C NOT FOR ALL

item (c).
When the A/C flies above the transition altitude and the altitude scale still displays a baro corrected altitude (QNH), the baro setting value and the QNH message displayed below the scale flashes to signal the pilot to change to STD baro setting. Reciprocally, if the A/C flies below the transition level with a display of the standard altitude scale the STD message below the scale flashes as described previously signalling the pilot to change the baro setting to the corrected one . It has to be notified that when the pilot changes the baro setting reference from the STD reference to the corrected one the pressure reference value is the standard value i.e 1013 Hpa. He has to adjust the right value through the FCU.

(9) Linear Vertical Deviation

PFD - Other Altitude Indications ** ON A/C NOT FOR ALL

item (a)
In descent, a filled magenta circle indicates the linear vertical deviation with respect to the FMGC computed theoretical vertical flight path. It is presented from the top of descent down to the final intercept altitude.
The value displayed is transmitted by the FMGC on the label 125.

(10) Radio Altitude Analog Indication

PFD - Other Altitude Indications ** ON A/C NOT FOR ALL

item (b)
When below 2500 ft. a digital radio height indication is displayed on the attitude scale.
In the same way on the altitude tape when the altitude is less than 570 ft, an analog indication is displayed on the altitude scale by means of a red ribbon located along the right hand side of the tape.
The distance between the top of the ribbon and the center of the altitude window represents the A/C actual radio altitude. In case of failure of the radio altimeter a dedicated flag is presented in the lower sector of the altitude window.
The value displayed for the radio altitude is transmitted by the radioaltimeter on the label 164.

(11) Check Altitude

PFD - Other Altitude Indications ** ON A/C NOT FOR ALL

item (c)
ITEM LIST

PFD - Other Altitude Indications ** ON A/C NOT FOR ALL

-----------------------------------------------------------------------------

ITEM PARAMETER EQUIPMENT LABEL COLOUR

-----------------------------------------------------------------------------

RADIO ALTITUDE RA 164 RED

LINEAR VERTICAL DEVIATION FMGC EIS 125 MAGENTA

LANDING ELEVATION FIELD FMGC 256 BROWN

(12) Linear vertical deviation

LINEAR DEVIATION INDICATION ** ON A/C NOT FOR ALL

In descent, a filled green circle indicates the linear vertical deviation with respect to the FMGC computed theoretical vertical flight path. It is presented from the top of the descent to the final intercept altitude when:

(a) The linear deviation from FMGEC is valid.

(b) The difference between the theoretical flight plan altitude and the aircraft current altitude is between -540 ft and +540 ft.
When the difference between flight plan altitude and the aircraft current altitude is more than 540 ft, the linear deviation is displayed as a green filled half-circle on a fixed position close to the extremity of the altitude scale.
The value displayed is transmitted by the FMGC on the label 125.

(13) Radio altitude analog indication

PFD - Other Altitude Indications ** ON A/C NOT FOR ALL

item (a)
When below 2500 ft., a digital radio height indication is displayed on the attitude scale.
In the same way, on the altitude tape when the altitude is less than 570 ft., an analog indication is displayed on the altitude scale by means of a red ribbon located along the right hand side of the tape.
The distance between the top of the ribbon and the center of the altitude window represents the A/C actual radio altitude. In case of failure of the radio altimeter, a dedicated flag is displayed in the lower sector of the altitude window.
The value displayed for the radio altitude is transmitted by the radio altimeter on the label 164.

(14) Check altitude

PFD - Other Altitude Indications ** ON A/C NOT FOR ALL

item (b)
In case of discrepancy between the altitude given by the CAPT air data source and the altitude given by the F/O air data source, a CHECK ALT amber message is presented on the right side of the altitude scale.
This message flashes for 9 seconds then steady( ALT discerpancy can be due to the display system or due to the sensors).

ITEM LIST

-----------------------------------------------------------------------------

ITEM PARAMETER EQUIPMENT LABEL COLOUR

-----------------------------------------------------------------------------

RADIO ALTITUDE RA 164 RED

LINEAR VERTICAL DEVIATION FMGC EIS 125 GREEN

LANDING ELEVATION FIELD FMGC 256 BROWN

E. Altitude Data - Back-up altitude scale

Back-Up GPS Altitude Scale ** ON A/C NOT FOR ALL

The Back-up GPS altitude scale is shown when:

The Back-up Speed Scale function is installed.
The GPS option is installed.
All the three ADR are OFF and the BUSS pushbutton is not installed or the BUSS is manually activated.
With ADR monitoring functionality, a GPS altitude is provided by the IRS.
The back-up altitude scale is built with the following characteristics:
The two last digits are dashed with two thin amber lines to point out the accuracy loss between the GPS altitude and the barometric one (item 1)
A white "GPS ALT" message is displayed under the scale instead of the QNH reference (item 3)
This is reinforced by a white GPS indication at the right side of the altitude drum (item 2)
No barometric references are available but only GPS altitude and radio altimeter
Linear deviation, MDA and MDH, constraint altitude, vertical speed scale and TCAS data are inhibited, however selected altitude, radio height indication and landing elevation still may be displayed
Feedback monitoring of altitude is inhibited.

(1) MDA/MDH indication

PFD - MDA/MDH indication ** ON A/C NOT FOR ALL

MDA/MDH is only displayed if QFE/QNH pin proram is active. It is represented by an amber ribbon going from the ground altitude to the MDA/MDH value.
The table below gives the conditions of display:

-------------------------------------------------------------------------------

! PARAMETERS ! DISPLAY !

!---------------------!-------------------------------------------------------!

! RA valid and not ! This ribbon is displayed from the top of the RA !

! NCD ! ribbon(bottom of the scale if RA is outside the !

! ! scale) if: !

! !- MDA/MDH is valid and its value is inside the !

! ! displayed area of the scale. !

!---------------------!-------------------------------------------------------!

! RA not valid or ! This ribbon is displayed from the landing elevation !

! NCD, and QNH ref. ! symbol (bottom of the scale if landing elevation is !

! selected ! outside of the scale) if: !

! ! - MDA/MDH is valid and is inside the displayed area of!

! ! the scale, and !

! ! - flight phase is 7 or 8, and !

! ! - aircraft is not in standard reference, and !

! ! - landing elevation is valid. !

-------------------------------------------------------------------------------

! RA not valid or NCD,! This ribbon is displayed from 0 feet graduation !

! and QFE reference ! (bottom of the scale if 0 ft graduation is outside !

! selected ! the scale) if: !

! ! - MDA/MDH is valid and is inside the displayed area of!

! ! the scale, and !

! ! - flight phase is 7 or 8, and !

! ! - aircraft is not in standard reference. !

(2) MDA/MDH indication

PFD - MDA/MDH indication ** ON A/C NOT FOR ALL

MDA/MDH is only displayed if QFE/QNH pin program is active. It is represented by an amber bug at the MDA/MDH value.
The table below gives the conditions of display:

-------------------------------------------------------------------------------

! PARAMETERS ! DISPLAY !

!---------------------!-------------------------------------------------------!

! RA valid and not ! The bug is displayed at the MDA/MDH value if: !

! NCD ! - MDA/MDH is valid and its value is inside the !

! ! displayed area of the scale, and !

! ! - Back-up GPS altitude is not activated or BUSS is !

! ! manually activated via the specific push-button. !

! ! !

!---------------------!-------------------------------------------------------!

! RA not valid or ! The bug is displayed at the MDA value if: !

! NCD, and QNH ref. ! - MDA is valid and is inside the displayed area of !

! selected ! the scale, and !

! ! - flight phase is 7 or 8, and !

! ! - aircraft is not in standard reference, and !

! ! - landing elevation is valid, and !

! ! - Back-up GPS altitude is not activated or BUSS is !

! ! manually activated via the specific push-button. !

-------------------------------------------------------------------------------

! RA not valid or NCD,! The bug is displayed at the MDH value if: !

! and QFE reference ! - MDH is valid and is inside the displayed area of!

! selected ! the scale, and !

! ! - flight phase is 7 or 8, and !

! ! - aircraft is not in standard reference, and !

! ! - Back-up GPS altitude is not activated or BUSS is !

! ! manually activated via the specific push-button. !

F. Altitude Data - Condition of Display
The table below gives the conditions of display of the altitude information:

-------------------------------------------------------------------------------

! PARAMETERS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! Altitude scale ! - White. !

! ! - Upper and lower values white, red when altitude is !

! ! not valid. !

!--------------------!--------------------------------------------------------!

! Actual altitude ! - Green if altitude (standard or baro) is valid. !

! (digital value) ! - Amber when altitude is below MDA. !

! ! - Actual altitude is not displayed if altitude is not !

! ! valid. !

! ! - Altitude reference line yellow. !

-------------------------------------------------------------------------------

! PARAMETERS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! Baro correction ! - If standard altitude used (selected on FCU) : STD !

! ! cyan in a yellow box, flashing when actual altitude !

! ! is below transition altitude. !

! ! - If baro altitude used (selected on FCU) : QNH white !

! ! below the correction value. !

! ! - The correction value is displayed in Hpa or inches !

! ! of Hg according to FCU selection (in cyan colour). !

! ! - The selected baro reference and the digital value !

! ! are both flashing when actual altitude is above !

! ! transition altitude. !

-------------------------------------------------------------------------------

! PARAMETERS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! Baro correction ! - If standard altitude used (selected on FCU) : STD !

! ! cyan in a yellow box, flashing when actual altitude !

! ! is below transition altitude. !

! ! - If baro altitude used (selected on FCU) : QNH or QFE !

! ! (This last displayed in a white box ) white below !

! ! the correction value. !

! ! - The correction value is displayed in Hpa or inches !

! ! of Hg according to FCU selection (in cyan colour). !

! ! - The selected baro reference and the digital value !

! ! are both flashing when actual altitude is above !

! ! transition altitude. !

!--------------------!--------------------------------------------------------!

! Landing elevation ! - brown ribbon on altitude scale when baro altitude !

! (ground reference) ! is used, landing elevation is valid and the !

! ! difference between landing elevation and actual !

! ! altitude is less than 570 ft. Moreover, landing !

! ! elevation is displayed only during flight phases !

! ! 7 and 8. !

-------------------------------------------------------------------------------

! PARAMETERS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! Altitude digital ! - Yellow when actual altitude is between the boundaries!

! readout window ! (sel alt. -250ft., sel alt. +250ft.). !

! ! - Pulsing in yellow when actual altitude is outside !

! ! the above interval, but gets closer to selected !

! ! altitude. !

! ! - Flashing in amber when actual altitude is outside !

! ! the above interval and the difference with selected !

! ! altitude increases. !

!--------------------!--------------------------------------------------------!

! Selected altitude ! - Cyan if altitude is selected on FCU. !

! ! - Magenta if altitude constraint comes from FMGC. !

! ! When the value is within the boundaries (actual !

! ! altitude -575ft., actual altitude +575ft.), it is !

! ! boxed by the selected altitude symbol, in the same !

! ! color. !

! ! Out of these boundaries, the digital value is !

! ! displayed above or below the altitude scale according!

! ! to the difference with actual altitude. !

! ! Baro altitude is displayed in feet, standard altitude!

! ! is displayed in hundreds of feet. !

-------------------------------------------------------------------------------

! PARAMETERS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! Radio altitude ! - Red ribbon located on the right side of the altitude !

! reference ! scale when radio altitude is valid. !

!--------------------!--------------------------------------------------------!

! Linear deviation ! - Filled magenta circle when flight path altitude is !

! with respect to ! valid. !

! vertical profile ! !

-------------------------------------------------------------------------------

! PARAMETERS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! Radio altitude ! - Red ribbon located on the right side of the altitude !

! reference ! scale when radio altitude is valid. !

!--------------------!--------------------------------------------------------!

! Linear deviation ! - Filled green circle when flight path altitude is !

! with respect to ! valid. !

! vertical profile ! !

PFD - Other Altitude Indications ** ON A/C NOT FOR ALL

PFD - METRIC ALTITUDE ** ON A/C NOT FOR ALL

Depending on the pin program installed, the pilot selects the metric reference on the FCU for the alitude indication.
In this case:

The actual/current altitude value im meters is displayed inside a yellow box below the altitude setting reference.The digits are green when the value is greater than MDA and amber when it is less.
Altitude in meters is displayed equivalent in meters (-1500 FT and 50000 FT) on five digits with minus sign when necessary by a step of 10 meters.
The selected altitude in meters is displayed in cyan at the left top of the altitude scale when the altitude is selected on the FCU and is valid. The digits are displayed in magenta when the altitude is controlled by the FMGC.
The selected altitude in meters is displayed on five digits and can vary from 0 to 18000 meters by a step of 10 meters.

PFD - Landing elevation symbol ** ON A/C NOT FOR ALL

-------------------------------------------------------------------------------

! PARAMETERS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! Landing elevation ! - brown ribbon on altitude scale when baro altitude !

! (ground reference) ! is used, landing elevation is valid and the !

! ! difference between landing elevation and actual !

! ! altitude is less than 570 ft. Moreover, landing !

! ! elevation is displayed only during flight phases !

! ! 7 and 8. !

-------------------------------------------------------------------------------

! PARAMETERS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! Landing elevation ! - brown ribbon on altitude scale when baro altitude !

! (ground reference) ! is used (only when QNH baro setting is used), !

! ! landing elevation is valid and the difference !

! ! between landing elevation and actual altitude is !

! ! less than 570 ft. Moreover, landing elevation is !

! ! displayed only during flight phases 7 and 8. !

The table below gives the conditions of display of the altitude flags:

-------------------------------------------------------------------------------

! FLAGS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! ALT ! - Red flag replacing altitude scale when either baro !

! ! altitude is selected from FCU and no baro altitude !

! ! signal is valid or no standard altitude is selected !

! ! from FCU and standard altitude signal is valid. !

! ! - This flag flashes during 9s then is steady. !

!--------------------!--------------------------------------------------------!

! ALT SEL ! - Red flag on top of the altitude scale when neither !

! ! the selected altitude from the FCU, nor the altitude !

! ! constraints from the FMGC are valid. !

!--------------------!--------------------------------------------------------!

! CHECK ALT ! - Amber message on the right side of the altitude scale!

! ! when there is a discrepancy between displayed !

! ! altitude value and the actual altitude. !

The table below gives the conditions of display of the altitude flags:

-------------------------------------------------------------------------------

! FLAGS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! ALT ! - Red flag replacing altitude scale when either baro !

! ! altitude is selected from FCU and no baro altitude !

! ! signal is valid or standard altitude is selected !

! ! from FCU and no standard altitude signal is valid. !

! ! - This flag flashes during 9s then is steady. !

!--------------------!--------------------------------------------------------!

! ALT SEL ! - Red flag on top of the altitude scale when neither !

! ! the selected altitude from the FCU, nor the altitude !

! ! constraints from the FMGC are valid. !

! ! - This flag flashes 9s then steady. !

!--------------------!--------------------------------------------------------!

! CHECK ALT ! - Amber message on the right side of the altitude scale!

! ! when there is a discrepancy between displayed !

! ! altitude value and the actual altitude. !

! ! - This message flashes 9s then steady. !

G. Airspeed

PFD - Airspeed Presentation ** ON A/C NOT FOR ALL

The speed scale, in the left part of the PFD contains all the airspeed data displayed on a conventional airspeed indicator plus significant limits, protection and target speeds.

(1) Computed Airspeed (Vc)

PFD - Vc Indication Display ** ON A/C NOT FOR ALL

The Vc indication is displayed in analog form by means of a tape with graduations every 10 kts and digital values every 20 kts. This tape moves up and down so as to indicate the aircraft actual speed value in front of a fixed yellow reference line.
This reference line is made up of two yellow dashes linked together by means of a thin yellow line and completed with a yellow triangle.
The displayed part of the scale represents an 84 kts range. The scale is graduated from 30 kts to 520 kts and the digital values from 40 to 520 kts.
In no case can the displayed Vc be lower than 30 kts.
The value for the displayed Vc is transmitted by the ADIRU on the label 206.

(2) Vc Trend

PFD - Vc Indication Display ** ON A/C NOT FOR ALL

This yellow arrow gives an analog display of the Vc trend. The head of the arrow points on the scale to the indication of the Vc value which will be reached in 10 s if the aircraft keeps its present acceleration.
This symbol is presented if the speed difference exceeds a 2 kts threshold and it is removed when the speed difference becomes less than 1 kt.
speed difference is absolute value of: (speed in 10 s minus actual speed).
The gradient for the display of the symbol is limited to 12 kts/s.
The value for the displayed Vc trend is transmitted by the FAC on the label 262.

(3) Computed Airspeed (Vc)

PFD - Vc Indication Display ** ON A/C NOT FOR ALL

The Vc indication is displayed in analog form by means of a tape with graduations every 10 kts and digital values every 20 kts. This tape moves up and down so as to indicate the A/C actual speed value in front of a fixed yellow reference line.
This reference line is made up of two yellow dashes linked together by means of a thin yellow line and completed with a yellow triangle.
The displayed part of the scale represents an 84 kts range. The scale is graduated from 30 kts to 660 kts and the digital values from 40 to 660 kts.
In no case can the displayed Vc be lower than 30 kts.
The value for the displayed Vc is transmitted by the ADIRU on the label 264 if available, 206 else.

(4) Vc Trend

PFD - Vc Indication Display ** ON A/C NOT FOR ALL

This yellow arrow gives an analog display of the Vc trend. The head of the arrow points on the scale to the indication of the Vc value which will be reached in 10 s if the A/C keeps its present acceleration.
This symbol is presented if the speed difference exceeds a 2 kts threshold and it is removed when the speed difference becomes less than 1 kt.
speed difference is absolute value of: (speed in 10 s minus actual speed).
The gradient for the display of the symbol is limited to 12 kts/s.
The value for the displayed Vc trend is transmitted by the FAC on the label 262.

(5) Selected Speed (Vsel)
A cyan triangular symbol indicates on the Vc scale the selected speed. That speed is:

either the speed elaborated by the FMGC in speed auto control (the symbol changes from cyan to magenta if that speed is a constrained speed)
PFD - Selected Speed Display ** ON A/C NOT FOR ALL
PFD - Selected Speed Display ** ON A/C NOT FOR ALL
item (a),
or the speed selected on the FCU and validated by pulling the speed knob, or automatically chosen if the 2 FMGCs have failed
PFD - Selected Speed Display ** ON A/C NOT FOR ALL
PFD - Selected Speed Display ** ON A/C NOT FOR ALL
item (b).

If the selected speed is outside the displayed portion of the Vc scale, it is presented in digital form, written just above or just below the scale according to the sign of the difference (Vsel -Vc).

In descent mode, with the ECON mode, the selected speed symbol is different: it indicates the range of possible speed values
PFD - Selected Speed Display ** ON A/C NOT FOR ALL
PFD - Selected Speed Display ** ON A/C NOT FOR ALL
item (c).
If the range of possible speed values is outside the displayed portion of the Vc scale:
- if Vc less than (minimum possible speed value -42 kts), that minimum possible speed is indicated in digital form below the Vc scale
PFD - Selected Speed Display ** ON A/C NOT FOR ALL
PFD - Selected Speed Display ** ON A/C NOT FOR ALL
item (d).
- if Vc more than (maximum possible speed value +42 kts), that maximum possible speed is indicated in digital form above the Vc scale
PFD - Selected Speed Display ** ON A/C NOT FOR ALL
PFD - Selected Speed Display ** ON A/C NOT FOR ALL
item (e).

The selected speed information (from FMGC or FCU) is always displayed.
The selected speed is the speed corresponding to the selected mach number with the AFS operating in mach mode.

ITEM LIST

PFD - Selected Speed Display ** ON A/C NOT FOR ALL

-----------------------------------------------------------------------------

ITEM PARAMETER EQUIPMENT LABEL COLOUR

-----------------------------------------------------------------------------

V SEL FMGC 103 CYAN

V SEL FCU 103 or MAGENTA

IV SEL RNGH FMGC 307 CYAN

IV SEL RNGL FMGC 306 CYAN

(6) Selected Speed (Vsel)
A triangular symbol indicates on the Vc scale the selected speed. That speed is:

either the speed elaborated by the FMGC in speed auto control. The symbol is then magenta.
PFD - Selected Speed Display ** ON A/C NOT FOR ALL
item (a).
or the speed selected on the FCU and validated by pulling the speed knob, or automatically chosen if the 2 FMGCs have failed. The symbol is then cyan.

If the selected speed is outside the displayed portion of the Vc scale, it is presented in digital form, written just above or just below the scale according to the sign of the difference (Vsel -Vc).
In case when, RTA managed speed condition is detected, the letter "R" is displayed in magenta next to the triangular symbol for selected speed or next to numerical indication if the selected speed is outside the displayed portion of the Vc scale.
In case of selected speed failure, a red SPD SEL flag is displayed above the scale and the letter "R" is inhibted.(item b)

In descent mode, with the ECON mode, the selected speed can be displayed by high and low margins on the speed scale.They indicate the range of the possible speed values.
The high and low margins are represented by two bars displayed in magenta when both margins and Vc are valid.Each margin must be between (Vc - 42 kts) and (Vc + 42 kts) to be displayed.
In case when, RTA managed speed condition is detected, the letter "R" is displayed in magenta next to the selected speed in descend mode only if the triangular symbol is displayed.
The selected speed information (from FMGC or FCU) is always displayed.
The selected speed is the speed corresponding to the selected mach number with the AFS operating in mach mode.

ITEM LIST

PFD - Selected Speed Display ** ON A/C NOT FOR ALL

-----------------------------------------------------------------------------

ITEM PARAMETER EQUIPMENT LABEL COLOUR

-----------------------------------------------------------------------------

V SEL FMGC 103 CYAN

V SEL FCU 103 or MAGENTA

IV SEL RNGH FMGC 307 MAGENTA

IV SEL RNGL FMGC 306 MAGENTA

(7) Decision Speed (V1)

PFD - V1 Display ** ON A/C NOT FOR ALL

The V1 indication which is entered before take-off through the MCDU (take-off page), is displayed in cyan color by means of a mark across the scale and a 1 figure. If the V1 value is outside the displayed portion of the Vc scale, the mark and the 1 are replaced by the digital value of V1 written at the top of the scale.
V1 (symbol or digits) is displayed only on the ground.

(8) Rotation Speed (VR)
The VR indication which is entered before take-off through the MCDU, is displayed by means of cyan circle.
The VR symbol is displayed when label is valid and on ground.

(9) Mach Number

PFD - Mach Number Display ** ON A/C NOT FOR ALL

When the mach number is above 0.5 it is displayed just below the speed scale in green color. In case of failure, a red MACH flag is presented.

(10) Mach Number

PFD - Mach Number Display ** ON A/C NOT FOR ALL

The mach number is displayed under following conditions:

Mach number is valid.
Mach number is above 0.5 in acceleration or above 0.45 in deceleration.
BUSS is not manually activated through the specific pushbutton.
It is displayed just below the speed scale in green color. In case of failure, a red MACH flag is presented.

(11) Limit Speeds
The following flight envelope protection speeds are displayed through the appropriate symbols according to the flight phase and the A/C configuration. They are all computed by the FAC:

Vsw (Stall Warning Speed),
Vls (Minimum Selectable Speed)
Vmax (Vfe or Vle or Vmo)
Valim
Vaprot
Vprot
Vman (Optimum Manoeuver Speed),
V3 (Minimum Flap Retraction Speed),
V4 (Minimum Slat Retraction Speed),
Vfe next (Vfe corresponding to the next flap handle detent).

The corresponding symbols are presented only in analog form, and provided that the corresponding Vc values are within the displayed portion of the Vc scale.
Except where specified, the limit speeds are displayed only 10 s after main landing gear is unloading. The FAC manages all the logic conditions for display or non display (NCD) of the relevant symbols.

(12) Limit Speeds - Vsw

PFD - Limit Speed Indication Display ** ON A/C NOT FOR ALL

item (a).
The Stall Warning Indication is represented by means of a red and black stripe, the top of which indicates the Vsw value.
Vsw = k.Vs is a stall speed which depends on the A/C configuration.
Vsw is displayed only 5 s after A/C lift-off and provided that the speed protections (normally given by the flight controls) are lost. In this case, Vsw replaces both Valim and Vaprot indications.

(13) Limit Speeds - Valim

PFD - Limit Speed Indication Display ** ON A/C NOT FOR ALL

item (b) The top of a red stripe represents absolute speed protection limit given by the flight controls in their normal law.

(14) Limit Speeds - Vaprot

PFD - Limit Speed Indication Display ** ON A/C NOT FOR ALL

item (c)
The top of a black amber stripe represents the speed protection limit given by the flight controls in their normal law with the side stick controller in the neutral position.

(15) Limit Speeds - Vls

PFD - Limit Speed Indication Display ** ON A/C NOT FOR ALL

item (d).
The minimum selectable speed according to the A/C configuration is indicated by an amber tape a little bit thinner than the Vsw tape.
The top of the Vls tape indicates the Vls value on the speed scale.
The Vls value is computed and then sent by the FAC.
The Vls value is equal to:

1.2 Vs in take-off phase,
1.3 Vs in the other phases,
the speed value providing a 0.2 g margin with respect to the buffeting at high altitude (Z > 20000 ft.).

(16) Limit Speeds - Vmax

PFD - Limit Speed Indication Display ** ON A/C NOT FOR ALL

item (e)
The Vmax is indicated by means of a red/black stripe starting from the top of the speed scale and ending at the Vmax value on the Vc scale.
Vmax represents:

either Vmo (360 kts) or the speed corresponding to Mmo (.84) when that speed is lower than Vmo
or the maximum speed corresponding to the A/C configuration when the slats/flaps and/or the landing gear are extended: Vfe for slats/flaps extended and/or Vle for the landing gear extended.

Vmax is the minimum value out of the above values.

(17) Limit Speeds - Vprot

PFD - Limit Speed Indication Display ** ON A/C NOT FOR ALL

item (f)
Two small green lines inside the speed scale, at Vnext 6 kts , indicate that the protections are available.

(18) Limit Speeds - Optimum Maneuver Speed (Vman)

PFD - Limit Speed Indication Display ** ON A/C NOT FOR ALL

item (g).
This green dot indication gives the optimum maneuver speed, i.e:

1.45 Vs below 15000 ft (VFTO);
drift down speed above 15000 ft (engine out of optimal speed for descent).
This indication is given only in clean configuration and provided that the A/C is in flight.

(19) Limit Speeds - Vprot

PFD - Limit Speed Indication Display ** ON A/C NOT FOR ALL

item (f)
Two small green lines inside the speed scale, at Vmax + 6 kts , indicate at which overspeed value the protection becomes active.It is displayed when:

Vc is valid.
Vmax is valid.
Normal law is active.
Vmax strcitly superior to 240 kts.
Vprot is inside the speed scale displayed values.

(20) Limit Speeds - Optimum Maneuver Speed (Vman)

PFD - Limit Speed Indication Display ** ON A/C NOT FOR ALL

item (g).
This green dot indication gives the optimum maneuver speed, i.e:

1.45 Vs below 15000 ft (VFTO);
drift down speed above 15000 ft (engine out of optimal speed for descent).
This indication is given only in clean configuration and provided that the A/C is in flight.

(21) Limit Speeds - Minimum Flap Retraction Speed (V3)

PFD - Limit Speed Indication Display ** ON A/C NOT FOR ALL

item (h)
The green F indication shows the minimum speed for flaps retraction.
It is presented when the flaps are extended, but not in the FULL position.

(22) Limit Speeds - Minimum Slat Retraction Speed (V4)

PFD - Limit Speed Indication Display ** ON A/C NOT FOR ALL

item (j)
The green S indication shows the minimum speed for slats retraction.
It is presented only when the slats are extended.

(23) Limit Speeds - Minimum Flap Retraction Speed (V3)

PFD - Limit Speed Indication Display ** ON A/C NOT FOR ALL

item (h)
The green F indication shows the minimum speed for flaps retraction.
It is presented when the flaps are extended, but not in the FULL position.

(24) Limit Speeds - Minimum Slat Retraction Speed (V4)

PFD - Limit Speed Indication Display ** ON A/C NOT FOR ALL

item (j)
The green S indication shows the minimum speed for slats retraction.
It is presented only when the slats are extended.

NOTE: In case of superimposition of the symbols "F" or "S" with the letter "R" next to the selected speed, priority is given to the manoeuvring speed ( "F" or "S" symbols).

(25) Limit Speeds - Vfe NEXT (Vfen)

PFD - Limit Speed Indication Display ** ON A/C NOT FOR ALL

item (k)
This indication (two small amber lines inside the scale) provides the pilot with the value of the maximum authorized speed corresponding to the next slat/flap configuration in extension.

H. Air Speed - Back-up speed scale

PFD - INDICATION DISPLAY WITH BACK UP SPEED SCALE ** ON A/C NOT FOR ALL

When air data is no longer reliable, speed and altitude indications cannot be provided anymore by the ADR, after having switched off all ADR, a back-up speed scale comes into view.
It is displayed under following conditions:
- Back-up Speed Scale function is installed.
- All ADR are OFF and the BUSS pushbutton is not installed or
the BUSS pushbutton is installed and activated.
- The Angle Of Attack is valid.
The Back-up speed scale is built upon the angle of attack value from the IRS and slat/flap configuration from the SDAC. The whole ADR OFF condition is computed by the FWC.
The scale is represented by a tape constituted of the following parts:

A red lower area representing the stall speed with a white "slow" indication
An amber and red lower area between VLS and VSW
A green area between VLS and VFE with normal load margin
An amber and red area between VFE with normal load margin and VFE with decreased load margin
A red upper area above VFE with decreased load margin with white "FAST" indication.

(1) ITEM LIST

PFD - Limit Speed Indication Display ** ON A/C NOT FOR ALL

-----------------------------------------------------------------------------

ITEM PARAMETER EQUIPMENT LABEL COLOUR

-----------------------------------------------------------------------------

V MAX FAC 207 RED

V MAN FAC 265 GREEN

V1 FMGC 073 CYAN

V FEN FAC 267 AMBER

V3 FAC 263 GREEN

V C ADIRU ADC 206 YELLOW

V4 FAC 264 GREEN

V TREND FAC 262 YELLOW

V SEL FMGC 103 CYAN

V SEL FCU 103 or MAGENTA

V LS FAC 245 AMBER

V SW FAC 256 RED

IV SEL RNGH FMGC 307 CYAN

IV SEL RNGL FMGC 306 CYAN

V ALIM FAC 243 RED

V APPROT FAC 247 BLACK/AMBER

V PROT FAC 207 GREEN

(2) ITEM LIST

PFD - Limit Speed Indication Display ** ON A/C NOT FOR ALL

-----------------------------------------------------------------------------

ITEM PARAMETER EQUIPMENT LABEL COLOUR

-----------------------------------------------------------------------------

V MAX FAC 207 RED

V MAN FAC 265 GREEN

V1 FMGC 073 CYAN

V FEN FAC 267 AMBER

V3 FAC 263 GREEN

V C ADIRU ADC 206 YELLOW

V4 FAC 264 GREEN

V TREND FAC 262 YELLOW

V SEL FMGC 103 CYAN

V SEL FCU 103 or MAGENTA

V LS FAC 245 AMBER

V SW FAC 256 RED

IV SEL RNGH FMGC 307 CYAN

IV SEL RNGL FMGC 306 CYAN

V ALIM FAC 243 RED

V APPROT FAC 247 BLACK/AMBER

V PROT FAC 207 GREEN

V R FMGC 074 CYAN

PFD - VR Display ** ON A/C NOT FOR ALL

(3) ITEM LIST

PFD - Limit Speed Indication Display ** ON A/C NOT FOR ALL

-----------------------------------------------------------------------------

ITEM PARAMETER EQUIPMENT LABEL COLOUR

-----------------------------------------------------------------------------

V MAX FAC 207 RED

V MAN FAC 265 GREEN

V1 FMGC 073 CYAN

V FEN FAC 267 AMBER

V3 FAC 263 GREEN

V C ADIRU ADC 264 or 206 YELLOW

V4 FAC 264 GREEN

V TREND FAC 262 YELLOW

V SEL FMGC 103 CYAN

V SEL FCU 103 or MAGENTA

V LS FAC 245 AMBER

V SW FAC 256 RED

IV SEL RNGH FMGC 307 CYAN

IV SEL RNGL FMGC 306 CYAN

V ALIM FAC 243 RED

V APPROT FAC 247 BLACK/AMBER

V PROT FAC 207 GREEN

V R FMGC 074 CYAN

PFD - VR Display ** ON A/C NOT FOR ALL

(4) ITEM LIST

PFD - Limit Speed Indication Display ** ON A/C NOT FOR ALL

-----------------------------------------------------------------------------

ITEM PARAMETER EQUIPMENT LABEL COLOUR

-----------------------------------------------------------------------------

V MAX FAC 207 RED

V MAN FAC 265 GREEN

V1 FMGC 073 CYAN

V FEN FAC 267 AMBER

V3 FAC 263 GREEN

V C ADIRU ADC 206 YELLOW

V4 FAC 264 GREEN

V TREND FAC 262 YELLOW

V SEL FMGC 103 CYAN

V SEL FCU 103 or MAGENTA

V LS FAC 245 AMBER

V SW FAC 256 RED

IV SEL RNGH FMGC 307 CYAN

IV SEL RNGL FMGC 306 CYAN

V ALIM FAC 243 RED

V APPROT FAC 247 BLACK/AMBER

V APPROT FAC 244 BLACK/AMBER

V PROT FAC 207 GREEN

V R FMGC 074 CYAN

PFD - VR Display ** ON A/C NOT FOR ALL

(5) Failures Indications

PFD - Airspeed Failure Indications ** ON A/C NOT FOR ALL

Airspeed Failure Indications
When a parameter is unavailable (NCD), it is replaced by a flag.
For a given DMC, if the onside FAC is faulty, the speed limit indications are taken from the offside FAC.

I. Airspeed - Condition of Display
The table below gives the conditions of display of the speed information:

-------------------------------------------------------------------------------

! PARAMETERS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! Speed reference ! - Two fixed yellow dashes linked together by a thin !

! ! yellow line and completed with a yellow triangle !

! ! when computer airspeed is valid,or on the ground !

! ! when computer airspeed is NCD. !

!--------------------!--------------------------------------------------------!

! Speed scale ! - White when Vc is valid and more than 30 knots. !

! ! - Partially displayed when Vc is between 30 knots and !

! ! 72 knots. !

!--------------------!--------------------------------------------------------!

! Vsw (Stall warning)! - Vsw value indicated by the top of a red and black !

! ! stripe if computed airspeed and Vsw are valid and !

! ! (computed airspeed - Vsw) > 42kts, and pitch law is !

! ! no longer available. !

!--------------------!--------------------------------------------------------!

! Vaprot ! - Indicated by the top of an amber and black stripe if !

! ! computed airspeed and Vaprot given by FAC are valid !

! ! and (computed airspeed - Vaprot) < 42kts, under !

! ! pitch law. !

!--------------------!--------------------------------------------------------!

! Valim ! - Indicated by the top of a red stripe if computed !

! ! airspeed and Valim given by FAC are valid and !

! ! (computed airspeed - Valim) > 42kts under pitch law. !

!--------------------!--------------------------------------------------------!

! Vls ! - Indicated by the top of an amber tape if computed !

! ! airspeed and Vls given by FAC are valid and !

! ! (computed airspeed - Vls) > 42kts, and Vc valid. !

!--------------------!--------------------------------------------------------!

! V1 ! - Cyan 1 figure and mark across the Vc scale on the !

! ! ground if V1 given by FMGC is valid and computed !

! ! airspeed ok and V1 is between (Vc - 42kts) and !

! ! (Vc + 42kts). !

! ! - If V1 is above Vc + 42kts, cyan digits above the !

! ! speed scale. !

!--------------------!--------------------------------------------------------!

! V3 ! - Green F when V3 and computed airspeed are valid and !

! ! V3 is between (Vc - 42kts) and (Vc + 42kts) and Vc !

! ! valid. !

!--------------------!--------------------------------------------------------!

!V4 ! - Green S when V4 and computed airspeed are valid and !

! ! V4 is between (Vc - 42kts) and (Vc + 42kts) and Vc !

! ! valid. !

!--------------------!--------------------------------------------------------!

! Vfe next ! - Two amber lines inside speed scale when Vfen !

! ! computed by FAC is valid and between (Vc - 42kts) !

! ! and (Vc + 42kts), and Vc valid. !

!--------------------!--------------------------------------------------------!

! Vman ! - Green dots when Vman and computed airspeed are valid !

! ! and Vman is between (Vc - 42kts) and (Vc + 42kts), !

! ! and Vc valid. !

!--------------------!--------------------------------------------------------!

! Vc trend ! - Yellow arrow when computed airspeed and Vc trend are !

! ! valid. !

!--------------------!--------------------------------------------------------!

! Selected speed ! - Cyan triangle when selected speed is valid and !

! ! between (Vc - 42kts) and (Vc + 42kts), and there is !

! ! no ECON mode and no constraint. !

! ! - If speed is constrained, the cyan triangle becomes !

! ! magenta. !

! ! - If selected speed is not between (Vc - 42kts) and !

! ! (Vc + 42kts), cyan or magenta digits above or below !

! ! speed scale according to the sign of the difference !

! ! (Vsel - Vc). !

-------------------------------------------------------------------------------

! PARAMETERS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! Selected speed ! - In ECON mode, high speed margin and low speed margin !

! margin ! magenta when both of them and Vc are valid. To be !

! ! displayed each margin must be between (Vc - 42kts) !

! ! and (Vc + 42kts). !

-------------------------------------------------------------------------------

! PARAMETERS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! Vmax ! - Red and black stripe when computed airspeed and Vmax !

! ! are valid and Vmax < Vc + 42kts. !

!--------------------!--------------------------------------------------------!

! Selected speed ECON! - Double bar in speed scale when Vc, high speed margin !

! ! and low speed margin are valid and at least one !

! ! margin is between (Vc - 42kts) and (Vc + 42kts). !

! ! - Cyan or magenta when a constraint exists. !

-------------------------------------------------------------------------------

! PARAMETERS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! VR ! - which is entered before take off through the MCDU !

! ! (take off page) is displayed by means of a cyan !

! ! colour circle. !

! ! The VR symbol is displayed during the flight !

! ! preparation, at take off and go around. It is not !

! ! displayed in the other configurations. !

The table below gives the conditions of display of the speed flags:

-------------------------------------------------------------------------------

! FLAGS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! SPD ! - Red flag replacing speed scale when Vc signal is !

! ! neither valid nor NCD on the ground. It is flashing !

! ! during 9s then is steady. !

!--------------------!--------------------------------------------------------!

! V1 INOP ! - Red flag on the right side of the top of the speed !

! ! scale, on the ground, when V1 signal is not in !

! ! normal operation (NO). !

!--------------------!--------------------------------------------------------!

! SPD SEL ! - Red flag on the top of the speed scale when no !

! ! selected speed signal is valid (neither FMGC valid !

! ! selected speed, nor valid approach speed target, nor !

! ! valid selected speed from FCU). !

!--------------------!--------------------------------------------------------!

! SPD LIM ! - Red flag on the right side of the bottom of the speed!

! ! scale, when FACs are seen invalid by DMCs. !

!--------------------!--------------------------------------------------------!

! MACH ! - Red flag on the left bottom corner of the PFD in !

! ! flight when no approach data is available and MACH !

! ! data is not valid. !

The table below gives the conditions of display of the speed flags:

-------------------------------------------------------------------------------

! FLAGS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! SPD ! - Red flag when Vc signal is neither valid nor NCD !

! ! on the ground !

! ! - This flag and the scale are flashing during 9s then !

! ! are steady. !

!--------------------!--------------------------------------------------------!

! V1 INOP ! - Red flag on the right side of the top of the speed !

! ! scale, on the ground, when V1 signal is not in !

! ! normal operation (NO). !

!--------------------!--------------------------------------------------------!

! SPD SEL ! - Red flag on the top of the speed scale when no !

! ! selected speed signal is valid (neither FMGC valid !

! ! selected speed, nor valid approach speed target, nor !

! ! valid selected speed from FCU). !

! ! - This flag flashes !

!--------------------!--------------------------------------------------------!

! SPD LIM ! - Red flag on the right side of the bottom of the speed!

! ! scale, when FACs are seen invalid by DMCs. !

! ! - This flag flashes !

!--------------------!--------------------------------------------------------!

! speed margins ! - speed margins in descent mode are displayed by means !

! ! of two double lines (magenta) !

! ! - Selected speed in descent mode is displayed by means !

! ! of a triangle (magenta or cyan it depends on the !

! ! target speed constraint) !

!--------------------!--------------------------------------------------------!

! MACH ! - Red flag on the left bottom corner of the PFD in !

! ! flight and MACH data is not valid. !

J. Vertical Speed

PFD - Vertical Speed Presentation ** ON A/C NOT FOR ALL

The vertical speed indications and TCAS avoidance orders are shown on the right side of the PFD.

PFD - Vertical Speed Presentation ** ON A/C NOT FOR ALL

The vertical speed indications and TCAS avoidance orders are shown on the right side of the PFD.

(1) Description of the vertical speed scale without TCAS option

PFD - Vertical Speed Display ** ON A/C NOT FOR ALL

PFD - Examples of Vertical Speed Display ** ON A/C NOT FOR ALL

The vertical speed scale consists of:

a trapezoidal grey background colored surface. (See note)
a fixed white scale with 500 ft/mn spaced marks from -2000 ft/mn to +2000 ft/mn,
a needle giving in analog form the actual vertical speed value. This needle ends against the vertical scale. It rotates around a point which is located outside the display.
Only the portion of the needle which is within the colored background is displayed.

The value for the analog vertical speed is transmitted by the ADIRU (IRS part) on the label 365

a number in a moving blanking window. This window accompanies the needle (above the needle if V/S > 0, below if V/S < 0).
The number gives the V/S value in hundreds of ft/mn.
Between -200 ft/mn and +200 ft/mn, both the window and the number disappear.
above +6000 ft/mn (or below -6000 ft/mn), the needle remains stopped where it is.

The value for the displayed digital vertical speed is transmitted by the ADIRU (IRS part) on the label 365.

If the label 365 is invalid, the values are transmitted by the ADIRU (ADR part) on the label 212.

NOTE: On a detection of a ventilation failure (DUs no longer cooled), the grey background colored areas of the PFD image might be removed, in order to decrease the thermal dissipation of the DUs.

(2) Description of the vertical speed scale without TCAS option

PFD - Vertical Speed Display ** ON A/C NOT FOR ALL

PFD - Examples of Vertical Speed Display ** ON A/C NOT FOR ALL

The vertical speed scale consists of:

a trapezoidal grey background colored surface.
a fixed white scale with 500 ft/mn spaced marks from -2000 ft/mn to +2000 ft/mn, and 2000 ft/mn spaced marks from +/- 2000ft/mn to -/+ 6000ft/mn.
the reference of the scale is yellow
the scale features graduation numbers
a needle giving in analog form the actual vertical speed value. This needle is displayed out of the vertical scale. It rotates around a point which is located outside the display.
Only the portion of the needle which is within the colored background is displayed.

(3) Excessive Vertical Speed

PFD - Particular Vertical Speeds Displays ** ON A/C NOT FOR ALL

item (A)
When the vertical speed exceeds +6000 ft/mn or -6000 ft/mn, the digital indication and the analog needle change from green to amber.
In addition, those indications change to amber in approach, in the following cases:

V/S less than -2000ft/mn betwwenw 2500ft (RA) and 1000ft (RA).
V/S less than -1200ft/mn below 1000ft (RA).

(4) Degraded Data

PFD - Particular Vertical Speeds Displays ** ON A/C NOT FOR ALL

item (B)
When the source giving the V/S parameter is no more the IR but the ADR, an amber window surrounding the digital value appears cautioning the pilot that this is a degraded data indication.

(5) Failure Indication

PFD - Particular Vertical Speeds Displays ** ON A/C NOT FOR ALL

item (C),item (D)
In case of failure warning, the V/S scale is removed and replaced by a red flag indication.
In case of TCAS computer failure, an amber TCAS flag appears next to the V/S scale.

(6) Parameters Definition

(7) Excessive Vertical Speed

item (A)
When the vertical speed exceeds +6000 ft/mn or -6000 ft/mn, the digital indication and the analog needle change from green to amber.
In addition, those indications change to amber in approach, in the following cases:

V/S less than -2000ft/mn below 2500ft (R/A)
V/S less than -1200ft/mn below 1000ft (RA)

(8) Degraded Data

item (B)
When the source giving the V/S parameter is no more the IR but the ADR, an amber window surrounding the digital value appears cautioning the pilot that this is a degraded data indication.

(9) Failure Indication

item (C).
In case of failure warning, the V/S scale is removed and replaced by a red flag indication.

(10) Parameters Definition

(11) Excessive Vertical Speed

PFD - Particular Vertical Speeds Displays ** ON A/C NOT FOR ALL

item (a)
When the vertical speed exceeds +6000 ft/mn or -6000 ft/mn, the digital indication and the analog needle change from green to amber.
In addition, those indications change to amber in approach, in the following case:

the A/C is within the range : 1000ft to 2500ft (R/A)
-2000ft/mn < V/S < -1200ft/mn

(12) Degraded Data

PFD - Particular Vertical Speeds Displays ** ON A/C NOT FOR ALL

item (b)
When the source giving the V/S parameter is no more the IR but the ADR, an amber window surrounding the digital value appears cautioning the pilot that this is a degraded data indication.

(13) Failure Indication

PFD - Particular Vertical Speeds Displays ** ON A/C NOT FOR ALL

item (c).
In case of failure warning, the V/S scale is removed and replaced by a red flag indication.

(14) Parameters Definition

PFD - Vertical Speed Parameters ** ON A/C NOT FOR ALL

(15) The table below gives the conditions of display of the vertical speed information:

-------------------------------------------------------------------------------

! PARAMETERS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! Digital vertical ! - Green if altitude rate (from ADR) or inertial !

! speed ! vertical speed (from IR) are valid, and !V/S! more !

! ! than or equal to 200ft/mn. !

! ! - Amber when !V/S! more than or equal to 6000ft/mn !

! ! or V/S less than or equal to -2000ft/mn below 2500ft !

! ! or V/S less than or equal to -1200ft/mn below 1000ft.!

!--------------------!--------------------------------------------------------!

! Vertical speed ! - Green or amber; same conditions as for display of !

! needle ! digital vertical speed. !

!--------------------!--------------------------------------------------------!

! Window surrounding ! - Amber if altitude rate from ADR is valid but inertial!

! digital indication ! vertical speed from IR is not valid. !

!--------------------!--------------------------------------------------------!

! Vertical speed ! - Black if altitude rate from ADR or inertial vertical !

! window ! speed from IR are valid !V/S! more than or equal to !

! ! 200ft/mn. !

(16) The table below gives the conditions of display of the vertical speed flag:

-------------------------------------------------------------------------------

! FLAG ! DISPLAY !

!--------------------!--------------------------------------------------------!

! V/S ! - Red flag replacing vertical speed scale when neither !

! ! inertial vertical speed nor altitude rate are valid. !

(17) The table below gives the conditions of display of the vertical speed flag:

-------------------------------------------------------------------------------

! FLAG ! DISPLAY !

!--------------------!--------------------------------------------------------!

! V/S ! - Red flag replacing vertical speed scale when neither !

! ! inertial vertical speed nor altitude rate are valid. !

! ! - This flag flashes 9s then steady.

(18) Description of the vertical speed scale with TCAS option (resolution advisories present)
On the vertical speed scale, the resolution advisories are represented by a band made up of colored sectors:

the red sector represents a vertical speed range to be avoided
the green sector indicates the range the aircraft must fly in to avoid collision.

The corrective resolution advisories are displayed to advise the crew to perform an avoidance maneuver in the vertical sense (climbing, descending, reducing vertical speed in climb or descent phase, etc.).

PFD - TCAS Indications - Corrective Resolution Advisories ** ON A/C NOT FOR ALL

The pilot's task is to maneuver the aircraft promptly to keep the needle out of the red sector and place it in the adjacent green "Fly-to" sector.
The vertical speed indication is red-colored when the vertical speed is within the forbidden sector whereas it becomes green when the vertical speed enters the authorized sector.
The preventive resolution advisories advise the pilot to avoid vertical speeds that could lead to a hazardous situation.

PFD - TCAS Indications - Preventive Resolution Advisories ** ON A/C NOT FOR ALL

They are represented by one or two red zones on the scale. The pilot must keep the aircraft vertical speed outside these zones. If the aircraft can neither climb nor descend, then two red sectors appear on the vertical speed scale and a range sector (+/- 250 ft ) around the zero figure is left uncolored. This uncolored area around the zero figure informs the pilot to maintain the aircraft at its current level.

PFD - TCAS Indications ** ON A/C NOT FOR ALL

In case of system or TCAS computer failure, the NAV TCAS FAULT message generated by the FWC appears in the warning section of the upper ECAM DU.

PFD - TCAS Failure Message ** ON A/C NOT FOR ALL

If this message is generated further to a failure of the TCAS computer, an amber TCAS flag also appears next to the vertical speed scale.

PFD - Particular Vertical Speeds Displays ** ON A/C NOT FOR ALL

PFD - TCAS Flag Indication ** ON A/C NOT FOR ALL

NOTE: When the resolution advisories are no longer displayed, the shape and color of the vertical speed scale return to initial configuration.
On a detection of a ventilation failure (DUs no longer cooled), the grey background colored areas of PFD image might be removed, except for the V/S scale when TCAS information is displayed on it.

(19) Description of the vertical speed scale with TCAS option (resolution advisories present)
On the vertical speed scale, the resolution advisories are represented by a band made up of colored sectors:

the red sector represents a vertical speed range to be avoided
the green sector indicates the range the aircraft must fly in to avoid collision.

PFD - TCAS Indications - Corrective Resolution Advisories ** ON A/C NOT FOR ALL

PFD - TCAS Indications - Preventive Resolution Advisories ** ON A/C NOT FOR ALL

PFD - TCAS Indications ** ON A/C NOT FOR ALL

In case of system or TCAS computer failure, the NAV TCAS FAULT message generated by the FWC appears in the warning section of the upper ECAM DU.

PFD - TCAS Failure Message ** ON A/C NOT FOR ALL

If this message is generated further to a failure of the TCAS computer, an amber TCAS flag also appears next to the vertical speed scale.

PFD - Particular Vertical Speeds Displays ** ON A/C NOT FOR ALL

NOTE: When the resolution advisories are no longer displayed, the shape and color of the vertical speed scale return to initial configuration.

K. Flight Mode Annunciator

PFD - Flight Mode Annunciator Presentation ** ON A/C NOT FOR ALL

(1) Description of the Different Zones
The FMA zones are divided into zones which are referenced with their line number (1, 2, 3) and their column letter (A, B, C, D, E).
The columns are separated by vertical bars (the second one may cover 2 or 3 FMA lines depending on the annunciations and messages to be written).

PFD - FMA Zones ** ON A/C NOT FOR ALL

Briefly, the 5 columns are dedicated to the display of the AFS armed and active modes, sub-systems engagement status and approach operational capabilities.
In addition, warning messages associated with the AFS operation may be presented.
Assignment of the FMA zones (except special messages in zones AB3 and BC3):

1st column : indications related to the auto-throttle system operation : modes and alert messages.
2nd column : indications related to the A/C longitudinal control: active and armed modes.
3rd column : ditto for the A/C lateral control.
4th column : approach capability indications.
5th column : AFS sub-system engagement status AP, FD, A/THR.

The various messages/mode indications are presented in various colors, according to the following code:

green : active mode.
cyan : armed mode, preset value (VC or Mach).
magenta : mode armed or engaged because of a constraint which will be or which is followed by the AFS in longitudinal or lateral auto-control.
white : engagement status of the APs, the FDs and the A/THR sub-systems of the AFS.
white (flashing) : the FD2 indication on the FD1 flashes white for 10 seconds and then remains steady in case of automatic FMGC switching.
amber (flashing) : indications calling for immediate attention and action to be carried out.
amber (fixed) : indications corresponding to special operation and modes requiring special attention.

NOTE: (1) The 2nd vertical bar (from the left) disappears in case of display of common mode indication:
- FLARE.ROLL OUT.LAND. which concern both the longitudinal and lateral part.
(2)The first vertical bar is shorter when there are messages to be displayed in the AB3 zone.
(3)The 2nd vertical bar is shorter when there are messages to be displayed in the BC3 zone.
(4)In a given zone, all the possible indications/messages at the same location exclude each other (logic made by the FMGCs).
When a message appears in one of the following places: A1, B1, C1, D1, E1, BC1, E2, E3, D2, it is surrounded by a white box during 10 seconds.

L. Flight Mode Annunciator - Messages
The following tables show the different messages with the associated colors (G for green, C for cyan, M for magenta, R for red, A for amber, W for white).
The colors of the surrounding boxes and flashing condition are also given.

-------------------------------------------------------------------------------

! ZONE A1 ! ZONE B1 ! ZONE C1 ! ZONE D1 ! ZONE E1 !

!--------------------!-------------------!------------!-----------!-----------!

! ------------ ! SRS (G) ! HDG (G) ! CAT1 (W) ! AP1 (W) !

! I MAN (W) I ! ! ! ! !

! I TOGA (W) I (W) ! ALT CRZ (G) ! GA TRK (G) ! CAT2 (W) ! AP2 (W) !

! ------------ ! ! ! ! !

! ! ALT CST (G) ! LOC (G) ! CAT3 (W) ! AP1+2 (W) !

! ------------------ ! ! ! ! !

! I MAN (W) I ! ALT CST * (G) ! LOC * (G) ! ! !

! I FLX (W) XX (C) I ! ! ! ! !

! ------------------ ! V/S (G) ! NAV (G) ! ! !

! (W) ! +/- XXXX (C) ! ! ! !

! ! ! APP NAV (G)! ! !

! ----------- ! FPA (G) ! ! ! !

! I MAN (W) I ! +/- X.X degree (C)! RWY (G) ! ! !

! I MCT (W) I (W) ! ! ! ! !

! ----------- ! EXP CLB (G) ! TRACK (G) ! ! !

! ! ! ! ! !

! ----------- ! EXP DES (G) ! RWY TRK (G)! ! !

! I MAN (W) I ! ! ! ! !

! I THR (W) I (A) ! G/S (G) ! ! ! !

! ----------- ! ! ! ! !

! ! G/S * (G) ! ! ! !

! --------------- ! ! ! ! !

! I A.FLOOR (G) I ! CLB (G) ! ! ! !

! --------------- ! ! ! ! !

! (A) (flashing) ! DES (G) ! ! ! !

! ! ! ! ! !

! --------------- ! OP CLB (G) ! ! ! !

! I TOGA LK (G) I ! ! ! ! !

! --------------- ! OP DES (G) ! ! ! !

! (A) (flashing) ! ! ! ! !

! ! FINAL (G) ! ! ! !

! SPEED (G) ! ! ! ! !

! ! ALT (G) ! ! ! !

! MACH (G) ! ! ! ! !

! ! ALT * (G) ! ! ! !

! THR MCT (G) ! ! ! ! !

! ! ! ! ! !

! THR CLB (G) ! ! ! ! !

! ! ! ! ! !

! THR LVR (G) ! ! ! ! !

! ! ! ! ! !

! THR IDLE (G) ! ! ! ! !

The following tables show the different messages with the associated colors (G for green, C for cyan, M for magenta, R for red, A for amber, W for white).
The colors of the surrounding boxes and flashing condition are also given.

-------------------------------------------------------------------------------

! ZONE A1 ! ZONE B1 ! ZONE C1 ! ZONE D1 ! ZONE E1 !

!--------------------!-------------------!------------!-----------!-----------!

! ------------ ! SRS (G) ! HDG (G) ! CAT1 (W) ! AP1 (W) !

! I MAN (W) I ! ! ! ! !

! I TOGA (W) I (W) ! ALT CRZ (G) ! GA TRK (G) ! CAT2 (W) ! AP2 (W) !

! ------------ ! ! ! ! !

! ! ALT CST (G) ! LOC (G) ! CAT3 (W) ! AP1+2 (W) !

! ------------ ! ! ! ! !

! I MAN (W) I ! ! ! ! !

! I GA SOFT (W)I (W) ! ! ! ! !

! ------------ ! ! ! ! !

! ------------------ ! ! ! ! !

! I MAN (W) I ! ALT CST * (G) ! LOC * (G) ! ! !

! I FLX (W) XX (C) I ! ! ! ! !

! ------------------ ! V/S (G) ! NAV (G) ! ! !

! (W) ! +/- XXXX (C) ! ! ! !

! ! ! APP NAV (G)! ! !

! ----------- ! FPA (G) ! ! ! !

! I MAN (W) I ! +/- X.X degree (C)! RWY (G) ! ! !

! I MCT (W) I (W) ! ! ! ! !

! ----------- ! EXP CLB (G) ! TRACK (G) ! ! !

! ! ! ! ! !

! ----------- ! EXP DES (G) ! RWY TRK (G)! ! !

! I MAN (W) I ! ! ! ! !

! I THR (W) I (A) ! G/S (G) ! ! ! !

! ----------- ! ! ! ! !

! ! G/S * (G) ! ! ! !

! --------------- ! ! ! ! !

! I A.FLOOR (G) I ! CLB (G) ! ! ! !

! --------------- ! ! ! ! !

! (A) (flashing) ! DES (G) ! ! ! !

! ! ! ! ! !

! --------------- ! OP CLB (G) ! ! ! !

! I TOGA LK (G) I ! ! ! ! !

! --------------- ! OP DES (G) ! ! ! !

! (A) (flashing) ! ! ! ! !

! ! FINAL (G) ! ! ! !

! SPEED (G) ! ! ! ! !

! ! ALT (G) ! ! ! !

! MACH (G) ! ! ! ! !

! ! ALT * (G) ! ! ! !

! THR MCT (G) ! ! ! ! !

! ! ! ! ! !

! THR CLB (G) ! ! ! ! !

! ! ! ! ! !

! THR LVR (G) ! ! ! ! !

! ! ! ! ! !

! THR IDLE (G) ! ! ! ! !

NOTE: When the V/S or FPA target is not held due to an AP speed protection, an amber box flashes around the V/S or FPA message and target, and the cyan target is pulsing.
When AP/FD/ATHR modes change and this change has not been selected by the crew, a white box is displayed around the relevant mode.
When a white box is displayed around several modes, a particular box can flash which indicates that this mode has to be highlighted for the pilot.

-------------------------------------------------------------------------------

! ZONE A1 ! ZONE B1 ! ZONE C1 ! ZONE D1 ! ZONE E1 !

!--------------------!-------------------!------------!-----------!-----------!

! ------------ ! SRS (G) ! HDG (G) ! CAT1 (W) ! AP1 (W) !

! I MAN (W) I ! ! ! ! !

! I TOGA (W) I (W) ! ALT CRZ (G) ! GA TRK (G) ! CAT2 (W) ! AP2 (W) !

! ------------ ! ! ! ! !

! ! ALT CST (G) ! LOC (G) ! CAT3 (W) ! AP1+2 (W) !

! ------------------ ! ! ! ! !

! I MAN (W) I ! ALT CST * (G) ! LOC * (G) ! ! !

! I FLX (W) XX (C) I ! ! ! ! !

! ------------------ ! V/S (G) ! NAV (G) ! ! !

! (W) ! +/- XXXX (C) ! ! ! !

! ! ! APP NAV (G)! ! !

! ----------- ! ! ! ! !

! I MAN (W) I ! ! ! ! !

! I DTO (W) I (W) ! ! ! ! !

! ----------- ! ! ! ! !

! ! ! ! ! !

! ----------- ! FPA (G) ! ! ! !

! I MAN (W) I ! +/- X.X degree (C)! RWY (G) ! ! !

! I MCT (W) I (W) ! ! ! ! !

! ----------- ! EXP CLB (G) ! TRACK (G) ! ! !

! ! ! ! ! !

! ----------- ! EXP DES (G) ! RWY TRK (G)! ! !

! I MAN (W) I ! ! ! ! !

! I THR (W) I (A) ! G/S (G) ! LOC B/C*(G)! ! !

! ----------- ! ! ! ! !

! ! G/S * (G) ! LOC B/C (G)! ! !

! --------------- ! ! ! ! !

! I A.FLOOR (G) I ! CLB (G) ! ! ! !

! --------------- ! ! ! ! !

! (A) (flashing) ! DES (G) ! ! ! !

! ! ! ! ! !

! --------------- ! OP CLB (G) ! ! ! !

! I TOGA LK (G) I ! ! ! ! !

! --------------- ! OP DES (G) ! ! ! !

! (A) (flashing) ! ! ! ! !

! ! FINAL (G) ! ! ! !

! SPEED (G) ! ! ! ! !

! ! ALT (G) ! ! ! !

! MACH (G) ! ! ! ! !

! ! ALT * (G) ! ! ! !

! THR MCT (G) ! ! ! ! !

! ! ! ! ! !

! THR CLB (G) ! ! ! ! !

! ! ! ! ! !

! THR LVR (G) ! ! ! ! !

! ! ! ! ! !

! THR IDLE (G) ! ! ! ! !

-------------------------------------------------------------------------------

! ZONE A1 ! ZONE B1 ! ZONE C1 ! ZONE D1 ! ZONE E1 !

!--------------------!-------------------!------------!-----------!-----------!

! ------------ ! SRS (G) ! HDG (G) ! CAT1 (W) ! AP1 (W) !

! I MAN (W) I ! ! ! ! !

! I TOGA (W) I (W) ! ALT CRZ (G) ! GA TRK (G) ! CAT2 (W) ! AP2 (W) !

! ------------ ! ! ! ! !

! ! ALT CST (G) ! LOC (G) ! CAT3 (W) ! AP1+2 (W) !

! ------------------ ! ! ! ! !

! ------------ ! ! ! ! !

! I MAN (W) I ! ! ! ! !

! I GA SOFT (W)I (W) ! ! ! ! !

! ------------ ! ! ! ! !

! I MAN (W) I ! ALT CST * (G) ! LOC * (G) ! ! !

! I FLX (W) XX (C) I ! ! ! ! !

! ------------------ ! V/S (G) ! NAV (G) ! ! !

! (W) ! +/- XXXX (C) ! ! ! !

! ! ! APP NAV (G)! ! !

! ----------- ! ! ! ! !

! I MAN (W) I ! ! ! ! !

! I DTO (W) I (W) ! ! ! ! !

! ----------- ! ! ! ! !

! ! ! ! ! !

! ----------- ! FPA (G) ! ! ! !

! I MAN (W) I ! +/- X.X degree (C)! RWY (G) ! ! !

! I MCT (W) I (W) ! ! ! ! !

! ----------- ! EXP CLB (G) ! TRACK (G) ! ! !

! ! ! ! ! !

! ----------- ! EXP DES (G) ! RWY TRK (G)! ! !

! I MAN (W) I ! ! ! ! !

! I THR (W) I (A) ! G/S (G) ! LOC B/C*(G)! ! !

! ----------- ! ! ! ! !

! ! G/S * (G) ! LOC B/C (G)! ! !

! --------------- ! ! ! ! !

! I A.FLOOR (G) I ! CLB (G) ! ! ! !

! --------------- ! ! ! ! !

! (A) (flashing) ! DES (G) ! ! ! !

! ! ! ! ! !

! --------------- ! OP CLB (G) ! ! ! !

! I TOGA LK (G) I ! ! ! ! !

! --------------- ! OP DES (G) ! ! ! !

! (A) (flashing) ! ! ! ! !

! ! FINAL (G) ! ! ! !

! SPEED (G) ! ! ! ! !

! ! ALT (G) ! ! ! !

! MACH (G) ! ! ! ! !

! ! ALT * (G) ! ! ! !

! THR MCT (G) ! ! ! ! !

! ! ! ! ! !

! THR CLB (G) ! ! ! ! !

! ! ! ! ! !

! THR LVR (G) ! ! ! ! !

! ! ! ! ! !

! THR IDLE (G) ! ! ! ! !

-------------------------------------------------------------------------------

! ZONE A1 ! ZONE B1 ! ZONE C1 ! ZONE D1 ! ZONE E1 !

!--------------------!-------------------!------------!-----------!-----------!

! ------------ ! SRS (G) ! HDG (G) ! CAT1 (W) ! AP1 (W) !

! I MAN (W) I ! ! ! ! !

! I TOGA (W) I (W) ! ALT CRZ (G) ! GA TRK (G) ! CAT2 (W) ! AP2 (W) !

! ------------ ! ! ! ! !

! ! ALT CST (G) ! LOC (G) ! CAT3 (W) ! AP1+2 (W) !

! ------------------ ! ! ! ! !

! ------------ ! ! ! ! !

! I MAN (W) I ! ! ! ! !

! I GA SOFT (W)I (W) ! ! ! ! !

! ------------ ! ! ! ! !

! I MAN (W) I ! ALT CST * (G) ! LOC * (G) ! ! !

! I FLX (W) XX (C) I ! ! ! ! !

! ------------------ ! V/S (G) ! NAV (G) ! ! !

! (W) ! +/- XXXX (C) ! ! ! !

! ! ! APP NAV (G)! ! !

! ----------- ! ! ! ! !

! I MAN (W) I ! ! ! ! !

! I DTO (W) I (W) ! ! ! ! !

! ----------- ! ! ! ! !

! ! ! ! ! !

! ----------- ! FPA (G) ! ! ! !

! I MAN (W) I ! +/- X.X degree (C)! RWY (G) ! ! !

! I MCT (W) I (W) ! ! ! ! !

! ----------- ! EXP CLB (G) ! TRACK (G) ! ! !

! ! ! ! ! !

! ----------- ! EXP DES (G) ! RWY TRK (G)! ! !

! I MAN (W) I ! ! ! ! !

! I THR (W) I (A) ! G/S (G) ! LOC B/C*(G)! ! !

! ----------- ! ! ! ! !

! ! G/S * (G) ! LOC B/C (G)! ! !

! --------------- ! ! ! ! !

! I A.FLOOR (G) I ! CLB (G) ! ! ! !

! --------------- ! ! ! ! !

! (A) (flashing) ! DES (G) ! ! ! !

! ! ! ! ! !

! --------------- ! OP CLB (G) ! ! ! !

! I TOGA LK (G) I ! ! ! ! !

! --------------- ! OP DES (G) ! ! ! !

! (A) (flashing) ! ! ! ! !

! ! FINAL (G) ! ! ! !

! SPEED (G) ! ! ! ! !

! ! ALT (G) ! ! ! !

! MACH (G) ! ! ! ! !

! ! ALT * (G) ! ! ! !

! THR MCT (G) ! ! ! ! !

! ! V/S +0 (G) ! ! ! !

! THR CLB (G) ! ! ! ! !

! ! FPA +0 (G) ! ! ! !

! THR LVR (G) ! ! ! ! !

! ! ! ! ! !

! THR IDLE (G) ! ! ! ! !

! ! ! ! ! !

! THR (G) ! ! ! ! !

-------------------------------------------------------------------------------

! ZONE A2 ! ZONE B2 ! ZONE C2 ! ZONE D2 ! ZONE E2 !

!-----------!------------------!---------------!--------------!---------------!

! ! ALT (M) ! NAV (C) ! SINGLE (W) ! _ !

! ! ALT (C) ! APP NAV (C) ! DUAL (W) ! FD1 (W) ! * !

! ! CLB (C) ! LOC (C) ! ! FD2 (W) _! !

! ! DES (C) ! LOC B/C (C) ! ! _ !

! ! G/S (C) ! ! ! 1FD2 (W) ! !

! ! FINAL (C) ! ! ! 1FD1 (W) ! !

! ! ALT (C) G/S (C) ! ! ! 2FD2 (W) ! !

! ! ALT (M) G/S (C) ! ! ! 1FD- (W) ! ** !

! ! ALT (C) FINAL (C)! ! ! 2FD- (W) ! !

! ! ALT (M) FINAL (C)! ! ! -FD1 (W) ! !

! ! DES (C) G/S (C) ! ! ! -FD2 (W)_! !

! ! DES (C) FINAL (C)! ! ! !

* : A/THR programming pin of FMGC not activated
** : A/THR programming pin of FMGC activated

-------------------------------------------------------------------------------

! ZONE A2 ! ZONE B2 ! ZONE C2 ! ZONE D2 ! ZONE E2 !

!-----------!------------------!---------------!--------------!---------------!

! ! ALT (M) ! NAV (C) ! SINGLE (W) ! _ !

! ! ALT (C) ! APP NAV (C) ! DUAL (W) ! FD1 (W) ! * !

! ! CLB (C) ! LOC (C) ! ! FD2 (W) _! !

! ! DES (C) ! LOC B/C (C) ! ! _ !

! ! G/S (C) ! ! ! 1FD2 (W) ! !

! ! FINAL (C) ! ! ! 1FD1 (W) ! !

! ! ALT (C) G/S (C) ! ! ! 2FD2 (W) ! !

! ! ALT (M) G/S (C) ! ! ! 1FD- (W) ! ** !

! ! ALT (C) FINAL (C)! ! ! 2FD- (W) ! !

! ! ALT (M) FINAL (C)! ! ! -FD1 (W) ! !

! ! DES (C) G/S (C) ! ! ! -FD2 (W)_! !

! ! DES (C) FINAL (C)! ! ! !

* : A/THR programming pin of FMGC not activated
** : A/THR programming pin of FMGC activated

---------------------------------------------------------------------------------

! ZONE A2 ! ZONE B2 ! ZONE C2 ! ZONE D2 ! ZONE E2 !

!--------------!------------------!---------------!--------------!---------------!

! ADAPTED(G) ! ALT (M) ! NAV (C) ! SINGLE (W) ! _ !

! ! ALT (C) ! APP NAV (C) ! DUAL (W) ! FD1 (W) ! * !

! ! CLB (C) ! LOC (C) ! ! FD2 (W) _! !

! ! DES (C) ! LOC B/C (C) ! ! _ !

! ! G/S (C) ! ! ! 1FD2 (W) ! !

! ! FINAL (C) ! ! ! 1FD1 (W) ! !

! ! ALT (C) G/S (C) ! ! ! 2FD2 (W) ! !

! ! ALT (M) G/S (C) ! ! ! 1FD- (W) ! ** !

! ! ALT (C) FINAL (C)! ! ! 2FD- (W) ! !

! ! ALT (M) FINAL (C)! ! ! -FD1 (W) ! !

! ! DES (C) G/S (C) ! ! ! -FD2 (W)_! !

! ! DES (C) FINAL (C)! ! ! !

! ! OP CLB (C) ! ! ! !

*A/THR programming pin of the FMGC not activated
**A/THR programming pin of the FMGC activated

-------------------------------------------------------------------------------

! ZONE A2 ! ZONE B2 ! ZONE C2 ! ZONE D2 ! ZONE E2 !

!-----------!------------------!---------------!--------------!---------------!

! ! ALT (M) ! NAV (C) ! SINGLE (W) ! _ !

! ! ALT (C) ! APP NAV (C) ! DUAL (W) ! FD1 (W) ! * !

! ! CLB (C) ! LOC (C) ! ! FD2 (W) _! !

! ! DES (C) ! ! ! _ !

! ! G/S (C) ! ! ! 1FD2 (W) ! !

! ! FINAL (C) ! ! ! 1FD1 (W) ! !

! ! ALT (C) G/S (C) ! ! ! 2FD2 (W) ! !

! ! ALT (M) G/S (C) ! ! ! 1FD- (W) ! ** !

! ! ALT (C) FINAL (C)! ! ! 2FD- (W) ! !

! ! ALT (M) FINAL (C)! ! ! -FD1 (W) ! !

! ! DES (C) G/S (C) ! ! ! -FD2 (W)_! !

! ! DES (C) FINAL (C)! ! ! !

* : A/THR programming pin of FMGC not activated
** : A/THR programming pin of FMGC activated

---------------------------

! ZONE BC1 !

!-------------------------!

! FINAL APP (G) !

! FLARE (G) !

! ROLL OUT (G) !

! LAND (G) !

---------------------------

-------------------------------

! ZONE AB3 !

-------------------------------

! SPEED SEL : XXX (C) !

! MACH SEL : .XX (C) !

-------------------------------

-------------------------------------------------------------------------------

! ZONE A3 ! ZONE BC3 ! ZONE D3 ! ZONE E3 !

!--------------!------------------------- !-------------------!---------------!

! ! MAN PITCH TRIM ONLY (R) ! ! !

! ! ! ! !

! ! USE MAN PITCH TRIM (A) ! ! !

! ! ! ! !

! ! FOR GA: SET TOGA (A) ! ! !

! ! ! ! !

! ! TCAS (C) ! ! !

! ! ! ! !

! ! DISCONNECT AP FOR LDG (A)! ! !

! ! ! ! !

! ! TCAS RA INHIBITED (w) ! ! !

! ! ! ! !

! ! TRK FPA DESELECTED (w) ! ! !

! ! ! ! !

! THR LK (A) ! SET GREEN DOT SPEED (W) ! QFE/QNH pin prog ! !

! ! ! ! !

! (flashing) ! ! not activated: ! A/THR (W) !

! ! ! ! !

! LVR TOGA (W) ! ! : ! !

! (flashing) ! ! ! !

! ! T/D REACHED (W) ! - DH (W) XXX (C) ! A/THR (C) !

! LVR ASYM (A) ! ! - NO DH (W) ! !

! ! MORE DRAG (W) ! - MDA (W) XXXXX(C)! !

! LVR CLB (W) ! ! - MDH (W) XXXXX(C)! !

! (flashing) ! CHECK SPEED MODE (W) ! ! !

! ! ! QFE/QNH pin prog ! !

! LVR MCT (W) ! CHECK APPR SELECTION (W) ! activated: ! !

! (flashing) ! ! - RADIO (W) XXX(C)! !

! ! ! ! !

! ! TURN AREA EXCEEDANCE (W) ! ! !

! ! ! ! !

! ! SET HOLD SPEED (W) ! - NO DH (W)! !

! ! ! - BARO (W) XXXX(C)! !

! ! VERT DISCONT AHEAD (A) ! ! !

! ! ! ! !

! ! FINAL APP SELECTED (W) ! ! !

---------------------------

! ZONE BC1 !

!-------------------------!

! FINAL APP (G) !

! FLARE (G) !

! ROLL OUT (G) !

! LAND (G) !

---------------------------

-------------------------------

! ZONE AB3 !

-------------------------------

! SPEED SEL : XXX (C) !

! MACH SEL : .XX (C) !

-------------------------------

----------------------------------------------------------------------------------

! ZONE A3 ! ZONE BC3 ! ZONE D3 ! ZONE E3 !

!--------------!-----------------------------!-------------------!---------------!

! ! MAN PITCH TRIM ONLY (R) ! ! !

! ! ! ! !

! ! USE MAN PITCH TRIM (A) ! ! !

! ! ! ! !

! ! FOR GA: SET TOGA (A) ! ! !

! ! ! ! !

! ! TCAS (C) ! ! !

! ! ! ! !

! ! DISCONNECT AP FOR LDG (A) ! ! !

! ! ! ! !

! ! TCAS RA INHIBITED (w) ! ! !

! ! ! ! !

! ! TRK FPA DESELECTED (w) ! ! !

! ! ! ! !

! THR LK (A) ! SET GREEN DOT SPEED (W) ! QFE/QNH pin prog ! !

! ! ! ! !

! (flashing) ! ! not activated: ! A/THR (W) !

! ! ! ! !

! LVR TOGA (W) ! ! : ! !

! (flashing) ! ! ! !

! ! T/D REACHED (W) ! - DH (W) XXX (C) ! A/THR (C) !

! LVR ASYM (A) ! ! - NO DH (W) ! !

! ! MORE DRAG (W) ! - MDA (W) XXXXX(C)! !

! LVR CLB (W) ! ! - MDH (W) XXXXX(C)! !

! (flashing) ! CHECK SPEED MODE (W) ! ! !

! ! ! QFE/QNH pin prog ! !

! LVR MCT (W) ! CHECK APPR SELECTION (W) ! activated: ! !

! (flashing) ! ! - RADIO (W) XXX(C)! !

! ! ! ! !

! ! TURN AREA EXCEEDANCE (W) ! ! !

! ! ! ! !

! ! SET HOLD SPEED (W) ! - NO DH (W)! !

! ! ! - BARO (W) XXXX(C)! !

! ! VERT DISCONT AHEAD (A) ! ! !

! ! ! ! !

! ! FINAL APP SELECTED (W) ! ! !

! ! ! ! !

! ! FCU ALT ABOVE A/C (W) ! ! !

! ! ! ! !

! ! FCU ALT BELOW A/C (W) ! ! !

! ! ! ! !

! ! AP AVAIL: V/S+0 HDG ONLY (W)! ! !

! ! ! ! !

! ! AP AVAIL: FPA+0 TRK ONLY (W)! ! !

! ! ! ! !

! ! AP IN PROT (A) ! ! !

---------------------------

! ZONE BC1 !

!-------------------------!

! FINAL APP (G) !

! FLARE (G) !

! ROLL OUT (G) !

! LAND (G) !

---------------------------

-------------------------------

! ZONE AB3 !

-------------------------------

! SPEED SEL : XXX (C) !

! MACH SEL : .XX (C) !

-------------------------------

-------------------------------------------------------------------------------

! ZONE A3 ! ZONE BC3 ! ZONE D3 ! ZONE E3 !

!---------------!-------------------------!-------------------!---------------!

! THR LK (A) ! SET GREEN DOT SPD (W) ! DH (W) XXX (C) ! A/THR (W) !

! (flashing) ! ! ! !

! ! DECELERATE (W) ! NO DH (W) ! A/THR (C) !

! LVR ASYM (A) ! ! ! !

! ! MORE DRAG (W) ! MDA (W) XXXXX (C) ! !

! LVR CLB (W) ! ! ! !

! (flashing) ! SET MANAGED SPD (W) ! ! !

! ! ! ! !

! LVR MCT (W) ! CHECK APP SEL (W) ! ! !

! (flashing) ! ! ! !

! ! SET HOLD SPD (W) ! ! !

! ! ! ! !

! ! VERT DISCONT AHEAD (A) ! ! !

! ! ! ! !

! ! USE MAN PITCH TRIM (A) ! ! !

! ! ! ! !

! ! MAN PITCH TRIM ONLY (R) ! ! !

---------------------------

! ZONE BC1 !

!-------------------------!

! FINAL APP (G) !

! FLARE (G) !

! ROLL OUT (G) !

! LAND (G) !

---------------------------

-------------------------------

! ZONE AB3 !

-------------------------------

! SPEED SEL : XXX (C) !

! MACH SEL : .XX (C) !

-------------------------------

-------------------------------------------------------------------------------

! ZONE A3 ! ZONE BC3 ! ZONE D3 ! ZONE E3 !

!---------------!--------------------------!------------------!---------------!

! ! MAN PITCH TRIM ONLY (R) ! ! !

! ! ! ! !

! ! USE MAN PITCH TRIM (A) ! ! !

! ! ! ! !

! ! FOR GA: SET TOGA (A) ! ! !

! ! ! ! !

! ! TCAS (C) ! ! !

! ! ! ! !

! ! DISCONNECT AP FOR LDG (A)! ! !

! ! ! ! !

! ! TCAS RA INHIBITED (w) ! ! !

! ! ! ! !

! ! TRK FPA DESELECTED (W) ! ! !

! ! ! ! !

! THR LK (A) ! SET GREEN DOT SPEED (W) ! DH (W) XXX (C) ! A/THR (W) !

! (flashing) ! ! ! !

! ! ! ! !

! LVR TOGA (W) ! ! ! !

! (flashing) ! ! ! !

! ! T/D REACHED (W) ! NO DH (W) ! A/THR (C) !

! LVR ASYM (A) ! ! ! !

! ! MORE DRAG (W) ! MDA (W) XXXXX (C)! !

! LVR CLB (W) ! ! ! !

! (flashing) ! CHECK SPEED MODE (W) ! ! !

! ! ! ! !

! LVR MCT (W) ! CHECK APP SELECTION (W) ! ! !

! (flashing) ! ! ! !

! ! TURN AREA EXCEEDANCE (W) ! ! !

! ! ! ! !

! ! SET HOLD SPEED (W) ! ! !

! ! ! ! !

! ! VERT DISCONT AHEAD (A) ! ! !

! ! ! ! !

! ! FINAL APP SELECTED (W) ! ! !

M. Flight Mode Annunciator - Messages Signification
The following table shows the indications related to the autothrottle system operation.

-------------------------------------------------------------------------------

! DISPLAY ! COLOR ! BUS ! LABEL ! BIT No. ! SIGNIFICATION !

!-------------!----------!-------!---------!---------!------------------------!

! MAN TOGA ! WHITE ! FCU ! 147 ! 11 ! !

! MAN FLX ! WHITE ! FCU ! 147 ! 13 ! !

! MAN MCT ! WHITE ! FCU ! 147 ! 12 ! Max Continuous Thrust !

! or ! ! ! ! ! !

! THR MCT ! GREEN ! FCU ! 147 ! 12 ! !

! THR CLB ! GREEN ! FCU ! 147 ! 14 ! !

! MAN THR ! WHITE ! FCU ! 147 ! 15 ! !

! or ! ! ! ! ! !

! THR LVR ! GREEN ! FCU ! 147 ! 15 ! !

! THR IDLE ! GREEN ! FCU ! 147 ! 16 ! !

! A.FLOOR ! GREEN ! FCU ! 147 ! 17 ! Alpha Floor !

! TOGA LK ! GREEN ! FCU ! 147 ! 18 ! TOGA Lock !

! SPEED ! GREEN ! FCU ! 147 ! 19 ! !

! MACH ! GREEN ! FCU ! 147 ! 20 ! !

! LVR MCT ! WHITE ! FCU ! 147 ! 23 ! !

! LVR CLB ! WHITE ! FCU ! 147 ! 22 ! !

! LVR ASYM ! AMBER ! FCU ! 147 ! 21 ! !

! THR LK ! AMBER ! ECU ! 355 ! 12 ! Thrust Lock !

! ! !or EEC ! 270 ! 22 ! !

The following table shows the indications related to the autothrottle system operation.

-------------------------------------------------------------------------------

! DISPLAY ! COLOR ! BUS ! LABEL ! BIT No. ! SIGNIFICATION !

!-------------!----------!-------!---------!---------!------------------------!

! MAN TOGA ! WHITE ! FCU ! 147 ! 11 ! !

! MAN FLX ! WHITE ! FCU ! 147 ! 13 ! !

! MAN MCT ! WHITE ! FCU ! 147 ! 12 ! Max Continuous Thrust !

! or ! ! ! ! ! !

! THR MCT ! GREEN ! FCU ! 147 ! 12 ! !

! THR CLB ! GREEN ! FCU ! 147 ! 14 ! !

! MAN THR ! WHITE ! FCU ! 147 ! 15 ! !

! or ! ! ! ! ! !

! THR LVR ! GREEN ! FCU ! 147 ! 15 ! !

! THR IDLE ! GREEN ! FCU ! 147 ! 16 ! !

! A.FLOOR ! GREEN ! FCU ! 147 ! 17 ! Alpha Floor !

! TOGA LK ! GREEN ! FCU ! 147 ! 18 ! TOGA Lock !

! SPEED ! GREEN ! FCU ! 147 ! 19 ! !

! MACH ! GREEN ! FCU ! 147 ! 20 ! !

! LVR MCT ! WHITE ! FCU ! 147 ! 23 ! !

! LVR CLB ! WHITE ! FCU ! 147 ! 22 ! !

! LVR ASYM ! AMBER ! FCU ! 147 ! 21 ! !

! THR LK ! AMBER ! ECU ! 355 ! 12 ! Thrust Lock !

! ! !or EEC ! 270 ! 22 ! !

! DTO display ! WHITE ! FCU ! 147 ! 29 ! !

The following table shows the indications related to the autothrottle system operation.

-------------------------------------------------------------------------------

! DISPLAY ! COLOR ! BUS ! LABEL ! BIT No. ! SIGNIFICATION !

!-------------!----------!-------!---------!---------!------------------------!

! MAN TOGA ! WHITE ! FCU ! 147 ! 11 ! !

! MAN GA SOFT ! WHITE ! FMGC ! 227 ! 21 ! !

! MAN FLX ! WHITE ! FCU ! 147 ! 13 ! !

! MAN DTO ! WHITE ! FCU ! 147 ! 29 ! !

! MAN MCT ! WHITE ! FCU ! 147 ! 12 ! Max Continuous Thrust !

! MAN THR ! WHITE ! FCU ! 147 ! 15 ! !

! SPEED ! GREEN ! FCU ! 147 ! 19 ! !

! MACH ! GREEN ! FCU ! 147 ! 20 ! !

! THR MCT ! GREEN ! FCU ! 147 ! 12 ! !

! THR CLB ! GREEN ! FCU ! 147 ! 14 ! !

! THR LVR ! GREEN ! FCU ! 147 ! 15 ! !

! THR IDLE ! GREEN ! FCU ! 147 ! 16 ! !

! A.FLOOR ! GREEN ! FCU ! 147 ! 17 ! Alpha Floor !

! TOGA LK ! GREEN ! FCU ! 147 ! 18 ! TOGA Lock !

! THR LK ! AMBER ! ECU ! 355 ! 12 ! Thrust Lock !

! ! !or EEC ! 270 ! 22 ! !

! LVR TOGA ! WHITE ! FMGC ! 267 ! 23 ! !

! LVR CLB ! WHITE ! FCU ! 147 ! 22 ! !

! LVR MCT ! WHITE ! FCU ! 147 ! 23 ! !

! LVR ASYM ! AMBER ! FCU ! 147 ! 21 ! !

The following table shows the indications related to the A/C longitudinal control.

-------------------------------------------------------------------------------

! DISPLAY ! COLOR ! BUS ! LABEL ! BIT No. ! SIGNIFICATION !

!--------------!------------!------!-------!---------!------------------------!

! SRS ! GREEN ! FMGC ! 274 ! 15-16 ! Pitch Take-off/Pitch Go!

! ! ! ! ! ! around !

! ALT CRZ ! GREEN ! FMGC ! 274 ! 26 ! Cruise Level Hold !

! ALT * ! GREEN ! FMGC ! 274 ! 21-19 ! Alt Capture Mode !

! ALT ! GREEN ! FMGC ! 274 ! 20-19 ! !

! V/S +/- XXXX ! GREEN/CYAN ! FMGC ! 274 ! 17 ! Vertical Speed Mode !

! FPA +/- X.X ! GREEN/CYAN ! FMGC ! 274 ! 18 ! FPA mode !

! EXP CLB ! GREEN ! FMGC ! 274 ! 24-11 ! !

! EXP DES ! GREEN ! FMGC ! 274 ! 24-12 ! !

! G/S * ! GREEN ! FMGC ! 274 ! 20-21 ! Glide Capture Mode !

! G/S ! GREEN ! FMGC ! 274 ! 20-22 ! Glide Track Mode !

! CLB ! GREEN ! FMGC ! 274 ! 26-11 ! !

! ! ! ! ! 14-17 ! !

! ! ! ! ! 18-24 ! !

! DES ! GREEN ! FMGC ! 274 ! 12-26 ! !

! ! ! ! ! 14-17 ! !

! ! ! ! ! 18-24 ! !

! OP CLB ! GREEN ! FMGC ! 274 ! 11-14 ! Open Climb !

! OP DES ! GREEN ! FMGC ! 274 ! 12-14 ! Open Descent !

! FINAL ! GREEN ! FMGC ! 274 ! 23 ! Final Descent Mode !

! ALT CST * ! GREEN ! FMGC ! 274 ! 19 ! Constrained Level !

! ! ! ! ! ! Capture !

! ALT CST ! GREEN ! FMGC ! 274 ! 19-26 ! Constrained Level Hold !

! ! ! ! !or 19-20 ! !

! ALT ! MAGENTA ! FMGC ! 273 ! 12 ! !

! ALT ! CYAN ! FMGC ! 273 ! 12 ! Acquired Altitude Armed!

! CLB ! CYAN ! FMGC ! 273 ! 24 ! Climb Armed !

! DES ! CYAN ! FMGC ! 273 ! 25 ! Descent Armed !

! G/S ! CYAN ! FMGC ! 273 ! 22 ! Glide Armed !

! FINAL ! CYAN ! FMGC ! 273 ! 23 ! !

!SPEED SEL XXXX! CYAN ! FMGC ! 107 ! ! !

!MACH SEL .XX ! CYAN ! FMGC ! 106 ! ! !

The following table shows the indications related to the A/C lateral control.

-------------------------------------------------------------------------------

! DISPLAY ! COLOR ! BUS ! LABEL ! BIT No. ! SIGNIFICATION !

!-------------!----------!-------!---------!---------!------------------------!

! HDG ! ! FMGC ! 275 ! 16 ! !

! LOC * ! ! FMGC ! 275 ! 13 ! LOC capture !

! LOC ! GREEN ! FMGC ! 275 ! 14 ! !

! NAV ! GREEN ! FMGC ! 275 ! 12 ! !

! RWY ! ! FMGC ! 275 ! 11-20 ! Runway Mode !

! TRACK ! ! FMGC ! 275 ! 17 ! Track Mode !

! RWY TRK ! ! FMGC ! 275 ! 11-23 ! !

! GA TRK ! ! FMGC ! 275 ! 11-15 ! !

! NAV ! CYAN ! FMGC ! 273 ! 14 ! _ !

! APP NAV ! GREEN ! FMGC ! 275 ! 12 ! NAV Mode ! with FMGC !

! APP NAV ! CYAN ! FMGC ! 273 ! 14 ! NAV Armed ! 273-23 or !

! ! ! ! ! ! _! 274-23 !

! LOC ! CYAN ! FMGC ! 273 ! 16 ! LOC Armed !

The following table shows the common mode indications and special messages.

-------------------------------------------------------------------------------

! DISPLAY ! COLOR ! BUS ! LABEL ! BIT No. ! SIGNIFICATION !

!-------------!----------!-------!---------!---------!------------------------!

! FLARE ! GREEN ! FMGC ! 274 ! 25 ! !

! ROLL OUT ! GREEN ! FMGC ! 275 ! 26 ! !

! LAND ! GREEN ! FMGC ! 146 ! 14 ! Land track mode !

! SET GREEN ! WHITE ! FMGC- ! 271 ! 14 ! !

! DOT SPD ! ! EIS ! ! ! !

! DECELERATE ! WHITE ! FMGC- ! 271 ! 15 ! !

! ! ! EIS ! ! ! !

! MORE DRAG ! WHITE ! FMGC- ! 271 ! 16 ! !

! ! ! EIS ! ! ! !

! SET MANAGED ! WHITE ! FMGC- ! 271 ! 17 ! !

! SPD ! ! EIS ! ! ! !

! CHECK APP ! WHITE ! FMGC- ! 271 ! 21 ! !

! SEL ! ! EIS ! ! ! !

! SET HOLD ! WHITE ! FMGC- ! 271 ! 24 ! !

! SPD ! ! EIS ! ! ! !

! VERT DISC ! AMBER ! FMGC- ! 271 ! 27 ! !

! AHEAD ! ! EIS ! ! ! !

! FINAL APP ! GREEN ! FMGC ! 274 ! 23 ! !

! ! ! ! 273 ! 23 ! !

! USE MAN ! AMBER ! FWC ! 040 ! ! !

! PITCH TRIM ! ! ! ! ! !

! MAN PITCH ! RED ! FWC ! 040 ! ! !

! TRIM ONLY ! ! ! ! ! !

The following table shows the common mode indications and special messages.

-------------------------------------------------------------------------------

! DISPLAY ! COLOR ! BUS ! LABEL ! BIT No. ! SIGNIFICATION !

!-------------!----------!-------!---------!---------!------------------------!

! ROLL OUT ! GREEN ! FG ! 275 ! 26 ! Roll out mode active !

! ! ! ! ! ! !

! FLARE ! GREEN ! FG ! 274 ! 25 ! Flare mode active !

! ! ! ! ! ! !

! LAND ! GREEN ! FG ! 146 ! 14 ! Land track mode active !

! ! ! ! ! ! !

! FINAL APP ! GREEN ! FG ! 274 ! 23 ! Final approach mode !

! ! ! FG ! 275 ! 12 ! active !

! ! ! ! ! ! !

! ! ! ! ! 11 12 13! !

! MAN PITCH ! RED ! FCDC ! 040 ! 15 ! !

! TRIM ONLY ! ! ! ! ! !

! ! ! ! ! ! !

! USE MAN ! AMBER ! FWC ! 124 ! 29 ! !

! PITCH TRIM ! ! FCDC ! 040 ! 15 ! !

! ! ! ! ! ! !

! FOR GA: ! AMBER ! FG ! 267 ! 26 ! !

! SET TOGA ! ! ! ! ! !

! ! ! ! ! ! !

! TCAS ! CYAN ! FG ! 277 ! 12 ! !

! ! ! ! ! ! !

! ! ! ! ! 20 ! !

! DISCONNECT ! AMBER ! FG ! 273 ! 12 18 17! !

! AP FOR LDG ! ! FG ! 274 ! 23 ! !

! ! ! LGC ! 20 ! 25 ! !

! ! ! LGC ! 22 ! 13 ! !

! ! ! ! ! ! !

! TCAS RA ! WHITE ! FG ! 277 ! 24 ! !

! INHIBITED ! ! ! ! ! !

! ! ! ! ! ! !

! TRK FPA ! WHITE ! FG ! 277 ! 25 ! !

! DESELECTED ! ! ! ! ! !

! ! ! ! ! ! !

! SET GREEN ! WHITE ! FM ! 271 ! 14 ! !

! DOT SPEED ! ! ! ! ! !

! ! ! ! ! ! !

! T/D REACHED ! WHITE ! FM ! 271 ! 15 ! !

! ! ! ! ! ! !

! MORE DRAG ! WHITE ! FM ! 271 ! 16 ! !

! ! ! ! ! ! !

! CHECK SPEED ! WHITE ! FM ! 271 ! 17 ! !

! MODE ! ! ! ! ! !

! ! ! ! ! ! !

! CHECK APPR ! WHITE ! FM ! 271 ! 21 ! !

! SELECTION ! ! ! ! ! !

! ! ! ! ! ! !

! TURN AREA ! WHITE ! FM ! 272 ! 29 ! !

! EXCEEDANCE ! ! ! ! ! !

! ! ! ! ! ! !

! SET HOLD ! WHITE ! FM ! 271 ! 24 ! !

! SPEED ! ! ! ! ! !

! ! ! ! ! ! !

! VERT DISCONT! AMBER ! FM ! 271 ! 27 ! !

! AHEAD ! ! ! ! ! !

! ! ! ! ! ! !

! FINAL APP ! WHITE ! FM ! 273 ! 29 ! !

! SELECTED ! ! ! ! ! !

! ! ! ! ! ! !

The following table shows the indications of approach capabilities.

-------------------------------------------------------------------------------

! DISPLAY ! COLOR ! BUS ! LABEL ! BIT No. ! SIGNIFICATION !

!-------------!----------!-------!---------!---------!------------------------!

! CAT 1 ! WHITE ! FMGC ! 146 ! 14-20- ! !

! ! ! ! !23-24-25 ! !

! CAT 2 ! WHITE ! FMGC ! 146 ! 23-25 ! !

! CAT 3 ! WHITE ! FMGC ! 146 ! 24-25 ! !

! SINGLE ! WHITE ! FMGC ! 146 ! 24-25 ! !

! DUAL ! WHITE ! FMGC ! 146 ! 25 ! !

! DH XXX !WHITE/CYAN! FMGC- ! 370 ! ! DH value !

! ! ! EIS ! ! ! !

! NO DH ! WHITE ! FMGC- ! 270 ! 29 ! !

! ! ! EIS ! ! ! !

! MDA XXXX !WHITE/CYAN! FMGC- ! 270 ! 28 ! MDA value !

! ! ! EIS ! ! ! !

The following table shows the indications of approach capabilities.

-------------------------------------------------------------------------------

! DISPLAY ! COLOR ! BUS ! LABEL ! BIT No. ! SIGNIFICATION !

!-------------!----------!-------!---------!---------!------------------------!

! CAT 1 ! WHITE ! FMGC ! 146 ! 14-20- ! !

! ! ! ! !23-24-25 ! !

! CAT 2 ! WHITE ! FMGC ! 146 ! 23-25 ! !

! CAT 3 ! WHITE ! FMGC ! 146 ! 24-25 ! !

! SINGLE ! WHITE ! FMGC ! 146 ! 24-25 ! !

! DUAL ! WHITE ! FMGC ! 146 ! 25 ! !

! DH XXX !WHITE/CYAN! FMGC- ! 370 ! ! DH value !

! ! ! EIS ! ! ! !

! NO DH ! WHITE ! FMGC- ! 270 ! 29 ! !

! ! ! EIS ! ! ! !

! MDA XXXX !WHITE/CYAN! FMGC- ! 270 ! 28 ! MDA value !

! ! ! EIS ! ! ! !

! MDH XXXX !WHITE/CYAN! FMGC- ! 164 ! ! MDA or MDH value !

! ! ! EIS ! 270 ! 28 ! !

! BARO XXXX ! CYAN ! FMGC- ! 272 ! 15 ! QFE/QNH pin prog !

! ! ! EIS ! 164 ! ! !

! RADIO XXX ! CYAN ! FMGC- ! 272 ! 15 ! QFE/QNH pin prog !

! ! ! EIS ! 370 ! ! !

The following table shows the indications related to AFS subsystem engagement status.

-------------------------------------------------------------------------------

! DISPLAY ! COLOR ! BUS ! LABEL ! BIT No. ! SIGNIFICATION !

!-------------!----------!-------!---------!---------!------------------------!

! AP1 + 2 ! WHITE ! FMGC ! 017 ! 16-24 ! !

! ! ! ! 146 ! 12 ! !

! AP1 ! WHITE ! FMGC ! 146 ! 12 ! !

! AP2 ! WHITE ! FMGC ! 017 ! 16-24 ! !

! ! ! _ ! ! ! !

! FD1 ! WHITE !! FMGC ! 146 ! 13 ! !

! ! !!_FCU ! 272 ! 23 ! !

! ! ! _ ! ! ! !

! FD2 ! WHITE !! FMGC ! 272 ! 23 ! !

! ! !!_FCU ! 272 ! 23 ! !

! ! ! _ ! ! ! !

! XFDY ! WHITE !! FMGC ! 146 ! 13 ! !

! ! !!_FCU ! 272 ! 23 ! !

! ! ! ! ! ! !

! A/THR ! WHITE ! FMGC ! 270 ! 13 ! A/THR ENGAGED !

! A/THR ! WHITE ! FMGC ! 270 ! 13-14 ! A/THR ENGAGED AND !

! ! ! ! ! ! ACTIVATED !

NOTE: As an option (A/THR programming pin of FMGC, label 270 bit 15), in zone E2 of FMA, identification of the flight director used by the pilot must also indicate FD selection of the opposite side, as follows:
XFDY where X = CAPT side selection and Y = F/O side selection.
X or Y = 1, 2 or - depending on whether FD1, FD2 or no FD is selected.
As soon as an FD is engaged on one side, corresponding FMA display is shown on both CAPT and F/O PFDs even if the FD has not been selected on the opposite side.

N. Flight Mode Annunciator - Condition of Display
The table below gives the conditions of display of the FMA messages:

-------------------------------------------------------------------------------

! MESSAGES ! DISPLAY !

!----------------------!------------------------------------------------------!

! MAN PITCH TRIM ONLY ! - Red message in zone BC3 of FMA when manual pitch !

! ! trim is the only pitch control available, flashing !

! ! for 9s then steady. !

!----------------------!------------------------------------------------------!

! USE MAN PITCH TRIM ! - Amber message in zone BC3 of FMA when automatic !

! ! pitch trim is no longer available, pulsing for 9s !

! ! then steady. !

!----------------------!------------------------------------------------------!

! CHECK APP SEL ! - White message in zone BC3 of FMA when the approach !

! ! phase of the FM flight plan has to be reviewed. !

!----------------------!------------------------------------------------------!

! SET MANAGED SPD ! - White message in zone BC3 of FMA when aircraft !

! ! speed control has to be transferred to the FM. !

!----------------------!------------------------------------------------------!

! SET GREEN DOT SPD ! - White message in zone BC3 of FMA when the final !

! ! take-off speed had to be set while in engine out !

! ! mode. !

!----------------------!------------------------------------------------------!

! SET HOLD SPD ! - White message in zone BC3 of FMA when a speed has !

! ! to be set before entering a holding pattern. !

The table below gives the conditions of display of the FMA messages:

-------------------------------------------------------------------------------

! MESSAGES ! DISPLAY !

!----------------------!------------------------------------------------------!

! MAN PITCH TRIM ONLY ! - Red message in zone BC3 of FMA when manual pitch !

! ! trim is the only pitch control available, flashing !

! ! for 9s then steady. !

!----------------------!------------------------------------------------------!

! USE MAN PITCH TRIM ! - Amber message in zone BC3 of FMA when automatic !

! ! pitch trim is no longer available, pulsing for 9s !

! ! then steady. !

!----------------------!------------------------------------------------------!

! CHECK APPR SELECTION ! - White message in zone BC3 of FMA when the approach !

! ! phase of the FM flight plan has to be reviewed. !

!----------------------!------------------------------------------------------!

! SET MANAGED SPEED ! - White message in zone BC3 of FMA when aircraft !

! ! speed control has to be transferred to the FM. !

!----------------------!------------------------------------------------------!

! SET GREEN DOT SPEED ! - White message in zone BC3 of FMA when the final !

! ! take-off speed had to be set while in engine out !

! ! mode. !

!----------------------!------------------------------------------------------!

! SET HOLD SPEED ! - White message in zone BC3 of FMA when a speed has !

! ! to be set before entering a holding pattern. !

The table below gives the conditions of display of the FMA messages:

-------------------------------------------------------------------------------

! MESSAGES ! DISPLAY !

!----------------------!------------------------------------------------------!

! MAN PITCH TRIM ONLY ! - Red message in zone BC3 of FMA when manual pitch !

! ! trim is the only pitch control available, flashing !

! ! for 9s, then steady. !

!----------------------!------------------------------------------------------!

! USE MAN PITCH TRIM ! - Amber message in zone BC3 of FMA when automatic !

! ! pitch trim is no longer available, pulsing for 9s, !

! ! then steady. !

!----------------------!------------------------------------------------------!

! ! - Amber message in zone BC3 of the FMA when a go !

! FOR GA SET TOGA ! around with thrust levers is not in TOGA detent, !

! ! pulsing for 9s, then steady. !

! ! - Inhibited in case of excessive attitude. !

!----------------------!------------------------------------------------------!

! TCAS ! - Cyan message in zone BC3 of FMA when the AP/FD !

! ! TCAS mode is armed. !

! ! - Inhibited in case of excessive attitude. !

!----------------------!------------------------------------------------------!

! DISCONNECT AP ! - Amber message in zone BC3 of FMA when the crew has !

! FOR LDG ! to deselect the AP to continue the approach !

! ! manually in non precision approaches. !

! ! - Inhibited when the AP/FD TCAS mode is engaged. !

! ! - Inhibited in case of excessive attitude. !

!----------------------!------------------------------------------------------!

! TCAS RA INHIBITED ! - White message in BC3 zone of the FMA when the !

! ! AP/FD TCAS guidance is lost during a resolution !

! ! advisory. !

! ! - Inhibited in case of excessive attitude. !

!----------------------!------------------------------------------------------!

! TRK FPA DESELECTED ! - White message in zone BC3 of FMA when TRK-FPA !

! ! selection has been deselected in AP/FD TCAS mode. !

! ! - Inhibited in case of excessive attitude. !

!----------------------!------------------------------------------------------!

! SET GREEN DOT SPEED ! - White message in BC3 zone of FMA when the final !

! ! take-off speed had to be set while in engine out !

! ! mode. !

! ! - Inhibited when the AP/FD TCAS mode is engaged. !

! ! - Inhibited in case of excessive attitude. !

!----------------------!------------------------------------------------------!

! T/D REACHED ! - White message in BC3 zone of the FMA when the !

! ! thrust is not reduced when passing the top of !

! ! descent, and the aircraft is above the flight !

! ! profile. !

! ! - Inhibited when the AP/FD TCAS mode is engaged. !

! ! - Inhibited in case of excessive attitude. !

!----------------------!------------------------------------------------------!

! MORE DRAG ! - White message in BC3 zone of the FMA when the !

! ! speed brake has to be extended during descent. !

! ! - Inhibited in case of excessive attitude. !

!----------------------!------------------------------------------------------!

! CHECK SPEED MODE ! - White message in BC3 zone of the FMA when a speed !

! ! target is selected and a preselected SPEED does !

! ! not exist for the next phase. !

! ! - Inhibited when the AP/FD TCAS mode is engaged. !

! ! - Inhibited in case of excessive attitude. !

!----------------------!------------------------------------------------------!

! CHECK APPR SELECTION ! - White message in BC3 zone of the FMA when the !

! ! approach phase of the FM flight plan has to be !

! ! reviewed. !

! ! - Inhibited in case of excessive attitude. !

!----------------------!------------------------------------------------------!

! TURN AREA EXCEEDANCE ! - White message in zone BC3 of FMA when the aircraft !

! ! exceeded the maximal distance of excursion. !

! ! - Inhibited when the AP/FD TCAS mode is engaged. !

! ! - Inhibited in case of excessive attitude. !

!----------------------!------------------------------------------------------!

! SET HOLD SPEED ! - White message in zone BC3 of FMA when a speed has !

! ! to be set before entering a holding pattern. !

! ! - Inhibited when the AP/FD TCAS mode is engaged. !

! ! - Inhibited in case of excessive attitude. !

!----------------------!------------------------------------------------------!

! VERT DISCONT AHEAD ! - Amber message in BC3 zone of the FMA when a !

! ! vertical discontinuity has to be cleared in the !

! ! FM flight plan. !

! ! - Inhibited in case of excessive attitude. !

!----------------------!------------------------------------------------------!

! FINAL APP SELECTED ! - White message in zone BC3 of FMA when Final !

! ! Approach has been selected on MCDU whereas !

! ! LS push button is ON. !

! ! - Inhibited in case of excessive attitude. !

!----------------------!------------------------------------------------------!

-------------------------------------------------------------------------------

! VERT DISCONT AHEAD ! - Amber message in zone BC3 of the FMA when a !

! ! vertical discontinuity has to be cleared in the FM !

! ! flight plan. !

!----------------------!------------------------------------------------------!

! DECELERATE ! - White message in zone BC3 of the FMA when the crew !

! ! has to decelerate in order to match the descent !

! ! phase of the FM flight plan. !

!----------------------!------------------------------------------------------!

! MORE DRAG ! - White message in zone BC3 of the FMA when the speed!

! ! brake has to be extended during an FMGC approach. !

!----------------------!------------------------------------------------------!

! TCAS AREA EXCEEDANCE ! - White message in zone BC3 of the FMA when the !

! ! aircraft exceeded the maximal distance of excursion!

! ! with no excessive altitude. !

! ! - Inhibited when the AP/FD TCAS mode is armed. !

!----------------------!------------------------------------------------------!

! TCAS ! - Cyan message in zone BC3 of the FMA when the AP/FD !

! ! TCAS mode is armed with no excessive altitude. !

!----------------------!------------------------------------------------------!

! TCAS RA INHIBITED ! - White message in zone BC3 of the FMA when the AP/FD!

! ! TCAS guidance is lost during RA with no excessive !

! ! altitude. !

The table below gives the conditions of display of the FMA flags:

-------------------------------------------------------------------------------

! FLAGS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! MAN PITCH TRIM ONLY! - Red flag in zone BC3 of FMA when pitch trim is only !

! ! by mechanical back up, before flight phase 4 or !

! ! after flight phase 5, flashing during 9s then !

! ! steady !

!--------------------!--------------------------------------------------------!

! USE MAN PITCH TRIM ! - Amber message in zone BC3 of FMA when pitch trim is !

! ! only by direct law, pulsing during 9s then steady. !

O. ILS Guidance and Vertical Deviation
When the pilot presses the LS pushbutton switch located on his EFIS control section, the Glide Slope and Localizer scales come into view on his PFD (as well as the ILS CRS symbol on the HDG scale).

P. ILS Guidance and Vertical Deviation - LS Approach

PFD - ILS Approach Display ** ON A/C NOT FOR ALL

In addition to the scales and the ILS CRS symbol, the LS identification (if available) frequency and the DME distance, in case of co-located DME, or the distance to threshold, in case of GLS approach (if available), are displayed on the PFD left bottom corner.

PFD - ILS Approach Display ** ON A/C NOT FOR ALL

item (A).
item (a).
** MLS or GLS option is not installed on MMR **
If the LOC or G/S signals are not valid, the ILS red flag is displayed provided the L/S pushbutton switch is pressed on FCU. It flashes during 9s then is steady.

** MLS or GLS option is installed on MMR **
In case of an ILS approach:

If the LOC or G/S signals are not valid or if the function ILS is selected but not active, a ILS red flag is displayed provided the LS pushbutton switch is pressed on EFIS control panel. It flashes 9s then is steady.
If there is a discrepancy in the selected approach mode, a LS red flag is displayed provided LS pushbutton switch is pressed on EFIS control panel. It flashes 9s then is steady. The LS flag has priority on the ILS one.
In case of an MLS approach:
If the LOC or G/S signals are not valid or if the function MLS is selected but not active, a MLS red flag is displayed provided the LS pushbutton switch is pressed on EFIS control panel. It flashes 9s then is steady.
If there is a discrepancy in the selected approach mode, a LS red flag is displayed provided LS pushbutton switch is pressed on EFIS control panel. It flashes 9s then is steady. The LS flag has priority on the MLS one.
In case of an GLS approach:
If the LOC or G/S signals are not valid or if the function GLS is selected but not active, a GLS red flag is displayed provided the LS pushbutton switch is pressed on EFIS control panel. It flashes 9s then is steady.
If there is a discrepancy in the selected approach mode, a LS red flag is displayed provided LS pushbutton switch is pressed on EFIS control panel. It flashes 9s then is steady. The LS flag has priority on the GLS one.
PFD - ILS Approach Display ** ON A/C NOT FOR ALL
PFD - ILS Approach Display ** ON A/C NOT FOR ALL
item (B).

** The Microwave Landing System (MLS) or GBAS Landing System (GLS) or Satellite Landing System (SLS) option is not installed in the Multi-Mode Receiver (MMR) **
If the Localizer (LOC) or Glide Slope (G/S) signals are not correct, the Instrument Landing System (ILS) red flag is shown when the LS pushbutton switch is pushed on the (Flight Control Unit) FCU. It flashes during nine seconds, then is stable.
** The MLS or GLS or SLS option is installed in the MMR **

During an ILS Approach, on the left bottom corner of the PFD, an ILS red flag is shown if:

The LOC or G/S signals are not correct or the LS pushbutton switch is pushed on the Electronic Flight Instrument System (EFIS) control panel and the ILS function is off. It flashes nine seconds, then is stable.
There is a failure of the ILS Approach mode, when the LS pushbutton switch is pushed on the EFIS control panel. It flashes during nine seconds, then is stable.

During an MLS Approach, on the left bottom corner of the PFD, an MLS red flag is shown if:
The LOC or G/S signals are not correct or the LS pushbutton switch is pushed on the EFIS control panel and the MLS function is off. It flashes nine seconds, then is stable.
There is a failure of the MLS Approach mode, when the LS pushbutton switch is pushed on the EFIS control panel. It flashes during nine seconds, then is stable.

During an GLS Approach, on the left bottom corner of the PFD, a GLS red flag is shown if:
The LOC or G/S signals are not correct or the LS pushbutton switch is pushed on the EFIS control panel and the GLS function is off. It flashes nine seconds, then is stable.
There is a failure of the GLS Approach mode, when the LS pushbutton switch is pushed on the EFIS control panel. It flashes during nine seconds, then is stable.

During an SLS Approach, on the left bottom corner of the PFD, a SLS red flag is shown if:
The LOC or G/S signals are not correct or the LS pushbutton switch is pushed on the EFIS control panel and the SLS function is off. It flashes nine seconds, then is stable.
There is a failure of the SLS Approach mode, when the LS pushbutton switch is pushed on the EFIS control panel. It flashes during nine seconds, then is stable.
PFD - ILS Approach Display ** ON A/C NOT FOR ALL

item (B).

Q. ILS Guidance and Vertical Deviation - Markers
At the intersection of the G/S and LOC scales, the marker indication appears when the A/C overflies the corresponding beacon. These indications are respectively:

OM for Outer Marker (cyan color)
PFD - Marker Indications ** ON A/C NOT FOR ALL
item (A).
MM for Middle Marker (amber color).
IM for Inner Marker (white color).

In case of another message (ILS, MLS, GLS) displayed at the intersection , the markers are positionned lightly lower on the right.
When the pilot has selected an ILS approach on his MCDU and if he presses the APPR pushbutton switch on the FCU, without having pressed the ILS pushbutton switch before, an ILS amber message flashes to recall him to select the ILS indications on his PFD
In case of MLS or GLS approach ability installed the reminder ILS is replaced by LS with the same displaying conditions.

PFD - Marker Indications ** ON A/C NOT FOR ALL

item (B).
At the intersection of the G/S and LOC scales, when the aircraft flies over the related beacon and the LS pushbutton switch is pushed, the marker indication that follows is shown:

OM for the outer marker (in cyan), or
PFD - Marker Indications ** ON A/C NOT FOR ALL
item (A)
MM for the middle marker (in amber), or
IM for the inner marker (in white).

If there are other messages, the ILS, GLS, MLS, SLS, FLS or LOC/FLS indication is shown at the intersection of the G/S and LOC scale and the marker indication is shown at a small distance to the bottom right.

When the ILS Approach mode is selected on the Multipurpose Control & Display Unit (MCDU), the APPR pushbutton switch is pushed on the (Flight Control Unit) FCU and the ILS pushbutton switch is released, the ILS amber message flashes to tell the crew to select the ILS indications on its PFD.
This reminder message is shown only during the approach phase.

PFD - Marker Indications ** ON A/C NOT FOR ALL

item (B).

R. ILS Guidance and Vertical Deviation - Markers
At the intersection of the G/S and LOC scales, the marker indication appears when the A/C overflies the corresponding beacon. These indications are respectively:

OM for Outer Marker (cyan color)
PFD - Marker Indications ** ON A/C NOT FOR ALL
item (a).
MM for Middle Marker (amber color).
AWY for Inner Marker (white color).

When the pilot has selected an ILS approach on his MCDU and if he presses the APPR pushbutton switch on the FCU, without having pressed the ILS pushbutton switch before, an ILS amber message flashes to recall him to select the ILS indications on his PFD

PFD - Marker Indications ** ON A/C NOT FOR ALL

item (b).
When the DME distance is not available, a DME flag comes into view replacing the DME distance indication. On Captain's side this flag is DME1 and on F/O's it is DME2

PFD - Marker Indications ** ON A/C NOT FOR ALL

item (b).
(for the DME display conditions refer to AMM 31-65-00)

S. ILS Guidance and Vertical Deviation - Excessive Deviation
In case of excessive deviation of any of the 2 deviations (G/S or LOC) the corresponding scale and the associated index pulse.
In case of excessive deviation of any of the 2 deviations (G/S or LOC) the corresponding scale and the associated index flashes.

T. ILS Guidance and Vertical Deviation - Non Precision Approach

PFD - Back Course Display and Non Precision Approach Display ** ON A/C NOT FOR ALL

PFD - Non Precision Approach Display ** ON A/C NOT FOR ALL

If the pilot has selected a non precision approach (RNAV APP) through his MCDU, vertical deviation scale comes into view when the final descent is armed as well as the corresponding deviation index. These indications disappear below the MDA. If in that case, the pilot presses the ILS pushbutton switch, the GLIDE and the LOC scales appear.
but the V/DEV amber message flashes to remind the pilot to monitor the aircraft vertical trajectory on the vertical deviation scale. In this case, the pilot is expected to press the ILS pushbutton switch in order to display the V/DEV scale.

PFD - L/DEV and V/DEV Flags ** ON A/C NOT FOR ALL

PFD - V/DEV flag ** ON A/C NOT FOR ALL

The ILS symbology has priority on the vertical deviation one.
AS FOR THE ILS scales, when the pilot has selected a non-precision approach, the runway identificationand the associated runway heading are displayed on the PFD left bottom corner.

U. Lateral and Vertical Deviations - RNP Approach (non precision)
If the pilot has selected a RNP approach through his MCDU, vertical and lateral deviation scales come into view when in approach phase.
These indications disappear below the MDA when the pilot deselects the AP and continues the approach by flying the A/C manually.
The ILS symbology has priority over the vertical and lateral deviations. If ILS scale is selected, amber L/DEV and V/DEV messages flash to remind the pilot to monitor the aircraft lateral and vertical trajectories on the L/DEV and V/DEV scales. In this case, the pilot is expected to press the ILS pushbutton switch in order to display the L/DEV and V/DEV scales.

V. ILS Guidance and Lateral and Vertical Deviations - GPS PRIMARY Function
When GPS C1 option is fitted, the V/DEV scale and the index are displayed as soon as, either the FM approach phase from the FMS sequence has started or the A/C is in the FM approach area.
The V/DEV scale remains displayed until the Missed Approach Point of the sequence is reached, or basically the CLIMB phase is activated.

When GPS C1 option is fitted, the L/DEV and V/DEV scales and the index are displayed as soon as, either the FM approach phase from the FMS sequence has started or the A/C is in the FM approach area.
The L/DEV and V/DEV scales remain displayed until the Missed Approach Point of the sequence is reached, or basically the CLIMB phase is activated.

The V/DEV index disappears when the Minimum Descent Altitude is reached.

The L/DEV and V/DEV indexes disappear when the Minimum Descent Altitude is reached.

W. ILS Guidance and Vertical Deviation - Failure Indication

PFD - Failure Indication ** ON A/C NOT FOR ALL

In case of failure a red flag is displayed replacing the V/DEV scale.

PFD - Failure Indication ** ON A/C NOT FOR ALL

In case of failure a red V/DEV flag is displayed replacing the V/DEV scale. This flag flashes during 9s then is steady.

X. ILS Guidance and Lateral Deviation - Failure Indication

PFD - Failure Indication ** ON A/C NOT FOR ALL

In case of failure, a red L/DEV flag is displayed replacing the L/DEV scale. This flag flashes for 9s then is steady.

Y. ILS Guidance and Lateral and Vertical Deviations - Parameter Definition

PFD - ILS Guidance and V/DEV Parameters ** ON A/C NOT FOR ALL

LIST OF PARAMETERS

ITEM PARAMETER EQUIPMENT LABEL COLOUR

1 GLIDE DEVIATION ILS 174 MAGENTA

2 MARKER VOR 222 OM CYAN

MM AMBER

AWY WHITE

3 LOCALIZER DEVIATION ILS 173 MAGENTA

4 ILS COURSE ILS 105 MAGENTA

5 VERTICAL DEVIATION FMGC 124 MAGENTA

6 DME DISTANCE FMGC 203 MAGENTA

7 ILS FREQUENCY ILS 033 MAGENTA

8 ILS IDENT ILS 263 MAGENTA

PFD - ILS Guidance and V/DEV Parameters ** ON A/C NOT FOR ALL

LIST OF PARAMETERS

ITEM PARAMETER EQUIPMENT LABEL COLOUR

1 GLIDE DEVIATION ILS 174 MAGENTA

2 MARKER VOR 222 OM CYAN

MM AMBER

AWY WHITE

3 LOCALIZER DEVIATION ILS 173 MAGENTA

4 ILS COURSE ILS 105 MAGENTA

5 VERTICAL DEVIATION FMGC 124 GREEN

6 DME DISTANCE FMGC 203 MAGENTA

7 ILS FREQUENCY ILS 033 MAGENTA

8 ILS IDENT ILS 263 MAGENTA

9 LATERAL DEVIATION FMGC 116 GREEN

Z. ILS Guidance and Vertical Deviation - Condition of Display
The table below gives the conditions of display of the ILS guidance information:

-------------------------------------------------------------------------------

! PARAMETERS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! Mach number ! - Green if mach number valid and not in approach phase.!

!--------------------!--------------------------------------------------------!

! ILS frequency ! - Magenta if ILS P/B switch pressed and LOC and G/S !

! ! valid. !

!--------------------!--------------------------------------------------------!

! ILS ident ! - Magenta; same conditions as for ILS frequency, plus !

! ! ILS ident valid. !

!--------------------!--------------------------------------------------------!

! ILS-DME distance ! - Magenta if ILS P/B switch pressed and ILS-DME !

! ! distance valid. !

The table below gives the conditions of display of the approach trajectory deviation information:

-------------------------------------------------------------------------------

! PARAMETERS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! Glide slope ! - Yellow if ILS P/B switch pressed and ILS frequency !

! reference ! valid. !

!--------------------!--------------------------------------------------------!

! Glide slope scale ! - White if ILS P/B switch pressed and ILS frequency !

! ! valid, flashing when glide slope deviation is !

! ! excessive. !

!--------------------!--------------------------------------------------------!

! Glide slope index ! - Magenta if ILS P/B switch pressed and ILS frequency !

! ! valid, flashing when glide slope deviation is !

! ! excessive. !

!--------------------!--------------------------------------------------------!

! Localizer reference! - Yellow if ILS P/B switch pressed and ILS frequency !

! ! valid. !

!--------------------!--------------------------------------------------------!

! Localizer scale ! - White if ILS P/B switch pressed and ILS frequency !

! ! valid, flashing when localizer deviation is excessive!

!--------------------!--------------------------------------------------------!

! Localizer index ! - Magenta if ILS P/B switch pressed and ILS frequency !

! ! valid, flashing when localizer deviation is excessive!

The table below gives the conditions of display of the approach trajectory deviation information:

-------------------------------------------------------------------------------

! PARAMETERS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! Glide slope ! - Yellow if LS P/B switch pressed and ILS frequency !

! reference ! valid. !

!--------------------!--------------------------------------------------------!

! Glide slope scale ! - White if LS P/B switch pressed, glide slope vallid !

! ! or NCD and back course not selected. !

!--------------------!--------------------------------------------------------!

! Glide slope index ! - Magenta if LS P/B switch pressed and glide deviation !

! ! valid. It flashes when glide slope deviation is !

! ! excessive. It goes out view if glide is out of range !

!--------------------!--------------------------------------------------------!

! Localizer reference! - Yellow if LS P/B switch pressed, LOC valid or NCD. !

! ! It flashes when the glide slope deviation is !

! ! excessive. !

!--------------------!--------------------------------------------------------!

! Localizer scale ! - White if LS P/B switch pressed and ILS frequency !

! ! valid, flashing when localizer deviation is excessive!

!--------------------!--------------------------------------------------------!

! Localizer index ! - Magenta if LS P/B switch pressed and LOC deviation !

! ! valid, flashing when localizer deviation is excessive!

! ! It goes out of view if LOC is out of range. !

The table below gives the conditions of display of the approach trajectory deviation flags:

-------------------------------------------------------------------------------

! FLAGS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! G/S ! - Red flag replacing V/DEV scale if ILS P/B switch !

! ! pressed and G/S deviation signal invalid. !

!--------------------!--------------------------------------------------------!

! LOC ! - Red flag replacing LOC scale if ILS P/B switch !

! ! pressed and LOC deviation signal invalid. !

!--------------------!--------------------------------------------------------!

! V/DEV ! - Red flag replacing V/DEV scale if ILS P/B switch not !

! ! pressed and vertical deviation signal not valid. !

!--------------------!--------------------------------------------------------!

! ILS ! - Amber message flashing at the intersection of GLIDE !

! ! and LOC scales when approach is selected and ILS P/B !

! ! switch is not pressed. !

The table below gives the conditions of display of the approach trajectory deviation flags:

-------------------------------------------------------------------------------

! FLAGS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! G/S ! - Red flag replacing the index and the scale when the !

! ! G/S beacon is faulty. It flashes during 9s. !

!--------------------!--------------------------------------------------------!

! LOC ! - Red flag replacing the index and the scale when the !

! ! LOC beacon is faulty. It flashes during 9s. !

!--------------------!--------------------------------------------------------!

! V/DEV ! - Red flag flashing with the V/DEV scale !

!--------------------!--------------------------------------------------------!

! ILS or LS (if GLS ! - Amber message flashing at the intersection of GLIDE !

! or MLS installed) ! and LOC scales when approach is selected and ILS P/B !

! ! switch is not pressed. !

The table below gives the conditions of display of the approach trajectory deviation flags:

-------------------------------------------------------------------------------

! FLAGS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! G/S ! - Red flag replacing the index and the scale when the !

! ! G/S beacon is faulty. It flashes for 9s. !

!--------------------!--------------------------------------------------------!

! LOC ! - Red flag replacing the index and the scale when the !

! ! LOC beacon is faulty. It flashes for 9s. !

!--------------------!--------------------------------------------------------!

! V/DEV ! - Red flag replacing the index and the scale when the !

! ! vertical deviation is faulty. It flashes for 9s. !

!--------------------!--------------------------------------------------------!

! L/DEV ! - Red flag replacing the index and the scale when the !

! ! lateral deviation is faulty. It flashes for 9s. !

!--------------------!--------------------------------------------------------!

! ILS or LS (if GLS ! - Amber message flashing at the intersection of GLIDE !

! or MLS installed) ! and LOC scales when approach is selected and ILS P/B !

! ! switch is not pressed. !

The table below gives the conditions of display of the approach trajectory-deviation flags:

FLAGS	DISPLAY
G/S	When the G/S beacon is unserviceable: - A red flag comes into view and flashes during nine seconds. - The index and the scale go out of view.
LOC	When the LOC beacon is unserviceable: - A red flag comes into view and flashes during nine seconds. - The index and the scale go out of view.
V/DEV	When the vertical deviation is unserviceable: - A red flag comes into view and flashes during nine seconds. - The index and the scale go out of view.
L/DEV	When the lateral deviation is unserviceable: - A red flag comes into view and flashes during nine seconds. - The index and the scale go out of view.
ILS or LS (if GLS, MLS or SLS is installed	When the approach mode is selected and the ILS pushbutton switch is released, an amber message flashes at the intersection of the G/S and LOC scales.

-------------------------------------------------------------------------------

! FLAGS ! DISPLAY !

!--------------------!--------------------------------------------------------!

! B/C ! - Magenta flag displayed above the LOC scale and on !

! ! the left in ROSE ILS mode. The G/S scale disappears !

! ! when the BACK BEAM/BACK COURSE is selected. !

PFD - Back Course Display and Non Precision Approach Display ** ON A/C NOT FOR ALL

PFD - Back Course title on ILS scale ** ON A/C NOT FOR ALL

AA. Simplified symbols

PFD - Simplified symbology ** ON A/C NOT FOR ALL

With this FMA option, some symbols of the PFD image are modified to reduce tracing time and thus enable a correct FMA display.
When the programming pin MP-6C of the DMC is activated:

the double graduations on the roll scale are replaced by single dashes
the white mark for 45 deg. value on the roll scale is reduced by half of his lenght
the mach number display has only two digits instead of three.

** ON A/C NOT FOR ALL

4. EIS Acquisition and Wiring

EIS Acquisitions ** ON A/C NOT FOR ALL

A. FMGC

EIS Acquisitions : FMGC

(1) FMGC - EIS (Flight Management part)
The DMC uses a few data from the FMGC - EIS bus for display on the PFD

FMGCs EIS - DMCs Wiring Interface ** ON A/C NOT FOR ALL

For a complete description of the FMGC - EIS bus switching refer 31-65-00

(2) FMGC - A (guidance part)
Each DMC receives and processes both FMGC 1 and 2 'A' buses, and uses them (either 1 or 2) independently for the display of the flight director orders and the flight mode annunciations, according to the engagement status of the FDs and the APs.

(a) Display of the FD or FPD orders
The DMCs working on side 1 use the FMGC 1-A bus for the display of the FD orders.
If FD 1 fails, or if the FMGC 1-A bus is no longer valid, there is an automatic switching to the FD 2 and the DMC use the FMGC 2-A bus for the display of the FD orders.

NOTE: FD orders means : FD bars (pitch, roll, yaw) or FPD orders related to the Flight Path Vector in TRK/FPA mode.

(b) Display of the Flight Mode Announcements
Regarding the FMA, which displays the armed and active modes for the FD, the AP and the A/THR, the DMCs working on side 1 use:

FMGC 1-A bus if no AP is engaged or if AP1 is engaged alone or if the 2 APs are engaged (DUAL).
FMGC 2-A bus if AP2 is engaged.

If the FMGC 1-A bus is no longer valid, the DMCs read the AP/FD engagement status from the FWCs:

If there is no AP engaged, the FMA displays the flight mode annunciations from the FMGC 2-A bus (the CAPT PFD displays the FD 2 orders whatsoever).
If the AP 1 is engaged (in this case, the non validity of the FMGC 1-A bus is due most likely to a disconnection of this bus from the DMC). The FMA is blanked.

The same applies to the DMC working on side 2, replacing in the text FMGC 1 with 2 and vice versa.

The table below summarizes the logic of the selection of FMGC 1 and 2 'A' buses.

---------------------------------------------------------------------------

! FMGC 1-A ! FMGC 2-A !CAPT FMGC 1-A or FMGC 2-A!F/O FMGC 1-A or FMGC 2-A !

! valid ! valid !for FD! for FMA !for FD! for FMA !

! ! ! !no AP!AP1!AP2!DUAL! !no AP!AP1!AP2!DUAL!

!----------!----------!------------!---!---!----!------------!---!---!----!

! N ! N ! Permanent checking through of the FMGC 1 and 2 !

! ! ! 'A' buses until finding a valid one. !

O ! Y ! N ! 1 ! 1 ! 1 ! / ! / ! 1 ! 1 ! 1 ! / ! / !

! ! ! ! ! ! ! ! ! ! ! ! !

* ! Y ! N ! 1 ! 1 ! 1 !(1)! 1 ! 1 ! 1 ! 1 !(1)!(1) !

! ! ! ! ! ! ! ! ! ! ! ! !

O ! N ! Y ! 2 ! 2 ! / ! 2 ! / ! 2 ! 2 ! / ! 2 ! / !

! ! ! ! ! ! ! ! ! ! ! ! !

* ! N ! Y ! 2 ! 2 !(2)! 2 !(2) ! 2 ! (2) ! 2 ! 2 ! 2 !

! ! ! ! ! ! ! ! ! ! ! ! !

! Y ! Y ! 1 ! 1 ! 1 ! 2 ! 1 ! 2 ! 2 ! 1 ! 2 ! 2 !

NOTE: O: Cases where an FMGCX-A bus is lost, but the APX cannot be engaged (/).
*: Cases where an FMGCX-A bus is lost, but the APX can still be engaged.
The symbol (1) means: The FMGC1 'A' bus is valid, and is used by the DMC for the FD/FPD orders and the FMA. However, since the AP2 is engaged, there is most likely a wiring problem about the lost of the FMGC2 'A' bus. Therefore, the FMA, which always indicate the mode of operation of the working AP, is blanked.
The symbol (2) means: The FMGC 1-A bus is valid, and is used by the DMC for the FD/FPD orders and the FMA. However, since the AP1 is engaged, there is most likely a wiring problem about the lost of the FMGC1 'A' bus. Therefore, the FMA, which always indicate the mode of operation of the working AP, is blanked.

B. ADIRU
IR and ADR bus selections are completely independent.

(1) ADIRU : IR

EIS Acquisitions : ADIRU (IR)

In normal configuration, the parameters displayed on the PFDs come from the ADIRU1 for the CAPT PFD and from the ADIRU2 for the F/O PFD.
When a failure is detected on either CAPT PFD or F/O PFD, the switching on the ADIRU3 has to be done manually through the ATT/HDG selector switch of the SWITCHING panel.

NOTE: The DMC uses both ADIRU1 (or 2) and ADIRU3 for the lateral animation of the speed vector in order to decrease the error.

(2) ADIRU : ADR

EIS Acquisitions : ADIRU (ADR)

The ADR bus selection follows exactly the same rules (using the AIR DATA selector switch of the SWITCHING panel for the reconfiguration on the ADIRU3).

C. FAC Bus Selection

EIS Acquisitions : FAC

Each DMC receives the FAC 1 and 2 buses. The FAC1 or FAC2 bus selection inside each DMC is done automatically according to the logic given in the table below:

-------------------------------------------------------------------------------

! FAC 1 VALID ! FAC 2 VALID ! DMC SIDE 1 ! DMC SIDE 2 !

!-------------!-------------!------------------------!------------------------!

! Y ! Y ! FAC 1 ! FAC 2 !

!-----------------------------------------------------------------------------!

! Y ! N ! FAC 1 ! FAC 1 !

!-------------!-------------!------------------------!------------------------!

! N ! Y ! FAC 2 ! FAC 2 !

!-------------!-------------!------------------------!------------------------!

! N ! N ! FAC 1 <----> FAC 2 ! FAC 2 <----> FAC 1 !

! ! !permanent switching !permanent switching !

! ! !until finding one valid !until finding one valid !

! ! !FAC. !FAC. !

D. ILS Selection

EIS Acquisitions : ILS

The CAPT PFD displays the ILS1 data only when the F/O PFD displays the ILS2 data only.

E. Radio Altimeter

EIS Acquisitions : RA (Radio Altimeter)

Each DMC receives and processes radio altitude data from both radio altimeters.
The DMCs on side 1 select RA1 data as long as the RA1 bus is valid.
If it is no longer valid, the DMC automatically uses the RA2 bus.
It reverts to the RA1 as soon as it becomes valid again.
If both RA1 and RA2 buses are invalid, the DMCs check through the 2 buses at each cycle until finding a valid one.
A red RA flag is then displayed on the CAPT PFD.
The same applies regarding the F/O PFD (replacing RA1 by RA2).

F. FCU

EIS Acquisitions : FCU

The FCU is a dual unit, fully redundant with 2 processors 1 and 2.
Normally, the processor 1 operates and the processor 2 is a hot spare.
In case of failure of the processor 1, the processor 2 takes over and all the DMCs receive the same data as those sent by the processor 1.
This loss of redundancy is annunciated on the ECAM DUs (STATUS).
Briefly, the FCU bus X-A (1A and 2A) conveys EIS CP 1 (CAPT) selections, plus some AFS selections.
The FCU bus X-B (1B and 2B) conveys the EIS CP 2 (F/O) selections, the remaining AFS selections, and both the CAPT and F/O baro reference settings.
The DMCs on side 1 use the parameters from the buses 1A and 1B. The DMCs on side 2 use the parameters from the buses 2A and 2B. Each parameter to be used is checked separately for its validity. If one parameter is not valid, it is rejected but the other parameters from the same bus are still used as long as they are valid.

G. VOR

EIS Acquisitions : VOR

The PFD uses the Marker information from the VOR bus. The CAPT PFD can only display marker indications from the VOR 1 and the F/O PFD those from VOR 2.

H. DME

EIS Acquisitions : DME

The PFD displays the DME distance when the DME station is co-located to an ILS station. The PFD displays DME distance which is delivered on the FMGC-EIS bus.
The CAPT PFD can only display DME1 data, when the F/O PFD displays DME2 data.

I. TCAS

Interface with TCAS

The PFD display the forbidden vertical speeds on the vertical speed scale.
The DMC1 and DMC3 receive the channel 1 parameters (CAPT PFD).
The DMC2 receives the channel 2 parameters (F/O PFD). In case of channel invalidity, the related PFD displays the red TCAS flag.

[Rev.10 from 2021] 2026.04.01 00:38:35 UTC