PFD+&+ND+A320+A330

PFD & ND A320/A330

BADGER’S NOTES

Ig. P. Djatmiko

Note: 1. Reference: FCOM, DSC-22_30-100 2. Terdapat perbedaan dikarenakan MSN yg berbeda.

1st LINE 2

nd

LINE

Auto Thrust Operation

Vertical Mode

Lateral Mode

MAN FLEX 54

SRS

RWY

Approach Capabilities

1FD2

3th LINE 1st LINE 2

nd

LINE

3

th

LINE

A/THR SPEED

FIRST LINE MAN TOGA MAN FLEX 54 MAN MCT MAN DTO MAN THR THR MCT THR CLB THR DCLB 1(2) THR IDLE THR LVR THR DES SPEED / MACH A. FLOOR TOGA LK SECOND LINE LVR CLB (flashing) LVR MCT (flashing)

THIRD LINE LVR ASYM THR LK (flashing)

ALT* HDG G/S LOC SPEED SEL: 180

CAT 3 DUAL DH 100

AP1+2 1FD2 A/THR FIRST LINE AP1 + 2 AP1 AP2

FIRST LINE SRS CLB OP CLB ALT* ALT CST (*) ALT CRZ* ALT ALT CST ALT CRZ DES OP DES EXP CLB EXP DES G/S (*) V/S ± XXXX FPA ± X.X TCAS

FIRST LINE RWY RWY TRK HDG or TRK NAV LOC* LOC APP NAV GA TRK

FIRST LINE CAT 1

SECOND LINE CLB OP CLB ALT ALT ALT CRZ DES G/S FINAL

SECOND LINE LOC APP NAV NAV

SECOND LINE SINGLE DUAL

SECOND LINE X FD Y

THIRD LINE SPEED SEL:XXX MACH SEL:.XX TCAS

THIRD LINE

THIRD LINE MDA/MDH XXXX DH XXX / NO DH BARO XXX RADIO XXX / NO DH

THIRD LINE A/THR A/THR

AP/FD COMMON MODES (Combined Vert / Lat Modes) ROLL OUT FLARE LAND FINAL APP SPECIAL MESSAGES (at Third Line) USE MAN PITCH TRIM MAN PITCH TRIM ONLY DECELERATE MORE DRAG CHECK APPR SELECTION SET GREEN DOT SPEED SET HOLD SPEED MACH SEL: .XX / SPEED SEL: XXX

04 May 2004

Auto flight Status

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CAT 2 CAT 3

BADGER’S NOTES

PFD & ND A320/A330

Ig. P. Djatmiko

(Column 1)

Auto Thrust Operation FIRST LINE DISPLAY MAN TOGA MAN FLEX 54 MAN MCT MAN DTO MAN THR THR MCT THR CLB THR DCLB 1(2) THR IDLE THR LVR THR DES SPEED or MACH

A. FLOOR TOGA LK

MEANING A/THR is armed, at least one thrust lever is in TOGA detent. A/THR is armed, at least one thrust lever is in MCT/FLX detent, with FLX TO temp set at 50 °C. The other thrust lever is at, or below the MCT/FLX detent. 50 is displayed in blue. A/THR is armed, at least one thrust lever is in MCT detent. The other is at, or below this detent. A/THR is armed, at least one thrust lever is in MCT/FLX detent, with an entered derated level. The other thrust lever is at, or below the MCT/FLX detent. A/THR is armed. This indication is not displayed during TO or GA phases. The most advanced thrust lever is above the CL detent, while the other is in CL detent, or both thrust levers are above CL detent. A/THR is active in thrust mode and the most advanced thrust lever is in the MCT detent (engine-out). A/THR is active in thrust mode and the most advanced thrust lever is in the CL detent. A/THR is active in thrust mode. The most advanced thrust lever is in the CL detent, and the flight crew has selected a derated climb. A/THR is active in thrust mode and commands idle thrust. A/THR is active in thrust mode with either both thrust levers out of CL, or MCT detent, or at least one thrust lever in CL detent and the other beyond CL detent. A/THR is active in thrust mode and commands a reduced thrust, while DES mode is engaged. The auto thrust is armed; with the most forward thrust lever above the IDLE detent and up to and including the CLB detent. (MCT single engine) Thrust will vary as required to attempt to maintain the vertical path commanded. Airspeed is ignored if the vertical path cannot be maintained. SPEED is annunciated when IAS is being referenced MACH is annunciated when referencing MACH While in Alpha Floor conditions, the A/THR is engaged and TOGA thrust is commanded regardless of thrust lever position. TOGA Lock is engaged following an Alpha Floor engagement. A/THR must be disconnected and rearmed to regain A/THR control

SECOND LINE LVR CLB (flashing) LVR MCT (flashing)

Request to set the thrust levers in CL detent. Request to set the thrust levers in MCT detent.

THIRD LINE LVR ASYM THR LK (flashing)

04 May 2004

One thrust lever is set out of the CL (or MCT) detent with A/THR active (2 engines only). The thrust is frozen due to a non-standard A/THR disconnection (FCU disconnection or failure).

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BADGER’S NOTES

PFD & ND A320/A330

Ig. P. Djatmiko

(Column 2)

Vertical Modes FIRST LINE DISPLAY SRS

MEANING

REMARK

Mode used at takeoff, or go-around to maintain SRS speed (V2, V2+10, VAPP...).

Triggered by the thrust levers at FLX or TOGA position. Automatically disengages at ACC ALT, or when another VERT mode is engaged.

Speed Reference system is engaged. A/C will fly the vertical path appropriate for the phase of flight.  Normal Engines T/O = V2 + 10  Engine Failure (T/O) = V2 If failure occurs above V2, current speed up to V2 + 15  GO Around = VAPP or current speed if higher  Windshear = SRS will allow the speed to decrease to maintain 120 fpm climb.

CLB

DES

SRS is only available when at least one FD is on and Flap handle greater than FLAPS 1. Mode used to climb towards FCU selected altitude along VERT F-PLN The speed target may either be taking into account ALT CSTR. selected or managed. If Available, only if NAV mode engaged. managed, SPD CSTR, SPD LIM, The A/THR is in THRUST mode (CLB). and HOLD SPD are taken into account. Descent mode is engaged. The FMGES target altitude is lower than the ALT mode is always armed; actual altitude. ALT CSTR are taken into account. displayed in magenta, if the Vertical Navigation is engaged, and all constraints will be met. (Unless next level off is predicted at an the FCU altitude is above the constraint alt. NAV mode must be ALT CSTR; and in blue, if the engaged. If NAV mode is lost or changed DES will revert to OP DES. next level off is predicted at the If DES is pushed prior to the TOD the a/c will enter a 900-1000’ power FCU selected altitude. on descent. Once the descent profile is intercepted the a/c will attempt to fly the profile using an ECON speed range of ± 20 knots. VNAV calculates an IDLE descent from TOD to the first constraint, then a geometric (straight line) descent for the next segment.

OP CLB OP DES

ALT CST (*)

ALT CST ALT*

ALT ALT CRZ* ALT CRZ

EXP CLB EXP DES G/S (*)

V/S ± XXXX

FPA ± X.X

TCAS

04 May 2004

Note: If you must level off at an intermediate altitude, Selecting the PROG page and entering your altitude will force the VNAV to recalculate the descent. This will also allow you to change the speeds on the descent page once again if ATC issues a speed restriction Mode used to climb/descend directly to the FCU selected altitude. These modes disregard all ALT CSTR. The A/THR is in THRUST mode (CLB/IDLE). The aircraft will attempt to maintain the profile speed by varying pitch. ALT CAPTURE at the altitude constraint (vertical profile) is engaged. Indicates a CLB or DES altitude constraint has been engaged. (* If captured) and the FCU altitude is above (CLB) or below (DES) the constraint altitude. An altitude constraint is held (vertical profile). The FCU altitude has been captured. If a new altitude is selected prior to ALT engagement the FCU will revert to V/ S until a new vertical made is selected. On older aircraft if the FCU altitude is the cruise alt. selected in the MCDU, ALT* would be replaced by dashes in the vertical mode FMA window. An FCU altitude, which is not selected as the cruise altitude, has been engaged. The aircraft will maintain this altitude exactly. “Hard Altitude “ ALT CAPTURE at the CRZ FL is engaged. The FCU altitude, which is the preprogrammed cruise altitude or an altitude higher than the preprogrammed cruise altitude, has been engaged. Open Descent mode is engaged. The FCU selected altitude is lower than the actual altitude. A climb at Green Dot will be flown. Disengaged by selecting another vertical mode. An idle descent at .80M/340 Kts. Disengaged by selecting another vertical mode. Note: The aircraft will not slow to 250 knots @ 10000 feet. The ILS glide slope has been engaged. G/S* If captured, G/S in blue on line to for Armed. Once captured the aircraft will ignore all FCU altitudes to maintain GS. Vertical Speed mode is engaged to acquire and hold the V/S selected on the FCU. Target is displayed in blue. If the aircraft reaches VLS or VMAX and cannot maintain the target, the indication is boxed amber and flashes, and the target pulses.. Flight Path Angle mode is engaged to acquire and hold the FPA selected on the FCU. Target is displayed in blue. If the aircraft reaches VLS or VMAX and cannot maintain the target, the indication is boxed amber and flashes, and the target pulses. (latest MSNs) TCAS mode is engaged. The Auto Flight System (AFS) guidance provides a vertical guidance in accordance with the TCAS Resolution Advisory order.

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The speed target may either be selected or managed. ALT mode is systematically armed and blue. Altitude target is blue on the PFD. CLB/DES mode are systematically armed (blue).

A/THR SOFT mode engages when FCU selected altitude = CRZ FL. A/THR SOFT mode is part of the managed guidance.

(Not on A330)

Automatically engages when a RA is triggered.

PFD & ND A320/A330

BADGER’S NOTES

Ig. P. Djatmiko

SECOND LINE CLB OP CLB ALT ALT ALT CRZ DES G/S FINAL

Climb mode is armed before the climb phase. Open Climb mode is armed. Altitude mode is armed when the target altitude is the FCU selected altitude Altitude mode is armed when the target altitude is an altitude constraint. Altitude mode is armed. Target altitude is the CRZ FL. Descent mode is armed before the descent phase. Glide Slope mode is armed. Final descent mode is armed. The vertical deviation path of an Approach Nav has been engaged. Using IR data the FMGC will build its own vertical path. The Path is built from a point 50’ over the approach end of the runway back to the final approach altitude. FINAL engages automatically when the aircraft intercepts this vertical path. The vertical path will clear all crossing constraints associated with the approach in a constant descent without leveling off.

Note: Two modes may be armed at the same time : ALT G/S, ALT FINAL, DES G/S, DES FINAL.

THIRD LINE SPEED SEL:XXX MACH SEL:.XX TCAS

Indicates a preset speed associated with the cruise, climb or descent phase. Indicates a preset Mach associated with the cruise, climb or descent phase. (latest MSNs) TCAS mode is armed.

(Column 3)

Lateral Modes FIRST LINE DISPLAY RWY

MEANING Mode used at takeoff to guide the aircraft along the runway center line using LOC.

REMARK Triggered by the thrust levers at FLX or TOGA position.

RWY mode is engaged.

RWY TRK

GA TRK HDG or TRK

Provides a steering command utilizing the localizer for the departure runway from T/O roll through 30’ AGL. A LOC must be associated with the runway in use. If the LOC signal is lost during the T/O roll a memorized track will be flown. RWY mode is engaged once airborne at, or above 30 ft. Provides a lateral path along the extended runway centerline for all runways from 30’ AGL, Unless NAV mode is engaged. Provides a lateral path based on the actual aircraft track at the time a GA was initiated. HEADING or TRACK mode is engaged. The heading or track selected in the FCU window will be flown. If the heading knob is pulled before it is turned, the aircraft will turn in the direction the knob is rotated. If the desired heading is set prior to pulling the knob the aircraft will turn in the direction to make the shortest turn.

NAV

LOC* LOC APP NAV

NAV mode is engaged to guide the aircraft along the FM lateral F-PLN.

LOC capture mode is engaged. LOC track mode is engaged. NAV mode is engaged during a non-ILS approach. The APPR p/b has been pushed and the FMGC is flying the selected approach.

Triggered by the thrust levers at TOGA with Slats/Flaps in at least CONF 1. Note (A330 only): HDG/TRK is called "basic mode" because it is a back up mode for certain situations : ‐ F-PLN discontinuity entry ‐ AP engagement with no FD ‐ Loss of F-PLN ‐ MCDU NAV BACK UP. Automatically armed at takeoff unless HDG/TRK is preset. In that case RWY TRK engages after takeoff. Selected by pressing APPR pb on the FCU; the mode that engages depends upon the selected approach in the F-PLN.

SECOND LINE LOC APP NAV NAV

LOC mode is armed. NAV mode is armed for a non-ILS approach. NAV mode is armed. NAV in blue on line 2 indicates that NAV is armed. A cross track error should be present to indicate your displacement from the desired course. If not then LNAV will not intercept the course you have selected.

04 May 2004

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PFD & ND A320/A330

BADGER’S NOTES

Ig. P. Djatmiko

(COLUMNS 2 AND 3)

AP/FD Common Modes DISPLAY ROLL OUT

(Combined Vertical / Lateral Modes) MEANING

ROLL OUT mode is engaged.

FLARE

Lateral guidance is provided for tracking the LOC along the runway. FLARE mode is engaged.

LAND

At approximately 40’ RA LAND is replaced by FLARE. (30’ for an Autoland) LAND mode is engaged below 400 ft RA.

FINAL APP

At 400’ AGL the dividing line on the FMA column 2 & 3 disappears along with G/S and LOC and a single mode common to both vertical and lateral guidance is engaged. LAND appears first to indicate that approach guidance can no longer be disengaged on the FCU. From this point on the crew must select TOGA to activate the GA mode and disengage the APPR mode. APP NAV and FINAL modes are engaged during a non-ILS approach.

REMARK FD roll out symbol is displayed on PFD at touch down. Automatically engages when a RA is triggered. Engaged only if LOC mode and G/S mode are already engaged.

Is the combined mode for a non ILS approach, FINAL is engaged for vertical NAV and APP NAV is engaged for vertical NAV, the APP p/b has been pushed.

(Column 4)

Approach Capability FIRST LINE CAT 1 CAT 2

CAT 1 capability available. Autoland not available CAT 2 capability available.

CAT 3

CAT I Autoland approaches may be flown to CAT II/III runways CAT 3 capability available.

SECOND LINE SINGLE

DUAL

CAT 3 capability available, with FAIL PASSIVE condition. CAT II Autoland approaches may be flown to CAT II/III runways CAT 3 single will be annunciated until the second AP is coupled. CAT 3 capability available, with FAIL OPERATIONAL condition. CAT III Autoland approaches may be flown to CAT III runways

THIRD LINE MDA/MDH XXXX

Minimum Descent Altitude or Minimum Descent Height as inserted by the flight crew on the MCDU PERF APPR page.

DH XXX / NO DH

Decision height for ILS approaches or MAP altitude for Non-precision approaches has been entered in the PERF page of the MCDU. At this altitude the altimeter will change to amber. Decision Height as inserted by the flight crew on the MCDU PERF APPR page. NO DH: when NO is inserted on the MCDU PERF APPR page.

BARO XXX RADIO XXX / NO DH

04 May 2004

Radio Altimeter for CAT II and CAT III approach has been entered in the PERF page of the MCDU. Minimum Descent Altitude or Minimum Descent Height as inserted by the flight crew on the MCDU PERF APPR page. Decision Height as inserted by the flight crew on the MCDU PERF APPR page. NO DH: when NO is inserted on the MCDU PERF APPR page.

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PFD & ND A320/A330

BADGER’S NOTES

(COLUMN 5)

AP/FD - A/THR Engagement Status FIRST LINE AP1 + 2 AP1 AP2

Autopilot 1 and 2 are engaged. Autopilot 1 is engaged. Autopilot 2 is engaged.

SECOND LINE X FD Y

X and Y give the FD engagement status on PFD1 and PFD2. X and Y can be 1, 2, or –: ‐ –: No FD is engaged on the corresponding PFD ‐ 1: FD 1 is engaged on the corresponding PFD ‐ 2: FD 2 is engaged on the corresponding PFD. The normal status (FD 1 and 2 are engaged) is 1 FD 2.

THIRD LINE A/THR A/THR

A/THR is active. A/THR is armed and not active.

(COLUMNS 2 AND 3)

Special Messages Three types of messages are displayed on the third line: ‐ First priority is given to F/CTL messages ‐ Then vertical FM messages ‐ Then EFIS reconfiguration messages. MAN PITCH TRIM ONLY USE MAN PITCH TRIM CHECK APPR SELECTION

04 May 2004

Displayed in case of loss of L + R elevators. F/CTL are in direct law or in flare law with dual RA failure. F/CTL STAB CTL FAULT ECAM caution is trigerred The aircraft is in cruise at less than 100 nm from the top of descent or in descent or in approach and: ‐ A non-ILS approach has been selected ‐ An ILS frequency is tuned on the MCDU RAD NAV page.

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Ig. P. Djatmiko

BADGER’S NOTES

PFD & ND A320/A330

Speed Indications PFD

04 May 2004

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Ig. P. Djatmiko

BADGER’S NOTES

PFD & ND A320/A330

ND Symbols

04 May 2004

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Ig. P. Djatmiko