A320 Classic to Advanced Training CBT

A320 CLASSIC > FAMILIARIZATION BRIEFING > A320 ENHANCED

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This chapter presents new features for aircraft equipped with the enhanced program. Thus, this module is applicable to the A320 and to all retrofitted single aisle aircraft.

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On ENHANCED A/C, the Display Units (DU) are

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, p y ( )now full color Liquid Crystal Displays (LCD).

CLASSIC A/C ENHANCED A/C

On E/WD, given information remain unchanged, only the layout is modified.

Here you can see the CFMsee the CFM examples.

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CLASSIC A/C ENHANCED A/C

Here are the CFM ENGINE SD pages.

Note that a delta ISA is displayed in flight when standard baro reference isbaro reference is selected.

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CLASSIC A/C ENHANCED A/C

WHEEL page layout has been slightly modified.

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CLASSIC A/C ENHANCED A/C

Concerning the FUEL system, some elements have y ,been added:• total fuel used, total fuel flow indications, and• a new warning “F.Used/FOB disagree”.

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CLASSIC A/C ENHANCED A/C

On the NDs and PFDs some colors have been modified but the information is similar

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been modified but the information is similar.

CLASSIC A/C ENHANCED A/C

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On the NDs and PFDs some colors have been modified but the information is similar

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been modified but the information is similar.

CLASSIC A/C ENHANCED A/C

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The vertical speed display provides digital indications.

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CLASSIC A/C ENHANCED A/C

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The LCDs provide maximum brightness in the case of EGPWS, TCAS and predictive windshear alert.

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CLASSIC A/C ENHANCED A/C

HORIZON AIRSPEEDINDICATOR

ISIS

ALTIMETER In ENHANCED A/C, the standby instruments (horizon, airspeed and altimeter) are replaced by one Integrated Standby Instrument System called ISIS.

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It is located in the center of the instrument panel.

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AI

A

BUGS

IR

SP

AIRCRAFT ATTITUDE

GLID

LTITUE

ED

MACH

E

LOC

UDE

REFERENCEBAROMETRIC

PRESSUREPRESSURE

The ISIS system displays the following information:

• air speed,• MACH,• aircraft attitude,aircraft attitude,• LS function,• altitude,• barometric pressure,• and bugs.

Let’s summarize the information contained in it

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Let s summarize the information contained in it.

AIRSPEED

AIR SPEED SCALE

MACH

The airspeed scale moves in front of a yellowThe airspeed scale moves in front of a yellow triangle indicating the airspeed.

The MACH number is displayed in green when greater than 0.5.

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ROLL INDEX

ATTITUDE

ROLL SCALE

ROLL INDEX

LATERAL

FIXED AIRCRAFTSYMBOL

LATERALACCELERATION

PITCH SCALE

ATTITUDE RESET

On ISIS, the pitch attitude scale is identical to the one displayed on PFD.

The ATT RST pb is used for resetting the attitude indication by pressing it for at least 2 seconds. During this period “ATT 10s” is displayed on the screen.

Note: the flight must be stabilized (without pitch and roll angles d ith t bili d d)

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and with stabilized speed).

ROLL INDEX

ATTITUDE

ROLL SCALE

ROLL INDEX

LATERAL

FIXED AIRCRAFTSYMBOL

LATERALACCELERATION

PITCH SCALE

ATTITUDE RESET

On ISIS, the pitch attitude scale is identical to the one displayed on PFD.

The ATT RST pb is used for resetting the attitude indication by pressing it for at least 2 seconds. During this period “ATT 10s” is displayed on the screen.

Note: the flight must be stabilized (without pitch and roll angles d ith t bili d d)

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and with stabilized speed).

ATTITUDE

ATTITUDE RESET

On ISIS, the pitch attitude scale is identical to the one displayed on PFD.

The ATT RST pb is used for resetting the attitude indication by pressing it for at least 2 seconds. During this period “ATT 10s” is displayed on the screen.

Note: the flight must be stabilized (without pitch and roll angles d ith t bili d d)

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and with stabilized speed).

ALTITUDE

METRIC ALTITUDEMETRIC ALTITUDE INDICATION

ALTITUDE INDICATION

SELECTED

BAROMETRICSELECTION KNOB

SELECTEDBAROMETRIC REFERENCE

Altit d i f ti i id ti l t thAltitude information is identical to the one displayed on the PFD.

Note: the barometric pressure is simultaneously displayed in hectoPascal (hPa) and in inches of Hg.

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LS SELECTION pb

LANDING SYSTEM FUNCTION

GLIDE SLOPESCALE AND INDEX

LOCALIZER SCALE AND INDEXSCALEAND INDEX

The deviation scales appear when the LS pb is pp ppressed.

The indexes appear when the Glide Slope and localizer signals are valid with deviation scales displayed.

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BUGS

CAUTION

The Airbus SOP do not recommend to set bugs during a flight.

However the use of bugs may be recommended by Airlines Standard Operation Procedures.

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BUGS pb sw

BUGS

The BUGS pb sw is used to display or inhibit the bugs function.

The BUGS page has two columns positioned vertically:

• the speed bug column where four speed values (in knots) can be selected by the crew,

• and the altitude bug column where two altitude values (X 100) can be selected by the crew

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values (X 100) can be selected by the crew.

BUGS pb sw

BUGS

BOX ACTIVATION PUSHBUTTONS

BUGS VALUESELECTION KNOB

The BUGS value selection knob allows the bug to be set in the active box by rotating the BARO knob.

Movement from one box to another is made by the “+ or -” pushbuttons. The active box flashes.

Pressing the BARO setting knob once the bug value box is activated, will deselect the bug value. The OFF label comes on close to the activated box.

The entered values are memorized by the system when exiting the screen by pressing the BUGS pb sw or after 15 s

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exiting the screen by pressing the BUGS pb sw or after 15 s without any pilot action.

BUGS

Once a value is entered and activated, a cyanOnce a value is entered and activated, a cyan dash is displayed on the corresponding scale, representing the bug. Here, you can see two examples: a speed one and an altitude one.

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ISIS

COMPASS

To summarize ISIS is a PFD without FMA andTo summarize, ISIS is a PFD without FMA and heading.

Heading is, as before, given by the standby compass on the top of the windshield center post.

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CLASSIC A/C ENHANCED A/C

Concerning the EGPWS, the GPWS - GS pb switches of CLASSIC A/C have been modified on ENHANCED A/C to “PULL UP - GPWS”:• PULL UP comes on red when:

d 1 “E i R f D ” d b d i d- mode 1, “Excessive Rate of Descent”, second boundary is penetrated, or - mode 2, “Excessive Terrain Closure Rate”, is activated, or- any Terrain Awareness Display (TAD) or Terrain Clearance Floor (TCF) is activated.

• GPWS comes on amber when any other mode is activated.

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CLASSIC A/C ENHANCED A/C15‘‘ touch screen

The ENHANCED A/C cabin is equipped with a new Flight Attendant Panel (FAP) and a new In-Flight Entertainment (IFE) system. Data are contained in integrated memory cards.

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Module completed

SYSTEM INTRODUCTION

ENGINE WARNING DISPLAY

ECAM SD PAGE

ENGINE WARNING DISPLAY

EFIS PAGES PRESENTATION

ISIS PRESENTATION EXIT

EGPWS PB SW

GLOSSARY

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GLOSSARY

RETURN