117484282-A320-Classic-to-Advanced-Training-CBT.pdf

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 p y Units (DU) ( ) are now full color Liquid Crystal Displays (LCD).

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CLASSIC A/C

ENHANCED A/C

On E/WD, given information remain unchanged, only the layout is modified. Here you can see 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 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, y , some elements have 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. similar

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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. similar

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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

HORIZON

ENHANCED A/C

AIRSPEED INDICATOR

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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BUGS A I R S P E E D MACH

AIRCRAFT ATTITUDE

A L T I T U D E

G L I D E

LOC REFERENCE BAROMETRIC PRESSURE

The ISIS system displays the following information: • • • • • • •

air speed, MACH, aircraft attitude, LS function, altitude, barometric pressure, and bugs. Let’s Let s summarize the information contained in it it.

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AIRSPEED

AIR SPEED SCALE

MACH

The 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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ATTITUDE ROLL INDEX ROLL SCALE LATERAL ACCELERATION FIXED AIRCRAFT PITCH SCALE

SYMBOL

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 and d with ith stabilized t bili d speed). d)

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ATTITUDE ROLL INDEX ROLL SCALE LATERAL ACCELERATION FIXED AIRCRAFT PITCH SCALE

SYMBOL

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 and d with ith stabilized t bili d speed). d)

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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 and d with ith stabilized t bili d speed). d)

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ALTITUDE METRIC ALTITUDE INDICATION

ALTITUDE INDICATION SELECTED BAROMETRIC

BAROMETRIC

REFERENCE

SELECTION KNOB

Altit d information Altitude i f ti is i identical id ti l to t the th one displayed on the PFD. Note: the barometric pressure is simultaneously displayed in hectoPascal (hPa) and in inches of Hg.

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LANDING SYSTEM FUNCTION LS SELECTION pb

GLIDE SLOPE LOCALIZER

SCALE

SCALE

AND INDEX

AND INDEX

The deviation scales appear pp when the LS pb p is pressed. 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 BUGS pb sw

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 crew.

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BUGS BUGS pb sw

BOX ACTIVATION PUSHBUTTONS

BUGS VALUE SELECTION 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 without any pilot action.

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BUGS

Once 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, 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: - mode d 1, 1 “Excessive “E i Rate R off Descent”, D ” second d boundary b d is i penetrated, d 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/C 15‘‘ 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.

Module completed SINGLE AISLE CLASSIC TO ENHANCED

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SYSTEM INTRODUCTION ENGINE WARNING DISPLAY ECAM SD PAGE EFIS PAGES PRESENTATION

EXIT

ISIS PRESENTATION EGPWS PB SW

GLOSSARY RETURN SINGLE AISLE CLASSIC TO ENHANCED

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