Auszüge/Beispielseiten aus dem Trainingsmaterial der A320-Familie • ATA 22 Autoflight • ATA 79 Oil • ATA 71 Power Plant • ATA 34 Navigation • Cockpit Panel Descriptions • Airbus Abbreviation List Das Trainingsmaterial ist so aufbereitet, dass es auf unterschiedlichen Endgeräten dargestellt und verteilt werden kann. Extracts/sample pages - training material of the A320-family • ATA 22 Autoflight • ATA 79 Oil • ATA 71 Power Plant • ATA 34 Navigation • Cockpit Panel Descriptions • Airbus Abbreviation List The training material is optimized and available for different mobile end devices.

FO

RT

RA

ININ

GP

UR

PO

SE

SO

NLY

!

Page 402|--00|AFS Philosophy|L1

AUTO FLIGHTGENERAL

A318/A319/A320/A321

22--00

FRA US/T-5 PoL Dec 28, 2010

COMMAND

MONITOR

2

FLIGHTMANAGEMENT

FLIGHTGUIDANCE

FLIGHT CONTROL UNIT (FCU)

AUTOFLIGHT SYSTEM

ANALOGUE,DISCRETE& DIGITALA/C DATAINPUTS

(e.G. ADIRS)

MULTIPURPOSE CONTROL ANDDISPLAY UNIT (MCDU)

FADEC

FLIGHT CONTROLSYSTEM

FLIGHT AUGMENTATIONCOMPUTER (FAC)

COMMAND

MONITOR

1

2

FLIGHT MANAGEMENT &GUIDANCE COMPUTER (FMGC)

COMMAND

MONITOR

1

FLIGHTMANAGEMENT

FLIGHTGUIDANCE 1

2

SIDESTICK

F/O

CAPT

THRUST LEVERS

CAPT & F/O PFD/ND

DMC

FIDS

COMMAND

MONITOR

FIDSCFDIU

NOTACTIVE

Luft

hansa

Tech

nic

alT

rain

ing

Figure 2 Auto Flight System Design Philosophy

FO

RT

RA

ININ

GP

UR

PO

SE

SO

NLY

!

Page 215|--10|AP/FD|L2

AUTOFLIGHTAUTOPILOT/FLIGHT DIRECTOR (AP/FD)

A318/A319/A320/A321

22--10

FRA US/O-7 KnB Nov 07, 2012

10

12

34

56

78

9

TO FCU

MDCU 1,

MDCU 2

FCU

MDCU 2

MDCU 1

1 - ELEVATOR AILERON COMPUTER 12 - SPOILER AND ELEVATOR COMPUTER 13 - FLIGHT MANAGEMENT AND GUIDANCE COMPUTER 14 -- FLIGHT AUGMENTATION COMPUTER 15 -- FLIGHT AUGMENTATION COMPUTER 26 - FLIGHT MANAGEMENT AND GUIDANCE COMPUTER 27 - SPOILER AND ELEVATOR COMPUTER 28 - ELEVATOR AILERON COMPUTER 29 - SPOILER AND ELEVATOR COMPUTER 310 - BRAKE STEERING CONTROL UNIT

Lufthansa

Tech

nicalT

raining

Figure 1 AP/FD Layout & FLT CTRL Components

FO

RT

RA

ININ

GP

UR

PO

SE

SO

NLY

!

Page 202|79--00|Sys|5A|L2/B1/B2

OILGENERAL

A319/A320/A321CFM56--5A

79--00

FRA US/T-5 KoA Mar 4, 2011

LufthansaTechnicalTraining

Figure 1 Oil System General

FORTRAININGPURPOSESONLY!

Page 204|71--00|CTRLS|5A|L1/B1/B2

POWER PLANTGENERAL

A319/A320/A321CFM56--5A

71--00

FRA US/T-5 KoA Mar 4, 2011

FAULT

ON

FAULT

ON

DISCH DISCH

DISCH

DISCH DISCH

LufthansaTechnicalTraining

Figure 1 Engine Controls Overview

FORTRAININGPURPOSESONLY!

Page 1616|--48|Modes|L2

NAVIGATIONGROUND PROXIMITY WARNING SYSTEM

A318/A319/A320/A321

34--48

FRA US/O-7 KnB Nov 20, 2012

PULL UPPULL UP

LufthansaTechnicalTraining

MODETCF

Figure 8 Terrain Clearance Floor Mode

FO

R T

RA

ININ

G P

UR

PO

SE

S O

NLY

! �

Luft

hansa T

echnic

al T

rain

ing

Page 4 LufthansaTechnical Training

Cente

r P

edesta

l

00

INTRODUCTION

COCKPIT PANEL DESCRIPTION A318/A319/A320/A321

FRA US/O-7 KnB Feb 16, 2012

CENTER PEDESTAL PANEL

FO

R T

RA

ININ

G P

UR

PO

SE

S O

NLY

! �

Luft

hansa T

echnic

al T

rain

ing

Page 11LufthansaTechnical Training

ATA

22

22

AUTOFLIGHT

COCKPIT PANEL DESCRIPTION A318/A319/A320/A321

FRA US/O-7 KnB Feb 16, 2012

ATA 22 AUTO FLIGHT

FLIGHT CONTROL UNIT (FCU) 13VU

SPEED/MACH CONTROL AREA

SPEED/MACH WINDOW

� Shows selected SPD or MACH in “selectedguidance“.

� Shows after PWR UP: SPD 100 −“−−−“ in„managed guidance“.

� Display range: between 100 and 399 KT for speed,between 0.10 and 0.99 for MACH number.

SPD/MACH SELECTOR KNOB

� Knob pushed:

Engaged SPD/MACH for „managed guidance“.

� Knob pulled:

Engaged SPD/MACH for „selected guidance“.

SPD/MACH P/B

Depressing this PB changes SPD target to thecorresponding MACH target and vice versa (automaticon FL 305).

MANAGED SPD/MACH DOT

LATERAL CONTROL AREA

HDG/TRK WINDOW

� shows selected HDG or TRK in „selectedguidance“.

� shows after PWR UP: −−− , −“−−−“ in „managedguidance“.

� Display range: between 0 −359 deg.

HDG TRK SELECTOR KNOB

� Knob pushed:

Arms/engages NAV for „managed guidance“.

� knob pulled:

Engages HDG or TRK in „selected guidance“.

LOC MODE ENGAGEMENT P/B

Arms, engages or disengages the LOC mode.

MANAGED LATERAL DOT

13VU

FO

R T

RA

ININ

G P

UR

PO

SE

S O

NLY

! �

Luft

hansa T

echnic

al T

rain

ing

Page 68 LufthansaTechnical Training

ATA

33

33

LIGHTS

COCKPIT PANEL DESCRIPTION A318/A319/A320/A321

FRA US/O-7 KnB Feb 16, 2012

ATA 33 LIGHTS

INT LIGHTS, EMER LIGHTS ON 25 VU

OVHD INTEG LT KNOB

This knob turns the integral lighting for the overheadpanel on and off and adjusts its brightness.

STBY COMPASS SWITCH

This switch turns the integral lighting for the standbycompass on and off.

DOME SWITCH

This switch controls both dome lights.

� BRT

Both dome lights on bright.

� DIM

Both dome lights on dim.

� OFF

Both dome lights off.

ANN LT SWITCH

This switch sets the brightness of all the cockpitannunciator lights at either “bright“ or “dim“, and alsotests them.

� TEST

Illuminates all flight deck annunciator lights. Puts8‘s up in all LCDs (Liquid Crystal Displays).

� DIM

Reduces voltage to all annunciator lights.

� BRT

Allows annunciators to function normally.

EMER EXIT LT SWITCH

The selector has three detent positions.

� ON

Overhead emergency lights, EXIT signs andproximity marking system come on.

� OFF

Above lights are off.

� ARM

The proximity emergency escape path markingsystem comes on when the normal aircraftelectrical power or DC SHED ESS BUS is lost.

The overhead emergency lights come on if:

− Normal aircraft electrical power system fails or

− DC SHED ESS BUS fails or

− AC BUS 1 fails.

Exit signs come on if:

− Normal aircraft electrical power system fails or

− DC SHED ESS BUS fails or

NOTE: The LIGHT EMER pushbutton on thepurser‘s panel can turn on theemergency lighting independently of thepositions of this selector switch.

EMER EXIT LT “OFF“ LT

This light comes on amber when the EMER EXIT LTselector is selected OFF.

OFF

FO

R T

RA

ININ

G P

UR

PO

SE

S O

NLY

! �

Luft

hansa T

echnic

al T

rain

ing

Page 93LufthansaTechnical Training

ATA

71−8

0

71−80

ENGINE

COCKPIT PANEL DESCRIPTION A318/A319/A320/A321

FRA US/T-2 KnB Sep 01, 2010

ATA 71 POWER PLANT (e.g. CFM-56)

ENG MASTER SWITCH 1 (2)

� ON

LP fuel valve opens (if the ENG FIRE pushbutton isin).

− During an automatic start, the HP fuel valveopens if:

� The ENG MODE selector is at IGN/START.

� The engine accelerates to the appropriatethreshold, which is function of T2 and thealtitude.

− During a manual start, the HP FUEL valveopens if:

� The ENG MODE selector is at IGN/START.

� The MAN START pushbutton switch is ON.

� OFF

Close signals go directly to the HP fuel valve andthe LP fuel valve. These signals cause bothchannels of the FADEC to be reset.

NOTE: Releasing the ENG FIRE pushbuttonallows flight crew to shut down theengine by closing the LP fuel valve.There is a time delay of about 60seconds at ground idle as the engineburns the fuel left between the LPvalve and the nozzles.

ENG MODE SELECTOR

� CRANK

The start valve opens, if the MAN STARTpushbutton switch is ON. Ignition is not active.

� NORM

This turns on continuous ignition (A and B) whenthe engine is running and:

− The engine anti−ice pushbutton switch is ON, or

− a flame−out is detected, or

− the approach idle is selected.

− The master lever has been cycled from ON toOFF, then back to the ON position, or

− a surge is detected, or

− in case of severe rain or hail.

� IGN START

If the MASTER switch is ON and N2 . idle, thisposition selects continuous ignition (A and B).

− During an automatic start:

� On the ground, when N2 passes 16 %,ignition switches to A or B. However, if thereis an ignition delay during the start sequence,ignition is continuous (A and B).

� In flight, continuous ignition (A and B) beginswhen the start sequence begins.

− During a manual start, ignition commenceswhen the MASTER switch is turned ON.

NOTE: On the ground, the ignition isswitched off automatically at the endof the start sequence.

(N2 between 47 % and 53 %).

FIRE

FAULT

FIRE

FAULT

Airbus

Abbreviation List

bLufthansa

Technical Training

aLufthansa

Technical Training

4

ACR Avionics Communication Router ACRIF ACR Instrumentation Function ACRT Additional Cross Reference Table ACS Access ACS Air Conditioning System ACS Alternating Current Supply ACSC Air Conditioning System Controller ACT Active ACT Activity ACT Additional Center Tank ACTD Actuated ACTG Actuating ACTIV Active ACTN Action ACTR Actuator ACTVN Activation ACTVT Activate ACU Air Cooling Unit ACU Antenna Control Unit ACU Antenna Coupler Unit ACUTE AIRBUS Cockpit Universal Thrust Emulator ACVR Alternating Current Voltage Ratio AD Aerodrome AD Airplane Datum AD Airworthiness Directive A-D Airbus Deutschland ADAM Airbus Spares Distribution and

Materials System ADAU Auxiliary Data Acquisition Unit ADB Aeronautical Data Base ADB Airport Data Base ADB Area Distribution Box ADC Additional Control Device ADC Air Data Computer ADC Airbus Delivery Centre ADCL Airworthiness Directives Compliance List ADCN Avionics Data Communication Network

aLufthansa

Technical Training

91

P

P Purple P Roll Rate P Pressure

P(±OFF) Polarity (plus, minus, off) P.ALT Profile Altitude P.CLB Profile Climb P.DES Profile Descent P.EPR Profile EPR P.MACH Profile Mach P.N1 Profile N1 P.SPD Profile Speed P/B Pushbutton P/BSW Pushbutton Switch P/C Printed Circuit P/L Payload P/N Part Number P/P ROM Preprocessor ROM Pa Pascal PA Passenger Address PA Public Address PA AMP Passenger Address Amplifier PAD Partner Agreement Document PADS Pneumatic Air Distribution System PAL Programmable Array Logic PAMB Ambient Pressure PAR Precision Approach Radar PARAM Parameter PARK Parking PAS Pitch Attitude Sensor PATCC Production Aircraft Test Completion

Certificate PATM Production Aircraft Test Manual PATS Passenger Air-to-Ground Telephone System PAX PAX Announcement Entertainment and

Service Multiplex System