MAINTENANCE
T R A I N I N G H A N D B O O K
PART 1 : ELECTRO - AVIONICS SYSTEMS
FOR TRAINING ONLY - VDJ19511
JANUARY 2020
This document must be used for training purposes only
Under no circumstances should this document be used as a reference
It will not be updated.
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
No part of this manual may be reproduced in any form,
by photostat, microfilm, retrieal system, or any other means,
without the prior written permission of AIRBUS S.A.S.
AIRBUS Environmental Recommendation
Please consider your envrionmental responsability before printing this document.
- GENERAL - AVIONICS -
Training by Airbus
CHECK LIST - WALK AROUND & COCKPIT
P. 8
EXTERNAL PANELS
P. 23
COMPUTER & C/B LOCATIONS
P. 49
ATA 24 - ELECTRICAL POWER
P. 70
ATA 42 - INTEGRATED MODULAR AVIONICS AND AVIONICS DATA
COMMUNICATION NETWORK
P. 101
ATA 31 - INDICATING / RECORDING SYSTEMS
P. 109
ATA 46 - INFORMATION SYSTEMS
P. 126
ATA 45 - ONBOARD MAINTENANCE SYSTEM
P. 154
ATA 34 - NAVIGATION
P. 178
ATA 22 - AUTO FLIGHT
P. 209
ATA 23 - COMMUNICATIONS
P. 215
ATA 44 - CABIN SYSTEMS
P. 240
ATA 33 - LIGHTS
P. 247
SUMMARY
ATA 29 - HYDRAULIC POWER
ATA 32 - LANDING GEARS
ATA 52 - DOORS
ATA 25/50 - EQUIPMENT & FURNISHING AND CARGO
& ACCESSORY COMP.
ATA 27 - FLIGHTS CONTROLS
ATA 35 - OXYGEN
ATA 38 - WATER AND WASTE
ATA 28 - FUEL
- POWERPLANT -
ATA 26 - FIRE PROTECTION SYSTEMS
ATA 49 - AIRBORNE AUXILIARY POWER
ATA 70 - STANDARD PRACTICES - ENGINES
REF TO PART 2 : ELECTRO - MECHANICAL SYSTEMS
- AIRFRAME -
ATA 51 - STANDARD PRACTICES AND STRUCTURES
ATA 36 - PNEUMATIC
ATA 21 - AIR CONDITIONING
ATA 47 - INERT GAS SYSTEM
Gl.
ATA 30 - ICE & RAIN PROTECTION
CONVERSION TABLE, LIST ABBREVIATION & SYMBOLS CARD
P. 607
Training by Airbus
GENERAL
CHECK LIST - WALKAROUND & COCKPIT
P. 8
EXTERNAL PANELS
P. 23
COMPUTER & C/B LOCATIONS
P. 49
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
CHECK LIST - WALKAROUND
& COCKPIT
EXTERIOR WALKAROUND
2
1
4
5
22
7
23
24
21
8
6
9
12
18
13
20
LH FWD FUSELAGE :
- FUSELAGE / DOORS................................................... CHECK CONDITION
- WING AND ENGINE SCAN LIGHTS............................ CHECK CONDITION
- STATIC PROBES.......................................................... CLEAR
- NEGATIVE PRESSURE VALVE................................... CLOSED
- CREW OXYGEN DISCHARGE INDICATOR................ GREEN
- CAMERA LIGHT .......................................................... CHECK CONDITION
(if installed)
- AVIONICS COMPARTMENT DOOR............................. CLOSED
- BATTERY EXHAUST.............................…………...…... CHECK CONDITION
- STAND-BY STATIC PROBES....................................... CLEAR
- STAND-BY PITOT PROBE........................................... CHECK CONDITION
- MULTI-FUNCTIONS PROBE (MFP)…......................... CHECK CONDITION
- AOA PROBE................................................................. CHECK CONDITION
- ICE DETECTOR PROBE……………............................ CHECK CONDITION
3
1
Training by Airbus
10
2 NOSE SECTION :
19
11
14
17
- FUSELAGE................................................................... CHECK CONDITION
- RADOME....................................................CHECK CONDITION / LATCHED
- SIDESLIP PROBES (IF INSTALLED)........................... CHECK CONDITION
- ICE DETECTION VISUAL INDICATORS...................... CHECK CONDITION
- WIPERS......................................................................... CHECK CONDITION
CHECK CONDITION :
NO DAMAGE, NO DENT, NO IMPACT MARK,
NO DEFORMATION, NO CRACK, NO FOD PRESENCE,
NO MISSING ELEMENT, NO LEAK.
15
16
Page 8
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List
EXTERIOR WALKAROUND
2
3 NOSE L/G :
- FUSELAGE................................................................... CHECK CONDITION
- CHOCKS....................................................................... IN PLACE
- WHEEL WELL / DOORS.............................................. CHECK CONDITION
- TAKEOFF, TAXI AND TURN OFF LIGHTS ................. CHECK CONDITION
- NOSE GEAR STRUCTURE.......................................... CHECK CONDITION
- HYD AND ELEC LINES AND EQUIPMENT.................. CHECK CONDITION
- DOWNLOCK SPRINGS................................................ CHECK CONDITION
- WHEELS AND TIRES................................................... CHECK CONDITION
- OAT PROBES............................................................... CHECK CONDITION
- GROUND ELECTRICAL POWER DOOR (IF NOT REQUIRED)..... CLOSED
- WATER DRAIN VALVE................................................. NO LEAK
3
1
4
5
22
7
23
24
21
8
6
9
12
18
13
20
Training by Airbus
10
19
11
14
17
15
16
4 RH FWD FUSELAGE :
- FUSELAGE / DOORS................................................... CHECK CONDITION
- STAND-BY STATIC PROBES....................................... CLEAR
- MULTI-FUNCTIONS PROBES (MFP)…....................... CHECK CONDITION
- ICE DETECTOR PROBE……………............................ CHECK CONDITION
- NLG DOOR OPENING HANDLE……..………………... STOWED
- BATTERY EXHAUST.............................…..……...….... CHECK CONDITION
- CAMERA LIGHT .......................................................... CHECK CONDITION
- CARGO DOOR............................................................. CLOSED
- ACCESS DOORS (IF NOT REQUIRED)...................... CLOSED
- NEGATIVE PRESSURE VALVE................................... CLOSED
- STATIC PROBES.......................................................... CLEAR
- WING AND ENGINE SCAN LIGHTS............................ CHECK CONDITION
- CREW OXYGEN DISCHARGE INDICATOR................ GREEN
CHECK CONDITION :
NO DAMAGE, NO DENT, NO IMPACT MARK,
NO DEFORMATION, NO CRACK, NO FOD PRESENCE,
NO MISSING ELEMENT, NO LEAK.
Page 9
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EXTERIOR WALKAROUND
Training by Airbus
2
5 LOWER CENTER FUSELAGE :
3
1
4
5
22
7
23
24
8
6
21
9
12
18
13
20
10
19
11
14
- FUSELAGE................................................................... CHECK CONDITION
- ANTENNAS................................................................... CHECK CONDITION
- AVIONICS VENTILATION OVERBOARD VALVE........ CHECK CONDITION
- CAMERA....................................................................... CHECK CONDITION
- OUTFLOW VALVE........................................................ CHECK CONDITION
Normally wide open. If not, risk of pressurized A/C)
- DRAIN MAST................................................................. CHECK CONDITION
- COMPARTMENT AIR EXTRACTION OUTLET............ CHECK CONDITION
(Option)
- BILGE DRAIN HOLES.................................................. NO LEAK
- BELLY FAIRINGS......................................................... CHECK CONDITION
- PACK BAY VENTILATION AIR INTAKES.................... CLEAR
- RAM AIR INLET FLAP.................................................. CHECK CONDITION
- ACCESS DOORS (IF NOT REQUIRED)...................... CLOSED / CHECK CONDITION
- PACK AIR INTAKES..................................................... CLEAR
- BEACON LIGHT………................................................ CHECK CONDITION
- PACK BAY VENTILATION AIR OUTLETS................... CLEAR
- PACK AIR OUTLETS.................................................... CLEAR
- CONDITIONED SERVICE AIR SYSTEM OUTLETS…...................... CLEAR
- MLG BAY VENTILATION AIR INLET (ON LEFT SIDE ONLY)…...... CLEAR
- FUEL PUMPS DRAIN HOLES...................................... NO LEAK
6
17
15
16
CHECK CONDITION :
NO DAMAGE, NO DENT, NO IMPACT MARK,
NO DEFORMATION, NO CRACK, NO FOD PRESENCE,
NO MISSING ELEMENT, NO LEAK.
RH CENTER WING :
- WING / PANELS............................................................ CHECK CONDITION
- WING FUEL TANK WATER DRAIN VALVE.................. NO LEAK
- IGGS OUTLET............................................................... CHECK CONDITION
- LANDING LIGHT........................................................... CHECK CONDITION
- SLAT 1………................................................................ CHECK CONDITION
Page 10
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EXTERIOR WALKAROUND
Training by Airbus
7
2
- REVERSERS AND FAN COWLS................................. CLOSED / LATCHED / CHECK CONDITION
- AERODYNAMIC STRAKE............................................ CHECK CONDITION
- DRAIN MAST................................................................ CHECK CONDITION / NO LEAK
- STARTER VALVE OVERRIDE ACCESS..................... CLOSED
- ENGINE ANTI-ICE EXHAUST GRID............................ CHECK CONDITION
- ENGINE INLET AND FAN BLADES............................ CHECK CONDITION
3
1
4
5
22
8
7
23
24
6
9
12
18
13
10
19
11
14
ENG 2 RH SIDE :
- REVERSERS AND FAN COWLS................................. CLOSED / LATCHED / CHECK CONDITION
- ENGINE OIL FILL ACCESS DOOR.............................. CLOSED
- ENGINE VENTILATION EXHAUST GRID.................... CHECK CONDITION
- LATCH ACCESS DOORS…………………………...….. CLOSED
- TURBINE EXHAUST..................................................... CLEAR
8
21
20
ENG 2 LH SIDE :
9
RH WING LEADING EDGE :
- WING / PANELS........................................................... CHECK CONDITION
- REFUEL COUPLING DOOR........................................ CLOSED
- SLATS 2, 3, 4................................................................ CHECK CONDITION
10 RH WING TIP :
17
15
16
- WING / PANELS............................................................ CHECK CONDITION
- SLATS 5, 6, 7................................................................ CHECK CONDITION
- VENT / SURGE TANK FUEL WATER DRAIN VALVE.. NO LEAK
- FUEL VENTILATION OVERPRESSURE DISC ........... INTACT
- SURGE TANK AIR INLET............................................. CLEAR
- NAVIGATION AND STROBE LIGHTS.......................... CHECK CONDITION
- WINGLET....................................................................... CHECK CONDITION
- ANTENNAS ON TOP OF FUSELAGE.......................... CHECK CONDITION
CHECK CONDITION :
NO DAMAGE, NO DENT, NO IMPACT MARK,
NO DEFORMATION, NO CRACK, NO FOD PRESENCE,
NO MISSING ELEMENT, NO LEAK.
Page 11
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List
EXTERIOR WALKAROUND
Training by Airbus
2
11 RH WING TRAILING EDGE :
- WING / PANELS............................................................ CHECK CONDITION
- STATIC DISCHARGERS............................................... CHECK CONDITION
- CONTROL SURFACES................................................ CHECK CONDITION
- JETTISON OUTLET ..................................................... NO LEAK
(If installed)
- FLAPS AND FAIRINGS................................................ CHECK CONDITION
- CAMERA LIGHT .......................................................... CHECK CONDITION
(If installed)
3
1
4
5
22
7
23
24
8
12 RH LANDING GEAR :
6
21
9
12
18
13
20
10
19
- WING / PANELS............................................................ CHECK CONDITION
- CHOCKS....................................................................... IN PLACE
- WHEELS AND TIRES................................................... CHECK CONDITION
- BRAKES AND BRAKE WEAR INDICATORS.............. CHECK CONDITION
- ELEC AND HYDRAULIC LINES / EQUIPMENT........... CHECK
- LANDING GEAR / DOORS STRUCTURE.................... CHECK
- DOWNLOCK SPRINGS................................................ CHECK
CHECK CONDITION :
11
14
13 CENTER FUSELAGE :
17
15
16
NO DAMAGE, NO DENT, NO IMPACT MARK,
NO DEFORMATION, NO CRACK, NO FOD PRESENCE,
NO MISSING ELEMENT, NO LEAK.
- FUSELAGE / BELLY FAIRINGS................................... CHECK CONDITION
- ACCESS DOORS (IF NOT REQUIRED)...................... CLOSED
- FUEL DRAIN MAST...................................................... CHECK CONDITION / NO LEAK
- MLG DOORS................................................................. CHECK CONDITION
Page 12
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EXTERIOR WALKAROUND
Training by Airbus
14 RH AFT FUSELAGE :
2
3
1
4
5
22
7
23
24
8
6
21
9
12
18
13
20
10
- FUSELAGE / DOORS................................................... CHECK CONDITION
- BELLY FAIRINGS......................................................... CHECK CONDITION
- SUPPLEMENTAL COOLING AIR INTAKE(S) ..……… CLEAR
- RAT DOORS................................................................. CLOSED / CONDITION
- SUPPLEMENTAL COOLING AIR OUTLETS ……...... CLEAR / CONDITION
- ANTENNAS................................................................... CHECK CONDITION
- DRAIN MAST................................................................. CHECK CONDITION
- OUTFLOW VALVE........................................................ CHECK CONDITION
(Normally wide open. If not, risk of pressurized A/C)
- COMPARTMENT AIR EXTRACTION OUTLET............ CHECK CONDITION
- BILGE DRAIN HOLES.................................................. NO LEAK
- CARGO DOOR ............................................................ CLOSED
- ACCESS DOORS (IF NOT REQUIRED)...................... CLOSED
- POTABLE WATER SERVICE PANEL.......................... NO LEAK
- TOILET SERVICE PANEL............................................ NO LEAK
- VACUUM GENERATOR OUTLETS............................. CHECK CONDITION
- TAILSTRIKE INDICATORS.......................................... CHECK CONDITION
15 TAIL :
19
11
14
- FUSELAGE / DOORS / PANELS.................................. CHECK CONDITION
- STABILIZER, ELEVATOR, FIN AND RUDDER............ CHECK CONDITION
- STATIC DISCHARGERS (ELEVATOR AND RUDDER)..................... CHECK
- ACCESS DOORS.......................................................... CLOSED
CHECK CONDITION :
NO DAMAGE, NO DENT, NO IMPACT MARK,
NO DEFORMATION, NO CRACK, NO FOD PRESENCE,
NO MISSING ELEMENT, NO LEAK.
16 APU :
17
15
16
- FUSELAGE................................................................... CHECK CONDITION
- APU AIR INTAKE.......................................................... CHECK CONDITION
- APU EXHAUST............................................................. CLEAR
- NAVIGATION AND STROBE LIGHTS.......................... CHECK CONDITION
- ACCESS DOORS......................................................... CLOSED
- DRAIN MASTS............................................................. CHECK CONDITION / NO LEAK
Page 13
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EXTERIOR WALKAROUND
Training by Airbus
2
17 LH AFT FUSELAGE :
- FUSELAGE / DOORS / PANELS.................................. CHECK CONDITION
- STABILIZER, ELEVATOR, FIN AND RUDDER............. CHECK CONDITION
- BULK DOOR.................................................................. CLOSED
- SUPPLEMENTAL COOLING AIR OUTLETS…...…..... CLEAR
- DRAIN HOLES............................................................... NO LEAK
3
1
4
5
22
18 LH LANDING GEAR AND FUSELAGE :
7
23
24
8
6
21
9
12
18
13
20
10
19
11
14
17
15
16
- WING / PANELS............................................................ CHECK CONDITION
- CHOCKS........................................................................ IN PLACE
- WHEELS AND TIRES.................................................... CHECK CONDITION
- BRAKES AND BRAKE WEAR INDICATORS.............. CHECK CONDITION
- ELEC AND HYDRAULIC LINES / EQUIPMENT........... CHECK
- LANDING GEAR / DOORS STRUCTURE.................... CHECK
- DOWNLOCK SPRINGS................................................ CHECK
19 LH WING TRAILING EDGE :
- WING / PANELS............................................................ CHECK CONDITION
- STATIC DISCHARGERS............................................... CHECK CONDITION
- CONTROL SURFACES................................................. CHECK CONDITION
- JETTISON OUTLET ..................................................... NO LEAK
(If installed)
- FLAPS AND FAIRINGS................................................. CHECK CONDITION
- CAMERA LIGHT ........................................................... CHECK CONDITION
(If installed)
CHECK CONDITION :
NO DAMAGE, NO DENT, NO IMPACT MARK,
NO DEFORMATION, NO CRACK, NO FOD PRESENCE,
NO MISSING ELEMENT, NO LEAK.
Page 14
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EXTERIOR WALKAROUND
Training by Airbus
2
20 LH WING TIP :
- WING / PANELS........................................................... CHECK CONDITION
- SLATS 5, 6, 7................................................................ CHECK CONDITION
- VENT / SURGE TANK FUEL WATER DRAIN VALVE.. NO LEAK
- FUEL VENTILATION OVERPRESSURE DISC ........... INTACT
- SURGE TANK AIR INLET............................................. CLEAR
- NAVIGATION AND STROBE LIGHTS.......................... CHECK CONDITION
- WINGLET...................................................................... CHECK CONDITION
- ANTENNAS ON TOP OF FUSELAGE......................... CHECK CONDITION
3
1
4
5
22
7
23
24
8
21 LH WING LEADING EDGE :
6
21
9
- WING / PANELS........................................................... CHECK CONDITION
- REFUEL COUPLING DOOR (OPTION)....................... CLOSED
- SLATS 2, 3, 4................................................................ CHECK CONDITION
12
18
13
20
10
22 ENG 1 LH SIDE :
19
11
14
- REVERSERS AND FAN COWLS................................. CLOSED / LATCHED / CHECK CONDITION
- DRAIN MAST................................................................ CHECK CONDITION / NO LEAK
- STARTER VALVE OVERRIDE ACCESS..................... CLOSED
- ENGINE ANTI-ICE EXHAUST GRID............................ CHECK CONDITION
- ENGINE INLET AND FAN BLADES............................ CHECK CONDITION
CHECK CONDITION :
17
15
16
NO DAMAGE, NO DENT, NO IMPACT MARK,
NO DEFORMATION, NO CRACK, NO FOD PRESENCE,
NO MISSING ELEMENT, NO LEAK.
Page 15
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List
EXTERIOR WALKAROUND
Training by Airbus
2
23 ENG 1 RH SIDE :
- REVERSERS AND FAN COWLS................................. CLOSED / LATCHED / CHECK CONDITION
- AERODYNAMIC STRAKE............................................ CHECK CONDITION
- ENGINE OIL FILL ACCESS DOOR.............................. CLOSED
- ENGINE VENTILATION EXHAUST GRID.................... CHECK CONDITION
- LATCH ACCESS DOORS……………………………..... CLOSED
- TURBINE EXHAUST..................................................... CLEAR
3
1
4
5
22
7
23
24
8
24 LH CENTER WING :
6
21
9
12
18
13
20
10
19
11
14
- WING / PANELS............................................................ CHECK CONDITION
- IGGS OUTLET............................................................... CHECK CONDITION
- SLAT 1………................................................................ CHECK CONDITION
- LANDING LIGHT........................................................... CHECK CONDITION
- WING FUEL TANK WATER DRAIN VALVE................. NO LEAK
CHECK CONDITION :
NO DAMAGE, NO DENT, NO IMPACT MARK,
NO DEFORMATION, NO CRACK, NO FOD PRESENCE,
NO MISSING ELEMENT, NO LEAK.
17
15
16
Page 16
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NOTE
Training by Airbus
Page 17
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Training by Airbus
CHECKLIST - COCKPIT
OUTSIDE CHECK :
- AIRCRAFT WALK AROUND......................................... PERFORM
- ADAPTED WHEEL CHOCKS........................................IN PLACE
- PAX / CARGO DOOR RED CAB PRESS......................NOT FLASHING
CENTER PEDESTRAL :
- PARK BRK LEVER....................................................... ON
- LDG GEAR GRVTY EXTN SWITCHES........................ OFF / GUARDED
- A/SKID SWITCH............................................................ ON
- L/G LEVER.................................................................... DOWN
- THRUST LEVERS......................................................... IDLE / REVERSE STOWED
- ENG MASTER SWITCHES........................................... OFF
- ENG START SELECTOR.............................................. NORMAL
- BAT P/B SWITCHES..................................................... ALL OFF / CHECK VOLT
ABOVE 23 V
- RESET SWITCHES....................................................... CHECK
- CKPT EQPT POWER SUPPLY PANELS..................... CHECK
- FIRE PUSHBUTTONS (ENG + APU)............................ IN / GUARDED
- ALL PRIMS P/B SWITCHES......................................... NORMAL
- ALL SECS P/B SWITCHES.......................................... NORMAL
- FUEL PUMPS P/B SWITCHES..................................... OFF
- CROSS-BLEED VALVE SELECTOR............................ AUTO
- OXYGEN CREW SUPPLY P/B SWITCH...................... CHECK OFF
- WIPER SELECTORS.................................................... OFF
- DITCHING P/B SWITCH............................................... NOT SELECTED
- EMER EXIT LT............................................................... OFF
- EXT LT........................................................................... OFF
- EMER BAT 2 P/B SWITCH........................................... ON
- EMER BAT 1 P/B SWITCH........................................... ON
- BAT 1 P/B SWITCH...................................................... ON
- BAT 2 P/B SWITCH...................................................... ON
- EXT PWR 2 P/B SW (IF AVAIL ILLUMINATED) .......... ON
- EXT PWR 1 P/B SW (IF AVAIL ILLUMINATED)........... ON
- CDS (ALL EXCEPT OIS).............................................. ADJUST BRIGHTNESS
- ECAM AC and DC ELEC PAGE................................... SELECT / CHECK
- ON RMP 1...................................................................... ON / SET FREQ
- GEN P/B SW (ENG + APU)........................................... ON
• SCAN ELEC PANEL AND CHECK NO AMBER AND WHITE
LIGHTS (EXCEPT AMBER GEN FAULT LIGHT).
ECAM AC and DC ELEC PAGE.................................... SELECT / CHECK
- COCKPIT LIGHTS........................................................ AS REQUIRED
- VENTILATION PANEL.................................................. CHECK NO LIGHTS
ILLUMINATED
- DISPLAY UNITs............................................................. ADJUST BRIGHTNESS
AS REQD
- COCKPIT LIGHTING.................................................... AS REQUIRED
- ANN LT TEST................................................................. PERFORM
- SCAN SEQUENCE........................................................ PERFORM
NOTE : DURING THE SCAN SEQUENCE, IT IS A GENERAL RULE TO
EXTINGUISH ALL WHITE LIGHTS ON THE OVERHEAD PANEL AND TO
SET ALL THE ROTARY SELECTORS TO THE NORM/AUTO (12 O’CLOCK)
POSITION
- EXT LT SELECTORS.................................................... AS REQUIRED
- EMER EXIT LT SELECTOR.......................................... AS REQUIRED
- DITCHING P/B SWITCH................................................NOT SELECTED
WARNING
BE SURE THAT DITCHING PUSHBUTTON IS RELEASED OUT TO
PREVENT RISK OF CABIN PRESSURIZATION.
- ECAM CONTROL PANEL............................................. SELECT PRESS
• CHECK AVNCS OVBD AND OUTFLOW VALVES OPEN.
- RMP 2.............................................................................ON / SET TO INT
• CHECK TRANSMISSION AND RECEPTION WITH
GROUND CREW.
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
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Training by Airbus
CHECKLIST - COCKPIT
- ECAM CTL PNL (ROTARY KNOB /”ALL” KEY).......... SELECT C/B
- FLAPS / SPEED BRAKE LEVER POSITION............... CHECK
• IF LEVER DOES NOT AGREE WITH INDICATIONS ON
PFD/ ECAM, SET LEVERS TO CORRESPONDING POSITION.
- PARK BRK LEVER....................................................... ON
• CHECK BRAKES PRESS INDICATIONS.
• CHECK ACCUS PRESS INDICATIONS NORMAL (GREEN BAND).
IF NOT, PRESS ACCUS REINFLATE P/B SWITCH.
- On MFD SURV PAGE................................................... XPDR IN STBY
LEAVING THE AIRCRAFT :
- ADAPTED WHEEL CHOCK......................................... IN PLACE
- EXT PWR....................................................................... ON
- APU BLEED P/B SWITCH............................................ OFF
- APU................................................................................ OFF
- PARK BRK LEVER........................................................ CONFIRM ON
• CHECK BRAKES PRESS INDICATIONS.
• CHECK ACCUS PRESS INDICATIONS NORMAL (GREEN BAND).
IF NOT, PRESS ACCUS REINFLATE P/B SWITCH.
NOTE : WAIT 2 MIN FOR ACCUMULATOR RECHARGE CYCLE
- EFB................................................................................ OFF
- TOWING ON BAT P/B SWITCH.................................... OFF
- BAT VOLT SELECTOR................................................. OFF
- ADIRS MODE ROTARY SELECTORS.......................... OFF
- WIPER SELECTORS..................................................... OFF
- CREW OXYGEN SUPPLY P/B SWITCH....................... OFF
- EXT LT SELECTORS.................................................... OFF
- SIGNS AND EMER EXIT LT SELECTOR..................... OFF
- CABIN PRESS MODE P/B SWITCHES........................ CONFIRM BOTH IN AUTO
- FUEL PUMPS P/B SWITCHES..................................... CONFIRM OFF
- CROSSFEED P/B SWITCHES...................................... OFF
- CROSS-BLEED VALVE SELECTOR............................ AUTO
- DITCHING P/B SWITCH................................................ NOT SELECTED
- CDS................................................................................ DIMMED IF NECESSARY
- RECORDER GROUND CONTROL............................... NORMAL FLT (NOT ON)
- RMP 1, 2 AND 3............................................................. OFF
- L/G LEVER.................................................................... DOWN
- THRUST LEVERS ......................................................... IDLE / REVERSE STOWED
- ENG MASTER SWITCHES........................................... OFF
- ENG START SELECTOR.............................................. NORMAL
- LDG GEAR GRVTY EXTN SWITCHES........................ OFF / GUARDED
- A/SKID SWITCH............................................................ ON
- ELEC REMOTE C/B CTL.............................................. OFF
- BAT 2 P/B SWITCH....................................................... OFF
- BAT 1 P/B SWITCH....................................................... OFF
- EMER BAT 1 P/B SWITCH............................................ OFF
- EMER BAT 2 P/B SWITCH............................................ OFF
- EXT PWR 1 P/B SWITCH.............................................. OFF (AVAIL)
- EXT PWR 2 P/B SWITCH.............................................. OFF (AVAIL)
- AIRCRAFT WALK AROUND......................................... PERFORM
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
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Training by Airbus
OVERHEAD PANEL PRESENTATION
265VU
CKPT DOOR CTLR
A
RESET
B
C
231VM
D
E
FMC-A
GND COOLG
F
FMC-C
VCS
1
SCS
TR
1
EMER
TR1
SDS
1
SLATS
1
FLAPS
1
FQMS
1
AICS
1
FWS
1
LGCIS
1
BSCS
1
AESU
1
CIDS
1
ATC
EIM
1
1
1
OFF
OXYGEN
2
2
ELEC
BAT
OFF
SVCE INT
OVRD
REMOTE
C/B CTL
EMER 2
1
ON
ON
EMER 1
2
FADEC GND PWR
1
2
GND HF
DATALINK
RESET
ON
ENG
3
ON
ECON MODE
4
ON
CHARGE
GND
CONNECTION
HIGH
MED
LOW
ON
S
T
TR
2
EMER
TR2
AICS
2
FWS
2
232VM
U
V
W
SDS
2
SLATS
2
FLAPS
2
FQMS
2
LGCIS
2
BSCS
2
AESU
2
CIDS
2
DSCS
EIM
2
FMC-B
2
2
3
3
REFUEL
ON
OFF
OVRD
ON
VCS
2
1
COM
OIS OIS CAB
AVNCS & MAINT
END
4
PACK
2
1
ON
FUEL
APU
CKPT DOOR
LOCKG SYS
R
FAULT
POWER
26.8
88.8
8
8
RESET
255VM
HI
TOWING ON BAT
FAULT
3
A
U
T
O
NORM
LO
CKPT
AVNCS
PACK
1
CINS
4
ON
4
245VM
5
5
CCD 1
5
CKPT EQPT POWER SUPPLY
KBD 1
WHC 1
FCU
PRINTER
B
C
D
E
6
6
A
5
CCD 2
CKPT EQPT POWER SUPPLY
KBD 2
WHC 2
HUMID
EFB 3
S
T
U
V
6
F
6
R
221 VM
CVR
CABIN
B
O
O
M
S
E
T
TEST
PAX PERS LANDSCAPE
CAMERA
ELEC SPLY
ENG 1
OFF
OFF
PAX INFO
MOBILE COM
LAVATORY
OFF
OFF
F
I
R
E
OCCPD
ADIRS
IR1
ON BAT
IR2
IR3
FAULT
FAULT
OFF
OFF
FAULT
OFF
NAV
OFF
ATT
OFF
ADR1
SQUIB
DISCH
GREEN
H
Y
D
ADR2
ADR3
OFF
SQUIB
DISCH
SUPPLY
AGENT
YELLOW
ENG 1
SUPPLY
PUMP
OVHT
FAULT
OVHT
ISOL
OFF
ISOL
FAULT
OFF
FAULT
FAULT
OFF
OFF
SEC 3
FAULT
FAULT
OFF
OFF
FUEL JETTISON
ARM
ACTIVE
F
U
E
L
MAIN
L TK
EMER GEN
A
U
T
O
FAULT
TEST/RESET
ACMS
DFDR
RCDR
TRIGGER
EVENT
GND CTL
ON
MASK MAN O
ON
FAULT
E
L
E
C
OXYGEN
EVAC
HORN OFF
CALLS
CAB REST
OFF
SLOW
OFF
FAULT
FAULT
FAULT
OFF
OFF
OFF
1A
DRIVE
GEN
FAULT
FAULT
EXT 1
DISC
OFF
AVAIL
FAULT
DISC
FAST
1B
ELM
ON
AC 1B BUS
AC 1A BUS
DRIVE
SIDE 1 & 2
ISOL
BAT 2
OFF
PAX SYS
R TK
OFF
GND HYD
YELLOW ELEC PMP
GREEN ELEC PMP
A
U
T
O
A
U
T
O
FAULT
OFF
ON
FAULT
OFF
ON
FAULT
ISOL
OFF
OFF
FAULT
OFF
OFF
OFF
PRIM 2
SEC 2
FAULT
FAULT
OFF
A
U
T
O
OFF
DRIVE
FAULT
APU GEN
FAULT
OFF
FAULT
DISC
2B
TURB DAMPG
OFF
OFF
CARGO AIR COND
FWD
ISOL VALVES
AFT
ISOL VALVES
FAULT
FAULT
OFF
OFF
BULK
ISOL VALVES
FAULT
OFF
TEMP REGUL
15
TEMP REGUL
15
5
5
OFF
FAULT
EXT 2
FAULT
E
L
E
C
FAULT
OFF
AVAIL
DISC
OFF
AC 2A BUS
AC 2B BUS
BUS TIE
GEN
COMMERCIAL
1
2
OFF
212VM
F/CTL
F
U
E
L
STBY
FAULT
GALLEY
DRIVE
GEN
OFF
2A
GEN
25
25
25
25
OFF
FWD CARGO
PRESEL
HEATER
ACTIV
FAULT
OFF
ON
CAPT &
PURS
PACK 1
A
I
R
OFF
CKPT
HI VENT
RAIN
RPLNT
CABIN
COCKPIT
HI
LO
COLD
OFF
FAULT
FAULT
OFF
FF
FAULT
OFF
1
ENG
2
FAULT
FAULT
ON
ON
EXT LT
BEACON
ON
NAV
1
ON
FF
OFF
OFF
FF
CABIN ALT
DEC
INC
STBY
COMPASS
& EYE REF
ON
START
ON
A
U
T
O
MAN
UP
A
U
T
O
INT LT
ON
FIRE
SMOKE
FIRE
DISCH
VENT
ENG
215 VM
TRGT
DITCHING
M
DIM
NO PED
ON
AUTO
ON
RAIN
RPLNT
INTMT
FAST
ON
FAULT
OFF
NO MOBILE
ON
IFEC
OFF
FF
F
PAX BBAND
SMOKE
SMOKE
OFF
OFF
OFF
SLOW
FAST
INTMT
SLOW
EMER
EXIT LT
ON
AUTO
OFF
CAB SYS SMOKE
INTMT
MEDIUM
SIGNS
A
U
T
O
WIPER
DN
AUTO
OFF
F
FF
ON
CAB FANS
COOLG
A
U
T
O
MAN START
1
2
BRT
OFF
F
FF
OFF
F
FF
FAULT
OVRD
ANN LT
TEST
SEAT BELTS
ON
AVAIL
OFF
FF
AVNCS
EXTRACT
SMOKE
MLG BAY
AGENT TO AFT
CABIN V/S
MODE
ICE
IND
FAULT
AVNCS
SMOKE
FAULT
CABIN PRESS
MODE
MAN
MASTER SW
AUTO
OFF
FF
F
A
U
T
O
TRGT
APU
LOGO
ON
RAM AIR
OFF
PROBE &
WINDOW HEAT
2
WING
ON
ENG 2 BLEED
ON
AUTO MODE
STROBE
ON
FAULT
OFF
ANTI ICE
WING
HOT AIR 2
OPEN
FAULT
OFF
A
I
R
ON
AUTO
APU BLEED CLOSE
FAULT
WINDSHIELD
DEFOG
COLD
HOT
H
HOT
H
XBLEED
PURS SEL
HOT AIR 1
DISCH
BTL1
BTL1
BTL2
BTL2
BTL3
SMOKE
OFF
MAN
ENG 1 BLEED
AGENT TO FWD
PACK 2
FAULT
ON
EMER
AFT
AIR FLOW
NORM
AUTO
INTMT
SLOW
MAIN
FAULT
ON
CALL
CA
ALL
EXIT
WIPER
INTMT
MEDIUM
OFF
R
MAN
FAULT
ON
INTMT
FAST
ISOL
FAULT
ON
O
N
MID
OFF
ON
BAT EMER 1 BAT EMER 2
CAPT
APT
FWD
ISOL
R TK XFR
FAULT
ON
ALL
FAULT
FAULT
CREW
SUPPLY
OFF
FLT REST
OVHT
A
U
T
O
FAULT
OFF
OFF
GATELINK
CARGO SMOKE
EVAC
PURS
FAULT
L TK XFR
ON
SYS ON
COMMAND
MECH CALL
H
Y
D
PUMP
OVHT
CTR TK
FEED
FAULT
FAULT
OFF
BAT 1
A
U
T
O
PAX
A
U
T
O
OFF
225 VM
RAT MAN ON
ARMED
OFF
ON
EMER
R ELEC PWR
ELT
ON
CAB DATA
TO OIS
ON
L
STBY
OPEN
ON
SUPPLY
PUMP
OIS
OIS DATA
TO AVNCS
235 VM
YELLOW
ENG 2
ON
211VM
PRIM 3
SQUIB
DISCH
OPEN
CROSSFEED A
F/CTL
SQUIB
DISCH
CROSSFEED B
OFF
OPEN
SEC 1
AGENT 2
SQUIB
DISCH
SUPPLY
PUMP
OFF
PRIM 1
AGENT 1
GREEN
FAULT
FAULT
PUSH
PUSH
FIRE
TEST
AGENT 2
ATT
ATT
FAULT
AGENT 1
222VM
F
I
R
E
FIRE
RE
E
FIRE
RE
E
PUSH
ERASE
ENG 2
APU
FIRE
RE
E
NAV
OFF
NAV
W
ARM
OFF
FF
OFF
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
MAIN INSTRUMENT PANEL & GLARESHIELD PRESENTATION
ATC MESSAGE-INDICATOR
CAPT EFIS
CONTROL PANEL
ATTENTION
GETTERS
AUTOLAND LIGHTS
411 VU
TAXI
TAXI
QNH
MASTER
WARN
PTT
LOUDSPEAKER
OFF
LOUDSPEAKER SOUND
- LEVEL CONTROL
OIS
HUD
NORM
ATC
AUTO
MSG
LAND
CHRONO
DECLUTTER
SIDESTICK
PRIORITY
CAPT
M
MAX
XWIND
N
ND
OFF
CSTR
WPT
VORD
NDB
WX
TERR
TRAF
1016
in Hg
MASTER
CAUT
SPD
MAG
ARPT
40
ARC
---
MAG
HDG
HDG
HDG
V/SV/S
VV
SIDE-STICK
PRIORITY LIGHTS
AP1
10
320
640
V/S
1000
1000
100
100
A/THR
40
20
ED
ALT
WD
WPT
VORD
NDB
WX
TERR
TRAF
ARPT
TAXI
1016
hPa
APPR
ARC
VOR
160
10
320
ZOOM
640
MASTER
WARN
SIDESTICK
PRIORITY
MASTER
CAUT
PLAN
LS
ATC MESSAGE-INDICATOR
ATTENTION
GETTERS
412 VU
NAV
80
Training by Airbus
QNH
in Hg
DN
LOC
CSTR
----UP
AP2
PERMANENT
DATA
SD
IXAT
ALT
TRK
TRK
FPAFPA
7000
160
ZOOM
METER
---
80
20
PLAN
LS
LS
TRUE
TRUE
FD
NAV
B
BRT
R
MACH SPD SPD
hPa
VOR
F/O EFIS
CONTROL PANEL
AFS
CONTROL PANEL
VV
CHRONO
HUD
DECLUTTER
OFF
LOUDSPEAKER
NORM
F/O
LS
B
BRT
AUTO
ATC
LAND
MSG
OFF
IND
ND
D
XWIND
SIDE-STICK
PRIORITY LIGHTS
ATC
MAIL
BOX
311 VU
PTT
M
MAX
LOUDSPEAKER SOUND
- LEVEL CONTROL
OIS
312 VM
LIMIT SPEED
(IAS KT)
313 VU
VLO = VLE
NORM & GRVTY 250
M 0.55
255
220
212
195
190
186
VFE 1
1+F
2
3 T/O
3 LDG
FULL °
140
135
FLEX
5
0
EGT
°C
692
10
74. 0
78. 1
BRK FAN
83. 9 % 53°C
THR
%
N1
%
PACKS
5
0
10
692
T.O INHIBIT
NO SMOKING
SEAT BELTS
GND SPLRs ARMED
OIS
MAP LT
AVNCS
CONSOLE LT
CAPT ON
BKUP
AUTO
OIS
A/BRK
MAP LT
L/G
AIR DATA
VIEW
OFFSIDE
314 VU
140
135
EGT
°C
74. 0
78. 1
UP
F/O ON
BKUP
VIEW
OFFSIDE
INOP
CONSOLE LT
INOP
ON
ON
FMS
PEDALS LT
ON
BOTH
ON 2
NORM
PEDALS LT
ON
BOTH
ON 1
OFF
FF
OFF
FF
DOWN
301 VM
SLAT/FLAP
LIMITATION
MEMO
MODE
ND
PFD
MFD
VD
302 VM
LS/
MODE
+
LS/
ND
+
MENU
SET/SEL
+53°C
MENU
SET/SEL
DISPLAY
CYCLE
CAPT OIS
ON CENTER
F/O OIS
ON CENTER
DISPLAY
CYCLE
AVAIL
INOP
INOP
AVAIL
ON
ON
VD
SLAT/FLAP
LIMITATION
MEMO
PFD
MFD
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
Ch
List
Ch
List
Training by Airbus
CENTER PEDESTAL PRESENTATION
ESC
DIR
PERF
INIT
NAV
AID
C/L
MENU
ESC
DIR
PERF
INIT
NAV
AID
CLR
INFO
F-PLN
DEST
SEC
INDEX
SURV
ATC
COM
CLR
INFO
F-PLN
DEST
SEC
INDEX
SURV
Y
U
Y
U
Q
W
.
A
E.
R
S.
/
D
Z
OIS
T
F
X
C
V
H
O
J
B
K
N
.
M
Q
P
SPACE
A
ENT
1
2
3
4
5
6
7
8
9
0
+/-
.
W
.
NOTE
PAD
L
MAIL
BOX
MFD
ND
G
I
TO
GA
FLX
M
C
T
FLX
M
C
T
CL
CL
A
A
T
H
R
T
H
R
0
0
TEL
MENU
VHF1
121.900
VHF2
123.450
CALL
HF1
TEL1
CALL
CALL
CALL
VHF2
HF2
TEL2
CALL
VHF3
INT
FIRE
ON
ENG START
1
8
9
0
+/-
VHF
2
FAULT
IGN
START
OFF
OFF
MSG
CLR
RST
2
3
4
5
6
7
8
9
.
0
CLR
BRT
.
.OF
OFF
T.O
CONFIG
EMER
CANC
DEFRD
ATT
INT
CAB
STB
STBY
TB
ADF 2
RAD
1
NAV
LOAD
VOICE
MORE
STS
DOOR
FUEL
WHEEL
EL/AC
EL/DC
HYD
F/CTL
APU
BLEED
COND
PRESS
WXR
GND SPLRS ARMED
TCAS
ELEVN
DN
RET
RET
1/2
ABV
GAIN
MAIL
BOX
MFD
ENT
OIS
ND
TEL
SQWK
VHF1
121.900
VHF2
123.450
DATA
VHF3
DATA
FULL
L
WXR
SYS 1
R
XPDR
TCAS
+
F
/
O
VD AZIM
SYS 2
L
R
SYS 2
RST
CALL
CALL
CALL
VHF1
HF1
TEL1
CALL
CALL
CALL
VHF2
HF2
TEL2
0
ACCU
1
2
3
4
5
6
7
8
9
.
0
CLR
BRT
.
.OF
OFF
MECH
ATT
INT
CAB
STB
STBY
TBY
B
ADF 2
RAD
1
NAV
RAD
D
LOAD
VOICE
PA
LS 1
R
VOR
2
MKR
0
1
1
2
2
2
2
3
3
3
3
FLAPS
FULL
NOSE DN
3.5 PSI
3.5 x1000
1.6
0
INT
0
FULL
L
YELLOW
ON
STBY
115 VM
PITCH TRIM
ACCU
REINFLATE
NAV
SQUAWK: 2523
VHF3
UP
U
GAIN
OF
FF
OFF
+
VD AZIM
MENU
ELEVN
DN
G/S MODE
SYS 1
PULL & TURN
SPACE
WXR
TA
TA
ONLY
UP
U
C
A
P
T
1/2
FULL
OFF
M
123.125
CALL
CLEAR
BLW
PARK BRK
NOTE
PAD
L
121.700
VIDEO
VIDEO
CLEAR
R
VOR
2
MKR
ALL
SPEED
BRAKE
HF
SD
ENG
EMER
DESCENT
N
.
RCL
ALL
PA
LS 1
B
P
K
ABN
RCL
LAST
DISPCH
MECH
V
J
ESC
FIRE
NORM
CRANK
DATA
1
ARM
7
KBD
FAULT
RAD
D
6
H
ATC
COM
O
CCD 2
ON
VHF3
CALL
3
5
135 VM
VHF 1 RECEPTION NOT SELECTED
CALL
2
STBY
123.125
VHF1
C
1
ESC
NAV
121.700
DATA
MSG
CLR
SQWK
X
G
I
KBD 2
CCD 1
HF
F
4
.
T
SPACE
KBD 1
VHF
D
Z
SPACE
KBD
R
S.
/
TO
GA
E.
C/L
MENU
NOSE UP
GREEN
RUDDER TRIM
CKPT LT
L/G GRVTY EXTN
FLOOD LT
NOSE
R
NOSE
L
INTEG LT
RESET
VHF
HF
TEL
SQWK
MENU
NAV
RESET
BR
B
BRT
OFF
F
OFF
OFF
F
BR
B
BRT
CKPT DOOR
DU MASTER BRT
B
INHIBIT
ON
BIT
BI
N
DOME LT
OPEN
DOWN
FAULT
OFF
FF
STORM
UNLOCK
NORM
LOCK
BR
B
BRT
MSG
CLR
ABORT
SLEW
TEST
121.700
VHF1
121.900
123.125
VHF2
123.450
DATA
VHF3
DATA
STBY
RST
SQUAWK: 2523
STATUS
CALL
CALL
CALL
VHF1
HF1
TEL1
CALL
CALL
CALL
VHF2
HF2
TEL2
0123456789
1
2
3
4
5
6
7
8
9
.
0
CLR
MECH
CALL
VHF3
INT
LOAD
ATT
INT
CAB
STB
STBY
TB
RAD
NAV
RAD
D
.
.OF
OFF
BRT
VOICE
PA
ADF 2
1
LS 1
VOR
R
2
MKR
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
EXTERNAL
PANELS
FORWARD, NOSE FUSELAGE & CENTER FUSELAGE
Training by Airbus
NOTE
CENTER FUSELAGE
132BR
132AR
122AR
FORWARD & NOSE FUSELAGE
141AZ
142AZ
Page 23
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
Ext
Pa
AFT BOTTOM & AFT RIGHT
Training by Airbus
152BR
152AR
171AL
NOTE
AFT BOTTOM
164AR
FWD
AFT RIGHT
152BR
FWD
152BR
Page 24
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
Ext
Pa
BELLY FAIRING REAR
199
Training by Airbus
198VR
198RR
198UR
199BR
198CR
197MB
198AB
197RB
2L
197BB
197KB
197JB
197QB
197NB
197FB
197SB
198AR
198EB
198GB
199AB
198CR
198GR
198HB
198PB
FWD
NOTE
198YR
198QR
198PR
198NR
198SR 198MR 198LR
2R
197
198HR
198TR
199AR
198ER
198JR
198KR
198
197LB
197DB
197AB
197CB
197AL
197ML
197GL
199AL
197KL
197QL
197NL
197HL
197PL
197LL
197JL
197RL
197EL 197CL
197BL
Page 25
FR69
FR65
FR61
FR54
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
Ext
Pa
BELLY FAIRING FRONT
Training by Airbus
191
194
192
NOTE
194MR
193JR
194KR
194KB
194JB
194HR
194DB
194FB
193QB
193XB
193LL
193ML
193NL
194CR
193TB
194BR
191AB
2R
193AB
193FB
191BB
193BB
193KB
193HB
193LB
193MB
193GL
193KL
2L
191BL
193AL
193CL
193EL
193EB
193GB
193JL
193FL
193DB
193DL
191AL
193BL
FWD
193PL
FR54
192AR
193CB
194CB
193UB
193HL
192BR
194AB
193JB
193PB
194DR
194AR
194BB
193SB
193RB
193WB
194FR
194ER
194GB
194HB
193VB
194GR
194LR
194EB
194NR
193NB
194QR
194PR
193
FR49
FR42
Page 26
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
Ext
Pa
BELLY FAIRING LEFT - REAR & FRONT
Training by Airbus
FR54
FR61
195DT
195
FR65
197
NOTE
FR69
195ET
195FT
197BT
195GT 197ET
197CT
197DT
197AT
197DL
BELLY FAIRING LEFT - REAR
197SL
197CL
197FL
197LL
197PL
199AL
197JL
FWD
195
191
FR49
FR42
19
AT
191
1BT
195AT
195BT
FR54
195CT
191CL
BELLY FAIRING LEFT - FRONT
FWD
Page 27
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
Ext
Pa
BELLY FAIRING DETAIL A
Training by Airbus
OPTION A : EXTRA SCS ON RH WITH CDM PLUS 1 OR 2 VCRU
NOTE
198XR
198ZR
198AS
198RR
198WR
198FR
FWD
OPTION B : EXTRA SCS ON RH WITH ONLY A CDM
198XR
198ZR
Page 28
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
Ext
Pa
BELLY FAIRING RIGHT - BACK & FRONT
Training by Airbus
198
196
FR65
FR61
FR69
198FT
198ET
198BT
198DT
BELLY FAIRING RIGHT - BACK
199AR
NOTE
198CT
198UR
198RR
198VR
198KR
196ET
196FT
198GT
196GT
198AT
199BR
FR54
196DT
198DR
198FR
198CR
198JR
FWD
FR54
192BT
FR49
196CT
196BT
196AT
196
FR42
19
2
192
AT
192CR
BELLY FAIRING RIGHT - FRONT
FWD
Page 29
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
Ext
Pa
VTP LH & VTP RH
Training by Airbus
324AT
326AT
5F
32
L
2C
EL
32
L
5D
32
32
L
2A
5B
L
32
32
L
323DR
323ER
323CR
323BL 323CL
VTP LH
2A
323EL
32
325AR
BR
325AL
25
R3
323AL
FWD
5C
323DL
321AL
FWD
32
5C
L
R
L
5D
2B
32
32
2B
R
L 3
5E
25
32
32
L
R
2C
5F
32
32
L 3
R
322DL
NOTE
5G
25
326AT
32
GL
324AT
321AL
323AR
323BR
VTP RH
Page 30
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
Ext
Pa
HTP TOP & HTP BOTTOM
34
4E
33
T
34
4D
34
1E
T
T
Logo light
34
4C
T
34 344AT
4B
T
34
1D
T
F
W
D
Logo light
3
334AT
T
4B
33
34
343AT
34
1B
T
333AT
33
T
1B
33
33
NOTE
T
1E
T
1D
HTP BOTTOM
T
1C
332AT
342AT
334EB
331AT
341AT
T
DT
CT
33
34
1C
T
4
33
4E
332AT
342AT
Training by Airbus
33
332AB
33
344EB
4D
B
1E
T
33
HTP TOP
33
1D
T
4C
B
33
33
1C
T
4B
33
B3
34
AB
333AB
1B
T
331AT
34
B
4A
34
4
BB
343AB
T
1B
34
34
4
CB
34
4D
B
T
1E 342AB
34
T
1D
34
T
1C
34
341AT
F
W
D
Page 31
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
Ext
Pa
HTP LEFT & HTP RIGHT
Training by Airbus
NOTE
HTP LEFT
HTP RIGHT
FWD
FWD
333AT
343AT
333AB
343AB
Page 32
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
Ext
Pa
HTP RIGHT & LEFT ELEVATOR
Training by Airbus
NOTE
HTP RIGHT ELEVATOR
345CB
345AB
345BB
345DB
345EB
345FB
F
W
D
HTP LEFT ELEVATOR
F
W
D
335AB
335BB
335CB
335DB
335EB
335FB
Page 33
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
Ext
Pa
S19
Training by Airbus
S19 TOP
NOTE
S19 LEFT
311BL
317AB
317AB
315AL
317BB
311AL
FWD
FWD
S19 RIGHT
S19 BOTTOM
316BR
317AB
317AB
312BR
311BB
316AR
314AR
316AR
315AL
312AR
311AB
314AR
FWD
FWD
Page 34
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
Ext
Pa
PYLON 1 OUTBOARD & INBOARD
Training by Airbus
PYLON 1 OUTBOARD
455CL
455BL
4 52
AL
L
4 5 3B
45
4 5 5DL
4 5 5EL
4 5 5A L
4 5 3FL
4 5 3 EL 4 5 3GL
3 DL
45
5F
L
4 5 5 JL
55
4 5 5HL 4
4 5 5G
PYLON 1 INBOARD
KL
L
PL
455RL
455QL
455NL
L 459BL
455JR
SL
455
NOTE
L
459CL
4 59A L
455
4 5 5L
ML
455
S
455
455
PR
455DL
455ER
455CL
455M
R
455QR
455NR
455LR
455FR
455
KR 455H
R
4 5 5 BL
4 5 3 BR
4 5 3A R
4 5 2 BR
4 52 A L
459AR
Page 35
455GR
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
Ext
Pa
PYLON 2 OUTBOARD & INBOARD
Training by Airbus
PR
4 6 5M
465QR
R 4
65LR
465JR
465K
R
465NR
5F
465
R
PYLON 2 OUTBOARD
SL
46
465
465CR
4 6 5DR
4 6 5ER
4 6 5 BR
4 6 3 ER
4 6 3 F R 4 6 3 DR
4 6 3 BR
469AR
469CR
469BR
465HR
465GR
465BR
465EL
465CR
4 6 5A L
4 62 A
L
4 62 AL
463CR
465DR
PYLON 2 INBOARD
NOTE
4 6 3B
L
5
3 EL 4 6 3 F L 4 6
4 6 3 DL 4 6
FL 4 6 5
6 5M L
LL 4
JL 4 6 5
4 6 5K L
465
PL
465
SL
465RL
465QL
465NL
469AL
465HL
465GL
Page 36
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
Ext
Pa
ENGINE 1 INBOARD & OUTBOARD
Training by Airbus
ENGINE 1 INBOARD
ENGINE 1 OUTBOARD
NOTE
417FR
417FL
417DR
417DL
417AR
417GR
417CL
417AL
417GL
41
5A
41
7C
417ER
417QR
R
41
5A
415CL
L
417EL
R
5A
41
415CL
7C
41
R
5A
41
417RR
L
417QL
L
417RL
417BR
417BL
415BR
Page 37
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
Ext
Pa
ENGINE BOTTOM
417KL
417SL
Training by Airbus
417ML
417PL
ENGINE 1 BOTTOM
415AL
NOTE
417NL
411AL
417CL
417HL
417HR
415BL
417CR
415AR
417NR
417PR
417JL
417SR
417SR
417LL
427SR
427KL
427ML
427PR
ENGINE 2 BOTTOM
425AR
427NR
421AL
427CR
427HR
427HL
425BL
427CL
425AL
427NL
427PL
Page 38
427LL
427SL
427JL
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
Ext
Pa
ENGINE 2 OUTBOARD & INBOARD
Training by Airbus
ENGINE 2 INBOARD
ENGINE 2 OUTBOARD
427FR
NOTE
427FL
427DR
427DL
427AR
427AL
427CL
427GL
427GR
42
7C
42
R
42
427ER
427QR
427RR
5A
4 2 5 CL
5A
L
R
5A
42
4 2 5 CL
R
4
427BR
A
25
L
4
C
27
427EL
L
427QL
427RL
427BL
425BR
Page 39
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
Ext
Pa
LEFT WING TOP
Training by Airbus
NOTE
RIB1
522AT
F
W
D
RIB11
572CT
572BT
572AT
RIB23
534BB 534GB
534FB
5 81
AT
T
T
1C
534AT
571BT
57
534BT
57 1
581HT 581GT 581FT 581ET 581DT
DT
5 81
CT
5 81
B
57 1
AT
534JB
Page 40
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
Ext
Pa
LEFT WING BOTTOM IN & OUT
Training by Airbus
523FB
LEFT WING BOTTOM IN
LEFT WING BOTTOM OUT
RIB18
52
521AB
521BB
F
W
D
511AB
3G
NOTE
RIB20
B
52
3H
RIB22
F
5
RIB24
542MB 23J
542KB
W
B
521JB
D
54
3 A 52 3
RIB26
51
572EB
RIB4
B
1
KB
542NB
BB
52
5
57 2
43
1D
FB
CB 5 2 3
511EB
542PB
B 5 511C
RIB28
L
5
RIB6
21
521KB
7
2G
5
EB B 51
54 B 5
4
511AZ
B
3B
523NB
3
1D
EB 2 3M
B
B
57 3
B
RIB8
RIB30
5
A B 4 3D
54
B
523PB
3
521FB
5
GB
523QB
57 3
4
572HB
541AB
521GB
BB 3 F B
534GB
591AB
RIB11
1
522AB
534FB
541BB
591EB
550AB
52
57 3
572CT
523CB
3
C
541CB
AB
B
RIB33
550BB
591CB 591DB
541DB
57 3
52
RIB14
591FB
550CB
534BB
3
DB
541EB
BB
542CB
523EB
B
591GB
542AB
571BB
52
RIB16
3D
542BB
591HB 591KB
542EB
B
571EB
571MB
591LB 591MB
542DB
591JB
542FB
571FB
571AB
534HB
571GB
534JB
572AB
542GB
571CB
571JB
RIB2
542JB
57 2
571LB
571DB 571HB
571KB
572BB
542LB
CB
57 2
DB
B
542HB
Page 41
572EB
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
Ext
Pa
LEFT WING BOTTOM INSIDE
Training by Airbus
RIB7
542BZ
542AZ
NOTE
541AZ
541CZ
541BZ
515AZ
Page 42
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
Ext
Pa
LEFT WING FAIRING IN & OUT
Training by Airbus
531CR
531AR
531BR
531BB
NOTE
531AB
532AR
531DB
531AT
532BB
531CB
532AB
531EB
532AT
532CB
532DB
533AR
532CR
532EB
533BR
533AB
533AT
533EB
LEFT WING FAIRING IN
532BR
533BB
533DB
533CR
533CB
533AL
532BL
532AL
LEFT WING FAIRING OUT
533DL
533BL 533CL
533EB
533AB
532AB
533AT
533DB
533EL
532DB
532CL
532DL
532AT
532EB
532EL 531AT
531BL
531AL
531AB
531DB
531EB
531DL
531CL
Page 43
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
Ext
Pa
RIGHT WING TOP
Training by Airbus
NOTE
RIB1
622AT
RIB11
RIB23
634GB
672AT
672BT
634BB
672CT
634JB
634FB
AT
6 71
681FT
681DT
DT
671 81CT
6
T
BT
1C
681ET
681GT
6 81
67
T
A
6 81
671BT
681HT
634AT
634BT
Page 44
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
Ext
Pa
RIGHT WING BOTTOM OUT & IN
Training by Airbus
RIB18
RIB20
RIGHT WING BOTTOM OUT
RIB22
623FB
GB
NOTE
3
62
642KB
B
3H
62 642LB
642JB
621BB 621AB
JB
B
611AB
3
N
62
42
B 6
B
RIB26
A
RIB2
43
642MB
3K
672EB
F
62 B 6
611BB
FB
W
3B
B
RIB4
PB
RIB28
672
3L 6 4
6 42
D
62
B
B
G
B
2
611DB
B
C
1D
67
621JB
1C EB 62
MB 643DB 643
RIB6
1
3
6
611AZ
621KB
RIB30
62
21
AB
643EB
611EB
6
3
672HB
7
6
NB 643FB
RIB8
641AB
23
B
6
B
691AB
3
B 643GB
634GB
7
621FB
P
6
634FB
23
641BB
672CT
621GB
B 6 650AB 3CB
RIB11
691DB
Q
623CB RIB1
7
3 650BB
RIB33
6
B
2
691FB
641CB
6
622AB
691CB
3A
691EB
641DB
62
634BB
650CB 3DB
691GB
RIB14
B
671MB
67
641EB
691HB
3B
634JB
62
691KB 691JB
642AB
RIB16
RIB1
16
671BB
B
642CB
691LB
634HB
3D
642BB
671DB
62 642E
2EB
642EB
691MB
623EB
642DB
671FB
671AB
671GB
672AB
671CB
642HB
642FB
RIGHT WING BOTTOM IN
671JB
RIB24
642GB
F
W
D
67
2 DB
67 2
672KB
CB
672BB
671HB
671EB
671LB
Page 45
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
Ext
Pa
RIGHT WING FAIRING IN & OUT
Training by Airbus
631AL 631BL
631BB
631AB
632AL
632BB
631CB
631EB
632CL
632DB
633AL
63
632EB
633BL
3A
RIGHT WING FAIRING IN
632AT
632CB
633BB
NOTE
631AT
631DB
632BL
632AB
631CL
633CL
B
633AT
633DB
633CB
633EB
633DR
6
633BR
633AT
633EB
RIGHT WING FAIRING OUT
633CR
633ER
632AT
632EB
632ER
631EB
633DB
633AR
633AB
632DB
632AB
632DR
632CR
631BR
631DB
631AT
631DR 631CR
632BR 632AR
631AR
631AB
Page 46
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
Ext
Pa
RIGHT WING BOTTOM INSIDE
Training by Airbus
642BZ
RIB7
642AZ
NOTE
641AZ
641CZ
641BZ
615AZ
Page 47
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
Ext
Pa
FORWARD, NOSE & AFT FUSELAGE
Training by Airbus
NOTE
FORWARD & NOSE FUSELAGE
821BR
821AR
AFT FUSELAGE
Page 48
822BR 822AR
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
Ext
Pa
COMPUTER & C/B LOCATIONS
LOCATIONS OF C/B PANELS
Training by Airbus
NOTE
NORMAL ACCESS TO C/B MANAGEMENT
BACKUP ACCESS TO C/B MANAGEMENT
NOTE: FOR C/B STATUS SELECTION PAGE,SEE SHEET 2
Page 49
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
CO
&
C/B
LOCATIONS OF C/B PANELS
Training by Airbus
NOTE
C/B STATUS SELECTION PAGE
NOTE: FOR LOCATION ON PANEL, SEE SHEET 2
Page 50
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
CO
&
C/B
LOCATIONS OF C/B PANELS
Training by Airbus
C/B STATUS SELECTION PAGE
NOTE
FACE
NOTE : FOR LOCATION ON PANEL, SEE SHEET 2
POWER CENTER
Page 51
ZONE
MATRIX
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
CO
&
C/B
LOCATIONS OF C/B PANELS
CBP: Circuit Breaker Panel
EPDC: Electrical Power Distribution Center
Training by Airbus
EPDC 1 INNER FACE (FACE 1)
1A
1D
EPDC 1 OUTER FACE (FACE 3)
3A
1G
3C
3E
3G
NOTE
1K
CBP 1
CBP 2
5
6
1B
EPDC 1
1E
3L
1H
1L
3 1
1000
VU
1100 VU
2 4
1C
1F
01 03 05
02 04 06
1CE05
A
B
C
ZONE
MATRIX
FACE 1: EPDC 1 INNER
FACE 4: EPDC 2 OUTER
3F
3N
FWD
EPDC 2 INNER FACE (FACE 2)
EPDC 2 OUTER FACE (FACE 4)
2G
2D
2A
2H
2E
2B
2L
FACE 2: EPDC 2 INNER
FACE 3: EPDC 1 OUTER
3D
1M
4G
4E
4C
4J
4L
4H
2J
2F
2C
4M
4F
4D
2M
4N
FACE 5: CBP 1
FACE 6: CBP 2
4A
2K
D
E
F
G
1J
3H
3M
FWD
1200 VU
EXAMPLE OF C/B LOCATION:
FACE
3J
EPDC 2
Page 52
© Airbus SAS 2014. All rights reserved. Confidential and proprietary document.
FWD
FWD
CO
&
C/B
LOCATIONS OF C/B PANELS
Training by Airbus
CBP: Circuit Breaker Panel
EPDC: Electrical Power Distribution Center
NOTE
EPDCs
CBP 1
CBP 2
5
6
EPDC 1
3 1
EPDC 2
1000
VU
1100 VU
2 4
CBPs
1200 VU
EXAMPLE OF C/B LOCATION:
1CE05
5A
FACE
ZONE
6A
MATRIX
FACE 1: EPDC 1 INNER
FACE 2: EPDC 2 INNER
FACE 3: EPDC 1 OUTER
Page 53
FACE 4: EPDC 2 OUTER
FACE 5: CBP 1
CBP 2 FORWARD FACE (FACE 6)
VIEW LOOKING FWD
VIEW LOOKING FWD
© Airbus SAS 2014. All rights reserved. Confidential and proprietary document.
CO
&
C/B
FACE 6: CBP 2
CBP 1 FORWARD FACE (FACE 5)
COMPUTERS LOCATION BY VU - 1000 VU
Training by Airbus
NOTE
SCI 1
1TL1
CIDS 1
100RH1
CIDS 2
100RH2
SCI 2
1TL2
1011VU
1012 VU
1041 VU
AESU 1
1SE1
1051 VU
CRDC A08
1TS08
CRDC A09
FWD
1042 VU
OPU 1B
102XU1
DME 1
1SD1
1TS06 CRDC A06
FMC C
1CC3
1TS05
PRIM 3
1CE3
SW 9
1TH 09
1031 VU
CRDC A05
1022 VU
1TS03 CRDC A03
1021 VU
SW19
1 TH 19
IMCC-OSFC
2TC
AECM A
18GF1
IMCC-ASFC
1TC
SEC 3
2CE3
1000 VU
ADF 1
1RP1
ADF 2
1RP2
OPU 2B
102XU2
VOR 1
1RS1
GCU
VOR 2 2B
1RS2 2XU2
1TS09
GCU
1B
2XU1
1052VU
Page 54
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
CO
&
C/B
COMPUTERS LOCATION BY VU - 1100 VU
RBCU 1
10GL1
SW
FMC A 13
1CC1 1TH
13
SW
CPIOM CPIOM CPIOM 15 GCU
1A
H63
H61
J51
1TH
8TF63 8TF61 9TF51
15 1XU1
Training by Airbus
1100 VU
NOTE
1111VU
SW CPIOM CPIOM CPIOM CPIOM
11
J23
H33
H41
J11
1TH 9TF11 9TF23 8TF33 8TF41
11
BOMU CPIOM
QAR
H31
1
SPARE
14HA1 8TF31
FWD
1121VU
CDAU
2TU
CPIOM CPIOM
J71
H43
8TF43 9TF71
CMV 1
1TE1
SEC 1
2CE1
SW
1 OPU 1A
1TH 101XU1
01
PRIM 1
1CE1
1131VU
SDU
5RV1
SW
5
1TH
05
SW
3 CPIOM
1TH J21
03 9TF21
1141VU
AMU 1
1RN1
RA 1 MVDR
1
1SA1
1RC1
MMR 1
40RT1
SFCC 1
2CV1
HFDR 1
1RE1
1151VU
Page 55
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
CO
&
C/B
COMPUTERS LOCATION BY VU - 1200 VU
Training by Airbus
CPIOM
H44
8TF44
RBCU 2
10GL2
CPIOM CPIOM
J52
H62
9TF52 8TF62
AECM B
18GF2
GCU
EMER
2XE
OPU 2A
101XU2
NOTE
1212VU
BOMU SW CPIOM
16
FMC B
2
1TH H 32
14HA2 16 8TF32 1CC2
1200 VU
CPIOM CPIOM
J12
H34
9TF12 8TF34
GCU
2A
1XU2
FWD
1222VU
SEC 2
2CE2
SW CPIOM
4
J72
1TH
9TF72
04
SW
2
1TH
02
CMV 2
1TE2
SW CPIOM
6
H42
1TH 8TF42
06
1232VU
PRIM 2
1CE2
SW CPIOM
12
J22
1TH 9TF22
12
AESU 2
1SE2
SFCC 2
2CV2
1242VU
HFDR 2
1RE2
CPIOM MMR 2
H64
40RT2
8TF64
DME 2
1SD2
CPIOM SW MVDR 2
14
J24
1TH 1RC2
9TF24 14
AMU 2
1RN2
1252VU
Page 56
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
CO
&
C/B
PHYSICAL C/B LOCATION BY ATA
TO
ATA
DEVICE
FIN
PROTECTION DEVICE
DESIGNATION
FROM
EQUIPMENT
PHYSICAL
LOCATION
215200
3101HH
C/B-ASCU1 NORM
EPDC1
1FD07
215200
227700
3102HH
C/B-ASCU2 NORM
EPDC2
2FC05
3201CC
C/B-FMC-A
CBP1
5AH03
227700
227700
3102CC
C/B-FMC-B
EPDC2
2KM04
3101CC
C/B-FMC-C
EPDC1
1KL02
228100
3201CB
C/B-FCU CHAN1
CBP1
5AC11
228100
231100
3102CB
C/B-FCU CHAN2
EPDC2
2KJ01
3101RE
C/B-XCVR HFDR1
EPDC1
1JA07
231100
3102RE
C/B-XCVR HFDR2
EPDC2
2JA02
231200
3102RC
C/B-XCVR MVDR2
EPDC2
2KP03
231200
3202RC
C/B-XCVR MVDR2 EMER
CBP2
6AB01
232800
3101RV
C/B-SATCOM1
EPDC1
1JA06
235000
3201RN
C/B-AMU1 & RMP1
CBP1
5AD07
235000
3105RN
C/B-AMU1 & RMP1 BKUP SPLY
EPDC1
1KN01
235000
235000
3102RN
C/B-AMU2
EPDC2
2KN03
3202RN
C/B-AMU2 & RMP2
CBP2
6AF01
235300
3101WC
C/B-MECH CALL HORN
EPDC1
3AF02
237100
3203RK
C/B-CVR CTL
CBP1
5AD03
237100
3202RK
C/B-CVR SPLY
CBP2
6AE13
237500
3101RM
C/B-TAC BELLY
EPDC1
1FC01
Training by Airbus
PHYSICAL
LOCATION
TO
ATA
DEVICE
FIN
PROTECTION DEVICE
DESIGNATION
FROM
EQUIPMENT
237500
242200
242200
3104RM
C/B-TAC VERT STAB
EPDC2
2FC08
3201XU
C/B-GCU1A
CBP1
5AC09
3201XU
C/B-GCU1A
CBP1
5AH11
C/B-GCU1B
CBP1
5AC10
242200
3203XU
3203XU
C/B-GCU1B
CBP1
5AJ15
242200
242200
3202XU
3204XU
C/B-GCU2A
CBP2
6AB08
C/B-GCU2B
CBP2
6AE05
242200
242200
3204XU
3209XU
C/B-GCU2B
CBP2
6AJ06
C/B-OPU1A BKUP
CBP1
5AJ06
242200
242200
242200
3105XU
3211XU
3107XU
C/B-OPU1A POR
EPDC1
1GA01
C/B-OPU1B BKUP
C/B-OPU1B POR
CBP1
EPDC1
5AJ07
1DA03
242200
3210XU
C/B-OPU2A BKUP
CBP2
6AK09
242200
242200
3106XU
3212XU
C/B-OPU2A POR
EPDC2
2GA02
242200
242200
3108XU
3205XU
242200
3205XU
3101XU
C/B-VFG1A DISC
CBP1
5AH07
242200
C/B-VFG1A POR
EPDC1
1GA02
242200
3207XU
C/B-VFG1B DISC
CBP1
5AC15
242200
C/B-OPU2B BKUP
CBP2
6AJ14
C/B-OPU2B POR
EPDC2
2DA01
C/B-VFG1A DISC
CBP1
5AC14
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
CO
&
C/B
Training by Airbus
TO
ATA
DEVICE
FIN
PROTECTION DEVICE
DESIGNATION
FROM
EQUIPMENT
PHYSICAL
LOCATION
242200
3207XU
C/B-VFG1B DISC
CBP1
5AJ11
242200
242200
3103XU
C/B-VFG1B POR
EPDC1
1DA02
3206XU
C/B-VFG2A DISC
CBP2
6AB04
242200
3102XU
C/B-VFG2A POR
EPDC2
2GA01
242200
3208XU
C/B-VFG2B DISC
CBP2
6AE04
242200
242200
242400
3208XU
C/B-VFG2B DISC
CBP2
6AK06
3104XU
C/B-VFG2B POR
EPDC2
2DA02
3202XE
C/B-RAT POR
EPDC2
4GB03
242400
3208XE
C/B-RAT POR 1
EPDC2
4GA01
242400
3210XE
C/B-RAT POR 2
EPDC2
4GA02
242400
242400
242400
242800
242800
TO
ATA
DEVICE
FIN
PROTECTION DEVICE
DESIGNATION
FROM
EQUIPMENT
PHYSICAL
LOCATION
243400
243400
3203PE
C/B-EMER TR1 POM
EPDC1
3HZ15
3200PE
C/B-EMER TR2 BKUP
EPDC2
4HJ05
3202PE
C/B-EMER TR2 POM
EPDC2
4HZ14
1001PM
1002PM
C/B-701PM
C/B-702PM
EPDC1
EPDC2
1KZ02
2KZ02
243600
243600
3103PM
C/B-BAT1 VOLTAGE IND
EPDC1
3AE01
3102PM
C/B-BAT2 VOLTAGE IND
EPDC2
4AF04
243600
243600
3105PM
C/B-BMU1
EPDC1
3AG05
3104PM
C/B-BMU2
EPDC2
4AG07
2003PB
C/B-703PB
EPDC1
3HZ08
243400
243600
243600
3212XE
C/B-RAT POR 3
EPDC2
4GA03
3201XE
C/B-RAT SOL AUTO
EPDC1
3HH01
243800
243800
2004PB
C/B-704PB
EPDC2
4HZ08
3203PB
C/B-EMER BAT1 VOLTAGE IND
EPDC1
3HK02
3200XE
C/B-RAT SOL AUTO MANUAL
EPDC2
4HK05
243800
2001XB
C/B-STATIC INVERTER 1
EPDC1
3HZ09
243800
3202PB
C/B-EMER BAT2 VOLTAGE IND
EPDC2
4HH02
2002XB
C/B-STATIC INVERTER 2
EPDC2
4HZ09
243800
243800
3205PB
C/B-EMER BMU1
EPDC1
3HJ04
3204PB
C/B-EMER BMU2
EPDC2
4HK04
3101XG
C/B-EXT PWR1 AVAIL
EPDC1
1KJ03
3101PU
C/B-TR1 BKUP
EPDC1
3AG02
3103PU
C/B-TR1 POM
EPDC1
1KZ01
243200
243200
3100PU
C/B-TR2 BKUP
EPDC2
4AE04
244100
244100
3103XG
C/B-EXT PWR1 NOT IN USE
EPDC1
1KJ04
3102PU
C/B-TR2 POM
EPDC2
2KZ01
244100
3102XG
C/B-EXT PWR2 AVAIL
EPDC2
2KH04
243400
3201PE
C/B-EMER TR1 BKUP
EPDC1
3HK04
244100
3104XG
C/B-EXT PWR2 NOT IN USE
EPDC2
2KH03
243200
243200
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
CO
&
C/B
Training by Airbus
FROM
EQUIPMENT
PHYSICAL
LOCATION
C/B-ATUC1A
EPDC1
C/B-ATUC1B
EPDC1
C/B-ATUC2A
EPDC2
TO
ATA
DEVICE
FIN
PROTECTION DEVICE
DESIGNATION
245100
3101XN
245100
245100
245100
3103XN
3102XN
245100
245100
3AG07
TO
ATA
DEVICE
FIN
PROTECTION DEVICE
DESIGNATION
FROM
EQUIPMENT
PHYSICAL
LOCATION
3AE07
245500
3292XD
C/B-492XD
EPDC2
2CZ01
4AE01
245700
246100
3102XF
C/B-CFFC
EPDC2
2FD07
3104XN
C/B-ATUC2B
EPDC2
4AE02
3105XN
C/B-ATULC1A
EPDC1
3AE06
3107XN
C/B-ATULC1B
EPDC1
3AG06
245100
245100
3106XN
C/B-ATULC2A
EPDC2
4AG02
3108XN
C/B-ATULC2B
EPDC2
4AG01
245200
1001XP
C/B-101XP
EPDC1
1JZ02
245200
245200
1003XP
C/B-103XP
EPDC1
1JZ03
1005XP
C/B-105XP
EPDC1
246100
246100
246100
246100
246100
1001PN
C/B-101PN
EPDC1
1KZ03
1003PN
C/B-103PN
EPDC1
1KZ04
1011PN
C/B-111PN
EPDC1
1KZ13
1013PN
C/B-113PN
EPDC1
1KZ14
1071PN
C/B-171PN
EPDC1
1KZ15
1002PN
C/B-202PN
EPDC2
2KZ03
1004PN
C/B-204PN
EPDC2
2KZ04
1FZ01
246100
246100
1012PN
C/B-212PN
EPDC2
2KZ12
1014PN
C/B-214PN
EPDC2
2KZ13
245200
1007XP
C/B-107XP
EPDC1
1FZ04
246100
245200
245200
1051XP
C/B-151XP
EPDC1
1JZ01
246100
1072PN
C/B-272PN
EPDC2
2KZ14
1002XP
C/B-202XP
EPDC2
2JZ02
246100
1111PN
C/B-311PH NORM
EPDC1
1KZ05
245200
245200
1004XP
C/B-204XP
EPDC2
2JZ03
246100
1112PN
C/B-412PH NORM
EPDC2
2KZ05
1006XP
C/B-206XP
EPDC2
2FZ01
2001PH
C/B-301PH
EPDC1
3HZ12
245200
1008XP
C/B-208XP
EPDC2
2FZ04
246400
246400
245200
245500
1052XP
2001XD
C/B-252XP
C/B-301XD
EPDC2
EPDC1
2JZ01
1CZ02
246400
246400
245500
3291XD
C/B-391XD
EPDC1
1CZ01
245500
2002XD
C/B-402XD
EPDC2
2CZ02
246400
246400
2003PH
C/B-303PH
EPDC1
3HZ13
2005PH
C/B-305PH
EPDC1
3HZ14
2011PH
2071PH
2073PH
C/B-311PH EMER
C/B-371PH
C/B-373PH
EPDC1
EPDC1
EPDC1
3HZ05
3HD01
3HZ07
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
CO
&
C/B
Training by Airbus
TO
ATA
DEVICE
FIN
PROTECTION DEVICE
DESIGNATION
FROM
EQUIPMENT
PHYSICAL
LOCATION
TO
ATA
DEVICE
FIN
PROTECTION DEVICE
DESIGNATION
FROM
EQUIPMENT
PHYSICAL
LOCATION
247100
247100
3103XZ
C/B-SRPU 2A&2B AC1B SPLY
EPDC1
1KJ01
3202XZ
C/B-SRPU 2A&2B EMER2 SPLY
EPDC2
4HZ01
1016XZ
C/B-SRPU 2A&2B NORM2 SPLY
EPDC2
2KZ06
3102XZ
C/B-SRPU1A DC2 SPLY
EPDC2
2KZ10
245500
2002PH
C/B-402PH
EPDC2
4HZ13
245500
245500
2004PH
C/B-404PH
EPDC2
4HZ11
2006PH
C/B-406PH
EPDC2
4HZ12
245500
2012PH
C/B-412PH EMER
EPDC2
4HZ05
245500
245500
2072PH
C/B-472PH
EPDC2
4HD05
247100
247100
2074PH
C/B-474PH
EPDC2
4HZ07
247100
3101XZ
C/B-SRPU2B DC1 SPLY
EPDC1
1KZ11
247100
3205XZ
C/B-EPU1A
EPDC1
3HZ03
247100
3111XZ
C/B-TR1 INPUT NORM1
EPDC1
1HB08
247100
247100
3207XZ
C/B-EPU1B
EPDC1
3HZ04
247100
3112XZ
C/B-TR1 INPUT NORM2
EPDC2
2HB08
3206XZ
C/B-EPU2A
EPDC2
4HZ03
1017XZ
C/B-TR1 OUTPUT A NORM1
EPDC1
1HB01
247100
3208XZ
C/B-EPU2B
EPDC2
4HZ04
247100
247100
1018XZ
C/B-TR1 OUTPUT A NORM2
EPDC2
2HB01
247100
3107XZ
C/B-RCCB 115V NORM1 SPLY
EPDC1
1KZ07
247100
3113XZ
C/B-TR1 OUTPUT B NORM1
EPDC1
1HB02
247100
3108XZ
C/B-RCCB 115V NORM2 SPLY
EPDC2
2KZ07
247100
3114XZ
C/B-TR1 OUTPUT B NORM2
EPDC2
2HB02
247100
3203XZ
C/B-RCCB 230V EMER1 SPLY
EPDC1
3HZ02
247100
3115XZ
C/B-TR1 OUTPUT C NORM1
EPDC1
1HB03
247100
3204XZ
C/B-RCCB 230V EMER2 SPLY
EPDC2
4HZ02
247100
3116XZ
C/B-TR1 OUTPUT C NORM2
EPDC2
2HB03
247100
3105XZ
C/B-RCCB 230V NORM1 SPLY
EPDC1
1KZ08
3117XZ
C/B-TR1 OUTPUT D NORM1
EPDC1
1HB04
247100
3106XZ
C/B-RCCB 230V NORM2 SPLY
EPDC2
2KZ09
247100
247100
3118XZ
C/B-TR1 OUTPUT D NORM2
EPDC2
2HB04
247100
247100
247100
3109XZ
C/B-RCCB 28V NORM1 SPLY
EPDC1
1KZ09
247100
3119XZ
C/B-TR1 OUTPUT E NORM1
EPDC1
1HB05
3110XZ
3104XZ
C/B-RCCB 28V NORM2 SPLY
C/B-SRPU 1A&1B AC2B SPLY
EPDC2
EPDC2
2KZ08
2KH06
247100
247100
3120XZ
C/B-TR1 OUTPUT E NORM2
EPDC2
2HB05
3121XZ
C/B-TR1 OUTPUT F NORM1
EPDC1
1HB06
247100
3201XZ
C/B-SRPU 1A&1B EMER1 SPLY
EPDC1
3HZ01
247100
3122XZ
C/B-TR1 OUTPUT F NORM2
EPDC2
2HB06
247100
1015XZ
C/B-SRPU 1A&1B NORM1 SPLY
EPDC1
1KZ06
247100
3123XZ
C/B-TR1 OUTPUT G NORM1
EPDC1
1HB07
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
CO
&
C/B
Training by Airbus
TO
ATA
DEVICE
FIN
PROTECTION DEVICE
DESIGNATION
FROM
EQUIPMENT
247100
3124XZ
C/B-TR1 OUTPUT G NORM2
EPDC2
247100
3209XZ
C/B-TR2 INPUT EMER1
EPDC1
247100
3218XZ
C/B-TR2 INPUT EMER2
247100
3211XZ
247100
247100
3220XZ
PHYSICAL
LOCATION
2HB07
TO
ATA
DEVICE
FIN
PROTECTION DEVICE
DESIGNATION
FROM
EQUIPMENT
PHYSICAL
LOCATION
3HM04
256200
3103MJ
C/B-ASPSU GPU1
EPDC1
1JB07
EPDC2
4HM04
C/B-TR2 OUTPUT A EMER1
EPDC1
3HM01
256200
261100
3104MJ
3201WP
C/B-ASPSU GPU2
C/B-CM/A MLG BAY
EPDC2
CBP1
2JB01
5AA04
C/B-TR2 OUTPUT A EMER2
EPDC2
4HM01
3202WP
C/B-CM/B MLG BAY
CBP2
6AA15
3213XZ
C/B-TR2 OUTPUT B EMER1
EPDC1
3HM02
261100
261200
3211WD
C/B-CM/A ENG1
CBP1
5AA05
247100
3222XZ
C/B-TR2 OUTPUT B EMER2
EPDC2
4HM02
261200
3121WD
C/B-CM/A ENG2
EPDC1
1KC01
247100
3215XZ
C/B-TR2 OUTPUT C EMER1
EPDC1
3HM03
261200
3112WD
C/B-CM/B ENG1
EPDC2
2KQ05
247100
3224XZ
C/B-TR2 OUTPUT C EMER2
EPDC2
4HM03
3222WD
C/B-CM/B ENG2
CBP2
6AA14
247100
247100
3210XZ
C/B-TR2 RAT INPUT
EPDC2
4HN04
261200
262100
3211WE
C/B-FIRE BTL1/A ENG1
EPDC1
3HJ02
3212XZ
C/B-TR2 RAT OUTPUT A
EPDC2
4HN01
3121WE
C/B-FIRE BTL1/A ENG2
EPDC1
3AE05
247100
247100
3214XZ
C/B-TR2 RAT OUTPUT B
EPDC2
4HN02
262100
262100
3112WE
C/B-FIRE BTL1/B ENG1
EPDC2
4AF05
3216XZ
C/B-TR2 RAT OUTPUT C
EPDC2
4HN03
3222WE
C/B-FIRE BTL1/B ENG2
EPDC2
4HH03
247100
247100
3125XZ
C/B-TR3 INPUT NORM1
EPDC1
1HC02
262100
262100
3213WE
C/B-FIRE BTL2/A ENG1
EPDC1
3HH02
3126XZ
C/B-TR3 INPUT NORM2
EPDC2
2HC02
262100
3123WE
C/B-FIRE BTL2/A ENG2
EPDC1
3AF01
247100
3127XZ
C/B-TR3 OUTPUT NORM1
EPDC1
1HC01
262100
247100
3128XZ
C/B-TR3 OUTPUT NORM2
EPDC2
2HC01
3114WE
3224WE
C/B-FIRE BTL2/B ENG1
C/B-FIRE BTL2/B ENG2
EPDC2
EPDC2
4AE05
4HH04
251100
251100
3103MS
C/B-SEAT CAPT
EPDC1
1KF06
3104MS
C/B-SEAT F/O
EPDC2
2KD04
256200
3102MJ
C/B-ASPSU
EPDC2
2JB03
262100
262200
3203WF
C/B-EMER STOP RLY 1 APU
CBP1
5AH01
262200
262200
3204WF
C/B-EMER STOP RLY 2 APU
CBP2
6AK03
3201WF
C/B-FIRE BTL/1 APU
EPDC1
3HH05
262200
3202WF
C/B-FIRE BTL/2 APU
EPDC2
4HJ02
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
CO
&
C/B
Training by Airbus
PROTECTION DEVICE
DESIGNATION
FROM
EQUIPMENT
PHYSICAL
LOCATION
3101CV
C/B-SFCC1 FLAP
EPDC1
1KK03
3103CV
C/B-SFCC1 FLAP WTB
EPDC1
1KS01
3201CW
C/B-SFCC1 SLAT
CBP1
5AH13
3102CW
C/B-SFCC2 SLAT
EPDC2
2KD06
3104CW
C/B-SFCC2 SLAT WTB
EPDC2
2KL06
279100
279100
3223CE
C/B-ACCLRM DAMP LAT1 AFT
CBP1
3218CE
C/B-ACCLRM DAMP LAT2 AFT
279100
3218CE
C/B-ACCLRM DAMP LAT2 AFT
279100
3121CE
279100
3221CE
279100
3221CE
TO
ATA
DEVICE
FIN
275100
275100
278100
278100
278100
279100
3216CE
279100
3216CE
279100
3119CE
279100
3217CE
C/B-ACCLRM DAMP LAT3 AFT
C/B-ACCLRM DAMP VERT1
FWD
C/B-ACCLRM DAMP VERT1
FWD
C/B-ACCLRM DAMP VERT2
FWD
C/B-ACCLRM DAMP VERT2
FWD
C/B-ACCLRM DAMP VERT3
FWD
C/B-ACCLRM LAF VERT1 R
279100
279100
3210CE
C/B-ACCLRM LAF VERT2 L
3212CE
279100
3113CE
TO
ATA
DEVICE
FIN
PROTECTION DEVICE
DESIGNATION
FROM
EQUIPMENT
PHYSICAL
LOCATION
279100
279100
279100
3115CE
C/B-ACCLRM LAF VERT3 R
EPDC1
1KQ04
2001CE
C/B-PRIM 1
EPDC1
3HZ11
2002CE
C/B-PRIM 2
EPDC2
4HZ10
1005CE
C/B-PRIM 3
EPDC1
1KZ10
5AD15
279100
279100
3225CE
C/B-RGAU1
EPDC1
3HB01
CBP2
6AD02
279100
3231CE
C/B-RGAU2
EPDC1
3HB02
CBP2
6AG04
279100
3230CE
C/B-RGAU3
EPDC2
4HA01
EPDC1
1KQ05
CBP1
5AD13
279100
279100
3226CE
3131CE
C/B-RGAU4
C/B-RGAU5
EPDC2
EPDC1
4HA02
1KA06
CBP1
5AK12
279100
279100
2003CE
C/B-SEC 1
EPDC1
3HB05
2004CE
C/B-SEC 2
EPDC2
4HB01
CBP2
6AD04
1007CE
C/B-SEC 3
EPDC1
1KZ12
CBP2
6AG05
279100
282200
3200QC
C/B-APU FUEL LP V
CBP2
6AF06
282200
3206QC
C/B-APU FUEL V RLY
CBP2
6AJ10
EPDC1
1KA04
282200
282300
282300
3202QC
C/B-APU ISOL V
CBP2
6AK14
3201QE
C/B-CROSSFEED V A
CBP1
5AA07
3200QE
C/B-CROSSFEED V B
CBP2
6AE12
282400
282400
3201QG
C/B-LP V MOT1 ENG1
CBP1
5AE01
3200QG
C/B-LP V MOT1 ENG2
CBP2
6AA10
282400
3100QG
C/B-LP V MOT2 ENG1
EPDC2
2KE04
CBP1
5AG12
CBP2
6AD03
C/B-ACCLRM LAF VERT2 R
CBP2
6AD01
C/B-ACCLRM LAF VERT3 L
EPDC1
1KA03
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
CO
&
C/B
Training by Airbus
DEVICE
FIN
PROTECTION DEVICE
DESIGNATION
FROM
EQUIPMENT
PHYSICAL
LOCATION
282400
3101QG
C/B-LP V MOT2 ENG2
EPDC1
1KC03
285100
285100
3201QM
3200QM
C/B-TWDC1 A EMER
C/B-TWDC1 B EMER
CBP1
CBP2
285100
285100
3203QM
C/B-TWDC2 A EMER
3202QM
C/B-TWDC2 B EMER
285100
285100
3205QM
3204QM
291100
3205JG
C/B-G ENG1 FSOV CL/OP
CBP1
5AB01
291100
291100
291100
3209JG
C/B-G ENG1 FSOV CLOSE
CBP1
5AB02
TO
ATA
TO
ATA
DEVICE
FIN
PROTECTION DEVICE
DESIGNATION
FROM
EQUIPMENT
PHYSICAL
LOCATION
5AA08
6AE11
291300
3205JY
C/B-Y ENG1 PUMP XDCR SET2
CBP1
5AB04
291300
3208JY
C/B-Y ENG2 FSOV CL/OP
CBP2
6AB15
CBP1
5AE02
291300
3212JY
C/B-Y ENG2 FSOV CLOSE
CBP2
6AB14
CBP2
6AE10
291300
3203JY
C/B-Y ENG2 PUMP DEPRESS
CBP1
5AE03
C/B-TWDC3 A EMER
CBP1
5AA09
291300
3108JY
C/B-Y ENG2 PUMP XDCR SET1
EPDC2
2KE03
C/B-TWDC3 B EMER
CBP2
6AA09
291300
293100
3207JY
C/B-Y ENG2 PUMP XDCR SET2
CBP1
5AE07
3101JS
C/B-G SYS PRESS XDCR 1
EPDC1
1KL05
3202JS
C/B-G SYS PRESS XDCR 2
CBP2
6AB13
3201JS
C/B-Y SYS PRESS XDCR 1
CBP1
5AB06
3102JS
C/B-Y SYS PRESS XDCR 2
EPDC2
4AD04
1KC05
3202JG
C/B-G ENG1 PUMP DEPRESS
CBP2
6AA05
3105JG
C/B-G ENG1 PUMP XDCR SET1
EPDC1
1KC04
293100
293100
293100
291100
291100
3206JG
C/B-G ENG1 PUMP XDCR SET2
CBP2
6AE08
293200
3101JR
C/B-G RSVR PRESS XDCR
EPDC1
3207JG
C/B-G ENG2 FSOV CL/OP
CBP1
5AE04
293200
3102JR
C/B-Y RSVR PRESS XDCR
EPDC2
4AA03
291100
291100
3211JG
C/B-G ENG2 FSOV CLOSE
CBP1
5AE05
293300
3101JX
C/B-G FLTR CLOG MONIT LH
EPDC1
1KC06
3204JG
C/B-G ENG2 PUMP DEPRESS
CBP2
6AE06
C/B-Y FLTR CLOG MONIT RH
EPDC2
2KE02
3107JG
C/B-G ENG2 PUMP XDCR SET1
EPDC1
1KL04
293300
304200
3104JX
291100
291100
3201DG
C/B-WHC1 PWR SPLY
CBP1
5AH06
3208JG
C/B-G ENG2 PUMP XDCR SET2
CBP2
6AA07
291300
3206JY
C/B-Y ENG1 FSOV CL/OP
CBP2
6AF15
291300
3210JY
C/B-Y ENG1 FSOV CLOSE
CBP2
6AF14
291300
3201JY
C/B-Y ENG1 PUMP DEPRESS
CBP1
5AH12
291300
3106JY
C/B-Y ENG1 PUMP XDCR SET1
EPDC2
2KQ03
304200
304200
3100DG
C/B-WHC2 PWR SPLY
EPDC2
2KF05
3103DG
C/B-WINDOW AFT L PWR SPLY
EPDC1
1FD04
304200
304200
3104DG
C/B-WINDOW AFT R PWR SPLY
EPDC2
2FE06
3101DG
C/B-WINDOW FWD L PWR SPLY
EPDC1
1FB02
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
CO
&
C/B
Training by Airbus
TO
ATA
DEVICE
FIN
PROTECTION DEVICE
DESIGNATION
FROM
EQUIPMENT
PHYSICAL
LOCATION
EPDC2
2FB02
EPDC1
1CD05
304200
3102DG
304500
304500
3201DB
C/B-WINDOW FWD R PWR
SPLY
C/B-WIPER CAPT 115VAC
3100DB
C/B-WIPER F/O 115VAC
EPDC2
2FA04
308100
308100
3101DD
C/B-ICE DET1 115VAC
EPDC1
1FE05
3100DD
C/B-ICE DET2 115VAC
EPDC2
2FD10
311900
3202VM
C/B-ICP AIR & ELEC 2
CBP2
6AF13
311900
3203VM
C/B-ICP ENG START & ECP 1
CBP1
5AB08
311900
311900
3114VM
C/B-ICP ENG START & ECP 2
EPDC2
2KK04
3205VM
C/B-ICP FIRE 1
CBP1
5AE10
311900
3206VM
C/B-ICP FIRE 2
CBP2
6AF12
311900
3207VM
C/B-ICP FUEL & HYD 1
CBP1
5AB09
311900
311900
3209VM
C/B-ICP LOWER CTR 1
CBP1
5AE11
3210VM
C/B-ICP LOWER CTR 2
CBP2
6AF11
311900
311900
3211VM
3212VM
C/B-ICP LOWER L 1
C/B-ICP LOWER L 2
CBP1
CBP2
5AB10
6AB10
311900
311900
3213VM
C/B-ICP LOWER R 1
CBP1
5AF01
3214VM
C/B-ICP LOWER R 2
CBP2
6AF10
311900
311900
3215VM
C/B-ICP MAINTENANCE 1
EPDC1
3HC03
3216VM
C/B-ICP MAINTENANCE 2
CBP2
6AB09
311900
3217VM
C/B-ICP MID L 1
CBP1
5AF02
DEVICE
FIN
311900
3218VM
C/B-ICP MID L 2
CBP2
6AF09
311900
3219VM
3220VM
C/B-ICP MID R 1
C/B-ICP MID R 2
CBP1
CBP2
5AD02
6AA04
3101VM
C/B-ICP NORM1
EPDC1
1KD03
3102VM
C/B-ICP NORM2
EPDC2
2KQ01
3205TU
C/B-CDAU
CBP1
5AF05
3207TU
C/B-FDRS ACCLRM
CBP1
5AF03
311900
311900
311900
313300
313300
PROTECTION DEVICE
DESIGNATION
FROM
EQUIPMENT
PHYSICAL
LOCATION
TO
ATA
313300
316100
3201TU
C/B-SSFDR
EPDC1
1CC03
3107WK
C/B-DU INNER CAPT
EPDC1
1KB01
316100
3207WK
C/B-DU INNER CAPT STBY
CBP1
5AD09
316100
316100
3108WK
C/B-DU INNER F/O
EPDC2
2KG06
3106WK
C/B-DU LOWER CENTER
EPDC2
2KF06
316100
3206WK
C/B-DU LOWER CENTER STBY
CBP2
6AH09
316100
316100
3109WK
C/B-DU OUTER CAPT
EPDC1
1KB03
3110WK
C/B-DU OUTER F/O
EPDC2
2KP04
316100
316100
3105WK
C/B-DU UPPER CENTER
EPDC1
1KP01
3205WK
C/B-DU UPPER CENTER STBY
CBP1
5AH09
316200
3101WT
C/B-KCCU CAPT
EPDC1
1KM01
316200
3201WT
C/B-KCCU CAPT STBY
CBP1
5AF04
316200
3102WT
C/B-KCCU F/O
EPDC2
2KF04
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
CO
&
C/B
Training by Airbus
FROM
EQUIPMENT
PHYSICAL
LOCATION
TO
ATA
DEVICE
FIN
PROTECTION DEVICE
DESIGNATION
316200
3202WT
C/B-KCCU F/O STBY
CBP2
6AF08
316600
3101TE
C/B-CMV1
EPDC1
1KS04
PROTECTION DEVICE
DESIGNATION
FROM
EQUIPMENT
PHYSICAL
LOCATION
TO
ATA
DEVICE
FIN
328100
328100
3201GL
C/B-RBCU1 CHAN-B
CBP1
5AH08
3203GL
C/B-RBCU1 CHAN-E
EPDC1
3HH03
328100
3100GL
C/B-RBCU2 CHAN-A
EPDC2
2KD05
3200GL
C/B-RBCU2 CHAN-B
CBP2
6AH08
316600
3202TE
C/B-CMV2
CBP2
6AK08
323100
3103GA
C/B-L/G CTL LEVER SYS1
EPDC1
1KM02
323100
323300
323300
3102GA
3201GF
C/B-L/G CTL LEVER SYS2
C/B-AECM-A SPLY1
EPDC2
CBP1
2KJ06
5AH15
328100
328100
3202GL
C/B-RBCU2 CHAN-E
EPDC2
4HJ03
C/B-AECM-B SPLY1
C/B-L NBSELV RELAY S1
CBP2
EPDC1
6AC01
1KM03
3107GL
C/B-WRDC NLG
EPDC1
1KM06
324200
3200GF
3101GG
328100
328100
3109GL
C/B-WRDC1 L MLG
EPDC1
1KD06
324200
3100GG
C/B-L NBSELV RELAY S2
EPDC2
2KJ05
3111GL
C/B-WRDC1 R MLG
EPDC1
1KE01
324200
324200
3103GG
C/B-R NBSELV RELAY S1
EPDC1
1KD04
328100
328100
3110GL
C/B-WRDC2 L MLG
EPDC2
2KG05
3102GG
C/B-R NBSELV RELAY S2
EPDC2
2KF03
328100
3112GL
C/B-WRDC2 R MLG
EPDC2
2KB04
324300
324300
3101GY
C/B-ABSELV RELAY S1
EPDC1
1KM05
331200
3101LE
C/B-CKPT LT CAPT
EPDC1
1KR04
3100GY
C/B-ABSELV RELAY S2
EPDC2
2KJ04
331200
3201LE
C/B-CKPT LT EMER
EPDC1
3HD05
324300
3200GY
C/B-G BRK ACCU PRESS XDCR
EPDC2
4HJ04
3100LE
C/B-CKPT LT F/O
EPDC2
2KM02
324300
3201GY
C/B-Y BRK ACCU PRESS XDCR
EPDC1
3HH04
331200
331200
3107LE
C/B-OUTLET 115V/400HZ
EPDC1
1JB06
324400
324400
3201GZ
3200GZ
C/B-PARK BRK CTL S1
C/B-PARK BRK CTL S2
EPDC1
EPDC2
3HJ03
4HK03
331200
3105LE
C/B-OUTLET 28VDC
EPDC1
3AD04
331300
331400
3101LF
C/B-DIM CTL UNIT&INTEG LT
EPDC1
1KN02
3101LP
C/B-ANN LTG RELAY DC 1
EPDC1
1KE02
3102LP
C/B-ANN LTG RELAY DC 2
EPDC2
2KB03
3202LP
3215FP
C/B-ANN LTG RLY DC 2 EMER
C/B-ADIRU 1& 3 SWTG DC
CBP2
CBP1
6AA01
5AE15
324400
325100
3100GZ
C/B-PARK BRK RELAY S2
EPDC2
2KB02
3101GC
C/B-N/WS XMTR UNIT CAPT
EPDC1
1KD05
325100
328100
3100GC
3101GL
C/B-N/WS XMTR UNIT F/O
C/B-RBCU1 CHAN-A
EPDC2
EPDC1
2KF01
1KK04
331400
331400
341100
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
CO
&
C/B
Training by Airbus
PROTECTION DEVICE
DESIGNATION
FROM
EQUIPMENT
PHYSICAL
LOCATION
TO
ATA
DEVICE
FIN
341100
3203FP
C/B-ADIRU1
CBP1
341100
3201FP
C/B-ADIRU1 BKUP
EPDC1
341100
3100FP
C/B-ADIRU2
EPDC2
2KL05
341100
3114FP
C/B-ADIRU2 BKUP
EPDC2
4AF07
341100
341100
3102FP
C/B-ADIRU2 PROBE PWR SPLY
EPDC2
2KD03
3206FP
C/B-ADIRU3
CBP2
6AB07
PROTECTION DEVICE
DESIGNATION
FROM
EQUIPMENT
PHYSICAL
LOCATION
3131FC
C/B-STBY STAT L ANTI ICE
EPDC1
1FD01
3133FC
C/B-STBY STAT R ANTI ICE
EPDC1
1FE04
5AF06
TO
ATA
DEVICE
FIN
3HK03
342200
342200
343600
343600
341100
3204FP
C/B-ADIRU3 BKUP
EPDC2
4HJ01
341100
3101FP
C/B-AOA PROBE ANTI ICE
EPDC1
1FD07
341100
3103FP
C/B-AOA PROBE PWR SPLY
EPDC1
1KB05
341100
341100
3221FP
C/B-ISP1 ANTI ICE
EPDC1
1CB05
3112FP
C/B-ISP2 ANTI ICE
EPDC2
2JA04
341100
341100
3220FP
C/B-ISP3 ANTI ICE
EPDC2
2CE01
3219FP
C/B-MFP1 ANTI ICE
EPDC1
1CC06
341100
3104FP
C/B-MFP2 ANTI ICE
EPDC2
2JA07
341100
3216FP
C/B-MFP3 ANTI ICE
EPDC2
2CB06
341100
341100
3217FP
C/B-SSA1 ANTI ICE
EPDC1
1CE06
3108FP
C/B-SSA2 ANTI ICE
EPDC2
2JA03
341100
3218FP
C/B-SSA3 ANTI ICE
EPDC2
2CD02
342200
3201FC
C/B-ISIS IND1 28VDC EMER
EPDC1
3HA04
342200
342200
3202FC
3221FC
C/B-ISIS IND2 28VDC EMER
C/B-STBY PITOT ANTI ICE
CBP2
EPDC1
6AD15
1CB04
3101RT
C/B-MMR1
EPDC1
1JA03
3102RT
C/B-MMR2
EPDC2
2JA05
343600
3102RT
C/B-MMR2
EPDC2
2JA06
344200
344200
344200
3201SA
C/B-RA 1
EPDC1
1CE05
3102SA
C/B-RA 2
EPDC2
2FA06
3101SA
C/B-RA 3
EPDC1
1FC03
345100
3101SD
C/B-DME 1
EPDC1
1FC04
345100
345500
345500
3102SD
C/B-DME 2
EPDC2
2FE07
3101RS
3102RS
C/B-VOR1
C/B-VOR2
EPDC1
EPDC2
1FC07
2FE10
347100
3103SE
C/B-AESU1 (WXR + TAWS)
EPDC1
1JA03
347100
3101SE
C/B-AESU1 (XPDR + TCAS)
EPDC1
1JA05
347100
3104SE
C/B-AESU2 (WXR + TAWS)
EPDC2
2JA06
347100
421100
3102SE
C/B-AESU2 (XPDR + TCAS)
EPDC2
2JA02
3205TF
C/B-CPIOM H31
CBP1
5AF10
421100
421100
3108TF
C/B-CPIOM H42
EPDC2
4AC07
3103TF
C/B-CPIOM H43
EPDC1
1KR05
421100
3110TF
C/B-CPIOM H44
EPDC2
2KL02
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
CO
&
C/B
Training by Airbus
TO
ATA
DEVICE
FIN
PROTECTION DEVICE
DESIGNATION
FROM
EQUIPMENT
PHYSICAL
LOCATION
421100
3107TF
C/B-CPIOM H61
EPDC1
1KR06
TO
ATA
DEVICE
FIN
PROTECTION DEVICE
DESIGNATION
421100
421100
3114TF
C/B-CPIOM H62
EPDC2
2KL03
424100
3134TS
C/B-CRDC B02 DSO GP1
EPDC2
2KJ03
3109TF
C/B-CPIOM H63
EPDC1
1KH05
C/B-CRDC B02 DSO GP2
EPDC2
2KC01
3116TF
C/B-CPIOM H64
EPDC2
2KL01
424100
424100
3136TS
3138TS
C/B-CRDC B02 DSO GP3
EPDC2
2KJ02
3116TS
C/B-CRDC B04
EPDC2
4AA04
C/B-CRDC B05 DSO GP3
EPDC1
1KF05
421100
423100
FROM
EQUIPMENT
PHYSICAL
LOCATION
3211TH
C/B-AFDX SW 11
EPDC1
3HC02
424100
423100
423100
3212TH
C/B-AFDX SW 12
EPDC2
4HC03
424100
3145TS
3213TH
C/B-AFDX SW 13
EPDC1
3HD02
C/B-CRDC B09 DSO GP2
CBP1
5AF08
3214TH
C/B-AFDX SW 14
EPDC2
4HC04
424100
441100
3227TS
423100
3122RH
C/B-DEU-A CTR FWD ESS
EPDC2
4AD07
423100
3215TH
C/B-AFDX SW 15
EPDC1
3HC01
441100
3124RH
C/B-DEU-A CTR MID ESS
EPDC2
4AC06
423100
3216TH
C/B-AFDX SW 16
EPDC2
4HC05
441100
3226RH
C/B-DEU-A CTR1 AFT EMER
EPDC2
4HG03
423100
3219TH
C/B-AFDX SW 19
EPDC1
3HD03
441100
3126RH
C/B-DEU-A CTR1 AFT ESS
EPDC2
4AC05
424100
424100
3201TS
C/B-CRDC A01
CBP1
5AB15
441100
3222RH
C/B-DEU-A CTR1 FWD EMER
EPDC2
4HF04
3101TS
C/B-CRDC A03
EPDC1
1KR01
441100
3228RH
C/B-DEU-A CTR2 AFT EMER
EPDC2
4HG04
424100
3103TS
C/B-CRDC A05
EPDC1
1KA02
C/B-DEU-A CTR2 AFT ESS
EPDC2
4AB02
3106TS
C/B-CRDC A06
EPDC2
2KC05
3224RH
C/B-DEU-A CTR2 FWD EMER
EPDC2
4HE03
424100
3105TS
C/B-CRDC A07 BKUP
EPDC1
1KP02
441100
441100
441100
3128RH
424100
3111RH
C/B-DEU-A L FWD ESS
EPDC1
3AB04
424100
3107TS
C/B-CRDC A09
EPDC1
3AD01
3113RH
C/B-DEU-A L MID ESS
EPDC1
3AC03
424100
3110TS
C/B-CRDC A10 BKUP
EPDC2
2KG04
424100
3109TS
3113TS
C/B-CRDC A11
C/B-CRDC A15
EPDC1
EPDC1
1KA01
1KN06
441100
441100
441100
441100
3215RH
3115RH
C/B-DEU-A L1 AFT EMER
C/B-DEU-A L1 AFT ESS
EPDC1
EPDC1
3HF05
3AB03
3211RH
C/B-DEU-A L1 FWD EMER
EPDC1
3HE05
3114TS
C/B-CRDC B02
EPDC2
2KG02
441100
3217RH
C/B-DEU-A L2 AFT EMER
EPDC1
3HG01
424100
424100
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
CO
&
C/B
TO
ATA
DEVICE
FIN
PROTECTION DEVICE
DESIGNATION
FROM
EQUIPMENT
PHYSICAL
LOCATION
441100
441100
3117RH
3213RH
C/B-DEU-A L2 AFT ESS
C/B-DEU-A L2 FWD EMER
EPDC1
EPDC1
3AC02
3HE04
441100
441100
3112RH
3114RH
C/B-DEU-A R FWD ESS
C/B-DEU-A R MID ESS
EPDC2
EPDC2
4AC03
4AC04
441100
441100
441100
441100
441100
441100
441100
441100
441100
441100
441100
441100
441100
441100
441100
3216RH
3116RH
C/B-DEU-A R1 AFT EMER
C/B-DEU-A R1 AFT ESS
EPDC2
EPDC2
4HE02
4AB04
3212RH
3218RH
C/B-DEU-A R1 FWD EMER
C/B-DEU-A R2 AFT EMER
EPDC2
EPDC2
4HG01
4HG02
3118RH
3214RH
C/B-DEU-A R2 AFT ESS
C/B-DEU-A R2 FWD EMER
EPDC2
EPDC2
4AA07
4HE01
3243RH
3143RH
C/B-DEU-B L AFT EMER
C/B-DEU-B L AFT ESS
EPDC1
EPDC1
3HE03
3AA01
3241RH
3141RH
C/B-DEU-B L FWD EMER
C/B-DEU-B L FWD ESS
EPDC1
EPDC1
3HF04
3AC06
3247RH
3147RH
C/B-DEU-B L2 AFT EMER
C/B-DEU-B L2 AFT ESS
EPDC1
EPDC1
3245RH
3145RH
3244RH
C/B-DEU-B L2 FWD EMER
C/B-DEU-B L2 FWD ESS
C/B-DEU-B R AFT EMER
441100
3144RH
C/B-DEU-B R AFT ESS
EPDC1
EPDC1
EPDC2
EPDC2
3HG02
3AB02
3HE02
3AA02
4HF01
4AB05
441100
441100
441100
3242RH
3142RH
3201RH
C/B-DEU-B R FWD EMER
C/B-DEU-B R FWD ESS
C/B-DIR1 EMER
EPDC2
EPDC2
EPDC1
4HE04
4AB07
3HF01
Training by Airbus
TO
ATA
DEVICE
FIN
PROTECTION DEVICE
DESIGNATION
FROM
EQUIPMENT
PHYSICAL
LOCATION
441100
3101RH
C/B-DIR1 ESS
EPDC1
3AB05
441100
441100
441100
3202RH
3102RH
C/B-DIR2 EMER
C/B-DIR2 ESS
EPDC2
EPDC2
4HE05
4AD06
3251RH
C/B-FAP DR1 EMER
EPDC1
3HE01
441100
441100
3151RH
C/B-FAP DR1 ESS
EPDC1
3AB06
3253RH
C/B-FAP DR2 EMER
EPDC1
3HG03
441100
454500
461100
461100
461100
494100
494100
525100
715100
3153RH
C/B-FAP DR2 ESS
EPDC1
3AC05
3202TC
3201TL
C/B-OSFC EMER
C/B-SCI-1
EPDC2
EPDC1
2CA04
1CA04
3102TL
3102TL
3101KA
3200KA
3101MQ
3107KS
C/B-SCI-2
C/B-SCI-2
C/B-POR APU
C/B-SGCU BKUP SPLY
C/B-CDLCU
C/B-A/C PERMISSION DSCRT1
EPDC2
EPDC2
EPDC1
CBP2
EPDC1
EPDC1
2FD05
2FD08
1DA01
6AD06
1KB02
1KQ03
715100
3108KS
EPDC2
2KN05
715100
715100
732100
732100
741100
741100
3201KS
3202KS
3201KC
C/B-A/C PERMISSION DSCRT2
C/B-EEC1 CHAN-A
C/B-EEC2 CHAN-A
C/B-HP FUEL SOV ENG1
EPDC1
EPDC2
CBP1
1CA03
2CE01
5AG06
3202KC
3201EH
3202EH
C/B-HP FUEL SOV ENG2
C/B-IGN SYS A ENG1
C/B-IGN SYS A ENG2
CBP2
EPDC1
EPDC2
6AH04
1CE06
2CA02
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
CO
&
C/B
Training by Airbus
AVIONICS
ELECTRO-AVIONICS SYSTEMS
ATA 24 - ELECTRICAL POWER
P. 70
ATA 42 - INTEGRATED MODULAR AVIONICS AND AVIONICS DATA COMMUNICATION NETWORK
P. 101
ATA 31 - INDICATING / RECORDING SYSTEMS
P. 109
ATA 46 - INFORMATION SYSTEMS
P. 126
ATA 45 - ONBOARD MAINTENANCE SYSTEM
P. 154
ATA 34 - NAVIGATION
P. 178
ATA 22 - AUTO FLIGHT
P. 209
ATA 23 - COMMUNICATIONS
P. 215
ATA 44 - CABIN SYSTEMS
P. 240
ATA 33 - LIGHTS
P. 247
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
ATA 24
ELECTRICAL POWER
ELECTRICAL SYSTEM - GENERAL
VFG 1A
GLC1B
GLC1A
ASAC
RAT
MODULE
APU S/G
ATA49
VFG 1B
AGLC
BTC
1A
230 VAC
AC 1A
SIC1
BTC3
BTC
1B
230 VAC
230 VAC
AC 1B
ENEC1 AC EMER 1
ATUC
1A
ATUC
1B
TR
1
ATU
1A
BTAC
1B
ESTAC1
28 VDC
DC1 SGSC
1
RTNC1
RTBC1
EFCC1
28 VDC
DC
F/CTL 1
28 VDC
DC SHED
GS 1
28 VDC
DC NORM
BAT1
BAT
1
ASDC1
RLCE1
ETOPS
AC1
EMER
TR 1
STATIC
INVERTER
1
28 VDC
DC PDMI 1
ESTC1
EMER SIDE
1
ETLC1
28 VDC
DC EMER 1
PDMIC
1
EMER
TR 2
SPU
EBATLC1
ESEC3
28 VDC
DC EVAC 1
EMER
BAT 1
ETLC2
EBTDC
EBATLC2
ESEC4
115 VAC AC
EMER 2
EFCC
2 28 VDC
28 VDC
DC EMER 2
BTC
2B
230 VAC
AC 2B
BTC2A
230 VAC
AC 2A
ATUC
2A
ATUC2B
EMER
ATU 2
SGCU
115 VAC
INV AC2
FCC1
BATLC1
EBTC2
EBTC1
230 VAC
AC EMER 2 ENEC2
EATULC2
115 VAC AC
EMER 1
115 VAC
AC 1B
TLC1
BTAC
1A
EGLC
EATULC1
ATULC
1B
NOTE
GLC2A
SIC2
BTC4
EMER
ATU 1
ATU
1B
ATULC
1A
115 VAC
AC 1A
GLC2B
SLC
Training by Airbus
VFG 2A
VFG 2B
TR
2
ATU
2B
ATULC2B
115 VAC
AC 2B
ATULC2A
TLC2
BTAC
2A
FCC2
28 VDC
DC SHED
SGSC
GS 2
2
RTNC2
28 VDC
DC PDMI 2
28 VDC
DC EVAC 2
EMER EMER SIDE
BAT 2
2
115 VAC
AC 2A
BTAC2B
DC
F/CTL 2
PDMIC
2
ATU
2A
28 VDC
DC NORM
BAT2
28 VDC
DC2
BATLC2
RTBC
2
ASCD2
BAT
2
BTDC
MAIN NETWORK SIDE 2
REIC1
EPLC1
REIC2
SIC3
EXT PWR RCPT 1
SIC4
EPLC2
ETOPS
AC2
RLCE2
MAIN NETWORK SIDE 2
EXT PWR RCPT 2
Page 70
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
ELECTRICAL SYSTEM - CONTROLS
ELEC
BAT
OFF
REMOTE
C/B CTL
EMER 2
ON
EMER 1
1
2
Training by Airbus
TOWING ON BAT
POWER
26.8
88.8
8
8
ON
CHARGE
HIGH
MED
LOW
NOTE
225 VM
BAT 1
E
L
E
C
BAT EMER 1 BAT EMER 2
FAULT
FAULT
FAULT
OFF
OFF
OFF
SIDE 1 & 2
BAT 2
FAULT
ISOL
OFF
ELM
PAX SYS
FAULT
ISOL
OFF
OFF
GALLEY
OFF
COMMERCIAL
1
2
OFF
OFF
FAULT
FAULT
EXT 1
FAULT
FAULT
APU GEN
FAULT
FAULT
EXT 2
E
L
2A
DRIVE
E
GEN
C
FAULT
FAULT
DISC
OFF
AVAIL
DISC
OFF
FAULT
DISC
OFF
AVAIL
DISC
AC 1B BUS
AC 1A BUS
DRIVE
1A
DRIVE
GEN
1B
BUS TIE
OFF
GEN
ON
A
U
T
O
DRIVE
2B
GEN
OFF
ON
OFF
T.O
CONFIG
AC 2A BUS
AC 2B BUS
EMER
CANC
DEFRD
ABN
RCL
LAST
RCL
ALL
DISPCH
MORE
STS
SD
ENG
DOOR
WHEEL
FUEL
EL/AC
EL/DC
HYD
F/CTL
APU
BLEED
COND
PRESS
VIDEO
VIDEO
CLEAR
ALL
CLEAR
Page 71
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
ELECTRICAL SYSTEM - INDICATING
Training by Airbus
AC PAGE
DC PAGE
ELEC DC
ELEC AC
115
AC EMER 1
230
115
AC 1 A
230
115
AC EMER 2
230
TR
EMER 1
TR
EMER 2
115
AC 1 B
230
115
AC 2 B
230
BAT 1
27 V
8A
115
AC 2 A
230
TR 2
TR 1
GEN 1A
34 %
230 V
NOTE
GEN 1B
34 %
230 V
GEN 2B
34 %
230 V
GEN 2A
34 %
230 V
DC 1
BAT EMER 1
BAT EMER 2
DC EMER 1
DC EMER 2
27 V
8A
27 V
8A
STAT
INV
BAT 2
27 V
8A
DC 2
TR 1
TR EMER 1
TR EMER 2
TR 2
AC 1A
AC EMER 1
AC EMER 2
AC 2A
28 V
15 A
28 V
15 A
28 V
15 A
28 V
15 A
Page 72
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
EXTERNAL POWER - MANAGEMENT & INTERFACE
EXT 2
EXT 1
EPCU PROTECTION FUNCTIONS:
OVER/UNDERVOLTAGE
OPEN PHASE
OPEN NEUTRAL
UNDER/OVERFREQUENCY
INCORRECT PHASE SEQUENCE
LIGHT
TEST
AVAIL
AVAIL
AUTO
AUTO
AFDX NETWORK
EXT PWR 1
AVAIL
EXT PWR 1
NOT IN USE
EXT PWR 2
AVAIL
EXT PWR 2
NOT IN USE
Training by Airbus
115
AC EMER 1
230
115
AC EMER 2
230
EXT1
TR
EMER 1
TR
EMER 2
EXT 2
115
AC 1 A
230
115
AC 1 B
230
115
AC 2 B
230
115
AC 2 A
230
115 V
400 HZ
GEN 1B
GEN 2B
ELEC AC PAGE
VOLTAGE
EDMU
EPCU1
1A
1B
BITE
GEN 2A
VOLTAGE
EPDC
TR 2
TR 1
GEN 1A
115 V
400 HZ
LOAD
CDS
ELEC AC
SHEDDING
1925VU
925VU
NOTE
ENMU
ENMF
1A
CPIOM
ELMF
1B
SIDE 1
TO AC MAIN
NETWORK EPLC1
SIDE 2
VOLTAGE/FREQUENCY
MEASUREMENT
CT
POR
1
2
EXTERNAL POWER RECEPTACLES
CURRENT
MEASUREMENT
Page 73
FWD
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
APU GENERATION DESCRIPTION & INTERFACE
SG PROPERTIES:
MAXIMUM POWER RATING OF
150 kVA ON GROUND
THREE-PHASES
230VAC
CONSTANT FREQUENCY
CDS
62 %
115 V
400 HZ
ELMF
AC
115
AC EMER 1
230
TR
APU FU EMER
5001
NOTE
CPIOM
AVAIL
GEN
ELEC
115
BLEED
AC
EMER
PSI 2
46
230
TO AC MAIN
NETWORK
APU
APU STARTER
GENERATOR
TR
EMER 2
KG
10
N
0
100115%
115
AC 1 B
230
AC 1 A
230
115
AC 2 B
230
115
AC 2 A
230
GEN 2B
GEN 2A
TR 2
TR 1
5
GENERATE MODE
MAIN
GENERATOR
Training by Airbus
AFDX NETWORK
0
7
9
EGT
GEN 1A
545
°C
GEN 1B
APU GEN
110 %
115 V
400 HZ
A
CRDC
EPDC1
APU PAGE
ELEC AC PAGE
POR
CT
ECB
AGLC
CT
SGCU
CONTROL AND PROTECTION
EXCITER
GENERATOR
PERMANENT
MAGNET
GENERATOR
ELECTRICAL
NETWORK
VOLTAGE REGULATION
ENMU
POWER SUPPLY
OR
POWER READY
ENMF
1A
1B
A
INTERFACE
APU GEN
APU
FAULT
OFF
ELEC PANEL
FIRE PANEL
SGCU PROTECTION FUNCTIONS:
OVER/UNDERVOLTAGE
OVER/UNDER FREQUENCY
OVER CURRENT
FEEDER DIFFERENTIAL PROTECTION
OPEN CABLE
Page 74
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
VFG DESCRIPTION
Training by Airbus
TENSION BOLT
NOTE
2 VFGs FOR EACH ENGINE
100 kVA
230VAC
VARIABLE FREQUENCY (360Hz TO 800Hz)
INTERCHANGEABLE VFGs
V-BAND CLAMP
MOUNTING BOLTS
V-BAND FLANGE
VFG DISCONNECT MECHANISM OVERVIEW
VFG DISCONNECTION
MANUAL DRIVE GUARDED P/BSW TO ENERGIZE
SOLENOID
AUTOMATIC : THERMAL DEVICE
DRIVE
FAULT
DISC
DIS
SC
THERMAL (METAL ALLOY)/
ELECTRIC ACTUATING
SOLENOID
RESET
HANDLE
Page 75
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
VFG GENERATION MANAGEMENT & INTERFACE
Training by Airbus
AFDX NETWORK
115
AC 1 A
230
CPIOM
CDS
115
AC EMER 1
230
115
AC EMER 2
230
TR
EMER 1
TR
EMER 2
115
AC 1 B
230
115
AC 2 B
230
115
AC 2 A
230
GEN 1B
54 %
230 V
GEN 2B
54 %
230 V
GEN 2A
54 %
230 V
ELMF
C
B
TR 2
TR 1
GEN 1A
54 %
230 V
CRDC
ELEC AC PAGE
EPDC1
VFG
MAIN
GENERATOR
POR
CT
CT
GLC
GCU
CONTROL AND
PROTECTION
EXCITER
GENERATOR
EDMU
OPU
GLC
CONTROL
D
GLC CONTROL
PERMANENT
MAGNET
GENERATOR
VOLTAGE
REGULATION
A
1A
1B
ELECTRICAL
NETWORK
NOTE
TO AC MAIN
NETWORK
ELEC AC
OR
C
B
GCU PROTECTION FUNCTIONS:
OVER/UNDERVOLTAGE
OVER/UNDERFREQUENCY
OVER CURRENT
FEEDER DIFFERENTIAL PROTECTION
OPEN CABLE
POWER
SUPPLY
EXCITER GEN
SUPPLY
1A
1B
POWER
READY
D
A
INTERFACE
1A
1B
ENMU
ENMF
1A
1B
1A
1B
ENG 1
DRIVE
GEN
FAULT
FAULT
DISC
DIS
SC
OFF
SIDE 1 SHOWN
SIDE 2 SYMMETRICAL
Page 76
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
TRANSFORMER RECTIFIERS
Training by Airbus
AVIONICSVENTILATION
AFDX NETWORK
(NO VENTILATION FOR EMER TR )
POWER RATING: 155A
ELEC DC
BAT 1
27 V
8A
DC 1
CDS
BAT EMER 1
BAT EMER 2
DC EMER 1
DC EMER 2
27 V
8A
STAT
INV
27 V
8A
STAT
INV
CRDC
27 V
8A
DC 2
TR EMER 1
TR EMER 2
28 V
15 A
28 V
15 A
AC 1A
AC EMER 1
AC EMER 2
AC 2A
28 V
15 A
SIDE 1 SHOWN
SIDE 2 SYMMETRICAL
BAT 2
TR 1
28 V
15 A
NOTE
TR (EMERGENCY TR)
TR 2
ELEC DC PAGE
TR1 / EMERGENCY TR1
AC/DC CONVERSION
TR FAILURE DETECTION
OVERCURRENT PROTECTION
EPDC1
TLC1 /
ETLC1
28VDC BUSBAR DC1
/ EMER1
TLC / ETLC CONTROL
INTERFACE
230VAC BUSBAR AC 1A
/ AC EMER1
FROM EPGS
TR1 /
EMER
TR1
RESET PANEL
Page 77
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
BATTERIES
Training by Airbus
AFDX NETWORK
FWS
ELEC DC
BAT 1
27 V
8A
CRDC
CDS
BAT EMER 1
BAT EMER 2
DC EMER 1
DC EMER 2
27 V
8A
STAT
INV
DC 1
27 V
8A
STAT
INV
27 V
8A
DC 2
TR 1
TR EMER 1
TR EMER 2
28 V
15 A
28 V
15 A
AC 1A
AC EMER 1
AC EMER 2
AC 2A
28 V
15 A
28 V
15 A
SIDE 1 SHOWN
SIDE 2 SYMMETRICAL
BATTERIES FUNCTIONS:
APU START
NBPT
REFUELING
TOWING (BAT1 ONLY)
BAT 2
TR 2
ELEC DC PAGE
CMS
BATTERY 1
EPDC1
ASDC1
BMU 1
HOT BUS 1
CURRENT
BATLC1
SHUNT
NOTE
APU
Starter Power Unit
(SPU)
TR1
A
TLC1
28VDC DC1 BUS
VOLTAGE
TEMPERATURE
RTBC1
28VDC NORM/BAT1 BUS
TO SUPPLY
REFUEL AND TOWING
SYSTEMS
BAT1 FAILURE
BAT OVERDISCHARGE
REFUEL ON BAT
APU START
ENMU
A
1.A
1.B
FAULT
OFF
BAT
B
OFF
EMER 2
1
EMER 1
2
26.8
88.8
8
8
ELEC PANEL
TOWING ON BAT
POWER
BAT 1
ON
MAINTENANCE PANEL
REFUEL ON BAT
0123456789
BAT PANEL
INTEGRATED REFUEL PANEL
Page 78
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
BATTERY DESCRIPTION
Training by Airbus
AIRCRAFT SKIN
NOTE
BATTERY 1
VENTURI NOZZLE
VENTILATION PIPE
AVIONICS BAY - LEFT HAND SIDE
HANDLING STRAP
COVER
POWER CONNECTOR
LATCH
VENTING HOLE
SIGNAL CONNECTOR
SIDE 1 SHOWN
SIDE 2 SYMMETRICAL
BATTERY PROPERTIES:
NICKEL CADMIUM TECHNOLOGY
NOMINAL VOLTAGE OF 24 VDC
CAPACITY OF 50 Ah
WEIGHT OF 42.5 kg
Page 79
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
RAT DEPLOYMENT AND GENERATOR HEATING
Training by Airbus
EMER ELEC PWR
RAT MAN ON
RAT MODULE
EMER GEN
FAULT
DEPLOYMENT SOLENOID
A
U
T
O
EMER HOT BUS 2
AUTO SOLENOID
EPDC1
EMER HOT BUS 1
CBP2
EPDC2
SSPC
AC BUS
115VAC
WARNING
RAT STOWED
OR
2
AND
1
AND
AUTO/MANUAL SOLENOID
GENERATOR HEATER
NOTE
EPDC2
LMES
IN FLIGHT
TEFO
IN FLIGHT
RAT can be deployed on ground even on a
de-energized aircraft (EMER HOT BUS 2):
Put a safety pin in place before maintenance
operation.
Page 80
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
RAT GENERATOR MANAGEMENT - INTERFACE
Training by Airbus
AFDX NETWORK
ELEC AC
CDS
115
AC EMER 1
230
CRDC
115
AC EMER 2
230
TO AC
EMERGENCY
NETWORK
A/C SYSTEMS
RAT
110 %
230 V
RAT
GENERATOR
MAIN
GENERATOR
CT
EXCITER
GENERATOR
PERMANENT
MAGNET
GENERATOR
AC 1 A
AC 1 B
AC 2 B
AC 2 A
GEN 1A
%
V
GEN 1B
%
V
GEN 2B
%
V
GEN 2A
%
V
NOTE
EPDC2
ELEC AC PAGE
A
FLIGHT/GROUND
B
POR
EGLC
CT
RAT GCU
CONTROL AND PROTECTION
VOLTAGE REGULATION
POWER READY
POWER READY
EENMU
EENMF
BITE
ELECTRICAL
NETWORK
GCU PROTECTION FUNCTIONS:
OVER/UNDERVOLTAGE
DIFFERENTIAL CURRENT
OVERCURRENT
INTERFACE
B
A
PROTECTION INHIBIT
SIGNAL
EMER ELEC PWR
RAT MAN ON
EMER GEN
FAULT
A
U
T
O
Page 81
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
RAT STOWAGE COMPONENTS DESCRIPTION
Training by Airbus
NOTE
ACTUATOR
PRESSURE SWITCH
STOWED
SWITCH
RAT STOW PANEL
RAT STOW
RAT ACTUATOR SOLENOID VALVE
Page 82
RAT DEPLOYED
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
RAT STOWAGE - STOW PANEL DESCRIPTION & RETRACTION SEQUENCE DESCRIPTION
RAT STOWED
LAMP
ACTUATOR
PRESSURE
WARNING LAMP
NOTE
28VDC
VDC
GUARDED
ED POWER
SWITCH
WITCH
COMBINED
STOW/LAMP TEST
SWITCH
STOW PANEL
GREEN SYSTEM PRESSURIZED
28VDC POWER SWITCH ON
RAT BLADES ALIGNED
STOW/LAMP TEST SWITCH TO
STOW POSITION
ELECTRICALPOWER
POWERSUPPLIES
SUPPLIES
ELECTRICAL
28VDC
28VDC
RAT STOWED
AND
RAT STOWAGE
WARNING
STOW
STOW PANEL
PANEL
HYDRAULICPOWER
HYDRAULIC
POWERSUPPLIES
SUPPLIES
GREEN
GREEN HYDRAULIC
HYDRAULICSYSTEM
SYSTEM
Training by Airbus
STOW
STOW SOLENOID
SOLENOIDVALVE
VALVE
If the STOW switch is
released during the
retraction, RAT extends
again immediately.
Page 83
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
EMERGENCY BATTERY
Training by Airbus
AFDX NETWORK
FWS
CDS
ELEC DC
BAT 1
27 V
8A
CRDC
BAT EMER 1
BAT EMER 2
DC EMER 1
DC EMER 2
DC 1
27 V
8A
STAT
INV
27 V
8A
STAT
INV
27 V
8A
DC 2
TR 1
TR EMER 1
TR EMER 2
28 V
15 A
28 V
15 A
AC 1A
AC EMER 1
AC EMER 2
AC 2A
28 V
15 A
28 V
15 A
EMER BATTERIES FUNCTIONS:
PDMI
EVACUATION
NBPT
SUPPLY LOADS IN EMERGENCY
BAT 2
TR 2
EPDC1
ELEC DC PAGE
CMS
NOTE
ESTC1
INV AC 1 BUS
EMERGENCY
BMU 1
A
PDMIC1
TO SUPPLY
PDMI
SYSTEM
STATIC INVERTER
DC PDMI 1 BUS
CURRENT
SHUNT
ESEC3
VOLTAGE
TO SUPPLY CIDS
FOR EVACUATION
DC EMER EVAC 1 BUS
TEMPERATURE
EMER HOT BUS 1
EMERGENCY
BATTERY 1
EBATLC1
ETLC1
28VDC DC EMER 1 BUS
BAT EMER 1 FAILURE
BAT OVERDISCHARGE
EENMU
BAT EMER 1
BAT
B
OFF
EMER 2
1
EMER 1
2
FAULT
2
6.8
88.8
8
8
0123456789
MAINTENANCE PANEL
SIDE 1 SHOWN
SIDE 2 SYMMETRICAL
OFF
A
EMERGENCY
TR1
ELEC
REMOTE
C/B CTL
“ARM” OR “ON”
1.A
1.B
HORN
ELEC PANEL
ON
MAINTENANCE
PANEL
Page 84
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
COMPONENTS LOCATION
Training by Airbus
NOTE
EPGS
CABIN
SPDBs
2 EPDCs
2 CBPs
EPDCs
CBPs
12 SPDBs
CARGO SPDBs
CABIN SPDBs
CABIN
SPDBs
CABIN SPDBs
CARGO SPDBs
Page 85
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
EPDS DESCRIPTION
Training by Airbus
EPDS1
EPDC1
PRIMARY DISTRIBUTION
C/Bs
RCCBs
SECONDARY
DISTRIBUTION
SSPCs
SIDE 1 SHOWN
SIDE 2 SIMILAR
C/Bs
Contactors
TECHNICAL LOADS
> 15A
NOTE
TECHNICAL LOADS
≤ 15 A
EMERGENCY
DISTRIBUTION
RCCBs
Contactors
EMERGENCY LOADS
CBP1
SSPCs
6 SPDBs
SECONDARY
DISTRIBUTION
C/Bs
CABIN & CARGO LOADS
≤ 15 A
SSPCs
Page 86
...
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
EPDC (COMPONENTS LOCATION)
C/Bs
EDMUs
LPUs
RCCBs
EENMUs
ENMUs
C/Bs
NOTE
EDIU
EPCU
ATUPU
ELPU
CONTACTORS
Training by Airbus
SRPUs
CONTACTORS
SSPCs
EPDC1 (INBOARD FACE)
FUNCTIONS OF THE EPDC CARDS:
EPDC1
CONTACTORS
C/Bs
C/Bs
SSPCs
C/Bs
RCCBs
ENMU/EENMU: MANAGEMENT AND
PROTECTION OF ELECTRICAL
DISTRIBUTION OF THE PRIMARY /
EMERGENCY DISTRIBUTION PART
EDMU: ELECTRICAL LOADS
MANAGEMENT AND INTERFACE WITH
THE AFDX NETWORK
LPU AND ELPU: LIGHTNING OR
ELECTRICAL DAMAGE PROTECTION
ATUPU: PROTECTION OF THE ATUs
SRPU AND EPU: EPDS COMPONENTS
POWER SUPPLY
EPCU: EXTERNAL POWER PROTECTION
EDIU: PROTECTION AND/OR SWITCHING
DEVICES STATUS AND CONTRO
CONTACTORS
EPDC1 (OUTBOARD FACE)
CBP1
(FRONT FACE)
Page 87
SIDE 1 SHOWN
SIDE 2 SIMILAR
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
EPDC FUNCTIONS - COMMUNICATION - ELECTRICAL SYSTEM BITE FUNCTION (ESBF)
EPDC1/CBP1
EENMU
EENMF
1A
1B
Training by Airbus
CPIOM
CRDC
ESBF
ELMF
RCCBs
NOTE
SPDBs
EMERGENCY
CONTACTORS
SRPU
EDMU
PRIMARY
CONTACTORS
1A
1B
EPCU1
ATUPU1
PCBs
ENMU
ENMF
C/Bs
LPU
SSPCs
1A
1B
EPU
ELPU1
EDIU1
A
F
D
X
SSPCs
1A
1B
CDS
C/B
1A
1B
1A
1B
FUNCTIONAL DESIGNATION
LOCATION
RAT SOL AUTO MANUAL
RAT SOL AUTO
RAT POR
STATIC INVERTER 1
TR2
TR1
TR2 BKUP
TR1 BKUP
TR2 POM
TR1POM
TR EMER2
TR EMER1
TR EMER2 BKUP
TR EMER1 BKUP
TR EMER2 POM
TR EMER1 POM
701PM
702PM
BAT2 VOLTAGE IND
BAT1 VOLTAGE IND
4HK05
3HH01
4GB03
3HZ09
2GB05
1GC05
4AG03
3AF04
2KZ01
1KZ01
2AC06
1AV02
4HJ05
3HK05
4HZ16
3HZ16
1KZ02
2KZ02
4AH03
3AG02
C/B PAGE
1/1
FIN
3200XE
3201XE
3202XE
2001XB
1000PU
1001PU
3100PU
3101PU
3102PU
3103PU
2000PE
2001PE
3200PE
3201PE
3202PE
3203PE
1001PM
1002PM
3102PM
3103PM
N
E
T
W
O
R
K
OIS
PDMMF
DLCS
CB PAGE
ELPU1
EPDS FUNCTIONS:
SIDE 1 SHOWN
SIDE 2 SIMILAR
NETWORK PROTECTION
NETWORK MANAGEMENT
ELECTRICAL LOADS MANAGEMENT
BITE
COMMUNICATION
Page 88
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
SPDBS - LOCAL POWER MANAGEMENT FUNCTION (LPMF) & SEAT POWER SUPPLY FUNCTION (SPSF)
SIDE 1 SHOWN
SIDE 2 SIMILAR
Training by Airbus
NOTE
LPMF: Local Power Management Function
SPSF: Seat Power Supply Function
CABIN & CARGO LOADS
≤ 15 A
SPDB
EPDC1
SPDB
AC SSPCs
EPGS
EDMU
DC SSPCs
LPMF
1A
1B
SPSF
CABIN
CABIN
CABIN
CABIN
CARGO
CARGO
AFDX NETWORK
CDS
OIS
CPIOM
PDMMF
ESBF
DLCS
1
3
5
7
11
13
FOR EPDC1:
SPDBs 1, 3, 5, 7, 11, 13
FOR EPDC2:
SPDBs 2, 4, 6, 8, 12, 14
Page 89
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
ELECTRICAL NETWORK ARCHITECTURE - GROUND SERVICE CONFIGURATION
VFG 1A
VFG 1B
VFG 2B
RAT MODULE
APU GEN
MAIN NETWORK
MAIN NETWORK SIDE 2
APU START
SIDE 1
SYSTEM
EMERGENCY NETWORK SIDE 1
AC 1A
AC 1B
TR1
AC 1B
AC 1A
STAT
INV1
DC1
BAT1
AC EMER 2
EMER HOT
BUS 1
EMER
BAT1
SIC3
8
7448
2--7
7662 2
6 3A
NWS
LIGHT
TEST
NLG
LGT
GND SVCE
CTL 2
E
OFF
D
TO
TRUCK POWER
Switch GND
SVCE CTL2
ATU
2B
ATU
2A
TR2
AC 2A
DC2
HOT BUS 2
BAT2
L ON
J
F
AC 2A
AC 2B
SIC4
OFF
5
0V
NOTE
EXT PWR RCPT 2
GND SVCE CT
DISCONNECT
AC 2B
DC SHED/GS2
DC NORM/BAT2
EXT PWR RCPT 1
115 V
EMER HOT
BUS 2
EMER
BAT2
DC SHED/GS1
DC NORM/BAT1
HOT BUS 1
VFG 2A
EMERGENCY NETWORK SIDE 2
AC EMER 1
AC EMER 1
INV AC1
ATU
1B
ATU
1A
Training by Airbus
Switch GND
SVCE CTL1
GROUND SERVICE MAIN AVAILABLE FUNCTIONS
CARGO LOADING
CATERING AND CLEANING
PORTABLE AND WASTE WATER SERVICE
REFUELING
LIGHTING
Page 90
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
ELECTRICAL NETWORK ARCHITECTURE -TOWING ON BATTERY
Training by Airbus
ONLY BATTERY 1 USED FOR TOWING ON BAT
AVAILABLE FUNCTIONS:
NOTE
VHF1
FLIGHT INTERPHONE
COCKPIT AMBIENT LIGHTING
PARK BRAKE ON LIGHT
MAIN NETWORK SIDE 1
DC1
DC NORM/BAT1
SSPCs
HOT BUS 1
BATTERY 1
TOWING ON BAT
POWER
ON
STEERING DISCONNECT PANEL
Page 91
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
ELECTRICAL NETWORK ARCHITECTURE - REFUEL ON BATTERY CONFIGURATION
Training by Airbus
INTEGRATED
REFUEL PANEL
POWER
SUPPLY
NOTE
B
BATTERY
NORMAL
N
MAIN NETWORK SIDE 2
MAIN NETWORK SIDE 1
DC1
DC2
DC NORM/BAT1
HOT BUS 1
SSPCs
REFUEL SYSTEM
SSPCs
DC NORM/BAT2
HOT BUS 2
Page 92
BATTERY 1
BATTERY 2
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
VFG LUBRICATION AND COOLING
Training by Airbus
SAOHE
SAOHEs
SAOH
NOTE
FAN AIR
FLOW
A350
OVER
FULL
OVER
FULL
ADD
OIL
ADD
OIL
THERMAL
BYPASS
VALVE
FAN CASE
OIL INLET
PORT
OIL OUTLET
PORT
AGB
FAN COWL
VFG
VFG
VFG A
PUMP
PRESSURE
REGULATING
VALVE
VFG B
Page 93
AGB
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
VFG OIL SYSTEM MONITORING
Training by Airbus
DISPATCH MESSAGES EXAMPLES:
NWS DISCONNECT SAFETY PIN
NOT ENGAGED
ON GROUND
LOW OIL LEVEL
6 MN AFTER ENGINE SHUTDOWN
AND
LOW OIL LEVEL STATUS
SENT TO FWS AND CMS
VFG SENSORS:
OIL LEVEL: REMOTE OIL LEVEL SENSOR
(ROLS)
FILTER CLOGGING: DIFFERENTIAL
PRESSURE SENSOR
ELEC > DRIVE 1A OIL LEVEL LO
ELEC > DRIVE 1A OIL FILTER CLOGGED
FWS
CMS
DISPATCH
MESSAGE
MAINTENANCE
MESSAGE
NOTE
AFDX NETWORK
VFG
SENSORS
LOW OIL
LEVEL
GCU
FILTER
CLOGGING
Page 94
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
VFG OIL SYSTEM SERVICING
Training by Airbus
SAOHEs
NOTE
A350
VFG OIL SYSTEM
LINES
OVER
FULL
OVER
FULL
ADD
OIL
ADD
OIL
OIL OUTLET PORT
PRESSURE
FILL PORT
OIL INLET
PORT
OIL FILTER
O-RING
FILTER
HOUSING
CAP
UPPER RED AREA:
DRAIN EXCESS OF OIL
YELLOW AREA:
CAN BE NORMAL IF
OIL IS HOT
PRESSURE
FILL HOSE
OVERFLOW
DRAIN PORT
OVERFLOW
DRAIN HOSE
OIL CONTAINER
INER
OVER
FULL
TOP GREEN AREA:
NORMAL LEVEL AT
END OF SERVICING
GREEN AREA:
NO OIL SERVICING
NEEDED
O-RING
N
DRAIN
PORT
A350
OVER
FULL
ADD
OIL
LOWER RED AREA:
OIL SERVICING NEEDED
DRA
DRAIN
PL
PLUG
ADD
OIL
Page 95
PRESSURE
FILL HOSE
OIL SERVICI
SERVICING
PUMP
SIGHT GLASS
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
PDMI DESCRIPTION
LGERS
Training by Airbus
FLIGHT/GROUND
ADIRS
NOTE
AFDX NETWORK
SCI
FWS
EPDC
ELEC C/B TRIPPED
OIS
PDMMF
EDMU
1A
1B
ON
MAINTENANCE
PANEL
CBP
C/Bs
SSPCs
1
SPDBs
SSPCs
ELEC
REMOTE
C/B CTL
EDIU1
CDS
2
OMT
C/Bs
SSPCs
P-MAT
RCCBs
1
2
OIS
C/B
1/1
FUNCTIONAL DESIGNATION
LOCATION
RAT SOL AUTO MANUAL
RAT SOL AUTO
RAT POR
STATIC INVERTER 1
TR2
TR1
TR2 BKUP
TR1 BKUP
TR2 POM
TR1POM
TR EMER2
TR EMER1
TR EMER2 BKUP
TR EMER1 BKUP
TR EMER2 POM
TR EMER1 POM
701PM
702PM
BAT2 VOLTAGE IND
BAT1 VOLTAGE IND
4HK05
3HH01
4GB03
3HZ09
2GB05
1GC05
4AG03
3AF04
2KZ01
1KZ01
2AC06
1AV02
4HJ05
3HK05
4HZ16
3HZ16
1KZ02
2KZ02
4AH03
3AG02
C/B PAGE
FIN
3200XE
3201XE
3202XE
2001XB
1000PU
1001PU
3100PU
3101PU
3102PU
3103PU
2000PE
2001PE
3200PE
3201PE
3202PE
3203PE
1001PM
1002PM
3102PM
3103PM
Page 96
CB PAGE
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
PDMI ON BAT
Training by Airbus
NOTE
ONBOARD
MAINTENANCE
TERMINAL (OMT)
AIRCRAFT
ON
GROUND
BAT EMER 1
FAULT
OFF
BAT EMER 2
FAULT
AND
PDMI
SYSTEM
OFF
ELEC
REMOTE
C/B CTL
ON
Page 97
SSPCs/RCCBs
PDMI: POWER DISTRIBUTION
MAINTENANCE INTERFACE
24
BAT EMER 1+2 “ON”
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
ELECTRICAL STRU
STRUCTURE NETWORK (ESN) INTRODUCTION
Training by Airbus
TWO PRIM
PRIMARY TYPES OF ESN COMPONENTS
STRUCTURE METALLIC ELEMENTS:
FOR EXAMPLE, METALLIC FRAMES, CROSSBEAMS,
SEAT/ROLLER TRACKS...
NOTE
MECHANICAL ELEMENTS:
FOR EXAMPLE, AVIONICS BAY RACKS,
MECHANICAL JUNCTIONS, CABIN FURNISHING
STRUCTURE IN THE CROWN AREA...
SPECIFIC ESN COMPONENTS:
FOR EXAMPLE, RACEWAYS, FLEXIBLE
FUNCTIONS, ESN CABLES...
ESN PARTS
IDENTIFICATION SOLUTION
MECHANICAL ELEMENTS
RACEWAYS
BRACKETS
BULKHEAD STRIP
GREEN IDENTIFICATION
LABEL
ESN CABLE
DRAIN CABLE
ESN JUNCTION
GREEN IDENTIFICATION
SLEEVE
ESN JUNCTION (BRAID)
GREEN IDENTIFICATION
LABEL
75cm max
FOR THE REPAIR AND THE TESTS
OF THE ESN PARTS, REFER TO THE
AIRN@V ON-LINE DOCUMENTATION
75cm max
ABS1660A150A1- ESN
Page 98
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
ESN MEASUREMENT - TEST TOOL
Training by Airbus
ESN JUNCTION TEST TOOLS
NOTE
ESN CABLE
ATEQ LRT 6000
CURRENT CLAMP
FUCHS BLRT2 TESTER
AN ESN ELECTRIC LOAD ANALYSIS (ELA) MUST BE PERFORMED IN CASE OF
SYSTEM MODIFICATION OR ADDITION.
Page 99
AN AIRBUS ANALYSIS IS NECESSARY PRIOR TO ESN PHYSICAL MODIFICATION.
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
SPDB LOCATION
Training by Airbus
NOTE
SPDB-4
CABIN
4XY
SPDB-12
CARGO
12XY
SPDB-3
CABIN
3XY
SPDB-2
CABIN
2XY
SPDB-7
SPDB-8 CABIN
CABIN
7XY
8XY
FR47
FR45
11XY
SPDB-11
CARGO
FR32
FR28
FR24
FR21
SPDB-1
CABIN
1XY
SPDB-6
CABIN
6XY
SPDB-13
CARGO
SPDB-5 13XY
CABIN
5XY
FR90
FR82
FR77
FR75
FR14
FR67
14XY
SPDB-14
CARGO
FR59
FR57
FR55
Page 100
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
24
ATA 42
IMA AND ADCN
CPIOM ARCHITECTURE
Training by Airbus
H31
H33
H32
H34
J11
J12
HMCA Yellow 1
HMCA Green 1
HMCA Yellow 2
HMCA Green 2
FW 1
FW 2
DSCS A1
DSCS S1
DSCS A2
DSCS S2
FQMS COM 1
FQMS MON 1
FQMS COM 2
FQMS MON 2
IGGS 1
OSCM 1
J23
J22
OSCM 2
H41
H43
H42
H44
ACS 1
BAS 1
ACS 2
BAS 2
CPCS 1
OHDS 1
CPCS 2
OHDS 2
VCS L1
SCS 1
VCS L2
SCS 2
WIPS COM 2
WIPS COM 1
H61
H63
H62
H64
BCS COM 1
BCS MON 1
BCS COM 2
BCS MON 2
LGERS COM 1
LGERS COM 1
LGERS COM 2
LGERS COM 2
WSCS MON 1
WSCS COM 1
WSCS MON 2
WSCS COM 2
LGMS 1
LGMS 2
J21
NOTE
J24
FPS 1
FPS 3
FPS 2
FPS 4
EIF 1.1
EIF 1.2
EIF 2.2
EIF 2.1
AICF 1
AICF 3
AICF 2
AICF 4
J71
J72
J51
J52
FCDC 1
FCDC 2
ACR 1
ACR 2
ATC 1
OPTIONAL
FCUb 1
FCUb 2
ELMF 1
ELMF 2
ESBF 1
ESBF 2
ELCO 1
ELCO 2
Emer
Ground Servicing
Page 101
272PN: DC2 REFUEL on BAT
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
42
CRDC LOCATION
CRDC-A01
1TS01
Training by Airbus
NOTE
FR10
FR9
B
FR14
FR17
1TS07
CRDC-A07
A
FR23
1TS02
CRDC-A02
FR27
1TS04
CRDC-A04
1TS03
CRDC-A03
FR39
1TS05
CRDC-A05
1TS08
CRDC-A08
1TS09
CRDC-A09
2TS05
CRDC-B05
1TS06
CRDC-A06
1TS11
CRDC-A11
A
FR40
FR41
FR42
FR45
CRDC-B03
2TS03
1TS13
CRDC-A13
2TS08
CRDC-B08
2TS02
CRDC-B02
2TS06
CRDC-B06
2TS01
CRDC-B01
2TS04
CRDC-B04
Page 102
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
42
CRDC LOCATION
Training by Airbus
NOTE
FR60
CRDC-B09
2TS09
B
CRDC-B07
CRDC-B14
2TS14
A
CRDC-B10
2TS10
2TS12
2
CRDC-B12
FR82
FR83
FR86
2TS11
CRDC-B11
FR87
2TS13
CRDC-B13
FR93
F
1TS12
CRDC-A12
B
1TS10
CRDC
A10
CRDC-A10
1TS15
CRDC-A15
1TS17
CRDC-A17
Page 103
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
42
CRDC LOCATION (AVIONIC BAY)
Training by Airbus
NOTE
1042VU
1000VU
A
CRDC - A08
1TS08
CRDC - A04
1TS06
CRDC - A06
1TS04
CRDC - A09
CRDC - A02
1TS09
1TS02
1TS05
1TS03
CRDC - A03 CRDC - A05
1TS07
CRDC - A07
1TS01
CRDC - A01
A
Page 104
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
42
CRDC LOCATION (FWD LDCC)
CRDC - B04
2TS04
B
Training by Airbus
CRDC - B02
2TS02
NOTE
2TS06
CRDC - B06
CRDC - B03
2TS03
2TS08
CRDC - B08
FR46
FR41
FR38
FR44
FR42
FR40
2TS01
B
CRDC - B01
FR19
1TS13 CRDC - A13
B
1TS11
CRDC - B05
CRDC
- A11
2TS05
Page 105
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
42
CRDC LOCATION (AFT LDCC)
Training by Airbus
NOTE
C
CRDC - B09
2TS09
CRDC - B14
2TS14
FR82
C
2TS10
CRDC - B10
CRDC - B07
2TS07
2TS12
CRDC - B12
2TS11
CRDC - B11
FR61
2TS13
CRDC - B13
FR60
Page 106
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
42
CRDC LOCATION (BULK LDCC)
Training by Airbus
NOTE
D
CRDC - A12
1TS12
FR93
1TS15
1TS10
CRDC - A15
CRDC - A10
FR87
FR86
D
1TS17
CRDC - A17
FR85
FR82
Page 107
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
42
AFDX NETWORK OVERVIEW
SFCC1S
PRIM1A
SEC1A
PRIM3A
PRIM3B
ADIRU3
FMC3
CRDC
A05
CRDC
A15
SFCC2S
PRIM2A
SEC2A
SFCC1F
PRIM1B
SEC1B
SEC 3A
SEC 3B
CDLCU
ECBAPU
SCI
SDU1
SFCC2F
PRIM2B
SEC2B
ADIRU1
FMC1
CDS
DU-IC
ADIRU2
FMC2
CDS
DU-IF
CPIOM
J22
CPIOM
J72
CDS
DU-LC
CRDC
A02
CRDC
A04
CRDC
A10
AESU2
CPIOM
H42
CPIOM
J12
EMU2
CMV2
ETRAS2
CPIOM
J24
CPIOM
H32
CPIOM
H44
CPIOM
H62
CRDC
A06
CRDC
B08
CRDC
B10
CPIOM
J21
CPIOM
J71
CDS
DU-UC
CRDC
A11
CRDC
A07
CRDC
B13
CPIOM
J11
CPIOM
H41
CRDC
A01
36
SW
01
11
EEC1A
12
SW
EEC1B
AESU1
CMV1
EMU1
CPIOM
J23
ETRAS1
CPIOM
H31
CPIOM
H43
CPIOM
H61
CRDC
A03
CRDC
B05
CRDC
B09
36
24
02
SW
EEC2B
09
19
EEC2A
CDAU
22
SW
20
SW
13
14
EPDC1A
EPDC2A
SPDB1A
SPDB2A
EPDC1B
EPDC2B
CPIOM
J51
CIDS1
CDS
DU-OC
SPDB1B
SPDB2B
CPIOM
J52
CIDS2
CDS
DU-OF
CPIOM
H33
CRDC
B11
CPIOM
H63
24
24
CPIOM
H34
CRDC
B14
CPIOM
H64
CRDC
B07
CRDC
A09
CRDC
A13
CRDC
A08
CRDC
A12
CRDC
B02
CRDC
A17
CRDC
B01
CRDC
B03
CRDC
B04
CRDC
B06
CRDC
B12
SW
SW
15
LRU
16
CPIOM AND CRDC
Training by Airbus
2 links: one per network
1 link on network B only
Page 108
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
42
ATA 31
INDICATING / RECORDING SYSTEMS
ICP LAYOUT - SYSTEM ARCHITECTURE
& CAN NETWORK
Training by Airbus
CAN ICPs
NOTE
135 VM
ON
FIRE
ON
ENG START
1
NORM
FAULT
FIRE
2
IGN
START
CRANK
2
FAULT
OFF
ECP CAN NETWORK
CRDC
OFF
T.O
CONFIG
1
EMER
MME
R
E
CANC
AN
C
N
AC
DEFRD
ABN
RCL
LAST
...
RCL
ALL
DISPCH
SD
ENG
DOOR
...
MORE
STS
WHEEL
FUEL
ALL
EL/AC
EL/DC
HYD
F/CTL
APU
BLEED
COND
PRESS
4
VIDEO
VIDEO
CLEAR
CLEAR
2
ICP
AFDX NETWORK
ICP CAN NETWORK
4
4
1
4
...
...
4
...
A/C SYSTEMs
8
NO CAN ICPs
LRUs
SPECIAL CASES
(E.G. CABIN
PRESS)
ICP
1
AFDX
NETWORK
SUBSCRIBERS
Page 109
...
6
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
31
CDS ARCHITECTURE
Training by Airbus
AFDX NETWORK
NOTE
A
LEFT
OUTER DU
LEFT
INNER DU
UPPER
CENTER C
DU
B
FLEX
FLE
FL
LLEEX
EX
5
140
135
0
EGT
EG
E
G
GTT
°°C
C
69
69
692
92
2
10
10
74.
7
74
4 0
78.
7
78
81
83.
8
83
3
3. 9 % 53
53°°C
C
%
1150 Z from
PACK
PACKS
PA
P
A
ACK
CKS
CK
CKS
ctlLFBO
RIGHT
OUTER DU
OPEN
5
TH
THR
HR
N
N1
%
RIGHT
INNER DU
0
1100
140
135
EG
EGT
E
G
°°C
C
74.
74
7
4.
4 0
78.
7
78
81
69
6
692
92
9
2
T.O INHIBIT
NO SMOKING
SEAT BELTS
GND SPLRs ARMED
+53°C
C
B
LOWER
CENTER DU
A
CAN 2.1
CAN 1.1
ESC
CLR
INFO
Q
W
.
A
KEYBOARD
E
.
S
.
DIR
PERF
INIT
NAV
AID
C/L
ESC
F-PLN
DEST
SEC
INDEX
SURV
ATC
COM
CLR
INFO
R
D
T
F
/
Z
X
C
OIS
ND
MFD
MAIL
BOX
Y
G
V
OIS
MENU
U
H
B
I
J
N
.
O
K
M
NOTE
PAD
E
.
S
.
Z
1
2
4
5
6
4
5
7
8
9
7
8
9
0
+/-
0
+/-
KBD
PERF
INIT
NAV
AID
C/L
DEST
SEC
INDEX
SURV
ATC
COM
3
T
F
C
3
.
DIR
F-PLN
R
D
X
ENT
2
Y
G
V
U
H
B
I
J
N
.
O
K
P
NOTE
PAD
L
M
SPACE
MAIL
BOX
MFD
6
ENT
ND
ESC
CAPT KCCU
KBD
ESC
OIS
OIS
MENU
MENU
MENU
CCD
W
.
A
/
SPACE
1
.
CAN 1.2
Q
P
L
KEYBOARD
CCD
F/O KCCU
CAN 2.2
Page 110
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
31
ECAM FUNCTION
FLEX
140
135
0
EGT
°C
692
83. 9 % 53°C
ED
5
313 VU
10
74. 0
78. 1
PACKS
5
THR
%
0
N1
%
10
692
T.O INHIBIT
NO SMOKING
SEAT BELTS
GND SPLRs ARMED
OIS
SD
EFB
VIEW
OFFSIDE
OIS
MAP LT
WD
INOP
ON
VIEW
OFFSIDE
F
FF
OFF
ON
SFLMD
PEDALS LT
ON
FF
FF
OFF
+53°CC
BACK UP
BACK UP
PERMANENT
DATA ZONE
135 VM
ON
FWS
FIRE
ON
ENG START
1
NORM
FAULT
EMER
MME
R
E
CANC
AN
C
N
AC
DEFRD
ABN
RCL
ALL
DISPCH
SD
ENG
DOOR
MORE
STS
WHEEL
FUEL
VIDEO
VIDEO
CLEAR
ALL
CRITICAL
SYSTEMS
FAULT
OFF
T.O
CONFIG
AFDX NETWORK
FIRE
2
IGN
START
CRANK
OFF
RCL
LAST
CMV
T
INOP
SFLMD
PEDALS LT
ON
NOTE
314 VU
140
135
EGT
°C
74. 0
78. 1
MAP LT
T
Training by Airbus
EL/AC
EL/DC
HYD
F/CTL
APU
BLEED
COND
PRESS
CLEAR
CRDC
1
2
A/C DATA
(FOR SYSTEM PAGES)
Page 111
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
31
CDS CONTROLS
T.O
CONFIG
Training by Airbus
EMER
CANC
DEFRD
ABN
RCL
LAST
NOTE
RCL
ALL
DISPCH
MORE
STS
SD
ENG
DOOR
WHEEL
FUEL
VIDEO
VIDEO
CLEAR
EL/AC
EL/DC
HYD
F/CTL
APU
BLEED
COND
PRESS
ALL
CLEAR
ECP
ESC
DIR
PERF
INIT
NAV
AID
C/L
MENU
ESC
DIR
PERF
INIT
NAV
AID
C/L
MENU
CLR
INFO
F-PLN
DEST
SEC
INDEX
SURV
ATC
COM
CLR
INFO
F-PLN
DEST
SEC
INDEX
SURV
ATC
COM
Y
U
Y
U
Q
W
.
A
/
E.
S.
Z
OIS
R
D
X
ND
T
F
C
MFD
G
V
MAIL
BOX
H
B
I
J
N
.
O
K
M
Q
P
NOTE
PAD
L
SPACE
/
ENT
E.
S.
Z
R
D
X
1
2
3
1
2
3
5
6
4
5
6
7
8
9
7
8
9
0
+/-
0
+/-
.
G
V
H
B
I
J
N
.
O
K
P
NOTE
PAD
L
M
SPACE
MAIL
BOX
MFD
ENT
ND
OIS
SPACE
SPACE
KBD
T
F
C
4
.
CAPT KCCU
W
.
A
KBD 1
KBD 2
CCD 1
CCD 2
KBD
ESC
OIS
ND
MFD
MAIL
BOX
ESC
F/O KCCU
Page 112
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31
CDS MANUAL RECONFIGURATION FOR OIS
Training by Airbus
NOTE
“ DISPLAY CYCLE” CONTROL
TO DISPLAY OIS OR MFD
2nd
MFD
(FMS)
CAPT
OIS
CAPT
MFD
F/O
MFD
DISPLAY
CYCLE
CAPT OIS
ON CENTER
F/O OIS
ON CENTER
DISPLAY
CYCLE
AVAIL
INOP
INOP
AVAIL
ON
ON
CAPT DISPLAY
CONTROL PANEL
2nd
MFD
(FMS)
F/O DISPLAY
CONTROL PANEL
Page 113
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
31
CDS MANUAL RECONFIGURATION FOR OIS
Training by Airbus
NOTE
> MFD TRANSFERRED ON
OUTER DISPLAY
> SECOND MFD AVAILLABLE (FMS)
F/O
MFD
CAPT
OIS
2nd
MFD
(FMS)
F/O
OIS
F/O OIS
ON CENTER
DISPLAY
CYCLE
INOP
AVAIL
ON
Page 114
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
31
CDS MANUAL RECONFIGURATION FOR OIS
Training by Airbus
NOTE
VIEW
OFFSIDE
INOP
ON
O
N
F/O
OIS
VIEW
OFFSIDE
INOP
ON
Page 115
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
31
GENERAL (ARCHITECTURE)
DATA BROADCAST
DATA ACQUISITION AND ALERT PROCESSING
Training by Airbus
ALERT INDICATION
CDS (ECAM PART)
SCI
CMS
NOTE
AFDX NETWORK
CRDC
A/C SYSTEMS
A
LRUs
(WITH AFDX
INTERFACE)
BACKUP
135 VM
ON
FIRE
ON
ENG START
1
NORM
FAULT
LRUs
(WITHOUT AFDX
NETWORK
SUBSCRIBERS)
FIRE
2
IGN
START
CRANK
OFF
FAULT
OFF
T.O
CONFIG
EMER
MME
R
E
AN
CANC
C
N
AC
DEFRD
ABN
RCL
LAST
RCL
ALL
DISPCH
SD
WD
MORE
STS
ENG
DOOR
WHEEL
FUEL
EL/AC
EL/DC
HYD
F/CTL
APU
BLEED
COND
PRESS
VIDEO
VIDEO
CLEAR
ALL
AUDIO EQUIPMENT
CLEAR
ECP
OTHER
ATTENTION GETTERS
AUTO
LAND
PFD
L/G
UP
AMU
CPIOM
MASTER LIGHTS
FWS
411 VU
A
412 VU
WARN
MASTER
WARN
MASTER
CAUT
MASTER
CAUT
MASTER
ATC
MSG
Page 116
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
31
MEMOS, LIMITATIONS, DISPATCHS, STATUS & NORMAL CHECK LISTS, ABNORMAL PROCEDURES
STATUS PAGE
5
EGT
°C
0
751
%
0. 0
84.7
5
THR
10
STATUS MORE INFO PAGE
0
N1
%
1
10
0. 0
84.7
STATUS
DEFERRED PROCS : ALL PHASES, APPR, LDG
LIMITATIONS
INFO
F/O BARO REF : STD ONLY
SLATS SLOW
FLAPS SLOW
ALL PHASES
PRIM 2+3
ENG 2 REV
SEC 2+3
VHF 1+2+3
RA SYS A+B+C
FMS 2
INOP SYS
EGT
°C
751
MORE
STATUS
INOP SYS REDUND
YAW DAMPER 1
CANCELLED CAUTION
HYD GREEN RSVR OVHT
SYSTEM REDUNDANCY
LOSS
LIST OF ALERTS CANCELLED
WITH EMER CANC P/B
IF HYDRAULIC IS RECOVERED CORRESPONDING
LIMITATIONS WILL NOT APPLY
CLICK ON «MORE» BUTTON ON THE ECP
TO ACCESS TO THE STATUS MORE INFO PAGE
Training by Airbus
NOTE
MORE INFO :
ADDITIONAL INFO
TO PROCEDURE
APPR & LDG
AUTO CALLOUT
SLAT SYS 2
FLAP SYS 2
LIMITATIONS
ALL PHASES
MAX SPD : 200KT
APPR & LDG
LDG DIST x 1.4
CAT 3 SINGLE ONLY
MORE
SD
SEAT BELTS
NO SMOKING
ENG A ICE
ABCDEFGHIJKLMNOPQRSTUVWXYZxs
0123456789
à_è-()'"é&#[]|
+\°{}^ù*:;,¨%µ/.?<>=
INFO RELATED TO
DEGRADED A/C
SYSTEM
STS
WD
Page 117
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
31
MEMOS, LIMITATIONS, DISPATCHS, STATUS & NORMAL CHECK LISTS, ABNORMAL PROCEDURES
Training by Airbus
NOTE
ABNORMAL PROC
SMOKE / TOXIC FUMES REMOVAL
EMER DESCENT
DITCHING
FORCED LANDING
ON GROUND EMERGENCY EVAC
FIRE PROTECTION
FLIGHT CONTROLS
INDICATING / RECORDING
LANDING GEAR
NAVIGATION
POWER PLANT
MISCELLANEOUS
OPERATING TECHNIQUES
AIRLINE PROCEDURES
135 VM
ON
FIRE
ON
ENG START
1
FAULT
IGN
START
CRANK
FIRE
2
NORM
FAULT
WD
OFF
OFF
T.O
CONFIG
EMER
CANC
DEFRD
ABN
RCL
LAST
RCL
ALL
DISPCH
STS
MORE
SD
ENG
DOOR
WHEEL
FUEL
EL/AC
EL/DC
HYD
F/CTL
APU
BLEED
COND
PRESS
VIDEO
VIDEO
CLEAR
ALL
Page 118
CLEAR
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
31
MEMOS, LIMITATIONS, DISPATCHS, STATUS & NORMAL CHECK LISTS, ABNORMAL PROCEDURES
CHECKLISTS
APPROACH
ECAM STATUS CHECK
BRIEFING..............................................................CONFIRM
V BUG................................................................................SET
SEAT BELTS ON
BARO.................................................................................SET
MDA / DH........................................................................SET
COMPLETE
RESET
BEFORE START
AFTER START
BEFORE TAKEOFF
AFTER TAKEOFF / CLIMB
APPROACH
LANDING
AFTER LANDING
PARKING
SECURING AIRCRAFT
MFD
DIR
PERF
INIT
NAV
AID
F-PLN
DEST
SEC
INDEX
SURV
Y
U
W
.
A
/
MFD
E.
S.
Z
OIS
R
D
X
ND
T
F
C
MFD
G
V
MAIL
BOX
H
B
I
J
N
.
ATC
COM
O
K
M
NOTE
C/L
MENU
ESC
CLR
INFO
Q
Training by Airbus
MFD
P
NOTE
PAD
L
SPACE
ENT
1
2
3
4
5
6
7
8
9
0
+/-
.
MFD
SPACE
KBD 1
CCD 1
KBD
ESC
KCCU
Page 119
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
31
IDENTIFICATION OF FAILURE CONDITION
Training by Airbus
CIRCUIT B
CIRCUIT A
CDS
FR85
FR84
NOTE
CONNECTOR
TAIL STRIKE
> TAIL STRIKE DET
CRDC
CRDC
TAIL - STRIKE
INDICATION SENSOR
AFDX NETWORK
CPIOM
135 VM
CPIOM
FIRE
ON
ENG START
1
FAULT
IGN
START
CRANK
FIRE
2
NORM
FAULT
SENSOR TAIL STRIKE INDICATION
FWS
HYD
F/CTL
APU
BLEED
COND
PRESS
VIDEO
VIDEO
ALL
CLEAR
POST-FLIGHT
EL/DC
TAXIING
FUEL
EL/AC
CLEAR
TAXI IN
WHEEL
LANDING
DOOR
APPROACH
MORE
STS
ENG
CRUISE
DISPCH
SD
STEP 2
RCL
ALL
STEP 1
ABN
STEP 3
EMER
CANC
DEFRD
RCL
LAST
STEP 2
T.O
CONFIG
STEP 1
OFF
TAXI OUT
OFF
FF
PRE-FLIGHT
ON
1
2
3
4
5
6
7
8
9
10
11
12
13
TAKE-OFF
CLIMB
Page 120
TAIL-STRIKE DET FAULT ACTIVATION
TAIL-STRIKE DET FAULT INHIBITION
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
31
CMV DESCRIPTION AND INTERFACES
CONTROL MEANS
EFIS CONTROL PANELS
TAXI
TAXI
QNH
29.92
CSTR
WPT
29.92
VOR
TRAF
WX WPTTERR
VORD
0123456789
VORD
NDB
ARPT
CAPT INNER
DU
CENTER
UPPER DU
80
320 160
40
10
20
640
ZOOM
PLAN
10
LS
VV
F/O OUTER
DU
NOTE
CENTER
LOWER DU
160
20
PLAN
VOR
F/O INNER
DU
ARPT
80
40
ARC
VOR
LS
VV
LS
CAPT OUTER
DU
TRAF
NAV
LS
Training by Airbus
CDS
320
640
ZOOM
ECAM CONTROL PANEL
T.O
CONFIG
EMER
CANC
DEFRD
CMV SYSTEM
ABN
RCL
LAST
RCL
ALL
DISPCH
STS
MORE
CMV
SD
ENG
DOOR
EL/AC
EL/DC
APU
BLEED
VIDEO
VIDEO
CLEAR
ALL
CLEAR
CMV
CMV OPERATIONAL
PROGRAM
1
CMV OPERATIONAL
PROGRAM
2
SELECTION
INHIBITION
CDSS
221 VM
CABIN
PAX INFO
OFF
PAX PERS
ELEC SPLY
LANDSCAPE
CAMERA
OFF
OFF
IFE
SYSTEM
MOBILE COM LAVATORY
OFF
SMOKE
OCCPD
OVERHEAD PANEL
BELLY TAC
CAPT VGM
F/O VGM
OIS
LANDSCAPE
CAMERA
ETACS
ETACS
CVMS
LDSF
VERTICAL
STABILIZER TAC
Page 121
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
31
FLIGHT DATA RECORDING AND CENTRALIZED DATA ACQUISITION SYSTEM (ARCHITECTURE)
Training by Airbus
AFDX NETWORK
NOTE
A/C SYSTEMS
ACMS
DFDR
RCDR
TRIGGER
EVENT
GND CTL
ON
CRDC
CRDC
A
U
T
O
LGERS
PARAMETERS
PCS
ICP
ARINC 429
STATUS
S
RECORDING TRIGGERED WHEN:
- AT A/C POWER UP DURING 5 MINUTES
- IF 1 ENGINE IS STARTED
- UNTIL 5 MINUTES AFTER LAST
ENGINE SHUTDOWN
- IF RCDR GND CTL P/BSW IS PUSHED
ON GROUND
- IF A/C IN FLIGHT WHATEVER THE
OTHER CONDITIONS
LA
(3-AXIS ACCLRM)
RECORDING
START/STOP
CONTROL
OIS
VQAR
CDAU
SCI
SCI
FDIF
SSFDR
ARINC 717
ACMS-RT
ARINC 717
QAR
Page 122
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
31
HEAD-UP PROJECTION UNIT (HPU) - HEAD-UP DISPLAY (HUD)
Training by Airbus
CAPT PMM
NOTE
RIGHT SYSTEM SYMMETRICAL
(USING LOWER CENTER DU
AND F/O HUD CTL PNL)
CAPT HPU
CAPT F/O HUD
CONTROL PANEL
HUD
NORM
ND
X WIND
OFF
BRIGHTNESS
EXTERNAL
LUMINOSITY
COMBINER
DEPLOYED
CAPT HCU
DECLUTTER
PROJECTION
B
BRT
R
DECLUTTER
OFF
X WIND
HCU PMM HPU
DECLUTCHING
HANDLE
UPPER CENTER
DU
ARINC 429 (BACKUP)
AVIONICS
SYSTEMS
AFDX NETWORK
CMS
SCIs
COMBINER DEPLOYED & LOCKED
Page 123
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
31
FLIGHT DATA RECORDER SYSTEM (COMPONENTS LOCATION)
Training by Airbus
A
NOTE
B
FR55
FR54
FR87
FR86
A
6TU
ACCLRM-FDRS
1TU
SSFDR
B
Page 124
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
31
DISPLAY UNIT (DU) DESCRIPTION
Training by Airbus
LUMINOSITY
SENSOR
NOTE
BRIGHTNESS
CONTRAST
START/STOP
SIS CONNECTOR
A
LUMINOSITY SENSOR
ELECTRICAL AND
OPTICAL CONNECTORS
A
Page 125
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
31
ATA 46
INFORMATION SYSTEMS
OIS RESOURCES
Training by Airbus
NOTE
A/C
SYSTEMS
AIRLINE
FACILITIES
CIDS
EMER
PED
POWER
IPRAM
OIS DISPLAY
OMT
LIGHTS
MAIN
ON/OFF
MENU
LAV
MAINT
SCREEN
3D secLOCK
EVAC
CMD
EVAC
RESET
SMOKE
RESET
CAM
FAP-PC
RESET
PAX
SYS
OBRM
FAP
A/C SYSTEMS
OIS
E.G. FLIGHT
OPS
SCI
1
E.G.: OMS,
AOC
SDM
E.G. AirN@v
OIS
2
ASFC
OSFC
EFB LAPTOP(x2)
Page 126
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
46
OIS ARCHITECTURE
LIMIT SPEED
(IAS KT)
COCKPIT
HMIs
NORM
10
74. 0
78. 1
83. 9 % 53°C
%
N1
%
PACKS
HOT
5
THR
0
10
NORM
140
135
EGT
°C
74. 0
78. 1
692
PRINTER
Training by Airbus
PMAT*
T.O INHIBIT
NO SMOKING
SEAT BELTS
GND SPLRs ARMED
F/O
ON 3
L/G
AIR DATA
CAPT
ON 3
OMT
BRAKE
FLEX
5
0
EGT
°C
692
ATT HDG
CAPT
ON 3
312 VU
311 VU
VLO = VLE
NORM :
250
M 0.55
GRVTY :
250
255
220
212
195
186
VFE 1
1+F
2
3
FULL°
140135
UP
F/O
ON 3
FMS
BOTH
ON 2
CDS
NORM
BOTH
ON 1
NOTE
+53°C
OIS
AISD
ACD
ASFC
A/C
SYSTEMS
SCI
FAPs
EFB LAPTOP*
CABIN
AOC
FLIGHT
DOMAIN
FLIGHT
OPERATIONS
(EFF, FCOM,
PERFs)
SDM
1
CABIN HMIs
OSFC
CIDS
EMER
PED
POWER
IPRAM
LIGHTS
MAIN
ON/OFF
MENU
LAV
MAINT
SCREEN
3D secLOCK
CAM
EVAC
CMD
EVAC
RESET
SMOKE
RESET
FAP-PC
RESET
PAX
SYS
OBRM
A/L CABIN
LAPTOP*
EFB
MAINTENANCE
2
ACD
MAINTENANCE
MAINTENANCE
ACD
COMMUNICATION
COMMUNICATION
DOCKING
STATION
(x2)
PRINTER
A/L FACILITIES
* = Under Airline Responsibility
Page 127
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
46
OSFC & ASFC APPLICATIONS
Training by Airbus
OSFC FUNCTIONS
ACD
ASFC FUNCTIONS
FLIGHT OPERATIONS
FLIGHT OPERATIONS
A/C
SYSTEMS
AOC
FLIGHT OPS
HMI MANAGER
FLIGHT DOMAIN
SCI
1
ASFC
2
NOTE
MAINTENANCE
SDM
MAINTENANCE
MHM
BASIC
FUNCTIONS
LMF
MCA
AIRCRAFT
DOCUMENTATION
SYSTEM
CABIN
CMS-ACD
DLCS-ACD
SDL
OSFC
INTERNET PROTOCOL
COM MANAGER
IMACS
CCMAIL
CADOC
PDMMF
CABIN
WLM
ACMS
SPP
COMMUNICATION
AMEX
BASIC SERVICES
BASIC
SERVICES
PRINT, EXPORT
Page 128
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
46
OIS DETAILED ARCHITECTURE
FLEX
5
140135
0
EGT
°C
692
10
74. 0
78. 1
83. 9 % 53°C
%
N1
%
PRINTER
PACKS
Training by Airbus
CAPT & F/O SLIDING TABLES
5
THR
0
10
140
135
EGT
°C
74. 0
78. 1
692
T.O INHIBIT
NO SMOKING
SEAT BELTS
GND SPLRs ARMED
+53°C
CDS
NOTE
FAPs
KBD 1
CCD 1
CMV
CIDS
EMER
1
OIS
AVNCS
PED
POWER
IPRAM
LIGHTS
MAIN
ON/OFF
MENU
LAV
MAINT
SCREEN
3D secLOCK
EVAC
CMD
EVAC
RESET
SMOKE
RESET
FAP-PC
RESET
PAX
SYS
OBRM
CAM
2
ASFC
OSFC
OMT
SCI
A/C
SYSTEMS
MODULE
1
MODULE
2
EFBs
OIS CAB
& MAINT
USB
IFE,
INTERNET PROTOCOL COM,
INTERNAL WIRELESS SYSTEMS
USB PORTS
USB
CAPT & F/O
DOCKING STATION (x2)
Page 129
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
46
ASFC & OSFC MODULES
ASFC
Training by Airbus
OSFC
NOTE
ASFC
AS
ASF
A
SF
S
FC
FC
IMCC IPSM
SMM
ADSM ABPM
ABPM: Avionics Bare Processing Module
ADSM: Avionics Data Storage Module
AVM: Avionics Video Module
AVM
IPSM IMCC SDM ENRM
IMCC: Information Management Common Cabinet
IPSM: Intelligent Power Supply Module
SMM: System Management Module
ODSM
CRM: Communication Router Module
ENRM: Ethernet Network Router Module
IPSM: Intelligent Power Supply Module
NSM: Network Server Module
NSM
CRM VGM
ODSM: Open world Data Storage
Module
SDM: Smart Diode Module
VGM: Versatile Graphical Module
LEDs STATUS
POWER OFF
NORMAL
OPERATION
- STARTING
- CRITICAL OPERATION
- SECURING IN PROGRESS
FAILED
IRREVELANT
STATE
Page 130
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
46
OIS SECURITY ASPECTS - OIS SECURIY SPECIFIC FUNCTIONS
OIS DATA
TO AVNCS
CAB DATA
TO OIS
OFF
OFF
OIS
Training by Airbus
NOTE
AISD
ACD
FLIGHT
DOMAIN
WIRELESS
SYSTEM
A/C
SYSTEMS
SCI
1
ASFC
SDM
ITTY
CUURRRIT
SSEECU
OSFC
RITTY
CUURRIT
SSEECU
2
IFE
GATELINK
OFF
ITTY
SSEECCUUURRRIT
INTERNET PROTOCOL
GROUND NETWORKS
Page 131
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
46
VIDEO GENERATION ARCHITECTURE
Training by Airbus
CDS
312 VU
FLEX
5
140
135
0
EGT
°C
692
10
74. 0
78. 1
83. 9 % 53°C
%
N1
%
PACKS
5
THR
0
10
140
135
EGT
°C
74. 0
78. 1
692
T.O INHIBIT
NO SMOKING
SEAT BELTS
GND SPLRs ARMED
CAPT
EFB
F/O
EFB
CAPT KCCU
ESC
DIR
PERF
INIT
NAV
F/O KCCU
+53°C
CAPT SLIDING
TABLE
C/L
NOTE
F/O SLIDING
TABLE
ENT
0
KBD 2
CCD 1
KBD
CCD 2
ESC
CMV 2
CMV 1
OSFC
VGM 1
VGM 2
ASFC
AVM 1
AVM 2
Page 132
OMT KEYBOARD
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
46
INTER DOMAIN NAVIGATION
Training by Airbus
FLIGHT OPERATIONS HMI MANAGER
NOTE
OIS
OIS
AVNCS
AVNCS
EFB
B
EFB
VIEW
OFFSIDE
VIEW
OFFSIDE
INOP
INOP
ON
ON
ASFC
OSFC
EFB
Page 133
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
46
ONBOARD MAINTENANCE TERMINAL - OMT DESCRIPTION / KEYBOARD STORAWAGE
OMT UNIT
Training by Airbus
OMT KEYBOARD PLATE (COCKPIT)
OMT KEYBOARD
NOTE
ONBOARD MAINTENANCE TERMINAL
ETHERNET PLUG FOR
PMAT INITIALIZATION
CONNECTOR TO PLUG
KEYBOARD-OMT
USB PORT FOR DATA EXPORT
USB PORT FOR DATA IMPORT
Page 134
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
46
PMAT
Training by Airbus
PMAT IS NOT PART OF A/C DEFINITION
PMAT IS A GROUND SUPPORT EQUIPMENT
NOTE
NOTE:
ALL PMAT CONNECTION ARE INHIBITED DURING FLIGHT
1
A350
7
6
3
5
4
10
2
PMAT NETWORK PORT LOCATION
COM
GND
CONNECTION
ON
MAINTENANCE PANEL
1
AVIONIC RACK
2
REAR EBAY
3
FWD LDCC
4
STEERING DISCONNECT PANEL
5
REFUEL PANEL
6
CABIN 1 - DOOR 1
7
CABIN 2 - DOOR 3
10
AFT LDCC
PMAT CONNECTIONS
P-MAT
LIGHT
TEST
EXT PWR 1
AVAIL
EXT PWR 1
NOT IN USE
EXT PWR 2
AVAIL
EXT PWR 2
NOT IN USE
GROUND
POWER PANEL
STEERING
DISCONNECT PANEL
Page 135
COM GND CONNECTION P/BSW HAS TO BE ACTIVATED AND ONLY ONE CONNECTION IS USED AT A TIME
NO POWER SUPPLY CONNECTION ARE AVAILABLE IN THE NOSE LANDING GEAR BAY AT A TIME
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
46
EFB CONNECTION TO DOCKING STATION
NOTE: ALL CONNECTING CABLES BETWEEN
LAPTOP AND DOCKING STATION ARE NOT PART
OF THE AIRCRAFT, THEY ARE UNDER
AIRLINE RESPONSIBILITY
THE FOUR CABLES MUST BE RECONNECTED
EACH TIME YOU WANT TO CONNECT
LAPTOP TO THE EFB
STANDARD PC
INTERFACES
Training by Airbus
NOTE
ETHERNET
USB
VGA OR DVI
POWER
NOTE: VGA OR DVI CAN BE REPLACED BY
VIDEO OVER USB. THEN VGA/DVI CABLE
CAN BE REMOVED
Page 136
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
46
DOCKING STATION CONTROL PANEL
Training by Airbus
NOTE
DOCK STATION
OFF
PWR
SPLY
LAPTOP
ON
START
LED
LABEL & ANNUNCIATOR
LABEL LIGHTING LOGICS
THE LAPTOP DOCKING STATION RECEIVES THE A/C 28VDC POWER SUPPLY FROM A/C
ANNUNCIATOR LIGHTING LOGICS
OFF BUTTON IS ON : DOCKING STATION IS OFF --> PUSH THE OFF BUTTON TO START THE DOCKING STATION
START BUTTON IS ON : LAPTOP IS OFF --> PUSH THE START BUTTON TO START THE LAPTOP
LED LIGHTING LOGICS
PWR SPLY : LAPTOP POWER SUPPLIED BY THE DOCKING STATION
ON : LAPTOP IS OPERATING
Page 137
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
46
LAPTOP START CONFIGURATIONS
PILOT ATTACHED CONFIGURATION
1 / START THE DOCKING STATION
PUSH THE DOCKING STATION P/BSW
A/C ATTACHED CONFIGURATION
Training by Airbus
NOTE
NOTE: IN THIS CONFIGURATION THE LAPTOP IS
ALREADY STOWED IN THE DOCKING STATION
SINCE IT IS ATTACHED TO THE AIRCRAFT SO
THAT CABLES ARE ALREADY CONNECTED
2 / START THE LAPTOP
ON THE LAPTOP, PUSH THE
LAPTOP PWR ON P/BSW
3 / CONNECT CABLES BETWEEN THE LAPTOP AND
THE DOCKING STATION
VIDEO CABLE (IF APPILACABLE)
USE CABLE
ETHERNET CABLE
POWER SUPPLY CABLE
1 / START THE DOCKING STATION
PUSH THE DOCK STATION P/BSW
2 / START THE LAPTOP (FROM THE DOCKING
STATION)
PUSH THE LAPTOP START P/BSW ON
THE DOCKING STATION
Page 138
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
46
INTERNAL WIRELESS DETAILED ARCHITECTURE AND COMPONENTS
Training by Airbus
LEAKY LINE ANTENNAS
WIRELESS
WIRELESS
NOTE
PED
LAPTOP
CONNECTIVITY RACK
RF COMBINER
PASSENGER
CABIN ATTENDANT
PASSENGER DOMAIN
WLU
A350
ON/OFF
RESET
LEAKY LINE
IFE
LIVE TV
CRDC
INTERNET ACCESS
OSFC
OMTS
CABIN
(CCOM, CABIN CREW MAIL)
WIRELESS MANAGER
Page 139
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
46
ATC ARCHITECTURE
Training by Airbus
CDS
BUZZER
CVR
BUZZER
ATC
ATC
MSG
MFD
UPPER CENTERED
DU
ESC
DIR
PERF
INIT
NAV
AID
C/L
MENU
CLR
INFO
F-PLN
DEST
SEC
INDEX
SURV
ATC
COM
NOTE
ATC
MSG
CPIOM
ATC
COM
ATC DATA LINK
AMU
AMU
1
2
0
SPACE
E
KBD 1
CCD 1
KBD
MAIL
BOX
ESC
FWS
AFDX NETWORK
CPIOM
AESU
ACR
ADIRU
ACARS
NETWORK
HF, VHF,
SATCOM
1
FMC
2
A
3
B
C
ATC CENTERS
Page 140
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
46
ASFC / OSFC MODULE MAINTENANCE - FAILED MODULE IDENTIFICATION
IDENTIFICATION OF A
FAILED CABINET MODULE
Training by Airbus
NOTE
1 ASFC MODULE FAILURE
E
1 OSFC MODULE FA
URE
FAILURE
--> DISPATCH MESSAGE
COM > OIS AVNCS REDUNDANCY
--> ASFC in “degraded mode”
--> DISPATCH MESSAGE
COM > OIS CAB & MAINT REDUNDANCY
--> OSFC in “degraded mode”
FAULTY MODULE RECORDED IN PFR
AND SHOWN IN ACTIVE ECAM ALERT
Page 141
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
46
ASFC / OSFC MODULE MAINTENANCE - FAILED MODULE IDENTIFICATION
Training by Airbus
PDMMF
ACMS_SA
1234567890123456789012
ADSM-3
ADSM-4
ABPM-3
ABPM-4
SMM-2
IPSM-2
ADSM-2
ABPM-2
NBF
NAIF
AOC
AMEX
1234567890123456789012
AVM-2
ADSM-1
ABPM-1
NOTE
SMM-1
AVM-1
IPSM-1
FROM OMT (OR OIS DISPLAY/PMAT)
1234567890123456789012
1234567890123456789012
1234567890123456789012
1234567890123456789012
1234567890123456789012
1234567890123456789012
1234567890123456789012
1234567890123456789012
1234567890123456789012
1234567890123456789012
1234567890123456789012
CMS
ABDC
1234567890123456789012
SPP_BA
DLCS_DL
DLCS_CONF
BACK
ASFC MODULES STATUS
OR
HOME
MENU
WORKAREA 1
22-JUL-2009 / 22:00 UTC
WORKAREA 2
WORKAREA 3
WORKAREA 4
WORKAREA 5
QUIT
WORKAREA 6
Application 1 Application 2 Application 3
FAILED
INTERACTIVE BITE
System: OSF
Function:
BACK
LED statuses
PRINT
EXPORT
IPSM2
CRM
VGM2
ENRM2
ODSM4
ODSM3
NSM2
ODSM2
NSM1
SDM
ENRM1
VGM1
IPSM1
ODSM1
LED statuses
PRINTER
MODULE STATUS ON THE MODULE ITSELF
(LED AMBER STATE)
Page 142
OSFC MODULES STATUS
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
46
ASFC / OSFC MODULE MAINTENANCE - REMOVAL / INSTALLATION OF THE MODULE AND RELATED TOOL
WEAR A WRIST STRAP CONNECTED TO THE GROUND TO
DECREASE ELECTROSTATIC DISCHARGE RISK
Training by Airbus
NOTE
CAUTION
WEDGE CLAMP
PRESS TO POWER-OFF
THE MODULE
WEDGE CLAMP
Page 143
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
46
ASFC / OSFC MODULE MAINTENANCE - SMART DIODE MODULE UPLOADING SPECIFIC CONDITION
Training by Airbus
NOTE
SDM
ASFC
OSFC
SDM UPLOADING IN THREE STEPS:
- SDM FRONT FACE USB PORT (HIGH SECURITY S/W)
AVIONICS
SYSTEMS
SCI
SDM
- DLCS (ACD) HMI (SECURITY S/W)
- SDL (OSFC) HMI (OPERATIONAL S/W)
Page 144
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
46
KEY COMBINATIONS
Training by Airbus
NOTE
ASF Back-Up
Maintenance
Menu
Main Maintenance
Menu
AVNCS
SHIFT + OIS
Switch to the last AVNCS
session
(AOC, Maintenance page, ...)
CTRL + OIS
EFB
Main Flight Menu
OIS
EFB display
Page 145
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
46
SECURE COMMUNICATION INTERFACE REMOVAL ANS INSTALLATION
Training by Airbus
NOTE
AVIONICS SYSTEMS
SCI 2
ARINC 429
COMPUTERS
AFDX COMPUTERS
(THROUGH
NETWORK)
ASFC
OSFC
SCI 1
CDAU
ONLY SCI 1 IS CONNECTED TO COMPUTERS WITH AFDX INTERFACES (THROUGH AFDX NETWORK):
AS A CONSEQUENCE, IF THE SCI 1 IS REMOVED, ALL COMMUNICATIONS BETWEEN
THE OIS (ASFC/OSFC) & AFDX NETWORK WILL BE CUT UNTIL THE RE-INSTALLATION OF THE SCI 1
Page 146
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
46
ELECTRONIC FLIGHT BAG LAPTOP MAINTENANCE - MONITORING PAGE HMI
Training by Airbus
NOTE
OK / FAILED STATUS EASY TO
MANAGE BY MAINTAINER
NOT AVAILABLE
NOT AVAILABLE
NOT AVAILABLE
Page 147
Advanced T/S
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
46
Training by Airbus
PRINTER MANAGEMENT
DATA EXPORT - AVAILABLE FILES
NOTE
Page 148
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
46
DATA EXPORT - EXPORT QUEUES
Training by Airbus
NOTE
Page 149
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
46
LINK STATUS
Training by Airbus
NOTE
Page 150
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
46
OIS SYSTEM TEST INTERFACE 1/2
Training by Airbus
NOTE
Page 151
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
46
OIS SYSTEM TEST INTERFACE 2/2
Training by Airbus
NOTE
Page 152
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
46
FAP MAINTENANCE MENU
Training by Airbus
NOTE
Page 153
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
46
ATA 45
ON BOARD MAINTENANCE SYSTEMS
OMS DESCRIPTION - OMS APPLICATIONS & OMS ARCHITECTURE
OMT
411 VU
TAXI
CSTR
WPT
1016
ATC
AUTO
MSG
LAND
DECLUTTER
CHRONO
WX
VORD
NDB
TERR
TRAF
ARPT
CSTR
---
313 VU
-----
WPT
VORD
NDB
WX
TERR
TRAF
AP1
MASTER
WARN
SIDESTICK
PRIORITY
5
0
EGT
°C
692
NORM
VV
CHRONO
DECLUTTER
HUD
F/O
ATC
LAND
MSG
10
74. 0
78. 1
5
THR
%
N1
%
PACKS
0
10
314 VU
140
135
EGT
°C
74. 0
78. 1
692
T.O INHIBIT
NO SMOKING
SEAT BELTS
GND SPLRs ARMED
F/O
ON 3
MAP LT
L/G
AIR DATA
UP
F/O
ON 3
INOP
INOP
ON
OFF
NOTE
LOUDSPEAKER
AUTO
LS
312 VU
83. 9 % 53°C
AVNCS
NORM
APPR
BRAKE
FLEX
ATT HDG
OIS
ALT
311 VU
VLO = VLE
NORM :
250
M 0.55
GRVTY :
250
VFE 1
255
1+F
220
2
212
3
195
186
FULL°
140135
MASTER
CAUT
PLAN
A/THR
PMAT*
1016
ARC
AP2
PLAN
LOC
PRINTER
412 VU
QNH
ARPT
UP
NAV
ARC
VV
LIMIT SPEED
(IAS KT)
MAP LT
7000
NAV
MASTER
CAUT
LS
COCKPIT
HMIs
--FD
SIDESTICK
PRIORITY
CAPT
TAXI
MAG
QNH
MASTER
WARN
HUD
LOUDSPEAKER
ON
OFF
B
R
BRT
FMS
PEDALS LT
ON
NORM
BR
R
BRT
PEDALS LT
ON
BOTH
ON 1
FF
F
OFF
FF
OFF
301 VM
302 VM
MODE
+
MODE
LS/
MENU
SET/SEL
+
MENU
+53°C
DISPLAY
CAPT OIS
F/O OIS
DISPLAY
AVAIL
MAN
INOP
INOP
ON
ON
AVAIL
MAN
CDS
CABIN
HMIs
ONBOARD INFORMATION SYSTEM
AICRAFT CONTROL DOMAIN
FLIGHT
DOMAIN
ASFC
FAP
OSFC
ADS
CMS-ACD
CIDS
EMER
AIRCRAFT
SYSTEMS
DLCS-ACD
SCI
1
Training by Airbus
SDM
PED
POWER
IPRAM
LIGHTS
MAIN
ON/OFF
MENU
LAV
MAINT
SCREEN
3D secLOCK
CAM
EVAC
CMD
EVAC
RESET
SMOKE
RESET
FAP-PC
RESET
PAX
SYS
OBRM
MCA
A/L CABIN
LAPTOP*
2
ACMS
LMF
PDMMF
SDL
PRINTER
Page 154
* = UNDER AIRLINE RESPONSIBILITY
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
45
CMS DESCRIPTION - CMS GENERAL ARCHITECTURE
OMT
CONTROL AND DISPLAY SYSTEM
411 VU
TAXI
CSTR
WPT
1016
MASTER
WARN
AUTO
LAND
CAPT
WX
VORD
NDB
TERR
TRAF
ARPT
SPD
MAG
---
HDG
ALT
---
80
ARC
MASTER
CAUT
V/S
7000
WPT
WX
VORD
NDB
TERR
TRAF
1016
MASTER
WARN
160
ALT
MASTER
CAUT
PLAN
APPR
VV
F/O
AUTO
ATC
LAND
MSG
BRT
LS
312 VU
311 VU
VLO = VLE
NORM :
250
M 0.55
GRVTY :
250
255
220
212
195
186
FLEX
5
VFE 1
1+F
2
3
FULL°
412 VU
QNH
ARPT
80
DN
A/THR
LOC
VV
LIMIT SPEED
(IAS KT)
0
EGT
°C
692
10
74. 0
78. 1
83. 9 % 53°C
%
N1
%
NOTE
PACKS
5
THR
10
0
314 VU
140
135
EGT
°C
74. 0
78. 1
692
T.O INHIBIT
NO SMOKING
SEAT BELTS
GND SPLRs ARMED
F/O
ON 3
BRT
CSTR
AP1
160
PLAN
LS
140135
-----
1000
1000
FD
hPa
SIDESTICK
PRIORITY
ATC
MSG
MAX
313 VU
TAXI
METER
QNH
COCKPIT
HMIs
Training by Airbus
PRINTER
A/BRK
L/G
EFB
BRT
EFB
UP
F/O
ON 3
INOP
INOP
ON
ON
T
PEDALS LT
ON
PEDALS LT
ON
BOTH
ON 1
OFF
OFF
DOWN
301 VM
302 VM
MODE
+
MODE
LS/
MENU
SET/SEL
+
MENU
AVAIL
MAN
SET/SEL
+53°C
INOP
INOP
ON
ON
AVAIL
MAN
PMAT*
ONBOARD INFORMATION SYSTEM - CORE
ACD
ASFC
FLIGHT DOMAIN
FWS
CDS
OSFC
ACD
MAINTENANCE
GLOBAL
MAINTENANCE
FAPs
SCI
1
SDM
2
AIRCRAFT
SYSTEMS
CIDS
EMER
PED
POWER
IPRAM
BITES
AIRLINE FACILITIES
CABIN HMIs
ASFC BITES
FUNCTIONS
OSFC BITES
LIGHTS
MAIN
ON/OFF
MENU
LAV
MAINT
SCREEN
3D secLOCK
CAM
EVAC
CMD
EVAC
RESET
SMOKE
RESET
FAP-PC
RESET
PAX
SYS
OBRM
PRINTER
FUNCTIONS
- ACD FAULT CENTRALIZATION
- A/C FAULT CENTRALIZATION
- ACD REPORT GENERATION
- A/C REPORT GENERATION
- ACD TESTING MANAGEMENT
- A/C TESTING MANAGEMENT
- ACD FAULT DATA STORAGE
- A/C FAULT DATA STORAGE
* = Under Airline Responsability
Page 155
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
45
CMS DESCRIPTION - CMS DETAILED ARCHITECURE AND FUNCTIONS
Training by Airbus
ACD
MAINTENANCE HMIs
NOTE
OTHER SYSTEMS
(LGERS,PCS, ADIRS,
FMS)
ASFC
OSFC
AIRBUS
DOCUMENT SERVICES
(LAST
2 LEGS)
(AirN@v)
MAINTENANCE DATA
LRUs
MEL
MCA
SCI
BITE
CMS-ACD
SDM
LMF
(LAST
20 LEGS)
APPLICATIONS
CDS
BITE
APPLICATIONS
FWS
BITE
WIRELESS SYSTEMS BITE
Page 156
(WACS + CABIN WIRELESS)
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
45
BITE DESCRIPTION - FAULT CODE DESCRIPTION
Training by Airbus
FAULT CODE : UNIQUE IDENTIFIER FOR EACH EVENT
(DISPLAYED IN PFR AND ON LOGBOOK DATA PAGE)
NOTE
E.G.: 2270 F 3KH
FAULT MESSAGE
DU-PFD, F/P (1WK2)/AFDX NETWORK
ATA
LETTER
SEQUENCE
4 DIGITS ATA BREAK-DOWN
FAULT EFFECT CATEGORY
SEQUENCE IN ALPHANUMERIC
W: ECAM WARNING
N: ECAM INOPERATIVE STATUS
F: FAULT MESSAGE
G: FLAG ON CDS
A: ADVISORY ON CDS
D: OTHER FDCE ON CDS
X: LOCAL MONITORED
L: LOCAL + CDS NON MONITORED
C: OBS NON MONITORED AND NOT LOCALIZED
B: OBS OUT OF TSM SCOPE FOR ELECTRONIC
LOGBOOK
Page 157
E: CABIN MALFUNCTION
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
45
DEFERRED ALERTS - ALERTS BY COMBINATION
SINGLE FAULT WITHOUT ALERT
Training by Airbus
ALERTS BY COMBINATION
NOTE
SYSTEM X
FAULT 1
SYSTEM X
MM 1
ASFC
FAULT 1 (EXISTING)
+
FAULT 2 (NEW)
MM 1 & 2
CMS-ACD
MM 1&2/ALERT
CORRELATION
CMS-ACD
FAULT
FWS
ASFC
FAULTS
COMBINATION
FWS
ALERT
ALERT
Page 158
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
45
PFR RECORDING
CAS > 80 Kts
Training by Airbus
OR
NEW FLIGHT NUMBER
ONE ENGINE RUNNING
START PFR BUILD-UP
AND
NOTE
+120s
NO ENGINE OPERATES
STOP PFR BUILD-UP
OR
FLIGHT
FLIGHT
GROUND
80 KTS
LIFT OFF
80 KTS
CRUISE
TOUCH DOWN
CAS < 80 Kts
DURING 150 SEC.
GROUND
PFR BUILD-UP
Page 159
LEG X
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
45
DATA LOADING INTRODUCTION
DATA LOADING
COMPUTERS THAT HOST
FIELD LOADABLE SOFTWARES
FIELD LOADABLE SOFTWARE
IMPORT
LOA
FIELD LOADABLE SOFTWARE
UPLOADING
OAD
FIELD LOADABLE SOFTWARE
CONFIGURATION
REPORTING & VALIDATION
D
L
Training by Airbus
COCKPIT MAINTENANCE HMIs
NOTE
OMT
DATA DOWNLOAD
USB DEVICE
AIRLINE FACILITIES
Page 160
PMAT
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
45
DLCS SUBSCRIBERS
E.G.: DEUs, RBCU, ETC.
E.G.: CIDS DIRECTORS
REMOTE
LRU
AFDX NETWORK
SUBSCRIBERS
Training by Airbus
NOTE
MAINTENANCE HMIs
1
...
UPLOADING ORDERS
X
ASFC
E.G.: ADIRUs, ETC.
AFDX NETWORK
SUBSCRIBERS
DLCS-ACD
1
...
SCI
X
ASFC LOADS
LOAD B
E.G.: AMUs, ETC.
LRU
1
...
Page 161
X
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
45
ONBOARD SOFTWARE DATABASE CONTENT
ASFC OR OSFC
Training by Airbus
NOTE
IMPORTED FIELD LOADABLE SOFTWARE:
DLCS-ACD IN ASFC
OR
SDL IN OSFC
- IMPORTED
&
- AUTHENTICATED
&
- READY FOR UPLOADING.
COPY OF ALL FIELD LOADABLE SOFTWARE
(UPLOADED ONBOARD)
INBOX
REP
Page 162
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
45
SOFTWARE UPLOADING FROM INBOX
Training by Airbus
41
TAXI
TAXI
QNH
CSTR
WPT
1016
WX
VORD
NDB
TERR
TRAF
ARPT
SPD
MAG
---
MASTER
WARN
HDG
TRK
TRK
FP FPA
---
ALT
7000
V/S
CSTR
WPT
WX
-----
VORD
NDB
TERR
TRAF
412 VU
QNH
ARPT
1016
MASTER
WARN
FD
SIDESTICK
PRIORITY
ATC
AUTO
MSG
LAND
ARC
CAPT
AP1
20
CAUT
AP2
320
A/THR
640
LIMIT SPEED
(IAS KT)
313 VU
20
160
10
320
ZOOM
640
CAUT
FLEX
5
0
EGT
°C
692
ATT HDG
F/O
AUTO
ATC
LAND
MSG
VV
312 VU
311 VU
VLO = VLE
250
NORM :
M 0.55
GRVTY :
250
255
220
212
195
186
VFE 1
1+F
2
3
FULL°
140135
10
74. 0
78. 1
83. 9 % 53°C
%
N1
%
PACKS
5
THR
0
10
314 VU
140
135
EGT
°C
74. 0
78. 1
692
T.O INHIBIT
NO SMOKING
SEAT BELTS
GND SPLRs ARMED
L/G
NOTE
T
UP
INOP
INOP
ON
ON
T
301 VM
302 VM
MODE
NEW LOAD A
+
AVAIL
MAN
OMT
NEW LOAD B
NEW LOAD D
PMAT
UPLOADING
ORDERS
ASFC
MODE
LS/
MENU
SET/SEL
+
MENU
+53°C
INOP
INOP
ON
ON
AVAIL
MAN
CDS
MANUAL TRANSFER
MAINTENANCE HMIs UPLOADING
ORDERS
OSFC
DLCS-ACD
SDL
SDM
SECURITY BOX
(AUTHENTICATION)
LRM
NEW LOAD A
SCI
1
INBOX
NEW A
NEW B
...
REP
A
NEW A
B
NEW B
AUTO
TRANSFER
NEW LOAD C
INBOX
NEW C
NEW D
REP
C
NEW C
D
NEW D
X
ASFC LOADS
OSFC LOADS
NEW LOAD C
NEW LOAD B
AIRLINE FACILITIES
NEW LOAD C
WIRELESS SYSTEMS
(WACS + CABIN WIRELESS)
Page 163
NEW LOAD D
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
45
CONFIGURATION REPORTING
CONFIGURATION REPORTING
CONFIGURATION
VALIDATION
ASFC
MAINTENANCE HMIs
CONFIGURATION
FEEDBACK
NEW LOAD A
SCI
1
CONFIGURATION REPORTING
NOTE
CONFIGURATION
VALIDATION
OSFC
DLCS-ACD
LRM
Training by Airbus
INBOX
...
X
REP
A
NEW A
B
NEW B
ASFC LOADS
NEW LOAD B
SDL
SECURITY BOX
(AUTHENTICATION)
CONFIGURATION
FEEDBACK
INBOX
REP
C
NEW C
D
NEW D
OSFC LOADS
NEW LOAD C
WIRELESS SYSTEMS
(WACS + CABIN WIRELESS)
Page 164
NEW LOAD D
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
45
UPLOAD MENUS - DOMAINS
SOFTWARE A
Training by Airbus
SOFTWARE C
B
D
NOTE
ACD (AVIONICS + ASFC)
DLCS-ACD MENU
SOFTWARE UPLOAD
OSFC + WIRELESS SYSTEM
SDL MENU
Page 165
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
45
FILES DOWNLOADING
Training by Airbus
411 VU
TAXI
CSTR
WPT
1016
DECLUTTER
ATC
AUTO
MSG
LAND
WX
VORD
NDB
TERR
TRAF
ARPT
CSTR
---
---
7000
100
FD
SIDESTICK
PRIORITY
CAPT
TAXI
MAG
QNH
MASTER
WARN
PTT
NAV
40
ARC
MASTER
CAUT
80
AP2
WPT
WX
-----
VORD
NDB
TERR
TRAF
1016
SIDESTICK
PRIORITY
NAV
80
ARC
MASTER
CAUT
PLAN
320
DECLUTTER
F/O
AUTO
ATC
LAND
MSG
T
VV
312 VU
311 VU
FLEX
5
0
EGT
°C
692
ATT HDG
CAPT
ON 3
10
74. 0
78. 1
83. 9 % 53°C
%
N1
%
PACKS
FAN
HOT
5
THR
0
ON
10
140
135
EGT
°C
74. 0
78. 1
314 VU
692
NORM
T.O INHIBIT
NO SMOKING
SEAT BELTS
GND SPLRs ARMED
L/G
VIEW
OFFSIDE
T
UP
CAPT
ON 3
VIEW
OFFSIDE
INOP
ON
OFF
BRT
BR
PEDALS LT
ON
OFF
301 VM
MODE
302 VM
LS/
+
PMAT
MODE
LS/
MENU
SET/SEL
+
MENU
SET/SEL
+53°C
DISPLAY
CAPT OIS
F/O OIS
DISPLAY
AVAIL
MAN
INOP
INOP
ON
ON
AVAIL
MAN
CDS
TO USB
DEVICE
OSFC
BRT
BR
PEDALS LT
ON
BOTH
ON 2
OFF
FF
ASFC
CONSOLE LT
INOP
ON
OMT
NOTE
MASTER
WARN
40
A/THR
LIMIT SPEED
(IAS KT)
VLO = VLE
NORM :
250
M 0.55
GRVTY :
250
255
220
212
195
186
VFE 1
1+F
2
3
FULL°
140135
412 VU
QNH
ARPT
1000
PLAN
T
313 VU
OIS
AVNCS
CONSOLE LT
OFF
LRM
SCI
FILES
DLCS-ACD
1
...
X
ASFC
LOADS
FILES
COM MANAGER
AIRLINE
GROUND
FACILITIES
Page 166
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
45
ACMS ARCHITECTURE
Training by Airbus
ACMS
TRIGGER
NOTE
OIS DISPLAY
OMT
CDAU
ASFC
PMAT
PRINTER
ACD
ACMS-RT
LRUs
A/C DATA
A
F
D
X
N
E
T
W
O
R
K
OSFC
ACMS-SA
SDM
SCI
RSA
ABDC
AIRLINE FACILITIES
IFE
EFB LAPTOP
Page 167
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
45
ACMS REPORTS - ACMS REPORTS GROUPS
Training by Airbus
ACMS REPORTS GROUPS
NOTE
A350
STANDARD REPORTS
ON-REQUEST
AIRBUS REPORTS
AIRLINE / SUPPLIERS
PROGRAMMED REPORTS
ONBOARD / ON-GROUND
PROGRAMMED REPORTS
ACMS REPORTS TRIGGERING CONDITIONS
- AUTOMATIC PREDEFINED TRIGGER CONDITION
- MANUAL REQUEST VIA HMI (OMT, PMAT, ETC.)
- ACMS REMOTE TRIGGER BUTTON
- REQUEST FROM THE GROUND (VIA ACARS)
- REQUEST FROM CMS FOR BITE CORRELATION
ACMS REPORTS DATA RETRIEVAL
- DISPLAY ON HMI (OMT, PMAT, ETC.)
- TRAMSMISSION TO THE GROUND
- DOWNLOAD ON USB KEY
- VIA ONBOARD COCKPIT PRINTER
STANDARD REPORTS LIST AND DETAILS
ARE AVAILABLE IN AIRN@V 45-33
SYSTEM DESCRIPTION
Page 168
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
45
POST FLIGHT REPORT
Training by Airbus
NOTE
Page 169
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
45
EFFECT DETAILS
Training by Airbus
NOTE
Page 170
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
45
ACTIVE ECAM ALERTS
Training by Airbus
NOTE
Page 171
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
45
ASFC BACKUP
Training by Airbus
NOTE
Page 172
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
45
Training by Airbus
CMS BACKUP MENU
NOTE
DLCS BACKUP MENU
Page 173
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
45
UPLOAD & CONF VALIDATION - TARGET LIST
Training by Airbus
NOTE
Page 174
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
45
Training by Airbus
ACD CONFIGURATION STATUS
CONFIGURATION HISTORY
NOTE
Page 175
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
45
SOFTWARE REPOSITORY MANAGEMENT
Training by Airbus
NOTE
Page 176
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
45
ACMS MENU
Training by Airbus
NOTE
Page 177
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
45
ATA 34
NAVIGATION
NAVIGATION SYSTEM CONTROLS
ANTI ICE
ADIRS
IR1
FAULT
F
FAU
L
LT
IR3
OFF
OFF
NAV
A
A
AT
ATT
T
ON
ON
ON
A
AT
ATT
T
A
AT
ATT
T
ON
EXT LT
L
NAV
NA
AV
1
DEC
TRGT
INC
OFF
F
OFF
F
OFF
F
OFF
F
WING
ON
LDG
ON
NOSE
T
T.O
OFF
F
OFF
FF
OFF
2
AUTO
MAN
OFF
FAULT
F
FAU
L
LT
A
U
T
O
START
S
INT LT
TRGT
DITCHING
DIM
SEAT BELTS
ON
NO SMOKING
ON
AUTO
OFF
SIGNS
EMER
EXIT LT
ON
AUTO
OFF
ARM
TAXI
TAXI
OFF
QNH
OFF1013
CSTR
WPT
VORD
NDB
1013
VOR
WX
TERR
TRAF
OFF
ADIRS CONTROL PANEL
NOTE
ON
DN
BRT
IND
OFF
AVAIL
ON
MAN
UP
A
U
T
O
ANN LT
TEST
FAULT
ON
215 VM
CABIN V/S
MODE
MODE
MASTER SW
MAS
T
TAXI
FAULT
F
FAU
L
LT
ADR3
OFF
A
U
T
O
APU
A
LOGO
ON
ADR2
ADR1
FAULT
F
FAU
L
LT
CABIN ALT
PROBE &
WINDOW HEAT
BEACON
ON
AUTO
NAV
A
OFF
NAV
A
OFF
FAULT
STROBE
ON
OFF
FAULT
F
FAU
L
LT
OFF
2
1
FAULT
IR2
ON BAT
FAULT
F
FAU
L
LT
ENG
WING
FAULT
Training by Airbus
CABIN PRESS
ARPT
hPa
in Hg
NAV
80
160
20
PLAN
LS
LS
40
ARC
VOR
VV
10
320
ZOOM
640
CAPT EFIS CTRL PANEL
ESC
DIR
CLR
INFO
Q
F-PLN
W
.
A
/
E.
S.
Z
OIS
R
D
X
ND
T
F
C
MFD
INIT
DEST
SEC
INDEX
Y
U
G
V
MAIL
BOX
PERF
H
B
C/L
MENU
SURV
ATC
COM
I
J
N
.
NAV
AID
O
K
M
T.O
CONFIG
P
SPACE
EMER
M
AN
CANC
DEFRD
NOTE
PAD
L
ENT
RCL
ALL
DISPCH
1
2
3
4
5
6
7
.
8
9
0
+/-
SPACE
KBD
CAPT KCCU
ABN
RCL
LAST
SD
MORE
STS
ENG
DOOR
WHEEL
FUEL
EL/AC
EL/DC
HYD
F/CTL
APU
BLEED
COND
PRESS
CLEAR
ALL
VIDEO
VIDEO
CLEAR
ECAM CONTROL PANEL
ESC
Page 178
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
ADIRS START PROCEDURE (ALIGN ON GPS POSITION)
Training by Airbus
NOTE
Page 179
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
PROBES DESCRIPTION - LOCATION
Training by Airbus
MFP
(AOA, TAT, Pt)
WING VANE
FOR AOA
NOTE
PITOT PROBE
FOR Pt
TUBE FOR
TAT
ADIRU
MFP1
MFP3
ADR
1
PFCS AOA
AOA
PROBE
ISP (Ps)
MFP2
ADIRU
WING VANE
E
FOR AOA
A
ADR
ISP
2
ISP
ISP
ADIRU
ISP
ADR
OAT SENSOR
3
ISP
ISP
IF POWER SOURCE IS LOST, ADIRUs
REVERT TO HOT BUS
OAT1
AT1
OA
OAT2
Page 180
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
ANTI - ICING FUNCTION
Training by Airbus
NOTE
PROBE ANTI-ICING LOGIC ACTIVATION
AUTOMATIC MODE
ONE ENGINE RUNNING
GS > 30kts
IN FLIGHT
ADIRU
MFP1
MFP3
ADR
1
AOA
PROBE
OR
OR
MANUAL MODE
(ON GROUND)
PROBE/WINDOW
HEAT P/BSW
PROBE
ANTI-ICING
ACTIVATION
MFP2
ADIRU
ADR
ISP
2
ISP
ISP
MANUAL ANTI-ICING
ISP
ADIRU
PROBE &
WINDOW HEAT
ON
A
U
T
O
ADR
3
ISP
ISP
PROBE
OAT2
OAT
ADR
ANTI-ICING AND TEST ACTIVATION
AIR DATA
OAT1
AT1
ADIRU
BITE
OPERATIONAL AND BITE DATA
Page 181
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
COMPUTATION & INTERFACE
ICP ADIRS
ADIRS
IR1
OFF
FAULT
OFF
NAV
ATT
NDs
MFDs
OFF
CONTROLS
STATUS & SWITCHING
TRAFFIC
CONTROLS
WXR
ATT
ATT
ELEVN/TILT
WXR/PWS
TURB
AUTO
AUTO
OFF
OFF
TERR
SYS
ADR2
ADR1
FMS
FAULT
ADR3
OFF
OFF
FAULT
GAIN
WX
AUTO
MAP
MAN
ON
OFF
AUTO
A RPTG
ALT
adS-B
RPTG
2000
ON
STBY
ON
OFF
adS-B
TA/RA
NORM TRAFFIC
TA ONLY
ABV
STBY
BLW
ON
OFF
ELEVN
TILT
FL 0
ON
OFF
IDENT
%
FLAP
MODE
OFF
TCAS
A
ON
OFF
SURV
DEFAULT
SETTINGS
CLEAR
INFO
B
C
PROBES
AFDX NETWORK
AOA
ADIRU
BARO-SETTING
CRDC
OAT
PFCS
ADR
GPS DATA
CPIOM
IR
IRS
FCU
BACK-UP
1
2
VMO/MMO
SEL SW
ISIS
MODE
LS/
MODE
LS/
+
BARO-SETTING
3
PRIM
1
2
3
LGERS
AIR DATA
AUTO
CAPT ON
BKUP
F/O ON
BKUP
SWITCHING
PANEL
FCU
TAXI
QNH
1016
TRUE
+
MMR
ON
SQWK
FMC
MFP
G/S
MODE
GPWS
XPDR
OFF
ISP (Ps)
TAWS
ON
OFF
AUTO
MODE
0
FAULT
NOTE
SURV
NAV
NAV
OFF
PFDs
FAULT
IR3
OFF
OFF
IR2
ON BAT
FAULT
Training by Airbus
CDS
MAG
in Hg
hPa
Page 182
MLS
TOE
1
2
MLS
MENU
TOE
SET/SEL
MENU
SET/SEL
LS
VV
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
ADIRS SWITCHING PANEL - NAIADS
CDS CAPT SIDE
HUD
Training by Airbus
CDS F/O SIDE
AIR DATA
AUTO
CAPT ON
BKUP
F/O ON
BKUP
NOTE
CRDC
SOURCE SELECTION
SOURCE SELECTION
ADIRU + ISIS + BACKUP DATA
ADIRU + ISIS + BACKUP DATA
AFDX NETWORK
ADR AND
IR DATA
ISIS & BACKUP DATA
ISIS
SOURCE SELECTION
LS/
MODE
MODE
ISIS
SPD & ALT & ATT
PFCS
CPIOM
PRIM
EIF
2
MLS
TOE
MLS
MENU
TOE
BACKUP
SPD & ALT
ADR
SET/SEL
MENU
ADIRU 3
IR
+
1
3
ADIRU 1
ADR
LS/
+
SET/SEL
ADIRU 2
IR
ADR
Page 183
IR
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
COMPONENTS LOCATION
Training by Airbus
NOTE
A
L/G DOWN VMO / MMO
SELECTION SELECTOR
SWITCH
27FP
A
1FP3
ADIRU -3
Page 184
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
GENERAL
Training by Airbus
NOTE
STANDBY COMPASS
STANDBY
STAN
PITOT
PITO PROBE
RH STANDBY
STATIC PROBE
LS/
MODE
LH STANDBY
STATIC PROBE
LS/
MODE
TOTAL PRESSURE
+
+
STATIC PRESSURE
GPIR3 N48 15,5/W003 32,3
MENU
SET/SEL
MENU
ISIS
STATIC WLI
411 VU
TAXI
MACH SPD SPD
QNH
MASTER
WARN
LOUDSPEAKER
OFF
CHRONO
ATC
AUTO
MSG
LAND
SIDESTICK
PRIORITY
CAPT
M
MAX
A
CSTR
WPT
1016
in Hg
VORD
WX
NDB
TERR
40
ARC
MAG
HDG
HDG
HDG
V/SV/S
320
640
CSTR
-----
WX
VORD
TERR
NDB
10
APPR
1016
160
320
ARC
VOR
VV
SIDESTICK
PRIORITY
LOUDSPEAKER
CHRONO
F/O
AUTO
ATC
LAND
MSG
OFF
LS
MAX
M
312 VM
FLEX
5
0
EGT
°C
10
74. 0
78. 1
83. 9 % 53°C
%
N1
%
PACKS
5
THR
0
10
140
135
EGT
°C
74. 0
78. 1
314 VU
692
T.O INHIBIT
NO SMOKING
SEAT BELTS
GND SPLRs ARMED
OIS
A/BRK
MAP LT
L/G
AIR DATA
AUTO
MASTER
WARN
MASTER
CAUT
PLAN
LS
BRAKE
AVNCS
CAPT ON
BKUP
hPa
NAV
80
ZOOM
311 VU
VLO = VLE
250
NORM :
M 0.55
GRVTY :
250
255
220
212
195
186
VIEW
OFFSIDE
412 VU
QNH
ARPT
TRAF
in Hg
40
20
ALT
WPT
UP
DN
692
CONSOLE LT
1000
1000
100
100
AP2
A/THR
LOC
OIS
MAP LT
V/S
7000
AP1
10
ZOOM
VFE 1
1+F
2
3
FULL°
140
135
TAXI
METER
ALT
TRK
TRK
FPAFPA
---
80
160
20
PLAN
VV
LIMIT SPEED
(IAS KT)
313 VU
TRUE
TRUE MAG MAG
SPD
---
FD
NAV
VOR
LS
LS
ARPT
TRAF
hPa
MASTER
CAUT
SET/SEL
ISIS
PITOT WLI
BRT
B
R
UP
F/O ON
BKUP
VIEW
OFFSIDE
INOP
CONSOLE LT
INOP
ON
ON
BRT
B
R
FMS
PEDALS LT
ON
BOTH
ON 2
NORM
PEDALS LT
ON
BOTH
ON 1
301 VM
MODE
302 VM
LS/
+
MENU
SET/SEL
+53°C
DISPLAY
CYCLE
CAPT OIS
ON CENTER
F/O OIS
ON CENTER
DISPLAY
CYCLE
AVAIL
INOP
INOP
AVAIL
ON
ON
Page 185
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
AFDX NETWORK
STATUS AND WARNING
DATA
CPIOM
1
TRAFFIC
CONTROLS
WXR
ELEVN/TILT
TURB
WXR/PWS
AUTO
OFF
GAIN
WX
AUTO
OFF
MAP
MAN
0
MFD
TERR
SYS
GPWS
ON
ON
OFF
AUTO
MODE
AUTO
TAWS
G/S
MODE
ON
ELEVN
TILT
%
FL 0
FLAP
MODE
ON
OFF
OFF
OFF
AUTO
ALT RPTG
A
adS-B
RPTG
XPDR
SQWK
2000
IDENT
ON
ON
ON
STBY
OFF
OFF
TCAS
TA/RA
adS-B
NORM TRAFFIC
TA ONLY
ABV
ON
STBY
BLW
OFF
2
IR+GPS+PROBE
DE-ICING
AUTOMATIC
DATA
STATUS & SWITCHING
SURV
DEFAULT
SETTINGS
PRIM
CPCS
MODE
AUTO ANTI-ICING
ACTIVATION
SPD
---
MAG
HDG
HDG
HDG
V/SV/S
ALT
TRK
TRK
FPAFPA
V/S
7000
AP1
1000
1000
100
100
FD
-----
AP2
A/THR
ALT
MODE
LS/
MENU
SET/SEL
MMR 1
+
APPR
FCU
STATIC PRESSURE
AUTO ANTI-ICING
PROBE &
ACTIVATION
WINDOW HEAT
ON
115VAC
3
UP
DN
LOC
SET/SEL
AUTOMATIC
RECONFIGURATION
METER
---
2
LS/
GPIR3 N48 15,5/W003 32,3
MENU
TRUE
TRUE MAG MAG
1
+
CLEAR
INFO
MACH SPD SPD
NOTE
CRDC
ADIRU
EIF
SURV
CONTROLS
Training by Airbus
TOTAL
PRESSURE
FCU BACK-UP
PAGE
STANDBY NAVIGATION SYSTEM INTERFACES
S
STANDBY
S
STATIC
L
LEFT
115VAC
S
STANDBY
S
STATIC
R
RIGHT
115VAC
S
STANDBY
P
PITOT
P
PROBE
A
U
T
O
MANUAL
ANTI-ICING
ACTIVATION
Page 186
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
INTEGRATED STANDBY INSTRUMENT SYSTEM (ISIS)
MODE
LS/
+
NOTE
LEVELING
RESULT : OK
+
LRU IDENT
ENGINEERING DATA
FUNCTIONAL TESTS
INPUT STATUS TESTS
DISPLAY TESTS
AIR DATA TESTING
BORESIGHTING
PITCH
ROLL
ADIRU 3 +00.90°
+00.40°
ISIS
return
MENU
LS/
MODE
MAINTENANCE
Training by Airbus
+00.90°
+00.40°
return
SET/SEL
MENU
MAINTENANCE MENU
MODE
BORESIGHTING RESUTL
LS/
340
+
SET/SEL
135
320
AIR DATA
300
130
TESTING
280
IN PROGRESS
12820
00
260
. 57
PUT ISIS1 AND 2
IN THIS MODE
BEFORE TESTING
125
29.92
return
MENU
SET/SEL
Page 187
AIR DATA TESTING IN PROGRESS
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
GNSS FUNCTION DESCRIPTION
GNSS SATELLITES
FMS
Training by Airbus
CDS
PFD
ND
PFD
ND
NOTE
A/C POSITION
A/C POSITION
F/O EFIS
CAPT EFIS
AFDX NETWORK
SURV
CONTROLS
STATUS & SWITCHING
CONTROLSSURV
WXR
WXR/PWS
AUTO
OFF
CONTROLS
TURB
TURB
WXR/PWS
AUTO
TAWS
OFF
ON
TERROFF
SYS
OFF
G/S
MODE
ON
TA ONLY
STBY
CLEAR
INFO
ON
OFF
ALT
A
RPTG
AUTO
IDENTNORM
ABV
BLW
0
%
FL 0
adS-B
RPTG
ON
XPDR
STBY
SQWK
TCAS
2000
TA/RA
FL 0
FLAP
MODE
GPWS
OFF AUTO
2000
%
FLAP
MODE
TAWS
XPDR
ON
IDENT
0
AUTO
GPWS
ON
OFF
SQWK
A/C POSITION
ELEVN/TILT
CONTROLS
AUTO
OFF WXR
TERR
SYS
CRDC
TRAFFIC
STATUS & SWITCHING
MODE
GAIN
ON
adS-B
TRAFFIC
STBY
OFF
ALT RPTG
OFF
adS-B
RPTG
ON
ON
OFF
OFFSURV
TCAS ON
DEFAULT
SETTINGS
adS-B
TRAFFIC
TA/RA
NORM
TA ONLY
ABV
ON
STBY
BLW
OFF
SURV
DEFAULT
SETTINGS
CLEAR
INFO
MFDs
A/C POSITION
MMR
ADIRS
IRS POSITION
ILS
GNSS
FLS
GLS
GNSS INITIALIZATION
GNSS DATA
GNSS ANTENNA 1
(POSITION, VELOCITY, TIME)
ISIS
MODE
LS/
MODE
GNSS ANTENNA 2
MIX LOC
/VNAV
GNSS DATA
SLS
1
+
+
MENU
2
Page 188
SET/SEL
MENU
SET/SEL
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
LS FUNCTION DESCRIPTION
Training by Airbus
RMP
VHF
HF
TEL
121.700
MSG
CLR
SQWK
MENU
NAV
STBY
VHF1
TEL
121.900
123.125
VHF2
123.450
DATA
VHF3
DATA
HF
CALL
CALL
CALL
CALL
CALL
2
3
4
5
7
8
9
.
0
CLR
.
6
RST
3
ATT
INTCALL CAB .
INT
VOICE
PA 0
CLR
1
RAD
1
INT
NAV
CAB
VOICE
2
PA
MKR
CALL
VHF3
NOTE
123.450
RST
DATA
1
MECH
CALL
FMS
NAV
STBY
VHF 1 RECEPTION NOT SELECTED
CALL
MENU
121.900
ADF
1
1
CDS
LS CONTROL
GNSS SATELLITES
2
MKR
PFD
ND
SURV
CONTROLS
STATUS & SWITCHING
CONTROLSSURV
WXR
CONTROLS
TURB
WXR/PWS
AUTO
OFF
TRAFFIC
ELEVN/TILT
TRAFFIC
STATUS & SWITCHING
MODE
GAIN
AUTO
CONTROLS
AUTO
WX
OFF WXR MAP
AUTO
TURB
MODE
0 %
GAIN
FL 0
WX
MAP
FLAP
MODE
AUTO
G/S
MODE
GPWS
OFF
G/S
MODE
WXR/PWS
TAWS
TERR
SYS
GPWS
ELEVN
SYS
0
ON
2000
ON
OFF
ON
OFF
SQWK
TA ONLY
ILS
BLW
ON
OFF
TCAS ON
OFF
OFFSURV
DEFAULT
SETTINGS
adS-B
TA/RA
NORM TRAFFIC
TA ONLY
ABV
STBY
BLW
SURV
DEFAULT
SETTINGS
ON
OFF
CLEAR
INFO
CAPT EFIS
GNSS
PFD
GNSS ANTENNAS
MFD
ND
ESC
DIR
CLR
INFO
Q
PERF
F-PLN
W
.
E.
A
/
R
S.
Z
OIS
ND
F
X
C
V
A
S.
D
MFD
MAIL
BOX
Y
G
OIS
GLS
ND
MFD
U
H
B
NAV
AID
INIT
SEC
INDEX
DEST
T
D
BOX
C/L
ATC
COM
SURV
I
DEST
J
N
.
M
H
NAV
AID
P
O
K
G
B
OIS
MENU
FLS
ON
adS-B
TRAFFIC
ABV
STBY
CLEAR
INFO
adS-B
RPTG
ALT RPTG
TCAS
2000
MMR
ELEVN
TILT
FL 0
%
FLAP
MODE
adS-B
OFF
RPTG
SQWK
AUTO
MAN
ON
XPDR
ELEVN/TILT
TILT
MAN
NOTE
COM
PAD
L
I
SPACE
ENT
1
2
O
3
4
5
6
7
8
9
0
MENU
KBD
.
6
8
9
0
+/-
ESC
ESC
SPLITTER 1
DGPS LOC
ANTENNA
3
+/7
GROUND
EQUIPMENT
NOTE
PAD
ENT
.
GLIDE SLOPE
ANTENNA
P
2
MIX LOC/VNAV
F/O EFIS
SLS
1
KCCU
Page 189
2
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
LS FUNCTION : ILS
QNH
CSTR
1016
in Hg
WPT
VORD
NDB
WX
TERR
TRAF
ARPT
DISPLAY CONTROL
PFDs
NDs
hPa
NAV
VOR
40
ARC
80
160
20
PLAN
LS
LS
Training by Airbus
CDS
TAXI
VV
SURV
CONTROLS
STATUS & SWITCHING
10
320
CONTROLS
WXR
ZOOM
640
WXR/PWS
TURB
AUTO
AUTO
EFIS CONTROL PANEL
HUD
OFF
TERR
SYS
TAWS
ON
AUTO
ON
OFF
MAN
ILS DATA
SQWK
AUTO
2000
ON
IDENT
STBY
ALT RPTG
A
adS-B
RPTG
ON
ON
A
/
FL 0
OIS
S.
NAV
AID
PERF
INIT
F-PLN
DEST
SEC
INDEX
T
Y
U
R
D
F
Z
X
C
ND
MFD
MAIL
BOX
G
H
V
B
O
J
N.
K
OIS
MENU
P
L
M
NOTE
C/L
ATC
COM
SURV
I
SPACE
NOTE
PAD
ENT
1
2
4
5
7
8
9
0
+/-
.
3
6
OFF
adS-B
NORM TRAFFIC
TA ONLY
ABV
STBY
BLW
ON
OFF
SURV
DEFAULT
SETTINGS
KBD
ESC
CLEAR
INFO
G/S DATA
MFDs
LANDING MODE
TUNING
KCCUs
ILS DATA
TUNING
(BACK-UP CONFIGURATION)
AFDX NETWORK
FGES
VHF
MMR
ILS DATA
HF
TEL
FREQ
SQWK
MENU
NAV
CRS
ILS
108.10
350
ACTIVE
GLS >
ILS
GNSS
ILS DATA
LOC ANTENNA
SPLITTER 1
E.
MENU
TCAS
TA/RA
ELEVN
ON
OFF
OFF
%
W
.
TILT
FLAP
MODE
OFF
XPDR
Q
AUTO
WX
MAP
G/S
MODE
GPWS
ON
OFF
(TAWS)
FMS
OFF
DIR
CLR
INFO
ELEVN/TILT
GAIN
0
AESS
ESC
TRAFFIC
MODE
2
LOC AND G/S
DEVIATION
FLS
MLS >
CRDC
GLS
ILS TUNING
GLIDE SLOPE ANTENNA
MIX LOC/VNAV
SLS
RST
CALL
CALL
CALL
VHF1
HF1
TEL1
CALL
CALL
CALL
CALL
VHF3
INT
1
2
3
4
5
6
7
8
9
.
0
CLR
MECH
ATT
INT
CAB
RAD
D
RMPs
1
ILS GROUND
STATIONS
MSG
CLR
.
BRT
.OF
OFF
VOICE
PA
1
1 VOR
R
2
MKR
AUDIO
MANAGEMENT
2
ISIS
MODE
LS/
MODE
AUDIO GROUND STATION
IDENTIFICATION
+
+
ILS DATA
MENU
SET/SEL
MENU
SET/SEL
AMU
1
RAIMS
2
Page 190
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
GLOBAL NAVIGATION SATELLITE SYSTEM (GNSS) & INSTRUMENT LANDING SYSTEM (ILS)
Training by Airbus
NOTE
Page 191
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
MMR & ILS CONTROL AND INDICATING
PRIMARY FLIGHT
DISPLAY (PFD)
SPEED
ALT
Training by Airbus
MULTIFUNCTION DISPLAY
(MFD)
NAVIGATION DISPLAY (ND)
NOTE
AP1+2
1FD2
550 A/THR
HDG
MDA
6
240
20
030
20
2
1
220
10
10
1 3 6 20
0252 5 00
200
1 1 4 80
10
10
20
20
180
30
160
MANUAL
TUNING
1
020
30
2
6
QNH 1013
760 M
34
35
0
1
2
BACKUP TUNING
NAV PAGE
P/B
RMP
VHF
HF
TEL
SQWK
MENU
NAV
NAV
LS >
ROTARY
SELECTOR
SW
VOR >
ADF >
MSG
CLR
RST
CALL
CALL
CALL
VHF1
HF1
TEL1
CALL
CALL
CALL
VHF2
HF2
TEL2
1
2
3
4
5
6
7
8
9
.
0
CLR
MECH
CALL
VHF3
INT
INT
.
.OF
OFF
BRT
ATT
CAB
NAV BACK-UP
P/B
VOICE
PA
ADF
1
NAV SYSTEMS
AUDIO CONTROL
NAV
1 VOR
R
2
MKR
ST
STB
STBY
TBY
ADF 2
RAD
1
NAV
EFIS CP
TAXI
TAXI
Std
VOICE
in Hg
CSTR
WPT
VORD
NDB
ARPT
VOR1
WX
TERR
TRAF
ADF2
hPa
ESC
NAV
VOR
LS
LS 1
POSITION / NAVAIDS PAGE
VOR
R
2
MKR
LS
VV
ARC
PLAN
40
20
2
KBD
80
10
320
ZOOM
640
5
7
8
9
0
+/-
.
160
3
4
CCD
6
KBD
ON
ON
OFF
OFF
OF
FF
KCCU
Page 192
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
ANF DESCRIPTION - CONTROL
Training by Airbus
RUNWAY ADVISORIES (IN ADDITION OF CDS ADVISORIES)
CDS OUTER DU
CDS INNER DU
CDS CORE
SOFTWARE
ANF
ND
CAPT HUD
ESC
DIR
CLR
INFO
ND CAPT
Q
PERF
F-PLN
W
.
A
/
OIS
OIS
MENU
E.
S.
R
D
X
C
ND
MFD
MAIL
BOX
Y
G
V
SEC
INDEX
DEST
T
F
Z
U
H
B
NAV
AID
INIT
ESC
ATC
COM
O
K
M
Q
NOTE
PAD
3
1
2
3
5
6
4
5
6
7
8
9
7
8
9
0
+/-
0
+/-
10
320
ZOOM
640
NAV
OANS
A/C GPS
POSITION
MMR
ARC
VOR
ESC
CAPT
F/O
C/L
ATC
COM
SURV
I
J
N
.
O
K
ND F/O
P
NOTE
PAD
L
M
SPACE
MAIL
BOX
MFD
ENT
ND
OIS
OIS
MENU
MENU
KBD
ESC
C
F/O KCCU
ADIRU
LGERS
PLAN
LS
.
U
H
B
NAV
AID
INIT
Y
G
V
SEC
INDEX
DEST
T
F
C
2
CAPT KCCU
160
R
D
X
4
KBD
80
E.
S.
Z
1
CAPT
F/O
PERF
F-PLN
W
.
A
/
ENT
MENU
40
DIR
CLR
INFO
P
L
SPACE
.
20
F/O HUD
ANF UADF
SOFTWARE
C/L
SURV
I
J
N.
NOTE
FCU
EFIS
CONTROL PANEL
A/C GPS POSITION
GROUND SPEED
FLIGHT/
GROUND
TAXI
QNH
CSTR
WPT
1016
in Hg
TRAF
NDB
ARPT
TRAF
40
ARC
PLAN
LS
VV
40
20
NDB
TERR
VORD
WX NAV
TERR
WPT
VOR
LS
VORD
WX
hPa
CSTR
TAXI
QNH
160
20
320
640
640
PLAN
LS
VV
AFS
TRUE
TRUE
AUTOMATIC
AIRPORT
SELECTION
hPa
ARC
VOR
160
1016
in320
Hg
10
NAV
ZOOM
80
10
ZOOM
AFDX NETWORK
ARPT
80
MAG
HDG
---
LS
CRDC
SELECTED RANGE
DISPLAY MODE
TRUE/MAGNETIC
NORTH REFERENCE
BTV
ROP / ROW
T.O SURV
FMS
FMC
PFCS
FWS
OANS AMDB
DLCS
OVERHEAD PANEL
PRIM
Page 193
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
ANF NORMAL OPERATION
CAPT EFIS CONTROL PANEL
TAXI
TAXI
QNH
1013
CSTR
WPT
VORD
VOR
WX
TERR
1013
NDB
TRAF
ARPT
NAV
VV
40
ZOOM
640
NAV
AID
C/L
MENU
ESC
DIR
PERF
INIT
NAV
AID
SURV
ATC
COM
CLR
INFO
F-PLN
DEST
SEC
INDEX
SURV
Y
U
Y
U
/
Z
OIS
X
ND
C
MFD
G
V
MAIL
BOX
H
B
1013
J
N
.
K
M
Q
P
NOTE
PAD
L
SPACE
W
.
A
S.
/
ENT
E.
Z
R
D
X
1
2
3
1
2
3
5
6
4
5
6
7
8
9
7
8
9
0
+/-
0
+/-
.
.
CAPT KCCU
G
V
H
B
I
J
N
.
80
160
10
320
ZOOM
640
LS
ARC
PLAN
VV
LS
CURSOR
A/C SYMBOL
ATC
COM
O
K
P
NOTE
PAD
L
M
SPACE
MAIL
BOX
MFD
ENT
ND
NOTE
ZOOM POSITION
OIS
SPACE
SPACE
KBD
F
C
4
T
hPa
40
20
C/L
MENU
INIT
O
VOR
160
640
SEC
INDEX
I
80
ZOOM
DEST
F
ARPT
1013
NAV
320
PERF
D
TRAF
10
DIR
S.
TERR
320
F-PLN
A
WX
20
160
20
ESC
T
VOR
10
PLAN
CLR
INFO
R
NDB
TAXI
QNH
AIRPORT MAP
LS
E.
VORD
80
40
ARC
VOR
W
.
WPT
TAXI
in Hg
LS
Q
CSTR
hPa
in Hg
Training by Airbus
F/O EFIS CONTROL PANEL
ESC
KBD 1
KBD 2
CCD 1
CCD 2
KBD
ESC
F/O KCCU
OIS
ND
MFD
MAIL
BOX
SOFT CONTROL PANEL
Page 194
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
VOR / MKR / DME / ADF DESCRIPTION - INTERFACES
Training by Airbus
HUDs
PFDs
NDs
MFDs
KCCUs
ESC
DIR
CLR
INFO
Q
PERF
F-PLN
W
.
A
E
.
S
.
R
D
/
Z
X
C
OIS
ND
MFD
MAIL
BOX
Y
G
V
U
H
B
NAV
AID
INIT
SEC
INDEX
DEST
T
F
N
.
O
K
M
OIS
MENU
C/L
ATC
COM
SURV
I
J
P
L
NOTE
NOTE
PAD
SPACE
ENT
1
2
3
4
5
6
7
8
9
.
0
+/-
MENU
ESC
CDS
DATA PARAMETERS
STATUS
INFORMATION
FROM VOR/MKR
FMS
FMC
A
B
VOR/MKR or
ADF or DME
DATA
AFDX NETWORK
DME ANTENNAS
ADF ANTENNAS
TUNING
SELECTION
INFORMATION
DGPS LOC ANTENNA
SPLITTER 1
SPLITTER 1
C
CRDC
TUNING SELECTION
TO PORT A
VOR/MKR or ADF or DME
(MKR ACTIVE ONLY
VOR/MKR or ADF or DME DATA
ON VOR 1)
1
TUNING
SELECTION
FROM FMCs
VHF
HF
TEL
SQWK
MENU
NAV
TUNING
SELECTION
STBY
MSG
CLR
121.700
VHF1
121.900
123.125
VHF2
123.450
DATA
VHF3
DATA
CALL
CALL
CALL
CALL
CALL
1
2
3
4
5
6
7
8
9
.
0
CLR
MECH
RMPs
RST
VHF 1 RECEPTION NOT SELECTED
CALL
BRT
.
.OFF
OF
ATT
VOICE
INT
CALL
ADF
1
TO PORT B
PORT A/B SELECTION
2
GROUND
STATION
IDENTIFICATION
MARKER ANTENNA
MARK
AUDIO MANAGEMENT
AMU
Page 195
1
2
MKR
1
2
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
ADF OPERATION & VOR / DME OPERATION
ESC
CLR
INFO
Q
W
.
A
/
E.
OIS
F-PLN
DEST
SEC
INDEX
Y
U
T
D
X
F
C
G
V
INIT
H
B
J
N
.
ATC
COM
O
K
DIR
PERF
INIT
NAV
AID
C/L
MENU
F-PLN
DEST
SEC
INDEX
SURV
ATC
COM
P
NOTE
PAD
L
M
Training by Airbus
C/L
MENU
SURV
I
SPACE
MAIL
BOX
MFD
ND
PERF
R
S.
Z
DIR
NAV
AID
ENT
1
2
3
4
5
6
7
8
9
0
+/-
.
NOTE
TAXI
TAXI
QNH
1013
CSTR
WPT
VORD
NDB
VOR
WX
TERR
TRAF
1013
hPa
in Hg
NAV
VOR
LS
SPACE
ARPT
LS
VV
ARC
PLAN
40
20
80
160
10
320
ZOOM
640
CAPT EFIS CTRL PANEL
KBD
ESC
CAPT KCCU
VHF
MSG
CLR
HF
TEL
SQWK
MENU
NAV
STBY
121.700
VHF1
121.900
123.125
VHF2
123.450
DATA
VHF3
DATA
RST
VHF 1 RECEPTION NOT SELECTED
CALL
CALL
CALL
VHF1
HF1
TEL1
CALL
CALL
CALL
VHF2
HF2
TEL2
CALL
INT
1
2
3
4
5
6
7
8
9
.
0
CLR
MECH
ATT
INT
CAB
VHF3
RAD
NAV
BRT
.
.OF
OFF
LOAD
VOICE
PA
ADF
1
CAPT RMP
1
2
MKR
Page 196
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
ADF OPERATION & VOR / DME OPERATION
NAV KEY
FREQ
POSITION / NAVAID PAGE
ON MFD TYPICAL LAYOUT
VHF
HF
TEL
SQWK
MENU
Training by Airbus
LS PAGE ON RMP SCREEN
TYPICAL LAYOUT
108.10
NAV
ILS
ACTIVE
NOTE
CRS
350
GLS >
LINE SELECTION KEY
MSG
CLR
NAV PAGE ON RMP SCREEN
TYPICAL LAYOUT
RST
CALL
CALL
CALL
VHF1
HF1
TEL1
CALL
CALL
CALL
VHF2
HF2
TEL2
CALL
INT
1
2
3
4
5
6
7
8
9
.
0
CLR
MECH
ATT
INT
CAB
VHF3
RAD
NAV
RMP
NAV
.
BRT
.OF
OFF
NUMERIC KEYBOARD
VOR >
ADF >
VOICE
PA
ADF
1
LS >
1
VOICE MODE KEY
RAD NAV RECEPTION KNOB
2
MKR
RAD NAV SELECTOR SW
TYPICAL LAYOUT
RAD NAV
STBY KEY
Page 197
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
RADIO ALTIMETER INTERFACE - FLIGHT CONTROLS SYSTEM - TAWS
CDS
CDS
Training by Airbus
RADIO HEIGHT INFORMATION
NOTE
140
135
AESS
RA ANTENNAS 1
RA TRANSCEIVER 2
TAWS
PFDs
NDs
RA TRANSCEIVER 1
RA ANTENNAS 2
RA TRANSCEIVER 3
PCS
RA ANTENNAS 3
AFDX NETWORK
CRDC
SEC
RADIO HEIGHT DATA
RA RECEIVER
ANTENNA
PRIM
FGES
1
CPIOM
FWS
RADIO HEIGHT DATA
2
RA TRANSCEIVER
3
1
WARNING INFORMATION
AND AUTO CALL-OUT
AUDIO MANAGEMENT
AMU
1
STATUS INFORMATION, WARNING MESSAGES
RADIO HEIGHT (AUTO CALL-OUT FUNCTION)
2
3
GROUND/FLIGHT
RA TRANSMITTER
RANSMITT
ANTENNA
Page 198
LGERS
2
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
GENERAL
Training by Airbus
AESS
4 TCAS/ATC MODE S
ANTENNAS
MAIN USERS
AESU
NOTE
CDS
ESC
DIR
CLR
INFO
Q
/
ATC XPDR
SURVEILLANCE
PERF
F-PLN
W
.
A
E.
S.
Z
OIS
ND
R
D
X
C
MFD
MAIL
BOX
Y
G
V
NAV
AID
INIT
SEC
INDEX
DEST
T
F
U
H
B
N.
C/L
ATC
COM
SURV
I
J
O
K
M
OIS
MENU
P
L
SPACE
NOTE
PAD
ENT
1
2
4
5
7
8
9
0
+/-
.
3
6
MENU
ESC
TCAS
AIRBORNE COLLISION
WXR/PWS
WXR/PWS/TURBULENCE
FWS
SURVEILLANCE
AFS
TAWS
1
WEATHER
RADAR ANTENNA
WXR
TCAS
ELEVN
DN
ABV
TA
ONLY
UP
U
WXR
TA
AESU
1
ELEVN
DN
UP
U
2
AESU
2
VHF
BLW
GAIN
C
A
P
T
VD AZIM
L
GAIN
G/S MODE
OF
FF
FF
OFF
+
SYS 1
R
SYS 1
WXR
TAWS
XPDR
TCAS
+
F
/
O
VD AZIM
SYS 2
L
R
SYS 2
AESS CONTROL PANEL
MSG
CLR
RESET PANELS
HF
TEL
SQWK
MENU
NAV
STBY
121.700
VHF1
121.900
123.125
VHF2
123.450
DATA
VHF3
TAXI
DATA
RST
VHF 1 RECEPTION NOT SELECTED
CALL
CALL
CALL
VHF1
HF1
TEL1
CALL
CALL
CALL
VHF2
HF2
TEL2
1
2
4
5
7
8
9
.
0
CLR
MECH
CALL
AESS
RECONFIGURATION CONTROL
HUD
RAIMS
CSTR
3
6
VOICE
INT
1
RAD
NAV
RMP
1
VORD
NDB
WX
TERR
TRAF
ARPT
QNH
1016
hPa
in Hg
ATT
VHF3
WPT
2
MKR
40
20
NAV
80
160
10
320
ZOOM
640
VOR
LS
ARC
PLAN
VV
LS
Page 199
EFIS CONTROL PANEL
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
XPDR - TCAS AND XPDR FUNCTIONS & AESUS XPDR - TCAS FUNCTIONS INTERFACES
CDS
HUDs
FCU
MAG
HDG
HDG
HDG
V/SV/S
METER
ALT
TRK
TRK
FPAFPA
---
V/S
7000
1000
1000
100
100
FD
AP1
-----
PFDs
NDs
SELECTED
ALT + HEADING
KCCUs
ESC
DIR
CLR
INFO
Q
E
.
R
S
.
/
OIS
UP
D
Z
X
C
MFD
MAIL
BOX
A/THR
ALT
Y
G
V
U
H
B
NAV
AID
INIT
SEC
INDEX
DEST
T
F
ND
OIS
MENU
AP2
N
.
NOTE
P
L
SPACE
NOTE
PAD
ENT
1
2
4
5
7
8
9
0
+/-
3
6
APPR
FLIGHT NUMBER
TRACK
MENU
ESC
RA
PRIM
C/L
O
K
M
MFDs
Training by Airbus
ATC
COM
SURV
I
J
.
DN
LOC
PERF
F-PLN
W
.
A
RADIO HEIGHT
CRDC
LGERS
TAXI
QNH
CSTR
TAXI
1016
in Hg
1016
hPa
WPT
VORD
WX
TERR TRAF
WPT VORD
WX
NDB
hPa VOR
ARC
LS
NAV
PLAN
VV
LS
LS
VV
ARPT
TERR
NAV
LS
TRAF
40
PLAN
320
80
160
10
ZOOM
XPDR REPLY
320
TCAS/MODE S
ANTENNAS
XPDR REPLY
ADR, IR, GPIRS, GPS,
A/C POSITION, ETC.
ALERT
PRIORITY
80
160
20
10
ARC
ZOOM
TCAS
INTERROGATIONS
ATC
INTERROGATIONS
AP/FD
AFDX NETWORK
EFIS CONTROL PANEL
ADIRU
CPIOM
FWS
AUDIO MANAGEMENT
AMU
AESU
TCAS
WXR/
PWS
XPDR
TAWS
RMPs
XPDR CODE
(SQUAWK)
VHF
HF
TEL
MENU
SQWK
NAV
SQWK
0163
1
* IDENT
2
MSG
CLR
R
PULSE
SUPPRESSOR
SPD
---
TRUE
TRUE MAG MAG
FLIGHT/GROUND
MACH SPD SPD
FMS
AESS CONTROL PANEL
WXR
TCAS
ELEVN
DN
ABV
WXR
TA
TA
ONLY
UP
U
GAIN
C
A
P
T
DME
RST
SQUAWK: 3615
ELEVN
DN
UP
U
GAIN
G/S MODE
OF
OFF
FF
F
VD AZIM
+
SYS 1
WXR
SYS 2
SYS 1
XPDR
TCAS
SYS 2
L
F
/
O
Page 200
VD AZIM
L
R
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
WXR / PWS - WXR / PWS INTERFACES
HUDs
PFDs
CDS
NDs
KCCUs
ESC
DIR
CLR
INFO
Q
W
.
A
/
OIS
OIS
MENU
E.
S.
NAV
AID
PERF
INIT
F-PLN
DEST
SEC
INDEX
T
Y
U
R
D
F
Z
X
C
ND
MFD
MAIL
BOX
G
V
H
B
J
N.
O
PCS
SPACE
ENT
2
3
4
5
6
7
8
9
NOTE
0
ENGINE
DATA
ESC
CRDC
CSTR
TAXI
1016
in Hg
1016
hPa
WPT
VORD
WX
TERR TRAF
WPT VORD
NDB
WX
NDB
LANDING GEAR
STATUS
LS
ARC
LS
NAV
PLAN
VV
LS
LS
VV
ARPT
TERR
NAV
hPa VOR
80
160
PLAN
40
20
320
80
640
LGERS
160
10
320
ZOOM
640
AFS
DATA
ALERT
PRIORITY
ARPT
TRAF
40
20
10
ARC
ZOOM
FMS
DATA
AFDX NETWORK
TAXI
QNH
ADR, IR,
GPIRS, GPS
A/C POSITION, ETC.
+/-
MENU
RA
ADIRU
PAD
1
.
RADIO
HEIGHT
FMS
P
L
K
M
MFDs
C/L
ATC
COM
SURV
I
Training by Airbus
PRIM
CPIOM
FWS
FLIGHT/
GROUND
EFIS CONTROL PANEL
AUDIO MANAGEMENT
AMU
WEATHER RADAR ANTENNA
ANTENNA
PLATE
WAVE GUIDES
RTU
WEATHER RADAR
CONTROL AND
MONITORING
RF
SWITCH
SWITCH
CONTROL
WADU
AESU
TCAS
XPDR
1
POWER SUPPLY
2
(200 VDC)
AESS CONTROL PANEL
WXR/
PWS
WXR
TCAS
ELEVN
DN
ABV
WXR
TA
TA
ONLY
UP
U
ELEVN
DN
UP
U
BLW
TAWS
GAIN
C
A
P
T
L
2
OFF
OF
OFF
F
+
VD AZIM
1
GAIN
G/S MODE
+
SYS 1
WXR
TAWS
SYS 2
SYS 1
XPDR
TCAS
SYS 2
R
F
/
O
VD AZIM
L
Page 201
R
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
AESS RECONFIGURATION
AESU 2
AESU 1
WXR/
PWS
TAWS
TCAS
XPDR
A
F
D
X
I
/
O
M
O
D
U
L
E
I
/
O
M
O
D
U
L
E
N
E
T
W
O
R
K
AESU 1
WXR/
PWS
WXR/
PWS
TAWS
TAWS
TCAS
TCAS
XPDR
XPDR
AESU 2
WXR/
I
PWS
/
O TAWS
M
O
D
TCAS
U
L
E
XPDR
A
F
D
X
I
/
O
M
O
D
U
L
E
N
E
T
W
O
R
K
Training by Airbus
AESU 1
WXR/
PWS
TAWS
TCAS
XPDR
AESU 2
I
/
O
M
O
D
U
L
E
A
F
D
X
N
E
T
W
O
R
K
I
/
O
M
O
D
U
L
E
SYS 1
WXR
TAWS
SYS 2
SYS 1
WXR
TAWS
SYS 2
SYS 1
WXR
TAWS
SYS 2
SYS 1
XPDR
TCAS
SYS 2
SYS 1
XPDR
TCAS
SYS 2
SYS 1
XPDR
TCAS
SYS 2
NORMAL MODE
AESU 1 OR AESU 2: MASTER
(2 FUNCTION GROUPS ARE
ACTIVATED IN ONE AESU)
MFDs - SURV PAGE SURV
CONTROLS
STATUS &SWITCHING
TRAFFIC
MIXED MODE
AESU 1 (2): MASTER
THE FUNCTION ARE SHARED
BETWEEN THE 2 AESUs (WITH OR
WITHOUT FAILUREs)
WXR/
PWS
NOTE
TAWS
TCAS
XPDR
DOWNGRADED MODE
ONE OR SEVERAL FUNCTIONS
ARE COMPLETELY LOST
AESU WITH TAWS/WXR FUNCTION
GROUP ACTIVATED IS MASTER
STATUS & SWITCHING
SYS 2
SYS 1
WX DISPLAY 2
YURB 2
PRED W/S 2
TERR SYS 2
GPWS 2
WXR
WX DISPLAY 2
YURB 2
PRED W/S 2
TAWS
TERR SYS 2
GPWS 2
TAWS IN USE
SYS 1
SYS 2
XPDR 1
XPDR
XPDR 2
TCAS 1
TCAS
TCAS 2
AESU 1
AESU HIGHLIGHTED IN YELLOW
IS THE MASTER
Page 202
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
AESS CONTROLS
TAXI
TAXI
QNH
1013
CSTR
WPT
VORD
NDB
VOR
WX
TERR
TRAF
1013
ARPT
CSTR
WPT
VORD
NDB
VOR
WX
TERR
TRAF
Training by Airbus
ARPT
NAV
40
ARC
VOR
10
VV
40
80
20
PLAN
LS
LS
TAXI
QNH
1013
ZOOM
CAPT EFIS CONTROL PANELS
160
320
640
20
NOTE
1013
in Hg
hPa
in Hg
TAXI
hPa
NAV
80
160
10
320
ZOOM
640
VOR
LS
ARC
PLAN
VV
DIR
PERF
INIT
NAV
AID
F-PLN
DEST
SEC
INDEX
SURV
Y
U
Q
LS
W
.
E.
A
F/O EFIS CONTROL PANELS
/
S.
R
D
Z
OIS
X
F
C
MFD
ND
T
G
V
H
B
I
J
N
.
HF
TEL
ATC
COM
O
K
M
MAIL
BOX
RMP
VHF
C/L
MENU
ESC
CLR
INFO
P
ENT
1
2
3
4
5
6
7
8
9
0
+/-
.
SQWK
MENU
NOTE
PAD
L
SPACE
NAV
SPACE
MSG
CLR
STBY
120.425
VHF1
118.300
115.300
VHF2
122.465
DATA
VHF3
125.500
KBD
CAPT KCCU
RST
SQUAWK: 3615
CALL
CALL
CALL
VHF1
HF1
TEL1
CALL
CALL
CALL
VHF2
HF2
TEL2
CALL
VHF3
INT
D
RAD
ESC
1
2
3
4
5
6
7
8
9
.
0
CLR
MECH
ATT
INT
CAB
BRT
.
.OF
OFF
WXR
ABV
ELEVN
DN
UP
U
BLW
GAIN
C
A
P
T
VD AZIM
L
GAIN
G/S MODE
OFF
OF
FF
FF
+
PA
1 VOR
R
2
MKR
WXR
TA
TA
ONLY
UP
U
LOAD
VOICE
ADF
1
TCAS
ELEVN
DN
SYS 1
WXR
SYS 1
XPDR
TCAS
R
+
F
/
O
VD AZIM
SYS 2
L
R
SYS 2
Page 203
AESS CONTROL PANELS
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
AESS INDICATING
Training by Airbus
MFD CONTROL PAGE
NOTE
Page 204
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
ADIRS SYSTEM (COMPONENTS LOCATION)
Training by Airbus
NOTE
A
Z120
3FP3
PROBEMULTIFUNCTION, 3
3FP1
PROBEMULTIFUNCTION, 1
3FP2
PROBEMULTIFUNCTION, 2
10FP1
PROBE-AOA
Page 205
A
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
ADIRS SYSTEM (COMPONENTS LOCATION)
Training by Airbus
NOTE
A
61FP2
SENSOR-OAT, 2
61FP1
SENSOR-OAT, 1
A
Page 206
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
SNS SYSTEM (COMPONENTS LOCATION)
Training by Airbus
NOTE
Z210
Z120
A
PROBE-STANDBY STATIC,L
15FC1
PROBE-STANDBY STATIC,R
15FC2
PROBE-STANDBY PITOT
13FC
A
Page 207
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
SNS SYSTEM (COMPONENTS LOCATION)
Training by Airbus
NOTE
Z110
FR0
A
A
Page 208
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
34
ATA 22
AUTO FLIGHT
FLIGHT GUIDANCE AND ENVELOPE SYSTEM
THROTTLE CONTROL
LEVERS
Training by Airbus
EFIS/FCU - AFS CONTROL PANEL
MACH
MACH
ARPT
SPD
SPD
SPD
TRUE
TRUE
MAG
---
MAG
MAG
HDG
HDG
V/S
TRK
FPA
CPIOM
METER
V/S
CSTR
-----
VOR
ALT
---
7000
FD
1000
100
AP1
160
LS
LS
VV
PLAN
10
320
ZOOM
640
AP2
DN
A/THR
LOC
ALT
10
APPR
ZOOM
NOTE
EFIS/FCU
BACKUP
UP
80
PLAN
VV
LS
FCDC
WBBC
PRIM 1
SIDE STICK
UNIT
SIDE A
RUDDER
PEDALS
ESC
DIR
CLR
INFO
E.
S.
Z
OIS
PERF
F-PLN
W
.
A
R
D
X
ND
MFD
Y
G
V
U
H
B
MAIL
BOX
ATC
COM
SURV
I
J
N
.
O
K
M
FMA
A/THR
C/L
MENU
NAV
AID
INIT
SEC
INDEX
DEST
T
F
C
FWS
AP/FD
CDS
/
CPIOM
FE
ADIRS/NAV
SENSORS
Q
SIDE B
P
NOTE
PAD
L
SPACE
2
4
5
7
8
9
0
+/-
.
FMS
ENT
1
3
6
SPACE
KBD
KCCU
ESC
MFD
CONTROL
SURFACES
(ACTUATORS)
WSCS
BTV
PCS
PFD
Page 209
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
22
AUTO FLIGHT CONTROLS
CSTR
WPT
VORD
NDB
VOR
WX
TERR
TRAF
ARPT
SPD
TAXI
QNH
1013
SPD
1013
---
in Hg
40
TRUE
MAG
MAG
HDG
HDG
V/S
TRK
FPA
METER
ALT
---
V/S
-----
7000
FD
hPa
1000
100
TAXI
TAXI
QNH
1013
CSTR
WPT
VORD
NDB
VOR
WX
TERR
TRAF
1013
UP
in Hg
160
10
320
ZOOM
640
NAV
ARC
VOR
AP1
DN
VV
LS
LOC
RESET SWITCH LEFT PANEL
A
PACK
1
RESET
RES
B
C
VCS
1
SCS
D
FMC-A
A/THR
ALT
E
R
1
EMER
TR1
SDS
1
SLATS
1
FLAPS
1
FQMS
1
LGCIS
1
BSCS
1
AESU
1
CIDS
1
2
BOTH
ON 2
3
FMS
SOURCE SELECTOR
INSTINCTIVE
DISCONNECT P/BSW5
VCS
2
TR
2
EMER
TR2
RESET
RES
T
U
FMC-B
SDS
2
SLATS
2
FLAPS
2
FWS
2
LGCIS
2
BSCS
2
AESU
2
5
WHC 1
FCU
6
6
6
FAULT
F
FAU
L
LT
OFF
PRIM 2
SEC 2
FAULT
FAULT
F
FAU
L
LT
OFF
DSCS
OFF
CINS
F/CTL
211VM
PRIM 3
SEC 3
FAULT
FAULT
FAULT
F
FAU
L
LT
OFF
OFF
OFF
F/CTL
CIDS
2
212VM
EIM
2
4
CCD 2
PRINTER
SEC 1
3
4
5
PRIM 1
2
OIS OIS CAB
AVNCS & MAINT
4
PRIM P/BSWS
FQMS
2
3
CKPT EQPT POWER SUPPLY
KBD 1
320
640
W
NAV
AID
CCD 1
160
ZOOM
232VM
V
1
AICS
2
EIM
1
4
S
PACK
2
2
3
ATC
VV
1
2
FMS
80
20
10
RESET SWITCH RIGHT PANEL
F
FMC-C
LS
40
ARC
PLAN
LS
APPR
231VM
1
TR
1
VOR
AP2
PLAN
LS
NOTE
ARPT
hPa
NAV
80
20
MACH
TAXI
Training by Airbus
CAPT EFIS CONTROL PANEL
AFS - CP
F/O EFIS CONTROL PANEL
C/L
MENU
INSTINCTIVE
DISCONNECT
P/BSW
CKPT EQPT POWER SUPP
KBD 2
WHC 2
HUMID
S
T
U
EFB 3
SPACE
A
SIDE STICK UNIT
B
C
D
E
R
F
RUDDER PEDALS
ARM
EMER
DESCENT
KCCU
THRUST
CONTROL LEVERS
Page 210
© Airbus SAS 2014. All rights reserved. Confidential and proprietary document.
22
FLIGHT GUIDANCE
SIDE STICK
UNITs(X2)
RUDDER PEDAL
LINKAGE
MACH
MACH
SPD
SPD
SPD
TRUE
MAGMAG
MAG
---
HDG
HDG
V/S
TRK
ALT
FPA
---
V/S
7000
FD
AP1
1000
100
CONTROL
SURFACES
----UP
(ACTUATORS)
AP2
DN
LOC
28VDC
A/THR
ALT
Training by Airbus
FMA
METER
NOTE
AMS
APPR
FCU
PRIM 1
SSPCs
SIDE A
SEC
SIDE B
PFD
FE
MMR
AP DISENGAGEMENT
ADIRU
CPIOM
AP/FD
FLIGHT
CONTROL
ISIS
ADIRS/NAV
SENSORS
CPIOM
FCU
BACKUP
AP DISENGAGEMENT
EMER
DESCENT
DC POWER
SEGREGATION
FMC
FWS
FCDC
FROM SIDE STICK
UNIT/AP
DISCONNECT P/BSW
WBBC
ARM
SPEED BRAKE
CONTROL PANEL
SFCC
AESS
(TCAS)
ELEC.
SYSTEM
HYD.
SYSTEM
CPCS
PCS
WSCS
LGERS
Page 211
AFDX NETWORK
© Airbus SAS 2014. All rights reserved. Confidential and proprietary document.
22
AUTOTHRUST
MACH
MACH
SPD
SPD
SPD
---
TRUE
MAG
MAGMAG
HDG
HDG
V/S
TRK
FPA
METER
ALT
---
V/S
7000
FD
1000
100
AP1
Training by Airbus
THROTTLE CONTROL LEVERS
NOTE
----UP
AP2
DN
A/THR
LOC
ALT
APPR
FCU
PRIM 1
ADIRU
SIDE A
A/THR
ADIRS/NAV
SENSORS
AESS
(TCAS)
SIDE B
CPIOM
FE
CPIOM
LGERS
FWS
CPIOM
FCU
BACKUP
FMC
PCS
FCDC
Page 212
AFDX NETWORK
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
22
FLIGHT MANAGEMENT SYSTEM
Training by Airbus
NOTE
PFD
FMC
ND
PRIM
COMPUTATION
LATERAL
FG
LATERAL FUNCTIONS
FLIGHT PLAN
LATERAL STEERING
ORDERS
VERTICAL FUNCTIONS
PERFORMANCE FUNCTIONS
MFD
ESC
DIR
PERF
INIT
NAV
AID
C/L
MENU
CLR
INFO
F-PLN
DEST
SEC
INDEX
SURV
ATC
COM
Q
W
.
A
/
E
.
S
.
Z
OIS
R
D
X
ND
T
F
C
MFD
Y
G
V
U
H
B
I
J
N
.
MAIL
BOX
O
K
M
VERTICAL
P
NOTE
PAD
L
SPACE
ENT
1
2
4
5
7
8
9
0
+/-
.
3
+
VERTICAL STEERING
ORDERS/THRUST
COMMAND
6
SPACE
KBD
AFDX NETWORK
ESC
KCCU
DME
CRDC
MMR
RMP
ADIRU
CPIOM
CPIOM
ATC DATA
LINK
ACR
SCI
VOR
FQMS
ADF
ABORT
READY
FORM
TEST
POWER
RESET
PAPER
FEED
FAULT
ON
0123456789
OPERATIONAL
GROUND CENTERS
HFDR, VDR,
SATCOM
Page 213
PRINTER
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
22
NOTE
Training by Airbus
Page 214
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
22
ATA 23
COMMUNICATIONS
GENERAL DESCRIPTION OF HF AND VHF SYSTEMS
VHF SYSTEM
Training by Airbus
HF SYSTEM
VHF
ANTENNA 3
VHF
ANTENNA 1
NOTE
HF
ANTENNA
VOICE
VHF
ANTENNA 2
MVDR 1
VHF 1
COM A
VHF 3
COM B
HFDR
COUPLER
MVDR 2
VHF 2
COM A
2
HFDR
COUPLER
VOICE & DATA
1
STBY
COM B
HFDR
XCVR
DATA
COMMUNICATIONS
2
HFDR
XCVR
1
AIRPORT FACILITIES
&
AIRLINE OPERATIONS
VOICE COMMUNICATIONS
ACRS
RAIMS
Page 215
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
23
HF SYSTEM
Training by Airbus
DATA LINK
NOTE
AMU
AUDIO
SELCAL
PTT
ADIRU
1
TEL
VHF
HF
ACR
MSG
CLR
SQWK
MENU
TEL
VHF1
NAV
121.900
MENU
123.125
VHF2
DATA
VHF3
123.450
STBY
DATA
RST
SQUAWK: 2523
DATA
CALL
CALL
CALL
VHF1
HF1
TEL1
CALL
CALL
CALL
VHF2
HF2
TEL2
VHF3
1
2
4
5
7
8
9
.
0
CLR
MECH
CALL
INT
VHF2
INT
3
.
6
CAB
VOICE
PA
1
1
1
1
GND HF
DATALINK
LGERS
FQMS
OVRD
HF
ANTENNA
VOICE
1
VHF3
HFDR
COUPLER
VOICE
PA
2
MKR
VHF3
CALL
RST
.
ATT
NAV
RST
BRT
VHF3
CALL
NAV
HF
HFDR
TRANSCEIVER
X-TALK BUS
HF
121.700
1
PTT
SELCAL
AUDIO
CONTROL/
STATUS
VHF
CPIOM
HF 2 I/O
2
INTERLOCK
FUNCTION
HF 1 I/O
RAIMS
1
2
MKR
ADF
1
1
2
MKR
RMPs
HFDR
TRANSCEIVER
HFDR
COUPLER
2
2
DATA LINK
ADIRU
Page 216
2
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
23
HF SYSTEM (COMPONENTS LOCATION)
Training by Airbus
Z320
Z270
NOTE
ANTENNA-HFDR
FEEDER-HFDR, 1
4RE1
3RE2
COUPLER-HFDR, 2
3RE1
COUPLER-HFDR, 1
Page 217
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
23
VHF SYSTEM
RAIMS
VHF 1 I/O
AUDIO
SELCAL
PTT
VHF 3 I/O
AUDIO
SELCAL
PTT
AMU
VHF 1
2
RMPs
HF
TEL
VHF
121.700
HF
SQWK
VHF 2 I/O
AUDIO
SELCAL
PTT
VHF 2 OR 3 STBY
AUDIO
SELCAL
PTT
MENU
TEL
NAV
DATA
MENU
VHF3
DATA
HF1
CALL
TEL1
CALL
CALL
VHF2
HF2
TEL2
VHF2
INT
VHF3
1
2
3
4
5
6
7
8
9
X-TALK
NAV
121.900
.
0
CLR
.
CALL
VHF3
MVDR XCVR 2
AUDIO
STBYRST
DATA
9
MECH
ATT
INT
CAB
RST
BRT
.
.OF
OFF
1
SELCAL
PTT
.
COM A
.OFF
F
VOICE
1
VHF 2
BRT
PA
TEL2
INTADF CAB
RAD
1
NAV
CALL
VHF3
VHF
ANTENNA 3
COM B
RST
CALL
CALL
2
DATA123.450
VHF3
CALLMSGCALL
CLR
VHF 3
STBY
SQUAWK: 2523
VHF1
1
121.900
HF
VHF2 VHF1
123.125
123.450
121.700
MSG
CLR
VHF
ANTENNA 1
COM A
SQWK
VHF1
VHF
NOTE
MVDR XCVR 1
1
VHF
Training by Airbus
VOICE
2 PA
MKR
ADF
1
VHF
ANTENNA 2
VOICE
1
2
MKR
ADF
RAD
1
NAV
1
2
MKR
2
AUDIO
SELCAL
PTT
VHF 2 OR 3
STBY
COM B
CPIOM
Page 218
ACR
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
23
VHF SYSTEM RECONFIGURATION
VHF
ANTENNA 3
VHF
ANTENNA 1
VHF SYSTEM IN NORMAL
CONFIGURATION
Training by Airbus
VHF
ANTENNA 2
NOTE
COMBINER/
SPLITTER
COMBINER/
SPLITTER
X-TALK
COM A
COM B
COM A
COM B
VHF 1
VHF 3
VHF 2
STANDBY
VHF
ANTENNA 1
VHF
ANTENNA 3
VHF SYSTEM RECONFIGURATION
AFTER THE FAILURE OF
THE MVDR 1 COM A XCVDR
VHF
ANTENNA 2
COMBINER/
SPLITTER
COMBINER/
SPLITTER
X-TALK
COM A
COM B
VHF 1
VHF 1
COM A
COM B
VHF 2
VHF 3
Page 219
MVDR 1
MVDR 2
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
23
VHF SYSTEM (COMPONENTS LOCATION)
Training by Airbus
NOTE
MVDR ANTENNA3
MVDR ANTENNA1
2 MVDR
TRANSCEIVERs
AVIONICS
COMPARTMENT
Page 220
MVDR ANTENNA2
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
23
SATELLITE COMMUNICATIONS - SATCOM SYSTEM
SATCOM 2 I/O
AMU
A/C
POSITION
SATCOM 1 I/O
AUDIO
AUDIO
ADIRU
1
2
2
HF
VHF
TEL
HF
SQWK
TEL
MENU
SQWK
SATCOM CONFIG
COCKPIT VOICE
COMMUNICATION
NAV
MENU
STATUS
LOGGED ON AUTO TEL
LOG OFF *
CABIN CALLS
DISABLED
ENABLE *
ICAO
24312601
NOTE
HGA
1
VHF
Training by Airbus
AFDX NETWORK
RAIMS
BEAM
STEERING
NAV
MULTICONTROL
SATCOM SETTINGS >
BITE
RST
MSG
RST
SIGNAL
POWER
RST
LOAD
MECH
VOICE
LOAD
SDU
NAV
1
2
MKR
1
2
MKR
Tx
RMPs
ACR
A/C DATA LINK
FUNCTION
Rx
HIGH
POWER
AMPLIFIER
Tx
DIPLEXER/
LOW NOISE
Rx AMPLIFIER
HIGH SPEED
DATA LINK
ATC
FMS
AOC
OMS
CABIN SERVICE
SCM
Page 221
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23
DESCRIPTION & INTERFACES
Training by Airbus
CPIOM
VHF
VHF
HF
HF
TEL
TEL
SQWK
MENU
SQWK
MENU
ASFC
NAV
ADIRS
FMS
ATC DATA LINK
NAV
AOC
DATALINK ROUTER
115.300 VHF2 INIT>
115.300 VHF2 122.425
VHF3
DATA
COM
STATUS>
VHF3
DATA
125.500
HF1 SELCAL
<RETURN
HF1 SELCAL
VHF PROVIDER>
CALL
CALL
1
HF1
TEL1 1
4 2
2
RST
.
.
CPDLC
AOC DATA LINK
MESSAGES
A/C
PARAMETERS
LOAD
LOAD
LOAD
VOICE
NOTE
A/C
POSITION
SCI
AFDX NETWORK
VOICE
MECH
OMS
- CMS
- DLCS
- ACMS
COM
MANAGER
CPIOM
RMP
STATUS/CONTROL
ACR
ACRS
OSFC
COM
MANAGER
HF
SYSTEM
VHF SYSTEM
(VHF3 ONLY)
ACARS COMMUNICATION MEANS
SATCOM
SYSTEM
WACS
SATCOM SYSTEM
(HIGH SPEED SERVICES)
Page 222
INTERNET PROTOCOL COMMUNICATION MEANS
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
23
NOTE
Training by Airbus
Page 223
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
23
WACS DESCRIPTION
Training by Airbus
WACS
NOTE
WACS ANTENNA
TRIPLEXER
TGCU
(CELLULAR)
TWLU
(WI-FI)
STATUS
RADIO ON/OFF
WIRED
GATELINK
PLUG
OSFC
AOC/OMS
GATELINK
RADIO POWER ENABLE
OFF
TRANSCEIVERS
SETTING
COM
MANAGER
WLM
A/C ON GROUND
LGERS
Page 224
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
23
WACS SYSTEM (COMPONENTS LOCATION)
Training by Airbus
NOTE
Z230
TRIPLEXER-WACS
7TT
TGCU
6TT
TWLU
1TT
FR29
FR28
FR27
Page 225
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
23
ACOUSTIC ARCHITECTURE
PTT
RMP INTERCONNECTIONS
VHF
RMP1
STATUS
MSG
CLR
HF
TEL
SQWK
MENU
NAV
120.425
VHF1
118.300
115.300
VHF2
12_.___
DATA
VHF3
VHF
STBY
125.500
CALL
CALL
HF1
TEL1
CALL
CALL
CALL
HF2
TEL2
VHF2
1
2
3
4
5
6
7
8
9
.
0
CLR
.
ATT
LOAD
MENU
NAV
118.300
VHF2
12_.___
DATA
VHF3
VHF
STBY
125.500
MSG
CLR
RST
HF1 SELCAL
CALL
CALL
CALL
VHF1
HF1
TEL1
CALL
CALL
CALL
HF2
TEL2
1
2
3
4
5
6
7
8
9
.
0
CLR
LOAD
ATT
TEL
1
MENU
118.300
VHF2
12_.___
DATA
VHF3
STBY
125.500
RST
HF1 SELCAL
CALL
CALL
CALL
VHF1
HF1
TEL1
CALL
CALL
CALL
HF2
TEL2
1
2
3
4
5
6
7
8
9
.
0
CLR
MECH
RMP2
STATUS
LOAD
ATT
VOICE
INT
1
2
MKR
RMP3
NOTE
NAV
VHF1
CALL
1
SQWK
115.300
VOICE
INT
2
MKR
HF
120.425
VHF2
MECH
CALL
1
SQWK
VHF1
VOICE
INT
RMP1
TEL
115.300
VHF2
MECH
CALL
MSG
CLR
RST
HF1 SELCAL
CALL
VHF1
HF
120.425
Training by Airbus
PTT
1
2
MKR
RMP2
RMP3 STATUS
611 VU
HAND MIC
611 VU
HAND MIC
HEADSET
HEADSET
STATUS
BOOMSET
BOOMSET
FLIGHT INTERPHONE
611 VU
HEADSET
611 VU
PTT
PTT
HEADSET
BOOMSET
AMU
PTT
PTT
LOUDSPEAKER
OFF
M
MAX
A
AMU
BOOMSET
4TH OCCUPANT
SIDE
HAND MIC
PTT
LOUDSPEAKERS
AUDIO LEVEL
LOUDSPEAKER
AVNCS VENT
LIGHT
HT TEST HORN RESET
SVCE INT
SVC
IN
CAPT SIDE
LOUDSPEAKERS
AUDIO LEVEL
3RD OCCUPANT
SIDE
ELT
E
1
PTT
GSP
OFF
PTT
M
MAX
A
APU
FIRE
2
APU
SHUT
OFF
COCKPIT
CALL
Page 226
FLT INT
NT
F/O SIDE
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
23
AUDIO MANAGEMENT
HF SYSTEM
HF
1
HF
VHF SYSTEM
2
VHF
1
VHF
2
SATCOM SYSTEM
VHF
3
TELECOM
1
TO/FROM
AMU1 & 2
CIDS
PA
TELECOM
2
Training by Airbus
RADIO NAV SYSTEM
INTPH
MMR
DME
ADF
VOR/MKR
NOTE
SAME AS HF1 SYSTEM
RMP
AUDIO ALERTS
AESS
NAV
MSG
CLR
R
CVRS
CALL
CALL
CALL
CALL
CALL
VHF2
HF2
CALL
TEL2
RST
CALL
ATT
VOICE
1
STBY
TBY
BY
Y
CHANNEL1
CHANNEL2
AUDIO I/O
PTT
SELCAL
LOAD
INT
1
HF1
FWS
2
MKR
NAV
1
2
MKR
TO/FROM HF1
CVR INTERCONNECTION
AMU
AURAL WARNINGS
.
MECH
AUDIO I/O
PTT
SELCAL
RADIO COM
TRANSMISSION KEY
HF1
CALL
AMU
HF1
CHANNEL3
RECEPTION KNOB
4TH OCCUPANT SIDE
AUDIO
PTT
CAPT SIDE
AUDIO
PTT
1
AUDIO
3RD OCCUPANT SIDE
PTT
2
Page 227
F/O SIDE
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
23
SELCAL / CALL FUNCTIONS
HF SYSTEM
HF
1
HF
VHF SYSTEM
2
VHF
VHF
1
VHF
2
SATCOM SYSTEM
TELECOM
3
TELECOM
1
Training by Airbus
CIDS
CABIN
INTPH
PA
2
NOTE
FLT REST
SELCAL
CALL
SAME AS HF1 SYSTEM
CRDCs
AFDX NETWORK
CALL
INDICATION
CALL
INDICATION
FWS
VHF
BUZZER
HF
TEL
SQWK
VHF
HF
TEL
NAV
SQWK
MENU
NAV
CALL
VHF
SQWK
MENU
NAV
VHF1TEL 118.300
120.425
5 HF
120.425 VHF1 STBY118.300
115 300 VHF2 12
115.300
12_.___
_.___
120.425 VHF1 STBY118.300
115.300 VHF2 12_.___
STBY
VHF3
DATA
125.500
VHF2 12_.___
115.300
HF1 SELCAL
VHF3
DATA
125.500RST
MSG
CLR
R
MSG
CLR
CALL
VHF1
DATA1
HF1 SELCAL
CALL
MSG
HF1
CLR
CALL
VHF1
HF1 SELCAL
TEL1
4
CALL
HF1
CALL VHF1
CALL
HF2
CALL
VHF2
CALL
VHF3
INT
TEL1
7
1
5
4
8
5
91
TEL1
7
0
CLR
C
LR
8
4
95
CALL
.
07
CLR
8
HF2
MECH
TEL2
INT CALL
CAB
CALL
MECH
HF2
ATT
TEL2
INT
STB
STBY
TB
BY
VHF3
INT
RAD
NAV
STBY
ST
TB
T
BY
RAD
OMS
. PA
ATT
MECH CALL
125.500
3
CALL
HF1.
INT
RAD
CALL
6
2
CALL
CALL
VHF2
CALL
D
RAD
VHF3
TEL2
CALL
HORN
RST
VHF3
3
2
CALL
CALL
CALL
CALL
VHF2
SELCAL
MODIFICATION
MENU
LOGIC
RELAYS
WIRING
LGERS
RMP
62
0
BRT
.
.OF
BRT
OFF
.
3 . OFF
LOAD
6
9
VOICE
CLR
RST
BRT
.
.OFF
LOAD
CALLS
LOAD
VOICE
PURS
CAB
PA
LS 1
R
ATTVOR
VOICE
2
CAB LS PA
MKR 1 VOR
ADF 2
2
1
MKR
LS 1
VOR
ADF 2
2
RAD
1
STB
STBY
TBY
TB
BY NAV
MKR
MECH
ADF
DF 2
1
INT
FLT REST
ALL
CAB REST
EMER
ELT
E
AVNCS VENT
APU
FIRE
CALL
RAD
NAV
ON
FWD
MID
EXIT
LIGHT
LIGH
H TEST HORN RESET
AFT
SVCE INT
SVC
APU
SHUT
OFF
COCKPIT
CALL
FLT INT
GSP
HF1
AUDIO
AUDIO I/O
PTT
SELCAL
TO/FROM
HF1
AMU
AUDIO I/O
PTT
SELCAL
RST
HF1
AMU
CALL
CALL
CALL
VHF1
HF1
TEL1
CALL
CALL
CALL
VHF2
HF2
TEL2
AUDIO
CALL
CAPT
SIDE
PTT
PTT
F/O
SIDE
VHF3
INT
MECH
ATT
INT
CAB
PA
D
RAD
Page 228
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
LSs AUDIO LEVEL
LSs AUDIO LEVEL
1
2
23
RADIO MANAGEMENT
VHF
VHF
HF
TEL
MENU
MSG
CLR
NAV
120.425
VHF1
118.300
115.300
VHF2
122.425
DATA
MSG
CLR
SQWK
VHF3
125.500
RST
TEL1
CALL
1
2
3
4
5
6
7
8
9
.
0
CLR
SQWK
MENU
Training by Airbus
NAV
VHF1
118.300
115.300
VHF2
122.425
DATA
VHF3
125.500
NOTE
STBY
RST
HF1 SELCAL
CALL
CALL
CALL
VHF1
HF1
TEL1
COM3 BUS1
1
2
3
4
5
6
7
8
9
.
0
CLR
VHF
.
BRT
.
BRT
HF
TEL
SQWK
MENU
LOAD
COM3 BUS2
MSG
CLR
VHF1
118.300
115.300
VHF2
122.425
DATA
VHF3
125.500
STBY
RST
HF1 SELCAL
1
2
3
4
5
6
7
8
9
.
0
CLR
VOR
R
.OF
OFF
MKR
RMP3
LOAD
COM2 BUS2
(BACKUP BUS)
(BACKUP BUS)
COM1 BUS1
HFDR
XCVR
VHF1
COM A
VHF3
COM B
MVDR1
1
.
BRT
.OF
OFF
LOAD
RMP INTERCOMMUNICATION BUS
COM1 BUS2
(PRIMARY BUS)
NAV
120.425
OFF
OF
VOICE
TEL2
RMP1
TEL
120.425
STBY
HF1 SELCAL
CALL
HF
HFDR
XCVR
RMP2
COM2 BUS1
2
(PRIMARY BUS)
VHF2
COM A
VHF STBY
Page 229
COM B
MVDR2
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
23
INTERPHONE COMMUNICATION - FLIGHT INTERPHONE SYSTEM & GROUND CREW CALLS
COCKPIT ENVIRONMENT
VHF
VHF
HF
HF
TEL
TEL
GROUND ENVIRONMENT
RST
SQWK
MENU
SQWK
MENU
NAV
INT
VHF1
121.900
HF 121.700
TEL
SQWK
MENU
NAV
STBY
121.700 VHF1 121.900
123.125 VHF2
STBY 123.450
121.700 VHF1
121.900
123.125 VHF2 123.450
VHF3
DATA
DATA
123.125 VHF2 123.450
MSG
CLR
VHF3
CALL
CALL
CALL
RST
VHF1
HF1
TEL1
CALL
CALL
CALL
VHF2
HF2
TEL2
INT
CALL
9
1
2
3
4
5
6
7
8
9
.
0
CLR
MECH
ATT
INT
CAB
VHF3
RAD
NAV
RST
RST
DATA
VHF 1 RECEPTION NOT SELECTED
1
CALL
CALL
NOTE
MECH
NAV
STBY
VHF
DATA
.
.
.
.
VOICE
VOICE
VOICE
PA
ADF
1
1
2
MKR
AMU
GROUND
HORN
RMP
NLG
GSP
HAND
MICROPHONE
FLIGHT
INTERPHONE
PTT
ELT
E
MECH CALL
CALLS
PURS
FLT REST
ALL
CAB REST
EMER
CALL
ON
FWD
MID
EXIT
Training by Airbus
SIDE
STICK UNIT
AVNCS VENT
LIGHT
LIGH
H TEST HORN RESET
SVCE INT
SVC
APU
FIRE
APU
SHUT
OFF
COCKPIT
CALL
FLT INT
AFT
Page 230
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
23
GENERAL - DISPLAY MANAGEMENT
Training by Airbus
ABN
RCL
ALL
ENG
DOOR
STS
WHEEL
FUEL
CLEAR
ALL
CDS
MORE
EL/AC
EL/DC
HYD
F/CTL
APU
BLEED
COND
PRESS
VIDEO
VIDEO
CLEAR
ECAM CTL PNL (FOR SD)
ACTIVATION TACS
DEFRD
RCL
LAST
SD
VIDEO
EMER
M
CANC
DISPCH
INSERT
ADJUSTMENT
VIDEO
T.O
CONFIG
TAXI
WPT
VORD
WX
TERR
NDB
NAV
VOR
LS
LS
ARPT
OMS
TRAF
hPa
VV
ARC
PLAN
40
20
80
160
10
320
ZOOM
640
CAPT F/O EFIS CTL (FOR PFDs)
CMVS
LANDSCAPE
CAMERA
IFE SYSTEM
CMV
OFF
CMV
1
2
NOTE
ADIRS
TACS
LIGHTS
FLIGHT/GROUND
CSTR
1016
in Hg
LGERS
GROUND SPEED INDICATION
INSERTED BY THE CDS
LANDSCAPE BELLY TAC
VERTICAL
CAMERA
STABILIZER TAC
EXTERNAL VIDEO SYSTEM
AIRCRAFT IN FLIGHT
OR
- INHIBITION OF THE TACS
DISPLAY ON THE PFDs
GS > 60Kts
FROM
FROM
VERTICAL BELLY
TAC
TAC
QNH
TAXI
GROUND SPEED
AFDX NETWORK
GS 0
Page 231
INSERTS GENERATED
BY THE CMVS
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
23
DESCRIPTION - RECORDING LOGIC - ERASE FUNCTION
FLIGHT INTERPHONE ACQUISITION
SSCVR
CIDS
DIGITAL MEMORY
UNIT
CABIN
INTPH
PA
AMU
1
RADIO
COMMUNICATION
SYSTEM
COCKPIT AREA
MICROPHONE
PARK BRK
ACCUS
REINFLATE
OFF
NOTE
DATA LINK
MESSAGE RECORDING
CHANNEL 4 (CAM AUDIO RECORDING)
TEST FUNCTION
AUDIO MONITORING
CVR
TEST
PULL & TURN
B
O
O
M
S
E
T
ERASE
CVR LOGIC
ERASURE FUNCTION
LOGIC RELAY
RECORDING FUNCTION
LOGIC RELAY
RCDR
ENGINES
GND CTL
A
U
T
O
AMPLIFIER
CHANNEL 1
(CAPT AUDIO RECORDING)
CHANNEL 2
(F/O AUDIO RECORDING)
CHANNEL 3
(3RD AUDIO RECORDING)
ON
LGERS
ON
CPIOM
ATC
CVR CU
UNDER WATER
LOCATING BEACON
Training by Airbus
SSCVR
RAIMS
ENG START
ON
NORM
CRANK
OFF
FIRE
ERASE FUNCTION
RECORDING ENABLED
135 VM
ON
IGN
START
OFF
Page 232
FIRE
1
2
FAULT
FAULT
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
23
EMERGENCY LOCATOR TRANSMITTER (ELT) FUNCTION
T
AUTOMATIC FIXED ELT
Training by Airbus
ELT ANTENNA
NOTE
ELT MANUAL CONTROL IF:
- THE G-SWITCH DOES NOT
START THE TRANSMISSION
OR
- TO STOP ELT TRANSMISSION FOR
MAINTENANCE OR IF THERE IS
UNWANTED TRANSMISSION
ELT
ON
ARMED
TEST/RESET
ELT REMOTE CONTROL PANEL
ELT
PORTABLE ELT
(DIFFERENT LOCATIONS AND
MODELS POSSIBLE)
ELT CONTROL PANEL
GROUND SERVICE PANEL
ELT INDICATOR LIGHT
HORN RESET CONTROL
SWITCH
ELT
E
AVNCS
C VENT
APU
FIRE
LIGHT
HT TEST HORN RESET
APU
SHUT
OFF
SVCE
SVC
SV
VC INT
VC
COCKPIT
CALL
Page 233
FLT INT
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
23
AUTOMATIC FIXED ELT SYSTEM DESCRIPTION
Training by Airbus
ELT REMOTE CONTROL PANEL
ELT
ELT
ON
NOTE
BATTERY
ARMED
WARNING
G-SWITCH
TEST/RESET
CAUTION
LGERS
GROUND/FLIGHT
RELAY
ELT
ELT ANTENNA
BATTERY
GROUND
HORN
T
A
APU
FIRE
TEST HORN RESET
APU
SHUT
OFF
COCKPIT
CALL
G-SWITCH
NAVIGATION
MODULE
FLT INT
GROUND SERVICE
PANEL
CRDC
ADIRUs
Page 234
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
23
RMP PRESENTATION - EXTERNAL VIDEO SYSTEM
Training by Airbus
265 VM
VHF
HF
TEL
SQWK
MENU
NAV
MECH CALL
STRIKE
231 VM
RESET
PACK &
VCS 1
SCS
FMC-A
FMC-C
TR
1
EMER
1
SDS
1
SLATS
1
FLAPS
1
FQMS
1
AICS
1
FWS
1
AESU
1
CIDS
1
FUEL
OXYGEN
VENT
RESET
AVNCS
GND COOLG
NOTE
2
REFUEL
END
EIM
1
ON
ENG
FADEC GND PWR
1
2
A
U
T
O
OFF
OFF
GND HF
DATALINK
CKPT DOOR
LOCKG SYS
OVRD
OFF
SVCE INT
OVRD
EMER 2
1
2
MAINT
GND
CONNECTION
ON
ON
AIR
REMOTE
C/B CTL
ON
ON
EMER
TR 2
FWS
2
SDS
2
SLATS
2
FLAPS
2
FQMS
2
AICS
2
LGCIS
2
BSCS
2
AESU
2
CIDS
2
OIS
OIS CAB
AVNCS & MAINT
DSCS
EIM
2
3
OVHT COND
FANS RESET
FAULT
ON
TR
2
2
26.8
EMER 1
TEST
MODE
5
232 VM
FMC-B
1
BAT
OFF
FAULT
ON
4
PACK &
VCS 2
HIGH
MED
LOW
ATC
3
RESET
CHARGE
POWER
ON
BSCS
1
1
CKPT DOOR CTLR
MID
BOT
255 VM
TOWING ON BAT
2
LGCIS
1
CHAN
TOP
1
4
ON
CKPT EQPT POWER SUPPLY
CCD 1
KBD 1
WHC 1
FCU
245 VM
6
A
MSG
CLR
RST
CALL
CALL
CALL
VHF1
HF1
TEL1
1
2
3
4
5
6
7
CALL
CALL
CALL
VHF2
HF2
TEL2
.
8
0
MECH
CALL
VHF3
INT
BRT
.
.OF
OFF
CAB
STB
STBY
TBY
RAD
NAV
C
COCKPIT
LOUDSPEAKERS
CKPT EQPT POWER SUPPLY
MECH CALL P/BSW
PAX INFO
OFF
OFF
ENG 1
F
I
R
E
IFEC
SMOKE
OFF
IR2
ON BAT
IR3
FAULT
OFF
ATT
OFF
ATT
ATT
OFF
FAULT
ADR3
OFF
SQUIB
DISCH
AGENT
GREEN
H
Y
D
SUPPLY
SUPPLY
OVHT
FAULT
ISOL
OFF
OVHT
FAULT
OFF
ISOL
OFF
ACTIVE
222 VM
FIRE
DISCH
CAB FANS
COOLG
FAULT
SMOKE
OFF
SUPPLY
OVHT
FAULT
OVHT
ISOL
OFF
ISOL
H
Y
D
PUMP
OFF
A
U
T
O
FAULT
OFF
MAIN
L TK
STBY
FAULT
FAULT
OFF
OFF
BAT 1
A MAN ON
AT
RAT
DFRD
RCDR
EVENT
GND CTL
ON
FAULT
PURS
A
I
R
1B
AVAIL
OFF
A
U
T
O
OFF
FAULT
APU GEN
DISC
OFF
FAULT
OFF
SEC 2
FAULT
FAULT
OFF
OFF
DRIVE
OFF
2A
GEN
EXT 2
FAULT
FAULT
AVAIL
DISC
OFF
CAB DATA
TO OIS
GATELINK
OFF
OFF
OFF
AUTO
OFF
FAULT
OFF
ON
WIPER
1
WINDSHIELD
DEFOG
BEACON
ON
ENG 2 BLEED
OFF
A
I
R
2
FAULT
ON
ON
NAV
1
AUTO
ON
F
OFF
OFF
F
LDG
ON
NOSE
O
T.O
OFF
FF
FF
F
OFF
OFF
FF
OFF
ON
TAXI
STBY
COMPASS
& EYE REF
MAN
UP
2
25
HEATER
FAULT
OFF
MAN
START
ENG
2
ALTN
MODE
ON
ON
ON
DN
WIPER
OFF
RAIN
RPLNT
INTMT
SLOW
INTMT
MEDIUM
EMER
EXIT LT
ON
SLOW
FAST
INTMT
FAST
ARM
AUTO
OFF
OFF
5
2
25
OFF
ACTIV
BRT
AUTO
FAULT
5
ON
SIGNS
BULK
ISOL VALVES
TEMP REGUL
15
DITCHING
INT LT
DIM
NO PED
ON
OFF
OFF
1
TRGT
A
U
T
O
ANN LT
TEST
F
FF
OFF
SEAT BELTS
ON
AVAIL
ON
A
U
T
O
ICE
IND
FAULT
START
FAULT
OFF
215 VM
CABIN V/S
MODE
MODE
MAN
MASTER SW
AUTO
OFF
F
WING
ON
CABIN ALT
TRGT
DEC
INC
APU
LOGO
ON
2
OFF
F
RWY TURN OFF
ON
A
U
T
O
AFT
ISOL VALVES
FAULT
TEMP REGUL
15
FWD CARGO
PRESEL
ON
OFF
PROBE &
WINDOW HEAT
RAM AIR
FAULT
FAULT
CABIN PRESS
ENG
FAULT
EXT LT
STROBE
ON
FAULT
FAULT
ON
ANTI ICE
FAULT
FWD
ISOL VALVES
PACK 2
HOT AIR 2
OPEN
FAULT
OFF
AUTO MODE
FAULT
CARGO AIR COND
ON
CABIN
COLD
HOT
H
HOT
H
XBLEED
PURS SEL
CLOSE
212 VM
OFF
OIS
E
L
E
C
FAULT
APU BLEED
OFF
TURB DAMPG
OFF
OFF
AC BUS 2A
DISC
COCKPIT
COLD
HOT AIR 1
ON
FAST
OFF
FAULT
HI
FAULT
FAULT
ON
OIS DATA
TO AVNCS
225 VM
COMMERCIAL
1
2
GALLEY
GEN
FAULT
OFF
ENG 1 BLEED
WING
2B
DRIVE
OFF
AIR FLOW
NORM
LO
MAN
YELLOW ELEC PMP
A
U
T
O
FAULT
PRIM 2
ISOL
OFF
AC BUS 2B
BUS TIE
GEN
FAULT
OFF
CALL
RAIN
RPLNT
ELEC PMP
ON
F/CTL
F
U
E
L
ON
EMER
AFT
PAX SYS
OFF
OFF
AC BUS 1B
DRIVE
ON
APT
CAPT
CAB REST
ELM
FAULT
FAULT
OFF
EXT 1
OFF
CKPT
HI VENT
ON
CALLS
BAT 2
FAULT
OFF
GEN
FAULT
ON
CAPT &
EVAC
SLOW
FAULT
ON
PACK 1
EVAC
HORN OFF
OFF
R TK
STBY
OFF
ON
FAULT
INTMT
FAST
MAIN
FAULT
FAULT
EMER BAT 1 EMER BAT 2
1A
FAULT
DISC
A
U
T
O
OFF
INTMT
SLOW
OFF
R TK XFR
AC BUS 1A
DRIVE
SYS ON
EXIT
MAN
FAULT
OFF
E
L
E
C
MASK
ASK MAN O
ON OXYGEN
CREW
SUPPLY
PAX
ALL
R
FAULT
A
U
T
O
FAULT
OFF
L TK XFR
FAULT
A
U
T
O
FAULT
ACMS
MID
GREEN
A
U
T
O
ON
CTR TK
FEED
L
FAULT
ON
TRIGGER
COMMAND
GND HYD
ON
F
U
E
L
OPEN
ON
INTMT
MEDIUM
MLG BAY
SMOKE
VENT
AVNCS
A
U
T
O
235 VM
YELLOW
ENG 2
PUMP
OPEN
OPEN
FAULT
OFF
FWD
DISCH
OVRD
CROSSFEED B
CROSSFEED A
SEC 3
FAULT
OFF
FLT REST
ERASE
AGENT TO AFT
BTL1
BTL2
SMOKE
AVNCS
EXTRACT
FAULT
SQUIB
DISCH
SUPPLY
PUMP
211 VM
PRIM 3
FAULT
OFF
PURS
AGENT 2
SQUIB
DISCH
GREEN
YELLOW
ENG 1
PUMP
OFF
SEC 1
FAULT
MECH CALL
AGENT 1
SQUIB
DISCH
FAULT
FAULT
F/CTL
PRIM 1
A
U
T
O
AGENT TO FWD
PUSH
PUSH
FIRE
TEST
AGENT 2
F
I
R
E
FIRE
FIRE
FIRE
FI
PUSH
SQUIB
DISCH
OFF
GROUND SERVICE PANEL
COCKPIT CALL
HORN RESET
COCKPIT CALL
CTRL SW
CTRL SW
INDICATOR LIGHT
Z
Y
B
O
O
M
S
E
T
CARGO SMOKE
ENG 2
APU
FIRE
AGENT 1
NAV
OFF
NAV
OFF
EMER
R ELEC PWR
RMP
X
OFF
FAULT
OFF
TRANSMISSION KEY
WITH MECH AMBER LEGEND
OFF
ADIRS
ARM
R
VOR
2
MKR
HUMID
W
CVR
OCCPD
OFF
FUEL JETTISON
LS 1
WHC 2
V
LAVATORY
PAX PERS
ELEC SPLY MOBILE COM
IR1
PA
ADF 2
1
KBD 2
U
CABIN
LANDSCAPE
CAMERA
EMER GEN
RAD
D
CCD 2
6
TEST
NAV
VOICE
5
F
221 VM
9
CLR
E
ON
ARMED
TEST/RESET
OFF
LOAD
D
ELT
FAULT
ATT
INT
B
ON
OFF
F
OFF
OVERHEAD PANEL
ELT
E
AVNCS VENT
LIGHT
HT TEST HORN RESET
SVCE
SVC
E INT
IN
FLT INT
APU
FIRE
APU
SHUT
OFF
COCKPIT
CALL
MECH CALL HORN
Page 235
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
23
RMP PRESENTATION - EXTERNAL VIDEO SYSTEM
LANDSCAPE CAMERA
P/BSW
Training by Airbus
BOOMSET RECEPTACLE
CABIN
LANDSCAPE
CAMERA
PAX INFO
P
OFF
OFF
IFEC
SMOKE
OFF
TAXI
T
AXI
QNH
QN
1013
013
1013
3
ERASE
ERASE
P/BSW
TYPICAL LAYOUT
OFF
OFF
TEST P/BSW
CAPT TAXI KEY
TAXI
B
O
O
M
S
E
T
TEST
OCCPD
PAX PERS
P
ELEC SPLY
L MOBILE COM
CSTR
WPT
VORD
NDB
VOR
WX
TERR
TRAF
ARPT
RCDR / GND
CTL P/BSW
ACMS
DFDR
RCDR
TRIGGER
EVENT
GND CTL
ON
ARC
PLAN
LS
VV
NOTE
CVR
LAVATORY
LAVAT
A ORY
40
20
80
160
T.O
CONFIG
320
ZOOM
640
ABN
RCL
LAST
RCL
ALL
DISPCH
CAPT F/O EFIS CONTROL PANEL
SD
CAPT PFD
ALL
TYPICAL LAYOUT
EMER
EM
MER
CANC
CANC
DEFRD
10
MORE
STS
ENG
DOOR
WHEEL
FUEL
EL/AC
EL/DC
HYD
F/CTL
APU
BLEED
COND
PRESS
VIDEO
IMAGE FROM
THE VERTICAL
STABILIZER
CAPT EFIS DISPLAY
VIDEO KEY
VIDEO
IMAGE FROM ECAM CONTROL PANEL
THE BELLY TAC
140
140
14
40
13
135
13
35
5
A
U
T
O
VIDEO
SELECTOR
SWITCH
CKPT
TAXI
T.O INHIBIT
NO SMOKING
SEAT BELTS
CABIN
IMAGE FROM
THE TACS SHOWN
ON THE SD
Page 236
ECAM DISPLAY
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
23
RMP PRESENTATIONTOWING ON BAT
POWER
HIGH
MED
ACTIVATION / NON ACTIVIATION
ON
LOW
SYMBOL OF RADIO RECEPTION
MAINTENANCE ICP
FUEL
REFUEL
RESET
END
FAULT
F
FAUL
LT
ON
ON
ENG
F
FADEC
GND PWR
1
2
VENT
OXYGEN
GND HF
DATALINK
AVNCS
EMER 2
GND COOLG
HF KEY
1
A
U
EMER 1
ACTIVATION
OFF
OFF T
O
CKPT DOOR
LOCKG SYS
SVCE INT
OVRD
Training by Airbus
RADIO CHANNEL
NAMES
LINE SELECTION
KEY
VHF
HF
TEL
SQWK
MENU
HF1
13.500
NAV
26.8
2
DATA
AIR
REMOTE
C/B CTL
OVHT COND
22.750
FANS RESET
STANDBY
FREQUENCIES
STBY
HF2
DATA
FAULT
ON
ON
OVRD
OVRD
OFF
ON
ON
MESSAGE LINE
TRANSMISSION
KEYS
ON
NOTE
BAT
OFF
DIALING KEY
MAINT
TEST
ACTIVE GND
MODE
CONNECTION
FREQUENCIES
255 VM
CHARGE
ON
MSG
CLR
RST
SQUAWK: 0163
CALL
CALL
CALL
VHF1
HF1
TEL1
CALL
CALL
CALL
VHF2
HF2
TEL2
RECEPTION
KEY
CALL
VHF3
INT
RAD
1
2
3
4
5
6
7
8
9
.
0
MECH
ATT
INT
CAB
RAD
NAV
BRT
.
.OF
OFF
LOAD
CLR
SELECTION
BOX (WITH
SCROLLING
LIST)
NUMERICAL
KEYPAD
VOICE
PA
ADF 2
1
LS 1
VOR
R
2
MKR
INTERCOM / RAD
SELECTOR SW
Page 237
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
23
RMP PRESENTATION
Training by Airbus
FOR ACTIVATION OF LOG OFF
SATCOM
FOR ACTIVATION OF
OR AUTOMATIC LOG ON
SETTINGS PAGE
LOG OFF OR MANUAL
ACTIVATION / DIALING
LINE SELECTION
ACCESS
LOG ON
KEY
KEY
*DIAL
MENU
TELEPHONE
LOGGINS
INDICATION
KEY
NUMBER
LOGGING STATUS
STATUS
TEL KEY
SATELLITE
NOTE
LIST
VHF
TELEPHONE
CHANNELS
* END
INDICATION
TRANSMISSION
KEYS
NUMERIC
KEYPAD
HF
TEL
SQWK
MENU
VHF
NAV
HF
TEL
MENU
003356158557
STATUS
LOGGED ON AUTO
LOG OFF *
* END
TEL 2
MEDICAL CENTER
SAT
SFTY
CABIN CALLS
DISABLED
ENABLE *
CONNECTING
CALL
HF1
TEL1
CALL
CALL
CALL
VHF2
HF2
TEL2
CALL
VHF3
INT
1
2
3
4
5
6
7
8
9
.
0
CLR
MECH
ATT
INT
CAB
NAV
MANUAL LOG ON *
SAT (2 /4)
GES (1/5)
< RETURN
RST
GOONHILLY
MSG
CLR
RST
GES
LIST
RMP, SATCOM
SETTINGS PAGE
LOAD
VOICE
PA
ADF
RAD
1
NAV
MENU
ATLANTIC WEST
RMP, SATCOM
CONFIG PAGE
BRT
.
.OF
OFF
SQWK
STATUS
LOGGED OFF
SATCOM SETTINGS >
MSG
CLR
RST
SQUAWK: 2631 ON
CALL
TEL
SATCOM SETTINGS
MEDICAL CENTER
PUBLIC
CALL
HF
SATCOM CONFIG
TEL 1
SAT
VHF1
VHF
NAV
* DIAL
ICAO
24312601
MSG
CLR
SQWK
1
2
MKR
A/C REGISTRATION AIRLINE
IDENTIFIER
NUMBER
EQUIPMENT
STATUS
DATALINK
COMMUNICATION
COMMUNICATION STATUS
SYSTEMS
VHF
VHF
RMP, TEL PAGE
HF
TEL
SQWK
MENU
HF
F - WWAY
SQWK
MENU
NAV
DATALINK COM STATUS
DATALINK INIT
A/C REGISTRATION
TEL
NAV
A/L IDENT
TI/TIA
< RETURN
MSG
CLR
RST
RMP, DATALINK INIT
SUB-PAGE
MSG
CLR
EQPT
STATUS
DTLNK COM
STATUS
VHF 2/3
DATA
AVAIL
HF 1/2
VOICE
SAT
DATA
AVAIL
RST
Page 238
RMP, DATALINK COM STATUS
SUB-PAGE
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
23
CVR SYSTEM (COMPONENTS LOCATION)
Training by Airbus
FR93
NOTE
A
FR86
Z172
FR85
B
CVR
2RK
A
B
Page 239
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
23
ATA 44
CABIN SYSTEMS
CIDS DESCRIPTION - CIDS DIRECTORS - MEMOR CARDS
COCKPIT CONTROLS
AND INDICATING
Training by Airbus
CABIN CREW RELATED FUNCTIONS
NOTE
AIP
AIRCRAFT SYSTEMS
(E.G.: ELM, CPCS)
HANDSET
AAP
CIDS DIRECTOR
CIDS
FUNCTION
LAVATORY SIGN
ACP
MIDDLE LINES
APPLICATION
ATA XX
TOP LINES
MEMORY
CIDS
PED
POWER
EMER
IPRAM
LIGHTS
MAIN
ON/OFF
MENU
LAV
MAINT
SCREEN
3D secLOCK
EVAC
CMD
EVAC
RESET
SMOKE
RESET
1
PAX
SYS
FAP-PC
RESET
DEU A
CB
1
...
42
1
...
8
2
PASSENGER RELATED FUNCTIONS
OBRM
CAM
DEU B
CB
FAP
- PAX CALL LIGHTS & BUTTONS
- PAX LIGHTED SIGNS & INFO
EMER
PED
POWER
IPRAM
LIGHTS
MAIN
ON/OFF
LAV
MAINT
SCREEN
3D secLOCK
CAM
EVAC
CMD
EVAC
RESET
SMOKE
RESET
FAP-PC
RESET
OBRM
PAX
SYS
CABIN SUPPORT SYSTEMS
(E.G.: CABIN TEMPERATURE,
CABIN LIGHTING)
Page 240
PSU
CABIN LIGHTING
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
44
CIDS INTERFACES - DESCRIPTION - EMERGENCY EVAC SIGNALING SYSTEM
AUDIO PERIPHERALS
SMOKE DETECTORS
SMOKE
DETECTION
FUNCTION
RAIMS
RMP
VHF
HF
TEL
121.700
MSG
CLR
SQWK
LOUDSPEAKERS
MENU
NAV
118.300
VHF2
122.465
DATA
VHF3
125.500
HF
NAV
CALL
CALL
CALL
CALL
1
2
7
8
.
0
FAP
NAV
RST
VHF 1 RECEPTION NOT SELECTED
CALL
NOTE
STBY
VHF1
TEL
123.125
CALL
Training by Airbus
IFE
3
T
RST
MECH
9
T
CLR
RST
ATT
VOICE
.
6
CALL
MECH
V INT
1
ATT 2
CAB MKR
. PA
AMU
VOICE
CALL
ADF
MECH
V
1
ATT 2
VOICE
MKR
2
MKR
CIDS
LIGHTS
MAIN
ON/OFF
MENU
LAV
MAINT
FWS
PED
POWER
IPRAM
EVAC
CMD
CAM
LIGHTS
MAIN
ON/OFF
EVAC
RESET
SMOKE
RESET
LAVATORY CALL & SMOKE
INDICATOR LIGHT
PAX
SYS
FAP-PC
RESET
MENU
LAV
MAINT
SCREEN
3D secLOCK
CAM
EVAC
CMD
OBRM
EVAC
RESET
SMOKE
RESET
FAP-PC
RESET
PAX
SYS
OBRM
CIDS
DIRECTOR
EVAC PANEL
EVAC
SCREEN
3D secLOCK
CIDS
IPRAM
EMER
BUZZER
COMMAND
PED
POWER
EMER
EVAC HORN
CAPT &
HORN OFF
PURS
EVAC
ON
DEU A
CAPT
APT
PSA
LOUDSPEAKERS
A/C SYSTEMS
SFCC
HANDSET
LGERS
PCS
CDLS
CABIN SUPPORT SYSTEM
(E.G.: TEMPERATURE CONTROL,
POTABLE WATER)
A
F
D
X
N
E
T
W
O
R
K
DEU B
1
AIP
AAP
ACP
Page 241
2
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
44
IVMS FUNCTION AND DESCRIPTION
Training by Airbus
AFDX NETWORK
NOTE
CDS
T.O
CONFIG
CDLS
DEFRD
RCL
LAST
PDLS
DISPCH
SD
ENG
DOOR
VIDEO
CLEAR
ALL
EL/AC
EL/DC
APU
BLEED
CLEAR
CIDS
ECP
SD
CIDS
DIRECTOR
CIDS
EMER
CMV
1
CVMS
PED
POWER
LIGHTS
MAIN
ON/OFF
MENU
LAV
MAINT
IPRAM
SCREEN
3D secLOCK
EVAC
CMD
EVAC
RESET
SMOKE
RESET
FAP-PC
RESET
PAX
SYS
OBRM
CAM
FAP
DEU B
2
CDSS
ADU
CIDS
ADU
2
3
EMER
PED
POWER
IPRAM
1
4
LIGHTS
MAIN
ON/OFF
MENU
LAV
MAINT
SCREEN
3D secLOCK
CAM
EVAC
CMD
EVAC
RESET
SMOKE
RESET
FAP-PC
RESET
1
PAX
SYS
OBRM
MASTER FAP
2
ECAS P/BSW
DVR
CAMERAS
(UP TO 20)
(VIDEO/AUDIO)
CAMERAS
(UP TO 4)
(VIDEO)
Page 242
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
44
IFE ARCHITECTURE OVERVIEW
Training by Airbus
OVERHEAD
DISPLAY UNIT
NOTE
CABIN DISTRIBUTION NETWORK
- EXTERNAL VIDEO SYSTEM
(ETACS, LANDSCAPE CAMERA)
- SATCOM SYSTEM
- ETC.
CIDS DIRECTORS
FDB
IFE CENTER RACK
A/C SYSTEMS
1
...
HEAD-END EQUIPMENT
- COMPUTERS
- VIDEO/AUDIO SOURCES
- FILES SERVERS
- THIRD PARTY EQUIPMENT
- TELEPHONE FUNCTION
X
SEB
1
...
IFE CONTROL
X
SEAT EQUIPMENT
Screen
Off
Pre-recorded Announcement
Group 1
Group 2
Information
IFE music
announcement
is active.is active.
File Selection
Playlist
-----------------
lish
Vid Eng
Term Stop SA Eng
Trans Out No Crew Eng
Trans Out Crew Eng
Trans SA Crew Eng
Term Stop SA Eng
Atlanta Eng
Aus Land Eng
Kinshasa Eng
Luanda Eng
Mauritius Eng
New York Eng
London Eng
Mauritius Eng
New York Eng
London Eng
Trans SA Crew Eng
Delete
Item
Delete
All
Water 340-2_3 Eng
Information
Player
Auto announcement running
Water 340-6 Eng
Add
to List
CIDS
Cabin
Status
Music
Pre
Ann
Lights
Seat
Sett
CIDS
EMER
PED
POWER
IPRAM
RCC CONTROL
PANEL
CWS CONTROL
PANEL
LIGHTS
MAIN
ON/OFF
Cabin
Status
Pax
Call
Lights
MENU
LAV
MAINT
SCREEN
3D secLOCK
CAM
EVAC
CMD
EVAC
RESET
SMOKE
RESET
FAP-PC
RESET
PAX
SYS
OBRM
FAP
SDU
PCU
Page 243
HEADSET
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
44
CABIN SIGNS CONTROLS
Training by Airbus
NOTE
CDS / SD
COMMAND
MECH CALL
EVAC
HORN OFF
CAPT &
PURS
EVAC
ON
CAPT
APT
CALLS
PURS
EMER
ALL
MID
EXIT
SIGNS
NO SMOKING
ON
AUTO
CALL
CA
ALL
ON
O
N
FWD
SEAT BELTS
ON
OFF
EMER
EXIT LT
ON
AUTO
OFF
ARM
OFF
F
OFF
AFT
Page 244
SIGNS PANEL
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
44
IFE POWER CONTROL
Training by Airbus
NOTE
CIDS
EMER
PED
POWER
IPRAM
LIGHTS
MAIN
ON/OFF
MENU
LAV
MAINT
SCREEN
3D secLOCK
EVAC
CMD
CAM
EVAC
RESET
SMOKE
RESET
FAP-PC
RESET
CF CARD REMOVAL
PAX
SYS
OBRM
FAP
CIDS
EMER
PED
POWER
IPRAM
LIGHTS
MAIN
ON/OFF
MENU
LAV
MAINT
SCREEN
3D secLOCK
EVAC
CMD
EVAC
RESET
CAM
SMOKE
RESET
FAP-PC
RESET
PAX
SYS
OBRM
Page 245
FAP CONTROL PANEL
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
44
IFE POWER CONTROL
Training by Airbus
NOTE
Page 246
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
44
ATA 33
LIGHTS
GENERAL AMBIENT LIGHTING
LIGHTING
MODULE (LEFT)
Training by Airbus
F/O DOME
F
LIGHT
NOTE
CAPT DOME
CA
LIGHT
ON/OFF
LIGHTING
MODULES (CENTER)
LIGHTING
MODULE (RIGHT)
CAPT DOME
LIGHT
ON/OFF
MAIN INSTRUMENT
PANEL LIGHT
F/O DOME
LIGHT
CENTER PEDESTAL LIGHT
DOME LIGHT SWITCH
NAV
AID
C/L
MENU
C/L
MENU
Q
CAPT OUTER
VU LIGHT
TO
GA
TO
GA
FLX
M
C
T
FLX
M
C
T
CL
CL
A
A
SPACE
SPACE
T
H
R
T
H
R
0
0
135 VM
VHF
MSG
CLR
F/O OUTER
VU LIGHT
HF
TEL
SQWK
MENU
NAV
VHF
STBY
121.700
VHF1
121.900
123.125
VHF2
123.450
DATA
VHF3
DATA
ON
CALL
CALL
CALL
CALL
1
2
4
5
7
8
3
ON
ENG START
1
NORM
FIRE
2
IGN
FAULT
CRANK
OFF
T.O
CONFIG
DEFRD
9
MORE
ENG
DOOR
WHEEL
FUEL
121.900
VHF2
123.450
VHF3
DATA
CALL
CALL
CALL
CALL
VIDEO
CALL
VIDEO
CLEAR
1
EL/AC
EL/DC
HYD
APU
BLEED
COND
CLEAR
ALL
WXR
TCAS
ELEVN
ABV
RET
1
2
4
5
7
8
.
3
F/CTL
9
VOICE
INT
1
SYS 1
SYS 1
XPDR
TCAS
MKR
BRT
BR
B
OFF
F
WXR
ELEVN
GAIN
FULL
FULL
INTEG LT
.
6
CLR
PRESS
TA
TA
ONLY
WXR
TAWS
FLOOD LT
RST
CALL
VHF3
BLW
GAIN
C
A
P
T
1/2
CKPT LT
STBY
MKR
RET
PARK BRK
NAV
VHF1
MECH
SD
INT
SPEED
BRAKE
SQWK
DATA
RCL
ALL
STS
DISPCH
VOICE
TEL
123.125
ABN
RCL
LAST
CLR
VHF3
HF
121.700
SQUAWK: 2523
CLR
.
6
.
MECH
CALL
FIRE
FAULT
OFF
RST
VHF 1 RECEPTION NOT SELECTED
F
/
O
0
0
1
1
2
2
SYS 2
2
2
SYS 2
3
3
DOME LT
FLAPS
INHIBI
BIT
INHIBIT
115 VM
ACCU
REINFLATE
YELLOW
0
4
ACCU
PSI
x1000
0
4
PULL & TURN
GREEN
L/G GRVTY EXTN
FLOOD LT
CKPT LT
NOSE
INTEG LT
R
RESET
VHF
HF
TEL
MENU
NAV
RESET
OFF
BRT
OFF
BRT
DU MASTER BRT
OFF
DOME LT
OFF
ON
OPEN
FAULT
DOWN
BRT
OFF
STORM
MSG
CLR
SLEW
TEST
121.700
VHF1
123.125
VHF2
DATA
VHF3
OFF
FF
121.900
123.450
STBY
DATA
RST
SQUAWK: 2523
STATUS
CALL
CALL
CALL
CALL
0123456789
CALL
CALL
1
2
3
4
5
6
7
8
9
MECH
CALL
STORM
BRT
BR
B
.
ATT
VOICE
INT
1
VHF3
1
Page 247
2
MKR
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
INSTRUMENT PANEL LIGHTING - PEDESTAL & OUTER VU LIGHTS
Training by Airbus
NOTE
CAPT OUTER
VU LIGHT
F/O OUTER VU LIGHT
OFF/BRT CONTROL
NAV
AID
STORM
C/L
MENU
C/L
MENU
ATC
245 VM
TO
GA
TO
GA
FLX
M
C
T
FLX
M
C
T
CL
CL
A
A
SPACE
SPACE
CKPT
PT LT
OFF/BRIGHT
CONTROL
FLOOD LT
T
H
R
T
H
R
0
0
135 VM
VHF
INTEG LT
MSG
CLR
HF
TEL
MENU
121.700
VHF1
123.125
VHF2
DATA
VHF3
NAV
VHF
STBY
121.900
ON
CALL
1
FIRE
NORM
FAULT
2
FAULT
OFF
MSG
CLR
RST
3
0
CLR
VOICE
1
1
OFF
F
DOOR
VHF2
FUEL
VIDEO
DU MASTER B
BRT
INHIBIT
ON
INHIBI
BIT
N
DOME LT
ENG 1
ENG 2
APU
F
SQUIB
FIRE
TEST
DISCH
1/2
COND
TCAS
3
.
HF2
0
CLR
TEL2
CLEAR
ATT
VOICE
INT
1
VHF3
F/CTL
1
2
MKR
PRESS
WXR
TA
ELEVN
TA
ONLY
DN
F
/
O
SYS 1
WXR
TAWS
SYS 2
SYS 1
XPDR
TCAS
SYS 2
FULL
FULL
PARK BRK
0
0
1
1
2
2
2
2
3
3
FLAPS
L
115 VM
ACCU
REINFLATE
YELLOW
4
PSI
x1000
0
STORM
HYD
BLEED
ABV
BLW
0
F
EL/DC
APU
ELEVN
C
A
P
T
ACCU
4
PULL & TURN
GREEN
L/G GRVTY EXTN
FLOOD LT
CKPT LT
NOSE
NOSE
INTEG LT
VHF
HF
TEL
SQWK
MENU
NAV
RESET
OFF
BRT
DOME LT
OFF
STORM
BRT
ON
CKPT DOOR
OPEN
FAULT
DOWN
BRT
BR
B
OFF
DU MASTER BRT
OFF
OFF
FF
AGENT 2
VIDEO
EL/AC
ALL
WXR
RET
RET
SPEED
BRAKE
STBY
DATA
2
7
CALL
MORE
WHEEL
CLEAR
2
MKR
BRT
BR
B
NAV
121.900
123.450
RST
1
MECH
ENG
CALL
VHF3
BRT
BR
B
VHF3
RCL
ALL
SD
CALL
OFF
FF
MENU
VHF1
VHF2
ABN
STS
DISPCH
ATT
TEL
DATA
SQUAWK: 2523
T.O
CONFIG
RCL
LAST
.
TEL2
MECH
HF
121.700
123.125
CALL
DEFRD
CALL
HF2
FIRE
IGN
OFF
DATA
2
7
CALL
VHF2
ON
ENG START
1
123.450
VHF 1 RECEPTION NOT SELECTED
CALL
BRT
OFF
STORM
CLR
SLEW
121.700
VHF1
121.900
123.125
VHF2
123.450
DATA
VHF3
DATA
STBY
RST
SQUAWK: 2523
TEST
CALL
CALL
CALL
CALL
CALL
CALL
0123456789
1
2
4
5
7
8
9
.
0
CLR
MECH
3
6
ATT
VOICE
CALL
1
2
MKR
Page 248
CENTER PEDESTAL LIGHT
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
Training by Airbus
CAPT CONSOLE
LIGHT
F/O CONSOLE
LIGHT
313 VU
MAP LT
L
OFF
BR
RT
BRT
CONSOLE LT
OFF
314 VU
OIS
OIS
A
AVNCS
A
AVNCS
EFB
EFB
VIEW
OFFSIDE
VIEW
OFFSIDE
INOP
INOP
ON
ON
L
MAP LT
OFF
BR
RT
BRT
CONSOLE LT
OFF
BR
BRT
BRT
BR
PEDALS LT
ON
PEDALS LT
ON
OFF
F
OFF
ON/OFF
NOTE
OFF / DIM / BRIGHT
OFF / DIM / BRIGHT
PILOT INDIVIDUAL WORKING - AREA LIGHTING
ON/OFF
Page 249
CAPT RUDDER-PEDALS LIGHTS F/O RUDDER-PEDALS LIGHTS
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
INSTRUMENT AND PANEL INTEGRATED LIGHTING - LEDS - DIMMING CONTROL UNIT
Training by Airbus
GLARESHIELD LIGHTING CONTROL
TAXI
MACH SPD SPD
TAXI
QNH
CSTR
1016
in Hg
WPT
VORD
NDB
WX
TERR
TRAF
TRUE
TRUE MAG MAG
SPD
MAG
---
HDG
HDG
HDG
V/SV/S
---
LS
ARC
PLAN
40
20
IXAT
V/S
7000
1000
1000
100
100
FD
NAV
VV
METER
ALT
TRK
TRK
FPAFPA
hPa
VOR
LS
ARPT
CSTR
-----
AP1
10
320
ZOOM
640
A/THR
20
ALT
NDB
TERR
TRAF
ARPT
TAXI
QNH
APPR
NOTE
1016
hPa
in Hg
40
AP2
DN
LOC
VORD
WX
UP
80
160
WPT
NAV
80
160
10
320
ZOOM
640
VOR
LS
ARC
PLAN
VV
LS
DIMMING CONTROL UNIT
INSTRUMENT & PANEL
INTEGRATED LIGHTING CONTROL
INPUT ORDERS
CKPT LT
FLOOD LT
BRT
BR
B
OFF
F
TORM
STORM
BRT
BR
B
DU MASTER BRT
INHIBIT
INHIBI
BIT
ON
DOME LT
OFF
FF
OFF
F
INTEG LT
Page 250
BR
B
BRT
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
ANNUNCIATOR LIGHT TEST AND DIMMING SYSTEM
Training by Airbus
ICP ANNUNCIATOR LIGHTS
CONNECTED TO CAN NETWORK
NOTE
FAULT
OFF
INOP
ON
VU PANEL
ANNUNCIATOR
LIGHTS
STBY
COMPASS
E REF
& EYE
ANN LT
TEST
ICE
IND
ON/OFF
INT LT
BRT
OFF
DIM
COMPASS
& EYE REF
ANN LT
TEST
FAULT
RELAY
OFF
ICP ANNUNCIATOR LIGHTS
NOT CONNECTED TO
CAN NETWORK
ICE
IND
FD
AP1
EYE REFERENCE LIGHT
LOC
AP2
A/THR
LIGHTED EQUIPMENT
ANNUNCIATOR LIGHTS
Page 251
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
UTILITY LIGHTS - PILOT UTILITY LIGHTS
Training by Airbus
POTENTIOMETER
DIAPHRAGM CONTROL
POTENTIOMETER
DIAPHRAGM CONTROL
NOTE
F/O READING LIGHT
CAPT READING LIGHT
M
CAPT MAP
LIGHT
P LIGHT
F/O MAP
313 VU
MAP LT
OFF
BRT
B
R
CONSOLE LT
L
OIS
OIS
A
AVNCS
A
AVNCS
EFB
EFB
VIEW
OFFSIDE
VIEW
OFFSIDE
INOP
ON
OFF
BR
RT
R
BRT
314 VU
POTENTIOMETER
POTENTIOMETER
MAP LT
OFF
BRT
B
R
L
CONSOLE LT
INOP
ON
OFF
BR
BRT
R
PEDALS L
LT
ON
PEDALS LT
L
ON
O
OFF
F
OFF
CAPT SLIDING
TABLE LIGHTS
Page 252
F/O SLIDING
TABLE LIGHTS
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
UTILITY LIGTHS - OCCUPANT UTILITY LIGHTS
Training by Airbus
NOTE
612 VU
3RD OCCPNT
READING LT
OFF/DIM/BRIGHT
OFF
3 RD OCCUPANT
OC
CONSO
CONSOLE LIGHT
BRT
B
R
3RD OCCPNT
CONSOLE LT
3 RD OCCUPANT
READING LIGHT
OFF
BRT
BR
OFF/DIM/BRIGHT
110VAC/60HZ
V
100W MAX
4 TH OCCUPANT
READING LIGHT
4TH OCCPNT
READING LT
OFF/DIM/BRIGHT
OFF
Page 253
B
BRT
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
UTILITY LIGHTS - COAT STOWAGE LIGHTS
Training by Airbus
NOTE
COAT STOWAGE
UPPER COAT
STOWAGE LIGHT
543 VU
AVNCS LT
OUTLET-115VAC
614 VU
115VAC
360-800 Hz
COAT
STWG LT
ON
OUTLET-28VDC
OFF
28VDC
LOWER COAT
STOWAGE LIGHT
Page 254
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
CABIN LIGHTING - GENERAL LIGHTING & APPLICATION LIGHTS
CONTROL AND MONITORING
APPLICATION LIGHTS
HANDRAIL LIGHTS
(OPTIONAL)
CEILING RECESS LIGHTS
Training by Airbus
GENERAL LIGHTS
NOTE
CEILING LIGHTS
SIDEWALL LIGHTS
FAP LIGHTS PAGE
CEILING LIGHTS
CEILING RECESS LIGHTS
HANDRAIL LIGHTS
ALL THE CABIN LIGHTING ELEMENTS
USE LED TECHNOLOGY
Page 255
SIDEWALL LIGHTS
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
ENTRANCE AREAS
CONTROL AND MONITORING
Screen
Off
Training by Airbus
ENTRANCE AREA (EXAMPLE)
Lights
Caution
Rooms
Zones
Entries
Aircraft-wide Adjustment
General Lights
Night
Mode
R/L
Off
R/L
On
Main
On
Rooms
Intensity
Room 1
Bright
100 %
Bright
Bright
Room 2
Off
0%
Decor
Lights
Entire Scenario
Room 3
Modified
63 %
Room 4
Bright
100 %
Room 5
Modified
90 %
Off
Off
Lights
Select
Cruise
Room 6
Off
0%
Room 7
Modified
35 %
Room 8
Off
CIDS
NOTE
63 %
Cabin
Status
Music
Pre
P
Video
Vide
Ann
PA
Lights
R/L
Off
R/L
On
Decor
Lights
0%
Doors/
Slides
Temp
Water/
Waste
Smoke
Detect
Seat
Sett
Cabin
Status
Pax
Call
FAP LIGHTS PAGE
SPOTLIGHTS
Lights
DIRECT CEILING LIGHT
SPOTLIGHTS
DOME LIGHT IN DOOR 2
(OPTIONAL)
Page 256
DIRECT CEILING LIGHTS
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
STANDALONE SIGNS
Training by Airbus
NOTE
PSU
PSU
PS
SU
CABIN
PAX PERS LANDSCAPE
CAMERA
ELEC SPLY
FASTEN SEAT BELT
LAVATORY OCCUPIED
OFF
OFF
PAX INFO
MOBILE COM
LAVATORY
OFF
OFF
OCCPD
SEAT BELTS
ON
O
SIGNS
NO SMOKING
ON
O
AUTO
OFF
NO SMOKING
NO MOBILE
ON
O
AUTO
AUTO
OFF
EMER
EXIT LT
ON
OFF
RETURN TO SEAT
ARM
OFF
OFF
NO PORTABLE
ELECTRONIC DEVICES
Page 257
STANDALONE SIGNS
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
ARCHITECTURE AND INTERFACES
Training by Airbus
A/C SYSTEMS
SIGNS
SEAT BELTS
NO SMOKING
ON
ON
O
AUTO
OFF
CABIN GENERAL LIGHTING
EMER
EXIT LT
ON
NOTE
ARM
AUTO
OFF
F
OFF
SPOTLIGHTS
OFF
LAVATORY LIGHTS
DEU A
PASSENGER READING LIGHTS
ATTENDANT WORK LIGHTS
CIDS
DIRECTOR
CIDS
EMER
PED
POWER
IPRAM
LIGHTS
MAIN
ON/OFF
1
...
MENU
LAV
MAINT
SCREEN
3D secLOCK
EVAC
CMD
EVAC
RESET
CAM
SMOKE
RESET
FAP-PC
RESET
PAX SIGNS (ATA 44)
X
PAX
SYS
OBRM
FAP
1
2
COCKPIT LAVATORY INDICATOR
DEU B
STANDALONE SIGNS
1
...
X
Page 258
AAP
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
CABIN - LIGNTING COMPONENT DESCRIPTION - FUNCTIONAL LOGIC
Training by Airbus
FAP
NOTE
CIDS
EMER
PED
POWER
IPRAM
Main
On
LIGHTS
MAIN
ON/OFF
ILLUMINATION
DEVICES
MENU
LAV
MAINT
SCREEN
3D secLOCK
EVAC
CMD
CAM
EVAC
RESET
SMOKE
RESET
FAP-PC
RESET
PAX
SYS
OBRM
LIGHTS
MAIN
ON/OFF
FULL
BRIGHTNESS
(100%)
1
NLG ON GROUND
COCKPIT DOOR UNLOCKED
ENGINES IN OPERATION
TOTAL LOSS OF CIDS DATA BUS SYSTEM
LOSS OF THE CIDS
CABIN DECOMPRESSION
AND
COCKPIT
DOOR
AND
FWD
SPOTLIGHT
ENTRANCE
DIMMED
(10%)
SPOTLIGHTS
OR
70%
FULL
BRIGHTNESS
1
Page 259
LAVATORY LIGHTS AND READING LIGHTS ALSO CONCERNED BY THIS FUNCTION
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
LAVATORY LIGHTING ARCHITECTURE AND INTERFACE
Training by Airbus
MIRROR LIGHTS (LEDs)
CEILING LIGHTS
(LEDs)
FAP
NOTE
WASHTABLE LIGHTS
(LEDs)
OPEN
LOCKED
CLOSED
CIDS
EMER
PED
POWER
IPRAM
LIGHTS
MAIN
ON/OFF
MENU
LAV
MAINT
SCREEN
3D secLOCK
CAM
EVAC
CMD
EVAC
RESET
SMOKE
RESET
100%
50%
10%
PAX
SYS
FAP-PC
RESET
OBRM
LAV MAINT KEY
(100% BRIGHTNESS)
CIDS DIRECTOR
1
LAVATORY
LIGHT
ADAPTER
DEU A
1
2
AAP
...
100%
BRIGHTNESS
SWITCH
X
LAVATORY OCCUPIED SIGN
DEU B
LAVATORY
Page 260
OCCPD
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
READING LIGHTS ARCHITECTURE AND INTERFACE - PASSENGER READING LIGHTS
Training by Airbus
LIGHT P/BSW
MAIN ON/OFF
FUNCTION
Main
On
READING LIGHTS P/BSWs
NOTE
FAP/CABIN
LIGHTING-PAGE
ATTENDANT WORK LIGHT
(IN STANDALONE LOCATION)
READING LIGHTS
ON/OFF FUNCTION
STANDALONE PSA
IFE
PSU
LED READING LIGHTS
(MAXIMUM 4 READING LIGHTS
FOR EACH PSU)
CIDS DIRECTOR
1
2
PCU
AFDX NETWORK
DEU A
1
...
PSA
X
(ONE PSA FOR EACH PSU)
(MAXIMUM 8 PSAs FOR EACH DEU A)
Page 261
LGERS
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
EMERGENCY LIGHTING SYSTEM
CABIN CEILING
EMERGENCY LIGHTS
MANUAL CONTROL
LED TECHNOLOGY
(EXCEPT PHOTOLUMINESCENT
FLOOR-PATH MARKING-SYSTEM)
FLIGHT CREW
Training by Airbus
MANUAL
CONTROL
NOTE
EMERGENCY
SPOTLIGHTS
FLOOR PATH
MARKING SYSTEM
CABIN ATTENDANT
EVACUATION
AREA LIGHTS
A/C SYSTEM
DOOR SILL LIGHTS
AUTOMATIC
CONTROL
EPSU (28VDC)
EXIT
LOCATION SIGNS
EMERGENCY LIGHTING
SYSTEM
EXIT SIGNS
Page 262
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
EMERGENCY LIGHTING CONTROL DESCRIPTION
115VAC NORM
(SPDB)
DETECTION
28VDC NORM
(SPDB)
POWER SUPPLY
AND DETECTION
28VDC EMER
(EPDC)
POWER SUPPLY
AND DETECTION
Training by Airbus
AFDX NETWORK
EPSU
CABIN
DECOMPRESSION
CIDS
DIRECTOR
1
LANDING GEARS
DOWNLOCKED
NOTE
CPIOM
CPIOM
CPCS
LGERS
1
2
...
1
X
...
X
EMER
EXIT LT
ON
ARM
OFF
F
OFF
EXIT SIGN ON
SIGNS
SEAT BELTS
NO SMOKING
ON
ON
O
AUTO
AUT
OFF
EMER
EXIT LT
ON
ARM
AUTO
OFF
OFF
F
OFF
BATTERY COVER
(7.2 VDC)
CIDS
EMER
PED
POWER
IPRAM
LIGHTS
MAIN
ON/OFF
EMERGENCY
LIGHTS AND SIGNS
MENU
LAV
MAINT
SCREEN
3D secLOCK
EVAC
CMD
EVAC
RESET
SMOKE
RESET
CAM
FAP-PC
RESET
PAX
SYS
OBRM
FAP
EMER
1
...
Page 263
8
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
21
EMERGENCY POWER - SUPPLY UNITS
PAX 3
PAX 2
PAX 1
Training by Airbus
PAX 4
NOTE
EPSUs
28VDC
(SPDB)
BATTERY COVER
B
(7.2 VDC)
28VDC
(EPDC)
EMERGENCY POWER-SUPPLY UNIT
CELLIs
CELLI STR
STRIP
Page 264
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
21
EMERGENCY SPOTLIGHTS
Training by Airbus
EMERGENCY SPOTLIGHT
NOTE
EPSUs
EP
28VDC
(SPDB)
28VDC
(EPDC)
ENTRY AREA
DOOR SILL LIGHT
GHT
EVACUATION AREA LIGHT
Page 265
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
FLOOR - PATH MARKING SYSTEM
Training by Airbus
EXIT MARKING SIGN
NOTE
EXIT LOCATION SIGN
WALL-MOUNTED
EMERGENCY LIGHT
28VDC
(SPDB)
EPSUs
EXIT IDENTIFIER
28VDC
(EPDC)
EDGE-MOUNTED
EMERGENCY LIGHT
PHOTO LUMINESCENT FPMS
Page 266
SEAT-MOUNTED EMERGENCY LIGHT
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
AVIONICS COMPARTMENT
LIGHT TOGGLE
SWITCH
Training by Airbus
POWER OUTLET
NOTE
NOTE: NO AUTOMATIC SWITCH OFF
BULK CARGO COMPARTMENT
SERVICE PANEL
PANEL LIGHT
LIGHT
TOGGLE
SWITCH
POWER OUTLET
AFT AND FWD CARGO
COMPARTMENT SERVICE PANEL
CARGO
COMPARTMENT LIGHTS
LOADING AREA LIGHT
TOGGLE SWITCH
PANEL LIGHT
AFT AND FWD CARGO
LOADING CONTROL PANEL
AFT AND FWD CARGO
DOOR OPERATION PANEL
LOADING AREA LIGHTS BULK CARGO LIGHTS
COCKPIT TOGGLE
SWITCH
AVIONICS COMPARTMENT
TOGGLE SWITCH (x2)
115VAC
115VAC AND 28VDC
POWER OUTLETS
Page 267
L
LED DOME LIGHT (x7)
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
CARGO LIGHTING OVERVIEW - SERVICE PANEL LIGHTS - CARGO COMPARTMENT LIGHTS
Training by Airbus
PANEL LIGHTS
NOTE
FWD CARGO DOOR
OPERATION PANEL
LOADING AREA LIGHTS
SWITCH ON
SPDB
SPDB
AFDX NETWORK
AFDX NETWORK
AFT CARGO DOOR
OPERATION PANEL
AFT & FWD CARGO
DOOR OPEN
DSCS
NOTE: AUTOMATIC SWITCH ON
AT LAST ENGINE SHUT DOWN
FWS
Page 268
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
NOSE LANDING GEAR BAYS & BELLY FAIRING COMPARTMENTS LIGHTING
AIR CONDITIONING DUCT & ACCESSORY
COMPARTMENT
NLG
BAY
MLG & BELLY
FAIRING BAY
Training by Airbus
MLG & BELLY
FAIRING LIGHTS
AIR CONDITIONING DUCT &
ACCESSORY COMPARTMENT
LIGHTS (LED TYPE)
TOGGLE
SWITCH
TOGGLE
SWITCH
(LED TYPE)
NOTE
NLG LIGHTS
(LED TYPE)
TOGGLE
SWITCH
115VAC & 28VDC
POWER OUTLETS
115VAC & 28VDC
POWER OUTLETS
SPDB
EPDC
AFDX NETWORK
28VDC POWER
OUTLET
NOTE: AUTOMATIC SWITCH OFF AT FIRST ENGINE START
Page 269
FWS
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
SERVICE AREA LIGHTING
Training by Airbus
WASTE-TANK AREA LIGHT
(LED TYPE)
LIGHTING CONTROL
SWITCH
NOTE
BULK CARGO AREA
SPDB
SPDB
28VDC POWER OUTLET
TOGGLE SWITCH
AFDX
NETWORK
AFDX
NETWORK
FWS
Page 270
NOTE: AUTOMATIC SWITCH OFF AT FIRST ENGINE START
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
STROBE LIGHTS - ANTI COLLISION STROBE LIGHTS
Training by Airbus
SYNCHRONIZATION WITH BEACON LIGHTS MONITORED
BY THE POWER SUPPLY UNIT OF THE LOWER BEACON
NOTE
POWER SUPPLY
UNIT
EXT LT
STROBE
ON
BEACON
ON
NAV
1
OFF
F
F
OFF
OFF
F
WING
ON
LDG
ON
NOSE
T.O
AUTO
OFF
LOGO
ON
AUTO
2
FF
F
OFF
WING-TIP STROBE LIGHT-LH
FROM THE LOWER
BEACON LIGHT PSU
TAXI
F
OFF
SYNCHRONIZATION
LED LIGHT TECHNOLOGY
OFF
CPIOM
ELCO
POWER SUPPLY
UNIT
A
F
D
X
FWS
LGERS
STROBE LIGHT OFF MEMO
N
E
T
W
O
R
K
WING-TIP STROBE LIGHT-RH
EPDC 2
POWER SUPPLY
UNIT
Page 271
REAR STROBE LIGHT IN THE
INTEGRATED TAILCONE LIGHT UNIT
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
ANTI-COLLING LIGHTS - ANTI COLLISION BEACON LIGHTS
Training by Airbus
NOTE
LED LIGHT TECHNOLOGY
EXT LT
BEACON
ON
NAV
1
F
OFF
OFF
F
F
OFF
WING
ON
LDG
ON
NOSE
T.
T.O
F
OFF
FF
OFF
OFF
AUTO
F
OFF
LOGO
ON
AUTO
2
TO THE PSUs OF
THE STROBE LIGHTS
TAXI
CPIOM
ELCO
A
F
D
X
N
E
T
W
O
R
K
SYNCHRONIZATION
STROBE
ON
EPDC 1
PSU
PSU
UPPER BEACON LIGHT
Page 272
LOWER BEACON LIGHT
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
21
NAVIGATION LIGHTS
Training by Airbus
WING-TIP NAV LIGHT-LH
(INTEGRATED POWER SUPPLY UNIT)
LED LIGHT TECHNOLOGY
REAR
NAVIGATION LIGHTS
CONNECTOR
NAV2
NOTE
CONNECTOR
NAV1
RH & LH
NAVIGATION LIGHTS
LED ARRAYS
EXT LT
STROBE
ON
CRDC
AUTO
2
WING
ON
LDG
ON
OFF
F
NOSE
T.O
T.
TAXI
OFF
F
OFF
FF
OFF
CPIOM
ELCO
A
F
D
X
N
E
T
W
O
R
K
1
15 V
115
BUL
50
50
V
REAR NAV LIGHT
28V
BUL
833
7448
2--7
762 2
76
6 3A
OFF
F
833
7448
2--7
762 2
76
6 3A
OFF
F
AUTO
OFF
F
WING-TIP NAV LIGHT-RH
(INTEGRATED POWER SUPPLY UNIT)
LOGO
ON
N
GI
NAV
1
V
3A
3A
3A
3
A
NWS
N
GI
BEACON
ON
LIGHT
TEST
GND SVCE
CTL 2
NLG
LGT
DISCONNECT
H
A
B
G
K
J
C
F
PMAT
E
D
TOW
TRUCK POWER
WING-TIP NAV LIGHT
STEERING
DISCONNECT
PANEL ON NLG
POWER SUPPLY UNIT
TOW TRUCK POWER
(CONNECTED TO NAV 1)
EPDC
1
2
CONNECTOR
NAV1
Page 273
CONNECTOR
NAV2
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
21
LOGO LIGHTS
Training by Airbus
LOGO LIGHTS-LH
NOTE
A35
0
EXT LT
STROBE
ON
BEACON
ON
NAV
1
AUTO
OFF
F
LOGO
ON
AUTO
2
OFF
F
F
OFF
OFF
F
WING
ON
LDG
ON
NOSE
T.
T.O
F
OFF
FF
F
OFF
OFF
LED TECHNOLOGY
POWER SUPPLY UNIT
TAXI
POWER SUPPLY UNIT
CPIOM
ELCO
A
F
D
X
SFCC
SLATS EXTENDED
LGERS
NLG ON GROUND
N
E
T
W
O
R
K
SPDB
Page 274
LOGO LIGHTS-RH
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
21
WING AND ENGINE SCAN LIGHTS
EXT LT
STROBE
ON
BEACON
ON
NAV
1
OFF
F
F
OFF
OFF
F
WING
ON
LDG
ON
NOSE
T.
T.O
FF
OFF
OFF
FF
OFF
AUTO
OFF
F
Training by Airbus
WING & ENGINE SCAN LIGHT-LH
LOGO
ON
NOTE
AUTO
2
TAXI
LED TECHNOLOGY
POWER SUPPLY UNIT
CPIOM
ELCO
POWER SUPPLY UNIT
A
F
D
X
N
E
T
W
O
R
K
EPDC 1
EPDC 2
Page 275
WING & ENGINE SCAN LIGHT-RH
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
21
RUNWAY TURNOFF AND TAXING LIGHTS
EXT LT
STROBE
ON
BEACON
ON
NAV
1
OFF
F
F
OFF
OFF
F
WING
ON
LDG
ON
NOSE
T.O
F
OFF
OFF
FF
F
OFF
AUTO
OFF
F
Training by Airbus
LOGO
ON
NOTE
AUTO
2
TAXI
LED TECHNOLOGY
CPIOM
ELCO
CRDC
A
F
D
X
N
E
T
W
O
R
K
NLG DOWNLOCKED
LGERS
Page 276
EPDC 1
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
21
TAXIING - AID CAMERA LIGHTS
EXT LT
STROBE
ON
BEACON
ON
NAV
1
AUTO
OFF
F
Training by Airbus
LOGO
ON
NOTE
AUTO
2
OFF
F
OFF
F
OFF
F
WING
ON
LDG
ON
NOSE
T.O
T.
F
OFF
OFF
FF
OFF
PSU
FWD TAXIING
CAMERA LIGHT-LH
FWD TAXIING
CAMERA LIGHTS
TAXI
AFT TAXIING
CAMERA LIGHTS
LED TECHNOLOGY
CPIOM
ELCO
PSU
AFT TAXIING
CAMERA LIGHT-LH
TAXI
A
F
D
X
CAPT EFIS
CONTROL PANEL
(SAME FOR F/O)
VIDEO
TACS ON
CMV
VIDEO
N
E
T
W
O
R
K
EPDC 1
PSU
FWD TAXIING
CAMERA LIGHT-RH
ECAM
CONTROL PANEL
LGERS
L/G ON GROUND
EPDC 2
Page 277
AFT TAXIING
CAMERA LIGHT-RH
PSU
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
21
LANDING LIGHTS
Training by Airbus
LED TECHNOLOGY
EXT LT
STROBE
ON
BEACON
ON
NAV
1
AUTO
F
OFF
LOGO
ON
LANDING LIGHT-LH
AUTO
2
F
OFF
OFF
F
F
OFF
WING
ON
LDG
ON
NOSE
T.
T.O
OFF
F
OFF
FF
F
OFF
EPDC 1
TAXI
CPIOM
ELCO
NOTE
A
F
D
X
N
E
T
W
O
R
K
CRDC
LANDING LIGHT-RH
Page 278
EPDC 2
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
21
TAKEOFF LIGHTS
Training by Airbus
NOTE
EXT LT
STROBE
ON
BEACON
ON
NAV
1
OFF
F
F
OFF
OFF
F
WING
ON
LDG
ON
NOSE
T.
T.O
F
OFF
FF
OFF
OFF
AUTO
OFF
F
LOGO
ON
TAKEOFF LIGHT-LH
AUTO
2
TAXI
LED TECHNOLOGY
EPDC 2
CPIOM
ELCO
A
F
D
X
NLG DOWNLOCKED
N
E
T
W
O
R
K
TAKEOFF LIGHT-RH
CRDC
LGERS
Page 279
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
21
EMERGENCY LIGHTING TEST FROM OMS INTERFACE
Training by Airbus
SCI
AFDX NETWORK
CMS
NOTE
OIS
CIDS
DIRECTOR
EMERGENCY LIGHTS
AND SIGNS
1
2
EPSU
DEU B
1
...
X
OIS
OMT
PMAT
MAINTENANCE
CREW
1
...
8
TESTS
SYSTEM TEST
DESCRIPTION
CHECKS THE LOGIC AND SWITCHING
CIRCUITS,BATTERY PACK VOLTAGE,
INTERIOR AND EXTERIOR CONNECTED LOADS.
BATTERY CAPACITY TEST
CHECKS THAT THE CAPACITY OF EACH EPSU
BATTERY IS SUFFICIENT TO SUPPLY ITS LOADS
FOR A MINIMUM OF 10 MINUTES.
Page 280
DURATION: AROUND 75 MINUTES
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
21
EPSU INDIVIDUAL LOCAL TEST
Training by Airbus
NOTE: IT IS NECESSARY TO ENSURE THAT ALL EMERGENCY
LIGHTS CONNECTED TO THE RELATED EPSU OPERATE CORRECTLY
BEFORE LAUNCHING THE TEACH IN PROCEDURE.
NOTE
EPSU
EPSU FRONT FACE
PRESS
TEST RESULT
GREEN = OK RED = FAULT
< 5 SEC FOR TEST
> 5 SEC FOR TEACH-IN
TEACH IN ACTIVE
WHEN 1 RED: EXCHANGE EPSU
UNIT
WHEN 1 FLASHING GREEN: SYSTEM TEST ACTIVE
BATTERY COVER
WHEN 2 RED: EXCHANGE BATTERY
WHEN 2 FLASHING GREEN:
BATTERY CAPACITY TEST ACTIVE
1
BATTERY
2
WHEN 3 OR 4 RED:
EXTERIOR LIGHT
CHECK EXTERIOR / INTERIOR LIGHT
WHEN 3 AND 4 FLASHING RED =
INTERIOR LIGHT
EPSU OVERLOAD:
EXIT SIGNS
CHECK ALL EMER LIGHTS
3
4
EMERGENCY
LIGHTS AND SIGNS
Page 281
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
21
EXTERIOR LIGHTING MAINTENANCE
Training by Airbus
OIS
SCI
AFDX NETWORK
NOTE
OMS
- TAXI CAMERA LIGHTS
- WING & ENGINE SCAN LIGHTS
- LOGO LIGHTS
CPIOM
ESBF
ELCO
FWS
A
F
D
X
N
E
T
W
O
R
K
OIS
OMT
PMAT
EXTERIOR LIGHTING SYSTEM
FAILURE DETECTION
D
LED
Page 282
POWER SUPPLY UNIT
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
ACMS EXTERIOR LIGHTING MAINTENANCE
NAVIGATION
ANTI COLLISION
NOSE
LANDING
WING & ENGINE
Training by Airbus
LOGO
TAXI CAMERA
NOTE
NAVIGATION
REAR
LEFT
1
1
2
1
18LA
17LA
FIN
RIGHT
2
2
16LA
Elapsed
0 h
0 h
8000 h
8000 h
12300 h
12300 h
Remaining
16660 h
16660 h
8860 h
8860 h
4360 h
4360 h
NO
NO
NO
NO
YES
YES
0,22 A
0
0,20 A
0
0,22 A
0
End of Life Reached
Consumption
A
A
A
Page 283
EXAMPLE OF LAYOUT OF THE EXTERIOR-LIGHTS SYSTEM PAGE FOR NAVIGATION LIGHTS
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
CABIN LIGHTING & EMERGENCY LIGHTING
Training by Airbus
FAP
NOTE
FAP
GENERAL LIGHTS
SECTION
ENTIRE SCENARIO
SECTION
CIDS
EMER
PED
POWER
LIGHTS
MAIN
ON/OFF
MENU
LAV
MAINT
SCREEN
3D secLOCK
IPRAM
CAM
EVAC
CMD
EVAC
RESET
SMOKE
RESET
FAP-PC
RESET
PAX
SYS
OBRM
LIGHTS
MAIN
ON/OFF
ENTIRE SCENARIO PAGE
LIGHT STRIPS SECTION
Page 284
LIGHTS KEY
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
33
Training by Airbus
GLOSSARY
CONVERSION TABLE, LIST ABBREVIATION & SYMBOLS CARD
P. 607
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
GLOSSARY
CONVERSION TABLE
Training by Airbus
From: S.I.
Measurement System
1 bar
1 mm2
1 cm2
1 daN
1g
1 hPa
1 kg
1 kg.min
1l
1l
1 l.min
1 mdaN
1 mdaN
1m
1 mm
1 cm3
1 hPa
=
=
=
=
=
=
=
=
=
=
=
=
=
=
=
=
=
To: US Customary
System
From : US Customary
System
14.5037 psi
0.0016 in.2
0.1550 in.2
2.2481 lbf
0.0353 oz
0.0295 in.Hg
2.2046 lb
2.2046 lb.min
0.2641 USgal
1.057 USquart
0.2641 USgal.min
88.4956 lbf.in
7.3801 lbf.ft
3.2809 ft
0.0394 in
0.06102 in3
0.0145 psi
1 psi
1 in.2
1 in.2
1 lbf
1 oz
1 in.Hg
1 lb
1 lb.min
1 USgal
1 USgal.min
1 USquart
1 lbf.in
1 lbf.ft
1 ft
1 in
1 in3
1 in.Hg
Temperature conversion from degrees Celsisus (deg.C) to degrees
Fahrenheit (deg.F) : deg.F = 1.8 x deg.C +32
Abbreviation
deg.F
ft
US gal
US quart
in
in.2
lb
lfb
lfb.in
To: S.I.
Measurement System
=
=
=
=
=
=
=
=
=
=
=
=
=
=
=
=
=
NOTE
0.0689 bar
645.1600 mm2
6.4516 cm2
0.4448 daN
28.3495 g
33.8640 hPa
0.4536 kg
0.4536 kg.min
3.7854 l
3.7854 l.min
0.9464 l
0.0113 mdaN
0.1356 mdaN
0.3048 m
25.4 mm
16.3871 cm3
0.491 psi
Temperature conversion from degrees Fahrenheit (deg.F) to degrees Celsius
(deg.C) : deg.C = 0.5555 x (deg.F - 32)
Definition
Abbreviation
Definition
Degrees Fahrenheit
Foot
US GALLON
US Quart
Inch
Square Inch
Pound
Pound Force
Pound Force Inch (Torque)
lfb.ft
in.Hg
oz
psi
US gal.min
ib.min
cc
daN
hPa
Pound Force -Foot (Torque)
Inch of Mercury
Ounce (Weight)
Pound Square Inch
US Gallon per minute
Pound per minute
Cubic Centimenter
Deca Newton
Hecto Pascal
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
LA
GLOSSARY
LIST ABBREVIATION
Training by Airbus
Abbreviation
Full Form
A/L
Under Airline
Responsibility
Airline
A/THR
Auto THRust
AAP
Additional Attednant Panel
ABDC
*
ABPM
ACARS
ACCLRM
ACMS
ACMS - RT
ACP
ACR
ACRS
ADIRU
Air Data / Inertial Reference
Unit
AICF - NAI
Anti Ice Control Function Nacelle Anti Ice
AOC
Airline Operational Control
ADR
Automatic Data Reference
AICS
Anti Ice Control System
AP
Autopilot
ADS
Automatic Dependent
Surveillance
AIP
Attendant Indication Panel
AP / FD
APU
Auxiliary Power Unit
ASCU
Air Systems Control Unit
ASF
Avionics Server Function
ASLC
ACD Security Log Collector
ASR
Aircraft Structural Repair
ATC
Air Traffic Control
ATIS
Automatic Terminal
Information Service
ADS - B
Automatic Dependent
Surveillance - Broadcast
AIRMAN
Avionics Broadcasr Data
Collector
ABS - C
Automatic Dependent
Surveillance - Contract
AISD
Aircraft Maintenance
Analysis
Airline Information Services
Domain
Avionics Bare Processing
Module
Aircraft Communication
Addressing and Reporting
System
AIU
Aircraft Interface Unit
ADSM
ALT
Altitude
AECM
AESS
Accelerometer
Aircraft Condition
Monitoring System
Aircraft Condition Monitoring
Sytem Real Time
Area Call Panel
Avionics Communication
Router
Avionics Communication
Routing System
AESU
Avionics Data Storage
Module
Alternate Extension Control
Module
Aircraft Environment
Surveillance System
Aircraft Environment
Surveillance Unit
ALT REFF
AMD
Alternate to a Retraction,
Extension and / or Free Fall
test
Aircraft Maintenance
Description
NOTE
Autopilot / Flight Director
AMDF
Airport Mapping DataBase
ATQC
Airbus Temporary Quick
Change
AMEX
Avionics Message
Exchanger
ATU
Auto Transformer Unit
AFDX
Avionics Full Duplex
AFI
Aircraft Fault Isolation
ATU Contactor
Air Traffic Service Facilities
Notification
AMP
Aircraft Maintenance
Procedure
ATUC
AFN
ATULC
ATU Line Contactor
AFR
Aircraft Fault Reporting
AMS
Audio Management System
ATUPU
ATU Protection Unit
AFS
Aircraft Flight System
AMU
Audio Management Unit
AVIs
Aircraft Virtual Insider
System
AVM
Avionics Video Module
AVNCS
Avionics
AWD
Aircraft Wiring Diagram
ACS
Air Conditioning System
AGB
Accessory GearBox
ANDT
Aircraft Non Destructive Test
ADF
Automatic Direction Finder
AGLC
ANF
Airport Navigation Function
ADGB
Active Differential Gearbox
Auxiliary Generator Line
Contactor
ANSA
At Nearest Suitable Airport
ADIRS
Air Data / Inertial Reference
System
AOA
Angle Of Attack
AICF
Anti Ice Control Function
BAM
Bleed Air Monitoring
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
LA
BAS
BATLC
BCM
BCR
BCS
BITE
Bleed Air System
Battery Line
Contactor
Backup Control
Module
BITE Contextual
Report
Braking Control
System
Built-In Test
Equipment
Training by Airbus
CIDS
Cabin Intercommunication
Data System
CLRNC
Clearance
CMD
Command
CMS
Central Maintenance System
Cabin Crew Rest
Compartment
CMV
Concentrator and Multiplexer
for Video
CSBSU
CCV
Coolant Control Valve
CMVS
Concentrator and Multiplexer
for Video System
CSDM
Cargo Smoke Detection
Module
CCW
Counter Clockwise
CNU
Cabin Network Unit
CT
Current Transformer
CDA
Continuous Descent
Approach
COAS
Cabin Operations
Applications System
CTB
Central Terminal Board
CTL
Control
COM
Communication
Compressor
CU
Control Unit
COMP
COMPT
Compartment
CVM
Cabin Video Monitoring
CP
Control Panel
CVR
Cockpit Voice Recorder
CPCS
Cabin Pressure Control
System
CVRS
Cockpit Voice Recorder
(CVR) System
CWS
Cabin Work Station
DA
Dipatch Advisory
DaFA
Data For Application
DAGS
Dry Air Generation System
BAS
Bleed Air System
CBV
Cross Bleed Valve
BATLC
Battery Line Contactor
CCD
Cursor Control Device
BCM
Backup Control Module
CCMAIL
Cabin Crew Mailing
BCR
BITE Contextual Report
CCOM
Cabin Crew Operating
Manual
BCS
Braking Control System
CCRC
BITE
Built - In Test Equipment
BOMU
Bleed and Overheat
Monitoring Unit
BPS
Backup Power Supply
BTAC
Bus Tie AC Contactor
BTCM
Brake Temperature
Compensation Module
BTDC
Bus Tie DC Contactor
BTSTRP
BTV
CDCV
Centralized Data
Acquisition Unit
Cargo Door Control Valve
Buttstrap
CDLS
Cockpit Door Locking
System
Brake to Vacate
CDM
Coolant Distribution Module
CaDoc
Cabin Documentation
Display
CAM
Cockpit Area Microphone
CAN
Controller Area Network
CAS
Calibrated Air Speed
CAX
Compartment Air Extraction
CB
Connection Box
CBP
Circuit Breaker Panel
CDAU
CDS
Control and Display System
CDSS
Cockpit Door Surveillance
System
CPDLC
Controller - Pilot DataLink
Communication
CELLI
Ceiling Emergency LED
Light
CPIOM
CFFC
Cockpit Fixed Frequency
Converter
CRDC
CFRP
Carbon Fiber Reinforced
Plastic
Core Processing Input /
Output Module
Common Remote Data
Concentrator
Communication
Communication Router
Module
CHAN
Channel
CRM
CSAS
CSBS
DATIS
DBTS
NOTE
Conditioned
Service Air
System
Controllable Sunlight
Blocking System
Controllable Sunlight
Blocking System Unit
Digital Automatic Terminal
Information System
Data Broadband
Transceiver System
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
DCL
Digital Cabin Logbook
DCL - CCT
Digital Cabin Logbook Cabin Configuration Tool
LA
Training by Airbus
DCL
Digital Cabin Logbook
EBAS
Engine Bleed Air System
DCL - CCT
Digital Cabin Logbook Cabin Configuration Tool
EBATC
Emergency Battery Contactor
Emergency Battery Line
Contactor
Electrical Backup Hydraulic
Actuator
DEFOG
Defogging
EBATLC
DEFRD
Deferred
EBHA
DELTA P
Differential Pressure
DET
DEU
Detector
Decoder / Encoder Unit
DEV
Deviation
DF
Definition File
DFDR
Digital Flight Data Recorder
DFPPU
Differential Feedback
Position Pick - Off Unit
Digital Global Positioning
System
DGPS
EFB
Electronic Flight Bag
EFCC
Emergency Flight Control
Contactor
EFF
Electronic Flight Folder
EFIS
Electronic Flight Instrument
System
EMEL
NOTE Emergency
Edge Mounted
Light
EMER
Emergency
ENEC
Emergency Normal to
Emergency Contactor
ENG
ENGine
EBTAC
Emergency Bus Tie AC
Contactor
EGCL
Emergency Generator Line
Contactor
EBTC
Emergency Bus Tie
Contactor
EGT
Exhaust Gas Temperature
Emergency Bus Tie DC
Contactor
Electronic Centralized
Aircraft Monitoring
EHA
Electro - Hydrostastic
Actuator
EHC
Electrical Heater Controller
EHSV
Electro Hydraulic Servo
Valve
EIF
Engine Interface Function
ELCO
Exterior Lights Controller
ELFDB
Emergency Light Floor
Disconnect Box
EPDS
EBTDC
ECAM
ECAS
Emergency Cabin Alerting
System
ECB
Electronic Control Box
ECP
ECAM Control Panel
ENMF
ENMU
ENRM
Ethernet Network Router
Module
EPCU
External Power Control Unit
EPDC
Electrical Power Distribution
Center
Electrical Power Distribution
System
Data Loading and
Configuration System
Distance Measuring
Equipment
ED
Engine Display
EDIU
Electrical Discrete Interface
Unit
ELM
Electrical Load
Management
EPGS
DSCS
Door and Slide Control
Sytem
EDMU
Electrical Distribution
Monitoring Unit
ELMF
Electrical Load
Managament Function
EPLC
DU
Display Unit
EEC
Engine Electronic Controller
ELPU
EENMF
Emergency Electrical
Network Managament
Function
ELT
Emergency Lightning
Protection Unit
Emergency Locator
Transmitter
EENMU
Emergency Electrical
Network Management Unit
DLCS
DME
DVI
Digital Visual Interface
DVR
Digital Video Recorder
EATULC
Emergency ATU Line
Contactor
EMCU
Electric Motor Control Unit
Electrical Network
Management Function
Electrical Network
Management Unit
DaFA
EPSU
Electrical Power Generation
System
External Power Line
Contactor
Data
For Application
EMergency
Power Supply
Unit
EPU
Emergency Power Unit
ESBF
Electrical System BITE
Function
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
LA
Training by Airbus
ESEC
ESMKTC
Emergency Smoke /
Evacuation Contactor
Emergency Smoke Tie
Contactor
ESN
Electrical Structure Network
ESPU
External Sources Protection
Unit
ESS
Engine Section Stator
ESTAC
ESTC
ETACS
ETLC
ETOPS
Emergency Static inverter
AC Contactor
Emergency STatic inverter
Contactor
External and Taxiing Aid
Camera System
Emergency TR Line
Contactor
Extensed Range
Twin-Engine Operations
FCU
Flight Control Unit
FOHE
Fuel / Oil Heat Exchanger
FCUb
Flight Control Unit Backup
FPF
Fire Protection Function
FD
Flight Director
FPMS
Floor-Path Marking System
FDB
Floor Disconnect Box
FPS
Fire Protection System
GPRS
FDBK
Feedback
FQMS
GPS
FDCE
Flight Deck and Cabin
Effects
Flight Data Interface
Function
Flight Data Recording
System
Fuel Quantity and
Management System
FSA-NG
FlySmart with Airbus-New
Generation
FDIF
FDRS
FWS
Flight Warning System
Flight Envelope
G/S
Glide Slope
FEDS
Fire Extinguishing Data
Converter
Front Secondary Structure
GAIN
GAlley INsert
GCU
Ground Cooling Unit
Fixed Frequency Supply
Unit
GFLI
Ground Fuel Level
Indication
Ground Fault Report
FFS
FFSU
Evacuation
EXLCO
EXterior Light Control
FG
Flight Guidance
FAP
Flight Attendant Panel
FGES
Flight Guidance and
Envelope System
FCC
Flight Control Contactor
FCDC
Flight Control Data
Concentrator
Flight Crew Rest
Compartment
Flight Control Remote
Module
FCRM
Flight Warning
FE
EVAC
FCRC
FW
FLS
FMS Landing System
FMA
Flight Mode Annunciator
FMC
Flight Management
Computer
Flight Management System
FMS
GFR
GPIRS
Global Positioning
NOTE and
Inertial Reference System
General Packet Radio
Service
Global Positioning System
GS
Ground Speed
GSP
Ground Service Panel
GUI
Graphical User Interface
HERTO
HES
High Energy Rejected
Takeoff
Head End Server
HEX
Hexagonal
HFDR
High Frequency Data Radio
HID
High Intensity Discharge
HMC
Hydraulic Monitoring and
Control
Hydraulic Monitoring and
Control Application
Hydraulic Monitoring and
Control Remote Function
HMCA
GLA
Glass Fiber Reinforced
Plastic
Gust Load Alleviation
GLC
Generator Line Contactor
HMCRF
GLS
GNSS Landing System
HMI
Human-Machine Interface
GND SVCE
CTL
Ground Service Control
HMU
Hydro Mechanical Unit
Global Navigation Satellite
System
HP
High Pressure
GNSS
GFRP
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
LA
Training by Airbus
HPSOV
High Pressure Shut-Off
Valve
IPCV
Intermediate Pressure
Check Valve
LLA
Lavatory Light Adapter
HUD
Head-Up Display
IPD
Illustrated Parts Data
LMES
Loss of Main Electrical
Supply
MFD
NOTEDisplay
MultiFunction
I/O
Input/Output
IPSM
Intelligent Power Supply
Module
Intermediate Pressure
Turbine Case Cooling
LMF
Local Maintenance Function
MFP
MultiFunction Probe
LOC
Localizer
MHM
Maintenance HMI Manager
LP
Low Pressure
MKR
Marker (radio) Beacon
Local Power Management
Function
Low Pressure Shut-Off
Valve
Low Pressure Turbine
Case Cooling
MLB
Maintenance LogBook
MLG
Main Landing Gear
MM
Maintenance Message
ICP
Integrated Control Panel
ICPS
Integrated Control Panel
System
IFE
In-Flight Entertainment
IPTCC
IR
Inertial Reference
IRP
Integrated Refuel Panel
LPMF
In-Flight Extertainment
Center
Inert Gas Generation
System
IRS
Inertial Reference System
ISIS
Integrated Standby
Instrument System
MMO
Maximum Operating Mach
IGN
Ignition
ISP
Integrated Static Probe
LPU
Lightning Protection Unit
MMR
Multi-Mode Receiver
IGSC
Inert Gas System Control
KCCU
LR
Long Range
MPV
Manifold Pressure Valve
ILS
Instrument Landing System
LRU
Line Replacable Unit
MSL
Maintenance System Load
IMACS
Information Management
Aircraft-ground
Communication System
Keyboard and Cursor
Control Unit
Local Area Network
LS
Loudspeaker
MVDR
Multiple VHF Data Radio
LSDS
Load Sensing Drive Strut
NBPT
No Break Power Transfer
LVDT
Linear Variable Differential
Transducer
NBR
Number
MAINT
Maintenance
NCU
Network Control Unit
MCA
Maintenance Central
Access
ND
Navigation Display
Manual Drive Unit
NLG
Nose Landing Gear
MDU
MEL
Minimum Equipment List
NMS
Noise Masking System
MES
Main Engine Start
NMU
Noise Masking Unit
IFEC
IGGS
IMCC
IND
INTPH
Information Management
Common Chassis
Indicator
Interphone
LAN
LAV
LDCC
Lavatory
Lower Deck Cargo
Compartment
LDG
Landing
LGCIS
Landing Gear Control
Indication System
Landing Gear Extension
and Retraction System
Landing Gear Monitoring
System
IP
Intermediate Pressure
LGERS
IPC
Intermediate Pressure
Compressor
LGMS
LPSOV
LPTCC
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
NSM Network Server Module
NTPH
Interphone NVM Non-Volatile Memory
NWS
Nose Wheel Steering OAT Outside Air Temperature
OBS
Observation OC Oceanic Clearance
OCED
Operator-Customized ECAM Database ODMS Oil Debris Monitoring System
OFW
Outer False Work OHDC Overhead Detection Card
OHDS
Over Heat
LA
Training by Airbus
NSM
Network Server Module
NTPH
Interphone
NVM
Non-Volatile Memory
NWS
Nose Wheel Steering
OAT
Outside Air Temperature
OBS
Observation
OC
Oceanic Clearance
OSFC
OTSSU
Open world Server Function
Cabinet
Outboard Transmission
Speed Sensor Unit
OXY
Oxygen
P/C
Premium Class
PA
Passenger Address
PERF
Performance
PFCS
Primary Flight Control
System
PSU
NOTE
Passenger
Service Unit
PFD
Primary Flight Display
Pt
Total Pressure
PFDB
Power Floor Disconnect Box
PTT
Push-to-Talk
PIESD
Passenger Information and
Entertainment Services
Domain
PVR
PAX
Passenger
Operator-Customized
ECAM Database
Oil Debris Monitoring
System
PBD
Place Bearing / Distance
PLC
Powerline Communication
PCS
Propulsion Control System
PLSP
PCU
Passenger Control Unit
PMAT
OFW
Outer False Work
PDB
Performance Database
Point Level Sensor
Processor
Portable Multipurpose
Access Terminal
OHDC
Overhead Detection Card
PDLS
Privacy Door Lock System
OCED
ODMS
OHDS
OHSC
OMT
OPSOV
OPU
OSCM
OSF
Over Heat Detection
System
Overhead Stowage
Compartment
Onboard Maintenance
Terminal
Over Pressure Shut-Off
Valve
Overvoltage Protection Unit
PDMI
PDMIC
PDMMF
PDOS
Power Distribution
Maintenance Interface
Power Distribution
Maintenance Interface
Contactor
Power Distribution
Monitoring and Maintenance
Function
Power Door Opening
System
PNL
Panel
PNTL
Pintle
Passenger Owned Devices
Domain
PODD
POR
Point Of Regulation
PRESS
Pressurization
PRIM
PRIMary Computer
PRV
Pressure Regulating Valve
Ps
Static Pressure
Oxygen System Control and
Monitoring
PDT
Probe Dual Temperature
PSA
Passenger Service Adapter
Open world Server Function
PDU
Power Drive Unit
PSC
Passenger Supply Channel
PWIP
PWS
PWSP
QFRP
Point of Voltage Reference
Potable Water Indication
Panel
Potable Water System
Potable Water Service
Panel
Quartz Fiber Reinforced
Plastic
RA
Radio Altimeter
RAD
RADio
RAI
Ram Air Inlet
Radio and Audio Integrating
Management System
RAIMS
RAT
Ram Air Turbine
RB
Resource BITE
RBCU
Remote Braking Control
Unit
RCC
Remote Control Center
RCCB
Remote Control Circuit
Breaker
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
LA
Training by Airbus
RCS
REIC
Radio Communication
System
Reconfigurable ETOPS
Isolation Contactor
SB
Service Bulletin
SGSC
SCI
Secure Communication
Interface
Sheddable Ground Servicing
Contactor
SIC
System Isolation Contactor
TAC
Taxiing NOTE
Aid Camera
SCM
SDU Configuration Module
SLC
Starter Line Contactor
TACS
Taxiing Aid Camera System
SCS
Supplemental Cooling
System
SLS
Slide Lever Switch
TAT
Total Air Temperature
SMK
SD
Smoke
System Display
TAWS
SDF
Smoke Detection Function
SMM
System Management
Module
Terrain Awareness and
Warning System
TCA
Throttle Control Angle
TCAS
Traffic Alert and Collision
Avoidance System
TCC
Turbine Case Cooling
TCPS
Temperature Compensated
Pressure Switch
TEFO
Total Engine Flame Out
TELECOM
Telecommunications
REP
Repository
RF
Radio Frequency
Rate Gyro and
Accelerometer Unit
Radio and Audio
Management Panel
Runway end Overrun
Protection
SDM
RSA
Remote Server Acquisition
RT
RGAU
RMP
Simple Data Loader
SOC
Status Of Charge
Smart Diode Module
SPB
Seat Power Box
SDS
Smoke Detection System
SPDB
Real-Time
SDU
Seat Display Unit
RTNC
Refuel and Towing on
Normal Contactor
SEB
Seat Electronic Box
Secondary Power
Distribution Box
SPP Broadcasting
Application
RTU
Radar Transceiver Unit
S/D
System Display
S/W
Software
SA
Single Aisle
SFCC
SACU
Semi-Automatic Control Unit
SFLM
SAOHE
Surface Air / Oil Heat
Exchanger
SFLMD
ROP
SAR
Smart Access Recorder
SATCOM
Satellite Communication
SDL
SEC
SEL
SELCAL
SG
SGCU
SECondary Computer
Selector
Selective Calling
System Slat Flap Control
Computer
Slats / Flaps / Limitations /
Memos
Slat / Flap / Limitation /
Memo Display
Starter Generator
Starter Generator Control
Unit
SPP-BA
SPS
Seat Power Supply
SPSF
Seat Power Supply Function
TEMP
Temperature
SPU
Starter Power Unit
TGCU
Terminal GPRS / UMTS
Client Unit
SRI
aircraft Structural Repair
Identification
TGT
Turbine Gas Temperature
SRPU
Safe Redundant Power Unit
THS
SSA
Side Slip Angle
Trimmable Horizontal
Stabilizer
SSFDR
Solid State Flight Data
Recorder
SSPC
SV
TIU
Terminal Interface Unit
TIV
Temperature Isolation Valve
Solid State Power Controller
TLA
Throttle Level Angle
Servovalve
TLB
Technical LogBook
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
LA
Training by Airbus
TLC
TM
TMLB
TPA
TR
TRA
TRANSLG
TR Line Contactor
Torque Motor
Technical and Maintenance
LogBook
Throttle Potentiometer
Angle
Radio and Audio
Management Panel
Translating
Real-Time
TSM
Trouble Shooting Manual
TWDC
TWLU
Torque Sensor Unit
Tank Wall Data
Concentrator
Terminal Wireless Local
Area Network (LAN) Unit
ULA
Universal Light Adapter
ULA M
Universal Light Adapter
Module
Universal Mobile
Telecommunications
System
Vapor Cycle Refrigeration
Unit
UMTS
VCRU
VCS
VHF Data Radio
WLU
VFG
Variable Frequency
Generator
WMEL
VGA
Video Graphics Array
WOW
Weight On Wheels
VGM
Versatile Graphical Module
WRDC
Wheel Remote Data
Concentrator
VIGV
Variable Inlet Guide Vane
WS
Wireless System
VMO
Maximum Operating Speed
WSCS
VNAV
Vertical Navigation
Wheel Steering Control
System
Virtual Quick Access
Recorder
WXR
Weather Radar
VQAR
XCVR
Transceiver
VSV
Variable Stator Vane
XPDR
Transponder
WACS
Wireless Airport
Communication System
X-TALK
Cross-talk
WADU
Weather Antenna Drive Unit
WAP
Wireless Access Point
WBBC
Weight and Balance Backup
Computation
Throttle Rhestart Angle
TSA
TSU
VDR
Ventilation Control System
WD
Warning Display
WHC
Window Heat Computer
WIP
Wing Ice Protection
WIPS
Wing Ice Protection System
WLI
Water Level Indicator
WLM
Wireless LAN Manager
Wireless LAN Unit
Wall Mounted Emergency
Light
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
LA
SYMBOLS CARD
DESIGN RULES
DESIGNATION
SYMBOL
AIR FLUIDS - GENERAL
SYMBOL
DESIGNATION
SYMBOL
DESIGNATION
NOTE
NORMAL PIPE
HOT AIR
28 VDC
SMALL PIPE
RECIRCULATED/AMBIANT AIR
115 VAC
SUCTION
REGULATED AIR
230 VAC
RETURN/DEPRESSURIZATION
COLD AIR
AIR FLUIDS - ATA 21
REGULATED PRESSURE
GEARCASE VENT
SYMBOL
DESIGNATION
CONNECTION TYPE
DESIGNATION
SYMBOL
SCAVENGE CASE DRAIN
HOT AIR 200°C (392°F)
FUNCTIONAL
MECHANICAL LINK
PACK COMP. ENTRY
DIGITAL
COOL AIR 15°C (59°F)
DISCRETE
FREEZING 0°C (32°F) or below
ANALOG
RAM AIR -30°C (-22°F)
AFDX BUS
WATER / WASTE FLUIDS
SYMBOL
DESIGNATION
POTABLE WATER
LAVATORY WATER
WASTE WATER
HYDRAULIC FLUIDS
SYMBOL
GREEN SUPPLY
YELLOW SUPPLY
OTHER FLUIDS
SYMBOL
LOW PRESSURE (LP)
ALTERNATE EXTENSION FOR ATA32
DESIGNATION
OIL FLUIDS
FUEL
FUEL HIGHLIGHT
DESIGNATION
SYMBOL
DESIGNATION
Training by Airbus
ELECTRICAL POWER SUPPLY
ETHERNET BUS
CAN BUS
TCSB BUS
1553 BUS
ARINC BUS
RS BUS
OPTICAL FIBER
COAXIAL
O2
ENGINE OIL
AFDX NETWORK
N2 / RAIN REPELLENT
VFG OIL
RADIO SIGNAL
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
SC
LA
SYMBOLS CARD
Training by Airbus
BOXES REPRESENTATION
INSIDE ATA CHAPTER
MECHANICAL
ELECTRONIC
COMPONENT
SYSTEM
/ FUNCTION
NOTE
SUB-SYSTEM
/ SUB-FUNCTION
APPLICATION
DATABASE
SUB-SYSTEM
/ SUB-FUNCTION
APPLICATION
DATABASE
OUTSIDE ATA CHAPTER
MECHANICAL
ELECTRONIC
COMPONENT
SYSTEM
/ FUNCTION
MAINTENANCE ADVICES
SYMBOL
DESIGNATION
SYMBOL
MISCELLANEOUS
DESIGNATION
MENTIONS
THE
RISKS
RISK TO THE
MAINTENANCE
TECHNICIAN HIMSELF
MENTIONS
THE
RISKS
REMOTE RISK TO
A COLLEAGUE
MENTIONS
THE
RISKS
RISK TO
THE AIRCRAFT
REMOVAL /
INSTALLATION
TOOL
SPECIFIC TOOL
SYMBOL
DESIGNATION
OPTION
MENTION THE
ENVIRONMENTAL
PRECAUTIONS
ENVIRONMENTAL
PRECAUTIONS
© Airbus SAS 2019. All rights reserved. Confidential and proprietary document.
SC
LA
AIRBUS S.A.S.
31707 BLAGNAC cedex. FRANCE
ST
REFERENCE V6D15311
DECEMBER 2019
PRINTED IN FRANCE
AIRBUS S.A.S 2019
ALL RIGHTS RESERVED