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    Guia CB Computer Reset Airbus

    Uploaded by

    Fabian Andres Soto Lineros (LATAM)
    This document provides an overview of the ATA 100 breakdown, which is an industry standard for aircraft maintenance manuals. It lists various aircraft systems and components categorized by their ATA chapter code. These include air conditioning, auto flight, communications, electrical power, equipment, fire protection, flight controls, fuel systems, hydraulic power, lighting, navigation, oxygen, pneumatics, and engines. The document serves as a reference guide for technicians to locate relevant maintenance information according to aircraft system or component.

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    © All Rights Reserved
    Download as PDF, TXT or read online from Scribd

    Guia CB Computer Reset Airbus

    Uploaded by

    Fabian Andres Soto Lineros (LATAM)
    472 views20 pages
    This document provides an overview of the ATA 100 breakdown, which is an industry standard for aircraft maintenance manuals. It lists various aircraft systems and components categorized by their ATA chapter code. These include air conditioning, auto flight, communications, electrical power, equipment, fire protection, flight controls, fuel systems, hydraulic power, lighting, navigation, oxygen, pneumatics, and engines. The document serves as a reference guide for technicians to locate relevant maintenance information according to aircraft system or component.

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    Guia__CB__Computer_Reset__Airbus

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    This document provides an overview of the ATA 100 breakdown, which is an industry standard for aircraft maintenance manuals. It lists various aircraft systems and components categorized by their ATA chapter code. These include air conditioning, auto flight, communications, electrical power, equipment, fire protection, flight controls, fuel systems, hydraulic power, lighting, navigation, oxygen, pneumatics, and engines. The document serves as a reference guide for technicians to locate relevant maintenance information according to aircraft system or component.

    Copyright:

    © All Rights Reserved
    Download as PDF, TXT or read online from Scribd
    Download as pdf or txt
    472 views20 pages

    Guia CB Computer Reset Airbus

    Uploaded by

    Fabian Andres Soto Lineros (LATAM)
    This document provides an overview of the ATA 100 breakdown, which is an industry standard for aircraft maintenance manuals. It lists various aircraft systems and components categorized by their ATA chapter code. These include air conditioning, auto flight, communications, electrical power, equipment, fire protection, flight controls, fuel systems, hydraulic power, lighting, navigation, oxygen, pneumatics, and engines. The document serves as a reference guide for technicians to locate relevant maintenance information according to aircraft system or component.

    Copyright:

    © All Rights Reserved
    Download as PDF, TXT or read online from Scribd
    Download as pdf or txt
    of 20

    ATA 100 BREAKDOWN

    12 SERVICING
    20 STANDARD PRACTICES - AIRFRAME
    21 AIR CONDITIONING
    22 AUTO FLIGHT
    23 COMMUNICATIONS
    24 ELECTRICAL POWER
    25 EQUIPMENT/FURNISHING
    26 FIRE PROTECTION
    27 FLIGHT CONTROLS
    28 FUEL
    AIRBUS 318/319/320 29
    30
    HYDRAULIC POWER
    ICE AND RAIN PROTECTION
    31 INDICATING/RECORDING SYSTEM
    32 LANDING GEAR
    33 LIGHTS
    - ATA 100 Pag 01 34 NAVIGATION
    - ABREVIATIONS Pag 02 35 OXYGEN
    36 PNEUMATICS
    - CIRCUIT BREAKERS LIST Pag 10 38 WATER/WASTE
    - COMPUTER RESET Pag 28 46 INFORMATION SYSTEM
    49 AIRBORNE AUXILIARY POWER
    - MESSAGE CLASSIFICATION Pag 38 52 DOORS
    - FAULTS Pag 39 56 WINDOWS
    70 STANDARD PRACTICES - ENGINE
    71 POWER PLANT
    72 ENGINE
    73 ENGINE FUEL AND CONTROL
    74 ENGINE IGNITION
    75 ENGINE AIR
    76 ENGINE CONTROLS
    77 ENGINE INDICATING
    78 EXHAUST
    79 OIL
    80 STARTING

    BASE MNT FLORIANÓPOLIS


    REV : 2011 01

    ADS Air Data System FACS Flight Augmentation Computer System


    ADU Align Display Unit FADEC Full Authority Digital Engine Control
    AEU Audio Electronic Unit FAP Flight Attendant Panel
    AEVC Avionics Equipment Ventilation Computer FAP Forward Attendant Panel
    AFCS Automatic Flight Control System FAS Flight Augmentation System
    AFECU Automatic Fire Extinguishing Control Unit FCC Flight Control Computer
    AFMC Auxiliary Fuel Management Computer FCDC Flight Control Data Concentrator
    AFS Automatic Flight System FCCS Flight Control Computer System
    AFU Artificial Feel Unit FCMC Fuel Control and Monitoring Computer
    AGB Accessory Gearbox FCMS Fuel Control Monitoring System
    AHRS Attitude and Heading Reference System FCPC Flight Control Primary Computer
    AHRU Attitude and Heading Reference Unit FCPI Flight Control Position Indicator
    AI Anti-Icing FCSC Flight Control Secondary Computer
    A-ICE Anti-Ice FCU Flight Control Unit
    AICU Anti Ice Control Unit FCU Fuel Control Unit
    AIDS Aircraft Integrated Data System FCU Flush Control Unit
    AM Amplitude Modulation FCV Flow Control Valve
    AMU Audio Management Unit FD Flight Director
    ANU Aircraft Nose Up FDAU Flight Data Acquisition Unit
    AOA Angle Of Attack FDR Flight Data Recorder
    AOG Aircraft On Ground FDU Fire Detection Unit
    AOHX Air/Oil Heat Exchanger FES Fire Extinguishing System
    AP Autopilot FF Fuel Flow
    AP/FD Autopilot/Flight Director FFCM Free Fall Control Module
    APU Auxiliary Power Unit FIN Functional Item Number
    ARU Audio Reproducer Unit FLC Feel and Limitation Computer
    AS Airspeed FLP Flap
    AT Autothrust FLSA Fuel Level Sensing Amplifier
    AT Autothrottle FLSCU Fuel Level Sensing Control Unit
    ATIS Automatic Terminal Information Service FM Frequency Modulation
    ATSU Air Traffic Service Unit FMC Flight Management Computer
    AVIONICS Aviation Electronics FMCS Flight Management Computer System
    BCN Beacon FMCU Flight Management Computer Unit
    BCU Brake Control Unit FME Flow Metering Equipment
    BITE Built-in Test Equipment FMGC Flight Management and Guidance Computer
    BLV Bleed Valve FMGEC Flight Management Guidance and Envelope Computer
    BSCU Braking/Steering Control Unit FMS Flight Management System
    03
    05
    ABBREVIATIONS
    A.ICE Anti-ice
    A.ICE Anti-icing
    A/BRK Autobrake
    A/C Aircraft
    A/COLL Anti-Collision
    A/D Analog/Digital
    A/DC Analog-to-Digital Converter
    A/F Auto Flight
    A/G Air to Ground
    A/SKID Anti-Skid
    A/STAB Auto Stabilizer
    A/T Adjustment/Test
    A/THR Autothrust
    AADC Analog Air Data Computer
    ABCM Alternate Brake Control Manifold
    ABCU Alternate Braking Control Unit
    ABS Autobrake System
    ACARS Aircraft Communication Addressing and Reporting System
    ACAS Airborne Collision Avoidance System
    ACCU Accumulator
    ACM Air Cycle Machine
    ACM Abbreviated Component Maintenance Manual
    ACOC Air Cooled Oil Cooler
    ACP Audio Control Panel
    ACSC Air Conditioning System Controller
    ACU Air Cooling Unit
    ACU Antenna Coupler Unit
    ADAU Auxiliary Data Acquisition Unit
    ADC Air Data Computer
    ADF Automatic Direction Finder
    ADG Air Driven Generator
    ADI Attitude Director Indicator
    ADIRS Air Data/Inertial Reference System
    ADIRU Air Data/Inertial Reference Unit
    ADL Aircraft Data Loader
    ADM Air Data Module
    02

    FMS Fuel Manifold Staging BTMU Brake Temperature Monitoring Unit


    FMU Fuel Metering Unit BTS Brake Temperature Sensor
    FMV Fuel Metering Valve CDAU Centralized Data Acquisition Unit
    FNCP Flight Navigation Control Panel CDU Control and Display Unit
    FNSG Flight Navigation Symbol Generator CIDS Centralized Fault Display System
    FOC Fuel/Oil Cooler CMC Central Maintenance Computer
    FPA Flight Path Angle CPC Cabin Pressure Controller
    FPMU Fuel Properties Measurement Unit CPCU Cabin Pressure Control Unit
    FPPU Feedback Position Pick-off Unit CPMU Cabin Passenger Management Unit
    FPS Fire Protection System CVR Cockpit Voice Recorder
    FQIC Fuel Quantity Indication Computer CWS Control Wheel Steering
    FQMS Fuel Quantity and Management System DADC Digital Air Data Computer
    FSOV Fire ShutOff Valve DAU Data Acquisition Unit
    FTMS Flight Test Management System DCP Display Control Panel
    FTU Force Transducer Unit DFDAU Digital Flight Data Acquisition Unit
    FU Feedback Unit DFDR Digital Flight Data Recorder
    FWC Flight Warning Computer DMU Data Management Unit
    FWS Flight Warning System DRMI Distance Radio Magnetic Indicator
    FWSD Flight Warning and System Display DU Display Unit
    G/S Glide Slope EADI Electronic Attitude Director Indicator
    GAPCU Ground Auxiliary Power Control Unit EBCU Emergency Brake Control Unit
    GNSS Global Navigation Satellite System ECAM Electronic Centralized Aircraft Monitoring
    GPCU Ground Power Control Unit ECS Environmental Control System
    GPIRS Global Positioning and Inertial Reference System ECU Electronic Control Unit
    GPS Global Positioning System EDP Engine Driven Pump
    GPSSU Global Positioning System Sensor Unit EFIS Electronic Flight Instrument System
    GPU Ground Power Unit EHSI Electronic Horizontal Situation Indicator
    GPWC Ground Proximity Warning Computer EIU Engine Interface Unit
    GPWS Ground Proximity Warning System ELAC Elevator Aileron Computer
    HADC Hybrid Air Data Computer ELT Emergency Locator Transmitter
    HCU Hydraulic Control Unit EMU Engine Monitoring Unit
    HDG Heading EMU Engine Maintenance Unit
    HPC High Pressure Compressor EPU Emergency Power Unit
    HPT High Pressure Turbine EVAC Engine Vibration Monitoring Unit
    HPV HP Bleed Valve EVMU Engine Vibration Monitoring Unit
    HPV High Pressure Valve F/CTL Flight Controls
    HSI Horizontal Situation Indicator FAC Flight Augmentation Computer
    06 04
    HSI Hot Section Inspection T2CAS Traffic and Terrain Collision Avoidance System
    HSMU Hydraulic System Monitoring Unit TAS True Airspeed
    IDG Integrated Drive Generator TAT Total Air Temperature
    IFES In-Flight Entertainment System TCAS Traffic Alert and Collision Avoidance System
    IFF Identification Friend Foe TCU Throttle Control Unit
    IFR Instrument Flight Rules THS Trimmable Horizontal Stabilizer
    IGV Inlet Guide Vane TIT Turbine Inlet Temperature
    INS Inertial Navigation System TLA Throttle Lever Angle
    INU Inertial Navigation Unit TOGA Takeoff/Go Around
    IPCU Ice Protection Control Unit TRP Thrust Rating Panel
    IPDU Ice Protection Data Unit UHF Ultra High Frequency
    IRAN Inspection and Repair As Necessary VSC Vacuum System Controller
    IRS Inertial Reference System WAI Wing Anti-Ice
    IRU Inertial Reference Unit WARN Warning
    L/G Landing Gear WG Wave Guide
    LGCIU Landing Gear Control and Interface Unit WGDC Windshield Guidance Display Computer
    LGMS Landing Gear Management System WGDS Windshield Guidance Display System
    LOC Localizer WHC Window Heat Computer
    LPC Low Pressure Compressor WIPCU Water Ice Protection Control Unit
    LPT Low Pressure Turbine WIPDU Water Ice Protection Data Unit
    LRU Line Replaceable Unit WOW Weight On Wheels
    LVDT Linear Variable Differential Transducer WPT Waypoint
    MCDU Multipurpose Control & Display Unit WR Weather Radar
    MCPU Motor Control and Protection Unit WSHLD Windshield
    MLG Main Landing Gear WXR Weather Radar
    MLW Maximum Landing Weight X BLEED Crossbleed
    MMR Multi Mode Receiver X FEED Crossfeed
    MTOW Maximum Takeoff Weight XCVR Transceiver
    MTP Maintenance and Test Panel XMTR Transmitter
    MWC Master Warning Computer ZFW Zero Fuel Weight
    MZFW Maximum Zero Fuel Weight α Angle-of-Attack
    N1 Engine Fan Speed Θ Pitch Attitude
    N2 High Pressure Rotor Speed ∆P Differential Pressure
    NLG Nose Landing Gear
    OCM Outflow Valve Control Module
    OPV Overpressure Valve
    P/B Pushbutton
    07 09

    (2) AUTO FLIGHT system (4) ELECTRICAL POWER system


    ON A/C ALL
    121VU AUTO FLT/FCU/2 9CA2 M21
    105VU ELEC/STAT INV/BUS 901XP/SPLY 12XB H02
    121VU AUTO FLT/RUDDER/TRIM/IND 15CC M20
    105VU ELEC/BAT BUS/REF/BCL2 8PB2 J02
    121VU AUTO FLT/FAC2/28VDC 5CC2 M19
    106VU AC ESS BUS/STBY/CNTOR/CTL 5XC B08
    121VU AUTO FLT/FAC2/26VAC 14CC2 M18
    106VU AC ESS BUS/EMER/CNTOR/CTL 5XE B07
    121VU AUTO FLT/FMGC/2 10CA2 M17
    106VU 26VAC/ESS BUS/SPLY 4XH B06
    121VU AUTO FLT/MCDU/2 11CA2 N20
    106VU CSM/G /EV/MAN/SPLY 6XE B04
    121VU AUTO FLT/RUDDER/ARTF/FEEL 14CA N17
    106VU AC ESS/BUS NORM/CNTOR/CTL 4XC B03
    121VU AUTO FLT/STICK/LOCK 13CA N16
    106VU AC ESS/BUS/EMER/CNTOR/SPLY 15PC C08
    106VU EMER/SHED/CNTOR/SPLY 1PH C07
    (3) COMMUNICATION system 106VU AC ESS BUS/EMER/STBY/CNTOR/SPLY 10XE C06
    TBD 5TT 106VU AC ESS BUS/MONG/SPLY 2XH C05
    ON A/C 001-016, 101-102, 201-252 106VU AC/SHED/ESS BUS/CNTOR/CTL 1XH C04
    49VU COM/CVR/SPLY 2RK E14 106VU ESS TR/CNTOR/CTL 5PE C02
    49VU COM/CVR/CTL 4RK E13 106VU ESS TR/SPLY 4PE C01
    ON A/C ALL ON A/C 014-014, 016-100, 203-300
    49VU COM/RMP/1 2RG1 G10 106VU 802PP SPLY 10PH B09
    49VU COM/VHF/1 2RC1 G09
    49VU INT 1 + 2 9RN G08 ON A/C ALL
    49VU ACP F/O BITE INT 2 AUDIO 3/5 OCCPNT 5RN G07 122VU ELEC/GALLEY/CNTOR 7MC S28
    49VU ACP CAPT SELCAL INT 1 AUDIO AVNCS 4RN G06 122VU ELEC/REFLNG/NORM 2PR S27
    49VU COM/CIDS/DEU B/ESS 153RH G03 122VU ELEC/GALY & CAB/CTL 1XA S26
    49VU COM/CIDS/DIR ESS/2 157RH G02 122VU ELEC/GALY & CAB/FAULT/LT CTL 8XA S25
    49VU COM/CIDS/DIR ESS/1 150RH G01 122VU ELEC/GALY & CAB/GND/FLT/LOGIC 7XA S24
    49VU COM/CIDS/FLT ATTND PNL/ESS 171RH H01 122VU ELEC/GEN2/OFF/BTC2 SPLY 8XU T31
    49VU COM HF1 1RE1 HA14 122VU ELEC/GEN1/OFF/BTC2 SPLY 14XU T30
    49VU COM/CIDS/DEU A ESS/AFT R 172RH HA12 122VU ELEC/GEN2/OFF/BTC1 SPLY 15XU T29
    49VU COM/CIDS/DEU A ESS/AFT L 179RH HA11 122VU ELEC/GEN1/OFF/BTC1 SPLY 5XU T28
    49VU COM/CIDS/DEU A ESS/FWD R 158RH HA10 122VU ELEC/GCU/2 2XU2 T27
    49VU COM/CIDS/DEU A ESS/FWD L 159RH HA09 122VU ELEC/GCU/1 2XU1 T26
    121VU AUDIO MIXING 14WW K03 122VU ELEC/IDG2/DISC 2XT T25
    121VU COM NAV/HF2 1RE2 L13 122VU ELEC/IDG1/DISC 1XT T24
    121VU COM NAV/VHF/3 2RC3 L05 122VU ELEC/DC SVCE/BUS/ON TR2 5PX U30
    121VU COM NAV/VHF/2 2RC2 L04 122VU ELEC/RFL/SPLY/LOGIC 4PR U29
    121VU COM NAV/RMP/3 2RG3 L03 122VU ELEC/REFLNG/ON/BAT 1PR U28
    121VU COM NAV/RMP/2 2RG2 L02 122VU ELEC/DC SHED BUS/CNTR 9PN U26
    11 13
    (1) AIR CONDITIONNING system PA Passenger Address
    PANEL DESIGNATION IDENT. LOC PAS Pitch Attitude Sensor
    49VU AIR COND/FWD CARGO/VENT/CTL & MONG 2HN C08 PBE Protective Breathing Equipment
    49VU AIR COND/AFT CARGO/VENT/CTL & MONG 31HN C07 PC Pack Controller
    49VU AIR COND/RAM/AIR/INLET 1HZ D10 PCU Power Control Unit
    49VU AIR COND/CAB/PRESS/CTL1 1HL D09 PFD Primary Flight Display
    49VU AIR COND/TEMP CTL/SYS 1 CHAN B/28VDC 52HH D08 PFTU Pedal Feel and Trim Unit
    49VU AIR COND/TEMP/CTL/IND 58HH D07 PHC Probe Heat Computer
    49VU AIR COND/AVNCS VENT/CTL 6HQ D06 PIM Programming and Indication Module
    49VU AIR COND/AVNCS VENT/CTL 5HQ D05 PIN Personal Identification Number
    122VU FWD CARGO VENT/FAN 1HN T22 PMA Permanent Magnet Alternator
    122VU AIR C/LAV/GALLEY VENT CTL/EXTRACT FAN/CTL 5HU U21 PMU Power Management Unit
    122VU AIR C/LAV/GALLEY VENT CTL/EXTRACT FAN/SPLY 6HU U19 PRAM Prerecorded Announcement and Music
    122VU AIR COND/TEMP CTL SYS 2/CHAN A/115VAC 53HH W22 PSU Passenger Service Unit
    122VU AIR COND/TEMP CTL SYS 2/CHAN A/28VDC 55HH W21 PTU Power Transformer Unit
    122VU AIR COND/RECIRC FAN/R/CTL 11HG W20 PWCU Potable Water Control Unit
    122VU AIR COND/RECIRC FAN/R/SPLY 3HG W18 QRH Quick Reference Handbook
    122VU RPCU 4HL X23 RA Radio Altimeter
    122VU AIR COND/TEMP CTL SYS 1/CHAN A/115VAC 49HH X22 RACON Radar Beacon
    122VU AIR COND/TEMP CTL SYS 1/CHAN A/28VDC 51HH X21 RAT Ram Air Turbine
    122VU AIR COND/RECIRC FAN/L/CTL 2HG X20 RAT Ram Air Temperature
    122VU AIR COND/RECIRC FAN/L/SPLY 1HG X18 RCVR Receiver
    122VU AIR COND/CAB PRESS/CTL/MAN 3HL Y23 RDDMI Radio Dual Distance Magnetic Indicator
    122VU AIR COND/CAB PRESS/CTL/2 2HL Y22 RFU Radio Frequency Unit
    122VU AIR COND/TEMP CTL SYS 2/CHAN B/28VDC 56HH Y21 RMI Radio Magnetic Indicator
    122VU AIR COND/TEMP CTL SYS 2/CHAN B/115VAC 54HH Y20 RMP Radio and Audio Management Panel
    122VU AIR COND/TEMP CTL SYS 1/CHAN B/115VAC 50HH Y18 RMP Radio Management Panel
    122VU AIR COND/AVNCS/VENT/MONG 3HQ Y17 RMU Radio Management Unit
    123VU AVNCS VENT/BLOWER/FAN 1HQ AD10 SAT Static Air Temperature
    123VU AVNCS VENT/EXTC/FAN 2HQ AE02 SAV Starter Air Valve
    SDCU Smoke Detection Control Unit
    (2) AUTO FLIGHT system SEC Spoiler Elevator Computer
    SFCC Slat Flap Control Computer
    49VU AUTO FLT/FCU/1 9CA1 B05
    SFPI Slats/Flaps Position Indicator
    49VU AUTO FLT/FAC1/28VDC 5CC1 B04
    SGU Symbol Generator Unit
    49VU AUTO FLT/FAC1/26VAC 14CC1 B03
    SHF Super High Frequency
    49VU AUTO FLT/FMGC/1 10CA1 B02
    SOV Shut-off Valve
    49VU AUTO FLT/MCDU/1 11CA1 B01
    10 08

    (4) ELECTRICAL POWER system (3) COMMUNICATION system


    ON A/C ALL ON A/C ALL
    122VU ELEC/AC SHED BUS/CNTOR 26XN U25 121VU COM NAV/CIDS/DEU A NORM/R AFT 168RH M12
    122VU ELEC/CNTOR/DC BUS/TIE 1/FAULT 14PC U24 121VU COM NAV/CIDS/DEU A NORM/L AFT 167RH M11
    122VU ELEC/AC PWR/SVCE/CTL 3XX V29 121VU COM NAV/CIDS/DEU A NORM/R FWD 164RH M10
    122VU ELEC/COML/SHED/SYS2 8XN V28 121VU COM NAV/CIDS/DEU A NORM/L FWD 163RH M09
    122VU ELEC/BUS/2XP/CTL 17XN2 V27 121VU COM NAV/CIDS/DEU B/NORM 162RH M08
    122VU ELEC/COML/SHED/SYS1 9XN V26 121VU COM NAV/CIDS/DIR NORM/2 156RH M06
    122VU ELEC/AC/BUS1/CTL 17XN1 V25 121VU COM NAV/CIDS/DIR NORM/1 151RH M05
    122VU ESS NTWK AUTO ALTN 6XC V24 121VU COM NAV/SELCAL 8RN M04
    122VU ELEC/DC BUS/TIE2//APU/START 18PC W31 121VU COM NAV/ACP/THIRD/OCCPNT 6RN M02
    122VU ELEC/TR2/FAULT/DC BUS TIE/CONFIG 7PC2 W30 121VU EIS/HORN/SPLY 2WC P09
    122VU ELEC/TR1/FAULT/DC BUS TIE/CONFIG 7PC1 W29 121VU COM/FAP1/NORM 170RH Q14
    122VU ELEC/CNTOR/ESS/DC BUS/TIE 3PC W26 122VU DOORS/CKPT/VIDEO/SPLY 5RA T16
    122VU ELEC/CNTOR/DC/BUS/TIE1 9PC W25
    ON A/C 002-100, 201-300
    122VU ELEC/GAPCU 17XG W24
    2000VU IFE/SEAT-POWER-PAX SYS 20MK C07
    122VU ELEC/EXT PWR/LT CLT/AVAIL 4XG X31
    2000VU IFE-CABIN-ADB2 24MK C06
    122VU ELEC/EXT PWR/LT CLT/NOT IN/USE 6XG X30
    2000VU IFE-CABIN-ADB1 23MK C05
    122VU ELEC/EXT PWR/CTL 11XG X29
    2000VU IFE-IFE CENTER-AC-IFEC 22MK C04
    122VU ELEC/TR2/MONG 3PU2 X26
    2000VU IFE-IFE CENTER-DC-VCC 20MH C01
    122VU ELEC/TR1/MONG 3PU1 X25
    122VU ELEC/DC/SVCE/BUS 5PN X24 ON A/C 201-300
    122VU ELEC/EMER GEN AUTO/2 9XE Z26 2000VU IFE-IFE CENTER-DC-IFEC 21MK C03
    122VU ELEC/EMER GEN AUTO/1 11XE Z25
    123VU APU GEN/EGIU2/115VAC 23XS AA08 (4) ELECTRICAL POWER system
    123VU SVCE/BUS 2/214XP SPLY 4XX AA05 ON A/C ALL
    123VU BUS 1/131XP-A/SPLY 5XN1 AB12 49VU ELEC/AC BUS/8XP/MONG 6XH H11
    123VU BUS 1/103XP/SPLY 3XN1 AB11 49VU ELEC/LT/CTL 13XG H10
    123VU TR1/SPLY 2PU1 AB10 105VU ELEC/CSM/G /EV AUTO/SPLY 7XE C01
    123VU TR2/SVCE/BUS 2/SPLY 1XX AB08 105VU ELEC/HOT BUS/702PP SPLY 5PB2 D02
    123VU GND/PWR/PROT 2XG AB07 105VU ELEC/HOT BUS/701PP SPLY 5PB1 D01
    123VU SVCE/BUS 2/212XP SPLY 2XX AB05 105VU ELEC/HOT BUS/702PP SPLY 12PB2 E02
    123VU TR2/214XP/SPLY 2PU2 AB04 105VU ELEC/HOT BUS/701PP SPLY 12PB1 E01
    123VU BUS 2/204XP/SPLY 3XN2 AB02 105VU ELEC/BAT REF/BCL2 9PB2 F02
    123VU BUS 2/231XP-A/SPLY 5XN2 AB01 105VU ELEC/BAT REF/BCL1 9PB1 F01
    123VU AC ESS/BUS ON/BUS 1 1XC AC12 105VU ELEC/STAT INV/CNTOR/CTL 14XB G02
    123VU FWD GALLEY/FEEDER F 16MC AC10 105VU ELEC/BAT BUS/REF/BCL1 8PB1 G01
    14 12
    (4) ELECTRICAL POWER system (7) FLIGHT CONTROLS system
    ON A/C ALL
    49VU FLIGHT CONTROLS/FCDC1/SPLY 20CE1 B10
    123VU SHED BUS/218XP/220XP SPLY 28XN AC02
    49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09
    123VU AC ESS/BUS ON/BUS 2 2XC AC01
    49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08
    123VU BUS 1/101XP/SPLY 1XN1 AD11
    49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07
    123VU AFT GALLEY/FEEDER B 12MC AD09
    49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06
    123VU FWD GALLEY/FEEDER D 2MC AD04
    105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02
    123VU BUS 2/212XP/SPLY 10XN AD03
    105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01
    123VU BUS 2/202XP/SPLY 1XN2 AD02
    105VU FLT CTL/SEC1/STBY SPLY 22CE B01
    123VU FWD GALLEY/FEEDER C 1MC AE10
    121VU FLIGHT CONTROLS/WTB/FLP/SYS2 12CV P20
    123VU BUS 1/110XP/SPLY 7XN1 AF11
    121VU FLIGHT CONTROLS/WTB/SLT/SYS2 11CV P19
    123VU AFT GALLEY/FEEDER E 14MC AF09
    121VU FLIGHT CONTROLS/SLT FLP/POS/IND2 2CN P16
    123VU AFT GALLEY/FEEDER A 3MC AF04
    121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
    123VU BUS 2/210XP/SPLY 7XN2 AF02
    121VU FLIGHT CONTROLS/FCDC2/SPLY 20CE2 Q20
    124VU SHED BUS 210PP/212PP/SPLY 11PN BA01
    121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19
    124VU SVCE/601PP/602PP/SPLY 1PX BB01
    121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18
    124VU TR2/CNTOR/SPLY 4PU2 BC01
    121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17
    124VU DC SVCE/602PP/SPLY 7PN BD01
    121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16
    124VU 206PP/208PP/SPLY 6PN BE01
    121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
    124VU 204PP/SPLY 3PN2 BF01
    121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
    124VU 202PP/SPLY 1PN2 BG01
    121VU RUDDER FTU 75CE R16
    125VU BAT BUS/301PP/SPLY 11PB CC01
    122VU FLIGHT CONTROLS/WTB/FLP/SYS1 10CV S07
    125VU 101PP/SPLY 1PN1 CD01
    122VU FLIGHT CONTROLS/WTB/SLT/SYS1 9CV S06
    125VU 103PP/SPLY 3PN1 CE01
    125VU TR1/CNTOR/SPLY 4PU1 CF01
    8) FUEL system
    (5) EQUIPMENT/FURNISHINGS system 49VU FUEL/SMOKE/CONFIG/PUMP CTL 55QA A14
    49VU FUEL/FQI/CHAN/1 1QT A13
    TBD 36ME
    49VU FUEL/X FEED/VALVE/MOT1 2QE A12
    TBD 51MF
    49VU FUEL/XFR VALVE1/WING/R 2QP A11
    TBD 61MF
    49VU FUEL/XFR VALVE1/WING/L 1QP A10
    121VU PILOTS OUTLETS/STAT INV 1NA K25
    49VU FUEL/LP VALVE/MOT1/ENG2 2QG A09
    121VU PILOTS OUTLETS/115V 60HZ 2NA K23
    49VU FUEL/LP VALVE/MOT1/ENG1 1QG A08
    121VU ELT NAV&A/C IDENT 114MX R14
    49VU APU/FUEL/BLOW OFF/PUMP 2QC B14
    122VU COCKPIT SEATS/SEAT CTL/F/O 1MS2 U14
    121VU APU/FUEL/BLOW OFF/CTL 1QC K39
    122VU COCKPIT SEATS/SEAT CTL/CAPT 1MS1 U11
    121VU FUEL/FQI/CHANNEL/1 AND 2 8QT L26
    121VU FUEL/HI/LVL/SPLY 1QJ L25
    15 17

    (9) HYDRAULIC POWER system (11) INDICATING RECORDING system


    121VU HYDRAULIC/LOW/LVL/IND 1832GQ N32 49VU CAPT/LOUD/SPKR 5WW F10
    121VU HYDRAULIC/HYD POWER/Y 3803GX N30 49VU SDAC/1 AND 2/28VDC/ESS BUS 12WV F05
    121VU HYDRAULIC/HYD/QTY/IND 1831GQ P35 49VU SDAC/1/SPLY 3WV F04
    121VU HYDRAULIC/RAT/SPLY/EXTN/SOL1 2803GE P33 49VU SDAC/2/26VAC SYNC/AC ESS BUS 6WV F03
    121VU HYDRAULIC/Y HYD/PUMP ENG2/MONG 3700GD Q37 49VU SDAC/1/26VAC SYNC/AC ESS BUS 5WV F02
    121VU HYDRAULIC/Y HYD/PUMP ENG2/CTL 3701GD Q36 49VU FWS/FWC1/SPLY 3WW F01
    121VU HYDRAULIC/G HYD/PUMP ENG1/CTL 1701GK R35 49VU NAV/DME/1 1SD1 G14
    121VU HYDRAULIC/G HYD/PUMP ENG1/MONG 1702GK R34 106VU EMER/GEN/REF 27WV B05
    106VU DC BUS/1 AND 2/MONG 68WV C03
    ON A/C 013-014, 016-100, 203-300
    121VU PTR/SPLY 6TW J21
    121VU PTU INHIT/Y SYS 1808GL Q33
    121VU CFDS/TEST PLUG/2 10TW J20
    121VU PTU INHIT/G SYS 1807GL Q32
    121VU CFDS/TEST PLUG/1 9TW J19
    ON A/C ALL 121VU CFDS/CFDIU/SPLY 2TW J18
    123VU B HYD/ELEC PUMP 2701GJ AB09 121VU CFDS/CFDIU/BACK/UP 8TW J17
    123VU Y HYD/ELEC/PUMP 3802GX AB06 121VU DATA/LOADER/SPLY 3TD J16
    123VU Y HYD/ELEC/ELEC PUMP/NORM 3801GX AB03 121VU DLS&/DLRB/SPLY 5TD J15
    121VU RCDR/ACCLRM 9TU K18
    (10) ICE AND RAIN PROTECTION system 121VU AIDS & RCDR/QAR 14TU K17
    121VU RCDR/DFDR 7TU K16
    49VU ANTI ICE/WING/CTL 2DL C02 121VU AIDS & RCDR/FDIMU 5TV K15
    49VU ANTI ICE/WING/MONG 1DL C01 121VU COM NAV/DME/2 1SD2 K06
    49VU ANTI ICE/PROBES/AOA/1 4DA1 D04 121VU CLOCK/STBY/SPLY 4FS N02
    49VU ANTI ICE/PROBES/PHC/1 2DA1 D03 121VU EIS/F/O/LOUD/SPKR 4WW P08
    49VU ANTI ICE/PROBES/PITOT/1 3DA1 D02 121VU EIS/SDAC1 AND 2/DOOR/DET/PAX 48WV P05
    49VU ANTI ICE/RAIN/RPLNT/CAPT 1DB1 D01 121VU EIS/SDAC1 AND 2/BUS1/28VDC 14WV P04
    122VU ANTI ICE/WINDOWS/R 4DG2 W14 121VU EIS/SDAC1 AND 2/BUS2/28VDC 4WV P03
    122VU ANTI ICE/WHC/2 5DG2 W13 121VU EIS/SDAC1 AND 2/DOOR/DET/AVNCS 46WV P02
    122VU ANTI ICE/F/O/WIPER 4DB2 W12 121VU EIS/DMC3/SPLY 10WT3 Q09
    122VU ANTI ICE/RAIN/RPLNT/F/O 1DB2 W11 121VU EIS/DMC2/SPLY 10WT2 Q08
    122VU ANTI ICE/ENG/2 1DN2 W10 121VU EIS/FWC2/SPLY 2WW Q07
    122VU ANTI ICE/WINDOWS/L 4DG1 X14 121VU EIS/SDAC/2/SPLY 2WV Q06
    122VU ANTI ICE/WHC/1 5DG1 X13 121VU EIS/SDAC/2/BUS1/26VAC SYNC AC 10WV Q05
    122VU ANTI ICE/WIPER/CAPT 4DB1 X12 121VU EIS/SDAC/1/BUS2/26VAC SYNC AC 7WV Q03
    122VU ANTI ICE/ENG/1 1DN1 X10 121VU EIS/SDAC/2/BUS2/26VAC SYNC AC 8WV Q02
    122VU ANTI ICE/PROBES/PHC/3 2DA3 Y16 121VU EIS/ECAM DU/LOWER/SPLY 13WT2 R11
    122VU ANTI ICE/PROBES/2/TAT 1DA2 Y15 121VU EIS/ECAM DU/LOWER/SWTG 24WT2 R10
    19 21
    (8) FUEL system (5) EQUIPMENT/FURNISHINGS system
    ON A/C 002-100, 201-300
    121VU FUEL/RFL/DFL/SPLY 2QU L24
    2000VU SEAT POWER-MCU 2 59HP B08
    121VU FUEL/RFL/DFL/XFR/DEFUEL/VALVE 1QU L23
    2000VU SEAT POWER-MCU 1 58HP B05
    121VU APU/FUEL/LP VALVE/CTL 1QF M40
    121VU APU/FUEL/LP VALVE/SPLY 2QF M39 ON A/C ALL
    121VU APU/FUEL/PUMP/CTL 3QC M38 2001VU MEDICAL OUTLET-AC-RH 18MF C07
    121VU FUEL/FQI/CHAN/2 2QT M27 2001VU MEDICAL OUTLET-DC-RH 17MF C05
    121VU FUEL/LP VALVE/MOT2/ENG2 4QG M26 2001VU MEDICAL OUTLET-AC-LH 7MF C03
    121VU FUEL/LP VALVE/MOT2/ENG1 3QG M25 2001VU MEDICAL OUTLET-DC-LH 6MF C01
    121VU FUEL/X FEED/VALVE/MOT2 1QE M24
    121VU FUEL/XFR VALVE2/WING/R 4QP M23 (6) FIRE PROTECTION system
    121VU FUEL/XFR VALVE2/WING/L 3QP M22
    121VU FUEL/L WING TK/PUMP2 SPLY 7QA N26 49VU ENGINE/2/FIRE DET/LOOP B 8WD2 A07
    121VU FUEL/L WING TK/PUMP1 SPLY 1 QA N23 49VU ENGINE/1/FIRE DET/LOOP A 7WD1 A06
    121VU FUEL/CTR TK/PUMP2 SPLY 30QA P26 49VU AIR COND/CIDS/SDF/DIR2 ESS 18WH C06
    121VU FUEL/CTR TK/PUMP1 SPLY 29QA P23 49VU AIR COND/CIDS/SDF/DIR1 ESS 15WH C05
    121VU FUEL/R WING TK/PUMP2 SPLY 8QA Q26 121VU APU/FIRE AND OVHT/DET/LOOP B 2WG L44
    121VU FUEL/R WING TK/PUMP1 SPLY 2QA Q23 121VU APU/FIRE AND OVHT/DET/LOOP A 1WG L43
    121VU FUEL/PUMPS/2/R CTL AND L IND 10QA R29 121VU APU/AUTO/EXTIG/GND/TEST 30WF L40
    121VU FUEL/PUMPS/1/R CTL AND L IND 4QA R28 121VU APU/FIRE/EXTIG/SQUIB/B 2WF L39
    121VU FUEL/CTR TK/AUTO/CTL 47QA R27 121VU APU/FIRE/EXTIG/SQUIB/A 1WF L38
    121VU FUEL/CTR TK/PUMPS1 AND 2/CTL AND IND 32QA R26 121VU APU/FIRE/LP VALVE/NORM 4WF M42
    121VU FUEL/CTR TK/PUMPS1 AND 2/CTL AND IND 31QA R25 121VU APU/FIRE/LP VALVE/STBY 3WF M41
    121VU FUEL/PUMPS/2/L CTL AND R IND 9QA R24 121VU ENG/ENG1 AND 2 FIRE EXTIG/BTL1/SQUIB/B 2WE1 Q44
    121VU FUEL/PUMPS/1/L CTL AND R IND 3QA R23 121VU ENG/ENG1 AND 2 FIRE EXTIG/BTL1/SQUIB/A 1WE1 Q43
    123VU L WING TK/PUMP 1/STBY SPLY 11QA AD12 121VU ENG/ENG1 AND 2 FIRE EXTIG/BTL2/SQUIB/B 2WE2 Q42
    123VU R WING TK/PUMP 1/STBY SPLY 12QA AE12 121VU ENG/ENG1 AND 2 FIRE EXTIG/BTL2/SQUIB/A 1WE2 Q41
    121VU ENGINE/ENG2/FIRE DET/LOOP A 7WD2 Q39
    (9) HYDRAULIC POWER system 121VU ENGINE/ENG1/FIRE DET/LOOP B 8WD1 Q38
    122VU AIR COND/CARGO/FIRE/EXTIG 1WX T19
    49VU HYD/FIRE VALVE/Y/ENG2 3702GD C14 122VU AIR COND/CIDS/SDF/DIR NORM/2 14WH T18
    49VU HYD/FIRE VALVE/G/ENG1 1703GK C13 122VU AIR COND/CIDS/SDF/DIR NORM/1 17WH T17
    49VU HYD/HYD PWR/B WARN/& CTL 2702GJ C12
    49VU HYD/HYD/PRESS/XMTR 1841GN C11 (7) FLIGHT CONTROLS system
    49VU HYD/RAT/CTL 2801GE D14
    121VU HYDRAULIC/SOL VALVES/G/Y/B/LEAK/TST 1881GP N35 49VU FLIGHT CONTROLS/SLT FLP/POS/IND 1 1CN B12
    121VU HYDRAULIC/SOL VALVES/G/Y/PTU 1801GL N34 49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11
    18 16

    (11) INDICATING RECORDING system (10) ICE AND RAIN PROTECTION system
    121VU EIS/DMC2/SWTG 21WT2 R08 122VU ANTI ICE/PROBES/2/PITOT 3DA2 Y14
    121VU EIS/ND/F/O/SWTG 23WT2 R06 122VU ANTI ICE/PROBES/2/AOA 4DA2 Y13
    121VU EIS/PFD/F/O/SWTG 22WT2 R05 122VU ANTI ICE/PROBES/PHC/2 2DA2 Y12
    121VU EIS/ND/F/O 12WT2 R04 122VU ANTI ICE/PROBES/2/STATIC 5DA2 Y11
    121VU EIS/PFD/F/O 11WT2 R03 122VU ANTI ICE/PROBES/3/PITOT 3DA3 Z16
    122VU ANTI ICE/PROBES/3/AOA 4DA3 Z15
    (12) LANDING GEAR system 122VU ANTI ICE/PROBES/3/STATIC 5DA3 Z14
    122VU ANTI ICE/PROBES/1/STATIC 5DA1 Z13
    49VU ABCU &/Y BRK/PRESS IND 61GG C10 122VU ANTI ICE/PROBES/1/TAT 1DA1 Z12
    49VU L/G/LGCIU/SYS1/NORM 1GA C09 123VU ANTI ICE/L/WHSLD 1DG1 AF10
    121VU HYDRAULIC/BRK/TEMP/DET/UNIT 1GW M37 123VU ANTI ICE/R/WHSLD 1DG2 AF03
    121VU HYDRAULIC/BRAKING AND STEERING/SYS2/SPLY 4GG M36 2000VU POT/WASTE WIP-HEATER-LINE 1DW A02
    121VU HYDRAULIC/BRAKING AND STEERING/SYS2/CTL 3GG M35 2000VU POT/WASTE WIP-HEATER-CTL 2DW A01
    121VU HYDRAULIC/BRAKING AND STEERING/SYS1/CTL 1GG M34
    121VU HYD/BRAKING AND STEERING/SYS1/IND AND/SPLY 2GG M33 ON A/C 251-300
    121VU HYDRAULIC/PARK BRK/CTL/STBY 71GG N37 2000VU WASTE WIP-DRAINMAST-FWD 1DU B06
    121VU HYDRAULIC/PARK BRK/CTL/NORM 70GG N36
    ON A/C ALL
    121VU ABCU/HOT BUS/SPLY 110GG P30
    2001VU WASTE WIP-DRAINMAST-AFT 11DU E01
    121VU HYDRAULIC/LGCIU/SYS2 2GA Q35
    121VU HYDRAULIC/LGCIU/SYS1/GRND SPLY 52GA Q34 ON A/C 101-102, 201-300
    2001VU POT/WASTE WIP-SVCE-PNL 15DV D01
    ON A/C 002-100, 201-300
    121VU LGCIU/BAT SPLY/SYS2 59GA R33
    121VU LGCIU/BAT SPLY/SYS1 58GA R32 (11) INDICATING RECORDING system

    ON A/C 251-300 49VU EIS/ECAM/CTL/PNL 15WT E12


    49VU EIS/DMC1/SPLY 10WT1 E11
    121VU HYDRAULIC/BRK FAN/WHEELS/3 AND 4 2GS L35
    121VU HYDRAULIC/BRK FAN/WHEELS/1 AND 2 1GS L32 49VU EIS/DMC3/STBY/SPLY 14WT1 E10
    49VU EIS/DMC1/SWTG 21WT1 E09
    121VU HYDRAULIC/BRK/FAN/CTL 3GS M32
    49VU EIS/DMC3/SWTG 21WT3 E07
    49VU EIS/ECAM DU/UPPER/SWTG 24WT1 E06
    (12) LIGHTS system 49VU EIS/ECAM DU/UPPER/SPLY 13WT1 E05
    49VU EIS/PFD CAPT/SWTG 22WT1 E04
    49VU LIGHTING/EMER LT/CKPT/DOME 1LE H08 49VU EIS/PFD/CAPT/SPLY 11WT1 E03
    49VU LIGHTING/EMER LT/CABIN 79WL H07 49VU EIS/ND CAPT/SWTG 23WT1 E02
    49VU LIGHTING/EMER LT/CABIN 2WL H06 49VU EIS/ND CAPT/SPLY 12WT1 E01
    49VU LIGHTING/EMER LT/CABIN 1WL H05 49VU CLOCK/NORM/SPLY 6FS F11
    22 20
    (12) LIGHTS system (14) NAVIGATION system
    49VU NAV PROBES/ADIRU3/PWR/SWTG 8FP F09
    49VU LIGHTING/ICE AND STBY/COMP/LIGHT 1LF H04
    49VU NAV PROBES/ADIRU 1/AND AOA 1/26VAC 5FP1 F07
    49VU LIGHTING/XFMR/115V.5V/ESS BUS 29LP H03
    49VU NAV PROBES/ADIRU1/115VAC 4FP1 F06
    122VU LIGHTING/LANDING LT/R/CTL 4LB T07
    49VU NAV/VOR/1 2RS1 G13
    122VU LIGHTING/LANDING LT/R/SPLY 2LB T06
    49VU NAV/MMR/1 42RT1 G12
    122VU LIGHTING/LANDING LT/L/CTL 3LB T05
    49VU COM NAV/ATC/1 5SH1 G11
    122VU LIGHTING/LANDING LT/L/SPLY 1LB T04
    49VU NAV/ADF/1 1RP1 H14
    122VU LIGHTING/EXT LT/NAV1/AND LOGO/LT 1LA T03
    105VU ADIRS/ADIRU1/28VDC 6FP1 C02
    122VU LIGHTING/EXT LT/NAV2/AND LOGO/LT 2LA T02
    105VU NAV/STBY/INST/BAT 23FN J01
    122VU LIGHTING/EXT LT/BEACON/UPPER 1LV U06
    121VU COM NAV/RADAR/2 5SQ2 K14
    122VU LIGHTING/EXT LT/BEACON/LOWER 5LV U03
    121VU COM NAV/RADAR/1 5SQ1 K13
    122VU LIGHTING/CABIN/EMER/LT 3WL V07
    121VU COM NAV/RAD ALTM/2 1SA2 K12
    122VU LIGHTING/WING/STROBE 10LV V05
    121VU COM NAV/RAD ALTM/1 1SA1 K11
    122VU LIGHTING/LOGO/L 2LY V03
    121VU COM NAV/TCAS 4SG K10
    122VU LIGHTING/LOGO/R 1LY V02
    121VU COM NAV/VOR/2 2RS2 K08
    122VU LIGHTING/EXT LT/TAXI AND TAKE OFF/CTL 2LR W09
    121VU COM NAV/ATC/2 5SH2 K07
    122VU LIGHTING/EXT LT/TAXI AND TAKE OFF/TAXI 1LR W08
    121VU COM NAV/ADF/2 1RP2 K02
    122VU LIGHTING/EXT LT/TAXI AND TAKE OFF/TO 3LR W07
    121VU COM NAV/MMR/2 42RT2 L07
    122VU LIGHTING/EXT LT/RWY TURN OFF/L 1LC1 W06
    121VU ADIRS/ADIRU/2PWR/SHED 10FP N10
    122VU LIGHTING/EXT LT/RWY TURN OFF/R 1LC2 W05
    121VU ADIRS/ADIRU/3PWR/SWTG 9FP N09
    122VU LIGHTING/EXT LT/WING/AND ENG SCAN/R 1LX W03
    121VU ADIRS/ADIRU/2/26VAC AND AOA 5FP2 N08
    122VU LIGHTING/EXT LT/WING/AND ENG SCAN/L 5LX W02
    121VU ADIRS/ADIRU/3/26VAC AND AOA 5FP3 N07
    122VU LIGHTING/WHL WELL/LTG/DOME 2LL X08
    121VU ADIRS/ADIRU/2/115VAC 4FP2 N06
    122VU LIGHTING/WHL WELL/LTG/OUT 1LL X07
    121VU ADIRS/ADIRU/3/115VAC 4FP3 N05
    122VU LIGHTING/TST/BOARD/SPLY 30LP X06
    121VU ADIRS/ADIRU/2/28VDC 6FP2 N04
    122VU LIGHTING/ANN LT SPLY/XFMR/BUS 2 27LP X05
    121VU ADIRS/ADIRU/3/28VDC 6FP3 N03
    122VU LIGHTING/ANN LT SPLY/XFMR/BUS 1 26LP X04
    121VU EIS/GPWS/115VAC 3WZ P07
    122VU LIGHTING/ANN LT SPLY/XFMR/STAT INV 28LP X03
    121VU EIS/GPWS/28VDC 2WZ P06
    122VU LIGHTING/CKPT/DOME 3LE Y06
    122VU LIGHTING/INSTL LT/GLARE/SHLD 5LF Y05
    122VU LIGHTING/INSTL LT/MAIN INST/PNL AND/PED 4LF Y04 (15) OXYGEN system
    122VU LIGHTING/INSTL LT/OVHD/PNL 3LF Y03 49VU OXYGEN/PASSENGER/ACTUATION 7WR HA08
    122VU LIGHTING/AVNCS COMPT/OUT/115VAC 12LS Z09 49VU OXYGEN/PASSENGER/ACTUATION 6WR HA07
    122VU LIGHTING/AVNCS COMPT/OUT/28VDC 11LS Z08 49VU OXYGEN/PASSENGER/ACTUATION 5WR HA06
    122VU LIGHTING/AVNCS COMPT/DOME 1LS Z07 49VU OXYGEN/PASSENGER/ACTUATION 4WR HA05
    122VU LIGHTING/FLOOD/F/O/SIDE 4LE Z06 49VU OXYGEN/PASSENGER/CTL AND WARN 3WR HA04
    23 25

    (19) AIRBORNE AUXILIARY POWER system TASK 24-00-00-810-818 - Computer Reset


    ATA 22 - Auto Flight
    121VU APU/OIL/HTR/SPLY 1KT K41
    ON A/C ALL
    121VU APU/APU/CTL 2KD L42
    SYSTEM
    121VU APU/ECB/SPLY 1KD L41 COMPUTER RESET PROCEDURE
    MALFUNCTION

    (20) DOORS system AUTO FLT FAC1(2) Open these C/Bs with the Yellow and
    YAW Green hydraulic systems pressurized:
    121VU EIS/SLIDES/ARM AND WARN/FLT 15WN P11 DAMPER - for the FAC 1: on the panel 49VU, C/B
    121VU EIS/SLIDES/ARM AND WARN/GND 13WN P10 1(2) FAULT B04
    122VU DOORS CKPT LOCK 1MQ T13 - for the FAC 2: on the panel 121VU, C/B
    122VU DOORS/CARGO 1MJ T12 M19
    Then close the C/Bs after 10 seconds.
    (21) ENGINE system WINDSHEA FAC Open then close the C/Bs in this the order:
    R DET 1+2 - on the panel 49VU, C/B B04 and C/B B03
    49VU ENGINE/2/FADEC A/AND EIU 2 2KS2 A05 FAULT or - on the panel 121VU, C/B M19 and C/B
    49VU ENGINE/1/FADEC A/AND EIU 1 2KS1 A04 REAC W/S M18.
    49VU ENGINE/1 AND 2/IGN/SYS A 1JH A03 DET FAULT
    49VU ENGINE/2/HP FUEL SOV 1KC2 A02
    49VU ENGINE/1/HP FUEL SOV 1KC1 A01 AUTO FLT FCU For the FCU1:
    121VU ENG2/REV/LOCK 1EG2 N45 FCU 1(2) - on the panel 49VU, open the C/B B05.
    FAULT For the FCU2:
    121VU ENG1/REV/LOCK 1EG1 N44
    121VU ENGINE/ENG2/OIL/CHIP/DET 4EN2 N43 - on the panel 121VU, open the C/B M21.
    121VU ENGINE/ENG2/OIL/PRESS 2EN2 N42 Close the C/B after 5 seconds.
    121VU ENGINE/ENG2/OIL/QTY 1EN2 N41 If the fault does not continue, do a check
    121VU ENGINE/ENG1/OIL/PRESS 2EN1 N40 of the target and barometer references
    121VU ENGINE/ENG1/OIL/QTY 1EN1 N39 shown, and correct then if necessary
    121VU ENGINE/ENG1/OIL/CHIP/DET 4EN1 N38 (reset successful).
    121VU ENGINE/IGN/ENG2/SYS B 3JH2 P42 If the fault continues, open again the two
    C/Bs B05 on 49VU and M21 on 121VU.
    121VU ENGINE/IGN/ENG1/SYS B 3JH1 P41
    Close the C/Bs after 7 min, with an
    121VU ENGINE/IGN/ENG2/SYS A BAT 2JH2 P40
    interval less than 5 sec between side 1 and
    121VU ENGINE/IGN/ENG1/SYS A BAT 2JH1 P39 side 2.
    121VU ENGINE/ENG2/FADEC B 4KS2 Q40 At least 30 sec are necessary until the end
    121VU ENGINE/ENG1 AND 2/EVMU 1EV R44 of the FCU1 and FCU2 safety test.
    121VU ENGINE/ENG1/FADEC B/AND EIU 4KS1 R41
    If the fault does not continue, do a check of the target and barometer
    references shown, and correct them if necessary (reset successful)
    If the fault continues, end of procedure (reset unsuccessful).
    27 29
    (15) OXYGEN system (13) LIGHTS system
    49VU OXYGEN/PASSENGER/CTL AND WARN 2WR HA03 122VU LIGHTING/FLOOD/CAPT/SIDE 5LE Z05
    49VU OXYGEN/PASSENGER/CTL AND WARN 1WR HA02 122VU LIGHTING/FLOOD/CTR INST/PNL 2LE Z04
    49VU OXYGEN/CREW/OXY/SPLY 1HT HA01 2000VU LAV FWD-OCCUPIED 1WJ F01
    2000VU AIR CONDTN-COMPT-OUTLET 1LK G08
    (16) PNEUMATIC system 2000VU PASSENGER READING LIGHT 6LW G06
    2000VU PASSENGER READING LIGHT 5LW G05
    49VU AIR BLEED/X FEED/VALVE/BAT 2HV D13 2000VU PASSENGER READING LIGHT 4LW G04
    49VU AIR BLEED/ENG 1/CTL 3HA1 D12 2000VU PASSENGER READING LIGHT 3LW G03
    49VU AIR BLEED/ENG 1/MONG 2HA1 D11 2000VU PASSENGER READING LIGHT 2LW G02
    122VU AIR BLEED/ENG 2/CTL 3HA2 Z23 2000VU PASSENGER READING LIGHT 1LW G01
    122VU AIR BLEED/ENG 2/MONG 2HA2 Z22 2000VU CAB LIGHT PWR-CEILING-AFT 307LG H08
    122VU AIR BLEED/X FEED VALVE/NORM 1HV Z20 2000VU CAB LIGHT PWR-CEILING-AFT 304LG H07
    2000VU CAB LIGHT PWR-CEILING-FWD 306LG H06
    (17) WATER/WASTE system 2000VU CAB LIGHT PWR-CEILING-FWD 305LG H05
    2000VU CAB LIGHT PWR-WINDOW-AFT 302LG H04
    ON A/C 101-102, 201-300
    2000VU CAB LIGHT PWR-WINDOW-AFT 301LG H03
    2000VU LAV FWD & MID-HOT WATER-A 1MB F02
    2000VU CAB LIGHT PWR-WINDOW-FWD 303LG H02
    ON A/C ALL 2000VU CAB LIGHT PWR-WINDOW-FWD 300LG H01
    2001VU VACU TOIL SYS-VACUUM-GEN 33MG A08 2000VU LIGHT-LDG-AREA 3LU J08
    2001VU VACUUM TOILET SYSTEM 32MG A01 2000VU LIGHT-CARGO COMPT-AFT 2LU J07
    2001VU VACU TOIL SYS-LAV PWR- 39MG B04 2000VU LIGHT-CARGO COMPT-FWD 1LU J06
    2001VU LAV AFT-HOT WATER-E 9MB B03 2000VU LIGHT-CABIN-ENTRY 308LG J02
    2001VU LAVATORY AFT 2MB B02 2000VU LIGHT-LAV 1LQ J01
    2001VU WATER SYS-AIR-COMPRESSOR 19MD F01
    ON A/C 101-102, 201-300
    ON A/C 101-102, 201-300 2000VU LIGHT-ATTND-WORK 1LZ J03
    2001VU VACU TOIL SYS-VACUUM-SYS 35MG A06
    ON A/C ALL
    2001VU VACU TOIL SYS-LAV PWR-E 34MG A04
    2001VU LAVATORY AFT-OCCUPIED 11WJ B04
    2001VU WATER SYS-QUANT IND 1MA B06
    2001VU LIGHT-APU 2LJ E08
    2001VU WATER SYS-DRAIN 1MP B05
    2001VU LIGHT-SEC 191LJ E07
    (18) INFORMATION system
    (14) NAVIGATION system
    121VU ATSU 1 3TX1 L16
    121VU ATSU 1/SWTG 5TX1 L15 TBD 1004SG
    49VU NAV/VOR/DME/RMI 12FN F13
    49VU NAV/STBY/INST 5FN F12
    26 24

    TASK 24-00-00-810-818 - Computer Reset TASK 24-00-00-810-818 - Computer Reset


    ATA 22 - Auto Flight ATA 21 - Air Conditioning
    ON A/C ALL ON A/C 015-049, 106-299, 301-399
    SYSTEM SYSTEM
    COMPUTER RESET PROCEDURE COMPUTER RESET PROCEDURE
    MALFUNCTION MALFUNCTION

    One MCDU MCDU Open then close the C/B of the CAB PR SYS CABIN For CPC 1:
    locked or blank FMGC defective MCDU and close it after 10 1(2) FAULT PRESSURE - On panel 49VU, open the C/B D09.
    Both MCDUs seconds: CONTROLLER For CPC 2:
    locked or blank - For the MCDU1: on the panel 121VU 1(2) - On panel 122VU, open the C/B Y22.
    or panel 49VU, C/B B01. After 5 seconds, close the C/B.
    - For the MCDU2: on the panel 121VU,
    C/B N20. AIR FWD CARGO On the panel 49VU:
    - For the MCDU3: on the panel 121VU, (AFT) CRG VENTILATION - Open the C/B 2NH
    C/B 11CA3. VENT FAULT CONTROLLER - Open the C/B C07
    After 5 seconds, close the C/B.
    FMGC FMGC On the panel 121VU or 49VU:
    malfunction - open the FMGC 1 C/B B02 and close it VENT AVNCS AEVC On the panel 122VU:
    after 10 seconds. SYS FAULT - open the C/B Y17
    If there is no reset of the FMGC 1, do a After 5 seconds, close the C/B.
    reset of the FMGC 2 on the panel
    121VU: AIR PACK AIR COND For the AIR COND SYSTEM
    - open the C/B M17 and close it after 10 1(2) REGUL SYSTEM CONTROLLER 1:
    seconds. FAULT CONTROLLER - on the panel 122VU, open the C/B X22,
    1(2) C/B Y18 and C/B X21
    - on the panel 49VU, open the C/B D08
    ATA 23 - Communications
    Then close the C/Bs .
    ON A/C 201-250
    SYSTEM
    For the AIR COND SYSTEM
    MALFUNCTIO COMPUTER RESET PROCEDURE
    N CONTROLLER 2:
    - on the panel 122VU, open the C/B W22,
    COM CIDS 1+2 CIDS - Open the C/Bs in this order: C/B Y20 , C/B W21 and C/B Y21
    FAULT on the panel 49VU, C/B G01 Then close the C/Bs.
    on the panel 121VU, C/B M05
    on the panel 49VU, C/B G02 COND AFT AFT CARGO On the panel 49VU:
    CRG HEAT HEAT - Open the C/B C07.
    on the panel 121VU, C/B M06
    FAULT CONTROLLER - After 5 seconds, close the C/Bs.
    - After 10 seconds, close the C/Bs in this
    order: M06, G02, M05 and G01.

    30 28
    TASK 24-00-00-810-818 - Computer Reset TASK 24-00-00-810-818 - Computer Reset
    23 - Communications ATA 27 - Flight Controls
    ON A/C 201-250 ON A/C ALL
    SYSTEM SYSTEM COMPUTER RESET PROCEDURE
    COMPUTER RESET PROCEDURE
    MALFUNCTION MALFUNCTION
    Uncommanded CIDS Press the EVAC/HORN SHUT -OFF E/W FCDC On the panel 49VU:
    EVAC horn switch. FCDC1(2) - For FCDC1, open the C/B B10
    actuation If unsuccessful: FAULT - For FCDC2, open the C/B Q20
    - Open the C/Bs in this order: - After 5 seconds, close the C/Bs.
    on the panel 49VU, C/B G01
    F/CTL ELAC ELAC Reset the defective ELAC:
    on the panel 121VU, C/B M05
    1(2) FAULT - Make sure that the hydraulic systems
    on the panel 49VU, C/B G02 F/CTL ALTN are depressurized before the reset.
    on the panel 121VU, C/B M06 LAW FAULT - Set the ELAC pushbutton switch to
    - After 10 seconds, close the C/Bs in this OFF, then to ON.
    order:
    M06, G02, M05 and G01. ELAC or SEC ELAC or SEC Reset the defective ELAC:
    malfunction - Make sure that the hydraulic systems
    Frozen RMP RMP You must do a reset of all the RMPs, one are depressurized before the reset.
    after the other.
    Open, then close the C/B of the
    On the RMP control panel: defective ELAC or SEC.
    - set the ON/OFF switch to OFF For the ELAC 1(2):
    - after 5 seconds, set the ON/OFF switch - On the panel 49VU, C/B B11
    to ON.
    - On the panel 121VU, C/B R20
    Frozen FAP FAP Open the C/Bs in this order: For the SEC 1(2)(3):
    on the panel 49VU, C/B H01 - on the panel 49VU, C/B B08.
    on the panel 121VU, C/B Q14 - on the panel 121VU, C/B Q18 or Q19.
    - After 10 seconds, close the C/Bs in this
    order: Q14, H01

    ON A/C 015-049, 106-200, 251-299,


    301-399
    If unsuccessful:
    on the panel 2000VU
    - open the tape reproducer /PRAM C/B
    2RX.
    After 10 seconds, close the C/B.
    33
    31

    TASK 24-00-00-810-818 - Computer Reset TASK 24-00-00-810-818 - Computer Reset


    ATA 32 – Main Landing Gear ATA 70 - Engine
    ON A/C ON A/C ALL
    SYSTEM SYSTEM
    COMPUTER RESET PROCEDURE COMPUTER RESET PROCEDURE
    MALFUNCTION MALFUNCTION

    Braking BSCU On the panel 121VU: ENG IGN FADEC and On the panels 49VU and 121VU open
    malfunction - open the C/Bs M34, M33, M35 and A+B FAULT EIU then close the C/B of the defective
    M36. FADEC
    ENG 1(2) FADEC
    - After 5 seconds, close the C/Bs. - For the FADEC 1, C/Bs A04 and R41.
    FADEC A(B)
    FAULT - For the FADEC 2, C/Bs A05 and Q40.
    L/G LGCIU 1(2) LGCIU 1(2) For the LGCIU 1:
    FAULT - on the panel 121VU, open the C/B Q34
    then on 49VU, C/B C09. Then close the
    ATA 77 – Engine Indicating
    C/B C09 and C/B Q34
    For the LGCIU 2: ON A/C ALL
    - on the panel 121VU, open then close SYSTEM
    the C/B Q35. MALFUNCTIO COMPUTER RESET PROCEDURE
    N

    Loss of EVMU On the panel 121VU:


    ATA 34 – Navigation
    N1VIB and - Open the C/B R44.
    ON A/C 001-049, 051-099, 101-299
    N2VIB - After 5 seconds, close the C/B
    SYSTEM indications
    COMPUTER RESET PROCEDURE
    MALFUNCTION for ENG1(2)
    NAV TCAS TCAS On the panel 121VU: in ECAM SD
    FAULT - Open the C/B K10.
    - After 5 seconds, close the C/B.
    NAV MMR 1(2) MMR1(2) For the MMR 1:
    FAULT - On the panel 49VU, open the C/B G12.
    - After 5 seconds, close the C/B.

    For the MMR 2:


    - On the panel 121VU, open the C/B L07.
    - After 5 seconds, close the C/B.

    35 37
    TASK 24-00-00-810-818 - Computer Reset TASK 24-00-00-810-818 - Computer Reset
    ATA 24 - Electrical Power
    ATA 28 - Fuel
    ON A/C ALL
    ON A/C ALL
    SYSTEM
    SYSTEM MALFUNCTION COMPUTER RESET PROCEDURE COMPUTER RESET PROCEDURE
    MALFUNCTION
    Loss of fuel quantity FQIC On the overhead circuit breaker GPU cannot GAPCU If at least one power source (IDG 1 or
    indication or, panel 49VU: be IDG 2, APU GEN or batteries) is
    Simultaneous triggering - Open the C/B A13. connected connected to the electrical network of
    of FUEL L XFR VALVE On the rear circuit breaker panel to the the aircraft:
    CLOSED and FUEL R XFR 121VU: aircraft - On the ELEC control panel 35VU:
    VALVE CLOSED, although - Open the C/B M27. . Push and release the EXT PWR
    FUEL SD indicates no
    - After 5 seconds, close the two pushbutton switch.
    anomaly.
    C/Bs. If no power source is connected to the
    electrical network of the aircraft:
    - On the ELEC control panel 35VU:
    ATA 30 - Ice and Rain Protection
    . Push the BAT 1 and BAT 2 pushbutton
    ON A/C ALL
    switches (the OFF legend goes off).
    SYSTEM
    COMPUTER RESET PROCEDURE
    MALFUNCTION

    WHC
    ATA 26 - Fire Protection
    ANTI ICE L(R)/ Open then close the C/B of the defective
    WHC. ON A/C 001-014, 051-099, 101-105
    WINSHIELD
    (WINDOW) For the WHC1: SYSTEM COMPUTER RESET PROCEDURE
    MALFUNCTION
    - on the panel 122VU, C/B X13
    For the WHC2: SMOKE LAV SDCU On the panel 49VU:
    - on the panel 122VU, C/B W13 + CRG DET - open the C/B C06
    FAULT On the panel 122VU:
    - open the C/B T18
    ATA 31 - Indicating/Recording Systems
    After 10 seconds, close the two C/B's.
    ON A/C
    SYSTEM
    COMPUTER RESET PROCEDURE
    ENG1(2) ENGINE FDU On the panel 49VU:
    MALFUNCTION LOOP k - For ENG1 FDU, open the C/B A06
    FAULT - For ENG2 FDU, open the C/B A07
    FWS FWC 1(2) FWC Open then close the C/B of the defective
    FAULT FWC . On the panel 121VU:
    For the FWC1: - For ENG1 FDU, open the C/B Q38.
    - on the panel 49VU, C/B F01. - For ENG2 FDU, open the C/B Q39
    For the FWC2: - After 5 seconds, close the C/Bs.
    - on the panel 121VU, C/B Q07.
    32
    34

    TASK 24-00-00-810-818 - Computer Reset


    ALERT CLASSIFICATION (ECAM)
    LEVEL 3 : RED WARNING ATA 34 - Navigation
    LEVEL 2 : AMBER CAUTION – With Chime ON A/C 001-049, 051-099, 101-299
    LEVEL 1 : AMBER ECAM MESSAGE – Without Chime SYSTEM
    COMPUTER RESET PROCEDURE
    MALFUNCTION

    FAILURE CLASSIFICATION (OMS) NAV GPWS FAULT GPWC On the panel 121VU:
    CLASS 1 : Log Book Entry : MEL - Open the C/B P07.
    CLASS 1 : Log Book Entry : Delayed Maintenance Action NAV GPWS TERR - After 5 seconds, close the C/B.
    DET FAULT
    CLASS 1 : No Log Book Entry : Scheduled Maintenance
    NAV GPS 1(2) GPSSU On the panel 121VU:
    SYSTEM TYPES (OMS) FAULT - For GPSSU1, open the C/B 2SN1.
    TYPE 1 : Memorization of 64 Flights
    TYPE 2 : Memorization of Last Flight - For GPSSU2, open the C/B 2SN2.
    TYPE 3 : No Memorization - After 5 seconds, close the C/Bs.
    NAV RA 1(2) XCVR-RA On the panel 121VU:
    FAULT - For XCVR-RA 1, open the C/B K11.

    - For XCVR-RA 2, open the C/B K12.


    - After 5 seconds, close the C/Bs.

    ATA 46 - Information Systems


    ON A/C 001-049, 051-099, 101-299
    SYSTEM
    COMPUTER RESET PROCEDURE
    MALFUNCTION

    ATSU ATSU On the rear circuit breaker panel


    malfunction 121VU:
    - Open the C/Bs in this order: L16 and
    L15.
    - After 5 seconds, clos e the C/Bs in this
    order: L15 and L16.

    36
    38
    ATA 21 Fault VU121 M17 FMGC2
    21 AIR PACK REGULATOR FAULT all data will be dumped
    Pack1 VU122 Y18 X21 X22 --------------------------------------------------------------------------------------------------
    Pack2 VU122 Y20 Y21 W21 W22 22 FMGC msg “set offside mg/mode”
    -------------------------------------------------------------------------------------------------- Select ILS on both ND's then back to NAV
    21 CABIN TRIM AIR VALVE IF NO HELP
    VU122 V17 ZONE TEMP CTL AC SYS 1 VU49 B02 FMGC1
    VU122 V19 ZONE TEMP CTL DC SYS 1 VU121 M17 FMGC2
    VU122 V18 ZONE TEMP CTL AC SYS 2 --------------------------------------------------------------------------------------------------
    VU122 V20 ZONE TEMP CTL DC SYS 2 22 FMGC msg “set offside mg/mode”
    -------------------------------------------------------------------------------------------------- (ON GROUND ONLY)
    21 VENTS AVIONICS EXTRACT FAULTS Turn off all flight control switches and back on
    VU122 Y17 AVNCS VENT MONG IF NO HELP
    IF NO HELP CAPT'S side
    VU49 D05 AVNCS VENT CTL VU49 B03 FAC1 26VAC
    VU49 D06 AVNCS VENT CTL VU49 B04 FAC1 28VDC
    IF NO HELP F/O's side
    VU123 AE2 AVNCS VENT EXTC FAN VU121 M18 FAC2 26VAC
    -------------------------------------------------------------------------------------------------- VU121 M19 FAC2 28VDC
    21 VENT AVIONICS FAULT --------------------------------------------------------------------------------------------------
    VU122 Y17 AVNCS VENT MONG 22 Rudder travel limit system #1
    IF NO HELP VU49 B03 FAC1 26VAC
    VU49 D05 AVNCS VENT CTL VU49 B04 FAC1 28VDC
    VU49 D06 AVNCS VENT CTL Cycle FAC switchs after CB reset
    -------------------------------------------------------------------------------------------------- IF NO HELP
    AIR – CPC1 FAULT Reset VU49 D09 VU49 B02 FMGC1
    AIR – CPC2 FAULT Reset VU122 Y22 Y23 See autopilot #1 fault
    --------------------------------------------------------------------------------------------------
    Operational Test of the Pack Temperature Control System 22 Rudder travel limit system #2
    AMM 21-61-00-710 VU121 M18 FAC2 26VAC
    Operational Test of the Pressure Control and Monitoring (CPC) VU121 M19 FAC2 28VDC
    AMM 21-31-00-710 Cycle FAC switchs after CB reset
    Operational Test of the Avionics Equipment Ventilation IF NO HELP
    Computer (AEVC) AMM 21-26-00-710 VU121 M17 FMGC2
    Pack Flow Control Valve ( 8HB AND 11HB) See autopilot #2 fault
    Removal / Instalation AMM 21-51-51-400 --------------------------------------------------------------------------------------------------
    Operational Test of the AFS AMM 22-96-00-710
    -------------------------------------------------------------------------------------------------- Operational Test of the Rudder Trim Function AMM 22-62-00-710
    ATA 22 Fault Operational Test of the Yaw Damper AMM 22-63-00-710
    22 AUTO FLT RUD TRV LIM SYS FAULT Operational Test of the Land CAT III Capability AMM 22-96-00-710
    Reset FAC 1 & 2 Pushbuttom switchs
    39 41

    -------------------------------------------------------------------------------------------------- Operational Test of the DC Generation Switching


    23 RMP FAULTS AMM 24-32-00-710-001
    Turn OFF then ON to reset --------------------------------------------------------------------------------------------------
    IF NO HELP ATA 25 Fault
    VU49 G10 RMP1 25 CREW SEAT PROBLEMS
    VU121 L02 RMP2 VU122 U11 CKPT SEAT CTL CAPT
    VU121 L03 RMP3 VU122 U14 CKPT SEAT CTL F/O
    -------------------------------------------------------------------------------------------------- Also each seat has a CB located on the control box
    23 SEAT VIDEO SYS UNIT PROBLEMS --------------------------------------------------------------------------------------------------
    Reset video unit with reset switch located fwd of screen behind 25 CARGO TESTING SYSTEM
    hole. Check cargo door ful open (green light)
    IF NO HELP Lower door off upper limit a few inches
    TURN SYSTEM OFF TO STOW raise door to full open
    -------------------------------------------------------------------------------------------------- IF NO HELP
    23 TCAS INOP MSG FWD CARGO SYSTEM
    VU121 K10 TCAS V2000 J01 FWD CARGO PWR
    NOTE: system thru MCDU V2000 J03 FWD CARGO CTL
    -------------------------------------------------------------------------------------------------- AFT CARGO SYSTEM
    23 VHF SYSTEM INOP V2001 E01 AFT CARGO PWR
    VU49 G09 VHF1 V2001 E03 AFT CARGO CTL
    VU121 L04 VHF2 IF NO HELP
    VU121 L05 VHF3 DEFER SYSTEM PER MEL
    -------------------------------------------------------------------------------------------------- --------------------------------------------------------------------------------------------------
    Static Discharge Long P/N E0399-01 IPC23-61-05 Lav. A Door Assy-Single IPC 24-41-41-61E
    Static Discharge short P/N E0400-01 IPC23-61-04 Lav. D – E Door Assy-Folding IPC 25-43-41/42
    -------------------------------------------------------------------------------------------------- Seat Assy Toilet P/N D254709100300 IPC 25-43-41
    Operational Test of the HF system AMM 23-11-00-710 Oven IPC.25-35-19
    Bite Test of the HF system with the CFDS: AMM 23-11-00-740 Coffee Maker IPC 25-35-15
    Operational Test of the VHF system AMM 23-12-00-710 Sun visor Install IPC 25-13-01-23
    Bite Test of the VHF system with the CFDS: AMM 23-12-00-740 Clip-Sun visor Front P/N 160-11105-080/-10797-090
    Operational Test of the Radio Management AMM 23-13-00-710 Box Assy-Sidewall Ovhd Stwg IPC 25-24-41
    Bite Test of the Radio Management with the CFDS: Pin P/N A2528652720200 Damper P/N 195405
    AMM 23-13-00-740 Washer P/N NAS1149C0432R
    Bite Test of the Satellite Communication system with the CFDS: Ring Retainer P/N NS16624-4025
    AMM 23-28-00-740 Headrest
    Operational Test of the Passenger Address System Button P/N F206838A006D
    AMM 23-73-00-710 Screw P/N B10042200000 / CMM 25-24-132
    Bite Test of the Passenger Entertainment System (Music) with the Table
    Programming an Test Panel (PTP) AMM 23-33-00-740-002 Latch Assy P/N 31128770006A
    Bite Test of the Cabin Intercommunication Data System (CIDS) Through Latch P/N 31127410006A / CMM 25-24-01
    the PTP AMM 23-73-00-740-003 Stop Curtain P/N 7722 / IPC 25-26-09
    43 45
    ATA 23 Fault 22 AUTO PILOT #1 FAULT
    23 Amp's freq's will not change from stby to active VU49 B02 FMGGC1
    Turn affected RMP OFF then ON --------------------------------------------------------------------------------------------------
    IF NO HELP 22 AUTO PILOT #2 FAULT
    VU49 B02 FMGC1 VU121 M17 FMGC2
    VU121 M17 FMGC2 --------------------------------------------------------------------------------------------------
    -------------------------------------------------------------------------------------------------- 22 DUAL CAT III MSG
    23 CID's system fault Reset FAC 1 & 2 Pushbuttom switchs first
    Attempt a reset at PTP panel first (RESET CB's TOGETHER) IF NO HELP
    IF NO HELP VU49 B04 FAC 1 28VAC
    A320 VU121 M19 FAC 2 28VDC
    VU49 G02 CID DIR 1&2 ESS --------------------------------------------------------------------------------------------------
    VU121 M05 CID DIR 1&2 NORM 22 FAC FAULTS SYS #1 YAW DAMPER 1(2)
    A319 Reset FAC 1 Pushbuttom switchs first
    VU49 G01 CID DIR ESS/1 IF NO HELP
    VU49 G02 CID DIR ESS/1 Note: open these CB's for 90 seconds
    -------------------------------------------------------------------------------------------------- VU49 B03 FAC1 26VAC
    23 COM VHF emitting fault MSGS CHECK: VU49 B04 FAC1 28VDC
    Transmission key on audio panel side stick radio sel hand mike --------------------------------------------------------------------------------------------------
    sel not trans positioning 22 FAC faults
    IF NO HELP VU49 B05 FCU1
    VU49 G09 VHF1 VU121 M21 FCU2
    VU121 L04 VHF2 --------------------------------------------------------------------------------------------------
    VU121 L05 VHF3 22 FMGC msg “opposite FM in progress of FMA shows OFFSIDE
    -------------------------------------------------------------------------------------------------- FDS”
    23 FLIGHT ATTND PANEL LOCKED UP VU49 B02 FMGC1
    A320 VU121 M17 FMGC2
    VU121 M14 CIDS FWD ATTND/PNL --------------------------------------------------------------------------------------------------
    A319 22 MDCU fault system #1
    VU121 Q14 CIDS FWD ATTND/PNL Recycle RPM 1 NAV switch
    -------------------------------------------------------------------------------------------------- IF NO HELP
    23 PAX ENT WILL NOT TURN ON or OFF VU49 B01 MCDU1
    VU2000 F6 CABIN COM SYS PES IF NO HELP
    IF NO HELP VU49 B02 FMGC1
    A320 all data will be dumped
    VU121 M07 THROUGH M13 --------------------------------------------------------------------------------------------------
    A 319 22 MDCU fault system #2
    VU121 M18 THROUGHT M14 Recycle RPM 1 NAV switch
    -------------------------------------------------------------------------------------------------- IF NO HELP
    23 PAX SEAT AUDIO INOP VU121 N20 MCDU2
    VU2000 F06 CABIN COM SYS PES IF NO HELP
    40
    42

    Fairing Sliding Plate Tab P/N K206278A006A Bite Test of the Cabin Intercommunication Data System (CIDS) Through
    Dish Locating P/N D2511043720000 / IPC 25-13-01-36 the CFDS AMM 23-73-00-740-005
    -------------------------------------------------------------------------------------------------- Operational Test of the Cockpit Voice Recorder (CVR)
    ATA 26 Fault AMM 23-71-00-710-001
    26 FWD & AFT CARGO DETECTS MSGS Operational Test of the Passagen Entertainment System (Video)
    Reset CB's together AMM 23-73-00-710-017
    VU49 C06 SDCU CHAN1 Operational Test of the Cabin Signs AMM 23-73-00-710-017
    VU122 T18 SDCU CHAN2
    IF NO HELP Passenger Control Unit
    A320 (Right) P/N 1303089-100 IPC. 23-33-12-07
    VU49 C06 SDCU CHAN1 (Left) P/N 1303088-100 IPC. 23-33-12-05
    VU122 T18 SDCU CHAN2
    VU49 C07 AFT CARGO VENT & HEAT CTL / MONG Reading Light Power Unit (RLPU)
    VU122 S22 AFT CARGO VENT & HEATING FAN P/N Z250H2103110 IPC 23-73-09
    -------------------------------------------------------------------------------------------------- --------------------------------------------------------------------------------------------------
    26 FWD & AFT CARGO HEAT DETECT FAULTS ATA 24 Fault
    A320 ONLY 24 ENG 1(2) GENERATOR ON LINE & NO PARAMETER SHOWN
    VU49 C07 AFT CARGO VENT & HEAT CTL / MONG CAUTION: ENGINES (S) MUST BE SHUT DOWN
    VU122 S22 AFT CARGO VENT & HEATING FAN VU122 T28 GCU1
    -------------------------------------------------------------------------------------------------- VU122 T27 GCU2
    26 LAV SMOKE DETECT MSG --------------------------------------------------------------------------------------------------
    VU49 C06 SDCU CHAN1 24 NO “AVAIL” ON EXT PWR SWITCH
    VU122 T18 SDCU CHAN2 CAUTION: ENGINE AND APU OFF AND GROUND POWER CONNECTED
    -------------------------------------------------------------------------------------------------- VU122 Y24 GPCU
    26 SDCU FAULTS --------------------------------------------------------------------------------------------------
    Reset CB's together 24 TRANSFORMER RECTIFIER FAULTS
    Pull out for 10 seconds Reset T/R thru MCDU or reset all three using GUARDED button
    Reset on 103VU panel in electrical bay
    Wait for 2 min before testing system --------------------------------------------------------------------------------------------------
    VU49 C06 SDCU CHAN1 24 BATTERY CHARGER LIMITER (BCL)
    VU122 T18 SDCU CHAN2 Reset ships battery on at a time with APU operating
    IF NO HELP IF NO HELP
    A320 ONLY VU105 BAT REF BCL1
    VU49 C06 SDCU CHAN1 VU105 BAT BUS REF BCL1
    VU122 T18 SDCU CHAN2 VU105 REF BCL2
    VU49 C07 AFT CARGO VENT & HEAT CTL / MONG VU105 BAT BUS REF BCL2
    -------------------------------------------------------------------------------------------------- --------------------------------------------------------------------------------------------------
    Operational Test of the Avionics Equipament Ventilation from the Operational Test of the Ground Power Control Unit (GPCU)
    MCDU AMM 26-15-00-710 AMM 24-41-00-740-002
    Test of the Cargo-Compartment Smoke-Detection System Operational Test oh the Battery Charger Limiter (BCL)
    AMM 26-16-00-710 AMM 24-38-00-710-001
    46 44
    Portable Fire-Extinguisher AMM 26-24-00 27 SPOILER 4 & 5 FAULT
    -------------------------------------------------------------------------------------------------- Use pushbutton switchs first
    ATA 27 Fault 4 & 5 SPR SEC3 & ELAC3
    27 ELAC 1 OR 2 FAULTS --------------------------------------------------------------------------------------------------
    Use Pushbutton Switch first Operational Test of the ELAC (Elevator Aileron Computer)
    Turn OFF for 15 Sec and then reset AMM 27-93-00-710-001
    IF NO HELP Operational Test of the SEC (Spoiler Elevator Computer)
    VU49 B11 ELAC NORM SPLY (ELAC1) Computer 1 (SEC1) AMM 27-94-00-710-002
    VU105 A01 ELAC 1 STABY SPLY (ELAC1) Computer 2 (SEC2) AMM 27-94-00-710-003
    VU121 R20 ELAC 2 NORM 2 NORM SPLY (ELAC2) Computer 3 (SEC3) AMM 27-94-00-710-001
    VU105 A20 ELAC STABY SPLY (ELAC2) Operational Test of the POB (Pressure Off Brake)
    -------------------------------------------------------------------------------------------------- AMM 27-51-00-710-???
    27 FCDC 1 (2) MSG Reset of the WTB (Wing Tip Brake) of the Flap System on the Ground
    VU49 B10 FCDC1 SPLY AMM 27-50-00-869-006
    VU121 Q20 FCDC2 SPLY --------------------------------------------------------------------------------------------------
    -------------------------------------------------------------------------------------------------- ATA 28 Fault
    27 FLIGHT CONTROL FLAPS LOCKED OUT 28 FQI INOP
    Perform wing tip brake (WTB) reset trough VU49 A13 FQI CHAN 1
    MCDU (Caution: HYD'S MUST BE OFF) VU121 M27 FQI CHAN 2
    -------------------------------------------------------------------------------------------------- VU121 L26 FQI CHAN 1 & 2
    27 FLT/CTL MAINTENANCE MSG --------------------------------------------------------------------------------------------------
    (Can be deferred) 28 FUEL APU LP VALVE FAULT MSG
    VU49 B10 FCDC1 SPLY Triggered when the APU master switch is selected OFF during
    VU121 Q20 FCDC2 SPLY an EMERG SHUT DOWN or AUTO SHUT DOWN. Cycling the MASTER
    -------------------------------------------------------------------------------------------------- switch ON then OFF may clear this msg.
    27 FLT/CTL MSG WITH SLAT/FLAP FAULTS --------------------------------------------------------------------------------------------------
    VU49 B06 SLT CTL & MONG SYS1 FQIC Reset for 5 sec CB's 1QT and 2QT
    VU49 B07 FLP CTL & MONG SYS1 1QT - VU49 A13 FUEL/FQI/CHAN 1
    VU121 R21 SLT CTL & SYS2 2QT - VU121 M27 FUEL/FQI/CHAN 2
    VU121 Q21 FLP CTL & MONG SYS2 --------------------------------------------------------------------------------------------------
    -------------------------------------------------------------------------------------------------- Functional (BITE) Test FQIC AMM 28-46-00-740-001
    27 SEC 1 FAULTS Functional (BITE) Test FLSCU AMM 28-46-00-740-001
    1 & 2 SPR SEC 1 & ELAC 1 Fuel System - Servicing AMM 12-11-28
    3 & 4 SPR SEC 2 & ELAC 2 Use of Magnetic Indicators FCOM-2-01 Loading MLI – Tables 2.01.30
    5 & 6 SPR SEC 3 & ELAC 3 Use of (MLI) Magnetic Level Indicator AMM 12-11-28-650-007
    IF NO HELP --------------------------------------------------------------------------------------------------
    VU49 B08 SEC1 NORM SPLY (SEC1)
    VU105 B01 SEC1 STBY SPLY (SEC1)
    --------------------------------------------------------------------------------------------------
    27 SEC 2 FAULTS
    1 & 2 SPR SEC 1 & ELAC 1
    47 49

    IF NO HELP VU121 N05 ADIRU 2 28VDC (SYS2)


    VU121 P34 for BLUE System or Reset SDAC's to clear all hyd's VU121 N06 ADIRU 3 115VAC (SYS3)
    msg's – see ATA31 VU121 N04 ADIRU 3 28VDC (SYS3)
    -------------------------------------------------------------------------------------------------- --------------------------------------------------------------------------------------------------
    HYS PUMP P/N 887673 IPC 29-11-51 31 ADIRU 1 FAULT
    Drainage of the Reservoir of the Hyd System VU49 F06 ADIRU 115VAC (SYS1)
    GREEN AMM 29-10-00-680-001 VU105 C02 ADIRS ADIRU 1 28VAC (SYS1)
    YELLOW AMM 29-10-00-680-002 --------------------------------------------------------------------------------------------------
    BLUE AMM 29-10-00-680-001 31 ADIRU 2 FAULT
    -------------------------------------------------------------------------------------------------- VU121 N07 ADIRU 2 115 VAC (SYS2)
    ATA 30 Fault VU121 N05 ADIRU 2 28VDC (SYS2)
    30 ANTI ICEENG 1 (2) --------------------------------------------------------------------------------------------------
    Normal at Idle 31 ADIRU 3 FAULT
    Acceptable provided indications are normal when power is VU121 N06 ADIRU 3 115VAC (SYS3)
    increased VU121 N04 ADIRU 3 28VDC (SYS3)
    -------------------------------------------------------------------------------------------------- --------------------------------------------------------------------------------------------------
    30 ANTI ICE L /R WINDSHIELD 31 CFDS REAL TIME FAILURE OR WARNING AUTOMATIC
    If warming occurs on ground with OAT greater than 40deg C PRINTING
    and AC packs of. Pull WHC CB's and place a damp towel on inner pane This report needs to be inhibited through CFDS ACARS print
    over the sensor for approx. 5 minutes. program.
    Reset the WHC CB's and turn the packs ON 1) Enter CFD.
    VU122 X13 WHC 1 (LEFT SIDE 2) Select page 2.
    VU122 W13 WHC 2 (RIGHT SIDE) 3) Select ACARS print program.
    -------------------------------------------------------------------------------------------------- 4) Select real time messages print OFF.
    30 ANTI-ICE MSGS 5) return CFDS to normal.
    VU49 D03 ANTI ICE PROBES PHC1 --------------------------------------------------------------------------------------------------
    VU122 Y12 ANTI ICE PROBES PHC 2 31 DIVERGENCE SUMMARY REPORT AUTO PRINTING
    VU122 Y16 ANTI ICE PROBES PHC 3 This report needs to be inhibited through AID system
    -------------------------------------------------------------------------------------------------- 1) Enter AIDS
    30 ANTI-ICE PROBE MSGS SYSTEM #1 2) Select programming.
    VU49 D02 PITOT 1 3) Enter password “SFIM”.
    VU122 Z13 STATIC 1 4) Select programming menus.
    VU49 D04 AOA 1 5) Select reports inhibit.
    VU122 Z12 TAT 1 6) Select “YES” for print & link functions
    IF NO HELP YES should be GREEN = report inhibited
    VU49 F07 ADIRU 1 & AOA 1 26 VAC 7) Select return
    VU49 F06 ADIRU 1 115VAC 8) Push MCDU key
    VU105 C02 ADIRU 1 28 VDC --------------------------------------------------------------------------------------------------
    -------------------------------------------------------------------------------------------------- 31 ECAM PAGE(S) LOCKED
    30 ANTI ICE PROBE MSGS SYSTEM #2 VU49 F01 FWS FWC 1 SPLY
    VU122 Y14 PITOT 2 VU121 Q7 EIS FWC 2 SPLY
    51 53
    Enter code: Roll – ROLL
    Pitch – PTCH 3 & 4 SPR SEC 2 & ELAC 2
    5 & 6 SPR SEC 3 & ELAC 3
    Pitch Ref Roll Ref
    IF NO HELP
    Minu 1.5 1 Minu 1.5 A VU121 Q18 SEC2 SPLY (SEC2)
    --------------------------------------------------------------------------------------------------
    Minu 1.0 2 Minu 1.0 B 27 SEC 3 FAULTS
    Minu 0.5 3 Minu 0.5 C 1 & 2 SPR SEC 1 & ELAC 1
    3 & 4 SPR SEC 2 & ELAC 2
    0.0 4 0.0 D 5 & 6 SPR SEC 3 & ELAC 3
    IF NO HELP
    Plus 0.5 5 Plus 0.5 E
    VU121 Q19 SEC3 SPLY (SEC3)
    Plus 1.0 6 Plus 1.0 F --------------------------------------------------------------------------------------------------
    27 SIDE STICK PRIORITY MSG
    Plus 1.5 7 Plus 1.5 G FAC 1 & 2 SWITCHS
    SEC 2, 2 & 3 SWITCHS
    ELAC 1 & 2 SWITCHS
    ATA 29 Fault --------------------------------------------------------------------------------------------------
    29 FAULTS CAUSED BY OPERATION WITHIN 30 SECONDS 27 SLOW SLATS
    AFTER SECOND ENGINE START AND PTU ECAM FAILURE MSG'S VU49 B06 SLT CTL & MONG SYS1
    OR PTU FAULTS VU121 R21 SLT CTL & SYS2
    Reset with engines running: IF NO HELP
    a) Reset msg using Master Caution pushbutton switchs. VU49 B06 SLT CTL & MONG SYS1
    b) Select HYD page on ECAM VU49 B07 FLP CTL & MONG SYS1
    c) Select Yelow Hyd Elec Pump ON VU121 R21 SLT CTL & SYS2
    d) Select Yelow Hyd Elec Pump OFF VU121 Q21 FLP CTL & MONG SYS2
    e) Wait a minimum of 30 seconds --------------------------------------------------------------------------------------------------
    f) Cycle PTU switch from ON to OFF to ON 27 THS (Trimmable Horizontal Stabilizer) WILL NOT RETURN
    g) Select #1 Eng Green Hyd Pump OFF TO ZERO ON LDG
    PTU should operate Yellow to Green Power up all three HYD systems and turn the ELAC pushbutton
    h) Select #1 Eng Green Hyd Pump ON switchs to OFF. Manually TRIM NOSE DOWN a few degrees and return
    i) Select #2 Eng Yellow Hyd Pump OFF ELAC switchs to ON. THS should return to zero. Turn OFF ELAC
    PTU should operate Green to Yellow switchs, manual TRIM NOSE UP and return ELAC switchs to ON.
    j) Select #2 Eng Yellow Hyd Pump ON THS SHOULD RETURN TO ZERO
    k) ECAM should be NORMAL --------------------------------------------------------------------------------------------------
    -------------------------------------------------------------------------------------------------- 27 SPOILER 1 & 2 FAULT
    29 PTU FAULTS (NOT CAUSED BY CARGO DOOR OPERATION Use pushbutton switchs first
    AFTER ENGINE START) 1 & 2 SPR SEC1 & ELAC1
    121VU N34 HYD/SOL VALVES/G/Y/PTU --------------------------------------------------------------------------------------------------
    -------------------------------------------------------------------------------------------------- 27 SPOILER 3 & 4 FAULT
    29 HYD REVS LOW PRESSURE MSG Use pushbutton switchs first
    Pressurize Hyd Reservoirs with either APU or Engines 3 & 4 SPR SEC2 & ELAC2
    50 48

    31 DMC FAULT MSG EIS DMC 1, 2 OR 3 VU122 Y11 STATIC 2


    VU49 E11 EIS DMC 1 SPLY (SYS 1) VU122 Y13 AOA 2
    VU121 Q08 EIS DMC 2 SPLY (SYS 2) VU122 Y15 TAT 2
    VU121 Q09 EIS DMC 3 SPLY (SYS 3) IF NO HELP
    VU49 E10 EIS DMC 3 STBY SPLY (SYS 3) VU121 N09 ADIRU2 16VAC & AOA
    -------------------------------------------------------------------------------------------------- VU121 N07 ADIRU 3 115VAC
    31 NO AIDS INDICATION DISPLAYED ON THE MCDU MENU VU121 N05 ADIRU 2 12VDC
    PAGE VU121 N11 ADIRU 2 PWR SHED
    VU121 K15 AIDS (DMU / QAR / DAR) --------------------------------------------------------------------------------------------------
    CB's labelled different but location name 30 FWD (AFT) DRAIN MAST ECAM MSG
    -------------------------------------------------------------------------------------------------- VU2000 D01 FWD DRAIN MAST
    31 SDAC 1 FAULTS VU2001 D05 AFT DRAIN MAST
    VU49 F02 SDAC 1 26 VAC SYNC AC ESS BUSS --------------------------------------------------------------------------------------------------
    VU49 F04 SDAC 1 SPLY 30 ANTI ICE PROBE MSGS SYSTEM #3
    VU49 F05 SDAC 1 & 2 28VAC ESS BUS VU122 Z16 PITOT 3
    VU121 Q04 SDAC 1 26VAC SYNC AC VU122 Z14 STATIC 3
    VU121 Q03 SDAC 1 26VAC SYNC AC VU122 Z15 AOA3
    VU121 P04 SDAC 1 26VAC IF NO HELP
    -------------------------------------------------------------------------------------------------- VU121 N08 ADIRU 3 26VAC & AOA
    31 SDAC 2 FAULTS VU121 N06 ADIRU 3 115VAC
    VU49 F05 SDAC 1 & 2 28VAC ESS BUS VU121 N04 ADIRU 3 28VDC
    VU121 Q02 SDAC 2 26VAC SYNC AC VU49 F09 ADIRU 3 STWG SPLY
    VU121 Q05 SDAC 2 26VAC SYNC AC VU121 N10 ADIRU 3 STWG SPLY
    VU121 Q06 SDAC 2 SPLY --------------------------------------------------------------------------------------------------
    VU121 P03 SDAC 2 26VAC 30 WINDSHIELD HEAT FAULTS
    -------------------------------------------------------------------------------------------------- VU122 X13 WHC 1 (LEFT SIDE)
    31 UNABLE TO SWITCH DU VU122 X14 WNDOW HEAT
    VU49 E02 EIS ND CAPT SWTG VU122 W13 WHC 2 (RIGHT SIDE)
    VU49 E04 EIS PFD CAPT SWTG VU122 W14 WINDOW R HEAT
    VU49 E06 EIS ECAM DU UPPER SWTG HEARNESS FOR SENSOR SWAP 9F21895-501
    VU121 R05 EIS PFD F/O SWTG --------------------------------------------------------------------------------------------------
    VU121 R06 EIS ND F/O SWTG Operational Test of the Probe Ice Protection
    VU121 R10 ECAM DU LOWER SWTG AMM 30-31-00-710-001
    -------------------------------------------------------------------------------------------------- Operational Test of the Windshield Anti-Icing and Defogging
    Operational Test of the Digital Flight Data Recorder AMM 30-42-00-710-001
    (DFDR) AMM 31-33-00-710-007 --------------------------------------------------------------------------------------------------
    Servicing of the printer AMM 31-35-22-600 ATA 31 Fault
    Paper P/N 8050917-002 31 ADIRU 1, 2 & 3 FAULT
    DMU-Dat Management Unit P/N ED45A300 VU49 F6 ADIRU 1 115VAC (SYS1)
    Test of the DMU AMM 31-36-00-710-001 VU105 C2 ADIRS ADIRU1 28VDC (SYS1)
    Bite Test of the CFDIU AMM 31-32-00-740-002 VU121 N7 ADIRU 2 115 VAC (SYS2)
    54 52
    31 CLOCK Brake MLG – Removal/ Installation AMM.32-42-27
    Reset MAIN BRAKE
    VU121 J18 CFDS/CFDIU/SPLY Torque 175/180 Lbf-Ft Direct
    -------------------------------------------------------------------------------------------------- Torque 125 Lbf-Ft With adapter.
    31 Loss of the CAPT ND Blennding of the Normal Braking at the Brake units
    VU49 E01 - VU49 E02 – VU49 E10 AMM 32-42-00-870-001
    VU49 E07 - VU49 E11 Blennding of the High Pressure Alternate Braking system.
    -------------------------------------------------------------------------------------------------- AMM 32-43-00-870-002
    31 Loss of the first Officer ND Nitrogen Filing of the Yelow Hidraulic System Brake
    VU121 R04 – VU121 R06 Pressure Accumulator. AMM 12-14-32-614-002
    VU121 Q08 – VU49 E07 BMTU – Brake Temperature Monitoring Unit
    -------------------------------------------------------------------------------------------------- P/N 35-1H5-1002
    31 Loss of the CAP PFD Bite Test of the BSCU AMM 32-46-00-740-001
    VU49 E3 – VU49 E04 – VU49 E07 Bite Test of the Landing Gear Interface Unit (LGIU)
    VU49 E10 – VU49 E11 AMM 32-69-00-740-001
    -------------------------------------------------------------------------------------------------- NGL Door Pin P/N 98D32203502000
    31 Loss of the First Officer PFD AMM 32-22-00-010
    VU121 R03 – VU121 R05 --------------------------------------------------------------------------------------------------
    VU121 Q09 – VU49 E07 ATA 32 Fault
    -------------------------------------------------------------------------------------------------- 33 APU AREA LIGHTS INOP
    31 Display Management Computer (DMC) VU2001 F06 APU SVC LIGHT
    DMC1 – VU49 E11, VU49 E09 --------------------------------------------------------------------------------------------------
    DMC2 – VU121 Q08, VU121 R08 33 CABIN LIGHT REMAINS ON BRIGHT
    DMC3 – VU49 E07, VU121 Q09 WHEN SELECTED OFF or DIM
    -------------------------------------------------------------------------------------------------- Check thru the PTP for failed DEU and reset DEU if possible.
    NOTE: Light controled by failed DEU will remain in bright
    ATA 32 Fault IF NO HELP
    32 BSCU FAULTS VU121 M08 THRU M13
    If A/C not moving turn nose wheel steering --------------------------------------------------------------------------------------------------
    ANTI-SKID OFF then ON. 33 CABIN LIGHT STRUK IN BRIGHT
    IF NO HELP Reset#2 CIDS through MCDU
    See BSCU FAULTS 1 & 2 IF NO HELP
    -------------------------------------------------------------------------------------------------- A320
    32 BSCU FAULTS SYSTEM #1 VU121 M14 CIDS FWD ATTND/PNL
    VU121 M33 BRK & STEERING SYS 1 IND & SPLY A319
    VU121 M34 BRK & STEERING SYS 1 CTL VU121 Q14 CIDS FWD ATTND/PNL
    -------------------------------------------------------------------------------------------------- --------------------------------------------------------------------------------------------------
    32 BSCU FAULTS SYSTEM #2 33 NO LIGHT IN MLG WHEEL AREAS
    VU121 M35 BRK & STEERING SYS 2 CTL VU2001 F5 LIGHTS SEC 19
    VU121 M36 BRK & STEERING SYS 2 SPLY --------------------------------------------------------------------------------------------------
    --------------------------------------------------------------------------------------------------
    55 57

    VU121 M18 FAC 2 26VAC Bleed Pressure- Regulator Valve (4001HA)


    VU121 M18 FAC 2 28VDC AMM 36-11-52=400-010 Removal / InstalLation
    -------------------------------------------------------------------------------------------------- IPC 36-11-52-80-030 Seal P/N NK 103102-0400
    NAV-ILS2 FAULT Reset K09
    NAV-GPS2 FAULT Reset K09 High Pressure Bleed Valve (4000HA)
    NAV-PRED W/S DET Reset K13 AMM 36-11-51-400-010 Removal / InstalLation
    -------------------------------------------------------------------------------------------------- IPC 36-11-51-80-030 Seal P/N NK 103102-0400
    Test of the Angle Of Attack (AOA) Warming AMM 34-10-00-710 --------------------------------------------------------------------------------------------------
    Bite Test of the ILS (A319 MMR) AMM 34-36-00-740 AIR BLEED Maintenance Message
    Bite Test of the Weather Radar AMM 34-41-00-740 Reset 49VU-F01, 121VU-Q07
    Bite Test of the Radio Altimeter AMM 34-42-00-740 TSM 36-00-00-810-802
    Bite Test of the TCAS AMM 34-43-00-740 --------------------------------------------------------------------------------------------------
    Operational Test of the GPWS Ground Self – Test ATA38 Fault
    Function AMM 34-48-00-710 38 GALLEY WATTER SYS NOISE
    Bite Test of the DME AMM 34-51-00-740 Removed aft galley rigth hand coffe maker and plug sump
    Bite Test of the ATC AMM 34-52-00-740 drain tube. This will reset the check valve. Remove plug and reinstall
    Bite Test of the ADF AMM 34-53-00-740 coffee maker
    Bite Test of the VOR/MKR AMM 34-55-00-740 --------------------------------------------------------------------------------------------------
    -------------------------------------------------------------------------------------------------- 38 LOSS OF WATER QUANTITY
    ATA35 FAULT VU2000 D3 WATER SYSTEM
    35 O2 LOW REG PRESSURE MSG --------------------------------------------------------------------------------------------------
    Check crewO2 suplly switch is ON 38 TOILET WILL NOT FLUSH
    -------------------------------------------------------------------------------------------------- make sure aft service painel door closed
    Crew Oxygen Storage Cylinder P/N 801307-04 VU2001 B01 VAC TOILET SYS LAV PWR
    Removal AMM 35-11-41-000-001 VU2001 B04 VAC TOILET SYS LAV PWR
    Installation AMM 35-11-41-400-001 A320 ONLY
    Leak Test AMM 35-11-41-790 VU2001 B3 VAC TOILET SYS LAV PWR
    Seal Conical P/N NSA835070-5C IPC.35-12-01 IF NO HELP ALSO RESET THESE
    Oxygen Door Manual Release Tool P/N 9955000 VU2001 B06 VACUUM TOILET SYS
    IPC.35-32-09 VACUUM SYSTEM.
    Portable Oxygen Cilinder AMM 35-32-42 VU2001 B07 VACUUM TOILET SYS
    VACUUM GEN
    Protective Breating Equipment (Smoke Hoods) --------------------------------------------------------------------------------------------------
    PBE AMM 35-32-52 Faucet Assy Water P/N 2980132100000
    -------------------------------------------------------------------------------------------------- IPC 38-12-41
    ATA36 Fault Wast Water Drain IPC 38-32-01
    36 AIR L (R) WING BLEED LEAK MSG Drain Assy IPC 38-32-42
    AFTER ELETRICAL TRANSIENTS -Sieve P/N 7700525 IPC 38-32-42-02c-070
    Reset affected bleed push button msg -Packing P/N 7750041-013
    IF NO HELP
    59 61
    33 CABIN LIGHTS WILL NOT TURN ON 32 HOT BRAKE or BRAKE TEMP
    VU121 M14 CIDSS FWD ATTND/PNL DIFFERENCES REPORTED BY CREWS
    -------------------------------------------------------------------------------------------------- See TASK AMM 05-51-16-200-001
    Operational Test of the annunciator ligth test system in the cockpit NOTE: HOT BRAKE ECAM MSG ABOVE 300 ºC
    AMM 33-14-00-710-001 A) 1 Temp diff between 2 brakes on same Truck of 150 deg. C,
    Box Install-Spare Lamp-Fuse IPC.33-12-01 AND
    Photo Luminescent strips PL22-412LHH055 2 Temp. of 1 brake at or above 600 deg.C
    Carpet Protector PL22-405LH00 OR
    End Cap PL22-422LH055 3 Temp. of 1 brake at or below 20 deg. C
    IPC.33-51-09-50H-10A B) Temp. diff between LH and RH trucks average brake temp. of
    -------------------------------------------------------------------------------------------------- 200 deg. C
    ATA34 FAULT --------------------------------------------------------------------------------------------------
    34 DAR MSG 32 LGCIU FAULTS SYSTEM #1
    VU121 K5 DMU &QAR NOTE: CARGO DOOR PROX SWITCHES MAY CAUSE FAULT
    VU121 K17 FDIU &QAR VU49 C9 L/G LGCIU SYS 1
    VU121 K18 ACCLRM VU121 Q34 HYD LGCIU SYS 1 GND SPLY
    NOTE: May be relatede to diskette being AFULL --------------------------------------------------------------------------------------------------
    diskette P/N VBR3H1 32 LGCIU FAULTS SYSTEM #2
    diskette Maller P/N S2-18-274 NOTE: CARGO DOOR PROX SWITCHES MAY CAUSE FAULT
    -------------------------------------------------------------------------------------------------- VU121 Q35 HYD LGCIU SYS 2
    34 FLT REC MSG --------------------------------------------------------------------------------------------------
    or FLT RECORDER PROBLEM IM FLIGHT 32 NO BRAKE TEMPS DISPLAYED
    VU121 K17 FCDR&QAR VU121 M37 BRK TEMP DET UNIT
    -------------------------------------------------------------------------------------------------- --------------------------------------------------------------------------------------------------
    34 GPWS FAULTS 32 NOSE WHEEL STEER FAULT
    VU121 P6 GPWS 28VDC With A/C not moving turn nose wheel
    VU121 P7 EIS GPWS 115VAC steering and anti-skid OFF then ON
    -------------------------------------------------------------------------------------------------- --------------------------------------------------------------------------------------------------
    34 RAD-NAV PAGE IS NOT ACCEPTING DATA Wheels/Tires Inspection / Check AMM 31-41-00-210-002
    Reset RMP NAV SWITCH'S Brake Inspection / Check AMM 32-42-27-210-006
    -------------------------------------------------------------------------------------------------- Wheel – NLG Removal / Installation AMM 32-41-12
    34 TCAS IN STANDY BY MODE
    NOTE: Verify TCAS is not selected in standy-by. NOSE WHEEL Torque 160/0/80 Lbf-Ft.
    VU121 K10 TCAS Tool Protector NLG P/N J47548
    -------------------------------------------------------------------------------------------------- Adapter NLG P/N J47549
    34 WINDSHEAR DET FAULT Wheel- MGL Removal / Installation AMM 32-41-11-000-006
    NOTE: Msg on ground system may not be at fault
    Reset FACS push button switch's first MAIN WHEEL Torque 300/150 Lbf-Ft.
    IF NO HELP Tool Protector MLG P/N F46754-100
    VU49 B03 FAC 1 26VAC Adaptor MLG P/N H47682
    VU49 B04 FAC 1 26VDC Disassembly Tool P/N Mg174-04
    58 56

    ATA49 Fault VU49 D11 AIR BLEED ENG 1 MONG (BMC1)


    49 APU BLEED FAULTS VU49 D12 AIR BLEED ENG 1 CTL
    NOTE: Shut down APU before reseting CB's --------------------------------------------------------------------------------------------------
    VU121 L41 ECB SPLY 36 BMC
    VU121 L42 APU CTL BMC# 1
    -------------------------------------------------------------------------------------------------- VU49 D11 AIR BLEED ENG 1 MONG (BMC1)
    49 APU ELEC NO VOLTS or FREQS VU49 D12 AIR BLEED ENG 1 CTL
    Select APU elect OFF and reset to ON BMC# 2
    IF NO HELP VU122 Z22 AIR BLEED ENG 2 MONG (BMC2)
    VU122 Y25 ELEC APU GCU VU122 Z23 AIR BLEED ENG 2 CTL
    -------------------------------------------------------------------------------------------------- FOR DUAL BMC FAULT RESET
    49 APU WILL NOT SHUT DOWN VU49 D11 AIR BLEED ENG 1 MONG (BMC1)
    VU121 L42 APU/CTL VU122 Z22 AIR BLEED ENG 2 MONG (BMC2)
    IF NO HELP --------------------------------------------------------------------------------------------------
    VU121 L41 APU/ECB/SPLY 36 CROSS BLEED FAULTS
    -------------------------------------------------------------------------------------------------- ALSO XFEED VALVE FAULTS MSG
    Operational Test of the APU Fuel-Pump System on ground to purge the VU49 D11 AIR BLEED ENG1 MONG (BMC1)
    fuel line AMM 28-22-00-710 VU49 D12 AIR BLEED ENG1 CTL
    FUEL FILTER (8028KM) AMM 49-32-41-920-001 VU122 Z22 AIR BLEED ENG2 MONG (BMC2)
    Packing-Preformed P/N S9412-218 VU122 Z22 AIR BLEED ENG2 CTL
    Element-Strainer P/N 3882496-1/ 2685336 VU49 F4 SDAC 1 SPLY
    Packing-Preformed P/N S9412-036 VU121 Q6 SDAC 2 SPLY
    OIL FILTER Module Lube (8069KM) and (80676KM) --------------------------------------------------------------------------------------------------
    AMM 49-91-41-200-002 IPC 49-91-45-70 36 CROSS BLEED VALVE MSG
    Filter Element Oil P/N 3880938-1 VU49 D13 AIR BLEED XFEED VALVE BAT
    Packing-Preformed P/N M83248-1-227 VU122 Z20 AIR BLEED XFEED VALVE NORM
    --------------------------------------------------------------------------------------------------
    ATA73 Fault 36 LEFT WING LEAK MSG
    73 ENG 1 (2) EPR MODE FAULT MSG VU49 D11 AIR BLEED ENG1 MONG (BMC1)
    NOTE: Recovery of EPR on both engines may be VU49 D12 AIR BLEED ENG1 CTL
    attempted by switching OFF each engine's --------------------------------------------------------------------------------------------------
    N1 mode switch 36 RIGTH WING LEAK MSG
    -------------------------------------------------------------------------------------------------- VU122 Z22 AIR BLEED ENG2 MONG (BMC2)
    73 ENG 1 (2) EIU FAULT VU122 Z23 AIR BLEED ENG2 CTL
    Turn FADEC push button switch ON then OFF to reset FADEC --------------------------------------------------------------------------------------------------
    IF NO HELP 36 AIR-APU BLEED LEAK MSG
    VU49 A4 ENG 1 FADEC A & EIU1 Reset APU bleed push button switch
    VU121 R41 ENG 1 FADEC A & EIU1 ON or OFF to ON to cler msg.
    VU49 A5 ENG 2 FADEC A & EIU2 --------------------------------------------------------------------------------------------------
    VU121 Q40 ENG 1 FADEC A& EIU2 Bite test of the BMC 1 (2) AMM 36-11-00-740-001
    62 60
    73 ENG 1 (2) FADEC AIDS REPORT ACRONYM MEANING LIST
    ENG 1 (2) FADEC A or B FAULT
    Turn FADEC push button switch ON then OFF to reset FADEC ACRNM MEANING
    IF NO HELP 2ENN EEC DISC EGT PEAK
    VU49 A04 ENG 1 FADEC A & EIU 1 ABV APU BLEED VLV
    VU121 R41 ENG 1 FADEC B & EIU 1 ACT TKO ACCEL TIME
    VU49 A05 ENG 2 FADEC A & EIU 2 ACYC APU CYCLE
    VU121 Q40 ENG 2 FADEC B & EIU 2 AHRS APU TIME
    -------------------------------------------------------------------------------------------------- AILP AILERON POS
    Operational Test of the FADEC System on the ground ALT ALTITUDE
    AMM 73-22-00-710 AOC AIR OIL COOLER VLV
    Operational Test of the Trusth Reverse System with the CFDS AT AUTOTHRUST
    AMM 78-31-00-710 ATO ABORTED TAKEOFF
    Operational Test of the Ignition System with BBV BROADBAND VIB
    the CFDS AMM 74-00-00-710-041 BNNN BMC DISCRETE WORDS
    Operational Test of the Pneumatic Start Valve with BVA 2.5 BLD VLV POS
    the CFDS AMM 80-13-51-710-040 CAOA ANGLE OF ATTACK
    Operational Test of the P2/T2 Probe Heater with CAS AIR SPEED
    the CFDS AMM 73-22-11-710-040 CG CENTER OG / F GRAVITY
    -------------------------------------------------------------------------------------------------- CNT REPORT
    ATA79 Fault CODE CONDITION
    79 ENG 1 (2) AIR EXCHANGE FAULT CRZ CRUISE REPORT
    Shut down Engine CV XFEED VALVE (1=OPEN)
    Cycle eng FADEC GND power push button DATE GMT DATE
    Restart engine DMU / SW DMU SOFTWARE VERSION
    -------------------------------------------------------------------------------------------------- DPFV DUCT PR @ FUEL VLV ON
    79 ENG 1 (2) OIL FILTER CLOG DPSV DUCT PR @ STRT VLV ON
    NOTE: No action required if oil is 10 to 32 Deg ºC and msg. EEC CHANNEL IN CONTROL
    goes out. EFT ENG FUEL TEMP
    All other times - maintenance action required EGT INDICATE EG
    -------------------------------------------------------------------------------------------------- AGTK TEMP CORRECTED EGT
    Engine Operational Limites, Guidelines and Special Procedures EGTM TKO EGT MARGIN
    AMM 71-00-00-860-010 EGTP PEEK EGT @ TKO
    Ground Test Requirements after Power Plant/ Module/ Component EI ENG ANTTI-ICE (1=ON)
    repair or replacement EI2 ENG ANTI-ICE @ EGT PK
    Procedures ELE ENG LIMIT EXCEEDANCE
    AMM 71-00-00-710-017 ELEV ELEVATOR
    Test No.1 Dry Motor Leak Check AMM 71-00-00-710-045 ENNN EEC DISCRETE WORDS
    Test No.2 Wet Motor Leak Check AMM 71-00-00-710-046 EPR EPR ACTUAL
    Test No.3 Idle Leak Check AMM 71-00-00-710-012 EPRC COMMAND APR
    Test No.4 Oil Sys Static Leak Check AMM 71-00-00-790-010 EPRM MAX AVAIL EPR
    63 65

    P12.5 FAN EXIT PRESS TLD15-25


    P2 FAN IN PRESSURE L15W25 ó L15-25
    P2.5 LPC EXIT PRESS Pax call lamp P/N 6839
    P5 LPT EXIT PRESS Window & Ceilling-long ABS0201-07G 33-21-09-401
    PA2 PACK VALVE EGT PEAK TLD30W25
    PAMB AMBIENT PRESS Window & Ceiling-short ABS0201-06G 33-21-09-401
    PAR EXCEEDANCE PARAMETER Map light (981/991 ABS0073-313 33-21-01-401
    PB HPC EXIT PRESS Map light (951/941) E0429-01 33-12-12-401
    PB10 10STG PRESS
    PCIP PRE-COOL IN PRESS --------------------------------------------------------------------------------------------------
    PCCP PRE-COOL OUT TEMP Emergency Equipment
    PCOT PRE-COOL OUT TEMP Cabin Escape Facilities AMM 25-62-00
    PEAK PEAK VALUE EXC PARM Escape slide Fwd, L (7500MM) AMM 25-62-44
    PF PACK AIR FLOW Escape slide Fwd, R (7501MM) AMM 25-62-44
    PF2 PACK AIR FLOW @ EGT PK Escape slide aft. L (7502MM) AMM 25-62-44
    PH FLIGHT PHASE Escape slide aft. R. (7503MM) AMM 25-62-44
    PRV PR ENG VALUE (1=OPEN) Escape slide of wing L. (7504MM) AMM 25-62-42
    PV PACK VALVE (1=OPEN) Escape slide off wing R. (7505MM) AMM 25-62-42
    PV2 PV POSS @ EGT PK Reservoir Assy OWS. L. (7506MM) AMM 25-62-46
    ROLL ROLL Reservoir Assy OWS. R (7507MM) AMM 25-62-46
    RPOS REVERSER POS
    RS2P ROLL SPOILER 2 Evacuation Signaling Equipment-WP AMM 25-63-00
    RS3P ROLL SPOILER 3 Miscellaneous Emergency Equipment. AMM 25-63-00
    RS4P ROLL SPOILER 4 Flash Lights, Crash Axe
    RS5P ROLL SPOILER 5 PBE AMM 35-32-52
    RTR RUDDER TRIM Emergency Locator Transmitter (ELT)
    RUD RUDDER Megaphone AMM 25-65-51
    SAT STATIC AIR TEMP First Aid Kit AMM25-64-00
    SLAP SLAP POSITION Emergency Medical Kit
    SOP #4 BRG SCAV OIL PRESS
    SSA SIDE SLIP ANGLE Floatation and Survival Equipment AMM 25-66-00
    STAB STABILIZER Life Verst, Demo (7582MM)
    STL ENG STALL REPORT Life Vest, Flight Crew (7583MM)
    STR ENG START REPORT Life Vest, Cabin Crew (7584MM)
    SVA STATOR VANE ACTUATOR Life Vest, Pax Schwimmweste (7580MM)
    SVC SCAV VLV FAIL CLOSED Life Line (7710MM)
    SVF SPILL VLV FEEDBACK Survival Kit (7518MM)
    SVFV TIME TO FUEL VLV ON Lift Raft (7519MM)
    SVN2 TIME TO START VLV43% N2 Captain / First Officer Emergency Descent Device
    SVO SCAV VLV FAIL OPEN AMM 25-61-41-000-01
    T2 FAN INLET TEMP
    67 69
    APRT TKO EPR FROM FMC Test No.6 EEC System Idle test AMM 71-00-00-710-022
    FAV FAN SIR VALVE (1=OPEN) Test No.8 Vibration Survey AMM 71-00-00-700-022
    FCT FLIGTH COUNTER Test No.9 - Low Pressure (LP) Compressor (FAN) Trim
    FF FUEL FLOW Balancing-one shot Method
    FFR FUEL FLOW REQUEST - LP Compressor (FAN) Trim Balancing-Trial
    FLAP FLAP POSITION Weight Method
    FLO FLAMEOUT REPORT AMM 71-00-00-700-012
    FLT FLIGHT # Test No.11 High Power Assurance Test AMM 71-00-00-710-013
    FPA FLIGHT PATH ACCEL Test No.13 Pretested Replacement Engine Test.
    FROM DEPARTURE STATION AMM 71-00-00-700-011
    FTM TANK FUEL TEMP Test No.5, No.7, No.10 and No.12 are RESERVED
    FTT FLEX TAKEOFF TEMP Work Mat P/N 2971124
    FVEGT FUEL VLV ON EGT RISE
    GW GROSS WEIGHT TOOL LIST
    HCCA TURBINE CASE COOL VLV STA LOCK WASHER and NUT KIT 1SF5049-101
    HPV HIGH PR VLV (1=OPEN) 3SF6391-101
    ICFQ WING IN CELL FUEL QTY “Y' CONNECTOR FOR AIR START 0007-0394
    IFE INFLIGHT SHUTDOWN STEERING BYPASS PIN D23156000
    IOT IDG OIL TEMP GEARS PINS: NOSE AST10A202
    IVV VERTICAL SPEED MAIN's 460005833
    LAT LATITUDE BULB SEAL ROLLER KIT 98A25207503000
    LIM LIMIT VALUE EXCEEDED HARNESS FOR SENSOR SWAP 9F21895-501
    LONG LONGITUDE VIDEO SCREEN REMOTE CONTROL RD-AV9510
    MN MACH NUMBER HYDRAULIC SERVICE ADAPTER 3SF6428-501
    N1 LP ROTOR SPEED LAF SERVICE EXTENSION 7381
    N1CP FAN VIB PHASE ANGLE
    N1DI FAN VIB-MILS ALTERNATE BRAKE SYSTEM FILL / BLEED
    N1K TEMP CORRECTED N1 ADAPTER 3SF6472-501
    N2 HP RPTOR SPEED Lead Bonding P/N E0092-10-160NN
    N2C CORRECTED NS FOR SVA
    N2D HP ACCELERATION QUAD ¼” HEX BITS
    N2DOT1 HP ACCEL FOR ACT 170-5
    N2DOT2 HP ACCEL FOR ACT 212-1/4
    N2K TEMP CORRECTED N2 212-5/16A
    N2P PAK N2 RPM 212-4
    NACT NACELLE TEMP 212-6
    OF OIL FILTER CLOG (CLOG=0) 212-8
    OIP OIL PRESSURE 212-10
    OIQ OIL QUANTITY
    OIT OIL TEMP DEPTH MICROMETER P/N 449AZ-6R (7GBA)
    OPV OVERPR VLV (1=OPEN)
    66 64

    IDG – INTEGRATED DRIVE GENERATOR T2.5 LPC EXIT TEMP


    IPC 24-21-51-81-170 T3 HPC EXIT TEMP
    Element -Filter P/N 5909812 TAT TOTAL AIR TEMP
    Packing-Preformed P/N M83248-1-214 TEPR EPR TARGET FMC
    Packing-Preformed P/N M83248-1-226 THDG TRUE HEADING
    Packing-Preformed P/N M83248-1-905 TKO TAKE OFF REPORT
    TO DESTINATION STATION
    FILTER ELEMENT INSTL-SCAVENGE OIL V2500 TODR TKO REDUCE THRUST
    IPC 79-22-44-80-70 TOVL1 TIME OVER LIMIT 1
    Element-Oil Filter P/N QA05654 / TOVL2 TIME OVER LIMIT 2
    CA00080A TOVL3 TIME OVER LIMIT 3
    Packing-Preformed P/N AS3208-08 TRA THROTTLE ANGLE
    Packing-Preformed P/N AS3208-153 UEGT MEASURE EGT
    UEGT2 MESA EGT @ EGT PK
    DETECTOR – MAGNETIC CHIP UTC GMT TIME
    (IAE) 79-22-45-400-010 Removal/Installation VIBC1 FAN VIB-UNITS
    IPC 79-22-45-80-60 Seal P/N 44066 VIBC2 N2 VIB-UNITS
    VIBC2P PEAK N2 VIB AT START
    STARTER INST – V2500 VNNN EVMU DISCRETE WORD
    IPC 80-13-41-80 WDIR WIND DIRECTION
    Packing Chip Detector P/N NAS1595-2 W1 WING ANTI-ICE (1=ON)
    Packing Preformed-Plug Drain P/N 720752-10 W12 WING ANTI-ICE @ EGT PK
    Ring Sealing – Plug P/N 720752-74 WSSP WIND SPEED
    YAW YAW
    For 1000EM1 (437AL, 438AR) --------------------------------------------------------------------------------------------------
    For 1000EM2 (447AL, 448AR) Position P/N AMM
    Landing Light Q4559 33-42-11-400
    Cockpit grid collector assy strainer P/N SF01381 Take-off light Q4559 33-46-11-400
    Cyllinder-Door Damper Diaphragm-Sealing Taxi light Q4554 33-46-12-000
    IPC 52-11-14-01B P/N FE240-221-001 Runway Turn-off GE4626 33-43-11-000
    Sellos de Plomo P/N 2013T11 Wing Scan Lighting MS25243-4594 33-49-11-000
    Pasadores - Cotter Pin 1/16” of Steel MS24665-155 Logo light GE4626 33-47-11-000
    Cotter Pin 3/32” of Steel MS24665-304 Lens Green 29120B2140089Z 33-41-11-000
    Cotter Pin 1/8” of Steel MS24665-370 Lens Red 29130B2140090L 33-41-11-000
    Cotter Pin 5/32” of Steel MS24665-443 Navigation W/Tip 29100A2140054K 33-41-11-000
    Cable tie wrap P/N NSA935401-05 Navigation Tail 8GH005597-12 33-41-15-000
    Cargo Comp. ABS0201-06E 33-34-00-000
    Cargo Loading Area MS25235-3011 33-34-12-400
    -------------------------------------------------------------------------------------------------- Dome Light NSA933239-2232 33-35-11-400
    Lav Sign Red/ Green 128-481/482 33-26-23-000
    Lav fluorescent ABS0201-06G 33-24-01-000
    70 68
    CONVERSÕES 05-59-32 - Ferry Flight with Gear Down
    --------------------------------------------------------------------------------------------------
    LIBRAS KILOGRAMAS
    Lbs = 2.2046 X Kg Kgs = 0.4536 X Lbs ZONING MM 06-20-00-001
    Lbs = Gals X 6.6 Kgs = Gals X 3.02 100 Lower half of the fuselage to aft. Press bulkhead
    Gals = Lbs Gals = Kgs 200 Upper half of the fuselage to aft. Press. Bulkhead
    6.6 3.028 300 Stabilizers
    400 Nacelles
    Gals = 0.264 X Litros Litros = 3.49 X Gals 500 Left wing
    600 Right wing
    1 Galão (USA) = 4 qt = 8 pints = 3.78 liters 700 Landing Gear
    1 qt = 0,945 liter
    800 Doors.
    Temperatura
    º C = º F-32 in. HG = Inch of Mercury
    5 9 h.Pa = Hecto Pascal

    Mach Number
    Means the ratio of true speed to the speed of sound

    Speed of Sound
    Sounds travels in air under standard atmosphere conditions at a rate
    of 760 miles per hour, 340 meters for second or 1,116 feet per second

    Torque
    1Lb / ft = 12 Lbs / in
    --------------------------------------------------------------------------------------------------
    ATA 5
    A – Unscheduled Inspection Listed on Maintenance Manual Chapter
    05-50
    05-50-00-360-050
    A – Measurement of Leaks
    1 - Measurement of Hydraulic System Leaks
    AMM 29-00-00-790-001
    2 - Measurement of Flight Control System Leaks
    AMM 29-00-00-790-001
    3 - Measurement of Fuel System Leaks
    AMM 28-11-00-280-002
    4 - Measurement of Landing Gear System Leaks
    AMM 29-00-00-790-001
    5 - Measurement of Cargo System Leaks
    71 73

    75 77
    AMM 29-00-00-790-001
    74
    6 - Measurement of Power Plant System Leaks
    AMM 71-70-00-600-010
    --------------------------------------------------------------------------------------------------
    05-51 - INSPECTIONS

    05-51-11 - Inspection after Hard/Overweight landing


    05-51-12 - Inspection after Landing Gear down Limiting Speed
    exceeded
    05-51-13 - Inspection after Flap/Slat Limiting Speed exceeded
    05-51-14 - Inspection after Flap/Slat Limiting Speed exceeded
    05-51-15 - Inspection after a Tire Burst or Thread trow or Failure
    05-51-16 - Inspection after Brabe Emergency Application or Overheat
    05-51-17 - Inspection after Flight in excessive turbulence or excess of
    VMO/MMO
    05-51-18 - Inspection after Lightning Strike
    05-51-19 - Inspection after Engine Bird Strike or Slush Ingestion
    05-51-21 - Inspection after Tail Runway Impact
    05-51-22 - Inspection after NLG Towing Overload or Overrun
    05-51-23 - Inspection after NLG Steering Angle Exceeded
    05-51-24 - Inspection after Leaving Runway or Taxiway
    05-51-25 - Inspection after flight through Dust Storm/Volcanic Ash or
    several conditions on Ground.
    05-51-26 - Inspection after engine failure
    05-51-27 - Inspection after impact on Engine Cowls
    05-51-28 - Procedure after fluid Spillage
    05-51-29 - Inspection after Abnormal Pax/Crew door movement
    05-51-31 - Inspection after significant MLG Vibration at Touch-Down
    05-51-34 - Inspection after Engine Windmilling (After engine in-flight
    shutdown)
    05-51-41 - Inspection after overweight taxiing
    05-51-42 - Inspection after work on System Electrical Installation
    --------------------------------------------------------------------------------------------------

    05-53 – Pressurization Test of Fuselage (leakage checks) after A/C


    abnormal operation or repair
    05-54 – Demagnetization
    05-56 – Leveling and Measurament after A/C abnormal operation
    05-57 – Aircraft Stability
    05-59 – Non-Revenue Flight-Requirement Following Maintenance
    actions.
    72

    78 76

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