A319 & 320 Fault Verification Guide

BSBMW PISTACCIIRRCCUUIITT BBRREEAAKKEERR AA331199//332200

RREEFF AAMMMM 2244--5500--0000--000011

Note

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CCIIRRCCUUIITT BBRREEAAKKEERR AA331199//332200 CCIIRRCCUUIITT BBRREEAAKKEERR AA331199//332200PPAANNEELL DDEESSIIGGNNAATTIIOONN LLOOCC PPAANNEELL DDEESSIIGGNNAATTIIOONN LLOOCC

AAIIRR CCOONNDDIITTIIOONNIINNGG SSYYSSTTEEMM 122VU AIR COND/FLOW/MIXER/FLAP V22

122VU AIR COND/FLOW/CTL & IND 2 V21

49VU AIR COND/RAM/AIR/INLET D10

49VU AIR COND/CAB/PRESS CTL 1 D09 123VU AVNCS VENT/BLOWER FAN AD10

49VU AIR COND/AVNCS VENT/CTL D06 123VU AVNCS VENT/EXTC FAN AE02

49VU AIR COND/FLOW/CTL & IND 1 D07

49VU AIR COND/AVNCS VENT CTL D05 AAUUTTOO FFLLIIGGHHTT

122VU AIRCO/LAV/GALL VENT CTL EXTR. FAN CTL U21 122VU AIRCO/LAV/GALL VENT CTL EXTR. FAN SPLY U19 49VU AUTO FLIGHT/FCU 1 B05

122VU AIR COND/ZONE TEMP CTL/28VDC/SYS 2 V20 49VU AUTO FLIGHT/FAC 1/28 VDC B04

122VU AIR COND/ZONE TEMP CTL/28VDC/SYS 1 V19 49VU AUTO FLIGHT/FAC 1/26 VAC B03

122VU AIR COND/ZONE TEMP CTL/115VAC/SYS 2 V18 49VU AUTO FLIGHT/FMGC/1 B02

122VU AIR COND/ZONE TEMP CTL/115VAC/SYS 1 V17 49VU AUTO FLIGHT/MCDU/1 B01

122VU AIR COND/PACK TEMP/CTL SYS1/2/115VAC W22

122VU AIR COND/PACK TEMP/CTL SYS1/2/28VDC W21 121VU AUTO FLIGHT/FCU 2 M21

122VU AIR COND/RECIRC FAN/R/CTL W20 121VU AUTO FLIGHT/RUDDER/TRIM/IND M20

122VU AIR COND/RECIRC FAN/R/SPLY W18 121VU AUTO FLIGHT/FAC 2/ 28 VDC M19

122VU AIR COND/PACK TEMP/CTL SYS 1/115VAC X22 121VU AUTO FLIGHT/FAC 2/ 26 VAC M18

122VU AIR COND/PACK TEMP/CTL SYS 1/28VDC X21 121VU AUTO FLIGHT/FMGC 2 M17

122VU AIR COND/RECIRC FAN/L/CTL X20 121VU AUTO FLIGHT/MCDU 2 N20

122VU AIR COND/RECIRC FAN/L/SPLY X18 121VU AUTO FLIGHT/RUDDER/ARTF/FEEL N17

122VU AIR COND CABIN PRESS./CTL/MAN Y23 121VU AUTO FLIGHT/STICK//LOCK N16

122VU AIR COND/CABIN PRESS./CTL 2 Y22

122VU AIR COND/PACK TEMP CTL SYS 2/2/28VDC Y21 CCOOMMMMUUNNIICCAATTIIOONN122VU AIR COND/PACK TEMP CTL SYS 2/2/115VAC Y20

122VU AIR COND/PACK TEMP CTL SYS 2/1/28VDC Y19 49VU COM/CVR/SPLY E14

122VU AIR COND/PACK TEMP CTL SYS 2/1/115VAC Y18 49VU COM/CVR/CTL E13

122VU AIR COND/AVNCS/VENT/MONG Y17 49VU COM/RMP 1 G10


49VU COM/VHF 1 G09 121VU COM NAV/CIDS/DEU A NORM/R MID MZA/MZF M12

49VU COM/ÁUDIO/FLT/INTPH G08 121VU COM NAV/CIDS/DEU A NORM/L MID MZA/MZF M11

49VU COM/AUDIO/ACP/F/O G07 121VU COM NAV/CIDS/DEU A NORM/R FWD MZA/MZF M10

49VU COM/AUDIO/ACP/CAPT G06 121VU COM NAV/CIDS/DEU A NORM/L FWD MZA/MZF M09

49VU COM/CIDS/DEU A ESS/LINE 2 G05 121VU COM NAV/CIDS/DEU B/NORM MZA/MZF M08

49VU COM/CIDS/DEU A ESS/LINE 1 G04 121VU COM NAV/CIDS/PROG &/TST PNL MZA/MZF M07

49VU COM/CIDS DEU B/ESS G03 121VU COM NAV/CIDS/DIR NORM 2 MZA/MZF M06

49VU COM/CIDS/DIR 1 AND 2 ESS MZG G02 121VU COM NAV/CIDS/DIR NORM 1 MZA/MZF M05

49VU COM DIR ESS 2 PT-MZA/MZF G02 121VU COM/CIDS/FWD ATTND/PNL MZA/MZF Q14

49VU COM DIR ESS 1 PT-MZA/MZF G01 121VU SATCOM MZG/MZJ K01

49VU COM HF 1 HA14 121VU COM NAV/CIDS/FWD ATTND/PNL MZG/MZJ Q14

121VU COM NAV/RMP 3 L03

121VU COM NAV/VHF 2 L02 121VU COM NAV/VHF 3 L05

121VU COM NAV/CIDS/FWD ATTND/PNL MZG/MZH M14

121VU COM NAV/CIDS/DEU A NORM/R AFT MZG/MZJ M13 EELLEETTRRIICCAALL PPOOWWEERR121VU COM NAV/CIDS/DEU A NORM/L AFT MZG/MZJ M12

121VU COM NAV/CIDS/DEU A NORM/R MID MZG/MZJ M11 49VU ELEC/LT/CTL H10

121VU COM NAV/CIDS/DEU A NORM/L MID MZG/MZJ M10 49VU ELEC/AC BUS/8XP/MONG H11

121VU COM NAV/CIDS/DEU A NORM/R FWD MZG/MZJ M09

121VU COM NAV/CIDS/DEU A NORM/L FWD MZG/MZJ M08 105VU ELEC/CSM/G/EV AUTO/SPLY C01

121VU COM NAV/CIDS/DEU B NORM MZG/MZJ M07 105VU ELEC/HOT BUS/702PP SPLY D02

121VU COM NAV/CIDS/PROG AND TEST PNL MZG/MZJ M06 105VU ELEC/HOT BUS/701PP SPLY D01

121VU COM NAV/CIDS/DIR 1 AND 2/NORM MZG/MZJ M05 105VU ELEC/HOT BUS/702PP SPLY E02

121VU COM NAV/SELCAL M04 105VU ELEC/HOT BUS/701PP SPLY E01

121VU COM NAV/ACP/THIRD/OCCPNT M02 105VU ELEC/ STATIC INV/CNTOR/CTL G02

121VU EIS/HORN/SPLY P09 105VU ELEC/STAT INV/BUS 901XP SPLY H02

121VU COM NAV/CIDS/DEU A NORM/R AFT MZA/MZF M14 105VU ELEC/BAT BUS/REF/BCL 1 AS01

121VU COM NAV/CIDS/DEU A NORM/L AFT MZA/MZF M13 105VU ELEC/BAT BUS/REF/BCL 2 AS01


105VU ELEC/BAT REF/BCL 1 AS01 122VU ELEC/REFLNG/ON/BAT U28

105VU ELEC/BAT REF/BCL 2 AS01 122VU ELEC/CNTOR/DC BUS/TIE 1/FAULT U24

122VU ELEC/AC PWR/SVCE/CTL V29

106VU AC ESS BUS/STBY/CNTOR/CTL B08 122VU ELEC/BUS/2XP/CTL V27

106VU AC ESS BUS/EMER/CNTOR/CTL B07 122VU ELEC/AC/BUS 1/CTL V25

106VU 26VAC/ESS BUS/SPLY B06 122VU ELEC/TR 2/FAULT/DC BUS TIE/CONFIG W30

106VU CSM/G/EV/MAN/SPLY B04 122VU ELEC/TR 1/FAULT/DC BUS TIE/CONFIG W29

106VU AC ESS/BUS NORM/CNTOR/CTL B03 122VU ELEC/CNTOR/ESS/DC BUS/TIE W26

106VU AC ESS/BUS/EMER/CNTOR/SPLY C08 122VU ELEC/CNTOR/DC BUS/TIE W25

106VU EMER/SHED/CNTOR/SPLY C07 122VU ELEC/EXT PWR/LT CLT/AVAIL X31

106VU AC ESS BUS/EMER/STBY/CNTOR/SPLY C06 122VU ELEC/EXT PWR/LT CLT/NOT IN/USE X30

106VU AC ESS BUS/MONG/SPLY C05 122VU ELEC/EXT PWR/CTL X29

106VU AC/SHED/ESS BUS/CNTOR/CTL C04 122VU ELEC/EXT PWR/COCKPIT/AVAIL/LT X28

106VU ESS TR/CNTOR/CTL C02 122VU ELEC/TR 2/MONG X26

106VU ESS TR/SPLY AS01 122VU ELEC/TR 1/MONG X25

122VU ELEC/DC/SVCE/BUS X24

122VU ELEC/GALLEY/CNTOR S28 122VU APU GEN/EGIU 2/28VDC Y31

122VU ELEC/REFLNG/NORM S27 122VU GEN 2/EGIU 2/28VDC Y30

122VU ELEC/GEN 2/OFF/BTC 2 SPLY T31 122VU ELEC/APU/GCU Y25

122VU ELEC/GEN 1/OFF/BTC 2 SPLY T30 122VU ELEC/GPCU Y24

122VU ELEC/GEN 2/OFF/BTC 1 SPLY T29 122VU ELEC/EXT PWR/EGIU 1/28VDC Y31

122VU ELEC/GEN 1/OFF/BTC 1 SPLY T28 122VU ELEC/GEN 1/EGIU 1/28VDC Z30

122VU ELEC/GCU 2 T27 122VU ELEC/EMER AUTO 2 Z26

122VU ELEC/GCU 1 T26 122VU ELEC/EMER GEN AUTO 1 Z25

122VU ELEC/IDG 2/DISC T25 122VU ELEC/DC BUS/TIE 2/APU START W31

122VU ELEC/IDG 1/DISC T24 122VU ELEC/GALY & CAB CTL S26

122VU ELEC/DC SVCE/BUS/ON TR 2 U30 122VU ELEC/GALY & CAB/FAULT/LT CTL S25

122VU ELEC/RFL/SPLY/LOGIC U29 122VU ELEC/GALY & CAB/GND/FLT/LOGIC S24


122VU ELEC/DC SHED BUS/CNTR U26 123VU AFT GALLEY/FEEDER B AD09

122VU ELEC/AC SHED BUS/CNTR U25 123VU MAIN FWD GALLEY/FEEDER C AE10

123VU SHED BUS/218XP/220XP SPLY AC02

123VU GALLEY PWR –E- AE10

123VU APU GEN/EGIU 2/115VAC AA08 124VU SVCE/601PP/602PP/SPLY BB01

123VU EXT PWR/EGIU 1/115VAC AA07 124VU TR 2/CNTOR/SPLY BC01

123VU SVCE/BUS 2/214XP SPLY AA05 124VU DC SVCE/602PP/SPLY BD01

123VU BUS 1/131XP-A/SPLY AB12 124VU 206PP/208PP/SPLY BE01

123VU BUS 1/103XP/SPLY AB11 124VU 204PP/SPLY BF01

123VU TR 1/SPLY AB10 124VU 202PP/SPLY BG01

123VU TR 2/SVCE/BUS 2/SPLY AB08 124VU SHED BUS 210PP/212PP/SPLY BA01

123VU GND/PWR/PROT AB07

123VU SVCE/BUS 2/212XP SPLY AB05 125VU BAT BUS/301PP/SPLY CC01

123VU TR 2/214XP/SPLY AB04 125VU 101PP/SPLY CD01

123VU BUS 2/204XP/SPLY AB02 125VU 103PP/SPLY CE01

123VU BUS 2/213XP-A/SPLY AB01 125VU TR 1/CNTOR/SPLY CF01

123VU AC ESS/BUS ON/BUS 1 AC12

123VU AC ESS/BUS ON/BUS 2 AC01 EEQQ UUIIPPMMEENNTT//FFUURRNNIISSHHIINNGGSS SSYYSSTTEEMM123VU BUS 1/101XP/SPLY AD11

123VU GALLEY D AD04 122VU COCKPIT SEATS/SEAT CTL/F/O U14

123VU BUS 2/212XP/SPLY AD03 122VU COCKPIT SEATS/SEAT CTL/CPT U11

123VU BUS 2/202XP/SPLY AD02 2001VU VACUUM CLEANER SOCKET CARGO Z0261 F01

123VU GEN 1/EGIU 1/115VAC AF12

123VU BUS 1/110XP/SPLY AF11 FFIIRREE PPRROOTTEECCTTIIOONN SSYYSSTTEEMM123VU BUS 2/210XP/SPLY AF02

123VU GEN 2/EGIU 2/115VAC AF01 49VU ENGINE 2/FIRE DET./LOOP B A07

123VU MAIN FWD GALLEY FEEDER F AC10 49VU ENGINE 1/FIRE DET./LOOP A A06

123VU MAIN AFT GALLLEY FEEDER A AF04 49VU AIR COND/SDCU/CHAN 1 C06


121VU APU/FIRE AND OVHT/DET/LOOP B L44 105VU FLT CTL/ELAC 1/STBY SPLY A01

121VU APU/FIRE AND OVHT/DET/LOOP A L43 105VU FLT CTL/SEC 1/STBY SPLY B01

121VU APU/AUTO/EXTIG/GND/TEST L40

121VU APU/FIRE/EXTIG/SQUIB B L39 121VU FLIGHT CONTROLS/WTB/FLP/SYS 2 P20

121VU APU/FIRE/EXTIG/SQUIB A L38 121VU FLIGHT CONTROLS/WTB/SLT/SYS 2 P19

121VU APU/FIRE/LP VALVE/NORM M42 121VU FLIGHT CONTROLS/SLT/PS/IND 2 P16

121VU APU/FIRE/LP VALVE/STBY M41 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS 2 Q21

121VU ENGIN/ENG 1 AND 2 FIRE EXTIG/BTL 1/SQUIB B Q44 121VU FLIGHT CONTROLS/FCDC 2/SPLY Q20

121VU ENGIN/ENG 1 AND 2 FIRE EXTIG/BTL 1/SQUIB A Q43 121VU FLIGHT CONTROLS/SEC 3/SPLY Q19

121VU ENGIN/ENG 1 AND 2 FIRE EXTIG/BTL 2/SQUIB B Q42 121VU FLIGHT CONTROLS/SEC 2/SPLY Q18

121VU ENGIN/ENG 1 AND 2 FIRE EXTIG/BTL 2/SQUIB A Q41 121VU FLIGHT CONTROLS/THS ACTR/MOT 3 Q17

121VU ENGINE/ENG 2/FIRE DET/LOOP A Q39 121VU FLIGHT CONTROLS/THS ACTR/MOT 1 Q16

121VU ENGINE/ENG 1/FIRE DET/LOOP B Q38 121VU FLIGHT CONTROLS/SLT/CTL/SYS 2 R21

121VU FLIGHT CONTROLS/ELAC 2/NORM/SPLY R20

122VU AIR COND/SDCU/CHAN 2 T18

122VU AIR COND/CARGO/FIRE/EXTIG T19 122VU FLIGHT CONTROLS/WTB/FLP/SYS 1 S07

122VU FLIGHT CONTROLS/WTB/SLT/SYS 1 S06

FFLLIIGGHHTT CCOONNTTRROOLLSS SSYYTTEEMMFFUUEELL SSYYSSTTEEMM

49VU FLIGHT CONTROLS/SLT FLP/POS IND 1 B12 49VU FUEL/SMOKE/CONFIG/PUMP CTL A14

49VU FLIGHT CONTROLS/ELAC 1/NORM/SPLY B11 49VU FUEL FQI CHAN 1 A13

49VU FLIGHT CONTROLS/FCDC 1/SPLY B10 49VU FUEL/X FEED/VALVE/MOT 1 A12

49VU FLIGHT CONTROLS/THS/ACTR/MOT 2 B09 49VU FUEL/X FR VALVE 1/WING R A11

49VU FLIGHT CONTROLS/SEC 1/NORM/SPLY B08 49VU FUEL/X FR VALVE 1/WING L A10

49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS 1 B07 49VU FUEL/LP VALVE/MOT 1/ENG 2 A09

49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS 1 B06 49VU FUEL/LP VALVE/MOT 1/ENG 2 A08

49VU APU/FUEL/BLOW OFF/PUMP B14

105VU FLIGHT CONTROLS/ELAC 2/STBY SPLY A02


121VU APU/FUEL/BLOW OFF/CTL K39 123VU L WING TK/PUMP 1/STBY SPLY AD12

121VU FUEL FQI CHANNEL 1 AND 2 L26 123VU R WING TK/PUMP 1/STBY SPLY AE12

121VU FUEL/HI/LVL/SPLY L25

121VU FUEL/RFL/DFL/SPLY L24 HHIIDDRRAAUULLIICC PPOOWWEERR SSYYSSTTEEMM121VU FUEL/RFL/DFL/XFR/DEFUEL/VALVE L23

121VU APU/FUEL/LP VALVE/CTL M40 49VU HYD/FIRE VALVE/Y/ENG 2 C14

121VU APU/FUEL/LP VALVE/SPLY M39 49VU HYD/FIRE VALVE/G/ENG 1 C13

121VU APU/FUEL/PUMP/CTL M38 49VU HYD/RAT/CTL D14

121VU FUEL FQI CHANN 2 M27 49VU HYD/HYD POWER/B WARN & CTL C12

121VU FUEL/LP VALVE/MOT 2/ENG 2 M26 49VU HYD/HYD/PRESS XMTR C11

121VU FUEL/LP VALVE/MOT 2/ENG 1 M25

121VU FUEL/X FEED/VALVE/MOT 2 M24 121VU HYDRAULIC/SOL VALVES/G/Y/B/LEAK TEST N35

121VU FUEL/X FR VALVE 2/WING R M23 121VU HYDRAULIC/SOL VALVES/G/Y/PTU N34

121VU FUEL/XFR VALVE 2/WING L M22 121VU HYDRAULIC/LOW/LVL/IND N32

121VU FUEL/L WING TK/PUMP 2 SPLY N26 121VU HYDRAULIC/HYD POWER Y N30

121VU FUEL/L WING TK/PUMP 1 SPLY N23 121VU HYDRAULIC/HYD/QTY IND P35

121VU FUEL/R WING TK/PUMP 2 SPLY Q26 121VU HYDRAULIC/RAT/SPLY/EXTN/SOL 1 P33

121VU FUEL/R WING TK/PUMP 1 SPLY Q23 121VU HYDRAULIC/Y HYD/PUMP ENG 2/MONG Q37

121VU FUEL/PUMPS 2 R CTL AND L IND R29 121VU HYDRAULIC/Y HYD/PUMP ENG 2/CTL Q36

121VU FUEL/PUMPS 1 R CTL AND L IND R28 121VU HYDRAULIC/G HYD/PUMP ENG 1/CTL R35

121VU FUEL/PUMPS 2 L CTL AND R IND R24 121VU HYDRAULIC/G HYD/PUMP ENG 1/MONG R34

121VU FUEL/PUMPS 1 L CTL AND R IND R23

121VU FUEL/CTR TK/PUMP 2 SPLY P26 123VU B HYDRAULIC/ELEC PUMP AB09

121VU FUEL/CTR TK/PUMP 1 SPLY P23 123VU Y HIDRAULIC/ELEC/PUMP AB06

121VU FUEL/CTR TK/PUMP/AUTO/CTL R27 123VU Y HIDRAULIC/ELEC/ELEC PUMP NORM AB03

121VU FUEL/CTR TK/PUMPS 1 AND 2 CTL AND IND R26

121VU FUEL/CTR TK/PUMPS 1 AND 2 CTL AND IND R25


IICCEE AANNDD RRAAIINN PPRROOTTEECCTTIIOONN SSYYSS 122VU ANTI ICE/PROBES/P 2/T 2/ENG 1 Z10

122VU ANTI ICE/PROBES 2/PHC Y12

49VU ANTI ICE/PROBES AOA 1 D04 122VU ANTI ICE/RAIN/RPLNT/F.O –MZC/MZF/MZG/MZJ W11

49VU ANTI ICE/PROBES PHC 1 D03

49VU ANTI ICE/PROBES PITOT 1 D02 123VU ANTI ICE WINDSHIELD L AF10

49VU ANTI ICE/RAIN/RPLNT/CAPT D01 123VU ANTI ICE WINDSHIELD R AF03

49VU ANTI ICE/WING CTL C02 2000VU WATER SYSTEM ICE PROT CTL D08

49VU ANTI ICE/WING/MONG C01 2000VU WATER SYSTEM ICE PROT HTR D07

122VU ANTI ICE/WINDOWS R W14 IINNDDIICCAATTIINNGG RREECCOORRDDIINNGG SSYYSSTTEEMM122VU ANTI ICE/WHC 2 W13

122VU ANTI ICE/FIRST OFFICER WIPER W12 49VU EIS/ECAM/CTL/PNL E12

122VU ANTI ICE/ENG 2 W10 49VU EIS/DMC 1/CTL/SPLY E11

122VU ANTI ICE/WINDOWS L X14 49VU EIS/DMC 3/STBY/SPLY E10

122VU ANTI ICE/WHC 1 X13 49VU EIS/DMC 1/SWTG E09

122VU ANTI ICE/ CAPT WIPER X12 49VU EIS/RLY/BOX/CAPT E08

122VU ANTI ICE/ENG 1 X10 49VU EIS/DMC 3/SWTG E07

122VU ANTI ICE/PROBES/PHC 3 Y16 49VU EIS/ECAM DU/UPPER/SWTG E06

122VU ANTI ICE PROBES Y15 49VU EIS/ECAM DU/UPPER/SPLY E05

122VU ANTI ICE PROBES Y14 49VU EIS/PFD CAPT/SWTG E04

122VU ANTIICE PROBES 2/AOA Y13 49VU EIS/PFD CAPT/SPLY E03

122VU ANTI ICE/PROBES AND SENSORS 2/STATIC Y11 49VU CLOCK/NORM/SPLY F11

122VU ANTI ICE/PROBES AND SENSORS 3/PITOT Z16 49VU CAPT/LOUD SPKR F10

122VU ANTI ICE/PROBES 3/AOA Z15 49VU SDAC 1 AND 2/28VDC/ AC ESS BUS F05

122VU ANTI ICE/PROBES Z14 49VU SDAC 1/SPLY F04

122VU ANTI ICE/PROBES AND SENSORS 1/STATIC Z13 49VU SDAC 2/26VAC SYNC/AC ESS BUS F03

122VU ANTI ICE/PROBES AND SENSORS 1/STATIC Z12 49VU SDAC 1/26VAC SYNC/AC ESS BUS F02

122VU ANTI ICE/PROBES/P 2/T 2/ENG 2 Y10 49VU NAV/DME 1 G14


49VU EIS/ND CAPT/SWTG E02 121VU EIS/SDAC 2/BUS 2/26VAC SYNC AC Q03

49VU EIS/ND CAPT/SPLY E01 121VU EIS/SDAC 1/BUS 2/26VAC SYNC AC Q02

49VU FWS/FWC 1/SPLY F01 121VU EIS/ECAM DU/LOWER/SPLY R11

121VU EIS/ECAM DU/LOWER/SWTG R10

106VU EMER/GEN/REF B05 121VU EIS/DMC 2/SWTG R08

106VU DC/BUS 1 AND 2/MONG C03 121VU EIS/RLY/BOX/FIRST OFFICER R07

121VU EIS ND/FIRST OFFICER/SWTG R06

121VU CLOCK/STBY/SPLY –PTMZC/MZD N02 121VU EIS PFD/FIRST OFFICER/SWTG R05

121VU PTR/SPLY J21 121VU EIS ND/FIRST OFFICER R04

121VU CFDS/TEST PLUG 2 J20 121VU EIS PFD/FIRST OFFICER R03

121VU CFDS/TEST PLUG 1 J19 121VU CLOCK/STBY/SPLY –PT-MZA/MZF/MZG/MZH N03

121VU CFDS/CFDIU/SPLY J18 121VU DATA LOADER/SPLY J16

121VU CFDS/CFDIU/BACKUP J17 121VU AIDS/DMU AND QAR K15

121VU RCDR/ACCLRM K18

121VU RCDR/FDIU AND QAR K17 LLAANNDDIINNGG GGEEAARR SSYYSSTTEEMM121VU RCDR/DFDR K16

121VU COM NAV/DME 2 K06 49VU LANDING GEAR Y BRK/PRESS IND C10

121VU EIS/FIRST OFFICER/LOUD SPKR P08 49VU LANDING GEAR/LGCIU/SYS 1/NORM C09

121VU EIS/SDAC 1 AND 2/DOOR DET PAX P05

121VU EIS/SDAC 1 AND 2/BUS1/28VDC P04 121VU HYDRAULIC/BRK FAN WHEELS 3 & 4 L35

121VU EIS/SDAC 1 AND 2/BUS 2/28VDC P03 121VU HYDRAULIC/BRK FAN WHEELS 1 & 2 L32

121VU EIS/SDAC 1 AND 2/DOOR DET AVCNS P02 121VU HYDRAULIC/BRK FAN CTL M32

121VU EIS/DMC 3/SPLY Q09 121VU HYDRAULIC/BRK TEMP DET UNIT M37

121VU EIS/DMC 2/SPLY Q08 121VU HYD BRAKING AND STEERING SYS2/ SPLY M36

121VU EIS/FWC 2/SPLY Q07 121VU HYD BRAKING AND STEERING SYS 2/CTL M35

121VU EIS/SDAC 2/SPLY Q06 121VU HYD BRAKING AND STEERING SYS 1/CTL M34

121VU EIS/SDAC 2/BUS 1/26VAC SYNC AC Q05 121VU HYD BRAKING AND STEERING SYS 1 IND/SPLY M33

121VU EIS/SDAC 1/BUS 1/26VAC SYNC AC Q04 121VU HYDRAULIC/PARK BRK/CTL/STBY N37


121VU HYDRAULIC/PARK BRK/CTL/NORM N36 122VU LIGHTING/EXT LT/RWY TURN OFF L W06

121VU HYDRAULIC/LGCIU SYS 2 O35 122VU LIGHTING/EXT LT/RWY TURN OFF R W05

121VU HYDRAULIC/LGCIU SYS 1/GRND SPLY Q34 122VU LIGHTING/EXT LT/WING AND ENG SCAN R W03

122VU LIGHTING/EXT LT/WING AND ENG SCAN L W02

LLIIGGHHTTSS SSYYSSTTEEMM 122VU LIGHTING/WHL WELL/LTG DOME X08

122VU LIGHTING/WHL WELL/LTG OUT X07

49VU LIGHTING EMER LT/CKPT DOME H08 122VU LIGHTING/TST BOARD SPLY X06

49VU LIGHTING EMER LT/CABIN H07 122VU LIGHTING/ANN LT SPLY/XFMR BUS 2 X05

49VU LIGHTING EMER LT/CABIN –PTMZG/MZH H06 122VU LIGHTING/ANN LT SPLY/XFMR BUS 1 X04

49VU LIGHTING EMER LT/CABIN H05 122VU LIGHTING/ANN LT SPLY/XFMR/STAT INV X03

49VU LIGHTING/XFMR/115V.5V/ESS BUS H03 122VU LIGHTING/CKPT DOME Y06

49VU LIGHTING/ICE AND STBY COMP LIGHT H04 122VU LIGHTING/INSTL LT/GLARE SHLD Y05

122VU LIGHTING/INSTL LT/MAIN INST/PNL AND PED Y04

122VU LIGHTING/EXT LT/NAV 1 AND LOGO LIGHT T03 122VU LIGHTING/INSTL LT OVHD PNL Y03

122VU LIGHTING/EXT LT/NAV 2 AND LOGO LIGHT T02 122VU LIGHTING/AVNCS COMPT/OUT 115VAC Z09

122VU LIGHTING LANDING LT R/CTL T07 122VU LIGHTING/AVNCS COMPT/OUT 28 VDC Z08

122VU LIGHTING LANDING LT R/SPLY T06 122VU LIGHTING/AVNCS COMPT DOME Z07

122VU LIGHTING LANDING LT L/CTL T05 122VU LIGHTING/FLOOD FIRST OFFICER SIDE Z06

122VU LIGHTING LANDING LT L/SPLY T04 122VU LIGHTING/FLOOD CAPT SIDE Z05

122VU LIGHTING EXT LT BEACON UPPER U06 122VU LIGHTING/FLOOD CTR INST PNL Z04

122VU LIGHTING EXT LT BEACON LOWER U03 2000VU AIR CONDTN COMPT OUTLET B08

122VU LIGHTING/CABIN/EMER LT V07 2000VU CARGO COMPT LIGHT-LDG AERA B06

122VU LIGHTING/WING STROBE V05 2000VU CARGO COMPT LIGHT-AFT B05

122VU LIGHTING/LOGO LEFT V03 2000VU CARGO COMPT LIGHT-FWD B04

122VU LIGHTING/LOGO RIGH V02 2000VU PASSENGER READING LIGHT G07

122VU LIGHTING/EXT LT/TAXI AND TAKE OFF/CTL W09 2000VU PASSENGER READING LIGHT G06

122VU LIGHTING/EXT LT/TAXI AND TAKE OFF/TAXI W08 2000VU PASSENGER READING LIGHT G05

122VU LIGHTING/EXT LT/TAXI AND TAKE OFF/TO W07 2000VU PASSENGER READING LIGHT G04


2000VU PASSENGER READING LIGHT G03 121VU ADIRS/ADIRU 2 PWR/SHED –PT-MZI/MZJ N10

2000VU PASSENGER READING LIGHT G02 121VU ADIRS/ADIRU 3 PWR/SWTG –PT-MZI/MZJ N09

2000VU CABIN LIGHT POWER-CEILING AFT H08 121VU ADIRS/ADIRU 2/26VAC AND AOA –PT-MZI/MZJ N08

2000VU CABIN LIGHT POWER-CEILING AFT HO7 121VU ADIRS/ADIRU 3/26VAC AND AOA –PT-MZI/MZJ N07

2000VU CABIN LIGHT POWER-CEILING FWD H06 121VU AIDRS/ADIRU 2/115VAC –PT-MZI/MZJ N06

2000VU CABIN LIGHT POWER-CEILING FWD H05 121VU ADIRS/ADIRU 3/115VAC –PT-MZI/MZJ N05

2000VU CABIN LIGHT POWER-WINDOW AFT H04 121VU ADIRS/ADIRU 2/28VDC –PTMZI/MZJ N04

2000VU CABIN LIGHT POWER-WINDOW AFT H03 121VU ADIRS/ADIRU 3/28VDC –PT-MZI/MZJ N03

2000VU CABIN LIGHT POWER-WINDOW FWD H02 121VI COM NAV/RADAR 1 K13

2000VU CABIN LIGHT POWER-WINDOW FWD H01 121VU COM NAV/RAD ALTIMETER 2 K12

2000VU LIGHT-ATTND WORK J05 121VU COM NAV/RAD ALTIMETER 1 K11

2000VU LIGHT-CABIN ENTRY J04 121VU COM NAV/ILS 2 –PTMZA/MZB K09

121VU COM NAV/VOR 2 K08

NNAAVVIIGGAATTIIOONN SSYYSSTTEEMM 121VU COM NAV/ATC 2 K07

121VU EIS/GPWS/115VAC P07

49VU NAV STBY ALTIMETER F14 121VU EIS/GPWS/28VDC P06

49VU NAV VOR DME RMI F13 121VU COM NAV/RADAR 2 –PT-MZF K14

49VU NAV STBY HORIZONT F12 121VU COM NAV/ADF 2 K02

49VU NAV PROBES ADIRU 3 PWR SWTG F09 121VU ADIRS/ADIRU 2/PWR/SHED –PT-MZA/ZF/ZG/ZH N11

49VU NAV PROBES ADIRU 1 AND AOA 1/26VAC F07 121VU ADIRS/ADIRU 3/PWR/SWTG –PT-MZA/ZF/ZG/ZH N10

49VU NAV PROBES ADIRU 1/115VAC F06 121VU ADIRS/ADIRU 2/26VAC AND AOA-MZA/ZF/ZG/ZH N09

49VU NAV VOR 1 G13 121VU ADIRS/ADIRU 3/26VAC AND AOA-MZA/ZF/ZG/ZH N08

49VU NAV ILS 1 –PTMZA/MZB G12 121VU ADIRS/ADIRU 2/115VAC –PT-MZA/ZF/ZG/ZH N07

49VU NAV ATC 1 G11 121VU ADIRS/ADIRU 3/115VAC –PT-MZA/ZF/ZG/ZH N06

49VU NAV ADF 1 H14 121VU ADIRS/ADIRU 2/28VDC –PT-MZA/ZF/ZG/ZH N05

49VU NAV MMR 1-PTMZA/MZB G12 121VU ADIRS/ADIRU 3/28VDC –PT-MZA/ZF/ZG/ZH N04

121VU COM NAV/MMR 2 –PTMZB/ZC L07

105VU ADIRS/ADIRU 1/28VDC C02 121VU COM NAV/MMR 2 –PT-MZA/ZF/ZG/ZH K09


OOXXIIGGEENN SSYYSSTTEEMM DDOOOORRSS SSYYSSTTEEMM

49VU OXYGEN/PASSENGER/ACTUATION HA08 121VU EIS/SLIDES/ARM AND WARN GND P10

49VU OXYGEN/PASSENGER/ACTUATION HA07

49VU OXYGEN/PASSENGER/ACTUATION HA06 122VU DOORS CARGO T12

49VU OXYGEN/PASSENGER/ACTUATION HA05 122VU DOORS PAX MONG T13

49VU OXYGEN/PASSENGER/CTL AND WARN HA04

49VU OXYGEN/PASSENGER/CTL AND WARN HA03 EENNGGIINNEE SSYYSSTTEEMM49VU OXYGEN/PASSENGER/CTL AND WARN HA02

49VU OXYGEN/CREW/OXYGEN/SPLY HA01 49VU ENGINE 2/FADEC A AND EIU 2 A05

49VU ENGINE 1/FADEC A AND EIU 1 A04

PPNNEEUUMMAATTIICC SSYYSSTTEEMM 49VU ENGINE 1 AND 2 ING SYS A A03

49VU ENGINE 2 HP FUEL SOV A02

49VU AIR BLEED/ENG 1 CTL D12 49VU ENGINE 1 HP FUEL SOV A01

49VU AIR BLEED/ENG 1 MONG D11

49VU AIR BLEED/X FEED VALVE/BAT D13 121VU ENGINE IGN ENG 2 SYS B P42

121VU ENGINE IGN ENG 1 SYS B P41

122VU AIR BLEED/ENG 2 CTL Z23 121VU ENGINE IGN ENG 2 SYS A BAT P40

122VU AIR BLEED/ENG 2 MONG Z22 121VU ENGINE IGN ENG 1 SYS A BAT P39

122VU AIR BLEED/X FEED VALVE NORM Z20 121VU ENGINE ENG 2 FADEC B Q40

121VU ENGINE ENG 1 AND 2 EVMU R44

AAIIRRBBOORRNNEE AAUUXXIILLIIAARRYY PPOOWWEERR SSYYSS 121VU ENGINE ENG 1 FADEC B AND EIU 1 R41

121VU ENG/ENG 2 OIL PRESS AND REV SNSR CHAN A N42

121VU APU/APU CTL L42 121VU ENG/ENG 2 OIL QTY AND VER SNSR CHAN B N41

121VU APU/ECB SPLY L41 121VU ENG/ENG 1 OIL PRESS AND VER SNSR CHAN A N40

121VU APU/OIL HTR SPLY K41 121VU ENG/ENG 1 OIL QTY AND VER SNSR CHAN B N39

121VU ENGINE 2 VER LOCK N45

121VU ENGINE 1 VER LOCK N44

AABBRREEVVIIAATTUURRAASS AA331199//332200 AABBRREEVVIIAATTUURRAASS AA331199//332200A/D ANALOG TO DIGITAL CONVERTER ADS AIR DATA SYSTEM

A/F AUTO FLIGHT ADU ALIGN DISPLAY UNIT

A/G AIR TO GROUND AEVC AVIONICS EQUIPMENT VENTILATION COMPUTER

A/R AUDIO REPRODUCER AFC AUTOMATIC FREQUENCY CONTROL

A/S AUTO STABILIZATION AFCS AUTOMATIC FLIGHT CONTROL SYSTEM

A/SKID ANTI-SKID AFECU AUTOMATIC FIRE EXTINGUISHER CONTROL UNIT

AADC ANALOG AIR DATA COMPUTER AFS AUTOMATIC FLIGHT SYSTEM

AAP ADITIONAL ATTENDENT PANEL AHRS ATTITUDE AND HEADING REFERENCE SYSTEM

ABD AIRBUS DIRECTIVES AIDS AIRCRAFT INTEGRATED DATA SYSTEM

ACARS AIRCRAFT COMM. ADRESS. REPORT SYS ALTU ANNUNCIATOR LIGHT TEST UNIT

ACC ACTIVE CLEARENCE CONTROL AMU AUDIP MANAGEMENT UNIT

ACCEL ACCELERATION/ACCELERATE AOA ANGLE OF ATTACK

ACCLRM ACCELEROMETER AOHX AIR/OIL HEAT EXCHANGER

ACMM ABBREVIATED COMPONENT MAINT MANUAL AP/FD AUTO PILOT/FLIGHT DIRECTOR

ACMR AIRCRAFT CONFIGURATION MANAG.RULES APLC AIRCRAFT POWER LINER CONDITIONER

ACMS AIRCRAFT CONDITION MONITORING SYSTEM APPU ASYMETRIC POSITION PICK OFF UNIT

ACOB AUTOMATIC CALL OUT BOX APU AFE APU AUTO. FIRE EXTINGUISHER CONTROL UNIT

ACOC AIR COOLED OIL COOLER ASP AUDIO SELECTOR PANEL

ACP AREA CALL PANEL AT AUTOTHRUST

ACU ANTENNA COUPLER UNIT ATCSS AIR TRAFIC CONTROL DATA LINK SIGNALL SYS

ADAU AUXILIARY DATA ACQUISITION UNIT ATSU AIR TRAFIC SERVICE UNIT

ADC AIR DATA COMPUTER AVRS AUDIO/VIDEO RECORDING SYSTEM

ADG AIR DRIVE GENERATOR BCDS BITE CENTRALIZED SYSTEM

ADI ATTITUDE DIRECTOR INDICATOR BFDAS BASIC FLIGHT DATA ACQUISITION SYSTEM

ADIRS AIR DATA/INERTIAL REFERENCE SYSTEM BIU BITE INTERFACE UNIT

ADIRU AIR DATA/INERTIAL REFERENCE UNIT BMC BLEED MONITORING COMPUTER

ADM AIR DATA MODULE BSCU BRAKE /STEERING SYSTEM UNIT

ADPM AIRCRAFT DEACTIVATION PROCEDURES MANUAL BTR BUS TIE RELAY

ADR AIR DATA REFERENCE BYDU BACK-UP YAW DAMPER UNIT

AABBRREEVVIIAATTUURRAASS AA331199//332200 AABBRREEVVIIAATTUURRAASS AA331199//332200CAS COMPUTED AIR SPEED EPSU EMERGENCY POWER SUPLLY UNIT

CBMS/U CIRCUIT BREAKER MONITORING SYSTEM/UNIT EWD ENGINE/WARNING DISPLAY

CCS CABIN COMMUNICATIONS SYSTEM FADEC FULL AUTHORITY DIGITAL ENGINE CONTROL

CECAM CENTRALIZED CABIN MONITORING FAP FORWARD ATTENDENT PANEL

CFDIU CENTRALIZED FAULT DISPLAY INTERFACE UNIT FC FULLY CLOSED

CFDS CENTRALIZED FAULT DISPLAY SYSTEM FCDC FLIGHT CONTROL DATA CONCENTRATOR

CIDS CABIN INTERCOMMUNICATION DATA SYSTEM FCMC FUEL CONTROL AND MONITORING COMPUTER

CLOG CLOGGING FCMS FUEL CONTROL AND MONITORING SYSTEM

CMC CENTRALIZER MAINTENANCE COMPUTER FCPC FLIGHT CONTROL PRIMARY COMPUTER

CMS CABIN MANAGEMENT SYSTEM FCSC FLIGHT CONTROL SECONDARY COMPUTER

CPC CABIN PRESSURE CONTROLLER FCU FLIGHT CONTROL UNIT

CPCS/U CABIN PRESSURE CONTROL SYSTEM/UNIT FCV FLOW CONTROL VALVE

CPMS/U CABIN AND PASSENGER MANAGEMENT SYS/UNIT FDIU FLIGHT DATA INTERFACE UNIT

DADC/S DIGITAL AIR DATA COMPUTER/SYSTEM FDU FIRE DECTECTION UNIT

DCDU DATA CONTROL AND DISPLAY UNIT FG FLIGHT GUIDANCE

DMC DISPLAY MANAGEMENT COMPUTER FIDS FAULT ISOLATION DETECTION SYSTEM

DSCS DOOR AND SCAPE SLIDES CONTROL SYSTEM FMA FLIGHT MODE ANNUNCIATOR

EADI ELECTRONIC ATTITUDE DIRECTOR INDICATOR FMGEC FLIGHT MANAGENT GUIDANCE ENVELOP COMPT

ECAM ELECTRONIC CENTRALIZED AIRCRAFT MONITORI FMGES FLIGHT MANAGENT GUIDANCE ENVELOPE SYS

ECP ECAM CONTROL PANEL FMV FUEL METERING VALVE

ECS ENVIRONMENTAL CONTROL SYSTEM FPEEPMS FLOOR PROXIMITY EMRG. ESCAP PATH MK. SYS

EEC ENGINE ELECTRONIC CONTROL GCR GENERATOR CONTROL RELAY

EFCC/S ELECTRONIC FLIGHT CONTROL COMPUTER/SYST. HCU HYDRAULIC CONTROL UNIT

EGIU ELECTRICAL GENERATOR INTERFACE UNIT HEGS HYDRAULIC ELECTRICAL GENERATING SYSTEM

EIU ENGINE INTERFACE UNIT HMU HYDROMECHANICAL UNIT

EIUVMU ENGINE INTERFACE/VIBRATION MONIT. UNIT HPTACC HIGH PRESSURE TURBINE ACTIVE CLEARNCE CTL

ELAC ELEVATOR AILERON COMPUTER HSMU HYDRAULIC SYSTEM MONITORING UNIT

EMLS EMERGENCY LIGHTING SYSTEM LA LINEAR ACCELEROMETER

EMU ENGINE MAINTENANCE UNIT LCIT LOAD COMPRESSOR INLET TEMPERATURE

AABBRREEVVIIAATTUURRAASS AA331199//332200 AABBRREEVVIIAATTUURRAASS AA331199//332200LGCIU LANDING GEAR CONTROL INTERFACE UNIT RAT RAM A IR TURBINE

LLDC LOW LEVEL DIRECT CURRENT VOLTAGE RCCB REMOTE CONTROL CIRCUIT BREAKER

LMS LEAKAGE MEASUREMENT SYSTEM RLA REVERSER LEVER ANGLE

LOP LOW OIL PRESSURE RMP RADIO MANGEMENT PANEL

LPTACC LOW PRESS TURBINE ACTIVE CLEARENCE CTL SDAC SYSTEM DATA ACQUISITION CONCENTRATOR

LVDT LINEAR VARIABLE DIFFERENTIAL TRANSDUCER SDCU SMOKE DETECTION CONTROL UNIT

MCDU MULTIPURPOSE CONTROL DISPLAY UNIT SFCC SLAT FLAP CONTROL COMPUTER

MDDU MULTIPURPOSE CONTROL DISPLAY UNIT SIC SYSTEM ISOLATION CONTACTOR

MÊS MAIN ENGINE START SSTU SIDE STICK TRANSDUCER UNIT

MICBAC MICRO-SYSTEM BUS ACCESS CHANNEL TCAS TRAFFIC ALERT COLLISION AVOIDANCE SYSTEM

MMR MLTI MODE RECEIVER THS TRIMMABLE HORIZONTAL STABILIZER

MSU MODE SELECTOR UNIT(IRS) TLA THROTTLE LEVER ANGLE

MSW MICROSWITCH TLU TRAVEL LIMITATION UNIT

N/WS NOSE WHEEL STEERING TRA THROTTLE RESOLVER ANGLE

OMS ONBOARD MAINTENANCE SYSTEM TRDV THRUST REVERSER DIRECTINAL VALVE

OOT OIL OUTLET TEMPERATURE TRPV THRUST REVERSER PRESSURIZING VALVE

OPV OVERPRESURE VALVE TTS TRIM TANK SYSTEM

PC PACK CONTROLLER VBV VARIABLE BLEED VALVE

PCU PASSANGER CONTROL UNIT VCO VOLTAGE CONTROLLED OSCILLATOR

PCU POWER CONTROL UNIT VCU VIDEO CONTROL UNIT

PES PASSANGER ENTERTAINMENT SYSTEM WBC/S WEIGHT AND BALANCE COMPUTER/SYSTEM

PHC PROBE HEAT COMPUTER WHC WINDOW HEAT COMPUTER

PIU PASSENGER INFORMATION UNIT WIPCU WATER ICE PROTECTION CONTROL UNIT

PSCU PROXIMITY SWITCH CONTROL UNIT WIPDU WATER ICE PROTECTION DATA UNIT

PSDU POWER SUPPLY DECOUPLING UNIT WTB WING TIP BRAKE

PSS/U PASSENGER SERVICES SYSTEM/UNI WXR WEATHER RADAR

PVIS PASSENGER VISUAL INFORMATION SYSTEM XDCR TRANSDUCER

RACC ROTOR ACTIVE CLEARENCE CONTROL ZFCG ZERO FUEL CENTER OF GRAVITY

RACSB ROTOR ACTIVE CLEARENCE START BLEED

AA331199//332200

PPRREESSSSÃÃOO DDOOSS PPNNEEUUSS

MAIN LANDING GEAR210 PSI

NOSE LANDING GEAR178 PSI

MAIN LANDING GEAR168 A 189 TROCAR PNEU

NOSE LANDING GEAR143 A 161 TROCAR PNEU

MAIN LANDING GEAR0 A 168 TROCAR O PAR

NOSE LANDING GEAR0 A 143 TROCAR O PAR

TORQUE DAS RODASLOCK BOLT 35.39 A 39.89 Lbs/Pol

MLG 1° 300.14 Lbs/Ft2° 149.70 Lbs/Ft

NLG 1º 160.76 Lbs/Ft2º 80.01 Lbs/Ft

FFOONNTTEE::LLIINNEE CCHHEECCKK SSUUPPPPOORRTTIINNGG DDAATTAA

MMAAXX.. DDEEFFAASSAAGGEEMM DDEE IINNDD.. AALLTTIITTUUDDEE AA--331199 MMAAXX.. DDEEFFAASSAAGGEEMM DDEE IINNDD.. AALLTTIITTUUDDEE AA--331199

FFLLIIGGHHTTLLEEVVEELL

SSPPEEEEDDAADDRR 11

AADDRR 22 FFttNNOO PPFFDD

AADDRR11// 22//33 FFtt

NNOO PPFFDD

SSTTDDBBYYAALLTT

AADDRR 11//2233 FFtt


SSPPEEEEDDAADDRR 11



NNOO PPFFDD

SSTTDDBBYYAALLTT

AADDRR 11//2233 FFtt

GGNNDD ------------------ 2200 2200 ------------ GGNNDD -------------- 66 66 66

5500 CCAASS 225500KKTTSS

5500 6655 112255 5500 CCAASS 225500KKTTSS

44 44 77


5555 8800 118855 110000 CCAASS 225500KKTTSS

44 55 88


9900 113355 229955 220000 CCAASS 330000KKTTSS

33 55 99

330000 MM AACCHH 00..7788 113300 119955 339900 330000 MM AACCHH 00..7788 33 55 99


RREEFF:: DD..EE.. AA3311993344--000011// 3344--1133--0000--881100--999988 RREEFF:: DD..EE.. AA3311993344--000022// 3344--1133--0000--881100--999988

MMAAXX.. DDEEFFAASSAAGGEEMM DDEE IINNDD.. AALLTTIITTUUDDEE AA--332200 MMAAXX.. DDEEFFAASSAAGGEEMM DDEE IINNDD.. AAIIRRSSPPEEEEDD AA--332200


SSPPEEEEDDAADDRR 11



NNOO PPFFDD

SSTTDDBBYYAALLTT

AADDRR 11//22//33 FFtt


SSPPEEEEDDAADDRR 11



NNOO PPFFDD

SSTTDDBBYYAAIISS AADDRR11//22//33 FFtt

GGNNDD ------------------ 2200 2200 -------------- GGNNDD -------------- 66 66 66


5500 6655 113300 5500 CCAASS 225500KKTTSS

44 44 77


5555 8800 118855 110000 CCAASS 225500KKTTSS

44 55 88


9900 113355 229955 220000 CCAASS 330000KKTTSS

33 55 99



RREEFF:: DD..EE.. AA3322003344--000011// 3344--1133--0000--881100--999988 RREEFF:: DD..EE.. AA3322003344--000022// 3344--1133--0000--881100--999988

IINNGGLLÊÊSS TTÉÉCCNNIICCOORREEFFEERRÊÊNNCCIIAA RR ÁÁPPIIDDAA

IINNGGLLÊÊSS TTÉÉCCNNIICCOORREEFFEERRÊÊNNCCIIAA RR ÁÁPPIIDDAA

01-ACCOMPLISHED THRU CHECK02-ACCOMPLISHED DAILY CHECK03-ACCOMPLISHED WEEKLY CHECK04-ACFT DISPATCHED ACCORDING MEL...05-NO AVAILABLE SPARE PART06-PERFOMED OPERATIONAL TEST ON GROUND...NO FAULTS FOUND...THE SYSTEM IS OK07-SWAPPED ( )WITH( )......TO BE REASEARCHED...BOTH SYSTEM WORKED NORMAL ON GROUND...THE FAULT REMAIN...THE CHANGEND OF SIDE08-PERFORMED TROUBLESHOOTING...THE FAULTS09-REPLACED ( ) AND OPERATIONAL TEST......ACCORDING TO MAINT. MANUAL...IN UNIT(SELF TEST)

0011--EEFFEETTUUAADDAA IINNSSPP.. DDEE TTRR ÂÂNNSSIITTOO0022--RREEAALLIIZZAADDOO CCHHEECCKK DDIIÁÁRRIIOO0033--RREEAALLIIZZAADDOO CCHHEECCKK SSEEMM AANNAALL0044--AACCFFTT DDEESSPPAACCHH AADDAA DDEE AACCOORRDDOO MM EELL......0055--ÑÑ PPOOSSSSUUÍÍMM OOSS MM AATTEERRIIAALL EESSTT QQ0066--EEFFEETTUUAADDOO TTEESSTTEE OOPPEERR AACCIIOONNAALL NNOO SSOOLLOO............NNEENNHHUUMM AA PPAANNEE FFOOII AACCHH AADDAA............OO SSIISSTTEEMM AA EESSTT AA OOKK0077--FFOOII IINNVVEERR TTIIDDOO(( ))CCOOMM (( ))............PPAARR AA SSEERR PPEESSQQUUIISSAADDOO......NNOO SSOOLLOO AAMM BBOOSS SSIISSTT.. OOPPEERR AAMM NNOORRMM AALLMM EENNTT......AA PPAANNEE AAIINNDDAA CCOONNTTIINNUUAA......AA PPAANNEE IINNVVEETTEEUU DDEE LLAADDOO0088--FFEEIITTOO PPEESSQQUUIISSAA......AA PPAANNEE EE......0099--FFOOII SSUUBBSSTT..(( )) EE FFEEIITTOO TT EESSTT EE OOPPEERR AACCIIOONNAALL......DDEE AACCOORRDDOO MM AANNUUAALL MM NNTT......NNAA UUNNIIDDAADDEE

10-REPLACED NOSE WHEEL (LH/RH) /MAIN WHEEL DUE......NORMAL WEAR...DEEP CUT...LEAKAGE11-REPALCED BRAKE # DUE......NORMAL WEAR

1100--SSUUBBSSTT.. RROODDAA DDEE NNAARRIIZZ ((LLHH//RRHH)) // TTRR EEMM PPRRIINNCC..DDEEVVIIDDOO ............DDEESSGGAASSTTEE NNOORRMM AALL......CCOORRTT EE PPRROO FFUUNNDDOO......VVAAZZAAMM EENNTTOO1111--SSUUBBTTIITTUUIIDDOO FFRR EEIIOO ## DDEEVVIIDDOO......DDEESSGGAASSTTEE NNOORRMM AALL

...LEAKAGE12-THE PLUG......HAS BEEN CLANED...HAS BEEN LOCKED13-SENSOR WITH ERRONEUS(FALSE) INDICATIONS14-MISSING15-DEACTIVETED HYDRAULIC PUMP ON ENG # DUE...

......VVAAZZAAMM EENNTTOO1122--OO PPLLUUGG((CCOONNEECCTTOORR))............FFOOII LLIIMM PPOO......FFOOII TTRR AAVVAADDOO1133--SSEENNSSOORR CCOOMM IINNDDIICCAAÇÇÃÃOO EERRRROONNEEAA1144--FFAALLTT AANNDDOO1155--DDAASSAATTIIVVAADDAA BBOOMM BBAA HHIIDD..((LLHH//RRHH)) DDOO MM OOTTOORR ##DDEEVVIIDDOO ......

...LEAKEGE16-RETORQUED THE LINES, AFTER TEST OK

......VVAAZZAAMM EENNTTOO1166--EEFFEETTUUAADDOO RREEAAPPEERRTTOO DDAASS LLIINNHH AASS AAPPÓÓSS TTEESSTTEE OOKK..

AATTAA PPRROOBBLLEEMM OORRMMSSGG

CCBB TTOO RREESSEETT AATTAA PPRROOBBLLEEMM OORRMMSSGG

CCBB TTOO RREESSEETT

2211

VENT AVIONCS FAULTS

VU 122 AVNCS VENT MONG

IF NO HELP, THEN RESET

VU 49 D5 AVNCS VENT CTLVU 49 D6 AVNCS VENT CTL

2211

VVEENNTT AAVVIIOONNCCSSEEXXTTRR AACCTT FFAAUULLTT

VVUU 112222 YY1177 AAVVNNCCSS VVEENNTT MM OONNGGIIFF NNOO HHEELLPP,, TTHHEENN RREESSEETT ::VU 49 D5 AVNCS VENT CTLVU 49 D6 AVNCS VENT CTLIF NO HELP, THEN RESET:

VU 123 AE2 AVNCS VENT EXTC FAN

1-CONDITIONS OF POWER-UP TESTS INITIALIZATIONHOW LONG THE COMPUTER MUST BE DE-ENERGIZED:1SA/C CONFIGURATION:A/C ON GROUND ANDBLOWER AND EXTRACT PUSH-BUTTONS ON VENTILATION PANEL:AUTODITCHING PUSH-BUTTON: OFF

2-DURATION:85 SECFLIGHT DECK EFFECTS:BLOWER AND EXTRACT LOCAL FAULTSSMOKE AT GEN 1 LINESKIN VALVES MOVING TO FULLY OPEN POSITION

3-RESULTS OF POWER-UP TESTSTESTS PASS:ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED

TESTS FAIL: (FAULT CONFIRMED)PROCEED TO MEL/TSM FOR DEFERAL/TROUBLESHOOTING

1-CONDITIONS OF POWER-UP TESTS INITIALIZATIONHOW LONG THE COMPUTER MUST BE DE-ENERGIZED:1SA/C CONFIGURATION:A/C ON GROUND ANDBLOWER AND EXTRACT PUSH-BUTTONS ON VENTILATION PANEL:AUTODITCHING PUSH-BUTTON: OFF

2-DURATION:85 SECFLIGHT DECK EFFECTS:BLOWER AND EXTRACT LOCAL FAULTSSMOKE AT GEN 1 LINESKIN VALVES MOVING TO FULLY OPEN POSITION



ATA PPRROOBBLLEEMM OORRMMSSGG



2211

COND. TRIM AIR SYS FAULT AND

MSG “TRIM AIR HI PR”

DISREGARD IF THE WARNING AND MSG “TRIM AIR HI PR”

IS TRIGGERED WHEN ALL TRIM AIR VALVES ARE CLOSED

REF FLT MANUAL 7-60

2211

CCAABBIINN TTRRIIMM AAIIRRVVAALLVVEE MM SSGG

VVUU 112222 VV1177 ZZOONN TT EEMM PP CCTTLLSSYYSS 11VVUU 112222 VV1188 ZZOONN TT EEMM PP CCTTLLSSYYSS 22VVUU 112222 VV1199 ZZOONN TT EEMM PP CCTTLLSSYYSS 11VVUU 112222 VV2200 ZZOONN TT EEMM PP CCTTLLSSYYSS 22RREESSEETT CCBB IINN AACCCCOORRDDAANNCCEE WWIITTHHTTHH EE FFOOLLLLOO WWIINNGG PPRROOCCEEDDUURREE

3-RESULTS OF POWER-UP TESTS

TESTS PASS:ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED


1-CONDITIONS OF POWER-UP TESTS INITIALIZATION

HOW LONG THE COMPTER MUST BE DE-ENERGIZED:200SA/C CONFIGURATION:A/C ON GROUND ANDBOTH PACK SELECTED: OFFFLOW CONTROL VALVES: CLOSED

NOTE: BOTH PACK CONTROLLERS ENERGIZED AND HAVING FINISHED THEIR POWER-UP TESTS PLUS 5 SEC. DELAY FOR CONFIRMATION

2-PROGRESS OF POWER-UP TESTSDURATION: 36 SEC.FLIGHT DECK EFFECTS:3 TRIM AIR VALVES ARE MOVING FROM COOL TO HOT AND FROM HOT TO COOL.





2222

AUTO FLIGHT A/THR LIMITED WARNING MSG

MSG IS DISPLAYED WHEN AUTO THR ENGAGED AND THE

THROTTLES ARE BELOW THE CL DETENT.

MOVE THROTTLES PER FLT MANUAL 7-50



2222

AAUUTTOO FFLLTT AA//TTHHRROOFFFF MM SSGG

UUPPPPEERR EECCAAMM MM SSGG AAFFTT EERREENNGGIINNEE SSTT AARRTT AANNDD BBEEFFOORREETT..OO.. TTHHRRUUSSTT IISS AAPPPPLLIIEEDD ((OONNTTHHEE GGRROOUUNNDD))..TTHHIISS MM SSGG SSHHOOUULLDD DDEEDDIISSRREEGGAARRDDEEDD BBYY FFLLIIGGHHTTCCRREEWW PPEERR FFLLTT MM AANNUUAALL 77--5500


TESTS PASS:ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED

TESTS FAIL: (FAULT CONFIRMED)PROCEED TO MEL/TSM FOR DEFERAL/TS




2222

FCU FAULTS VU 49 B5 FCU1VU 121 M21 FCU2

RESET CB’S IN ACCORDANCE WITH THE FOLLOWING

PROCEDURE

2222

FFMM GGCC MM SSGG““OOPPPPOOSSIITTEE FFMM IINNPPRROOGGRR EESSSS OOFFFFMM AA SSHHOO WWSSOOFFFFSSIIDDEE FFDD’’SS””

VVUU 4499 BB22 FFMM GGCC 11VU 121 M17 FMGC 2

VU 49 D6 AVNCS VENT CTLRESET CB’S IN ACCORDANCE WITH

THE FOLLOWING PROCEDURE


HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >7 MIN ON BOTH FCU’SA/C CONFIGURATION:A/C ON GROUND

2- PROGRESS OF POWER-UP TESTSDURATION: 10 SECFLIGHT DECK EFFECTS:ECAM STATUS PAGE: FCU 1&2 INOP – AP 1&2 INOP – A/THR INOP




HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >4 SEC.A/C CONFIGURATION:A/C ON GROUND WITH ENGINES STOPPED

2- PROGRESS OF POWER-UP TESTSDURATION:120 SECFLIGHT DECK EFFECTS:ECAM STATUS PAGE: AP 1&2 INOP






2222

FMGC MSG “SET OFFSIDE RANGE

MODE”

VU 49 B2 FMGC 1VU 121 M17 FMGCU 2

RESET CB’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE 2222

AAUUTTOO PPIILLOOTT ##11FFAAUULLTT

VVUU 4499 BB22 FFMM GGCC 11RESET CB’S IN ACCORDANCE WITH

THE FOLLOWING PROCEDURE


HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >1 SECA/C CONFIGURATION:A/C ON GROUND

2- PROGRESS OF POWER-UP TESTSDURATION: 120 SECFLIGHT DECK EFFECTS:ECAM STATUS PAGE: AP# 1 E 2 INOP





2- PROGRESS OF POWER-UP TESTSDURATION:120 SECFLIGHT DECK EFFECTS:ECAM STATUS PAGE: AP #1 E 2 INOP






2222AUTO PILOT #2 FAULT

VU 121 M17 FMGCU 2RESET CB’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE 2222

FFAACC FFAAUULLTTSSSSYYSSTT EEMM ##11

RREESSEETT FFAACC##11 PPUUSSHHBBUUTTTTOONNIIFF NNOO HHEELLPP,, TTHHEENN RREESSEETTVVUU 4499 BB33 FFAACC 11 2266 VVAACCVVUU 4499 BB44 FFAACC 11 2288 VVDDCCRESET CB’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE


HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >4 SECA/C CONFIGURATION:A/C ON GROUND WITH ENGINES STOPPED

2- PROGRESS OF POWER-UP TESTSDURATION: 120 SECFLIGHT DECK EFFECTS:ECAM STATUS PAGE: AP# 1 E 2 INOP




HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >4 SEC.A/C CONFIGURATION:1-A/C ON GROUND WITH ENGINES STOPPED FOR ELECTRICAL POWER-UP TESTS,2-A/C ON GORUND AND HYDRAULICALLY ENERGIZED FOR YAW DAMPER POWER LOOP POWER-UP TESTS

2- PROGRESS OF POWER-UP TESTSDURATION:1 –90 SEC 2 –5 SEC FLIGHT DECK EFFECTS:AUTO FLT RUDDER TRIM 1(2)AUTO FLT RUD TRAV LIM 192)AUTO FLT YAW DAMPER 1(2)FLT CTL PANEL: FAULT FLASHES ON FAC 1 PUSHBUTTON






2222FAC FAULTS SYSTEM #2

RREESSEETT FFAACC##22 PPUUSSHHBBUUTTTTOONNIIFF NNOO HHEELLPP,, TTHHEENN RREESSEETTVVUU 4499 BB33 FFAACC 11 2266 VVAACCVVUU 112211 MM 1199 FFAACC 22 2288 VVDDCCRESET CB’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE

2222DDUUAALL CCAATT IIIIII MM SSGG VVUU 4499 BB44 FFAACC 11 2288 VVAACC

VVUU 112211 MM 1199 FFAACC 22 2288 VVDDCCRESET CB’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE



2- PROGRESS OF POWER-UP TESTSDURATION:1 –90 SEC 2 –5 SEC FLIGHT DECK EFFECTS:AUTO FLT RUDDER TRIM 1(2)AUTO FLT RUD TRAV LIM 1(2)AUTO FLT YAW DAMPER 1(2)FLT CTL PANEL: FAULT FLASHES ON FAC 2 PUSHBUTTON





2- PROGRESS OF POWER-UP TESTSDURATION:1 –90 SEC 2 –5 SEC FLIGHT DECK EFFECTS:AUTO FLT RUDDER TRIM 1(2)AUTO FLT RUD TRAV LIM 192)AUTO FLT YAW DAMPER 1(2)FLT CTL PANEL: FAULT LEGEND FLASHES






2222MCDU FAULT SYSTEM #1

VVUU 4499 BB11 MM CCDDUU 11RESET CB’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE 2222

MM CCDDUU FFAAUULLTTSSYYSSTT EEMM ##22

VVUU 112211 NN2200 MM CCDDUU 22RESET CB’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE


HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >200 MS.A/C CONFIGURATION:A/C ON GROUND

2- PROGRESS OF POWER-UP TESTSDURATION:45 SEC FLIGHT DECK EFFECTS:MCDU SCREEN IS BLANK

3-RESULTS OF POWER-UP TESTSTESTS PASS:

ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED



HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >200 MS.A/C CONFIGURATION:A/C ON GROUND

2- PROGRESS OF POWER-UP TESTSDURATION:45 SEC FLIGHT DECK EFFECTS:MCDU SCREEN IS BLANK






2222AUTO FLT RUD TRV LIM SYS FAULT MSG

RREESSEETT FFAACC 11 AANNDD FFAACC 22PPUUSSHHBBUUTT TTOONN SSWWIITTCCHHEESS 2222

RRUUDDDDEERR TTRR AAVVEELLLLIIMM IITT SSYYSSTTEEMM ##11

VVUU 4499 BB33 FFAACC 11 2266VVAACCVVUU 4499 BB44 FFAACC 22 2288VVDDCCIIFF NNOO HHEELLPP,, TTHHEENN RREESSEETT ::VVUU 4499 BB22 FFMM GGCC 11 ((SSEEEE CCHH 2222,,AAPP##11 FFAAUULLTT FFOORR PPRROOCCEEDDUURREE))RESET CB’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE






2- PROGRESS OF POWER-UP TESTSDURATION:1 –90 SEC 2 –5 SEC FLIGHT DECK EFFECTS:AUTO FLT RUDDER TRIM 1(2)AUTO FLT RUD TRAV LIM 192)AUTO FLT YAW DAMPER 1(2)FLT CTL PANEL: FAULT LEGEND FLASHES






2222RRUUDDDDEERR TTRR AAVVEELLLLIIMM IITT SSYYSSTTEEMM ##22

VU 121 M18 FAC 2 26VACVU 121 M19 FAC 2 28VDCIF NO HELP, THEN RESET:VU 121 M17 FMGC 2 (SEE CH 22, AP #2 FAULT FOR PROCEDURE)RESET CB’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE

2233CCIIDDSS SSYYSSTT EEMMFFAAUULLTTSS

AATT TTEEMM PPTT AA RREESSEETT AATT PPTT PPFFIIRRSSTT,, IIFF NNOO HHEELLPP,, TTHH EENNRREESSEETT:: NNOOTTEE RREESSEETT CC..BB..’’SSTTOOGGEETTHHEERRVVUU 4499 GG22 CCIIDD DDIIRR 11&&22 EESSSSVVUU 112211 MM 55 CCIIDDSS DDIIRR 11&&22 NNOORRMMRESET CB’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE


HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >4 SEC.A/C CONFIGURATION:1-A/C ON GROUND WITH ENGINES STOPPED FOR ELECTRICAL POWER-UP TESTS,2-A/C ON GORUND AND HYDRAULICALLY ENERGIZED FOR YAW DAMPER POWER LOOP POWER-UP TESTS2- PROGRESS OF POWER-UP TESTSDURATION:1 –90 SEC 2 –5 SEC FLIGHT DECK EFFECTS:AUTO FLT RUDDER TRIM 1(2)AUTO FLT RUD TRAV LIM 1(2)AUTO FLT YAW DAMPER 1(2)FLT CTL PANEL: FAULT LEGEND FLASHES

3-RESULTS OF POWER-UP TESTSTESTS PASS:ABOVE MENTIONED FAULT MSG NO LONGER DISPLYEDTESTS FAIL: (FAULT CONFIRMED)PROCEED TO MEL/TSM FOR DEFERAL/TS

1-CONDITIONS OF POWER-UP TESTS INITIALIZATIONHOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 1-10 SEC; 2- 30 SEC.A/C CONFIGURATION:1-A/C ON GROUND WITH BOTH CABIN DOORS CLOSED2-A/C ON GROUND WITH ENGINES STOPPED AND A CABIN DOOR OPEN2- PROGRESS OF POWER-UP TESTSDURATION:1 –50 SEC 2 –120 SEC FLIGHT DECK EFFECTS:CIDS 1 ON THEN OFF AFTER 30 SECCIDS 2 ON THEN OFF AFTER 80 SECAUDIO CONTROL PANEL “ATT LIGHT IS FLASHING”

CABIN AFFECTS:1- CABIN LIGHTS ARE OFF DURING 1SEC2-CABIN LIGHTS AND PAX ATT LIGHTS ARE FLASHING




2233 FFLLTT AATT TTNNDD//PPNNLLLLOOCCKKEEDD UUPP

VVUU 112211 MM 1144 CCIIDDSS FFWWDDAATT TTNNDD//PPNNLL



2233PPAAXX

EENNTTEERRTT AAIINNMM EENNTTWWIILLLL NNOOTT TTUURRNN

OONN OORR OOFFFF

VVUU 22000000 FF66 CCAABBIINN CCOOMM SSYYSS PPEESSIIFF NNOO HHEELLPP,, TTHHEENN RREESSEETT :: AALLLLDDEEUU’’SSVVUU 112211 MM 77 TTHHRROOUUGGHH MM 1133



2233 PPAAXX SSEEAATT AAUUDDIIOOIINNOOPP

VVUU 22000000 CCAABBIINN CCOOMM SSYYSS PPEESS



2233

SSEEAATT VVIIDDEEOO SSYYSSUUNNIITT PPRROOBBLLEEMM SS

RREESSEETT IINNDDIIVVIIDDUUAALL VVIIDDEEOOUUNNIITT,, SSMM AALLLL HHOOLLEE JJ UUSSTT FFWWDDOOFF SSCCRR EEEENN OONN TTHHEE SSAAMM EEPPAANNEELL IISS RREESSEETT BBUUTT TTOONN((OONN--OOFFFF))



2233 RRMM PP FFAAUULLTT SS TTUURRNN AAFFFFEECCTTEEDD RRMM PP OOFFFFTTHHEENN OONN TTOO RREESSEETT



2233ACP FREQ’S WILL NOT CHANGE FROM THE STANDBY TO ACTIVE WINDOWS

TTRRUUNN AAFFFFEECCTTEEDD RRMM PP OOFFFFTTHHEENN OONN TTOO RREESSEETTIIFF NNOO HHEELLPP,, TTHHEENN RR EESSEETT::VVUU 4499 BB22 FFMM GGCC 11VVUU 112211 MM 1177 FFMM GGCC 22RESET CB’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE



2- PROGRESS OF POWER-UP TESTSDURATION:120 SEC FLIGHT DECK EFFECTS:ECAM STATUS PAGE: AP 1(2) INOP






2233 TTCCAASS IINNOO PP MM SSGG VVUU 112211 KK1100 TTCCAASSNNOOTTEE SSYYSS TT EESSTT TTHHRRUU MM CCDDUUAALLSSOO WWOORRKK SS



2233CCOOMM VVHHFF

EEMM IITTTTIINNGG FFAAUULLTTCCHHEECCKK::TTRRAANNSSMM IITTIIOONN KKEEYY OONN AAUUDDIIOOPPAANNEELLSSIIDDEE SSTTIICCKK RR AADDIIOO SSEELLHHAANNDD MM IIKKEE SSEELL NNOOTT IINN TTRR AANNSSPPOOSSIITTIIOONNIIFF NNOOTT FFOOUUNNDD IINN TTRR AANNSS PPOO SSRREESSEETT::VVUU 4499 GG99 VVHHFF 11**VVUU 112211 LL44 VVHHFF 22**VVUU 112211 LL55 VVHHFF 33**IIFF NNOO HHEELLPP LLEEAAVVEE CC ..BB..OOPPEENN((PPUULLLLEEDD))** RREEFF FFLLIIGGHH TTMMAANNUUAALL 77--5588



2233 VVHHFF SSYYSSTTEEMM IINNOOPP VVUU 4499 GG99 VVHHFF 11((SSYYSS11))VVUU 112211 LL44 VVHHFF 22((SSYYSS22))VVUU 112211 LL55 VVHHFF33((SSYYSS33))




2244ECAM MSG RELATED TO TRIPPED GREEN CB’S

NNOO RREEQQUUIIRREEMM EENNTTHHOOWWEEVVEERR,, IIFF TTIIMM EE PPEERRMM IITTSSRREESSEETT MM AAYY BBEE AATTTTEEMM PPTTEEDD,,IIFF UUNNSSUUCCCCEESSFFUULL,, DDOO NNOOTTMM AAKKEE AA SSEECCOONNDD AATTTTEEMM PPEETTFFLLTT MM AANNUUAALL 77--5577

2244EENNGGIINNEE 11((22))GGEENNEERR AATTOORR OONNLLIINNEE ((GGRREEEENNLLIINNEE)) AANNDDPPAARR AAMM EETT EERRSS NNOOTTSSHHOO WWNN

EENNGGIINNEE ((SS)) MM UUSSTT BBEE SSHHUUTTDDOOWWNNVVUU 112222 TT2266 GGCCUU 11 ((EENNGG 11))VVUU 112222 TT2277 GGCCUU 22 ((EENNGG 22))RESET CB’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE



TESTS FAIL: (FAULT CONFIRMED)PROCEED TO MEL/TSM FOR DEFERAL/TROUBLESHOOTIMG


HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 15MS.A/C CONFIGURATION:1-A/C ON GROUND WITH ENGINES STOPPED

2- PROGRESS OF POWER-UP TESTSDURATION: 30 MS

FLIGHT DECK EFFECTS:NONE






2244NO “AVAIL” GREEN LEGEND DISPLAYED ON “EXT PWR” PUSHBUTTON SWITCH

EENNGGIINNEESS AANNDD AAPPUU SSHHUUTT DDOO WWNNAANNDD GGRROOUUNNDD PPOO WWEERRCCOONNNNEECCTTEEDDVVUU 112222 YY2244 GGPPCCUURESET CB’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE

2244BBAATTTTEERRYYCCHHAARR GGEE LLIIMM IITTEERR((BBCCLL))

RREESSEETT SSHHIIPPSS BBAATTTTEERRIIEESS OONNEEAATT AA TTIIMM EE WWIITTHH AAPPUUOOPPEERR AATTIINNGGIIFF HHEELLPP,, TTHHEENN RREESSEETT::VVUU 110055 NN//AA BBAATT RR EEFF BBLLCC 11VVUU 110055 NN//AA BBAATT BBUUSS RREEFF BBLLCC 11VVUU 110055 NN//AA BBAATT RR EEFF BBLLCC 22VVUU 110055 NN//AA BBAATT BBUUSS RREEFF BBLLCC 22


HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: NONEA/C CONFIGURATION:1-A/C ON GROUND, ENGINES STOPPED, APU STOPPEDGROUND POWER UNIT CONNECTED TO THE A/C

2- PROGRESS OF POWER-UP TESTSDURATION: 35 MS

FLIGHT DECK EFFECTS:NONE









2244TRANSFORMER RECTIFIER FAULTS

RREESSEETT TT//RR TTHHRROOUUGGHH MM CCDDUU OORRRREESSEETT AALLLL TTHHRREEEE UUSSIINNGGGGUUAARRDDEEDD BBUUTT TTOONN OONN 110033 VVUUPPAANNEELL IINN EELLEECCTTRRIICCAALL BBAAYY

2255CCRREEWW SSEEAATTPPRROOBBLLEEMM SS

VVUU 112222 UU1111 CCKKPPTT SSEEAATT CCTTLLCCAAPPTTVVUU 112222 UU1144 CCKKPPTT SSEEAATT CCTTLL FF//OOAADDDDTTIIOONNAALL CC..BB.. IISS LLOOCCAATTEEDDUUNNDDEERR EEAACCHH SSEEAATT OONN TTHH EECCOONNTTRROOLL BBOOXX










2266FWD AND AFT CARGO DETECT MSGS

VU 49 C6 SDCU CHAN 1VU 122 T18 SDCU CHAN2NOTE: RESET C.B.’S TOGETHERIF NO HELP, THEN RESET:VU 49 C6 SDCU CHAN1VU 122 T18 SDCU CHAN 2VU 49 AFT CARGO VENT&HTG FANRESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE

2266FFWWDD AANNDD AAFFTTCCAARR GGOO HH EEAATTDDEETTEECCTT FFAAUULLTT SS

VVUU 4499 AAFFTT CCAARR GGOO VVEENNTT &&HHEEAATTCCTTLL//MM OONNGGVVUU 112222 SS2222 AAFFTT CCAARR GGOOVVEENNTT&&HH TTGG FFAANNRESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE


HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 200 MSA/C CONFIGURATION:1-A/C ON GROUND

2- PROGRESS OF POWER-UP TESTSDURATION: 10 SECFLIGHT DECK EFFECTS:NONE













2266LAV SMOKE DETECT MSG

VU 49 C6 SDCU CHAN 1VU 122 T18 SDCU CHAN2RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE

2277SSIIDDEE SSTTIICCKKPPRRIIOORRTTYY MM SSGG

FFAACC 11&&22 SSWWIITTCCHH EESSSSEECC 11,,22&&33 SSWWIITTCCHHEESSEELLAACC 11&&22 SSWWIITTCCHH EESS













2277SEC 1,2 OR 3 FAULTS

USE PUSH BUTTON SWITCHES FIRSTIF NO HELP, THEN RESETVU 49 B8 1 NORM SPLY SEC 1VU105 N/A SEC1 STBY SPLY SEC1 VU 121 Q18 SEC 2 SPLY SEC 2VU 121 Q19 SEC 3 SPLY SEC3RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE

2277EELLAACC 11 OORR 22FFAAUULLTTSS

USE PUSH BUTTON SWITCHES FIRSTIF NO HELP, THEN RESETVU49 B11 ELAC1 NORM SPLY ELAC 1VU105 N/A ELAC1 STBY SPLY ELAC1 VU121 R20 ELAC2 SPLY ELAC 2VU105 N/A ELAC2 STBY SPLY ELAC2RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE


HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 5SECA/C CONFIGURATION:HYDRAULIC SYSTEM DE-PRESSURIZED

2- PROGRESS OF POWER-UP TESTSDURATION: 18 SECFLIGHT DECK EFFECTS:ECAM F/CTL PAGE: SEC AMBER IND., ASSOCIATED ELEVATORS CROSSED, ASSOCIATED SPOILERS AMBER CROSSED THEN FLASHING AT THE END OF THE TEST.ECAM WARNING:F/CTL SEC 1(2)(3) FAULT DURING AROUND 23 SEC.FLT CONTROL PANEL: SEC FAULT LEGEND IS FLASHING AT THE BEGINNING AND AT THE END OF TEST.3-RESULTS OF POWER-UP TESTSTESTS PASS:

ABOVE MENTIONED FAULT MSG NO LONGER DISPLYEDTESTS FAIL: (FAULT CONFIRMED)PROCEED TO MEL/TSM FOR DEFERAL/TS


HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 30 MS BY C/B OR RESET PUSHBUTTON OFF THEN ONA/C CONFIGURATION:HYDRAULIC SYSTEM DE-PRESSURIZED

2- PROGRESS OF POWER-UP TESTSDURATION: 8 SECFLIGHT DECK EFFECTS:ECAM F/CTL PAGE: ELAC AMBER INDICATION AND ASSOCIATED AILERON SERVO CONTROL AMBER BOXEDECAM WARNING: F/CTL ELAC1(2) FAULT DISPLAYED DURING 8 SEC. IF SUBSEQUENT TO C/B RESETNOTE: NONE IF SUBSEQUENT TO PUSHBUTTON RESETFLT CONTROL PANEL:FAULT LEGEND ILLUMINATED DURING 8SEC.3-RESULTS OF POWER-UP TESTSTESTS PASS:




2277 FFLLIIGGHH TT CCOONNTTRROOLLFFLLAAPPSS LLOOCCKKEEDD

OOUUTT

MM UUSSTT PPEERR FFOOMM EEDD WWIINNGG TTIIPPBBRRAAKK EE((WWTTBB)) RREESSEETT TTHHRROOUUGGHHMM CCDDUU PPEERR AAMM MM 2277--5500--0000 PPGG220099--221111 ((HHYYDD MM UUSSTT BBEE OO FFFF))



2277FLT/CTL MSG WITH SLAT/FLAP FAULTS

VU 49 B6 SLT CTL & MONG SYS 1VU 49 B7 FLP CTL 7 MONG SYS 1 VU 121 R21 SLT CTL SYS 2VU 121 Q21 FLP CTL & MONG SYS 2RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE


HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 200 MSA/C CONFIGURATION:A/C ON GROUND WITH ENGINES STOPPED AND NEW DATE FROM CFDS2- PROGRESS OF POWER-UP TESTSDURATION: 2 SECFLIGHT DECK EFFECTS:ECAM WARNING: IF HYDRAULIC PRESSURIZED: FLT CTL SLAT SYS 1(2) OR FLAP SYS1(2) FAULTIF HYDRAULIC CIRCUIT NOT PRESSURIZED:NONE3-RESULTS OF POWER-UP TESTSTESTS PASS:ABOVE MENTIONED FAULT MSG NO LONGER DISPLYEDTESTS FAIL: (FAULT CONFIRMED)PROCEED TO MEL/TSM FOR DEFERAL/TS




2277FLT/CTL MAINTENANCE MSG(CAN BE DEFERRED)

VU 49 B10 FCDC 1 SPLYVU 121 Q20 FCDC 2 SPLYRESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE

2277SSLLOO WW SSLLAATTSS VU 49 B6 SLT CTL & MONG SYS 1

VU 121 R21 SLT CTL SYS 2RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE


HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >3SECA/C CONFIGURATION:A/C ON GROUND AND ENGINES STOPPED

2- PROGRESS OF POWER-UP TESTSDURATION: 3 SECFLIGHT DECK EFFECTS:ECAM WARNING:F/CTL FCDC 1(2) FAULT DURING 3 SEC.




HOW LONG THE COMPUTER MUST BE DE-ENERGIZED:>200 MS

A/C CONFIGURATION:A/C ON GROUND WITH ENGINES STOPPED AND NEW DATE FROM CFDS

2- PROGRESS OF POWER-UP TESTSDURATION: 2 SECFLIGHT DECK EFFECTS:ECAM WARMING: IF HYDRAULIC PRESSURIZED: FLT CTL SLAT SYS 1(2) OR FLAP SYS1(2) FAULTIF HYDRAULIC CIRCUIT NOT PRESSURIZED:NONE






2288FQI INOP VU 49 A13 FQI CHAN 1

VU 121 M27 FQI CHAN 2VU 121 L26 FQI CHAN 1&2RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE

2288FFUUEELL AAPPUU LLPPVVAALLVVEE FFAAUULLTTMM SSGG.. TTRRIIGGGGEERREEDDWWHHEENN TTHHEE AAPPUUMM AASSTT EERR SSWW IISSSSEELLEECCTTEEDD OOFFFFDDUURRIINNGG NNAA EEMM EERRSSHHUUTT DDOO WWNN OORRSSHHUUTT DDOO WWNN

CYCLING THE MASTER SWITCH ON THEN OFF MAY CLEAR THIS MSGREF FLT MANUAL 7-114RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE


HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >1SECA/C CONFIGURATION:A/C ON GROUND AND REFUEL PANEL DOOR OPEN

2- PROGRESS OF POWER-UP TESTSDURATION: 80 SEC MAXIMUMFLIGHT DECK EFFECTS:ECAM FUEL PAGE: INTER-CELL TRANSFER VALVE INDICATION MOVING, AMBER “XXX” IN PLACE OF FUEL QUANTITY INDICATIONS THEN NORMAL INDICATONS ARE DISPLAYED







2299 HHYYDD RREEVVSS LLOO WWPPRREESSSSUURREE MMSSGG

TTOO CC LLEEAARR:: RRUUNN EENNGGIINNEESS OORRPPRREESSSSUURR IIZZEE HHYYDDRR AAUULLIICCRREESSEERR VVOO IIRR SS WWIITTHH AAPPUU..NNOOTTEE:: TTHH IISS HHAAPPPPEENNSS AAFF TTEERRWWOORRKK IINNGG OONN HHYYDDRR AAUULLIICC SSYYSSTTEEMM



2299 PPTTUU FFAAUULLTTSS ((NNOO TTCCAAUUSSEEDD BBYY CC AARR GGOODDOOOORR OOPPEERRAATTIIOONN

AAFF TTEERR EENNGGIINNEESSSSTTAARR TTSS))

VVUU 112211 NN3344 SSOOLL VVAALLVVEE GG//YY PP TTUU



2299 PPTTUU FFAAUULLTTSS SSEEEE NNOO TTEESS TTHH AATT FFOOLLLLOO WWRREEGGAARRDDIINNGG FF AAUULLTTSS

FFAAUULLTTSS CC AAUUSSEEDD BBYY CCAARRGGOODDOOOORR OOPPEERRAATTIIOONN WWIITTHH IINN3300 SSEECCOONNDDSS AAFF TTEERR SSEECCOONNDDEENNGGIINNEE SSTTAARR TT AANNDD PP TTUUEECC AAMM FFAAIILLUURR EE MMEESSSSAAGGEESSNNOOTTEE:: TTHH IISS PPRROOCCEEDDUURREEWWIILLLL NNOO TT RR EESSEETT RR EEAALL PP TTUUFFAAIILLUURREESS OORR HH IIDDEE RREEAALLFFAAUULLTTSS IINN TTHH EE PP TTUU SSYYSSTTEEMM

RREESSEETT WWIITTHH EENNGGIINNEESS RR UUNNNNIINNGG::AA))RREESSEETT MMEESSSSAAGGEE UUSSIINNGGMMAASSTTEERR//CC AAUUTTIIOONN PPUUSSHHBBUUTTTTOONNSSWWIITTCCHHEESSBB))SSEELLEECC TT HHYYDD PP AAGGEE OONN EECC AAMMCC))SSEELLEECC TT YY HHYYDD EELLEECC PPMMPP OONNDD))SSEELLEECC TT YY HHYYDD EELLEECC PPMMPP OOFFFFEE))WWAAIITT AA MM IINNIIMMUUNN OOFF 3300 SSEECCFF))CCYYCCLLEE PP TTUU SSWWIITTCCHH FFRROOMM OONN TTOOOOFFFF TTOO OONNGG))SSEELLEECC TT##11 EENNGGIINNEE GGRREEEENN HHYYDDPPMMPP OOFFFFHH))SSEELLEECC TT##11 EENNGGIINNEE GGRREEEENN HHYYDDPPMMPP OONNII))SSEELLEECC TT##22 EENNGGIINNEE YY HHYYDD PPMMPP OOFFFFPPTTUU SSHHOOUULLDD OOPPEERR AATTEE GGRR EEEENN TTOOYYEELLLLOO WWJJ ))SSEELLEECC TT##22 EENNGGIINNEE YYEELLLLOO WW HHYYDDPPMMPP OONNKK))EECCAAMM SSHHOOUULLDD BBEE NNOORRMM AALL




3300ANTI ICE L ( R ) WINDSHIELD

IF THE WARNING OCCURS ON THE GROUND WITH OAT GREATER THAN 40 DEG C AND AC PACKS OFF, 5 MIN AFTER BOTH PACKS ARE SELECTED ON, RESET CB’SVU 121 X13 WHC 1 (LEFT SIDE)VU 122 W13 WHC 2 (RIGHT SIDE)RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE

3300WWIINNDDSSHHIIEELLDDHHEEAATT FFAAUULLTTSS

VU 122 X13 1(LEFT SIDE)VU 122 X14 WINDOW L HEATVU 122 W13 WHC 2 (RIGHT SIDE)VU 122 W14 WINDOWS R HEATRESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE


HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 5SECA/C CONFIGURATION:A/C ON GROUND

2- PROGRESS OF POWER-UP TESTSDURATION: 5 SEC FLIGHT DECK EFFECTS:NONE











3300FWD (AFT) DRAIN MASTER ECAM MSG

VU 2000 D1 FWD DRAIN MASTERVU 2001 D5 AFT DRAIN MASTER 3300

AANNTTII IICCEE MM SSGGSS VU 49 D3 ANT ICE PROBES PHC 1VU 122 Y12 ANTI ICE PROBES PHC2 VU 122 Y16 ANTI ICE PROBES PHC 3RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE










3300 AANNTTII IICCEE PPRROOBBEEMM SSGGSS SSYYSSTTEEMM ##11

VVUU4499 DD22 PPIITTOO TT 11VVUU 112222 ZZ1133 AATT AATTIICC 11VVUU4499 DD44 AAOO AA 11VVUU 112222 ZZ1122 TT AATT 11IIFF NNOO HHEELLPP,, TTHHEENN RREESSEETT ::VVUU4499 FF77 AADDIIRRUU 11&&AAOO AA 2266 VVAACCVVUU4499 TT66 AADDIIRRUU 11 111155 VVAAVVUU 110055 NN//AA AADDIIRRUU 11 2288 VVDDCC



3300 AANNTTII IICCEE PPRROOBBEEMM SSGGSS SSYYSSTTEEMM ##22

VVUU 112222 YY1144 PPIITTOOTT 22VVUU 112222 YY1111 SSTT AATTIICC 22VVUU 112222 YY1133 AAOO AA 22VVUU 112222 YY1155 TT AATT 22IIFF NNOO HHEELLPP,, TTHHEENN RREESSEETT ::VVUU 112211 NN99 AADDIIRRUU 22 2266VVAACC&& AAOO AAVVUU 112211 NN77 AADDIIRRUU 22 111155 VVAACCVVUU112211 NN55 AADDIIRRUU 22 2288 VVDDCCVVUU 112211 NN1111 AADDIIRRUU 22 PPWWRR SSHHEEDD



3300 AANNTTII II CCEE PPRROOBBEEMM SSGGSS SSYYSSTTEEMM ##33

VVUU 112222 ZZ1166 PPIITTOOTT 33VVUU 112222 ZZ1144 SSTT AATTIICC 33VVUU 112222 ZZ1155 AAOO AA 33IIFF NNOO HHEELLPP,, TTHHEENN RREESSEETT ::VVUU 112211 NN88 AADDIIRRUU 33 2266VVAACC&& AAOO AAVVUU 112211 NN66 AADDIIRRUU 33 111155 VVAACCVVUU 112211 NN44 AADDIIRRUU 33 2288 VVDDCCVVUU 4499 FF99 AADDIIRRUU 33 SSTT WWGG SSPPLLYYVVUU 112211 NN1100 AADDIIRRUU 33 SSTT WWGG SSPPLLYY





3311DMC FAULT MSG EIS DMC 1,2 OR 3

VU 49 E11 EIS DMC 1 SPLY (SYS1VU 121 Q8 EIS DMC 2 SPLY(SYS) VU 121 Q9 EIS DMC 3 SPLY (SYS3)VU 49 E10 EIS DMC 3 STBY SPLY (SYS3)RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE

3311UUNNAABBLLEE TTOOSSWWIITTCCHH DDUU

VU 49 E4 EIS PFD CAPT SWTGVU 49 E2 EIS ND CAPT SWTGVU 121 R5 EIS PFD F/O SWTGVU 121 R6 EIS ND F/O SWTGVU 49 E6 EIS ECAM DU UPPER SWTGVU 49 E6 EIS ECAM DU UPPER SWTGVU 121 R10 ECAM DU LOWER SWTGRESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE


HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >1SECA/C CONFIGURATION:A/C ON GROUND

2- PROGRESS OF POWER-UP TESTSDURATION: 4 SECFLIGHT DECK EFFECTS:ECAM WARNING:EIS DMC 1 OR 2 OR 3 FAULTNOTE: A DIAGONAL IS DISPLAYED ON THE THRRE ASSOCIATED DIPLAYED UNITS








3311NO AIDS INDICATION DISPLAYED ON THE MCDU MENU PAGE

VU 121 K15 AIDS DMU & QARRESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE 3311

AADDIIRRUU FFAAUULLTT VU 49 F6 ADIRU A 115 VAC SYS1VU 105 ADIRS ADIRU 1 28VDCVU 121 N7 ADIRU 2 115VAC (SYS2)VU 121 N5 ADIRU 2 28VDC (SYS2) VU 121 N6 ADIRU 3 115VAC (SYS3) VU 121 N4 ADIRU 3 28VDC (SYS3)RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE



2- PROGRESS OF POWER-UP TESTSDURATION: 40 SEC FLIGHT DECK EFFECTS:ECAM WARNING: NONENOTE: A DIAGONAL IS DISPLAYED ON THE THREE ASSOCIATED DISPLAY UNITS

3-RESULTS OF POWER-UP TESTSTESTS PASS:AIDS PROMPT RETURNS



HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 15 SEC

A/C CONFIGURATION:A/C ON GROUND AND IR 1(2)(3) ROTARY BUTTON (LOCATED ON THE ADIRS PANEL) SWITCHED TO OFF FOR 15 SEC, THEN TO NAV.

2- PROGRESS OF POWER-UP TESTSDURATION: 5 SECFLIGHT DECK EFFECTS:ADIRS PANEL: “ON BAT” LEGEND ILLUMINATED FOR 5 SEC, 2 SEC AFTER POWER-UP TEST INITIALIZATION.






3311ECAM PAGE(S) LOCKED (I.E. DOORS-WHEELS ETC.)

VU 49 F1 FWS FWC 1 SPLYVU121 Q7 EIS FWC 2 SPLY & QARRESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE

3311SSDDAACC 11 OORR 22FFAAUULLTTSS

VU 49 F2 SDAC 1 26VAC SYNC AC ESS BUSVU 49 F4 SDAC 1 SPLYVU121 Q3 SDAC1 26VAC SYNC ACVU121 Q4 SDAC1 26VAC SYNC AC VU 121 P4 SDAC 1 28 VACVU 49 F5 SDAC1&2 28VAC ESS BUSVU121 Q2 SDAC2 26VAC SYNC AC VU121 Q5 SDAC2 26VAC SYNC AC VU 121 Q6 SDAC 2 SPLYVU 121 P3 SDAC 2 28 VACRESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE



2- PROGRESS OF POWER-UP TESTSDURATION: 50 SEC FLIGHT DECK EFFECTS:ECAM WARNING: “EIS 1(2) FWS FAULT”

3-RESULTS OF POWER-UP TESTSTESTS PASS:AIDS PROMPT RETURNS




A/C CONFIGURATION:A/C ON GROUND

2- PROGRESS OF POWER-UP TESTSDURATION: 5 SECFLIGHT DECK EFFECTS:ECAM WARNING: “EIS 1(2) SDAC FAULT”






3322LGCIU FAULTS SYSTEM #1

VU 49 C9 L/G LGCIU SYS1VU 121 Q34 HYD LGCIU SYS 1 SPLYRESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE

3322 LLGGCCIIUU FFAAUULLTTSSSSYYSSTT EEMM ##22

VU121 Q35 HYD LGCIU SYS 2 RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE




2- PROGRESS OF POWER-UP TESTSDURATION: 210 MSEC FLIGHT DECK EFFECTS:LGCIU 1LDG GEAR PANEL “UNLK” RED INDICATIONS ARE FLASHING BRIEFLYLGCIU 2: NONE






2- PROGRESS OF POWER-UP TESTSDURATION: 210 MSEC FLIGHT DECK EFFECTS:LGCIU 2LDG GEAR PANEL “UNLK” RED INDICATIONS ARE FLASHING BRIEFLYLGCIU 1: NONE





3322 BBSSCCUU FFAAUULLTT SS IIFF AA//CC NNOO TT MM OOVVIINNGG TTUURRNN NNOOSSEEWWHHEEEELL SSTTEEEERRIINNGG AANNDD AANNTTII--SSKKDD OOFFFF TTHHEENN OONN,, IIFF NNOO HHEELLPP,,SSEEEE BBSSCCUU SSYYSSTTEEMM FFAAUULLTTSS 11&&22OONN FFOOLLLLOO WWIINNGG PPAAGGEESS..





3322 BBSSCCUU FFAAUULLTT SSSSYYSSTT EEMM ##11

VVUU 112211 MM 3333 BBSSCCUU SSYYSS11 SSPPLLYYVVUU 112211 MM 3344 BBSSCCUU SSYYSS11 CCTTLLRESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE










3322BSCU FAULTS SYSTEM #2

VVUU 112211 MM 3355 BBSSCCUU SSYYSS22 CCTTLLVVUU 112211 MM 3366 BBSSCCUU SSYYSS22 SSPPLLYYRESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE

3322 NNOO BBRR AAKKEE TT EEMM PPSSDDIISSPPLLAAYYSS

VU121 M32 BRK TEMP DET UNIT RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE











3333 NNOO LLIIGGHH TT IINN MM LLGGWWHHEEEELL

VVUU 22000011 FF55 LLIIGGHHTT SSEECC 1199



3333 AAPPUU AARREEAA LLIIGGHHTTSSIINNOOPP

VVUU 22000011 FF66 AAPPUU SSVVCC LLIIGGHHTT



3333 CCAABBIINN LLIIGGHHTT SSWWIILLLL NNOOTT TTUURRNN

OONN

RREESSEETT ##22 CCIIDDSS TTHHRROOUUGGHH MM CCDDUUIIFF NNOO HHEELLPP,, TTHHEENN RREESSEETT ::VVUU 112211 MM 88 TTHHRRUU MM 1133 DDEEUU



3333 CCAABBIINN LLIIGGHHTT SSRREEMM AAIINNSS OONN

BBRRIIGGHHTT WWHHEENNSSEELLEECCTTEEDD OOFFFF OORR

DDIIMM

CCHHEECCKK IIFF CCOORRRR EECCTT LLAAMM PPIINNSSTT AALLLLEEDD IIFF CCHHEECCKK CCIIDDSSTTHHRROOUUGGHH TTHHEE PPTTPP FFOORR FFAAIILLEEDDDDEEUU AANNDD RR EESSEETT DDEEUU IIFFPPOOSSSSIIBBLLEE..NNOOTTEE:: AALLLL LLIIGGHHTT SSCCOONNTTRROOLLLLEEDD BBYY TTHHEE FFAAIILLEEDDDDEEUU WWIILLLL RREEMM IIAANN OONN BBRRIIGGHH TT






3344DAR MSG MM SSGG MM AAYY BBEE RREELLAATTEEDD TTOO

MM EEDDIIAA((TT AAPPEE)) BBEEIINNGG FFUULLLLVVUU 112211 KK1155 DDMM UU && QQAARRVVUU 112211 KK1177 FFDDIIUU && QQAARRVVUU 112211 KK1188 AACCCCLLMMRESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE

3344FFLLTT RREECCOORRDDEERRPPRROOBBLLEEMM IINNFFLLIIGGHH TT OORR RR EECCMM SSGG

VU 121 K17 FCDR FDIU & QARRESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE



A/C CONFIGURATION:A/C ON GROUND AND ENGINES STOPPED

2- PROGRESS OF POWER-UP TESTSDURATION: 40 SEC FLIGHT DECK EFFECTS:MCDU “<AIDS” INDICATION DISAPPEARS






2- PROGRESS OF POWER-UP TESTSDURATION: 25 SEC MAX FLIGHT DECK EFFECTS:ECAM WARNING:”RECORDER FDIU FAULT” IS DISPLAYED 3 SEC3-RESULTS OF POWER-UP TESTSTESTS PASS:





3344 GGPPWWSS FFAAUULLTT SS

VU 121 P6 EIS GPWS 28VDCVU 121 P7 EIS GPWS 115VACTHIS PROBLEM MAY BE BY ILS FREQ’S THAT ARE CLOSE AND INTERFERING WITH THE GPWS SYSTEMHAVE FLT CREW TAXI FWD 2-4 FEET THIS WILL CAUSE THE GPWS RECHECK ITSELF AND MOST CASES CLEAR ALL FAULTSRESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE

3344

WWIINNDDSSHHEEAARR DDEETTFFAAUULLTT

ON THE GROUND MSG MAY OCCUR SPURIOUSLY, RESET FACS. REF FLT MANUAL 7-139ATTEMPT PUSHBUTTON SWITCHES RESET FIRST, IF NO HELP, THEN RESETVU 49 B3 FAC 1 26VACVU 49 B4 FAC 1 28VDCVU 121 M18 FAC 2 26VACVU 121 M19 FAC 2 28VDCRESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE




2- PROGRESS OF POWER-UP TESTSDURATION: 25 SEC MAX FLIGHT DECK EFFECTS:ECAM WARNING:”RECORDER FDIU FAULT” IS DISPLAYED 3 SEC3-RESULTS OF POWER-UP TESTSTESTS PASS:



HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >4 SEC

A/C CONFIGURATION:1-A/C ON GROUND AND ENGINES STOPPED FOR ELECTTRICAL POWER-UP TESTS2-A/C ON GROUND AND HYDRAULICALLY ENERGIZED FOR YAW DAMPER POWER LOOP POWER-UP TESTS2- PROGRESS OF POWER-UP TESTSDURATION: 1- 90 SEC 2- 5 SECFLIGHT DECK EFFECTS:AUTO FLT RUDDER TRIM 1(2)AUTO FLT RUD TRAV LIM 1(2)FLT CTL PANEL-“FAUTL” LEGEND FLASHES





3355O2 LOW PRESSURE MSG

IINNSSUURREE CCRR EEWW OO22 SSUUPPPPLLYYSSWWIITTCCHH IISS OONN





3366 BBMM CC VVUU 4499 DD1111 AAIIRR BBLLEEEEDD EENNGG 11MM OONNGG((BBMM CC 11))VVUU 112222 ZZ2222 AAIIRR BBLLEEEEDD EENNGG 22MM OONNGG ((BBMM CC 22))



3366 AAIIRR RR ((LL)) WWIINNGGBBLLEEEEDD LLEEAAKK ((OORR

AAPPUU BBLLEEEEDD LLEEAAKK))MM SSGG AAFFTTEERR

EELLEECCTTRRIICCAALLTTRRAANNSSIIEENNTT SS

AARREEAA LLIIGGHHTT SSIINNOOPP

RREESSEETT AAFFFFEECCTTEEDD BBLLEEEEDDPPUUSSHHBBUUTT TTOONN SSWWIITTCCHH OONN TTOOOOFFFF TTOO OONN TTOO CCLLEEAARR MM SSGG..RREEFF.. FFLLTT MM AANNUUAALL BBUULLLLEETTIINN9955--0011






3366LEFT WING LEAK MSGS

VVUU 4499 DD1111 AAIIRR BBLLEEEEDD EENNGG 11MM OONNGG((BBMM CC 11))VVUU 4499 DD1122 AAIIRR BBLLEEEEDD EENNGG 11 CCTT LLRESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE

3366RRIIGGHHTT WWIINNGGLLEEAAKK MM SSGG

VU 122 Z22 AIR BLEED ENG 2 MONG(BMC 2)VU 122 Z33 AIR BLEED ENG 2 CTLRESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE




2- PROGRESS OF POWER-UP TESTSDURATION: 10 SEC FLIGHT DECK EFFECTS:ECAM BLEED PAGE: BLEED TEMPERATURE INDICATION RESET TO 0 DEG.ENG 1 (2) BLEED AND APU BLEED PUSHBUTTON; LIGHT FLASHING






2- PROGRESS OF POWER-UP TESTSDURATION: 10 SEC FLIGHT DECK EFFECTS:ECAM BLEED PAGE: BLEED TEMPERATURE INDICATION RESET TO 0 DEG.ENG 1 (2) BLEED AND APU BLEED PUSHBUTTON; LIGHT FLASHING3-RESULTS OF POWER-UP TESTSTESTS PASS:





3366CROSS BLEED VALVE MSG

VVUU 4499 DD1133 AAIIRR BBLLEEEEDD XXFFEEEEDDVVAALLVVEE BBAATTVVUU 112222 ZZ2200 AAIIRR BBLLEEEEDD XXFFEEEEDDVVAALLVVEE NNOORRMM AALLRESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE

3366CCRROOSSSS BBLLEEEEDDFFAAUULLTTSS UUSSEE IINNAADDDDIITTIIOONN TTOOXXFFEEEEDD VVAALLVVEEFFAAUULLTTSS((MM SSGG))

VU 49 D11 AIR BLEED ENG 1 MONG(BMC 1)VU 49 D12 AIR BLEED ENG 1 CTLVU 122 Z 22 AIR BLEED ENG 1 MONG(BMC 2)VU 122 Z33 AIR BLEED ENG2 CTLVU 49 F4 SDAC 1 SPLYVU 121 Q SDAC 2 SPLYRESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE






2- PROGRESS OF POWER-UP TESTSDURATION: 5 SEC FLIGHT DECK EFFECTS:ECAM WARNING; “EIS SINGLE SDAC FAULT3-RESULTS OF POWER-UP TESTSTESTS PASS:ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED




3388 LLOOSSSS OOFF WWAATTEERRQQUUAANNTTIITTYY

VVUU 22000000 DD33 WWAATTEERR SSYYSSTTEEMM



3388 TTOOIILLEETT WWIILLLL NNOOTTFFLLUUSSHH

VVUU 22000011 BB11 VVAACC TTOOIILLEETT SSYYSS LLAAVVVVUU 22000011 BB33 VVAACC TTOOIILLEETT SSYYSS LLAAVVVVUU 22000011 BB44 VVAACC TTOOIILLEETT SSYYSS LLAAVV



3388 GGAALLLLEEYY WWAATTEERRSSYYSS NNOOIISSEE

RREEMM OOVVEE AAFFTT GGAALLLLEEYY RRIIGGHHTTCCOOFFFFEEEE MM AAKKEERR AANNDD PPLLAACCEEFFIINNGGEERR TTIIPP OO VVEERR DDRR AAIINN TTUUBBEE,,TTHHIISS WWIILLLL RREESSEEAATT TTHHEE CCHHEECCKKVVAALLVVEE






4499APU BLEED FAULTS

SSHHUUTT DDOO WWNN AAPPUU AANNDD RREESSEETTCC..BB..’’SSVVUU 112211 LL4411 EECCBB SSPPLLYYVVUU 112211 LL4422 AAPPUU CCTTLLRESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE

4499AAPPUU WWIILLLL NNOOTTSSHHUUTT DDOO WWNN

OPEN THESE C.B.’SVU 121 L42 APU CTL

IIFF NNOO HHEELLPP,, TTHHEENN RREESSEETT ;;VVUU 112211 LL4411 EECCBB SSPPLLYY


HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: NONE

A/C CONFIGURATION:A/C ON GROUND AND APU STOPPEDAPU CONTROL PANEL; MASTER SWITCH”ON’

2- PROGRESS OF POWER-UP TESTSDURATION: 3 SEC MAXFLIGHT DECK EFFECTS:APU CONTROL PANEL; ‘FAULT ON MASTER SWITCH PUSH-BUTTON




TESTS PASS:





4499APU ELEC NO VOLTS OR FREQS

SSEELLEECCTT AAPPUU EELLEECC OOFFFF AANNDDRREESSEETT TTOO OONNIIFF NNOO HHEELLPP,, TTHHEENN RREESSEETT ::VVUU 11221111 YY2255 EELLEECC AAPPUU GGCCUURESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE

7733FFAADDEECC FFAAUULLTTMM SSGGSS ““EENNGG 11((22))FFAADDEECC FFAAUULLTT OORR““EENNGG 11((22)) FFAADDEECC AAOORR BB FFAAUULLTTNNOOTT RREELLAATT EEDD TTOORREEAALL FFAAIILLUURREE

TRUN FADEC PUSHBUTTON SWITCH ON THEN OFF TO RESET FADECIF NO HELP, THEN RESETVU49 A4 ENG1 FADEC A& EIU 1VVUU112211 RR4411 EENNGG11 FFAADDEECC BB&&EEIIUU11VVUU4499 AA55 EENNGG22 FFAADDEECC AA&&EEIIUU 22VVUU 112211 QQ4400 EENNGG22 FFAADDEECC AA&&EEIIUU 22


HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 15 MS

A/C CONFIGURATION:A/C ON GROUND AND ENGINE STOPPED

2- PROGRESS OF POWER-UP TESTSDURATION: 30 MSFLIGHT DECK EFFECTS:NONE





A/C CONFIGURATION:A/C ON GROUND AND ENGINE STOPPED

2- PROGRESS OF POWER-UP TESTSDURATION: 2 SEC MAXFLIGHT DECK EFFECTS:NONE


TESTS PASS:





7733ENG 1(2) EPR MODE FAULT MSG

RREECCOOVVEERRYY OOFF EEPPRR OONN BBOOTTHHEENNGGIINNEESS MM AAYY AATTTTEEMM PPEEDD BBYYSSWWIITTCCHHIINNGG OO FFFF EEAACCHHEENNGGIINNEE”” SS NN11 MM OODDEE SSWWIITTCCHHRREEFF FFLLTT MM AANNUUAALL 77--8866

7799EENNGG 11((22)) OOIILLFFIILLTTEERR CCLLOO GG

MAINTENANCE ACTION REQUIRED!EXCEPT WHEN WARNING IS TEMPORARILY DISPLAYED DURING ENGINE START WITH ENGINE OLI TEMP. BETWEEM 10° - 32° CREF. FLT MANUAL 7-80


ABOVE MENTIONED FAULT MSG NO LONGER DISPLYEDTESTS FAIL: (FAULT CONFIRMED)

PROCEED TO MEL/TSM FOR DEFERAL/TROUBLESHOOTING


TESTS PASS:


AA332200--223322FFAAUULLTT VVEERRIIFFIICCAATTIIOONN GGUUIIDDEE

TTHHIISS DDOOCCUUMMEENNTT IISS FFOORR TTRRAAIINNIINNGG PPUURRPPOOSSEESSOONNLLYY AANNDD WWIILLLL NNOOTT BBEE RREEVVIISSEEDD AALLWWAAYYSS

RREEFFEERR TTOO UUAA MMAANNUUAALLSS FFOORR CCUURRRREENNTTAAPPPPRROOVVEEDD PPRROOCCEEDDUURREESS

Documents

A319 & 320 Fault Verification Guide