Airbus A330-243
Service difficulty reports · 5,645
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'A330243' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'A330243' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR HALA2020073100161Pcu · malfunctionedETOPS SIGNIFICANT SYSTEM - DURING 14 DAY CHECK, FOUND ENG 2 REV FAULT ON THRUST REVERSER CYCLE. DURING TROUBLE SHOOTING, FOUND FAULT CODE 783751, T LOCK (E2-
4005EG1 1/2/3/4) PCU (EG4007EG) BLOCKER DOORS 1 & 2 UPPER RIGHT AND LOWER RIGHT. REMOVED AND SDR HALA2020072800159Bleed Valve · inoperativeETOPS SIGNIFICANT SYSTEM - #1 ENG BLEED VALVE NOT CLOSED. REMOVED AND REPLACED #1 ENG PRV PER AMM 36-11-52. OPS AND LEAK CHECK OK. OK FOR SVC.SDR HALA2020072800158Bleed Valve · malfunctionedETOPS SIGNIFICANT SYSTEM - ENG 1 BLEED FAULT IMMEDIATELY AFTER TAKEOFF AT 1000' AS REDUCED THRUST AFTER MULTIPLE RESETS FAULT LIGHT EXTINGUISHED. // REMOVED & REPLACED #1 ENG. PRV PER AMM 36-11-52. ENGINE RUN & LEAK CHECK PENDING. PERFORMED ENG IDLE RUN & #1 BSDR HALA2020072400157Bleed Valve · malfunctionedETOPS SIGNIFICANT SYSTEM - #2 ENG BLEED VALVE NOT CLOSED. // REMOVED AND REPLACED #2 ENG PRV PER AMM 36-11-52-400-804-A UP TO STEP 4B. OPS AND LEAK CHECK PENDING. OPS AND LEAK
CHECK GOOD NO DEFECTS NOTED.SDR HALA2020072400156Bleed Valve · malfunctionedETOPS SIGNIFICANT SYSTEM - AIR ENG 2 BLEED NOT CLOSED ON ECAM DURING ENGINE RUN. RESET NO HELP. // PHYSICALLY MOVED THE PRV BLEED VALVE AND SUSPECT THE SHAFT IN
PRV IS SHEARED. NEED NEW PRV. REPLACED #2 ENG PRV PER AMM 36-11-52-400-804-A. OPS AND LEAK CHESDR HALA2020072400155Autothrottle Sys · malfunctionedETOPS SIGNIFICANT SYSTEM - AUTO THRUST DID NOT ENGAGE ON T.O. BUT EPR SETTING & INDICATION WERE CORRECT,SET THRUST MANUALLY. UNABLE TO ENGAGE W/ A/THRUST BUTTON. ENGAGE A/P 1, UNABLE TO ENGAGE A/THR. W/A.P.2 A/THR ENGAGED NORMALLY, ENGAGED AP1 AGAIN THIS TIME SDR HALA2020072400154Actuator · malfunctionedETOPS SIGNIFICANT SYSTEM - ENG 2 FUEL LP SHUT OFF VALVE MOTOR INOP. // VERIFIED ENG 2 LP FUEL VALVE MOTOR 1 INOP PER AMM 28-24-00-710-803-A 07/22/20 2020495. REPLACED THE NR 2 ENG LP FUEL VALVE ACTUATOR IAW AMM 28-24-51. OPS CHECKED OK.SDR HALA2020072200153Bleed Valve · malfunctionedETOPS SIGNIFICANT SYSTEM - ENG 1 BLEED VALVE NOT CLOSED. REMOVED ENG NR 1 PRV PER AMM 3611-52-000-804-A.REPLACED ENG #1 PRV
PER AMM 36-11-52-400-804-A UP TO 4B.E#2052488 LEAK CHECK PENDING. OPERATION AND LEAK CHECK GOOD PER AMM 36-11-52 OK FOR SERVICE.SDR HALA2020071900151Test Button · corroded#2 ENGINE AFT FIRE BOTTLE PRESSURE SWITCH TEST POINT CORRODED AND INOPERATIVE. // REMOVED AND REPLACED #2 ENGINE AFT FIRE BOTTLE IAW A330 AMM 26-
21-41.SDR HALA2020072090148Priority Valve · stuckETOPS SIGNIFICANT SYSTEM, NR 2 PRV VALVE STUCK OPEN DURING 14 DAY PARKING PROCEDURE CHECK. REMOVED AND REPLACED THE NR 2 ENG PRV PER AMM 36-11-52. OPS AND LEAK CHECKED OK.SDR HALA2020072090150Control Valve · malfunctionedETOPS SIGNIFICANT SYSTEM, PACK 1 TEMP CONTROL VALVE ECAM MSG. REPLACED PACK 1 TEMP CONTROL VALVE IAW AMM 21-53-53-400-801A. OPS CHECKED OK.SDR HALA2020071900149Fmu · leakingETOPS SIGNIFICANT SYSTEM, FUEL LEAKING FROM NR 2 ENGINE DRAIN MAST. MECHANIC FOUND LEAK COMING FROM FMU LINE. LINE DISCONNECTED FOR PARKING. RECONNECTED FMU LINE PER AMM 73-21-52-400-802-A. REMOVED AND REPLACED THE NR 2 ENGINE FMU IAW AMM 73-21-52-400-8SDR HALA2020071600146Motor · defectiveETOPS SIGNIFICANT SYSTEM - NR 1 ENG FUEL LP MOTOR 1 NOT TESTING REF TC 2060-9709-HAL STEP 10. REPLACED NR 1 ENG LP MOTOR PER AMM 28-24-51. OPS GOOD, OK FOR SVC.SDR HALA2020071600145Starter · malfunctionedETOPS SIGNIFICANT SYSTEM - NR 2 ENG NO N3 ROTATION ON START, START VALVE OPENS. REMOVED AND REPLACED NR 2 ENG STARTER IAW AMM 80-11-41-0401. OPS CHECK NORMAL, NO LEAKS NOTED. OK FOR SVC.SDR HALA2020071500144Actuator · malfunctionedETOPS SIGNIFICANT SYSTEM - BTB STATUS MSG AFT FUEL XFER INOP. REMOVED AND REPLACED RIGHT AFT FUEL TRANSFER VALVE ACTUATOR (FIN
603QL2) AS PER AMM 28-26-53-000-801-A/400-801-A. PERFORMED FUEL VALVES TEST- OPS CHECK GOOD. OK FOR SVC.SDR HALA2020071300143Valve · inoperativeETOPS SIGNIFICANT SYSTEM - ENG 1 BLEED NOT CLOSED. INSTALLED ENG #1 PRV PER AMM 36-11-52. OPS CHECK, LEAK CHECK GOOD. OK FOR SERVICE.SDR HALA2020071000142Bleed Valve · malfunctionedETOPS SIGNIFICANT SYSTEM, NR 1 ENG BLEED VALVE NOT CLOSED. VISUALLY CONFIRMED NR 1 PRV OPENING UNCOMMANDED WITH ENGINE OFF. VALVE BAD. REMOVED AND REPLACED THE NR 1 ENG PRV IAW AMM 36-11-52. OPS CHECKED OK, LEAK CHECKED OK.SDR HALA2020070900141Cdu · malfunctionedETOPS SIGNIFICANT SYSTEM - FOUND MCDU NR 1 FAILED. REMOVED AND REPLACED MCDU NR 1 PER AMM 22-82-12. PERFORMED AFS BITE TEST PER AMM 22-96-00. TEST PASSED. NO DEFECTS NOTED. OK FOR SVC.SDR HALA2020062600134Switch · malfunctionedETOPS SIGNIFICANT SYSTEM FUEL APU VALVE FAULT ON ECAM. FOUND APU ISOL VALVE (5QF) ON GRD RPT. REPLACED ACTUATOR. NO HELP. REINSTALLED ORG ACTUATOR. OPS CHK OF THE APU FUEL ISOL. VLV AND APU LP S/O VLV ACTUATOR FOUND STUCK OPEN. FOUND APU FUEL VENT P/BSWSDR HALA2020062300131Wire · looseETOPS SIGNIFICANT SYSTEM - ON PDC FOUND ECAM MSG APU LP VALVE FAULT.// T/S PER A330 TSM 28-29-00-810-801A. REPLACED 6QF RELAY. NO HELP. R/R APU LP FUEL SHUTOFF VALVE ACTUATOR PER A330 AMM 28-29. NO HELP. T/S PER A330 AWM 28-22-02 AND 28-29-02. FOUND LOOSE WISDR HALA2020062300130Actuator · malfunctionedETOPS SIGNIFICANT SYSTEM - "FUEL AFT XFER" INOP STATUS MESSAGE ON STATUS PAGE. // PER TSM TASK 28-27-00-810-829-A FOUND FUEL TRIM TANK ISOLATION VALVE
FAULTING (FIN 702QN). REMOVED AND REPLACED FUEL TRIM TANK ISOLATION VALVE ACTUATOR (FIN 702QN) PER AMM 28SDR HALA2020062200129Actuator · faultedETOPS SIGNIFICANT SYSTEM - APU START FAULT - 3 ATTEMPTS. REMOVED AND INSTALLED SERVICEABLE APU FLAP ACTUATOR PER AMM 49-16-51-000-801-A AND 49-16-51-400-801-A. OPS CHECK GOOD. OK TO CONTINUE.SDR HALA2020062200128Flow Divider · malfunctionedETOPS SIGNIFICANT SYSTEM APU FAULT AUTO SHUT DOWN. ACFT ARRIVED W/ APU RUNNING. T/S PER TSM 49-62-00-810-836-A. PERFORMED BLEED OF APU FUEL LINE PER 28-22. PERFORMED ALPHA CALL UP OF APU PARAMETERS. NO DEFECTS NOTED. NEXT STEP TO REPLACE FLOW DIVIDER ASSSDR HALA202006210127Fcu · malfunctionedETOPS SIGNIFICANT SYSTEM - APU DOES NOT GO ABOVE 96%. IAW TSM 49-00-00-810-834-A. FOUND FCU FAULTY. REMOVED AND REPLACED APU FCU PER AMM 49-32-51. OPS CHECK OK. LEAK CHECK OK. APU OPERATES AS NORMAL. AIRCRAFT OK FOR SVC.SDR HALA202006210126Cover · damagedOPEN - POSSIBLE DAMAGE AFT CARGO DOOR ACCESS COVER PANEL. 822BR. REPAIR IN WORK.SDR HALA2020061900125Cover · missingLEFT NR 1 FLAP TRACK FAIRING MISSING FORWARD ATTACHMENT BOLT CAP COVER RT SIDE. INSTALLED NEW FLAP TRACK FAIRING. OK FOR SVC.SDR HALA2020060500120Igniter · defectiveETOPS SIGNIFICANT SYSTEM - NR 2 ENG IGN B FAULT/ INOP. PERFORMED AUDIBLE TEST ON IGNITION B SYS PER AMM 74-00. VERY WEAK POPPING. REMOVED & INSTALLED IGNITER PER AMM 74-21 OPS CHECK NORMAL.SDR HALA2020060400119Pump · leakingETOPS SIGNIFICANT SYSTEM - NR 2 ENG HYD EDP LEAKING (GREEN). REMOVED AND INSTALLED NR 2 ENG HYD EDP (GREEN) PER AMM 29-11-51-400-810-A. LEAK CHECK OK. OK TO CONTINUE.SDR HALA2020060100118Cowling · scratchedSCRATCH FOUND ON NR 2 ENGINE INLET COWL, AROUND 7 O'CLOCK POSITION. DAMAGE ASSESSMENT CARRIED OUT IAW SRM 54-10-01. REFER TO ATTACHED FOR DETAILS. COMPOSITE REPAIR ON NR 2 ENGINE INLET COWL AROUND 7 O'CLOCK POSITION 03 OFF AREAS. CARRIED OUT AS IAW TV NO 2SDR HALA2020052800116Pitot Tube · obstructed"RTO" DISCONTINUED TAKEOFF DUE TO UN - RELIABLE AIRSPEED ON F/O AIRSPEED INDICATOR. DISCONTINUED ABOUT 100 KTS, MAX BRAKE TEMP 575*. BRAKE TEMP WITHIN LIMITS PER AMM 05-51-16-200-801-A. ACCOMPLISHED TASK CARDS 3411-7002 & 3411-7003-HAL. TSD & DEBRIS FLUSHED FSDR HALA2020051600109Actuator · malfunctionedETOPS SIGNIFICANT SYSTEM - BTB FUEL AFT XFR. // REMOVED AND REPLACED ACTUATOR FOR THE INNER TANK INLET VALVE 2
PER AMM 28-26-53. TESTS GOOD, OK FOR SVC.SDR HALA2020050800108Plenum · delaminatedETOPS SIGNIFICANT SYSTEM - DIRECT Z190 NT: LH PACK PLENUM FOUND BADLY DE-LAMINATED AT MOUNTING BOLT AREAS AND CRACK LINES AT AFT EDGE. // ELECTRICAL CONNECTORS 521HH5 AND 521HH7 DISCONNECTED. 1)LH PACK PLENUM CHAMBER, PRIMARY HEAT EX-CHANGER, MAIN HEAT EX-CHANSDR HALA2020050600105Skin · corrodedFUSELAGE SKIN FOUND SUSPECTED CORROSION AT FRAME 76 - FRAME 77, STRINGER 41 LH - STRINGER 42 LH. (AFT CUTOUT HOLE OF WASTE
EXHAUST SYSTEM). // FUSELAGE SKIN CORROSION AT FRAME 76 - FRAME 77, STRINGER 41 LH - 42 LH REPAIRED AS PER REPAIR DESIGN APPROVAL SSDR HALA2020050300104Fault Message · false activationETOPS SIGNIFICANT SYSTEM - ECAM- FUEL T TANK TRANSFER FAULT. // FCMC 1 & 2 BITE TEST OK IAW A330 AMM 28-51-00-740-801. FCMS LEVEL SENSE TEST OK AMM 28-51-00-710-802. NO ECAM FAULT EXISTED.SDR HALA2020050300103Fitting · corrodedDURING CCK AND DURING INSPECTION PER EM 5753-01164, CORROSION WAS FOUND ON THE LH MLG RIB 6 FITTING. THE CORROSION WAS REWORKED PER SECT I OF ERA 586363-14AD. // THE REWORKED LH RIB 6 FITTING IS APPROVED FOR 30,033 TOTAL FLIGHT CYCLES OR 193,119 TOTAL FLIGHT SDR HALA2020042900100Oil System · overservicedON T/OFF FA'S SMELLED AN FUME ODOR (BO-MUSTY SMELL IN CABIN). LASTED A FEW MINS. OPS NORMAL. // TROUBLE SHOT FUME SMELL PER TSM 21-00-00-810-805-A. FOUND #2 ENG OIL OVER SERVICED. DRAINED OIL PER AMM 12-13-79-680-801. PERFORMED IDLE ENG RUN WITH BOTH ENGINES.SDR HALA2020042800099Actuator · faultyETOPS SIGNIFICANT SYSTEM - DURING OPERATIONAL CHECK OF LP FUEL SHUT-OFF VALVES, PER HAL TC 2060-9709-HAL, FOUND LP FUEL VALVE ACTUATOR ENG. #1 (FIN 402QG1)FAULTING. // REMOVED AND REPLACED #1 ENG LP FUEL VALVE ACTUATOR (FIN 402QG1)PER AMM 28-24-51-400-803-A. OSDR HALA2020042800098Glowstrip · damagedFOUND EEPL DAMAGED AT GALLEY DOOR 2. // REPLACED PHOTO-LUMINESCENT STRIP FLOOR EMERGENCY ESCAPE PATH
MARKING AS PER AMM 33-51-21-000-801 AND 33-51-21-400-801. OPS CHECK GOOD.SDR HALA202004270097Shutoff Valve · malfunctionedETOPS SIGNIFICANT SYSTEM - DURING TEST OF RETURN AIRCRAFT FROM PARK, DURING HIGH POWER RUN
#2 PRSOV WILL NOT OPERATE CORRECTLY. // REMOVED AND REPLACED PRV VALVE PER AMM 36-11-52. OPS CHECK, LEAK
CHECK GOOD. OK FOR SVC. REPLACED BLEED TRANSDUCER PER AMM 36-SDR HALA2020041800091Bleed Valve · malfunctionedETOPS SIGNIFICANT SYSTEM - ECAM "ENG 2 BLEED NOT CLOSED". // REMOVED AND INSTALLED #2 ENG PRV PER AMM 36-11-52-400-804-A.
OPS CHECK LEAK CHECK GOOD PER AMM 36-11-52.SDR HALA2020041800090Bleed Valve · malfunctionedETOPS SIGNIFICANT SYSTEM - ECAM "ENG 1 BLEED NOT CLOSED". // REMOVED NUMBER 1 ENG PRV PER AMM 36-11-57.
INSTALLED NUMBER 1 ENGINE PRV PER AMM 36-11-52, OPS CHECK LEAK CHECK GOOD.SDR HALA2020041700089Actuator Valve · faultyETOPS SIGNIFICANT SYSTEM - FUEL AFT TRANSFER INOP ECAM AFTER 2ND ENG START RESET BOTH FCMC AND FWC BTB.// REMOVED AND REPLACED OUTER TANK FUEL INLET VALVE ACTUATOR
500QU1 PER 28-25-57 OPS CHECK OK OK FOR SVC.SDR HALA2020042700096Axle · corrodedFOUND #5 AXLE SLEEVE WITH CORROSION ON SHOULDER. // #5 AXLE SLEEVE REPLACED AS PER AMM 32-41-14 REV 75.02SDR HALA2020041700084Connector · damagedDURING C CHECK, FOUND EMERGENCY CEILING LIGHT INOPERATIVE ABOVE SEAT 2J, AND 2G, FOUND BOTH ELECTRICAL CONNECTORS DAMAGED. REPLACED TERMINAL LOGS AND EPSU BATTERY 14WL. 1549503SDR HALA2020041600088Cover · missingRT WING OUTBOARD FLAP TRACK #4 MISSING COVER. // REPLACED MISSING RT WING FLAP TRACK #4 COVER. OK FOR SERVICESDR HALA2020041300087Lug · corrodedZ670 RHW:RH WING MLG RIB 6 FWD LUG BORE CORROSION BEYOND WORK CARD #5753-01164-08B, FIGURE 1(FIGURE 02 OF 04). TO CARRY OUT
CORROSION REMOVAL. // CARRIED OUT CORROSION REMOVAL ON FWD LUG BORE IN ACCORDANCE TO STEPS INSTRUCTED IN ER/A 586359-14 REV 0 FINSDR HALA2020041300086Lug · corrodedLHW MLG: LH WING MLG RIB 6 FWD LUG BORE CORROSION BEYOND WORK CARD #5753-01164-08A, FIGURE 1(SHEET 20F4). TO CARRY OUT CORROSION
REMOVAL. // CARRIED OUT CORROSION REMOVAL ON FWD LUG BORE IN ACCORDANCE TO STEPS INSTRUCTED IN ER/A #586358-14 REV 0. FINAL DIMENSSDR HALA2020041202237Skin · corrodedDURING C CHECK, EXTERNAL FUSELAGE SKIN FOUND CORRODED BETWEEN FR 92 - 95 , STRINGER 14 LEFT TO BOTTOME CENTER LINE. REMOVED CORROSION, BLEND AREA AND INSTALLED REPAIR DOUBLE PER SRM 53-51-11-300-002 AND ER/A 14-586361. LP 1547461SDR HALA2020041000085Pin · corrodedFOUND LH MLG ECCENTRIC PIN BADLY CORRODED. // LH MLG ECCENTRIC PIN REPLACED AS PER TASK CARD REF.3211-9405-01
ITEM 9 CK OK.SDR HALA2020040900079Rib · corrodedDURING C CHECK, WHILE PERFORMING EM 5753-01164 (A330 SB 57-3124 R3), CORROSION WAS FOUND ON THE RH RIB 6 FWD LUG. CORROSION HAS BEEN REMOVED BY OVERSIZING AS PER R575-58471 ISSUE D WITH DEVIATIONS PER AIRBUS TECHNICAL ADAPTATION 80691523/046/2019 ISSUE 2 AND E
Back to Airbus A330-243