Airbus A330-243

Service difficulty reports · 5,643

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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.

SDR 2025FA0000305Seat Track · corrodedDURING ROUTINE MAINTENANCE INSPECTION, FOUND SEAT TRACK CORRODED AT FR71 (-Y1959).Apr 21, 2025 · N393HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR 2025FA0000304Seat Track · corrodedDURING ROUTINE MAINTENANCE INSPECTION, FOUND SEAT TRACK CORRODED AT FR62 - 63 (-Y450).Apr 21, 2025 · N393HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR 2025FA0000302Seat Track · corrodedDURING ROUTINE MAINTENANCE INSPECTION, FOUND SEAT TRACK CORRODED AT FR61 - 62 (Y1959).Apr 21, 2025 · N393HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR 2025FA0000299Seat Track · corrodedDURING ROUTINE MAINTENANCE INSPECTION, FOUND SEAT TRACK CORRODED AT FR53.6 (Y1959).Apr 21, 2025 · N393HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR 2025FA0000298Seat Track · corrodedDURING MAINTENANCE INSPECTION, FOUND SEAT TRACK CORRODED AT FR53.6 (Y1959).Apr 21, 2025 · N393HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA20250422113Check Valve · faultedETOPS-FOUND 2 CHECK VALVES IN LOWER DECK CARGO COMPARTMENT FIIRE EXTINGUISHING SYSTEM TO BE BAD DURING TASK CARD 330-262300-04-2 INSPECTION. REMOVED AND REPLACED CHECK VALVES (5016WE) (5017WE) PER AMM 26-23-21. LEAK CK GOOD. OK FOR SVC.Apr 21, 2025 · N370HA · Airbus A330243 · Extinguishing SystemSDR HALA20250421111Pressure Switch · inoperativeETOPS-AFTER LANDING DURING APU START APU AFT PUMP FAULT. REMOVED AND REPLACED APU LOW FUEL PRESSURE SWITCH PER AMM 49-31-000-801-A PERFORMED OPS CHECK GOOD LEAK CHECK GOOD BITE TEST GOOD OK TO CONTIUE SERVICE.Apr 20, 2025 · N380HA · Airbus A330243 · APU Engine Fuel and ControlSDR HALA20250414107Blade · damagedETOPS-FOUND BEND IN LEADING EDGE OF BLADE 20 ON ENG 1, OUT OF LIMITS. REMOVED AND REPLACED BLADE 20 ON ENGINE 1 PER AMM 72-31-401. OPS CHECK GOOD. NO VIBE. OK TO CONTINUE.Apr 11, 2025 · N395HA · Airbus A330243 · Turbine Engine Compressor SectionSDR HALA20250414106Filter · cloggedETOPS-ENG 1 FUEL FILTER FAULT CLOG.PERFORMED TSM 73-21-79-810-803A. REMOVED AND REPLACED FUEL FILTER PER AMM 73-11-41. NO VISIBLE DEBRIS OR MATERIAL IN FUEL FILTER. INSPECTED INDICATING SYSTEM. NO DEFECT NOTED. ENGINE RUN OK AND LEAK CHECK OK. A/C OK FOR SERVIApr 11, 2025 · N385HA · Airbus A330243 · Engine Fuel DistributionSDR HALA20250407103Wire Harness · chafedETOPS - DURING COMPLETION OF T/C: 330-783201-R2-1-2 FOUND #2 ENG OVERSPEED PROBE CHAFED. REMOVED AND REPLACED LP TURBINE OVERSPEED ELECTRICAL HARNESS W/REF TO A330 AMM 71-52-81. OK FOR SVC. EEC BITE TEST OK.Apr 5, 2025 · N392HA · Airbus A330243 · Engine Indicating System WiringSDR HALA20250407102Pump · faultedETOPS - FUEL APU AFT PUMP FAULT CAME ON AFTER START UP. REMOVED AND REPLACED APU AFT FUEL PUMP PER AMM 28-22-52. OPS AND LEAK CHKS OK. OK FOR SVC. NO FAULTS NOTEDApr 5, 2025 · N380HA · Airbus A330243 · APU Engine Fuel and ControlSDR HALA20250404100Seal · brokenETOPS - #2 ENG ANNULUS FILLER AT POS 2, POS 10, POS 5 BROKEN SEAL . REPLACED ANNULUS FILLER AT POS 2, POS 10, POS 5 PER AMM 72-31-41-400-802-AApr 3, 2025 · N389HA · Airbus A330243 · Turbine Engine Air Inlet SectionSDR HALA20250404099Fuse · inoperativeETOPS - APU AUTO SHUTDOWN (2-ATTEMPTS). FOUND FUSE FIN 6KA1 INOP-REMOVED AND REPLACED FUSE PER AMM 49-42-00 AND ACCOMPLISHED PRECAUTIONARY STARTER CHANGE DUE TO PREVIOUS SHUTDOWNS PER AMM 49-42-51. OPS CHECK GOOD.Apr 3, 2025 · N375HA · Airbus A330243 · APU Start/Ignition SystemSDR HALA20250403098Pressure Switch · faultedETOPS - INFO TO MAINT: ECAM FUEL APU PUMP FAULT CAME ON AFTER START ON TAXI 1N THEN LEEPED. REMOVED LOW PRESSURE SWITCH PER AMM 49-34-11-000-801-A. INSTALLED SWITCH AS NEEDED PER AMM 49-34-11-400-801-A. LEAK CHECK GOOD. OPS CHECK GOOD. OK FOR SVC.Apr 2, 2025 · N391HA · Airbus A330243 · APU Engine Fuel and ControlSDR HALA20250403097Pump · faultedETOPS - APU AFT FUEL PUMP FAULT ON ECAM PAGE. REMOVED AND REPLACED APU AFT FUEL PUMP PER AMM 28-22-52. OPS CHECK AND LEAK CHECK OKAY. OKAY FOR SERVICE.Apr 2, 2025 · N361HA · Airbus A330243 · APU Engine Fuel and ControlSDR HALA20250401095Bleed Valve · faultedETOPS - DURING ENG 2 IDLE RUN. HP VALVE NOT WORKING. REMOVED AND REPLACED #2 HP BLEED VALVE PER AMM 36-11-51. OPS/LEAK CHECK GOOD. OK FOR SVC.Mar 31, 2025 · N393HA · Airbus A330243 · Compressor Bleed ValveSDR HALA20250331094Hydraulic Line · failedETOPS - ENG 2 REVERSER FAULT AFTER LANDING. INSTALLED HYDRAULIC LINE P/N 91K049-00 ON UPPER O/B SIDE OF FAN THRUST REVERSER OPS CHECK & LEAK CHECK GOOD PER AMM 78-31-00 NO FAULTS NOTED. OK FOR SVC.Mar 29, 2025 · N389HA · Airbus A330243 · Engine Thrust ReverserSDR HALA20250331093Valve · faultedATB - ECAM AIR ABNORM BLEED CONFIG. ENG 1 BLEED OFF CAME ON EVERY 2 MINUTES. REMOVED AND REPLACED #1 ENGINE PRV PER AMM 36-11-52. OPS AND LEAK CHECK GOOD AFTER ENGINE ILD RUN. OK FOR SVC.Mar 29, 2025 · N361HA · Airbus A330243 · Pneumatic Distribution SystemSDR HALA20250326090Wire Harness · chafedETOPS - WHILE WORKING ON #2 ENG T/C'S, FOUND WIRE BUNDLE CHAFING AGAINST PRV UNDER ORANGE WRAP, SEVERAL WIRES FOUND DAMAGED/CHAFED. FOUND WIRES 3A005R+B 20, 3A008R+B, AND 3A010R+B20 BETWEEN 3009VCI-A AND 3012VCIA DAMAGED ON ENGINE #2. REMOVED + REPLACED WIRESMar 26, 2025 · N385HA · Airbus A330243 · Turbine Engine System WiringSDR HALA20250324086Hydraulic Line · leakingATB - AFTER TAKE OFF L/G RETRACTION FAULT. GEAR NEVER CAME UP. HOSE ON L/H L/G PITCH TRIMMER LEAKING. HOSE REPLACED IAW: 32-11-15-400-801-A (33) AND G SYST BLEEDING C/OUT. NIL LEAKS EVIDENT. PN ON: 201042197.Mar 22, 2025 · N381HA · Airbus A330243 · Hydraulic System, MainSDR HALA20250324087Transfer Sys · faultedETOPS - FUEL AFT XFR FAULT. REMOVED AND REPLACED INNER TK INLET VALVE ACTUATOT (603QL1) PER AMM 28-26-53. OPS CHECK OK.Mar 21, 2025 · N399HA · Airbus A330243 · Aircraft Fuel Distribution SystemSDR HALA20250324085Fuel Line · leakingETOPS - FUEL LEAKING FROM AFT DRAINMAST (TRIM TANK/APU DRAIN). PULLED BACK 5 TOTAL FUEL TRANSFER LINE SLEEVE COUPLINGS IN AFT/BULK CARGO COMPT TO FOM PER AMM 28-27-47-000-801-A STEPS 4A.1 TO 4.A.6. FOUND LEAK AT CONNECTOR OF FUEL LINE ASSY AROUND AT FRAME 64. Mar 21, 2025 · N373HA · Airbus A330243 · Aircraft Fuel Distribution SystemSDR HALA20250319083Probe · malfunctionedETOPS - DURING PREFLIGHT INNER TANK 2 FUEL LEVEL DROPPED FROM 39,000 LBS TO 32,160 LBS, ECAM ADV FOR FUEL IMBALANCE DUE TO LIMITATION EXCEEDANCE FOB ON E/WD & ECAM CHANGED PROPORTIONATELY. REMOVED AND REPLACED FUEL PROBE (26QTZ). OPS & LEAK CHECK GOOD. REF DAVMar 16, 2025 · N374HA · Airbus A330243 · Fuel Indicating SystemSDR HALA20250317018Fairing · cracked2 1/2 INCH CRACK ON AFT SECTION OF R/H PYLON LOWER FAIRING. REPAIRED PER E105-373018-INIMar 14, 2025 · N373HA · Airbus A330243 · Nacelle/Pylon Miscellaneous StructureSDR HALA20250317017Fairing · cracked2 INCH CRACK ON AFT SECTION OF L/H PYLON LOWER FAIRING. REPAIRED PER E105-373016-INI.Mar 14, 2025 · N373HA · Airbus A330243 · Nacelle/Pylon Miscellaneous StructureSDR HALA20250314012Channel · cracked#1 ENG LH UPPER PIVOT DOOR ACTUATOR CHANNEL FAIRING CRACKED. REPAIRED PER ROLLS ROYCE RB211 TRENT SRM 54-30-02 REPAIR NO 9 (FRSX010). DYE PENETRANT INSP OKAY, PER ENGINE ERA REINSP EVERY 25 CYCLESMar 12, 2025 · N382HA · Airbus A330243 · Engine Thrust ReverserSDR HALA20250314014Channel · cracked#1 ENG RH LOWER PIVOT DOOR ACTUATOR CHANNEL FAIRING CRACKED. REPAIRED PER ROLLS ROYCE RB211 TRENT SRM 54-30-02 REPAIR NO.9 (FRSX010). DYE PENETRANT INSP OKAY. PER ENGINEERING, REP INSP EVERY 25 FLIGHT CYCLE. PLACARD INSTALLEDMar 12, 2025 · N382HA · Airbus A330243 · Engine Thrust ReverserSDR HALA20250314013Channel · cracked#1 ENG LH LOWER PIVOT DOOR ACTUATOR CHANNEL FAIRING CRACKED. REPAIRED PER ROLLS ROYCE TRENT SRM 54-30-02 REPAIR NO 9 (FRSX 010). DYE PENETRANT INSP OKAY. PER ENGINNER REINSP EVERY 25 CYCLES. PLACARD INSTALLED.Mar 12, 2025 · N382HA · Airbus A330243 · Engine Thrust ReverserSDR HALA20250312079Oil Cooler · leakingETOPS - ECAM: APU LOW OIL LEVEL. WHILE SERVICING FOUND APU OIL COOLER LEAKING. REMOVED AND REPLACED APU OIL COOLER PER AMM 49-91-44. OPS/LEAK CHECK GOOD. OK FOR SVC.Mar 11, 2025 · N390HA · Airbus A330243 · APU Oil SystemSDR HALA20250311078Filter · contaminatedETOPS - ENG 2 OIL CHIP DETECT ECAM AFTER ENGINE SHUTDOWN. PERFORMED TSM 79-20-00-810-824-A. PER STEP 4.B. VISUALLY INSPECTED, REMOVED AND REPLACED SCAVENGE OIL FILTER ELEMENT PER AMM 79-00-00-200-821-A. NO DEFECTS NOTED. LEAK CHECK GOOD. BITE TEST GOOD. OK FORMar 10, 2025 · N390HA · Airbus A330243 · Turbine Engine Oil SystemSDR HALA20250310076Pump · leakingETOPS - #2 ENG GREEN SYS EDP LEAKING FROM PRESSURE LINK UNION. REMOVED AND REPLACED #2 ENG GREEN EDP PER AMM 29-11-51-400-805-A. OPS/ LEAK CHECK GOOD. OK FOR SERVICEMar 8, 2025 · N378HA · Airbus A330243 · Hydraulic Pump (Electric/Engine), MainSDR HALA20250303075Blades · bird ingestionETOPS - DURING INITIAL PDSC WALKAROUND. DISCOVERED EVIDENCE OF BIRD STRIKE ON #2 ENG INLET AND FAN BLADES. AWAITING RESOLUTION.Mar 2, 2025 · N390HA · Airbus A330243 · Turbine Engine Compressor SectionSDR HALA20250228009Selector Valve · leakingHYD B RESEVR LO LVL. HYD B ENG 1 PUMP NO PRESS. LEAK FOUND ON BRAKE AUTOMATIC SELECTOR VALVE. INSTALLED NEW PACKINGS ON HYD. PIPE UNIONS, IAW AMM 32-42-13-400-801-A. BLED NORMAL AND ALTERNATE BRAKE SYSTEMS. OPS TEST NORMAL AND ALTERNATES SYTEM GOOD. NO LEAKS NFeb 27, 2025 · N384HA · Airbus A330243 · Landing Gear Brake SystemSDR HALA20250225071Thermostat · faultedETOPS - ECAM AIR ENG2 BLEED HIGH TEMP ON APPROACH. REMOVED AND REPLACED #2 ENG FAV CONTROL THERMOSTAT PER AMM 36-11-43-400-804-A. RAN #2 ENG AS PRECAUTIONARY ACTION, NO FAULTS NOTED.Feb 24, 2025 · N392HA · Airbus A330243 · Pneumatic Distribution SystemSDR HALA20250225070Eec · malfunctionedETOPS - DURING DEACTIVATION OF T/R #1 NO MSG ON ECAM FOR "ENG1 REV INHIBITED". PERFORMED TSM 78-31-00-810-963-A. REPLACED ISOLATION CONTROL UNIT PER AMM 78-31-41. MSG "ENG1 REV INHIBITED" ON ECAM PER MEL 78-30-01 OK. LEACK CHECK GOOD. REPLACED #1 ENG EEC PER AFeb 24, 2025 · N390HA · Airbus A330243 · Engine Thrust ReverserSDR HALA20250224068Transducer · malfunctionedETOPS - INFO TO MAINT DURING CRUISE ENG 1 N1 VIB FLUCTUATES BETWEEN 2.1-3.1. PERFORMED TSM 77-00-00-810-814-A. EXAMINED ENG#1 LP COMPRESSOR BLADES, ANNULUS FILLERS, SPINNER. NO DEFECTS NOTED. PERFORM ENG #1 HPR AND VIB SURVEY PER AMM 77-00-00-700-838-A. N1 VIBFeb 21, 2025 · N396HA · Airbus A330243 · Engine Vibration AnalyzerSDR HALA20250224067Antenna · faultedETOPS - NAV PRED W/S DET FAULT. REMOVED AND REPLACED WEATHER RADAR ANTENNA ASSEMBLY PER AMM 34-41-11. BITE TEST OK. OK FOR SERVICE.Feb 21, 2025 · N385HA · Airbus A330243 · Weather Radar SystemSDR HALA20250220066Duct · damagedETOPS - FOUND APU BLEED DUCT DAMAGED BETWEEN COMPRESSOR AND SURGE VALVE. REMOVED AND REPLACED APU BLEED DUCT BETWEEN COMPRESSOR AND SURGE VALVE PER AMM 49-51-42. LEAK CHECK GOOD. OK FOR SERVICEFeb 19, 2025 · N388HA · Airbus A330243 · APU Bleed Air SystemSDR HALA20250217064Fadec · faulted"ETOPS - BTB ENG 2 FADEC SYS FAULT. PFR INDICATED N2 COMPRESSOR SPEED PROBES (E2-4089KS1 + 3) FAULT. PERFORMED RESISTANCE CHECK FROM OPU 2 CONNECTOR PIN 6-7 & OPU CONNECTOR PIN 12-13. OHMS READ 11.5 & 10.6 RESPECTFULLY. RESISTANCE WITHIN LIMITS PER TSM 77-11-0Feb 16, 2025 · N396HA · Airbus A330243 · Fuel Controlling SystemSDR HALA20250217061Bleed Valve · faultedATB - ECAM AIR ENGINE 1AND 2 BLEED FAULT ILLUMINATED CLIMBING. PER TSM 36-11-00-810-856-A , PFR ONLY SHOWS PRV E1-400 1HA ISOL 7HA1 SENSE LINE FAULT FOLLOWED TSM 36-11-81-810-908-A PER STEP 4.A.2 A REPLACED BLEED VALVE PER AMM 36-11-52 OPS AND LEAK CHECK OK RAFeb 16, 2025 · N361HA · Airbus A330243 · Compressor Bleed ValveSDR HALA20250217063Filter · unknownETOPS - BTB. AIRPLANE STOPS ABRUPTLY WHEN BRAKES ARE APPLIED AT LOW SPEED, PROGRESSIVELY GOT WORST, TOWED IN TO GATE. REMOVED AND REPLACED GREEN RESEVOIR FILTER ASST UP TO STEP 4 A 10 OF AMM 29-11-44-400-801A. PERFORMED STEPS C AND D OF AMM 29-11-44-400-801A GFeb 14, 2025 · N388HA · Airbus A330243 · Hydraulic System, MainSDR HALA20250217062Packing · misinstalledETOPS - UPON ENTERING FLT DECK, SMELL OF SOME THING (SMOKE OR FUMES). FOUND SCAVANGE FILTER BOWL PACKING NOT INSTALLED PROPERLY. REPLACED PACKING REF 49-91-41. OPS/ LEAK CHECK GOOD. NO ODORS. PACK BURN COMPLETED REF AMM 21-00-00 LEV. A DECON COMPLETED. NO DEFEFeb 14, 2025 · N383HA · Airbus A330243 · APU Oil SystemSDR HALA20250212060Actuator · faultedETOPS - ECAM: TRIM TANK TRANSFER FAULT. FOUND FUEL OUTER TK INLET VALVE 2 FAILED. REMOVED AND REPLACED OUTER TANK FUEL INLET-VALVE ACTUATOR PER AMM 28-25-57. OPS CHECK GOOD. OK FOR SVC.Feb 11, 2025 · N396HA · Airbus A330243 · Aircraft Fuel Distribution SystemSDR HALA20250211059Brake Assy · malfunctionedETOPS - BTB BRAKES AGGRESSIVELY STIP A/C AT LOW SPEED. (MAX BRAKES WITH VERY LIGHT TOUCH ON PEDALS.). FOUND GREEN RESERVOIR LP FILTER ASSY TURKEY POPPER EXTENDED PER TSM 32-42-00-810-820A. REPLACED FILTER, NO DEBRIS FOUND PER AMM 29-11-44-400-801A. OPS CHECKFeb 10, 2025 · N388HA · Airbus A330243 · Landing Gear Brake SystemSDR HALA20250210055Unknown · odorATB - AIR TURN BACK DUE TO STRONG METALIC ODOR, FROM PRIMARALY #1 AND #2 DOOR. COULD ALSO SMELL AT #3 ORDER AND LESS AT # 4 DOOR. BOROSCOPE APU FIRST STAGE COMPRESSOR. CHECK OK. INSPECTED IP CHECK VALVE ON ENG #1 & #2, NO DEFECTS FOUND. PER AMM 36-11-41-200-80Feb 9, 2025 · N399HA · Airbus A330243 · Air Distribution SystemSDR HALA20250210057Fcu · faultedETOPS - IN FLIGHT ECAM: AUTO FLIGHT FCU FAULT. INOP SYS: PART FCU. REMOVED AND REPLACED FCU PER 22-81-12. CAT III LAND TEST COMPLIED WITH PER 22-97-00. BITE TEST PASSED. NO FAULTS NOTED. OK FOR SERVICE.Feb 9, 2025 · N389HA · Airbus A330243 · Auto Flight SystemSDR HALA20250210056Fuel Line · leakingATB - FUEL LEAK #1 ENG. FOUND TUBE PN:FW53576 BETWEEN THE #1 ENG FUEL PUMP AND LP FUEL FILTER LEAKING. REMOVED DAMAGED TUBE. REPLACED TUBE P/N: FW53576 PER AMM 70-12-01-400-002-A. ENG IDLE RUN AND LEAK CHECKED GOOD. OK FOR SERVICE.Feb 9, 2025 · N375HA · Airbus A330243 · Engine Fuel DistributionSDR HALA20250207053Generator · faultedETOPS - ELEC GEN 2 FAULT, RESET DID NOT WORK, GEN #2 OFF. 5 MINS LATER ELEC - IDG#1 LO PR IDG 2 TO OFF PER PROCEDURE. REMOVED AND REPLACED #2 I.D.G. PER AMM 24-21-51. LEAK CHECK OPS CHECK GOOD. OK FOR SVC.Feb 6, 2025 · N361HA · Airbus A330243 · AC Generator-AlternatorSDR HALA20250205051Fire Detector · faultedETOPS - ON LANDING RECEIVED ECAM ENG1 FIRE LOOP-A. FOUND ENG #1 LOOP A FIRE DETECOTR 4011WD OPEN REMOVED & REPLACED 4011WD ON ENG #1 PER AMM 26-12-15. OPS CHECK OK FOR SERVICE.Feb 4, 2025 · N386HA · Airbus A330243 · Fire DetectionSDR HALA20250205050Interphone · malfunctionedETOPS - 2R INTERHPONE PA VOLUME IS SOFT. REMOVED AND REPLACED #2 INTERPHONE TEST OK PER: AMM 23-73-44.Feb 4, 2025 · N385HA · Airbus A330243 · Interphone/Passenger Announcement (PA) System
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