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 HALA2018123100688Warning Message · illuminatedETOPS SIGNIFICANT SYSTEM - ENG 1 REV FAULT ILLUMINATED AFTER STOWING REVERSER.// CONFIRMED FAULT. PERFORMED THRUST REVERSER DEPLOYMENT AND STOWAGE TEST. REF A330 AMM 78-31. CHANNEL A&B TEST OK. NO 60 DAY HISTORY. OK FOR SERVICE.SDR HALA2018123100686Skin · damagedCARGO REPORTED DAMAGE AFT CARGO DOOR.// FOUND DAMAGE AFT CARGO INNER SKIN BETWEEN FR62 AND FR63A 0.75"L X 0.50"W X 0.103D, INSPECTED DAMAGE WITH HFEC. NO CRACK NOTED. CUT OUT DAMAGE AREA. HFEC NO CRACKS NOTED. FABRICATED DOUBLER .063 224-T3 & FILLER .050 2024-SDR HALA2018123100682Fault Message · false activationETOPS SIGNIFICANT SYSTEM - ELEC IDG 1 OIL SYS FAULT.// RESET ACFT ELEC SYS PER TSM 24-20-00. OPS NORMAL.SDR HALA2018123100680Oil System · lowETOPS SIGNIFICANT SYSTEM - APU LOW OIL LEVEL MSG.// PERFORMED TSM 49-00-00810-815A. FAULT APU OIL LVL LOW, SERVICE APU PER AMM 12-13-49. NO LEAKS NOTED, OK FOR SVC.SDR AALA201812319002Cylinder · low pressureL4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER GAUGE TOUCHING YELLOW. SERVICED THE L4 DOOR DAMPER EMERGENCY OPERATION CYLINDER IAW AMM 52-10-00-600-802A.SDR HALA2018123100685Computer · faultedETOPS SIGNIFICANT SYSTEM - FUEL FCMC 2 FAULT.// REPLACED FCMC2 PER AMM 28-51-34. BITE TEST PER AMM 28-51-00 WAS OK, NO FAULTS NOTED. OK FOR SVC.SDR HALA2018122740678Warning Message · false activationOPEN - ATB - INTERMITTENT FWD CARGO VENT AND BULK VENT INOP SYS INDICATIONS. ATB DUE TO DOG IN BULK CARGO.// PERFORMED VC SYSTEM 21-28-00-710-802A. SYSTEM TEST PASSED. ON CONDITION PAGE UNABLE TO CONTROL BULK CARGO TEMP. DEACTIVATED BULK CARGO ISOL VALVES PER SDR HALA2018122400675Smoke Warning · false activationECAM SMOKE: LAVATORY DET FAULT.// PERFORMED CIDS - SDF 1 SYSTEM TEST SYSTEM TEST OK - NO FAULTS OR MESSAGE DISPLAYED. - OK FOR SVC. (NOTE: INSPECTED ALL LAVS - NO
DEFECTS OR SMELL NOTED.) REFERENCE 26-17-00.SDR HALA2018122400674Unknown · odorF/A SMELLED SMOKE IN LAV F.// INSPECTED LAV F - NO DEFECTS OR SMOKE SMELL NOTED - OK FOR SVC.SDR ANCF2018122201Link · abnormalATB - AFTER TAKE OFF ECAM MESSAGE: L/G LEFT LENGTHENING FAULT // DEC 23. TECHNICALLY CONCURS WITH MSN 1073 PERFORMING A MAXIMUM OF 2 FLIGHT CYCLES, IN ORDER TO REPOSITION THE AIRCRAFT FROM NYC TO RNG WITH THE LANDING GEARS RETRACTED. THIS TECHNICAL ADAPTATIONSDR HALA2018122400672Connector · brokenETOPS SIGNIFICANT SYSTEM - AFTER APU BLEED & PACKS COMMANDED ON. ENG 2 BLEED VALVE NOT CLOSED FAULT DISPLAYED ON ECAM.// INSPECTED ENG 2 BLEED VALVE & FOUND CONNECTOR BROKEN. REPLACED CONNECTOR(FIN 4001HA)PER AMM 71-71-20. RAN #2 ENG. ECAM WARNING "ENG 2 BLEEDSDR HALA2018122400671Smoke Detector · false indicationECAM MESSAGE "SMOKE LAVATORY DET FAULT".// REMOVED AND REPLACED LAV11 SMOKE DETECTOR PER AMM 26-17-15, PERFORMED OPS CHECK, CONDITION SAME. FAULTING DEUB (300RH1). MORE T/S REQUIRED. INSTALLED NEW DEU AT POSITION B PER AMM 23-73-47, GROUND SCANNING OF THE CIDSSDR HALA2018122400673Terminal · crackedETOPS SIGNIFICANT SYSTEM - #2 EGT INDICATES 122-140 C ALL OTHER ENGINE PARAMETERS NORMAL (FOR REFERENCE #1 EGT 570 C).// FOUND THERMOCOUPLE EGT 4 O'CLOCK POSITION TERMINAL POST CRACKED. REPLACED EGT THERMOCOUPLE PER AMM 77-21-11. KD 12/15/18 OPS CHECK PENDING.SDR HALA2018122400670Gear · damagedETOPS SIGNIFICANT SYSTEM - APU DOOR SHOWS OPEN WITH APU IN OFF POSITION/ AUTO SHUT DOWN ON ECAM.// PERFORMED BITE TEST ON APU SHUTDOWN MSG OIL CONTAMINATION OIL
CHIP DETECTION REMOVED AND REPLACED FILTERS, AND INSPECTED CHIP DETECTORS. MSG CLEARS DOOR ACTSDR HALA2018122100669Control Unit · malfunctionedETOPS SIGNIFICANT SYSTEM - ENG 2 CTL SYS FAULT. // ACCOMPLISHED VSV SYSTEM TEST AMM 75-33-00, TEST FAIL. FOUND VSV SYSTEM/VSV CONTROL UNIT FAULT. (E2-4081KS) TSM 75-33-00 SET PER 4.A
.(1) PENDING. ACCOMPLISHED 4A1 NO DEFECTS. ACCOMPLISHED TSM 75-33-00-810-80SDR HALA2018122000668Oil System · lowETOPS SIGNIFICANT SYSTEM - APU ECAM MAINTENANCE MSG / CK OIL QTY.// POST FLT REPORT SHOWS APU / CHECK OIL QUANTITY CLASS 2 HARD MSG. T/S PER A330 TSM 49-00-00-810-876-A. SERVICED APU OIL PER A330 AMM 12-13 & SAME BITE CK OK. RAN APU PER A330 AMM 49-00 & SAME NSDR HALA2018122000667A/C Pack · malfunctionedETOPS SIGNIFICANT SYSTEM - AMBER XX ON ENGINE #1 PACK DISCHARGE TEMP// RESET PACK CONT 1. ALL INDICATIONS RETURNED TO NORMAL. NO 30 DAY
HISTORY. OK FOR SERVICE.SDR AALA20190109919Engine · contaminatedDURING CLIMB OUT, BOTH PILOTS NOTICED A DIRTY-SOCK ODOR. RETURNED TO DEPARTURE. THE AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED THE NR 1 ENGINE IAW JC 33L40071003 DUE TO OIL INJESTION.SDR HALA2018121900665Fault Message · false activationETOPS SIGNIFICANT SYSTEM - ENGINE 1 REV. FAULT. // OPS TEST #1 ENG REV PER A330 AMM 78-31-00-740-802-A, OPERATION NORMAL. A/C, OK FOR SERVICE.SDR HALA2018121900664Warning Message · false activationETOPS SIGNIFICANT SYSTEM - AFTER TAKEOFF ENG 2 BLEED VALVE INOP. PER MX PERFORMED RESET OF BLEED OPERATION RETURNED TO NORMAL OPS. // T/S PER A330 TSM 36-11-00-740-804 NO BMS #2 FAULTS NOTED RAN #2 ENG AS PER A330 AMM 71-00-00 INDICATIONS SHOW NORMAL / OPEN ASDR AALA201812189058Nut · wornWORN NUT AND BOLT IN THE R2 DOOR SLIDE. REPLACED THE NUT AND BOLT IAW AMM, AND SRM 51-42-11.SDR HALA2018121700663Controller · malfunctionedETOPS SIGNIFICANT SYSTEM - COCKPIT TRIM AIR TEMPERATURE WAY TOO HOT. 125-130. TWICE RESET ZONE CONTROL WITHOUT EFFECT. RESET TEMP CONTROLLER PER A330 AMM 21-63. OPS CHECK GOOD. NO FAULTS. CLEANED TEMP SENSOR. OPS CHECK GOOD. OK FOR SERVICE.SDR HALA2018121700662Not Reported · malfunctionedETOPS SIGNIFICANT SYSTEM - APU DID NOT START AFTER 3 TRIES. C/W TSM 49-62-00-810-838A. NO FAULTS NOTED. STARTED APU TWICE ON GROUND WITH NO FAULTS. DUE TO LACK OF HISTORY. OK FOR CONTINUED SERVICE.SDR HALA2018121700660Warning System · false activationETOPS SIGNIFICANT SYSTEM - AIR BLEED 1 FAULT ON TAXI OUT. RESET ENG 1 BLEED PER MOC. ENG 1BLEED FUNCTION NORMAL. PERFORMED BITE OF BUC 1. NO FAULTS EXISTING. SUSPECT FAULT COINCIDED WITH PACK FAULT, REF LOG 5385779 AND 0863736. OK FOR SER.SDR HALA2018121700659Exciter · malfunctionedETOPS SIGNIFICANT SYSTEM - BRAKE RIDER REPORTS APU WON’T START. REMOVED AND REPLACED IGNITER PLUGS. NO HELP PER AMM 49-41-41. TROUBLESHOT PER TSM 49-41-00-810-804-A 'APU AUTO SHUT DOWN NO FLAME IGNITION EXCITER FAULT'. REMOVED AND REPLACED APU EXCITER BOX PER SDR HALA2018121700658Warning System · false activationETOPS SIGNIFICANT SYSTEM - AFTER LANDING & ENG NR 2 SHUTDOWN ENG NR 2 OIL CHIP DETECTED. ADVISED BY CREW FAULT WENT AWAY SHORTLY AFTER. PERFORMED BITE TEST ON CHANNEL A. NO FAULTS. NO HISTORY. CHANNEL B NO FAULTS NO HISTORY. CHECKED ENG NR 2 CHIP DETECTOR, NO SDR HALA2018121840364Anti-Ice Valve · inoperativeAIRCRAFT 386 DIV, DIVERTED TO LAX DUE TO THE ANTI-ICE LEFT AND RIGHT WING HIGH PRESSURE ECAM AND ASSOCIATED AMBER TRIANGLE AND AMBER ANTI-ICE DEPICTED ON BLEED PAGE. TURNING OFF THE WING ANTI-ICE PUSHBUTTON, ECAM MESSAGE DISAPPEARED. CORRECTIVE ACTION: REPLACESDR HALA2018121700661Fairing · puncturedLEFT WING NR 4 CANOE FAIRING HAS A PUNCTURE ON BOTTOM. INSTALLED PERMANENT REPAIR IAW SRM 57-56-00-300. A/C OK FOR SERVICE.SDR AALA201812179005Engine · overservicedDIRTY SOCK MIXED WITH AIRCRAFT DEICE FLUID ODOR IN THE CABIN. THE AIRCRAFT WAS GROUNDED. PERFORMED CABIN ODOR CARDS 33L00071001, 33L00021001, 33L00021001, AND 33L00021002. FOUND THE NR 2 ENGINE OVERSERVICED.SDR HALA2018121840346Skin · damagedAIRCRAFT LEFT FUSELAGE SKIN DAMAGED BETWEEN STR 41L AND STR 42L AT FR 35. REPAIRED PER SRM 53-21-11-015. LP 5409050SDR HALA2018121700657Anti-Ice Valve · malfunctionedATB - ETOPS SIGNIFICANT SYSTEM - ENCOUNTERED ICING CONDITIONS ECAM DIRECTED US TO TURN ON WING ANTI-ICE. AFTER APPROX 2 MINUTES OBSERVED A ICE L AND R WING HI PR ECAM AND ASSOCIATED AMBER TRIANGLE AND AMBER "ANTI ICE" DEPICTED ON BLEED PAGE. RECYCLED WING ANTISDR AALA201812149011Bottle · low pressureON PDC, L1 DOOR ASSIST SLIDE BOTTLE PRESSURE LOW. MAINTENANCE REPLACED THE DISK AND SEALS ON THE DOOR ASSIST BOTTLE IAW AMM 52-10-00-860-803-A, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.SDR HALA201812134653Pump · defectiveETOPS SIGNIFICANT SYSTEM - IN CRUISE ECAM FUEL - T TANK XFR FAULT. // T/S PER A330 TSM 28-27-00-810-823-A. FOUND TRIM TANK TRANSFER PUMP 709QN DEFECTIVE. ELECTRICAL CONNECTOR STILL OPEN. ALL WORK IN ACCORDANCE WITH SFAR 88 AND CDCCL. PULLED & COLLARED C/B E40 SDR HALA2018121340652Apu · unknownETOPS SIGNIFICANT SYSTEM - UNABLE TO START APU.// PERFORMED TSM 49-62-00-810-836-A. NO FAULTS NOTED. OPS CHECK GOOD. OK FOR SVC.SDR HALA2018121340650Unknown · odorSTRONG ODOR ON CLIMB OUT INTERMITTENTLY THROUGH CRUISE-ODOR AGAIN STRONG ON APPROACH- IN COCKPIT AND CABIN. // ISOLATED BLEED SOURCES APU, #1, & #2 ENGINES. PERFORMED OPERATIONAL
TEST OF PACK CONTROL AND INDICATING SYSTEM PER AMM 21-53-00-710-801-A. OPS NORMASDR HALA2018121340651Unknown · unknownETOPS SIGNIFICANT SYSTEM - ECAM AIR ENG 2 BLEED NOT CLOSED. ON SHUTDOWN. // FOUND NO FAULTS.PERFORMED 1/2 BMC TEST PER A330 AMM 36-11-00. NO
FAULTS NOTED. NO PREVIOUS HISTORY. OK FOR SVC.SDR AALA201812129001Damper · low pressureAIRCRAFT WAS NOT GROUNDED: 1L DOOR DAMPER CHARGE LOW. MAINTENANCE ACCOMPLISHED AMM 52-10-00 CHARGING OF THE DOOR DAMPER AND PERFORMED SATISFACTORY OPERATIONAL CHECKS OF EMERGENCY OPERATION CYLINDER.SDR HALA2018121200648Transceiver · faultedETOPS SIGNIFICANT SYSTEM - PWS ON WX RADAR NR 2 INOP. PULLED POST FLIGHT REPORT. FOUND WXR2 RTU (13SQ2) FAULTED. REPEATED WRITE UP 4 EVENTS WITHIN 60 DAYS. REMOVED AND REPLACED TRANSMITTER RECEIVER UNIT (13SQ2) PER AMM 34-41-51. BITE TEST OK. OK FOR SVC.SDR HALA2018121200647Transducer · malfunctionedETOPS SIGNIFICANT SYSTEM - DURING TAXI OUT OBSERVED ECAM: AIR ENG 1 BLEED FAULT. PER MOC PERFORMED RESET, FAULT CLEARED. REMOVED AND REPLACED ENG 1 PRESSURE TRANSDUCER PER AMM 36-11. OPS CK GOOD.SDR HALA2018121100645Apu · malfunctionedETOPS SIGNIFICANT SYSTEM - INFO TO MX APU DID NOT START BETWEEN 7000' - 3000' TWICE. STARTED SUCCESSFULLY ON GROUND AT 3RD ATTEMPT. // NOTED BY MAINTENANCE PERFORMED TROUBLESHOOTING OF APU AUTO SHUT DOWN PER TSM TASK 49-62-00-810-838-A. PERFORMED FAULT CONFIRMSDR HALA2018121100644Radar · malfunctionedETOPS SIGNIFICANT SYSTEM - WX RADAR #2 INOP.// BITE TESTED WXR 2 AS PER A330 AMM 34-41, OPS CHECKED NORMAL, AC OK FOR SVC.SDR HALA2018121000643Warning Message · false activationETOPS SIGNIFICANT SYSTEM - ENG #2 THRUST REVERSER FAULT.// T/S PER HAL330 TSM 78-31-00-810-974A NO FAULTS NOTED CONTACTED MCC OK FOR SVC.SDR HALA2018121000642Unknown · odorDURING CRUISE, ELECTRICAL SMELL REPORTED BY FLT. ATTEND. IN MID GALLEY & ROWS 14, 15, 16 AIRCRAFT RIGHT ONLY. GALLEY OVEN CIRCUIT BREAKERS PULLED & SMELL DISSIPATED. // REMOVED MID GALLEY OVENS 1 & 2 FROM GALLEY, & CHECKED FOR DEFECTS BEHIND OVENS. NO DEFECTSDR HALA2019061260106Skin · damagedLOAD HIGH PITCH NOISE HEARD IN LOWER DECK CREW REST MODULE. FOUND DAMAGE TO AFT CARGO DOOR INNER SKIN BETWEEN FR 64-64A AND BEAM 4-5. BLENDED OUT DAMAGED AREA, AND INSTALLED PERMANENT REPAIR AREA PER SRM 52-32-00-300-022 AND ER/A 573535-14. LP 4965119SDR HALA2018120600634Valve · malfunctionedETOPS SIGNIFICANT SYSTEM - ECAM: ENGINE AIR BLEED NOT CLOSED NR 2 ENG. REMOVED AND REPLACED NR 2 ENG PRV PER AMM 36-11-52. OPS CK & LEAK CK OK. A/C OK FOR SVC.SDR HALA2018120600633Fadec · malfunctionedETOPS SIGNIFICANT SYSTEM - AT ENG START 2 TIMES ON NR 1 GOT ENG 1 REV FAULT ENG 1 SHAFT PROT FAULT. RESET FADEC 1 PERFORMED ENG START, NO FAULTS. NR 1 ENG OK FOR SVC IAW TSM 73-21-00.SDR AALA201812069012Floor Panel · delaminatedDELAMINATED FLOOR PANEL 151CF IN THE AFT CARGO BAY. REPLACED THE FLOOR PANEL 151CF IAW SRM 53-02-00-300-009.SDR HALA2018120500630Warning Message · false activationETOPS SIGNIFICANT SYSTEM - INFO TO MX AFTER LEVEL OFF HAD ECAM FUEL R2 PRESS LOW. LASTED APPROX. 2 MIN AND 45 SEC. FIXED ITSELF AND HAD NO RECURRENCE.// CHECKED TANK FOR WATER NONE NOTED. PURGED PRESSURE SWITCH LINE REF A330 AMM 28-21-00. RAN PUMP FOR 30 MIN NSDR HALA2018120500629Warning Message · false activationETOPS SIGNIFICANT SYSTEM - LEFT FUEL PUMP #1 LOW PRESSURE DESCENT.// PERFORMED FCMC BITE & FUEL PUMP L#1 OPE NORMAL PER A330 AMM 28-
51-00. OK FOR SVC.SDR HALA2018120400628Actuator · malfunctionedETOPS SIGNIFICANT SYSTEM - APU AUTO-SHUT DOWN @ GATE FUEL TRIM LINE FAULT. // REMOVED & REPLACED TRIM TANK INLET VALUE ACTUATOR PER AMM 28-27-
52. FUEL TRIM LINE FAULT NO SHOW. BLEED APU FUEL LINE. OPS CHK OK. OK FOR SVC
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