N384HA
Service difficulty reports · 166
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N384HA' AND registry_match = 'registration' 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 n_number = 'N384HA' AND registry_match = 'registration' 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 HALA2022022400056None · noneETOPS - #2 ENG AFT UPPER INBD FIRE SEAL HAS 6" HOLE // REPLACED ENG2 AFT UPPER INBD FIRE SEAL PER TRENT 700 CMM 78-11-14. AC OK FOR SVC.SDR HALA2022012500027Valve · inoperativeBTFS AFTER SHUTTING DOWN APU RECEIVED "FUEL TRIM LINE FAULT" EICAS MESSAGE // REMOVED AND REPLACED APU FUEL ISOLATION VALVE PER A330 AMM 28-29 AND PERFORMED OPERATIONAL TEST. OPS TEST NORMAL OK FOR SERVICE. ACTUATOR ASSY, OFF 33-2409-9-0001 S/N 00757 ON 33-24SDR HALA2022011000008Valve · inoperativeETOPS - "FUEL TRIM LINE FAULT" ON ECAM // REMOVED & REPLACED APU ISOLATION VALVE (5QF) PER AMM 28-29-51-00 -801-A/400-801-A. OPS CHECK GOOD. NO MESSAGE ON ECAM ACTUATOR ASSY, OFF 33-2409-9-0001 S/N 01581 ON 33-2409-9-0001 S/N 00757SDR HALA2022010400005Valve · inoperativeETOPS - FUELER REPORTED END LIGHT FLASHING UNABLE TO REFUEL // GROUND SCAN SHOWS LH INLET INTR TANK ACTUATOR (603QL1) REMOVED AND REPLACED FUEL INLET VALVE (603QL1) ACTUATOR PER AMM 28-26-53. OPS AND LEAK CHK GOOD. OK FOR SVC. ACTUATOR, SINGL OFF 43-2826-9-000SDR HAL2022F00001Epsu · inoperativeSHIP 384 DURING EPSU TIME CHANGE, FOUND 16WL EPSU FAULTING. CORRECTIVE ACTION: REMOVED AND REPLACED EPSU ASSY 16WL. (7245616)SDR HALA2022010300003Controller · inoperativeETOPS - ENG 2 CTL SYS FAULT // ACCOMPLISHED TSM 75-33-00-810-808-A UP TO STEP 4.A(1)(B) MECH #565713 12/29/21. NEED TO CONTINUE FROM 4.A.2. ACCOMPLISHED TSM 75-33-00-810-808-A UP TO STEP 4.A.(2). RESITTANCE LIMITS OUT OF LIMITS. MECH #1825633 12/29/21. NEED SDR HALA2021111600160None · noneETOPS-APU AUTO SHUTDOWN // APU FAULTS NO FUEL SUPPLY. UNABLE TO BLEED APU NO FUEL EXITS FUEL LINE AT FUEL CONTROL. FOUND APU FUEL ISOLATION VALVE 5QF
DOES NOT OPEN FOUND 28 VDC PIN B OPEN WHEN MASTER SWITCH ON. SUSPECT ISOLATION VALVE ACTUATOR 5QF(AR0339SDR HALA2021102100173None · noneSHIP 384 EXIT SIGN ABOVE 3L DOOR CAME OFF. CORRECTIVE ACTION: RESECURED 3L EXIT DOOR SIGN. (7733357)SDR HALA2021092300122None · noneETOPS - DUE TO REPEAT ECAM WARNING ENG 2 MINOR FAULT. NEED TO REPLACE PCU // REMOVED & REPLACED ENG #2 PCU PER AMM 73-21-35. OPS CHECK GOOD.
OK FOR SVC. CONTROL, UNIT PN OFF 43-7321-9-0003 SN 80771 ON 43-7321-9-0003 SN 81750SDR HALA2021091200114Pump · low pressureETOPS - R STBY FUEL PUMP LOW PRESS. REMOVED AND REPLACED R STBY FUEL PUMP (112QA2) PER AMM 28-21-51-400-802-A. OPS / LEAK CHECK OK. A/C OK FOR SVC.SDR HALA2021090900110Coupler · inoperativeETOPS - UNABLE TO TUNE OR SELCAL CHECK HF#2 // REMOVED AND REPLACED HF2 COUPLER PER AMM 23-11-36. OPS CHECK GOOD. HF TUNNING WORKIS NORMAL. OK FOR SVC. COUPLER, ANTENN OFF P/N 43-2311-9-0001 S/N 03440 ON P/N 43-2311-9-0001 S/N 0336SDR HALA2021081600116Lens · unsecureSHIP 384 2L EMER EXIT SIGN LENSE NOT SECURED. CORRECTIVE ACTION: RE-SECURED 2L EMER EXIT SIGN. (7721493)SDR HALA2021081000101Exciter · faultedETOPS - GN A FAULT, REMOVED AND REPLACED ENG 1 A EXCITER A330 AMM 74-11-54. OPS CK GOOD.SDR HALA2021081000113Handle · unsecureSHIP 384 UPON LANDING AND NOSE WHEEL TOUCHDOWN ECAM DOOR - AVIONICS DOOR OPENED. CORRECTIVE ACTION: FOUND AVIONICS DOOR HANDLE EXTENDED. INSPECTED DOOR HANDLE AND SECURED. (7721427)SDR HALA2021072400089Engine · making metalETOPS - ON TAXI IN ECAM ENG 1 OIL CHIP DETECTED - NEED TO REPLACE #1 ENGINE S/N: 42177 DUE TO EMCD DEBRIS REF L/P 7250089 // REPLACED #1 ENGINE PER CARD 7100-9401-HAL. HIGH POWER RUN COMPLETED. OPS LEAK CHECK GOOD. OFF P/N 43-7110-9-0010 S/N 42177 ON P/N 43-SDR HALA2021072100101Light · inoperativeSHIP 384 3R EMERGENCY LIGHTS INOP. RESET AND TESTED EPSU. LIGHT OPS NORMAL.SDR HALA2021040900046Generator · defectiveETOPS - BITE TEST OF GAPCU SHOWS CLASS 1 FAULT 242300 WRG: GEN APU FEEDER. TROUBLESHOOT PER TSM TASK 24-20-00-810-998-A UP TO STEP 4A.(2)(B) & FOUND FEEDERS ARE CORRECT. REMOVED AND REPLACED APU-GEN (8XS) PER AMM 24-23-51. OPS TEST GOOD. BITE TEST OF THE GAPCUSDR HALA2021012500005Lug · corrodedCORROSION FOUND ON RT RIB 6 FWD LUG. CORRECTIVE ACTION: CORROSION REMOVED BY OVERSIZING BORE AND SPOTFACING AFT FACE.SDR HALA2021012500004Lug · corrodedRT RIB 6 RT CORROSION ON FWD LUG. CORRECTIVE ACTION: CORROSION REMOVED, IAW ERA 586375-14AD REVISION ORIGINAL.SDR HALA2021020300009Fitting · corrodedSHIP 0384 RT RIB 6 FITTING WAS FOUND CORRODED. CORRECTIVE ACTION RHS RIB 6 FITTING WAS REWORKED PER ERA.SDR HALA2020123000230Actuator · defectiveETOPS-FUEL ENGINE 1 LP VALVE FAULT AT SHUTDOWN. REMOVED & REPLACED NR 1 ENGINE LP VALVE ACTUATOR, PER AMM 28-24-51. PERFORMED OPERATIONS CHECK, PER AMM 28-24-00. OPERATIONS CHECK OK. NO FAULTS NOTED. OK FOR SERVICE. ACTUATOR, TWIN OFF 33-2820-9-0003 9089SDR HALA2020073100163Oil Cooler · leakingETOPS SIGNIFICANT SYSTEM - #1 ENG LEAKING FUEL FROM AOHE DRAIN LINE. // REPLACED #1 ENG AIR/OIL HEAT EX-CHANGER PER AMM 79-21-57-400-803-A UP TO STEP 4.A.(12),LEAK CHECK PENDING.
LEAK CHECK COMPLETED IN REF W/ A330 AMM 79-21-57-400-803-A. NO LEAKS NOTED. TSDR HALA2020073100162Priority Valve · malfunctionedETOPS SIGNIFICANT SYSTEM, NR 1 ENGINE BLEED NOT CLOSED. REPLACED THE NR 1 ENGINE PRV IAW AMM 36-11-52-804-A/ 36-11-52-400-804-A. OPS CHECK AND LEAK CHECK OK.SDR HALA2020030900053Pcu · malfunctionedETOPS SIGNIFICANT SYSTEM - APU GEN FAULT. // REMOVED & REPLACED APU GEN IAW HAL A330 TSM 24-23. FAULT REMAINS STILL. WAITING ADDITIONAL PARTS. DELL 111745. ALSO REF TSM 24-20
-00-810-986-A PERFORMED WIRE CHECK BETWEEN GAPCU AND APU GEN PER STEP 4.A.2. ALL CK'SDR HALA2019120900509Sign · detachedEXIT SIGN ABOVE DOOR 3R NEEDS TO BE RE-ATTACHED. FELL OFF DURING BOARDING. // REATTACHED EXIT SIGN AT 3R. OK FOR SVCSDR HALA2019081210386Idg · making metalETOPS SIGNIFICANT SYSTEM - ELECTRIC GENERATOR 2 FAULT. REMOVED AND REPLACED IDG 2 PER AMM 24-21 OPS CHECK GOOD.SDR HALA2019060700280Warning Message · false activationETOPS SIGNIFICANT SYSTEM - FCMC 2 FUEL FAULT ECAM. PERFORMED BITE TEST OF FCMC 2 PER AMM 28-51-00.NO FAULTS, MESSAGE EXTINGUISHED. OK TO CONTINUE.SDR HALA2019051700248Warning System · false activationETOPS SIGNIFICANT SYSTEM - FUEL - LEFT PUMP 1 LO PR ECAM ILLUMINATED IN - CRUISE. PERFORMED FCMC 1 AND 2 BITE PER AMM 28-51-00-740-801-A, TEST OK. PERFORMED OPERATIONAL CHECK OF L1 ENGINE 1 FUEL PUMP PER AMM 28-21-00-710-801-A. OPERATIONAL CHECK GOOD. OK FOR SDR HALA2019030100080Warning System · false activationETOPS SIGNIFICANT SYSTEM - ON SHORT FINAL FUEL L STBY PUMP LO PRES ECAM. NO FAULTS NOTED SYSTEM 1 & 2. NO CLASS 3 MESSAGES. PERFORMED FCMC SYSTEM TEST. FCMC 1 SYSTEM TEST OK. FCMC 2 SYSTEM TEST OK. OPERATED L STBY PUMP. OPS NORMAL. NO LOW PRESS INDICATION.SDR HALA2019021540955Filter · cloggedDIVERTED DUE TO THE NBR 1 ENGINE FUEL FILTER CLOG MESSAGE, AND ENG EPR MODE RECOVERABLE MESSAGE. CORRECTIVE ACTION: REPLACED NBR 1 ENGINE LP FUEL FILTER (4088327), OPU, PCU, AND ECC (4088328). LP 4088327, 4088328.SDR HALA2019020800052Warning Light · false activationETOPS SIGNIFICANT SYSTEM - ECAM FUEL LEFT PUMP 2 LO PRESS INDICATION FOR APPROX. 2-3 MIN DURING CRUISE @ FL390. // T/S PER A330 TSM 28-21-00-810-852-A. DURING GROUND TRANSFER OF
FUEL, ALL OPERATIONS WERE NORMAL AND ALL ECAM INDICATIONS WERE NORMAL. OK FOR SVCSDR HALA2019020700048Eec · faultyETOPS SIGNIFICANT SYSTEM - 1 ENGINE SN 41948 IS EXPERIENCING APPARENTLY UNCOMMANDED EEC CHANNEL CHANGES REPETITIVELY. REMOVED AND REPLACED NR 1 ENG EEC PER AMM 73-21-34-000-804-A/400-804-A. PERFORMED TEST OF EEC CONFIGURATION, TEST OF FADEC SYSTEM & LAND TEST.SDR HALA2019012800544Slide · defectiveDURING C CHECK, DOOR 1 RIGHT FAILED OPERATIONAL CHECK OF EMERGENCY LIGHTS. REPLACED DOOR 1 RIGHT SLIDE PACK.SDR HALA2019012500032Pump · leakingETOPS / NR 2 ENGINE YELLOW EDP IS LEAKING AT MOUNTING FLANGE. REF: N/R 183 FOR REMOVE AND REPLACEMENT OF NR 2 ENGINE YELLOW EDP.SDR HALA2019010700006Warning System · false activationETOPS SIGNIFICANT SYSTEM - APU BLEED FAULT AFTER LANDING. RESET 3X SAME EFFECT. PER TSM 49-62-00-810-846 PERFORMED APU FUNCTION CHECK & APU BITE TEST. ALL TESTS PASS & NO CURRENT FAULTS. OK TO CONTINUE.SDR HALA2019010400006Warning System · false activationETOPS SIGNIFICANT SYSTEM - APU BLEED FAULT AFTER LANDING. RESET 3X SAME EFFECT. PER TSM 49-62-00-810-846 PERFORMED APU FUNCTION CHECK & APU BITE TEST. ALL TESTS PASS & NO CURRENT FAULTS. OK TO CONTINUE.SDR HALA2019010700010Cover · missingLEFT NR 3 FLAP TRACK FAIRING COVER MISSING. INSTALLED SPEED TAPE UNTIL COVER CAN BE REPLACED.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 HALA2018111650333Scuff Plate · damagedAIRCRAFT 384, ATB, RETURNED TO LAX DUE TO A PRESSURIZATION LEAK AT DOOR 4R, UNABLE TO HOLD CABIN PRESSURE. CORRECTIVE ACTION: REMOVED DOOR 4R SCUFF PLATE AND SCRAPPED OFF OLD SEALANT AND CLEANED AREA. INSTALLED NEW SCUFF PLATE AND SEALANT. PRESSURIZED AIRCRAFTSDR HALA2018111400583Scuff Plate · damagedATB- PRESSURE LEAK AT 4R DOOR. UNABLE TO HOLD CABIN PRESSURE.// PRESSURIZED A/C PER A330 AMM 05-53-00 FOUND DOOR 4 RIGHT LEAKING AT BOTTOM CORNERS OF DOOR. PERFORMED REMOVAL OF DOOR 4 RIGHT SCUFF PLATE AND SCRAPPED OFF AND CLEANED OLD SEALANT PER A330 AMM 53-SDR HALA2018082200397Duct · disconnectedETOPS SIGNIFICANT SYSTEM - COCKPIT TEMP CYCLES BETWEEN 70* TO 80 DEGS. TRIM CYCLES BETWEEN 48* TO 124 DEGS. TEMP SELECTOR SET AT 12 O'CLOCK POSITION WHILE TEMP ELEVATES. CLEANED AND INSPECTED COCKPIT TEMP SENSOR PER AMM 21-63-17. NO DEFECTS FOUND. OPS NORMAL. SDR HALA0218082100394Controller · malfunctionedDUCT TEMP ON CONDITION PAGE INDICATING 110, WITH TEMP IN COCKPIT INDICATING 74. REMOVED AND REPLACED THE ZONE CONTROLLER IAW AMM 21-63-34-00-801-A. ECS TESTED OK. OPS CHECKED OF ZONE CONTROL SYSTEM NORMAL. NO DEFECTS. OK FOR SERVICE.SDR HALA2018081300368Bellows · failedBELLOWS ADJACENT TO THE RT PACK TEMPERATURE CONTROL VALVE BLOWN APART. THE RT PACK CONTROL VALVE BELLOWS WAS REPLACED AND TESTED. NO LEAKS.IAW AMM 21-52-21-000-801-A, AND 21-52-400-801-A, REV 61.05.SDR HALA2018012500013Fire Loop · faultedETOPS SIGNIFICANT SYSTEM - ENG 2 FIRE LOOP A FAULT. REMOVED & REPLACED ENG 2 PYLON LOOP A DETECTOR FIN# 6WD2 PER AMM 26-12-16. OPS CHECK GOOD.SDR HALA2017111900262Cover · looseEMERGENCY EXIT COVER LOOSE AND DOOR 3R. RE-INSTALLED DOOR 3R EXIT COVER.SDR HALA2017111600261Cover · unsecureDOOR 2L EXIT SIGN COVER FELL OFF. SECURED EXIT SIGN COVER AT DOOR 2L.SDR HALA2017082300233Smoke Detector · false activationECAM FOR CABIN REST SMOKE ALARM ACTIVATED. CONFIRMED NO SMOKE. PERFORMED TSM 26-18-00-810-855-A. BITE TEST OF SMOKE DETECTOR IAW AMM 26-16-00-740-801.TEST PASSED, ACFT OK FOR SERVICE.SDR HALA2017061200148Eec · malfunctionedDURING CLIMB AT 380 FOR 390, RECEIVED ECAM A/THR OFF FOLLOWED BY ECAM ENG 2 EPR MODE FAULT & ECAM ENG 1 EPR MODE FAULT. ECAM HAD US PUT BOTH ENGS IN N1 MODE BUT WE STARTED HAVING MULTIPLE ECAMS FLASH QUICKLY ACROSS THE SCREEN AND IT WAS IMPOSSIBLE TO FOLLOW. PSDR HALA2017053000127Warning Light · false activationCIDS 1 & 2 FAULT, RESET OF CIDS, 1 & 2 FAILED. PERFORMED CIDS 1 & CIDS 2 RESET IAW 23-73 OPS CHECKED NORMAL.SDR HALA2017051800174Brake · malfunctionedAIRCRAFT 0384, ABORTED TAKEOFF AT 80 KNOTS DUE TO NR 6 BRAKE SHOWING 305 DEGREES. DEFERRED PER MEL 32-42-1-HNL REPLACED NR 6 BRAKE.
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