N230HA

Service difficulty reports · 32

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 = 'N230HA' 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.

SDR ASAA2026082066433Smoke Detector · false activationLAVAORY SMOKE CAM DURING CRUISE , EXTINGUISHED AFTER A FEW SECONDS. NO ALERTS IN THE CABIN OCCURED. GROUNDED - YES. PERFORMED OPERTIONAL CHECK OF LAV SMOKE DECTECTION IAW AMM 26-17-00. OPS CHECKED GOOD. OK TO CONTINUE SERVICE.Aug 20, 2026 · N230HA · Airbus A321271N · Smoke DetectionSDR HALA20250903270Pump · faultedETOPS - AT CRUISE ECAM B SYS LO PR, FOLLOWED BY B RSVR LO LVL. ECAM ACTIONS COMPLETED, (SHUTDOWN B ELEC PUMP) NO FURTHER ACTIONS. REMOVED AND REPLACE BLUE ELECTRIC PUMP PER AMM 29-12-51. PERFORMED TEST OF BLUE ELEC PUMP PER AMM 29-12-00. TEST OK. NO LEAKS NOTESep 2, 2025 · N230HA · Airbus A321271N · Hydraulic Pump (Electric/Engine), MainSDR HALA20250109011Fire Loop · faultedETOPS - IN CRUISE AT FL320 ENG 2 FIRE LOOP B FAULT. REMOVED RH ENG AFT FIRE/OVERHEAT DETECTOR 4001WD2 PER AMM 26-12-17-000-803A. INSTALLED RH ENG FIRE/OVERHEAT DETECTOR 4001WD2 PER AMM 26-12-17-400-803-A. OPS CK GOOD. SECURITY CK GOOD.Jan 8, 2025 · N230HA · Airbus A321271N · Fire DetectionSDR HALA20241220375Packing · leakingETOPS - FOUND OIL STAINING @ BOTH ENG'S INLET CONE WEEP HOLES WHILE ACCOMPLISHING HAL CARD E1128-321-21-008-1. REPLACED BOTH ENGS FAN SHAFT COVERS PACKING PER AMM 72-15-00-960-801-A.LEAK CHK OK.Dec 19, 2024 · N230HA · Airbus A321271N · Turbine Engine Air Inlet SectionSDR HALA20241213363Diverter · cloggedDIV - ALL LAVS STOPPED FLUSHING IN FLIGHT. FL 360 2 HOURS INTO THE FLIGHT. ATTEMPTED RESET OF VACUUM SYSTEM VIA A5 CB ON AFT GALLEY OVHD PANEL PER MAINT DIRECTION WITHOUT SUCCESS. FOUND EXCESSIVE BUILD UP OF WASTE ON DIVERTER, FLUID LEVEL SENSOR, AND WASTE TRADec 12, 2024 · N230HA · Airbus A321271N · Waste Disposal SystemSDR HALA20241211356Sensor · failedDIV - ALL LAVS NOT FLUSHING ALL THE WAY UP TO FC. REMOVED AND REPLACED WASTE LIQUID LEVEL SENSOR (41MG) PER AMM 38-31-63. OPS CHECK GOOD. LEAK CHECK GOOD. NO FAULTS NOTED. OK FOR SVC.Dec 10, 2024 · N230HA · Airbus A321271N · Waste Disposal SystemSDR HALA20241127339Oil System · leakingETOPS - ENG #2 DURING THE WALKAROUND OIL WAS DISCOVERED DRIPPING CONTINOUSLY. REMOVED & REPLACED #2 ENGINE ENGINE DRIVEN PUMP PER AMM 29-13-51. OPS CHECK GOOD PER #2 ENGINE RUN. NO LEAKS NOTED. OK FOR SERVICE.Nov 26, 2024 · N230HA · Airbus A321271N · Turbine Engine Oil SystemSDR HALA20241112321Controller · faultedETOPS-BTB DUE TO ECAM: CAB PR SYS 1 FAULT. SWAPPED CPC 1 & CPC 2. OPS CHK NORMAL PER AMM 21-31-00.Nov 11, 2024 · N230HA · Airbus A321271N · Cabin Pressure ControllerSDR HALA20241031062Smoke Detector · no discrepancySMOKE LAVATORY SMOKE OCCURRED AT FL290 JUST PIROR TO THE ETP AT 0248Z TRANSIET ALERT DUE TO PASSENGER VAPING IN THE FORWARD LAV NO SMOKE OR FIRE PRESENT. PERFORMED OPERATIONAL CHECK OF LAV SMOKE DETECTION IN ACCORDANCE WITH AMM 26-17-00-710-001-A OPERATIOOct 29, 2024 · N230HA · Airbus A321271N · Smoke DetectionSDR HALA20240820234Sense Line · misinstalledETOPS - WHILE PERFORMING T/C E36-24-01-32 FOUND HPV SENSE LINE & UNION CROSS THREADED. INSTALLED NEW MUSCLE SENSE LINES FOR HPV PER AMM 36-11-49 OPS CHECK & LEAK CHECK GOOD IDLE RUN SUCCESSFULAug 19, 2024 · N230HA · Airbus A321271N · Pneumatic Distribution SystemSDR HALA20240808218Wire Harness · damagedATB - AIR TURN BACK DUE TO ENG 1 SYS FAULT ON CLIMB OUT. REMOVED AND REPLACED WO3 HARNESS PER AMM 73-21-63 OPS CHECK GOOD. PENDING BIFFLE INSTALL. INSTALLED BIFFLE PER AMM 73-21-63. OK FOR SVC.Aug 7, 2024 · N230HA · Airbus A321271N · Engine Fuel System WiringSDR HALA20240807215Fadec · faultedETOPS - ENG 1 FADEC SYS FAULT. REMOVED AND REPLACED N2 SPEED TACHOMETER PER AMM 77-11-23-400-801-A PENDING OPS CHECK. REMOVED AND REPLACED ENG 1 ECC PER AMM 73-21-34 UP TO STEP 5(2)A. COMPLETED REMAINING STEPS OF 73-21-34. OPS CHECK GOOD. OK FOR SERVICE.Aug 6, 2024 · N230HA · Airbus A321271N · Fuel Controlling SystemSDR HALA20240103001Unknown · unknownETOPS - APU AUTO SHUTDOWN. PERFORMED TSM 49-00-81-810-825-A. CONFIRMED FAULT "IGNITION UNIT SHOWS OPEN CIRUIT." REMOVED AND REPLACED IGNITION UNIT, ELECTRICAL LEAD, AND IGNITER PLUG PER AMM'S 49-41-38, 49-41-41, AND 49-41-43. OPS CHECK GOOD, MESSAGE CLEARED. OJan 2, 2024 · N230HA · Airbus A321271N · APU Start/Ignition SystemSDR HALA20231208266Transducer · faultedWHEEL TIRE PRESS LOW #2 ECAM 70-80PSI AT CRUISE DIVERTED TO HNL. REPLACED # 2 MLG TIRE PRESSURE TRANSDUCER REF AMM 32-49-16. OPS CHECKS GOOD. OK TO CONTINUE SERVICE. PLACARD REMOVED, MIC SHEET UPDATED.Dec 6, 2023 · N230HA · Airbus A321271N · TireSDR HALA202311274257Unknown · unknownETOPS-ENG 1 OIL CHIP DETECTED. REMEOVED AND REPLACED #1 ENG PER AMM 71-00-51Nov 25, 2023 · N230HA · Airbus A321271N · Engine (Turbine/Turboprop)SDR HALA20231122253Unknown · unknownETOPS - ENG 1 OIL CHIP DETECTED ECAM AFTER LANDING. PERFORMED MAGNETIC CHIP INSPECTION PER AIRBUS TSM 79-35-00-810A-808A. NO DEBRIS FOUND ON CHIP DETECTOR OR OIL FILTER. REMOVED AND REPLACED OIL FILTER. NO LEAKS NOTED NO DEFECTS NOTED. OK TO CONTINUE.Nov 21, 2023 · N230HA · Airbus A321271N · Engine Oil System (Airframe Furnished)SDR HALA20231121251Unknown · unknownETOPS - ENG 1 OIL CHIP DETECTED. PERFORMED MAGNETIC CHIP INSPECTION PER AMM 79-00-00-281-802A. NO DEBRI FOUND-CHECK GOOD. INSPECTED MAIN OIL FILTER & REPLACED PER AMM 79-21-06-960-801A. OPS CHECK GOOD. ENG IDLE RUN SATISFACTORY. A/C OK TO CONTINUE.Nov 20, 2023 · N230HA · Airbus A321271N · Engine Oil System (Airframe Furnished)SDR HALA20231002213Unknown · unknownETOPS - FOUND NACELLE ANTI-ICING DUCT DAMAGE. REMOVED AND REPLACED NACELLE ANTI-ICING DUCT PER AMM 30-21-49-000-807-A, OPS CHECKS GOOD, OK TO CONTINUE.Oct 1, 2023 · N230HA · Airbus A321271N · Engine Anti-Icing SystemSDR HALA20230925205Unknown · unknownETOPS - ENGINE 1 DIFF 1 BORESCOPE PLUG FOUND DAMAGED DURING BORESCOPE INSPECTION. #1 ENGINE REPLACED. ENG 1 VERIFICATION FLIGHT DUE TO ENG REPLACEMENT COMPLETED SUCESSFULLY. NO DEFECTS NOTED OK TO CONTINUE SVC.Sep 24, 2023 · N230HA · Airbus A321271N · Turbine Engine Combustion SectionSDR HALA2023081400172Eec · faultyETOPS - ENG 2 FUEL VALVE FAULT (FUEL VALVE NOT OPEN) ON ECAM AFTER ACCOMPLISHED OF TASK CARD # E73-23-01-32 (EEC SOFTWARE DATA LOAD). REMOVED AND REPLACED ENG #2 EEC PER AMM 73-21-01. ENGINE IDLE TEST GOOD, NO FAULTS NOTED. OK FOR SVC.Aug 12, 2023 · N230HA · Airbus A321271N · Fuel Controlling SystemSDR HALA2023071200143Unknown · unknownETOPS - WHILE PERFORMING BORESCOPE, FOUND #2 IGNITER PLUG WORN. REMOVED AND REPLACED #2 IGNITER PLUG PER AMM 74-21-01. OPS CHECK GOOD, OK FOR SERVICE.Jul 11, 2023 · N230HA · Airbus A321271N · Ignition SystemSDR HALA2023051500029Unknown · unknownMOMENTARY ENG 2 FIRE LOOP B FAULT ECAM IN CRUISE. NO FAULTS NOTED ON ECAM. PERFORMED BITE TEST OF FDU. NO FAULTS NOTED. OK FOR SVC IAW AMM 26-12-00.May 14, 2023 · N230HA · Airbus A321271N · Fire Protection SystemSDR HALA2023050800103Radar · faultyETOPS - DMI# 206909 WX RDR 2 GCS DOES NOT WORK ( WEATHER RADAR SYSTEMS TRANSCEIVER (AIRCRAFT WITH DUAL TRANSCEIVERS) (MAY BE INOPERATIVE). REMOVED AND REPLACED WEATHER RADAR TRANSMITTER PER AMM 34-41-33 BITE TEST OKAY NO FAULTS DETECTED PLACARD REMOVED MIC SHMay 5, 2023 · N230HA · Airbus A321271N · Weather Radar SystemSDR HALA2023031500038Wire Harness · faultyETOPS - DMI 206624 - [ENG 1 FUEL FILTER CLOG] FILTER REPLACED 50FH ( FUEL FILTER CLOG CAUTIONS ON ECAM E/W PW100G ENGINES (ONE MAY BE INOPERATIVE PROVIDED ASSOCIATED FILTER IS CHANGED BEFORE THE NEXT FLIGHT AND THEN EVERY 50 FLIGHT HOURS) ) REMOVED AND REPLACEMar 15, 2023 · N230HA · Airbus A321271N · Fuel Controlling SystemSDR HALA2023031000037Unknown · unknownETOPS - RECEIVED MULTIPLE ENG 1 FUEL SENSOR FAULT AND ENG 1 FUEL FILTER CLOG MESSAGES THROUGHOUT THE FLIGHT. ITEM ALREADY ON DEFERRAL, REMOVED AND REPLACED WC08 WIRING HARNESS PER AMM 73-31-21, OPS CHECK GOOD OK TO CONTINUE SERVICEMar 9, 2023 · N230HA · Airbus A321271N · Engine Fuel and ControlSDR HALA202303060034None · noneETOPS - ENG 1 FUEL FILTER CLOG ECAM INFLIGHT. REMOVED AND REPLACED FUEL FILTER IAW AMM 73-11-06-400-801-A. OPERATIONAL CHECK PERFORMED. OPS CHECK GOOD. LEAK CHECK GOOD.Mar 3, 2023 · N230HA · Airbus A321271N · Engine Fuel/Oil CoolerSDR HALA2023030300031Wire Harness · damagedETOPS- ENG 1 FUEL SENSOR FAULT HAPPENED 8 TIMES. FOUND DAMAGE ON WC08 WIRING HARNESS AFT OF FUEL FLOW SENSOR CONNECTOR (P27) REMOVED & REPLACED WC08 HARNESS PER AMM 73-31-21. NO FAULTS NOTED.Mar 2, 2023 · N230HA · Airbus A321271N · Fire DetectionSDR HALA2023030100030Pressure Sensor · false indicationETOPS-ENG 1 FUEL SENSOR FAULT FUEL FILTER SENSOR CAME ON 15 TIMES THROUGHOUT THE FLIGHT CLEARED ITSELF EVERYTIME. REMOVED AND REPLACED FUEL PRESSURE SENSOR IAW AMM 73-34-21-400-801-A AND 73-34-21-000-801-A. OPS CK GOOD.Feb 28, 2023 · N230HA · Airbus A321271N · Engine Fuel and ControlSDR HALA2022122800320Wire Harness · faultedETOPS, NR 1 ENGINE FIRE LOOP A FAULT MESSAGE ILLUMINATED, 15 MINUTES AFTER DEPARTURE AND REMAINED ON. AIRCRAFT DIVERTED TO HNL. REPLACED THE FIRE LOOP A, FIRE ELECTRICAL HARNESS IAW AMM 26-12-61-400-802-A, AND REPLACED FWD FIRE DETECTOR IAW AMM 26-12-17-400Dec 27, 2022 · N230HA · Airbus A321271N · Fire DetectionSDR HALA2022122700314Fire Loop · faultedETOPS - ECAM ENG 1 FIRE LOOP A FAULT PRIOR ENGINE START. REMOVED AND REPLACED LOOP-A FIRE DETECTORS CABLES PER AMM 26-12-61, AND REMOVED AND REPLACED FDU1 PER AMM 26-12-34. REMOVED AND REPLACED FWD AGB LOOP A PER AMM 26-12-17. FOUND FIRE ELECTRICAL HARNESS LOODec 24, 2022 · N230HA · Airbus A321271N · Fire DetectionSDR HALA2022081200143None · noneETOPS - ON TAXI IN APU AUTO SHUTDOWN // R/R EXCITER BOX IAW AMM 49-41-38 PB 401 OPS CHECK OKAY, A/C OK FOR SERVICEAug 11, 2022 · N230HA · Airbus A321271N · Airborne Auxiliary Power Unit (APU) SystemSDR HALA2022013100034None · noneBTB AFTER ENGINE STARTS FWD CRG HEAT / FWD CRG VENT // PERFORMED RESET AND BITE TEST IAW AMM 21-28-00. NO FAULTS NOTED AT THIS TIME.Jan 29, 2022 · N230HA · Airbus A321271N · Cabin Temperature Controller
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