N227HA

Service difficulty reports · 26

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 = 'N227HA' 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 ASAA2026062765513Battery · unserviceableEPSU BAT (15WL) FAIL. GROUNDED - YES. REMOVED AND REPLACED EPSU BATTERY (15WL) IAW AMM 33-51-38. BITE TEST OK. OK FOR SBC..Jun 27, 2026 · N227HA · Airbus A321271N · Emergency LightingSDR HALA20251002298Igniter · damagedETOPS - DURING T/C 321-724000-W2-1 FOUND ENG 2 LOWER IGNITER DAMAGED. REMOVED AND REPLACED IGNITER PER AMM 74-21-00. OPS TEST GOOD, OK TO CONTINUE.Oct 1, 2025 · N227HA · Airbus A321271N · Spark Plug/IgniterSDR HALA20250509026Smoke Detector · false activationSMOKE LAVATORY SMOKE LAV D. FA REPORTED ALL CLEAR. PERFORMED OPERATIONAL CHECK OF THE LAV SMOKE DETECTION PER AMM 26-17-00-710-001-A. OPS CHECK GOOD. NO FAULTS NOTED. A/C OK TO CONTINUEMay 6, 2025 · N227HA · Airbus A321271N · Fire DetectionSDR HALA20250314011Radome · damagedPOSSIBLE BIRD STRIKE DESCENDING BETWEEN 6-5000 FEET. REMOVED & REPLACED RADOME PER AMM 53-15-11. OK FOR SERVICE.Mar 12, 2025 · N227HA · Airbus A321271N · Aerodynamic FairingsSDR HALA20250115020B-Nut · damagedETOPS - WHILE PERFORMING E1128-321-73-019 FOUND AS11 TUBE B-NUT CROSS THREADED ON #2 ENGINE BURNER PRESSURE (PB) SENSOR. REMOVED & REPLACED AS11 TUBE PER AMM 73-21-23.Jan 14, 2025 · N227HA · Airbus A321271N · Engine Fuel and ControlSDR HALA20241230386Ignition Sys · malfunctionedETOPS - ECAM APU AUTO SHUTDOWN ON START ATTEMPT 3 UNSUCCESSFUL START ATTEMPTS. REMOVED AND REPLACED IGNITION UNIT PER A321 AMM 49-41-38 ECB TEST OK OPS CHECK NORMAL A/C OK FOR SERVICEDec 28, 2024 · N227HA · Airbus A321271N · APU Start/Ignition SystemSDR HALA20241226380Bolt · brokenETOPS - ECAM AIR ENG 2 BLEED FAULT ON REVERSE THRUST SELECTION ON LANDING. FOUND FAN AIR VALVE ACTUATOR ROD BOLT BROKEN, REPLACED BOLT IN REFERENCE TO AMM 36-11-54-400-802-A, ACCOMPLISHED ENG RUN CHECK PER AMM 71-00-00-860-823-A, NO DEFECTS NOTED ON GROUND, ALDec 25, 2024 · N227HA · Airbus A321271N · Pneumatic Distribution SystemSDR HALA20241216367Regulator Valve · faultedETOPS - AIR ENG 2 ABNORM PR ON THRUST LVR ADVANCE ON TO W/ RTO SYSTEM RESET SUCCESSFUL. FOUND PRESSURE REGULATING VALVE (PRV) FAULTING. REMOVED AND REPLACED PRV PER AMM 36-11-52-000-802-A/400-802-A. OPS AND LEAK CHECK GOOD. OK FOR SVC.Dec 14, 2024 · N227HA · Airbus A321271N · Pneumatic Distribution SystemSDR HALA20241212362Bleed Valve · faultedDIV - AIR ENG 2 BLEED FAULT DURING CLIMB. ACCOMPLISHED GVI OF #2 ENG BLEED VALVES. FOUND FAV ACTUATRO ROD BROKEN. REMOVED FAV PER AMM 36-11-54. INSTALLED FAN AIR VALVE ON ENG 2 PER AMM 36-11-54. OPS/BITE/LEAK CHECK GOOD.Dec 11, 2024 · N227HA · Airbus A321271N · Compressor Bleed ValveSDR HALA20241028301Seal · damagedETOPS - DURING VISUAL INSPECTION OF THE THRUST REVERSERS FIRE SEAL AND VAPOR BARRIER SEALS T/C: 321-783200-W3-1, FOUND 2 FIRE SEALS DAMAGED. REMOVED AND REPLACED BOTH FIRE SEALS PER IPC: 78-32-05-75 ITEM NUMBER 240, 350. OK TO CONTINUE SERVICE.Oct 26, 2024 · N227HA · Airbus A321271N · Engine Thrust ReverserSDR HALA20240722195Clamp · leakingETOPS - DURING TAXI IN, APU BLEED SELECTED ON TO CONFIRM PACKS 10 MINS AFTER SELECTING ON, OBSERVED AN INTENSE BURING ASPHALT/CHEMICAL ODOR IDENTICAL TO PREVIOUS TEST FLIGHTS. REMOVED #2 RT OZONE FILTER IAW AMM 21-51-41 TO FOM FOUND CONTAMINATED. INSTALLED #2Jul 17, 2024 · N227HA · Airbus A321271N · Cabin Cooling SystemSDR HALA20240716193Duct · contaminatedATB - AFTER TAKEOFF PRIOR TO THRUST REDUCTION, BURNING ELECTRICAL AND CHEMICAL SMELL OBSERVED IN THE COCKPIT. TAKEOFF THRUST WAS TOGA. PERFORMED DECONTAINATION OF THE BLEED AIR DUCTS LEVEL C AMM 36-10-00-615-806-A. NO BURNING SMELL WHEN PACKS 1 AND 2 ON AND OFJul 15, 2024 · N227HA · Airbus A321271N · Pneumatic SystemSDR HALA20240510023Smoke Detector · inoperativeLAV E SMOKE DETECTOR INOP. REMOVED AND REPLACED SMOKE DETECTOR AT LAV E PER AMM 26-17-15-400-807-A.OPS CHECK GOOD OK FOR SERVICE.May 9, 2024 · N227HA · Airbus A321271N · Smoke DetectionSDR HALA20240311064Warning Light · illuminatedETOPS-ON ARRIVAL DESENDING THRU 12,000 ECAM GEN 2 FAULT. COMPLETE ECAM ACTIONS GEN 2 FAULT STILL ILLUMINATED. STARTED APU. REMOVED AND REPLACED RH IDG IAW AMM 24-21-51-400-803-A UP TO AND INCLUDING STAEP 4. A. (15) (H). 12570/25041, 03/08/24.. NEED TO CONTINUEMar 9, 2024 · N227HA · Airbus A321271N · AC Generator-AlternatorSDR HALA20240212040Line · puncturedETOPS - #1 ENGINE EDP SUCTION LINE FOUND TO HAVE PUNCTURE/LEAKING. REMOVED AND REPLACED #1 ENGINE EDP SUCTION LINE PER AMM 29-11-51-400. LEAK CHECKED, OPS CHECKED. NO DEFECTS NOTED. OK FOR SERVICE.Feb 11, 2024 · N227HA · Airbus A321271N · Hydraulic System, MainSDR HALA20240125029Sensor · faultedETOPS - ENG 1 N1 AND N2 VIB DISPLAY LOST FOR 30 MIN IN FLT, CAME BACK. (SEEMED TO CORRESPOND WITH ENG I OIL SENSOR FAULT ECAM, WHICH IS MEL'D) REMOVED PHMU PER AMM 77-31-01-000-801-AAND INSTALLED PER AMM 77-31-0-400-801-A. RAN EEC OPERATION TEST PER TASK 7 3-2Jan 24, 2024 · N227HA · Airbus A321271N · Engine Oil System (Airframe Furnished)SDR HALA20231109242Unknown · unknownETOPS - AFTER BOTH ENG STARTS (2&1) GOT ECAM: ENG 2 EIU FAULT. DID QRH RESET PROCEDURE ECAM CLRD. OPS NORM. ACCOMPLISHED BITE TEST OF EIU 1 & 2 PER AMM 73-25-34. NO FAULTS FOUND. OK TO CONTINUE SERVICE. REMOVED AND REPLACED (6KS) SWITCH PER AWM 73-25-34 AS PNov 9, 2023 · N227HA · Airbus A321271N · Fuel Controlling SystemSDR HALA20231016224Eiu · faultyETOPS - RECIEVED FAULT MESSAGE EIU2-008-ENGINE START FAULT. REMOVED AND REPLACED EIU-2 PER AMM 73-25-34 OPS AND SECURITY CHECK GOOD OK FOR SERVICEOct 15, 2023 · N227HA · Airbus A321271N · Fuel Controlling SystemSDR HALA20240712189Brake Assy · unknownAFTER TOUCHDOWN, LOSS OF BRAKES WITH AUTOBRAKES ON LOW. PERFORM TSM 32-42-00-810-919-A, NO FAULTS PRESENT. PERFORM AMM TASK 32-42-00-710-001-A, ALL RESULTS AS INDICATED IN REFERENCE. OK TO CONTINUE SERVICE.Jul 11, 2023 · N227HA · Airbus A321271N · Landing Gear Brake SystemSDR HALA2023020600002Not Reported · not reportedLAV SMOKE WARNING IN FLIGHT. PERFORMED LAVATORY SMOKE TEST IAW TSM 26-17-00-810-804-A. TEST PASSED, OPS CHECK GOOD. NO DEFECTS NOTED. A/C OK TO CONTINUE.Feb 5, 2023 · N227HA · Airbus A321271N · Fire Protection SystemSDR HALA2022030400067None · noneETOPS - APU WILL NOT START // REMOVED AND REPLACED EXCITER-IGNITION PER AMM 49-41-38 OPS TEST OK. OK FOR SERVICEMar 3, 2022 · N227HA · Airbus A321271N · APU Start/Ignition SystemSDR HALA2021080300093Fire Loop · faultedETOPS - ENG 2 FIRE LOOP B FAULT DISPLAYED NUMEROUS TIMES DURING CRUISE // PERFORMED TSM 26-12-00-810-806-A. MEASURE OHMS 1472 OHMS, VISUAL INSP TERMINAL BLOCK 2WD-D (450VT2). NO DEFECTS NOTED. REMOVED AND REPLACED FIRE LOOP B AT PYLON & REMOVED AND REPLACED FIAug 2, 2021 · N227HA · Airbus A321271N · Fire DetectionSDR HALA2021072900091Wire Harness · malfunctionedETOPS - ENG 2 FIRE LOOP B FAULT CAME ON FOR 30 SECONDS. T/S PER A321 TSM 26-12-00-810-806-A. PERFORMED OP TEST ENG FIRE & OVERHEAT DET & SAME ALL TEST OK. PERFORMED GVI OF ENG 2 FIRE DET SYS IAW ESPM CH 20 & ENG 2. NEED HARNESS FIN 4166KS (DL304822). REMOJul 29, 2021 · N227HA · Airbus A321271N · Fire Protection System WiringSDR HALA2020113000214Anti-Ice Valve · defectiveETOPS-ANTI-ICE ENGINE 2 VALVE CLOSED. ECAM AND OVERHEAD AMBER FAULT. FAULT DID NOT CLEAR. REMOVED AND REPLACED ENGINE 2 UPPER ANTI-ICE VALVE, PER AMM 30-21-51. OPERATIONS CHECK GOOD. SECURITY AND CONDITION CHECK OK. MESSAGE CLEARED, NO FAULTS NOTED. A/CNov 27, 2020 · N227HA · Airbus A321271N · Engine Anti-Icing SystemSDR HALA2020031100059Eec · malfunctionedETOPS SIGNIFICANT SYSTEM - BTB - ECAM: ENG 2 FADEC SYS FAULT FOLLOWED BY ENG 2 MINOR FAULT OIL CHIP DETECTED. // INSTALLED NEW PHMU ON #2 ENG, CONDITION SAME. RE-INSTALLED ORIGINAL PHMU PER AMM 77-31-01. REMOVED AND REPLACED #2 EEC PER AMM 73-21-01. LAND TEST Mar 10, 2020 · N227HA · Airbus A321271N · Fuel Control/Turbine EnginesSDR HALA2019122300527Unknown · odorAT 1250Z A GARBAGE TYPE ODOR STARTED IN THE CABIN AND INCREASED FOR THE NEXT TEN MINUTES. ONE PASSENGER FELT ILL, AT FIRST, THE SMELL WAS IN CABIN. IT LATER DISAPPEARED. NOTED BY MX. OK TO CONTINUE.Dec 23, 2019 · N227HA · Airbus A321271N · Air Distribution System
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