N215HA

Service difficulty reports · 38

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 = 'N215HA' 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 HALA20250819254Igniter · faultedETOPS - ENG 1 A ING ECAM ON ENGINE START UP. REMOVED AND REPLACED LOWER IGNITER PLUG. PER AMM 74-21-01. OPS TEST BAD. FURTHER T/S REQUIRED. REMOVED AND REPLACED EXCITER PER AMM 74-11-01. OPS CHECK NORMAL. OK FOR SERVICE.Aug 18, 2025 · N215HA · Airbus A321271N · Spark Plug/IgniterSDR HALA20250804238Wire Harness · faultedETOPS - ENG 1 MINOR FAULT AFTER START. FOUND WC08 HARNESS WIRE SHOWING. REMOVED AND REPLACED PER AMM 73-21-68. PERFROMED IDLE ENGINE RUN. OPS GOOD.Aug 4, 2025 · N215HA · Airbus A321271N · Engine Fuel System WiringSDR HALA20250122028Wire Harness · chafedETOPS - INFO TO MX: ENG 1 FIRE LOOP A FAULT ECAM APPEARED AND DISAPPEARED MULTIPLE TIMES DURING FLIGHT. WHILE CHECKING INSULATION RESISTANCE AT FDU 1 LOOP A CONNECTOR PIN J-GRD & SHAKING LOOP A HARNESS 4165KS GOT A FLUCTUATION IN RESISTANCE FROM <100MOHMS TO 4Jan 21, 2025 · N215HA · Airbus A321271N · Fire Protection System WiringSDR HALA20241226378Elec Connector · damagedETOPS - BTB- HYD G ENG 1 PUMP LO PR. REPLACED CONTACTS IN CONNECTOR 1074GK-A PER ESPM 20-44-13. REMOVED AND REPLACED ENG HYD PUMP SWITCH PER TSM 29-11-00-810-804-A AND AMM 29-11-17. LEAK CHECK GOOD. OPS CHECK GOOD. RAND ENG 1 3 TIMES WITH CREW. CYCLED #1 ENG HDec 25, 2024 · N215HA · Airbus A321271N · Hydraulic Power System WiringSDR HALA20241226379Pump · low pressureATB - HYD G ENG 1 PUMP LO PR. REMOVED AND REPLACED #1 ENG GREEN EDP PER AMM 29-11-51. OPS & LEAK CHECK OK. HYD INDICATION OK & NO FAULT NOTED. PERFORMED TSM 29-11-00-810-804-A UP TO STEP 4.A. PRESSURE CHECK OK, MORE THAN 1812 PSI. NEED TO CONTINUE WIRING CHECDec 24, 2024 · N215HA · Airbus A321271N · Hydraulic Pump (Electric/Engine), MainSDR HALA20241223376Oil System · leakingIFSD / DIV - DURING CLIMB, ADV APPEARED W/FLASHING ZERO OIL QUANTITY. EVENTUALLY LOW OIL PRESSURE AND ECAM DROVE US TO SHUT DOWN ENG #1. AIR DIVERSION TO HNL. REMOVED #1 GREEN HYD EDP PER AMM 29-11-51. FOUND TORN SPLINE SEAL. NEED TO REPLACE SPLINE SEAL AND FLDec 22, 2024 · N215HA · Airbus A321271N · Turbine Engine Oil SystemSDR HALA20241112070Unknown · odorATB-FUME EVENT CABIN CREW NOTIFIED US SHORTLY AFTER TO OF "BURNING POPCORN" SMELL NEAR 3R DOOR. SMELL MOVED FWD TO ROWS 11-27. CONSTANT, NOT DISSAPATING FOR CLIMB, CRUISE, OR DESCENT. APU BLEED USED @ 10K TO LANDING. SMELL DISSAPATED. PERFORMED DUAL ENG WASH PNov 10, 2024 · N215HA · Airbus A321271N · Air Distribution SystemSDR HALA20240925168Fire Loop · faultedETOPS - ENG1 FIRELOOP B FAULT. ENG 1 REPLACED AGB LOOP B 4002WD2 PER AMM 26-12-17 OPS CHECK OKSep 24, 2024 · N215HA · Airbus A321271N · Fire DetectionSDR HALA20240815226Filter · unknownETOPS - APU AUTO SHUTDOWN AT GATE. REMOVED AND REPLACED APU OIL FILTER AND GEN SCAVENGE FILTER PER AMM 49-91-41-200.OPS/LEAK CHECK GOOD. OK FOR SERVICE.Aug 14, 2024 · N215HA · Airbus A321271N · APU Oil SystemSDR HALA20240705180Master Switch · faultedDMI 209186 - APU MASTER S/W INTERMIT HAVE TO TAP ( MASTER SWITCH ON LIGHT ). REPLACED APU MASTER SWITCH 14KD PER ESPM 20-45-11 OPS CHECK APU PER AMM 49-00-00 OKJul 3, 2024 · N215HA · Airbus A321271N · Airborne Auxiliary Power Unit (APU) SystemSDR HALA20240701174Wire · detachedETOPS - DURING PDSC FOUND GREEN EDP ENG 1 INDICATING ON WHEN OFF. FOUND BLUE WIRE AT CONNECTOR 1074GK-A SHEARED, RE-PINNED PER ESPM 20-48-24. ALSO FOUND INTERNAL LEAKAGE OF PRESSURE SWITCH. REMOVED AND REPLACED PRESSURE SWITCH REF AMM 29-11-17. OPS AND LEAK CHJun 28, 2024 · N215HA · Airbus A321271N · Hydraulic Power System WiringSDR HALA20240313065Probe · faultedETOPS - 1600LBS OF FUEL DISSAPEARED FROM FOB BEFORE PUSHBACK. REMOVED AND REPLACED RH WING FUEL PROBES 27QT2 AND 28QT2 PER AMM 28-42-15. PENDING 640BB FUEL PANEL INSTALL AND OPS CHECK. INSTALLED FUEL PANEL OPS, LEAK, AND BITE CHECKS GOOD PER AMM 28-42-15Mar 12, 2024 · N215HA · Airbus A321271N · Fuel Quantity SensorSDR HALA20240306062Packing · leakingETOPS - DURING DESCENT HYD G RSVR LO LVL L/G GRAVITY EXTENSION COMPLETED. FOUND PRESSURE SWITCH PACKING LEAKING. REMOVED AND REPLACED PRESSURE SWITCH PACKING PER AMM 29-11-17. LEAK CHECK GOOD. OK FOR SERVICE.Mar 3, 2024 · N215HA · Airbus A321271N · Hydraulic System, MainSDR HALA20240229055Tube · leakingATB - #1 ENG OIL QTY DROPPED TO ZERO. UPON INSEPCTION NOTICED THE OIL PRESSURE TUBE FROM ENGINE AIR/OIL HEAT EXCHANGER WITH EVIDENCE OF OIL SEEPAGE. REFER PIPC 79-21-49-08 SHEET 2 OF 5 ITEM #20. ALL BOLTS FOR OIL PRESSURE TUBE SECURE AND TORQUED IAW AMM 79-21-Feb 28, 2024 · N215HA · Airbus A321271N · Engine Oil Distribution (Airframe Furnished)SDR HALA20240108006Unknown · unknownDURING THRUST LEVER ADVANCEMENT, ENG 1 STALL MESSAGE APPEARED. MESSAGE CLEARED ITSELF WITHIN 2 SECONDS WHILE BRINGING THRUST LEVERS TO IDLE. PER INDICATED ENG 1 STALL MESSAGE. PILOT NOTED ALL ENGINE INDICATIONS NORMAL. POWER LEVER NOT AT TAKEOFF POWER @ EVENTJan 5, 2024 · N215HA · Airbus A321271N · Engine (Turbine/Turboprop)SDR HALA2023083100186Unknown · unknownETOPS - ENG 1 FIRE LOOP A FAULT ECAM CAME ON DURING DEPARTURE. REMOVED AND REPLACED # 1 ENG FIRE DETECTOR ELEMENT IAW AMM 26-12-17-000-802-A. OPS CHECK NORMAL IAW 26-11-00.Aug 26, 2023 · N215HA · Airbus A321271N · Fire DetectionSDR HALA2023061600126Unknown · unknownETOPS - ON A/C WAKE-UP, ENG 1 FIRE LOOP B FAULT. REMOVED AND REPLACED AGB FIRE LOOP B PER AMM 26-12-17. OPS TEST GOOD. SECURITY CHECK GOOD. OK FOR SERVICE.Jun 15, 2023 · N215HA · Airbus A321271N · Fire DetectionSDR HALA2022121600310Fire Loop · faultedETOPS, NR 2 ENGINE FIRE LOOP B ILLUMINATED IN CRUISE. PERFORMED TSM 26-12-00-810-861-A FOR ENG 2 LOOP B AGB LOSS. R & R ENG 2 FIRE LOOP B AND BITE TESTED OKAY IAW AMM 26-12-17 PB401. A/C OK FOR SERVICE.Dec 15, 2022 · N215HA · Airbus A321271N · Fire DetectionSDR HALA2022110400283Fire Loop · faultedETOPS - ECAM ENG 1 FIRE LOOP A FAULT. PERFORMED TSM 26-12 -00-810-857-A. 'LOSS OF DETECTION BY ENG 2 LOOP A CORE.' FOUND LOOP A CORE FIRE DETECTOR RESISTANCE VALUES OUT OF SPECIFIED LIMITS. REMOVED AND REPLACED ENG 2 LOOP A CORE LOOP PER AMM 26-12-17. OPS CHECNov 3, 2022 · N215HA · Airbus A321271N · Fire DetectionSDR HALA2022091200259None · noneETOPS-DURING LANDING PILOT NOTED LOSING OIL QUAINTY ON # 2 ENG. FOUND # 2 ENG STARTER DUCT TWISTED, REMOVED ANF REPLACED ENG STARTER PER AMM 80-11-03. FOUND CHIPS AND METALS ON STARTER CHIP DETECTOR REMOVED AND REPLACED PER AMM 80-11-01 AND REMOVED AND REPLACESep 10, 2022 · N215HA · Airbus A300* · Engine Oil System (Airframe Furnished)SDR HALA2022081100141None · noneBTB - L BLEED AIR FAULT - ABNORMAL PRESSURE // REMOVED AND INSTALLED HP BLEED VALVE IAW AMM 36-11-51. REMOVED AND INSTALLED OVERPRESSURE VALVE IAW AMM 36-11-53. OPS CHECK GOOG, BITE TEST OAK. PERFORMED IDLE ON BOTH ENGINES NO FAULTS NOTED OK FOR SERVICEAug 10, 2022 · N215HA · Airbus A321271N · Pneumatic SystemSDR HALA2022031000073None · noneETOPS - FO CONSTRAINT BUTTON CRACKED // REMOVED AND REPLACED FLIGHT CONTROL UNIT PER AMM 22-81-12. AFS TEST GOOD. LAND CAT 3 TEST GOOD. OK FOR SVC.Mar 9, 2022 · N215HA · Airbus A321271N · Auto Flight SystemSDR HALA2021102500143None · noneETOPS - 2 APU AUTO SHUTDOWNS // REMOVED AND REPLACED APU IGNITION UNIT PER AMM 49-41-38.PERFORMED APU GRD. SCAN NO FAULTS AND TEST PER AMM 49-00-00.STARTED APU NORMALLY OPS CK. GOOD.SECURED APU ACCESS DOORS PER AMM 49-00-00 P/N OFF:3888058-7 S/N OFF 180016 P/Oct 21, 2021 · N215HA · Airbus A321271N · Airborne Auxiliary Power Unit (APU) SystemSDR HALA2021031800036B-Nut · looseETOPS - ECAM:AIR ENG 1 BLEED FAULT DURING LANDING ROLLOUT. // FAULT CODE 361151, PERFORMED TSM 36-11-00-810-975-A. INSPECTED SENSE LINES, FOUND LOOSE B-NUT, TORQUED. PERFORMED LEAK CHECK PER AMM 36-22-00-790-802, AND TEST NO. 1- PNEUMATIC LEAK TEST PER AMM 71-Mar 17, 2021 · N215HA · Airbus A321271N · Pneumatic Distribution SystemSDR HALA2020060500121Valve · malfunctionedETOPS SIGNIFICANT SYSTEM. ENG 1 TURB COOL FAULT. PERFORMED DRY MOTOR OF ENG NR 1 PER AMM 73-21-00-710-809-A. PER MOC NEED TO CHANGE ACC VALVE. REMOVED AND REPLACED NR 1 ENG ACC VALVE PER AMM 75-24-01-400-801-A. PENDING OPS CHECK. OPS AND LEAK CHECK GOOD Jun 4, 2020 · N215HA · Airbus A321271N · Engine Cooling SystemSDR HALA2020020500029Display · abnormalETOPS SIGNIFICANT SYSTEM - WX RADAR DISPLAY ERROR, 60 DEGREE LEFT, OA MONITOR. // PERFORMED BITE TEST OF WEATHER RADAR SYSTEM PER AMM 34-41-00-740-002-A. NO FAULTS DISPLAY TEST PATTERN OPERATING NORMALLY, OK FOR SERVICE.Feb 5, 2020 · N215HA · Airbus A321271N · Weather Radar SystemSDR HALA2019091700377Engine · leakingECAM ENG. 1 CHIP DETECTED AFTER LANDING, STRANGE ODOR. DURING BOROSCOPE FOUND OIL LEAKING AT HPC STAGE 2. // ACCOMPLISHED #1 ENGINE CHANGE PER J321-72-HWI 02. OPS AND LEAK CHECK GOOD. VERIFICATION FLIGHT FOR #1 ENGINE CHANGES COMPLETED SATISFACTORY.Sep 15, 2019 · N215HA · Airbus A321271N · Turbine Engine Compressor SectionSDR HALA2019081900345Unknown · odorF/A REPORT CHEMICAL SMELL IN ALL LAVATORIES // INSPECTED ALL LAVS NO CHEMICAL SMELL NOTED. OK TO CONTINUE.Aug 17, 2019 · N215HA · Airbus A321271N · Air Distribution SystemSDR HALA2019071500353Fire Loop · faultedETOPS SIGNIFICANT SYSTEM - ENGINE #1 FIRE LOOP B FAULT. FOUND #1 ENG PYLON FIRE DETECTOR LOOP B INSULATION CHECK FAILED. REPLACED LOOP B PYLON FIRE DETECTOR PER AMM 26-12-16-400-803. REINSTALLED PYLON FIRE-DETECTOR RAMP ASSY PER AMM 26-12-16-400-802. OPS CHK Jul 11, 2019 · N215HA · Airbus A321271N · Fire DetectionSDR HALA2019070200344Warning System · false activationENG1 FIRE LOOP A FAULT ECAM CAME ON TWICE ON CLIMB OUT THEN DISAPPEARED. PERFORMED OPS TEST OF THE ENGINE FIRE AND OVERHEAT DETECTION WITH MCDU CFDS PER MM 26-12-00-710-002-A. OPS TEST OK. NO DEFECTS NOTED. OK TO CONTINUE.Jul 1, 2019 · N215HA · Airbus A321271N · Fire DetectionSDR HALA2019070200343Fire Warning · false activationENG 1 FIRE LOOP A FAULT CAME ON MOMENTARILY TWICE AT CRUISE. FDU1 RESET. NO FAULTS, TEST PASSED.Jun 30, 2019 · N215HA · Airbus A321271N · Fire DetectionSDR HALA2019050900241Relay · faultyETOPS SIGNIFICANT SYSTEM - DURING EMER GEN TEST ECAM MESSAGE ELEC AC ESS BUS FAULT ON ECAM. FOLLOWED TSM 24-50-00-810-804-A. RELAY 12XE REPLACED AS REQUIRED. OPS CHECKS GOOD. OK FOR SVC.May 9, 2019 · N215HA · Airbus A321271N · AC Power Distribution SystemSDR HALA2018120430625Warning Message · false activationSMOKE LAV RED ECAM IN CRUISE FL 330 (2-3 SEC) WENT OUT BY ITSELF. F/A DID CABIN WALK THROUGH. NO SIGNS OF SMOKE.// CHECK ALL LAV TRASH EXT BOTTLE WITHIN LIMIT. OPS CHK ALL TOILETS OK. PERFORMED LAV SMOKE TEST PER AMM 26-17-00-710-001-A. NO FAULTS. NO SMELL NOTDec 1, 2018 · N215HA · Airbus A321271N · Smoke DetectionSDR HALA2018112000600Oil System · pressure lossOPEN - ETOPS SIGNIFICANT SYSTEM - AIRCRAFT DIVERTED TO NEAREST AIRPORT, DUE TO #2 ENG OIL PRESS LOSS IN FLIGHT. ENGINE WAS SHUTDOWN IN FLIGHT. // REMOVED AND REPLACED #2 ENGINE. OPS AND LEAK CHECK OK. OK FOR SERVICE. VERIFICATION FLIGHT COMPLETED SATISFACTORY.Nov 19, 2018 · N215HA · Airbus A321271N · Engine Oil Indicating SystemSDR HALA2018101800523Fire Loop · defectiveETOPS SIGNIFICANT SYSTEM. ENG 1 LOOP A FAULT ON PDC. PERFORMED TSM 26-12-00-810-851-A. DURING FDU1 TEST, CHECK ENG 1 FIRE LOOP A CORE. RESISTANCE OF 4001WD1 DET-FIRE CORE VENT LOOP A, OUT OF LIMITS. REPLACED LOOP DETECTOR PER AMM 26-12-17. OPS CHECK BITE CHECKOct 17, 2018 · N215HA · Airbus A321271N · Fire DetectionSDR HALA2018092500435Mmr · malfunctionedETOPS SIGNIFICANT SYSTEM, HF DATA LINK INTERMITTENT. RESET MMR AND ATSU C/B AS REQUIRED. OPS CHECK GOOD.Sep 24, 2018 · N215HA · Airbus A321271N · HF Communications SystemSDR HALA2018092500433Monitor · faultyETOPS SIGNIFICANT SYSTEM, ENG 1 OIL CHIP DETECTED. TROUBLESHOOT PER TSM 79-35-00-810-808-A PER STEP 8(A) REPLACED OIL DEBRIS MONITOR IAW AMM 79-35-21. RAN NR 1 ENGINE AND PERFORMED TEST NO 3 PER AMM 71-00-00-720-811-A AND TEST NO 6 PER AMM 73-21-00-710-807-A Sep 24, 2018 · N215HA · Airbus A321271N · Engine Oil Indicating SystemSDR HALA2018092500431Warning System · false activationETOPS SIGNIFICANT SYSTEM - ENG 1 OIL CHIP DETECTED ECAM ON TAXI. INSPECTED NR 1 ENG OIL CHIP DETECTORS PER AMM 79-00-00-281-802A. NO CHIPS NOTED. INSPECTED NR 1 ENG OIL FILTER ELEMENT PER AMM 79-00-00-210-809A. NO CONTAMINATION NOTED. RAN ENGINE NO LEAK NOTED.Sep 24, 2018 · N215HA · Airbus A321271N · Engine Oil Indicating System
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