N217HA

Service difficulty reports · 68

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 = 'N217HA' 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 HALA20250929292Coupling · faultedETOPS - FUEL LEAKING FROM HOSE NOZZLE WHEN CONNECTED TO REFUEL/DEFUEL COUPLING. AIRCRAFT WONT TAKE FUEL. REMOVED AND REPLACED REFUEL/DEFUEL COUPLING ELEMENT ASSY PER AMM 28-25-41, OPS CHECK AND LEAK CHECK GOOD. A/C OK FOR SERVICE.Sep 26, 2025 · N217HA · Airbus A321271N · Fuel StorageSDR HALA20250904048Not Reported · not reportedTOW BAR SNAPPED ON PUSH. AWAITING FULL RESOLUTION.Sep 2, 2025 · N217HA · Airbus A321271N · Standard Practices/StructuresSDR HALA20250804239Fadec · faultedETOPS - ENG 2 FADEC SYS FAULT ON ECAM. REMOVED AND REPLACED ENG2 EEC PER AMM 73-21-01, OPS CHECK GOOD NO FAULT NOTED ON ECAM. A/C OK FOR SERVICEAug 1, 2025 · N217HA · Airbus A321271N · Fuel Controlling SystemSDR HALA20250514134Sensor · faultedETOPS - AIR PACK 2 REGUL FAULT IN CRUISE. AMBER XX C SENSOR ON BLEED PAGE. PERFORMED A320 FIM TASK 21-61-00-810-A. REMOVED AND REPLACED P2 COMP TEMP SENSOR PER A320 AMM 21-61-11. OPS CHK GOOD. OK FOR SVC.May 13, 2025 · N217HA · Airbus A321271N · Cabin Temperature Control SystemSDR HALA20250407101Switch · brokenETOPS - INFO TO MAINTENANCE: RADAR "SYS SWITCH DETENT IS BROKEN ALLOWING IT TO BE BUMPED TO THE ON POSITION, WHICH CAN CAUSE A HAZARD AT THE GATE. REMOVED AND REPLACED WXR CONTROL UNIT . BITE TEST PER 34-41-00. TEST OK, NO FAULTS NOTED. OK FOR SERVICE.Apr 4, 2025 · N217HA · Airbus A321271N · Weather Radar SystemSDR HALA20250303010Oil System · overservicedWEAK DIRTY SOCKS SMELL THROUGHOUT CABIN AND COCKPIT. STRONGER IN BACK OF PLANE. STARTED UNDER 5000'. TURNED ON APU BLEED AND SMELL DISAPATED. DURING ETOPS PDSC NOTICED #2 ENG OIL OVERSERVICED. REMOVED 2 QRTS. PERFORMED TSM 71-00-00-810-847-A. NO SMELLS NOTED.Feb 28, 2025 · N217HA · Airbus A321271N · Turbine Engine Oil SystemSDR HALA20250226072Pressure Sensor · faultedETOPS - FOUND OIL PRESSURE DIFFERENTIAL SENSOR BAD PER TASKCARD 321-730000-WI-1 W/O 335093 FIN- 4077KS. REMOVED AND REPLACED OIL PRESSURE DIFFERENTIAL SENSOR PER AMM 79-33-23. OPS AND SECURITY CHECK GOD. BITE AND LEAK CHECK GOOD.Feb 25, 2025 · N217HA · Airbus A321271N · Engine Oil PressureSDR HALA20250210005Tailpipe · fireUPON GATE ARRIVAL. REPORTED A SMALL ENGINE FIRE ON ENGINE 2 TAIL CONE- EXTINGUISHED ITSELF. PERFORMED VISUAL INSPECTION OF ENGINE AFTER FIRE NO FAULTS NOTED. PERFORMED IDLE RUN OF ENGINE2 PER AMM 71-00-00-710-806-A IDLE RUN GOOD A/C OK FOR SVC.Feb 6, 2025 · N217HA · Airbus A321271N · Engine (Turbine/Turboprop)SDR HALA20240830248Fcu · faultedETOPS - APU AUTO SHUT DOWN. FOLLOWED TSM 49-00-81-810-835-A AND REPLACED FCU AS PER AMM 49-32-11. OPERATION AND LEAK CHECK NORMAL. AIRCRAFT OK FOR SERVICEAug 30, 2024 · N217HA · Airbus A321271N · APU Engine Fuel and ControlSDR HALA20240830247Pressure Switch · faultedETOPS - APU STATUS MESSAGE (LOW OIL PRESSURE). FOLLOWED TSM 49-00-81-810-868-A AND REPLACED OIL PRESSURE SWITCH AS PER AMM 49-94-14. OPERATIONAL CHECK NORMAL. AIRCRAFT OK FOR SERVICE.Aug 30, 2024 · N217HA · Airbus A321271N · APU Oil SystemSDR HALA20240605155Switch · inoperativeETOPS - FOUND BLUE HYD OVRD PUSHBUTTON SWITCH INOP DURING TASK CARD. REMOVED AND REPLACED SWITCH PER ASM 29-12-01. OPS CHECK GOOD. OK FOR SERVICEJun 4, 2024 · N217HA · Airbus A321271N · Hydraulic System, MainSDR HALA20240308013Brake Assy · chatteringTAXI IN BELOW 6 KTS, FELT BRAKE CHATTER USING LEFT BRAKE PEDAL ONLY. CHECKED L/H MLG BRAKES PER AMM 32-42-00-710-001-A, 32-43-00-710-001-A, 32-44-00-710-002-A. OPS CHECK GOOD. RAISED GEAR & SPUN WHEELS. NO GRABBING. NO FAULTS ON PFR. OK FOR SERVICE.Mar 7, 2024 · N217HA · Airbus A321271N · Landing Gear Brake SystemSDR HALA20240226052Sensor · faultedETOPS - ECAM ENG2 OIL SENSOR FAULT. REMOVED AND REPLACED PHMU PER AMM 77-31-01. AND TROUBLESHOT PER TSM 79-35-00-810-806-A. OPS CHECK GOOD. NO FAULTS NOTED OK FOR SERVICE.Feb 25, 2024 · N217HA · Airbus A321271N · Engine Oil Indicating SystemSDR HALA20231124254Overheat Sensor · faultyETOPS - ENGINE 2 LOOP A FAULT ON ECAM FOUND DURING PDC WALKAROUND. PERFORMED TSM 26-12-00-710-002 FOUND LOOP 4002WD1 SHORTING. REMOVED & REPLACED ENG 2 LOOP A 4002WD1 IAW AMM 26-12-17 PB401. FDU TEST OKAY. NO FAULTS NOTED. A/C OK TO CONTINUE. MOC NOTIFIED.Nov 22, 2023 · N217HA · Airbus A321271N · Overheat DetectionSDR HALA20231019231Unknown · unknownATB - AIR TURN BACK DUE TO UNRELIABLE AIRSPEED - BUG IN PITOT TUBE. FOUND BUG IN F/O PITOT PROBE (9DA2) CLEANED AND FLUSHED PITOT PROBE PER AMM 34-10-00-170-004-A. OK FOR SERVICE.Oct 18, 2023 · N217HA · Airbus A321271N · Airspeed/Mach IndicatorSDR HALA20240712188Exciter · faultedETOPS - APU AUTO SHUTDOWN 2X ON TAXI IN TO GATE. REMOVED AND REPLACED APU EXCITER PER AMM 49-41-38. OPS AND SECURITY CHECK GOOD.Jul 11, 2023 · N217HA · Airbus A321271N · APU Start/Ignition SystemSDR HALA2023041300085Unknown · unknownATB - AFTER REACHING CRUISE ALT FL340 ENG 1 START VALVE FAULT ECAM. VERIFIED START VALVE POS CLOSED, MOVED FREELY (REF TSM 80-11-00-810-828-A) REMOVED AND REPLACED #1 STARTER PER AMM 80-AA-01. LEAK CHECK AND OPS CHECK GOOD.Apr 13, 2023 · N217HA · Airbus A321271N · Engine Start Valves/ControlsSDR HALA2023041300087Unknown · unknownETOPS - #1 ENGINE FAN BLADE NICK. BLEND #1 ENG #17 BLADE. ALSO INSPECT AND CLEAN WITHIN LIMITS. PRATT AND WITHNEY 72-11-03. OK FOR SVC.Apr 10, 2023 · N217HA · Airbus A321271N · Turbine Engine Air Inlet SectionSDR HALA2023041700088Unknown · unknownSUPPLEMENTAL SUBMISSION TO HALA2023040500079. UPDATED WITH RESOLUTION. DIV - SPOILER 1 FAULT - IN FLIGHT UNABLE TO RESET. DIV TO OAK. SPOILER ACTUATOR DEACTUATED. OK TO CONTINUE. UPDATED MIC SHEET AND INSTALLED PLACARD. REMOVED AND REPLACED SPOILER SERVO CONTApr 4, 2023 · N217HA · Airbus A321271N · Drag Control SystemSDR HALA2023040500079Unknown · unknownDIV - SPOILER 1 FAULT - IN FLIGHT UNABLE TO RESET. DIV TO OAK. DEFERED PER MEL 27-64-01A. SPOILER ACTUATOR DEACTUATED. OK TO CONTINUE. UPDATED MIC SHEET AND INSTALLED PLACARD.Apr 4, 2023 · N217HA · Airbus A321271N · Drag Control SystemSDR HALA2023033100072Unknown · unknownSUPPLEMENTAL SUBMISSION TO HALA2023032400060. RESOLUTION UPDATED. ETOPS - BLOCK TURN BACK, ENG 1 EGT OVERLIMIT. PER ENGINEERING. PERFORMED TSM 71-00-00-810-885-A STEPS 4.A(3) & (4). NO FAULTS NOTED. PERFORMED TSM 71-00-00-810-861-A STEP 4.A(15) & (21). REMOVEMar 24, 2023 · N217HA · Airbus A330243 · Engine Indicating SystemSDR HALA2023032400060Unknown · unknownETOPS - BLOCK TURN BACK, ENG 1 EGT OVERLIMIT. AWAITING RESOLUTIONMar 24, 2023 · N217HA · Airbus A321271N · Engine (Turbine/Turboprop)SDR HALA2023032100009Unknown · unknownREPORTED #1 ENGINE TAILPIPE FIRE. ACCOMPLISHED AMM 72-00-00-210-817-A. VISUAL INSPECTION OF ENG AFTER FIRE NO DEFECTA NOTED.Mar 21, 2023 · N217HA · Airbus A321271N · Engine Exhaust SystemSDR HALA2023032100053Unknown · unknownETOPS - #1 ENG CORE FIRE LOOP CLIP BROKEN (PN 636-5712-505) ON RAIL ASSY RH SIDE. REPLACED #1 ENG FIRE LOOP A RAIL ASSY PER AMM 26-12-61. OPS CHK OK. (PN 636-5712-505.Mar 21, 2023 · N217HA · Airbus A321271N · Smoke DetectionSDR HALA2023032100052Pump · faultyETOPS - ENGINE 1 START FAULT ENGINE 1 EGT OVERLIMIT HUNG START, EMGINE STALL. PERFORMED TSM 71-00-00-810-861-A, REMOVED AND REPLACED IFPC PER AMM 73-11-01-000-801-A AND 73-11-01-400-801-A. LEAK AND OPS TESTS GOOD, OK FOR SVC.Mar 21, 2023 · N217HA · Airbus A321271N · Fuel Control/Turbine EnginesSDR HALA2023022400005None · noneAT CRUZ FL350. ECAM MASTER WARN LAV SMOKE. FA'S REPORTED LAV E WEREINDICATION WAS GENERATED. PAX IN LAV SAID WAS NOT SMOKE/VAPING. LAV INSP NORMAL. INSPECTED LAV E SMOKE DETECTOR FOR CONDITION. SEAT INTACKED AND TAMPERING. PERFORMED SMOKE DETECTOR TEST IN REF/Feb 23, 2023 · N217HA · Airbus A321271N · Fire Protection SystemSDR HALA2023011700007Outflow Valve · faultedETOPS - VENT AVIONICS SYS FAULT. SKIN AIR OUTLET VALVE ON ECAM. REMOVED & REPLACED SKIN AIR OUTLET VALVE PER AMM 21-26-53-400-001-A01. OPS CHECK GOOD. OK FOR SVC. PN/SN OFF: VFT300B00 / 042607159, PN/SN ON: VFT300B00 / 2279Jan 15, 2023 · N217HA · Airbus A321271N · Pressure Regulator/Outflow ValveSDR HALA2022110800288Fire Loop · shortedPILOT REPORTS ENG 2 FIRE LOOP A FAULT. REMOVED AND REPLACED ENG 2 LOOP PER AMM 26-12-17. OPS CHECK GOOD OK TO CONTINUE SERVICE.Nov 7, 2022 · N217HA · Airbus A321271N · Fire DetectionSDR HALA2022110200282Fadec · faultedETOPS-DURING ENGINE START ECAM "ENG 2 FADEC SYS FAULT" RESET IN ACCORDANCE WITH HAL MX ENG 2 FADEC REMAINED. TWO ENGINE STARTS ATTEMPTED PER MOC DURING TAXI ENG 1 STALL FOLLOWED BY ENG 1 FAIL. ACTIONED ECAM AND TAXIED TO GATE. PER TSM 73-21-00-810-878-A REMOVNov 1, 2022 · N217HA · Airbus A321271N · Fuel Controlling SystemSDR HALA2022110100003Fire Loop · looseBTB ENG 2 FIRE LOOP FAULT A. OPEN COWL ENG 2. FOUND 2 OPEN LOOP CLAMPS, SECURED CLAMPS. DID BITE TEST PER AMM 26-12-00-710-002. NO FAULTS NOTED. OK TO CONTINUE.Oct 31, 2022 · N217HA · Airbus A321271N · Fire DetectionSDR HALA2022101900274Buffer Valve · usedSUPPLEMENTAL INFORMATION (THIS SUBMISSION IS FOR TYPO CORRECTION OF HALA2022101800274 - TYPO CORRECTION TO BLOCK 2.J FLIGHT NUMBER, 3.A AIRCRAFT SERIAL NUMBER, TOTAL TIME, AND TOTAL CYCLE, 5.E PARTS CONDITION) - PERFORMED TSM 71-00-00-810-854-APAR , 4.A(1)TO (Oct 12, 2022 · N217HA · Airbus A321271N · Compressor Bleed GovernorSDR HALA2022101400274Valve · faultedETOPS, CREW REPORTS #1 ENG STALL , RETURN TO BLOCK, MAINTENANCE COMPLETED BORESCOPE INSPECTION, NO DEFECT NOTED, ENGINE KEEPS STALLING DURING RUNS. PERFORMED TSM 71-00-00-810-854-APAR , 4.A (1) TO (3) STEP, PERFORMED BORESCOPE INSP OF HPC & LPC PER STEP 4.A (Oct 12, 2022 · N217HA · Airbus A321271N · Engine Bleed Air SystemSDR HALA2022081600145None · noneETOPS - FUEL LEAK FOUND AT ENG 1 FUEL DRAIN MAST. REMOVED AND REPLACED ENG #1 LOW PRESSURE COMPRESSOR BLEED VALVE PER AMM 75-32-01-00-00-801-A & AMM 75-32-01-400-801-A. PERFORMED ENGINE IDLE RUN PER AMM 71-00-720. NO LEAKS FOUND. A/C OK TO CONTINUEAug 17, 2022 · N217HA · Airbus A300* · Engine (Turbine/Turboprop)SDR HALA2022061300112None · noneETOPS - ECAM ENG 2 AIR SYS FAULT DESCENDING THROUGH 12,000' // REMOVED AND REPLACED #2 ENGINE BUFFER AIR VALVE PER AMM 75-26-04, PERFORMED TEST 3 IDLE RUN PER AMM 71-00-00, NO DEFECTS NOTED, SYSTEM CHECKED NORMAL. OK FOR SERVICE.Jun 10, 2022 · N217HA · Airbus A321271N · Compressor Bleed ValveSDR HALA2022021500044None · noneETOPS - IN FLIGHT ECAM "ENG 2 AIR SYS FAULT". WOULD APPEAR THEN CLEAR ITSELF SEVERAL TIME.// REMOVED AND REPLACED LPC BUFFER AIR VALVE. PER AM M75-26-00 PB 400 CONFIG 00. OPS AND LEAK CHECK GOOD. OK FOR SERVICE.Feb 14, 2022 · N217HA · Airbus A321271N · Engine Oil System (Airframe Furnished)SDR HALA2022020100035None · noneBTB - CAN NOT CONTROL FWD CABIN HEAT ACFT RETURNING TO THE GATE. COND TRIM AIR SYSTEM FAULT FWD CABIN TRIM VALVE ECAM // REMOVED AND REPLACED FWD CABIN TRIM VALVE (12HK) PER AMM 21-63-51. OPS CHECK GOOD, RAN BOTH ENGINES AT IDLE FOR FIVE MINUTES, NO FAULTS NOJan 31, 2022 · N217HA · Airbus A321271N · Air Conditioning SystemSDR HALA2021112400172None · noneETOPS - #1 ENG HYD PUMP LINE FOUND DAMAGED // REPLACED SUCTION LINE REF AMM 29-11-49. LEAK CHECK GOOD.Nov 22, 2021 · N217HA · Airbus A321271N · Hydraulic Power Accumulator, MainSDR HALA2021110100148Unknown · odorFAS REPORTED NOTICEABLE "DIRTY SOCK" SMELL IN FORWARD CABIN FROM 15 MINS OUT TO LANDING // PERFORMED TSM 05-50-00-810-831-A. ISOLATED BOTH PACKS WITH ENG 1, ENG 2, AND APU. UNABLE TO DUPLICATE ODOR IN CABIN. NO DEFECTS NOTED. OK FOR SVC.Oct 28, 2021 · N217HA · Airbus A321271N · Air Distribution SystemSDR HALA2021101800140None · noneEMER EQ - EXIT SIGN @ DOOR 3 CENTER DOES NOT ILLUMINATE. // RELAMPED EXIT SIGN AT DOOR 3 CENTER. OPS CHECK GOOD. OK FOR SERVICE.Oct 17, 2021 · N217HA · Airbus A321271N · Passenger Compartment LightingSDR HALA2021101500138None · noneETOPS - APU AUTO SHUTDOWN // REMOVED AND REPLACED EXCITER-IGNITION PER AMM 49-41-38 OPS CHECK GOOD. NO FAULTS NOTED.Oct 14, 2021 · N217HA · Airbus A321271N · APU Start/Ignition SystemSDR HALA2021092000119Fuel Filter · degradedETOPS - INFO TO MX:ON CLIMB OUT MOMENTARY ECAM ENG 2 FUEL FILTER DEGRADE APPEAR FOR A FEW SECONDS THEN CLEARED ITSELF // PERFORM T/S PER TSM 73-11-00-810-826-A. REPLACED FUEL FILTER PER AMM REF 73-11-06-400-801-A. PERFORM GRD ENG RUN #2 ENG., OPS CHECK GOOD. NSep 18, 2021 · N217HA · Airbus A321271N · Engine Fuel DistributionSDR HALA2021041300047Life Raft · expiredEMER EQ - LIFE RAFT IN AFT CEILING CONTAINER EXPIRED PER HALENGINEERING AND HAL901. NEDDS REPLACEMENT // REPLACED LIFE RAFT IN AFT CEILING CONTAINER WITH SERVICEABLE PART PER AMM 25-66-41. SECURITY CHECK OK. HAL 901 INSTALLED PER GMM VOL.2. OK FOR SERVICE.Apr 11, 2021 · N217HA · Airbus A321271N · Life RaftSDR HALA2020080500168Pitot Head · damagedDURING PITOT STATIC TEST, FOUND PITOT PROBE 1 (9DA1) BURNED. REMOVED AND REPLACED PITOT PROBE 1 (9DA1) PER AMM 34-11-15. OPS TESTED GOOD.Aug 4, 2020 · N217HA · Airbus A321271N · Pitot/Static SystemSDR HALA2020060600122Flap · puncturedOPEN - ON MX WALK AROUND PUNCTURE DAMAGE ON LT IB FLAP 32" FROM OUTB EDGE AND 0.5" FWD OF TE. LT INBOARD FLAP TAB HAS BEEN REPAIRED PER E105-C30022-TER, OK TO CLOSE OK FOR SERVICE.Jun 5, 2020 · N217HA · Airbus A321271N · Trailing Edge FlapsSDR HALA2020011700016Engine · vibrationATB, NR 2 ENGINE. HIGH VIBRATION. IFSD. REMOVED AND REPLACED THE NR 2 ENGINE.Jan 17, 2020 · N217HA · Airbus A321271N · Engine (Turbine/Turboprop)SDR HALA2019122600528Warning Message · false activationDURING DESENT THROUGH 12500, THE NR 1 ENGINE FIRE LOOP, A FAULT APPEARED ON ECAM WITH NO ASSOCITED CAUTION ALERT MASSAGE LASTED APPROX 2 MIN ON ECAM//T/S REF TSM 26-12-00-810-825-A, PERFORMED VI IAW AMM 26-12-00-200-802, VERFIED ALL CONNECTIONS TIGHT AND SECUDec 24, 2019 · N217HA · Airbus A321271N · Fire DetectionSDR HALA2019122300526Warning Message · false activationNR 1 ENGINE FIRE LOOP -A- FAULTED ECAM DURING APPROACH. TROUBLESHOT IAW TAM 26-12-00-810-851-A, POST SB 26-1112. DETECTOR CONFIRMED AND NO FAULTS NOTED ON OPERATIONAL TEST, VISUAL INSPECTION OF DETECTORS AND HARNESS FOUND NO DEFECTS NOTED, RESTIANCE CHEDec 21, 2019 · N217HA · Airbus A321271N · Fire DetectionSDR HALA2019121700520Fire Detector · malfunctionedETOPS SIGNIFICANT SYSTEM - ENG 1 FIRE LOOP A FAULT ON DESCENT INTO HNL. // REMOVED ENG 1 FDU 1 FOR TROUBLESHOOTING. REINSTALLED SAME. OPS CHK PENDING. CB'S Q38, Q39, A06, A07 PULLED + COLLARED. OPS CHK PENDING. FOUND HARDWARE NOT SECURED ON FIRE DETECTOR LOOP Dec 16, 2019 · N217HA · Airbus A321271N · Fire DetectionSDR HALA2019121700519Fire Loop · faultedETOPS SIGNIFICANT SYSTEM - ENG 1 FIRE LOOP A FAULT, REPEAT WRITE-UP // T/S PER TSM 26-12-00-810-803-A. REMOVED AND REPLACED #1 ENGINE LOOP A AFT DETECTOR PER AMM 26-12-17-000-803-A. OPS CHECK GOOD. NO DEFECTS NOTED.Dec 15, 2019 · N217HA · Airbus A321271N · Fire DetectionSDR HALA2019121700518Connector · looseETOPS SIGNIFICANT SYSTEM - ENG 1 FIRE LOOP A FAULT, REPEAT WRITE-UP // INSPECTED ENG 1 FIRE LOOP, FOUND LOOSE CONNECTOR @ ENG 1 FIRE LOOP. RE-TORQUED CONNECTOR AS REQUIRED. PERFORMED FDU BITE CHECKED, PER AMM 26-12-00. TEST PASSED NO FAULTS NOTED. OK TO CONTINDec 15, 2019 · N217HA · Airbus A321271N · Fire Protection System Wiring
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