N216HA

Service difficulty reports · 44

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 = 'N216HA' 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 ASAA2026092166991Outflow Valve · malfunctionedATB, AIRCRAFT UNABLE TO PRESSURIZE. ACCOMPLISHED BY VENT AVNCS SYS FAULT ECAM. ECAM ACTIONS COMPLETE HOWEVER STILL UNABLE TO PRESSURIZE. GROUNDED - YES. VERIFIED SKIN AIR OUTLET VALVE WAS SLIGHTLY OPEN. REAPPLIED MEL 21-26-04. VERIFIED MAIN FLAP CLOSED AND INTSep 21, 2026 · N216HA · Airbus A321271N · Pressure Regulator/Outflow ValveSDR ASAA2026082366480None · noneLAV SMOKE ECAM, RAN ECAM ACTION. GROUNDED - YES. FLT CREW REPORTED PASSENGER CAUGHT SMOKING. NO FAULTS NOTED. INDICATIONS NORMAL. AMM 26-17-00.Aug 23, 2026 · N216HA · Airbus A321271NX · Standard Practices/StructuresSDR ASAA2025112061797Battery · faultedWHILE PER TASK CARD I321-7DAY-CHECK. FOUND 11WL & 13WL EPSU BATTERY FAULT. GROUNDED - YES. REMOVED AND REPLACED 11WL AND 13WL EPSU BATTERY IAW AMM 33-51-38. OPS GOOD. OK FOR SERVICE.Nov 20, 2025 · N216HA · Airbus A321271N · Emergency LightingSDR HALA20251017321Pump · failedETOPS - Y ENG 2 PUMP INOP. REMOVED AND REPLACED NR 2 ENG. DRIVEN HYD. PUMP CONDITION SAME. ACCOMP. TEST OF PTU W/ENG. PUMPS PER AMM 29-23-00-710-004-A. ALL ENG.DRIVEN HYD PUMPS,ELECT HYD. PUMPS & PTU OPS NORMAL OK FOR SERVICE. SECURED NR 2 ENG.COWLINGS. P/N OFOct 16, 2025 · N216HA · Airbus A321271N · Hydraulic Pump (Electric/Engine), MainSDR HALA20251008308Fire Loop · faultedETOPS - IN FLIGHT, ENG 1 FIRE LOOP B FAULT. REMOVED AND REPLACED #1 ENG PYLON FIRE DETECTOR RAMP ASSY PER AMM 26-12-16. OPS CHECK GOOD. OK FOR SERVICE.Oct 7, 2025 · N216HA · Airbus A321271N · Fire DetectionSDR HALA20251001295Sensor · faultedETOPS - ENG2 OIL SENSOR FAULT MESSAGE FLASHED SPORADICALLY DURING CRUISE. REPLACED PHMU PER AMM 77-31-01 ON RH ENGINE. PERFORMED IDLE AND OPS CHECK. OPS CHECK GOOD. OK TO CONTINUE.Sep 30, 2025 · N216HA · Airbus A321271N · Engine Oil PressureSDR HALA20250618185Line · damagedETOPS - DURING ENGINE HARNESS REPLACEMENT FOUND HPC BLEED VALVE SOLENOID LINE DAMAGED. REMOVED 7 REPLACED HPC BVS LINE PER AMM 75-32-02-400-801A. LEAK CK GOOD. OK FOR SVC.Jun 17, 2025 · N216HA · Airbus A321271N · Compressor Bleed ValveSDR HALA20250618186Wire · damagedETOPS - DURING FOM FOUND WIRE DAMAGE ON #2 ENG N2 SENSOR O/B 4065KS-J64. FOUND WIRE BUNDLE DAMAGE ON #2 ENG BY TACC (FLAGGED) 4055KS-J31. REMOVED & REPLACED WIRE HARNESS W03 ON ENG #2 PER AMM 73-21-63. EEC OPS CK GOOD. OK FOR SVCJun 16, 2025 · N216HA · Airbus A321271N · Engine Fuel System WiringSDR HALA20250617033Starter · leakingEMERGENCY DECLARED. LOW OIL ENG #1 0.0 DECREASING FROM 18.0. AT SHUTDOWN ENG 1 QT 3.5. PILOT NOTED DURING EVENT OIL PSI 152 AND NO INFLIGHT SHUT DOWN PERFORMED. FOUND ENG STARTER LEAKING. REMOVED AND REPLACED PER AMM 80-11-01. LEAK AND OPS CHECK GOOD. ENGINE OJun 15, 2025 · N216HA · Airbus A321271N · Engine StarterSDR HALA20250610174Valve · faultedATB - AIR ENG BLEED 2 FAULT ECAM DURING CLIMBOUT @ MCT POWER PER WONT CLIMB PROC. UNABLE TTO RESET W/ ECAM OVERHEAT NOTED. T/S REMOVED & REPLACED #2 ENGINE FAN AIR VALVE IAW AMM 36-11-54-400-803-A.Jun 9, 2025 · N216HA · Airbus A321271N · Engine Bleed Air SystemSDR HALA20250423114Display · intermittentETOPS-CAPTAIN'S MCDU 3L BUTTON WORKS ONLY INTERMITTENTLY. REMOVED AND REPLACED CAPT'S MCDU PER AMM 22-82-12. OPS CHECK GOOD, OK TO CONT. SERVICE.Apr 22, 2025 · N216HA · Airbus A321271N · Central DisplaySDR HALA20241126337Fuel Filter · cloggedETOPS - INFO TO MX ON DEPARTURE CLIMB ENG 2 AMBER CLOG ANNUNCIATOR ILLUMINATED ON ENG SD PAGE. MESSAGE CLEARED AFTER A FEW MINS. PERFORMED TSM 73-11-00-810-822-A. REMOVED AND REPLAACED FUEL FILTER. FADEC SYSTEM IDLE TEST OK. NO LEAKS NOTED. OK FOR SVC.Nov 25, 2024 · N216HA · Airbus A321271N · Engine Fuel DistributionSDR HALA20241104065Smoke Detector · no discrepancyLAV SMOKE ECAM IN FLIGHT. ECAM CLEARED ITSELF AFTER 3 SECONDS, FA'S INVESTIGATED AND FOUND NO SOURCE OF FIRE. SUSPECT PAX VAPING. PERFORMED TSM 36-17-00-810-804-A NO DETECTORS FAULTING. NO FAULTS ON POST FLIGHT REPORT CLEANED DUST FROM ALL 4 LAVS. OK FOR SERVINov 1, 2024 · N216HA · Airbus A321271N · Smoke DetectionSDR HALA20241023296Connector · inoperativeETOPS - BTB. HYD G ENG 1 PUMP LO PR INDICATION 8X ON TAXI OUT. HYD PAGE PUMP LOW PRESSURE PTU OPERATING SHOWING AMBER AND GREEN INDICATIONS ENG 1 PUMP FAULT LIGHT ON OFF THROUGH INDICATIONS. REMOVED AND REPLACED PRESSURE SWITCH PART #450-1-3100-00 AND ELECTRICOct 22, 2024 · N216HA · Airbus A321271N · Hydraulic Power System WiringSDR HALA20241015049Latch · fod4R DOOR DISARMED DURING FLIGHT. WOULD NOT REARM. PERFORMED PRESSURIZATION CHECK WITH 4R DOOR ARMED. FOUND ARM/DISARM LEVER NOT FLUSH. FOUND SLIDE LOCK/LATCH BLOCKED WITH DEBRIS. RMEOVED DEBRIS. OPS CHECK OK. OK FOR SVC.Oct 13, 2024 · N216HA · Airbus A321271N · Escape SlideSDR HALA20240918259Pressure Switch · looseETOPS-ECAM HYD G ENG 1 PUMP LO PR TURNED OFF ENG 1 PUMP AS INSTRUCTED BY ECAM. PERFORMED TSM 29-11-00-810-804-A, FOUND PRESSURE SWITCH LOOSE. REMOVED AND REPLACED ENG 1 PUMP PRESSURE SWITCH (1047GK) PER AMM 29-11-17. OPS CHECK AND LEAK CHECK GOOD, NO FAULT NOTSep 17, 2024 · N216HA · Airbus A330243 · Hydraulic Pump (Electric/Engine), MainSDR HALA20240405086Seal · leakingETOPS - DURING WALK AROUND, FOUND OIL SEEPING FROM EN1 S/N: P770687 INLET CONE. UPON INSPECTION, FOUND OIL INSIDE INLET CONE. REMOVED & REPLACED FAN SHAFT COVER SEAL PER AMM 72-15-00-960-801-A. NO LEAKS NOTED POST IDLE RUN. OK FOR SERVICE.Apr 4, 2024 · N216HA · Airbus A321271N · Engine (Turbine/Turboprop)SDR HALA20240311063Selector · failedETOPS-FORWARD TRIM AIR VALVE NOT RESPONDING APPROPIATELY TO SWITCH POSITION. TEMP IN CABIN HOT WITH FULL COLD SET. PREVIOUSLY WRITTEN UP, NO CHANGE. REMOVED AND REPLACED TEMPERATURE SELECTOR PER AMM 21-63-11-000-001-A (21315 3/8/24. PENDING OPS CHECK. PERFORMEMar 9, 2024 · N216HA · Airbus A321271N · Cabin Temperature Control SystemSDR HALA20240311013Connector · dirtyAFT EXIT SIGN BURNT OUT AIRCRAFT LEFT SIDE. CLEANED AFT EXIT SIGN CONNECTORS. OPS CHECKED PER AMM 33-51-00 CHECK GOOD OK FOR SERVICE.Mar 8, 2024 · N216HA · Airbus A321271N · Light System WiringSDR HALA2026090300194Skin · corrodedDURING PERFORMING A 3 YEAR CHECK AT SIAEP, AN OF INSPECTION AS PER B321-ZL-500-02-1, CORROSION WAS FOUND ON THE LT WING BOTTOM SKIN PANEL 2 BETWEEN RIBS 24-25. AFTER DAMAGE ASSESSMENT AS PER SRM 57-21-11-283-014, CONTACT WITH AIRBUS IS REQUIRED SINCE THE BLENDFeb 13, 2024 · N216HA · Airbus A321271N · Wing, Plate/SkinSDR HALA2023072100155Pump · faultyETOPS - ENG #2 HYDRAULIC DRIPPING, 1 DRIP PER SECOND. REMOVED AND REPLACED ENG#2 HYD PUMP IAW AMM 29-13-51-000-806-A. ACCOMPLISHED ENG #2 IDLE RUN, NO LEAKS NOTED. AIRCRAFT OK FOR SERVICE.Jul 20, 2023 · N216HA · Airbus A321271N · Hydraulic Pump (Electric/Engine), MainSDR HALA2023051900111Unknown · unknownETOPS - INFO TO MTX: ON CLIMB OUT MOMENTARY ECAM OF: ENG 1 FIRE LOOP A FAULT. CLEARED ITSELF UP AS WE BEGAN ECAM ACTIONS. INSTALLED NEW #1 ENG FIRE ELEC HARNESS ASSY. PER AMM TASK 26-12-61, OPS TEST OK.May 18, 2023 · N216HA · Airbus A321271N · Fire Protection SystemSDR HALA2023051000024Unknown · unknownINFO TO MX: DURING CRUISE BRIEF ECAM (2X) ENG.1 FIRE LOOP A FAULT. ECAMS CLEARED AFTER APPROX 3 SECS. NOTED BY MAINTENANCE. PERFORMED OPERATIONAL TEST OF THE ENG. FIRE AND OVERHEAT DETECTION TEST I.A.W. AMM 26-12-00-710-002-B. TEST O.K.May 9, 2023 · N216HA · Airbus A321271N · Fire DetectionSDR HALA2023041300084Unknown · unknownATB - RIGHT WING FUEL AND TEMP INDICATIONS AMBER XX'S, FOB AMBER XX'S. ATTEMPTED QRH RESET WITH MX VIA SATCOM - UNSUCCESSFUL. REMOVED & REPLACED R WING TANK FUEL PROBES 30QT2 & 59QT2 PER AMM 28-42-15 R TANK INDICATION & FOB INDICATION & TEMP INDICATION SHOW NOApr 12, 2023 · N216HA · Airbus A321271N · Aircraft Fuel SystemSDR HALA2023011900010Wire Harness · out of limitsETOPS-ENG B FIRE LOOP ON ECAM. CHECKED RESISTANCE BETWEEN PINS J-K AT FDU 2 LOOP B. FOUND RESISTANCE FLUCTUATING FRANTICALLY OUT OF LIMITS WHILE TAPPING HARNESS 4166KS. REMOVED & REPLACED HARNESS 4166KS PER AMM 26-12-62. RESISTANCE STAYED SOLID AT 1.5K OHMS. EJan 18, 2023 · N216HA · Airbus A321271N · Fire Protection System WiringSDR HALA2023010300001Deu · faultedETOPS - ALL LAVATORIES NOT WORKING IN FLIGHT, HEADING BACK TO LAX. PERFORMED CIDS POWER UPTEST AND FAULTED 300RH8. REMOVED AND REPLACED DEU-B 300RH8 IAW AMM 23-73-47 PB 401, OPS CHECK OF ALL LAV AS OKAY. AC OK TO CONTINUE. ORIG SUB DATE: 1/3/2023Dec 31, 2022 · N216HA · Airbus A321271N · Waste Disposal SystemSDR HALA2022112100297Hpc · usedETOPS-DURING PDC FOUND #2 ENG LEAKING FUEL AT HPC PRIMARY STATOR VANE ACTUATOR. REMOVED AND REPLACED #2 ENG HPC PRIMARY STATOR VANE PER AMM 75-31-02-400-801-A. MECH 16488 / 21800. PENDING IDLE RUN / LEAK CHECK. COMPLETED IDLE RUN & LEAK CHECK PER AMM 71-00-00-Nov 20, 2022 · N216HA · Airbus A321271N · Compressor Bleed GovernorSDR HALA2022102200278Igniter · failedETOPS - APU AUTOSHUTDOWN - TRIED A SECOND TIME WITH ANOTHER AUTOSHUTDOWN. REMOVED AND REPLACED IGNITER AS PER AMM 49-41-41-400-0041-A, ALSO REMOVED AND REPLACED EXITER BOX AS PER AMM 49-41-38-400-003-A, PERFORMED OPS CHECK NORMAL. APU VERIFICATION FLIGHT FOROct 22, 2022 · N216HA · Airbus A321271N · APU Start/Ignition SystemSDR HALA2022102000277Sensor · faultedAIR ENG 1 HP VALVE FAULT. REPLACED PACK INLET PRESS SENSOR (LH) FIN (23HB1) PER AMM 21-51-13. LEAK CHECK OK. OPS PENDING 10-19-22 16801... REMOVED AND REPLACED #1 ENG HPV PER AMM 36-11-51. OPS AND LEAK CHECK PENDING 7880 10/18/22.. CONT ON LOG #895086 ITEM 1. Oct 19, 2022 · N216HA · Airbus A321271N · Pneumatic Distribution SystemSDR HALA2022081200142None · noneETOPS - ENG 2 FIRE LOOP B FAULT DURING CLIMB @ 16000' PRIOR TO ETOPS ENTRY // REMOVED & REPLACED ENG 2 FIRE LOOP B AGB PER AMM 26-12-17. OPS TEST OF ENG FIRE & OVERHEAT DETECTION GOOD PER AMM 26-12-00. OK FOR SERVICE.Aug 11, 2022 · N216HA · Airbus A321271N · Fire Protection SystemSDR HALA2022013100033Unknown · odorON APPROACH STRONG SOCK SMELL LEVELING OFF @ 4000 IN COCKPIT AND FWD CABIN. PERSISTING THROUGH ENG SHUTDOWN // PERFORMED #1 & #2 ENG IDLE RUN PER AMM 71-00-00-860-823-A.OPERATIONAL CHECK OF #1 & #2 PACK PER AMM 21-51-00-710-002-A. NO SMELL NOTED. OK FOR SVC.Jan 28, 2022 · N216HA · Airbus A321271N · Air Distribution SystemSDR HALA2022011200012Oil System · overservicedINFO TO MX ON DESCENT PASSING 5000' FAINT WET SOCK SMELL THROUGH AIR GASPRES. WENT AWAY AFTER A FEW MIN. FOUND ENG 1 OVER SERVICED BY APPROX 3 QTS. REMOVED EXCESS OIL FROM TANK. OPERATED ENG @ IDLE FOR FOR APPROX 5 MIN. NO SMELL. OK FOR SVC.Jan 11, 2022 · N216HA · Airbus A321271N · Turbine Engine Oil SystemSDR HALA2021112200168None · noneETOPS - APU SHUTDOWN PRIOR TO A/C REPOSITIONING // PERFORMED TSM 49-00-81-810-825-A NEED TO REPLACE IGNITION EXCITER PER PARAGRAGH 4A2A REMOVED AND REPLACED IGNITION EXCITER PER AMM 49-41-38. ALL CHECKS GOOD.Nov 19, 2021 · N216HA · Airbus A321271N · APU Start/Ignition SystemSDR HALA2021102500145Unknown · odorIMMEDIATELY AFTER ENGINE START (LIGHT) AND AFTER INITIATING DESCENT (STRONG) DIRTY SOCK SMELL IN COCKPIT. PERFORMED TROUBLESHOOTING OF ENGINES AFTER SMOKE/OIL FUMES IN THE CABIN PER TSM 71-00-00-810-847-A. RAN BOTH ENGINES 1&2 AND OPERATED ALL PAX SYSTEMS. NOct 22, 2021 · N216HA · Airbus A321271N · Air Distribution SystemSDR HALA2021040600044Battery · defectiveEMER EQ - EPSU BATTERIES 11WL AND 13WL FAULTING // REMOVED AND REPLACED EPSU BATTERIES AT 11WL AND 13WL PER AMM 33-51-38-400-002-A. OK FOR SVC.Apr 5, 2021 · N216HA · Airbus A321271N · Emergency LightingSDR HALA2019070800350Warning System · false activationETOPS SIGNIFICANT SYSTEM - ENG 2 IGN B ECAM WENT THRU THE ALT START PROCEDURES. THE ECAM WENT AWAY (STATUS) AFTER ENGINE SHUTDOWN AT DESTINATION. PERFORMED OPS TEST OF THE ENG 2 IGN A+B PER AMM 74-00-00-710-802-A, OPS NORMAL. NO CURRENT FAULT DISPLAYED, OK FOJul 6, 2019 · N216HA · Airbus A321271N · Ignition SystemSDR HALA2019032500142Transducer · defectiveATB - "F/CTL ELEV SERVO FAULT" ILLUMINATED ON CLIMB OUT. PERFORMED OPS TEST OF SIDE STICK ASSY PER AMM 27-96-00-710-020-A. PERFORMED WIRING CHK OF POS RVDT MON SIGNAL FROM ELAC 1 MON PART TO FIRST TERMINAL BLOCK REF 27-93-07. SWAP ELAC 1 AND ELAC 2 NO HELP SWAMar 22, 2019 · N216HA · Airbus A321271N · Elevator Control SystemSDR HALA2018121000636Transceiver · malfunctionedETOPS SIGNIFICANT SYSTEM - CAPTAIN'S SIDE ND FLICKERS BETWEEN WX + TERRAIN WHEN TERRAIN SELECTED. // DURING T/S FOUND FLICKERING ONLY OCCURS WHILE WXR 2 IS ON. REMOVED AND REPLACED #2 WXR TRANSCEIVER IAW AMM 34-41-33 PB 401 CONF 01 OPS TEST GOOD, FLICKERING BEDec 9, 2018 · N216HA · Airbus A321271N · Weather Radar SystemSDR HALA2018121000637Transceiver · malfunctionedETOPS SIGNIFICANT SYSTEM - WX + T + H AND TERR FLASH CONTINUOUSLY WHEN TERR ON ND IS SELECTED ON CA'S SIDE ND.// FOUND DEFECT ASSOCIATED WITH #2 RADAR SYS. RE-RACKED #2 WEATHER RADAR TRANSCEIVER "15Q2" DEFECT CLEARED. OPS CHECK GOOD. OK TO SERVICEDec 8, 2018 · N216HA · Airbus A321271N · Weather Radar SystemSDR HALA2018110100557Carbon Seal · missingETOPS SIGNIFICANT SYSTEM - DURING BOROSCOPE INSPECTION OF #1 ENG FOUND AFT #3 BRG DRY FACE CARBON SEAL MISSING.// REPLACED #1 ENGINE PER TASK CARD J321-72-HWI -02. ALL REQUIRED TESTS CHECK OK. OK FOR SERVICE. ENGINE: IAE, PW1133G-JM.Oct 31, 2018 · N216HA · Airbus A321271N · Engine (Turbine/Turboprop)SDR HALA2018103100554Control Valve · unknownATB AT 8,000 ECAM, AIR FAULT PACK 2. REMOVED AND REPLACED PACK FLOW CONTROL VALVE PER AMM 21-51-51-400-001-A AND PERFORMED OPS TEST OF FLOW CONTROL AND INDICATING SYSTEM PER AMM 21-51-00-710-002-A. OPS CHECK GOOD OK FOR SERVICE.Oct 30, 2018 · N216HA · Airbus A321271N · Cabin Cooling SystemSDR HALA2018102600546Warning System · false activationATB - AFT CARGO DOOR OPEN IN FLIGHT. INSPECTED DOOR, VERIFIED AFT CARGO DOOR CLOSED AND LOCKED PER AMM 52-70-00. PRESSURE CHECK OF AFT CARGO DOOR OK PER AMM 05-53-00-780-001-A. PERFORMED OVERWEIGHT LANDING INSPECTION PER AMM 05-51-11-200-004-B. NO DAMAGE NOTEDOct 25, 2018 · N216HA · Airbus A321271N · Door Warning SystemSDR HALA2018101600502Pressure Sensor · faultyETOPS SIGNIFICANT SYSTEM - ENGINE 1 OIL FILTER DEGRADE. (OIL FILTER DEGRADE CAUTION ON ECAM. REMOVED & REPLACED NR 1 OIL FILTER & NR 1 OIL FILTER DIFFERENTIAL PRESS SENSOR. ENG NR 1 OIL FILTER DEGRADE MESSAGE DID NOT RETURN. A/C IS OK FOR CONTINUE SERVICE.Oct 15, 2018 · N216HA · Airbus A321271N · Engine Oil PressureSDR HALA2018101200492Proximity Switch · malfunctionedOPEN - ATB - AFT CARGO OPEN WARNING IN CLIMB OUT 2500FT. ECAM DOOR PAGE INDICATIONS CARGO DOOR, (INDICATIONS MAY BE INOPERATIVE PROVIDED A VISUAL CHECK IS MADE BEFORE EACH DEPARTURE TO CONFIRM THAT DOORS ARE CLOSED AND LOCKED). SUP - ATB - PERFORMED ALTERNATIOct 11, 2018 · N216HA · Airbus A321271N · Door Warning System
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