Airbus A321-271N

Service difficulty reports · 1,580

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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 aircraft_model_key = 'A321271N'
  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 HALA20251003301Button · crackedETOPS - CAPTAIN FD PUSH BUTTON, ON GLARESHIELD CRACKED. REMOVED AND REPLACED FCU PER AMM 22-81-12. OPS CHECK GOOD. NO DEFECTS NOTED. OK TO CONTINUEOct 2, 2025 · N220HA · Airbus A321271N · Indicating/Recording SystemSDR 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 HALA20251002297Fire Loop · faultedETOPS - FIRE LOOP A CORE ECAM MESSAGE. REPLACED FIRELOOP A CORE PER AMM 26-12-17. OPS CHECK NOT GOOD. REPLACED LOOP A FIRE LOOP HARNESS PER AMM 26-12-61. OPS CHECK NOT GOOD. REMOVED AND REPLACED FIRE LOOP CORE LOOP B PER AMM 26-12-17. OPS CHECK IS GOOD. OKAY TOct 1, 2025 · N213HA · 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 HALA20250929291Pressure Switch · faultedETOPS - APU AUTO SHUTDOWN. REMOVED & REPLACED. ECB & OIL PRESSURE SW PER AMM 49-61-34 & AMM 49-91-14. OPS + LEAK CK GOOD. OK FOR SVCSep 27, 2025 · N213HA · Airbus A321271N · APU Oil SystemSDR 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 HALA20250922285Display · malfunctionedETOPS - MCDU #1 SCREEN FLICKERING AFTER ENG START. BTB. REMOVED AND REPLACED MCDU #1 TEST OK PER:AMM 22-82-12.Sep 19, 2025 · N209HA · Airbus A321271N · Central DisplaySDR HALA20250918281Exciter · faultedETOPS - APU AUTO SHUTDOWN ON TAXI IN. REMOVED AND REPLACED EXCITER - IGNITION BOX PER AMM 49-41-00. OPS CHECK GOOD. OK TO CONTINUE.Sep 17, 2025 · N218HA · Airbus A321271N · APU Start/Ignition SystemSDR HALA20250915278Gauge · abnormalETOPS - ACCUMULATOR GAUGE WAS FILLED WITH HYDRAULIC FLUID. REMOVED AND REPLACED GREEN SYSTEM ACCUMULATOR AND PRESSURE GAUGE. OPS CHECK GOOD, OKAY FOR SERVICE PER AMM 29-11-42.Sep 14, 2025 · N202HA · Airbus A321271N · Hydraulic System, MainSDR HALA20250904048Not Reported · not reportedTOW BAR SNAPPED ON PUSH. AWAITING FULL RESOLUTION.Sep 2, 2025 · N217HA · Airbus A321271N · Standard Practices/StructuresSDR 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 HALA20250829264Fuel Cap · missingETOPS - DURING WALKAROUND FOUND RIGHT WING MISSING FUEL CAP. REPLACED RIGHT WING FUEL COUPLING PER AMM 28-25-41. OK FOR SVC.Aug 28, 2025 · N220HA · Airbus A321271N · Fuel StorageSDR HALA20250826263Gcu · no testDIV - ECAM: GEN 1 FAIL. EPGS SYSTEM TEST: GCU 1 TEST FAILED. FAULT MESSAGE IDG1(E1-400XU)SERVO VLV/GCU1 (1XU1). PERFORMED TSM 24-20-00-810-914-A. FOUND CABLE E1-400XU CONTAMINATED AND SLIGHTLY LOOSE. CLEANED AND SECURED AS REQUIRED. RESISTANCE & WIRE CHECKS ALAug 26, 2025 · N214HA · Airbus A321271N · AC Generator-AlternatorSDR HALA20250826262Wire Harness · faultedETOPS - ENG 1 LOOP B FAULT. REPLACED ENG 1 LOOP B FIRE HARNESS PER A321 AMM 26-12-62 OPS CHECK GOOD , OK FOR SERVICEAug 25, 2025 · N214HA · Airbus A321271N · Fire DetectionSDR HALA20250825259Igniter · wornETOPS - DURING IGNITER SEGMENT INSPECTION, FOUND BOTTOM IGNITER PLUG WORN BEYOND LIMITS ON ENGINE #2. REMOVED AND REPLACED BOTTOM IGNITER PLUG PER AMM 74-21-01 ON ENGINE #2. OPS CHECK GOOD. OK TO CONTINUEAug 22, 2025 · N228HA · Airbus A321271N · Spark Plug/IgniterSDR YENA2025082200864Transfer Sys · faultedFLT# 073, JFK-EDI. (ETOPS) "AFTER DOORS CLOSED ECAM APPEARED FUEL ACT XFR FAULT ( CAUTION ON ECAM 5) ACT XFR FAULT (ACT) ); PER TSM 28-28-00-810-874-A FUEL DISTRUBUTION OUT AT TIME OF DEFFERAL WAS INCORRECT CAUSING MESSAGE TO APPEAR.FUEL DISTRIBUTION HAS BEENAug 21, 2025 · N2180J · Airbus A321271N · Aircraft Fuel Distribution SystemSDR YENA2025082200863Coffeemaker · odorFLT # 1908. CDG-JFK. (ETOPS) FAS REPORTED TO US THEY NOTICED AN INTERMITTENT BURNING SMELL BETWEEN ROWS 2-8. STARTED RIGHT BEFORE DESCENT. THEY DIDNT NOTICE ANYTHING FROM LAVS AND OVENS.; ACCOMPLISHED INFO NOTICE 2017-T015 SECTION A ISOLATED FAULT TO TYPE 10(FAug 20, 2025 · N4058J · Airbus A321271N · Buffet/GalleysSDR HALA20250820255Fire Loop · faultedETOPS - ENG 1 FIRE LOOP B FAULT IN FLT. REMOVED & REPLACED ENG 1 FIRE LOOP B PER AMM 26-12-17. OPS CK BITE TEST GOOD. OK FOR SVC.Aug 19, 2025 · N228HA · Airbus A321271N · Fire DetectionSDR YENA2025082200862Computer · failedFLT # 2288. JFK-AMS. (ETOPS) CLASS 2 STATUS MSG MAINTENANCE SMOKE ( CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 2) FAULT(S) INDICATED BY SMOKE );MEL 26-00-00B CAT C PLACARD MX 4 MCC HAROON. R/R FWC #2 IRT AMM 31-53-34. OPAug 18, 2025 · N4083J · Airbus A321271N · Flight Management Computing Hardware SystemSDR 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 HALA20250818249Generator · faultedETOPS - ELEC GEN 1 FAULT- AT CRUISE DID NOT RESET. REMOVED & REPLACED #1 IDG PER AMM 24-21-51. OPS CHECK IS GOOD. OKAY TO CONTINUE.Aug 17, 2025 · N214HA · Airbus A321271N · AC Generator-AlternatorSDR HALA20250818250Jumper · wornETOPS - DURING TASK CARD E1128-321-26-011 PYLON. FOUND JUMPER ON LPT ACC COOLING TUBE ON 3 OCLOCK WORN OVER LIMIT. REMOVED LPT ACC COOLING TUBE PER AMM 75-00-00-210-802-A ALEX 023895. INSTALLED LPT ACC TUBE WITH NEW JUMPER 1EA. IDLE RUN. FOUND NO LEAK. OK FOR Aug 15, 2025 · N220HA · Airbus A321271N · Nacelle/Pylon System WiringSDR HALA20250813246Cabin Pressure · malfunctionedDIV - AVIONICS DOOR OPEN IN FLIGHT MESSAGE A/C NOT PRESSURIZING NORMALLY. PERFORMED VISUAL INSPECTION OF AVIONICS DOOR. PERFORMED PRESSURIZATION TEST FOR AIR LEAKS PER AMM 05-53-00. NO DEFECTS NOTED. OK TO CONTINUE.Aug 12, 2025 · N208HA · Airbus A321271N · Cabin Pressure Control SystemSDR HALA20250812245Control Valve · faultedDIV - AFT CABIN VERY WARM DIV TO OAK: AT TOC NOTICED PACK 2 AMBER ON PRESS PG, BLEED PG. SHOWING NO PRESSURE & IP VALVE CLOSED. MX TROUBLESHOOT IN AIR W/ X BLEED STILL NO PRESSURE, NO RESET. REMOVED & REPLACED #2 FLOW CONTROL VALVE (24HB) PER AMM 21-51-51. PERAug 11, 2025 · N226HA · Airbus A321271N · Cabin Temperature Control SystemSDR HALA20250811241Fire Detector · damagedETOPS - ENG 1 FIRE LOOP A FAULT ON DESCENT. FOUND DAMAGE ON ENG 1 FIRE LOOP A DETECTOR. REMOVED AND REPLACED FIRE DETECTOR PER AMM 26-12-17. OPS CHECK NORMAL. OK FOR SERVICE.Aug 10, 2025 · N204HA · Airbus A321271N · Fire DetectionSDR 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 HALA2026090300193Stringer · corrodedDURING INSPECTION DURING HMV AS PER MPD TASK REFERENCE 534144-01-1, SIAEP FOUND CORROSION ON THE INTERNAL SIDE OF THE TOILET SERVICE PANEL REINFORCEMENT PLATE, FOUND ALONG FRAME 65 AND STRINGER 39R. UPON EVALUATION, THERE ARE NO APPLICABLE ADL AND REPAIRS IAW Aug 2, 2025 · N223HA · Airbus A321271N · Fuselage Main, Longeron/StringerSDR HALA2026090300195Stringer · corrodedDURING INSPECTION DURING HMV AS PER MPD TASK REFERENCE 534144-01-1, SIAEP FOUND CORROSION ON THE INTERNAL SIDE OF THE TOILET SERVICE PANEL REINFORCEMENT PLATE, FOUND ALONG FRAME 65 AND STRINGER 39R. UPON EVALUATION, THERE ARE NO APPLICABLE ADL AND REPAIRS AS PAug 2, 2025 · N223HA · Airbus A321271N · Fuselage Main, Longeron/StringerSDR 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 HALA20250728235Fuel Sys · leakingETOPS - FUEL LEAK COMING OUT LH AND RH WING DRY BAY WEEP HOLES. REPAIRED BOTH LEFT & RIGHT WING DRY BAY FUEL LEAKS IN ACCORDANCE WITH SRM 51-76-12. PERFORMED LEAK TEST PER AMM 28-11-00. NO LEAKS NOTED.Jul 26, 2025 · N208HA · Airbus A321271N · Fuel StorageSDR HALA20250724230Oil Filter · warning messageETOPS - ECAM: ENG 2 OIL SENSOR FAULT OCCURED DURING FLIGHT, NO ACTIONS GIVEN. PER TSM 79-35-00-810-808-A, INSPECTED THE MAGNETIC CHIP COLLECTORS AND WITHIN LIMITS. INSPECTED AND REPLACED MAIN OIL FILTER ELEMENT PER AMM 79-21-06-960-801-A, OPS CHECKED GOOD. IDLJul 23, 2025 · N205HA · Airbus A321271N · Turbine Engine Oil SystemSDR HALA20250721223Door · openATB - IN FLIGHT PAX OBSERVED THRUST REVERSER FLIPPER DOOR OPEN. #2 ENGINE. DEFERRAL OF #2 THRUST REVERSER FLIPPER DOOR. #2 ENG INBD AFT FLIPPER DOOR SPEED TAPED (THRUST REVERSER FLIPPER DOOR). OK FOR SERVICE.Jul 20, 2025 · N205HA · Airbus A321271N · Engine Thrust ReverserSDR HALA20250721222Pump · failedETOPS - DURING T.O. ROLL HYD Y ENG 2 PUMP LOW PRESSURE INTERMITTENT. Y LEVEL FLUCTUATING DURING TAXI. PERFORMED TSM 29-13-00-810-804-A. OPS TEST OF YELLOW HYDRAULIC SYSTEM FAILED. REMOVED AND REPLACED ENG #2 YELLOW ENGINE DRIVEN PUMP. ENGINE IDLE RUN, LEAK CHEJul 20, 2025 · N205HA · Airbus A321271N · Hydraulic Pump (Electric/Engine), MainSDR HALA20250721224Pin · out of limitsETOPS - APU AUTOSHUTDOWN ON TAXI INTO GATE. FOUND STARTER WEAR PIN BEYOND LIMITS. REMOVED AND REPLACED STARTER PER AMM 49-42-51. OPS CHECK GOOD. OK FOR SVC.Jul 18, 2025 · N209HA · Airbus A321271N · APU Start/Ignition SystemSDR HALA20250717039Smoke Detector · false activationSMOKE LAVATORY SMOKE MESSAGE CONFIRMED WITH FA FALSE ALERT. FFA DID RESET AND MESSAGE CLEARED. NO SMOKE/VAPE/FIRE PRESENTJul 17, 2025 · N214HA · Airbus A321271N · Smoke DetectionSDR HALA20250715212Wire Harness · faultedETOPS - ON CLIMB OUT MOMENTERY ECAM FOR ENG 1 LOOP B FAULT MESSAGE CLEAR ON ITS OWN AFTER A FEW MINUTES. REMOVED AND REPLACED ENGINE 1 HARNESS 4166KS PER AMM 26-12-62 AND REPLACED ENGINE 1 CORE AGB LOOP B FIN 4002WD2 PER AMM 26-12-17 OPS CHECK OKJul 14, 2025 · N214HA · Airbus A321271N · Fire Protection System WiringSDR HALA20250627199Exciter · faultedETOPS - ENG 1 IGN B FAULT. REMOVED & REPLACED IGNITION EXCITER PER AMM 74-11-01-000-801-A & AMM 74-11-01-400-801-A. REMOVED & REPLACED IGNITER PLUG PER AMM 74-21-01.PERFORMED OPS TEST OF IGNITION SYSTEM PER AMM 74-00-00-710-802-A. OPS TEST GOOD. NO FAULTS NOTEJun 26, 2025 · N214HA · Airbus A321271N · ExciterSDR YENA2025062300643Fire Loop · faultedFLT#215, JFK-SFO. (ETOPS) ENG 2 FIRE LOOP B FAULT INTERMITTENT ( ENGINE FIRE DETECTION SYSTEMS 2) LOOP B); REF LP # 4324107 ITEM #2 FOR R/R OF ABG ENG 2 FIRE LOOP B. NO FAULT NOTED SINCE REPLACEMENT. BITE TEST OF FDU 2 CARRIED OUT IAW AMM 26-12-00. NO FAULTS Jun 22, 2025 · N2193J · Airbus A321271N · Fire DetectionSDR YENA2025062300642Fire Loop · failedFLT#158, AUA-JFK. (ETOPS) "ON INBOUND FLIGHT ENG 2 FIRE LOOP B AGB REPORTED FAULT; REMOVED AND REPLACED ENG 2 FIRE LOOP B AGB (4002WD2) IAW AMM 26-12-17. OPS CHECK GOOD NO FAULTS AT THIS TIMEJun 21, 2025 · N2193J · Airbus A321271N · Fire DetectionSDR HALA20250623190Eec · faultedETOPS - DURING HIGH POWER RUN OF #1 ENG, " ENG 1 HOT AIR LEAK" MESSAGE. EEC BITE SHOWED "EEC INTERNAL FAIL NO GO" AND MULTIPLE PAGES OF FAULTS. REMOVED AND REPLACED #1 EEC PER AMM 73-21-01-400-801-A. IDLE RUN OK. CAT III TEST ACCOMPLISHED ON T/C 321-22-HWI-03.Jun 21, 2025 · N223HA · Airbus A321271N · Fuel Controlling SystemSDR YENA2025062300640Autopilot Sys · disengagedFLT#9, JFK-SDQ. (AIRCRAFT PERFORMED AN AIRTURN BACK TO JFK). "APPROX 10-15 MINS AFTER DEPARTURE A/C WAS LEVELING AT 12,000 FT, 250 KTS. A/C EXPERIENCED A GRADUAL UPDRAFT TO 12300 FEET, A/P KICKED OFF. F/O WAS CORRECTING, AS WE CLEARED WX. WE THEN ENCOUNTERED AJun 19, 2025 · N2029J · Airbus A321271N · Autopilot SystemSDR HALA20250620187Sdu · leakingETOPS - DIRTY SOCK SMELL DECSENDING THROUGH 6,000' - 3,000'. DURATION APPROXIMATELY 10 MIN. PUSHED DFDR EVENT BUTTON. FOUND OIL STREAKS COMING FROM #1 ENG INLET CONE WEEP HOLES AND OIL PUDDLING INSIDE OF #1 ENG INLET CONE. REPLACED THE FAN SHAFT COVER SEAL PE Jun 18, 2025 · N213HA · Airbus A321271N · Turbine Engine Oil SystemSDR 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 HALA20250617184Sensor · faultedETOPS - ON DECENT AS THRUST WENT TO IDLE "ENG 1 SENSOR FAULT". REMOVED BURNER PRESSURE SENSOR AND BURNER PRESSURE SENSOR TUBE IN REFERENCE TO AMM 73-21-23-000-801-A AND 73-21-23-000-802A K.H. 25197 06/15/2025. INSTALLED BURNER PRESSURE AND LINE PER AMM 73-21-2Jun 16, 2025 · N213HA · Airbus A321271N · Engine Indicating SystemSDR YENA2025061800635Unknown · odorFLT#169, JFK-PUJ. 'MAGIC MARKER SMELL DESCENDING THROUGH 11000, DISSIPATED AFTER APPROX 60 SECONDS; C/W INFORMATION NOTICE 2015-T015 SECTION A ISOLATED FAULT TO TYPE 10 PER TSM 05-50-00-810-805B NO CABIN ODOR DETECTED WHEN CREW REPORMED ENGINE RUN. A/C OK FOR Jun 15, 2025 · N2044J · Airbus A321271N · Air Distribution SystemSDR 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 HALA20250613179Pitot Head · obstructedETOPS - BTB: HIGH SPEED REJECT (100KTS) FOR NO AIRSPEED INDICATION ON THE CAPT'S SIDE (ND). FOUND CAPT'S PITOT TUBE OBSTRUCTED. REMOVED & REPLACED CAPT'S PITOT TUBE PER AMM 34-11-15. A/C OK FOR SERVICE.Jun 12, 2025 · N96 · Airbus A321271N · Pitot/Static SystemSDR 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 HALA20250609166Fire Loop · faultedETOPS - ENG 2 FIRE LOOP B FAULT -IN CRUISE FL320-. PERFORMED TSM TASK 26-12-00-801-861-A, FAULT CONFIRMED, REMOVED AND REPLACED FIRE LOOP ASSY FWD IAW AMM 26-12-17-000-802, 26-12-17-400-802-A OPS CHECK GOOD, OK FOR SERVICEJun 8, 2025 · N202HA · Airbus A321271N · Fire Detection
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