N208HA

Service difficulty reports · 50

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 = 'N208HA' 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 ASAA2026100867315Arming Lever · dirty4R DOOR SLIDE LEVER DOES NOT ARM. GROUNDED - YES. FOUND DEBRIS SMALL EXITPLACARD IN GIRT BAR LATCH, REWMOVED DEBRIS DOOR SRMED NORMALLY AND REINSATLLED EXIT SIGN AS REQUIRED AC OKAY TO CONTINUE.Oct 8, 2026 · N208HA · Airbus A321271N · Service DoorsSDR ASAA2026052865025Pressure Switch · unserviceableATB: ENG #1 HYD GREEN LO PRESSURE. GROUNDED - YES. REPLACED#1 ENG PUMP PRESSURE SWITCH (FIN 1074GK) PER AMM 29-11-17. 17261 05/29/26 PENDING WIRING, OPS & LEAK CHECK. PENDING WIRING, OPS && LEAK CHECK. REPAIRED WIRING TO 1074GK PER ESPM 20-53-22 OPS CHECK PENDMay 28, 2026 · N208HA · Airbus A321271NX · Hydraulic System, MainSDR 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 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 HALA20250606163Igniter · failedETOPS - ENG 2 IGN A FAULT DURING START. REMOVED AND REPLACED IGN A IGNITER PLUG ON ENG 2 PER AMM 74-21-01. OPS CHECK GOOD. NO DEFECTS NOTED. OK FOR SERVICEJun 5, 2025 · N208HA · Airbus A321271N · Spark Plug/IgniterSDR HALA20250529154Display · faultedETOPS - MCDU'S DON'T MATCH WHEN IT COMES TO FUEL PREDICTION, TIME PREDICTION, AND VERTICAL PATH ERROR. FO'S MCDU APPEARS TO SHOW TIME: 4 MINUTES EARLIER, FUEL BURN: 400 MORE POUNDS, ABOVE DESCENT PATH: 400 FEET. REMOVED AND REPLACED FQIC PER AMM 28-42-34-04. NMay 27, 2025 · N208HA · Airbus A321271N · Fuel Indicating SystemSDR HALA20250527150Valve · faultedATB DUE TO ECAM ENG 2 BLEED FAULT. REMOVED AND REPLACED #2 ENGINE FAN AIR VALVE PER AMM 36-11-54. BITE TEST OF LEFT ENGINE BLEED SYSTEM GOOD. PERFORMED IDLE RUN OF #2 ENGINE. ALL CHECKS GOOD. OK TO CONTINUEMay 25, 2025 · N208HA · Airbus A321271N · Engine Bleed Air SystemSDR HALA20250416108Igniter · failedETOPS-BTB: APU FAIL. REPLACED APU IGNITOR PLUG AND LEAD REF AMM 49-41-41 AND 49-41-43, OPS TEST NORMAL. OK FOR SVC.Apr 15, 2025 · N208HA · Airbus A321271N · APU Start/Ignition SystemSDR HALA20250210058Switch · faultedETOPS - BEFORE TOW OPERATIONS, ATTEMPTED TO START APU, "APU AUTO SHUT SHUTDOWN" MESSAGE SHOWN ON ECAM. APU GRANDSCAN CONFIRMS "OIL FILTER SWITCHES" FAULT. CLEAN CONNECTORS P5 & P9 IAW TSM 49-90-00-810-812-A. APU START NOT SUCCESSFUL. REMOVED & INSPECTED PRESSUFeb 7, 2025 · N208HA · Airbus A321271N · APU Oil SystemSDR HALA20241230385Oil Filter · cloggedETOPS - FOUND APU OIL FILTERS CLOGGED. REMOVED AND REPLACED APU OIL FILTERS PER AMM 49-91-41-200-002-A. LEAK AND OPS CHECK GOOD. OK FOR SERVICE.Dec 28, 2024 · N208HA · Airbus A321271N · APU Oil SystemSDR HALA20241227382Control Valve · faultedETOPS - PACK 2 FAULT PRIOR TO DEPARTURE. REMOVED AND REPLACED PACK 2 FLOW CONTROL VALVE PER AMM 21-51-51. OPS CHECK / LEAK CHECK OK.Dec 26, 2024 · N208HA · Airbus A321271N · Cabin Cooling SystemSDR HALA20241202345Connector · damagedETOPS - APU FAULT ON TAXI OUT BTB. ITEM ALREADY ON DMI, REPLACED AND RESECURED PINS/ JUMP CONNECTORS PER AMM 49-16-00-003-A OPS CHK OF APU GOOD OK TO REMAIN ON DMI.Dec 1, 2024 · N208HA · Airbus A321271N · APU System WiringSDR HALA20241023295Packing · leakingETOPS - #1 ENG OIL NEAR FAN BLADES (OIL BLADES). REMOVED AND REPLACED #1 ENG FAN SHAFT COVER PACKING IDLE POWER TEST GOOD. LK CK GOOD. OK FOR SERVICE IAW AMM 72-15-00-960-801-AOct 22, 2024 · N208HA · Airbus A321271N · Engine (Turbine/Turboprop)SDR HALA20240725197Filter · faultedETOPS - APU AUTO SHUTDOWN TWICE DURING PREFLIGHT. PERFORMED BITE TEST, FAULTED GEN SCAV AND LUBE FILTERS. REMOVED AND REPLACED BOTH FILTERS IN REF W/ AMM 49-91-41-200-002-A. APU OPS CHECK GOOD. LEAK CHECK GOOD. NO LEAK NOTED. OK FOR SVC.Jul 24, 2024 · N208HA · Airbus A321271N · APU Oil SystemSDR HALA20240703178Apu · shutdownETOPS - APU: AUTO SHUT DOWN ON TAXI IN 3X ATTEMPTS FAILED. REMOVED & REPLACED WIRING FROM APU STARTER MOTOR + TERMINAL LUG TO 7120VC PIN 1. WIRES X011A20, X011B14, X011C14 PER ESPM 20-33-11. REMOVED & REPLACED APU STARTER MOTOR CLUTCH PER AMM 49-42-52. PERFORMJul 2, 2024 · N208HA · Airbus A321271N · Airborne Auxiliary Power Unit (APU) SystemSDR HALA20240327077Packing · leakingETOPS - HYD LEAK COMING FROM LH AFT DRAIN MAST. REMOVED AND REPLACED PACKING ON # 1 ENG HYD PUMP PRESSURE SWITCH PER AMM 29-11-17, OPS AND LEAK CHECK OKAY.Mar 26, 2024 · N208HA · Airbus A321271N · Hydraulic System, MainSDR HALA20240207039Plug · missingETOPS - SAW A FEW DROPS OF OIL UNDER #1 ENGINE FAN COWL. FOUND LP05 OIL MANIFOLD DRAIN PLUG MISSING SCREW REF PIPC 79-21-49-01 ITEM 320 & 140 & 150. INSTALLED MISSING BOLT P/N: ST2601-06. NO LEAKS NOTED OK FOR SERVICE.Feb 6, 2024 · N208HA · Airbus A321271N · Turbine Engine Oil SystemSDR HALA20240131005Battery Pack · inoperativeFOUND EMER LT/EPSU (12WL) INOP DURING SERVICE CHECK. REMOVED AND REPLACED EPSU BATTERYPER AMM 33-51-38. BITE TEST GOOD. OK FOR SERVICEJan 30, 2024 · N208HA · Airbus A321271N · Emergency LightingSDR HALA20231223284Unknown · unknownETOPS - HYDRAULIC OIL LEAKING FROM RH ENGINE. REMOVED AND REPLACED O RING SEAL IN COUPLING HALFT FROM YELLOW HYDRAULIC SYSTEM PER AMM 29-13-39. LEAK CHECK WITH DRY MOTOR OF ENGINE PER AMM 71-00-00-860-817A GOOD. NO FAULTS. OK FOR SERVICEDec 22, 2023 · N208HA · Airbus A321271N · Hydraulic Pump (Electric/Engine), MainSDR HALA20231124255Unknown · unknownETOPS - 1L DOOR HANDSET UNREADABLE ON INTERCOMAND PA. REMOVED AND REPLACED 1L DOOR HANDSET. OPS CHECK GOOD. OK FOR SERVICE PER AMM 23-73-44.Nov 22, 2023 · N208HA · Airbus A321271N · Communications SystemSDR HALA20240520137Fire Loop · faultedETOPS - ENG 2 FIRE LOOP A FAULT ON ECAM PAGE. REMOVED AND REPLACED FIRE DETECTOR ELECTRICAL LOOP A PER AMM 26-12-61-000-807-A. OPS CHECK GOOD. OK FOR SERVICE.May 18, 2023 · N208HA · Airbus A321271N · Fire DetectionSDR HALA2023041300086Unknown · unknownSUPPLEMENTAL SUBMISSION TO HALA2023041300086. CORRECTION FROM REGISTRATION # 217HA TO 208HA. ATB - 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 Apr 10, 2023 · N208HA · Airbus A321271N · Engine Start Valves/ControlsSDR HALA2023032800067Unknown · unknownETOPS - DUIRNG T/C 321-72-HWI-03 LEAK CHECK FOUND PRV MUSCLE TUBE CRACKED AND LEAKING BLEED AIR. REMOVED AND REPLACED PRV MUSCLE TUBE IAW AMM 36-11-52-000-802-A. AND 36-11-52-400-802-A. OPS CK GOOD. LEAK TEST GOOD. OK TO CONTINUE.Mar 27, 2023 · N208HA · Airbus A321271N · Pneumatic SystemSDR HALA2023032200055Fan · faultySUPPLEMENTAL TO HALA2023032000051. UPDATED WITH RESOLUTION. ETOPS - DMI# 206665 VENT EXTRACT FAULT. (CREW PLACARD). REMOVED AND INSTALLED VENT EXTRACT FAN PER AMM 21-26-51-00. PERFORMED OPERATIONAL TEST OF VENTILATION SYSTEM PER AMM 21-26-00-710-001-A. OPS CHEMar 22, 2023 · N208HA · Airbus A321271N · Air Distribution FanSDR HALA2023032000051Unknown · unknownETOPS - DMI# 206665 VENT EXTRACT FAULT. (CREW PLACARD). AWAITING RESOLUTION.Mar 17, 2023 · N208HA · Airbus A321271N · Air Conditioning SystemSDR HALA2023031600043Unknown · unknownETOPS - DMI# 206657 ENG 1 FIRE LOOP B FAULT IN CRUISE ( ENGINE FIRE DETECTION SYSTEMS LOOP B (EXCEPT FOR ER OPERATIONS BEYOND 120 MINUTES, ONE MAY BE PROVIDED: ASSOCIATED LOOP A IS OPERATIVE / THE ENGINE FIRE TEST IS PERFORMED BEFORE EACH DEPARTURE) ) TROUBLEMar 15, 2023 · N208HA · Airbus A321271N · Fire DetectionSDR HALA202303060032Computer · faultedETOPS - AVNCS SYS FAULT DURING PREFLIGHT. FOUND INLET BYPASS V (16HQ) FAULT. DEFERRED PER MEL 21-26-03. REF TSM 21-26-00-810-806-A, CHSNGED INLET BYPASS VALVE (16HQ), CONDITION SAME. REMOVED & REPLACED AEVC COMPUTER. BITE CHECK GOOD, NO FAULTS NOTED. PLACARD RMar 3, 2023 · N208HA · Airbus A321271N · Air Conditioning SystemSDR HALA2022090600255None · noneETOPS - APU LEAK DETECT FAULT ON ECAM. PERFORMED TSM 36-22-00-810-876-A. FOUND ELEMENT SESOR (15HF) SHORTED TO GRN. REMOVED AND REPLACED OVHT SENS ELEMENT (15HF) PER AMM 36-22-17-400-001 BITE TESET GOOD. OK FOR SVC.Sep 3, 2022 · N208HA · Airbus A321271N · Pneumatic SystemSDR HALA2022080300138None · noneETOPS - AT 8000' "ENG 2 FADEC SYS FAULT THRUST LEVER 2 NOT ABOVE IDLE" THRUST LEVERS WERE IN CL DETENT // PERFORMED INSPECTION OF ENG #2 EEC AND N2 SPEED TRANSDUCER HARNESS & CONNECTIONS PER TSM 77-11-00. CHECKS OK. REMOVED & REPLACED ENG #2 N2 SPEED TRANSDUCEAug 2, 2022 · N208HA · Airbus A300* · Manifold Pressure (MP) IndicatingSDR HALA2022030200061None · noneETOPS - STATUS MSG , ENG # 1 FIRE LOOP A FAULT // RESET FDU 1 C/B'S PER AMM 26-12-34, AS PRECAUTIONARY REMOVED AND REPLACED FDU 1 CAS6465, RAN # 1 ENG AT IDLE FOR FIVE MINUTES NO FAULTS NOTED, OPS CHECK GOOD , OK FOR SERVICEMar 1, 2022 · N208HA · Airbus A321271N · Fire DetectionSDR HALA2022020400039Computer · faultedBTB 2 - SELECTING FLAPS 1 ECAM F/CTL FLAPS FAULT // PERFORMED BITE OF SFCC PER AMM 27-54-00. FAULTING SFCC2 22CV. REMOVED AND REPLACED SFCC2 PER AMM 27-51-34, OPS CHECK GOOD. OK FOR SVCFeb 3, 2022 · N208HA · Airbus A321271N · Leading Edge Slat Control SystemSDR HALA2022020400038None · noneBTB 1 - SPEED LIMIT DISPLAYED ON BOTH PFD’S FD+SPD LIM RED INDICATIONS // RE-SET A/C TO NORMAL CONDITIONS. BOTH PFD FD AND SPD LIM INDICATIONS ARE ABSENT. INDICATIONS READING NORMAL.Feb 3, 2022 · N208HA · Airbus A321271N · Indicating/Recording SystemSDR HALA2022011100010Skin · damagedDURING PDC FOUND BOTTOM TAIL AREA FUSELAGE SKIN DAMAGE AND AFT GALLEY DRAIN MAST DAMAGE. DAMAGE AREA: FRAME 61-70, STRINGER 42LH - 40 RH. 176" LONG 22" WIDE // REPAIRED DAMAGE TO BOTTOM TAIL AREA AT FRAME 61-70 STRINGER 42LH-40RH AS PER AIRBUS WOTD: M-308924-EJan 10, 2022 · N208HA · Airbus A321271N · Fuselage Structure (General)SDR HALA2021090600107Clamp · looseETOPS - ENG 1 FIRE LOOP A FAULT DURING TOW UP, FAULTING ENG 1 LOOP A CORE AND AGB LOOPS FOUND LOOSE CLAMP AND WIRE ON LOOP A HI TEMP WIRE HARNESS. SECURED CLAMP AND ADJUSTED SLACK ON HARNESS REPLACED ENG 1 LOOP A CORE DETECTOR PER AMM 26-12-17. ALL OPS CHECK GSep 6, 2021 · N208HA · Airbus A321271N · Fire DetectionSDR HALA2021072200087Fire Loop · malfunctionedETOPS - ENG2 FIRE LOOP A. PERFORMED TSM26-12-00-810-825-A & TSM 26-12-00-810-914-A. REPLACED ENG2 FIRE LOOP A PER AMM26-12-16-400-803-A AND INSTALLED PYLON FIRE DETECTOR IAW AMM 26-12-16-400-802-A. SECURITY CHECKED GOOD. RAMP ASSY.AMM26-12-00-710-001.SECURJul 22, 2021 · N208HA · Airbus A321271N · Fire DetectionSDR HALA2021061400070Fire Loop · faultedETOPS - PASSING FLI 80 "ENG 2 FIRE LOOP B FAULT" MSG. MSG CLEARED AFTER APPROX 5 MINS. REPEAT WRITE UP. FOUND ENG 2 LOOP B INTERMITTENT. PERFORMED CONTINUITY CHECK PER TSM 26-12-00. NO FAULT NOTED. PRECAUTIONARY ACTION, REMOVED AND REPLACED FWD FIRE LOOP ASSY Jun 13, 2021 · N208HA · Airbus A321271N · Fire DetectionSDR HALA2021060700084Fire Loop · faultedETOPS - ECAM ENG2 FIRE LOOP A FAULT, REMOVED AND REPLACED FIRE DETECTOR ENG 2 LOOP A PYLON IAW AMM 26-12-16 OPS CHECK OK NO FAULTS NOTED.Jun 6, 2021 · N208HA · Airbus A321271N · Fire DetectionSDR HALA2021032800038Fire Loop · brokenETOPS - #2 FIRE LOOP A FAULT // FOUND ENGINE 2 PYLON DETECTOR LOOP A (3WD2) BROKEN. REMOVED PYLON FIRE-DETECTOR RAMP ASSY PER A321 AMM 26-12-16-000-802-A. 21402. 3/29/21.Mar 28, 2021 · N208HA · Airbus A321271N · Fire DetectionSDR HALA2020022700044Chip Detector · false indicationETOPS SIGNIFICANT SYSTEM- AFTER LANDING: ECAM ENG 1 OIL CHIP DETECTED. // PERFORMED TSM 79-35-00-810-808-A "CHIP DETECTED ALERT BY ODM" NO METAL DEBRI FOUND. OK TO CONTINUE. REMOVED AND REPLACED OIL FILTER PER AMM 79-21-06-960-801-A. PERFORMED IDLE RUN LEAK CHFeb 26, 2020 · N208HA · Airbus A321271N · Turbine Engine Oil SystemSDR HALA2020021000920Fire Loop · faultedSUP - ECAM: ENG. 2 FIRE LOOP A FAULT ON CLIMB. // REPLACED FIRE LOOP A DETECTOR PER AMM 26-12-16, FUNCTIONAL CHECK OK. OK FOR SERVICE.Jan 29, 2020 · N208HA · Airbus A321271N · Fire DetectionSDR HALA20200130020Warning Light · false activationETOPS: ECAM - ENG 2 FIRE LOOP A FAULT ON CLIMB. REPLACED FIRE LOOP A DETECTOR PER AMM 26-12-16, FUNCTIONAL CHECKED OK.Jan 29, 2020 · N208HA · Airbus A321271N · Fire DetectionSDR HALA2020010600001Warning System · false activationETOPS SIGNIFICANT SYSTEM - AFTER GO AROUND ECAM "ENG 1 START VALVE FAULT. START VALVE NOT CLOSED" COMPLIED WITH ECAM ACTIONS. // PERF EEC OPS TEST NO.6 PER AMM 73-21-00-710-807-A. NO DEFECTS NOTED.Jan 6, 2020 · N208HA · Airbus A321271N · Engine Start Valves/ControlsSDR HALA2019092320382Start Valve · openETOPS SIGNIFICANT SYSTEM - ENGINE 2 START VALVE FAULT, VALVE NOT CLOSED. REMOVED AND REPLACED STARTER ON ENGINE 2, PER AMM 80-11-01. OPS CHECK GOOD. OK TO CONTINUE.Sep 22, 2019 · N208HA · Airbus A321271N · Engine Start Valves/ControlsSDR HALA2019082200350Fault Message · false activationATO - BRAKE SYSTEM 2 FAULT CAME ON @ TAKEOFF POWER. ABORTED TAKEOFF RESET A/SKID AND N/W STEG. RESET SUCCESSFUL. NO INBOUND FAULTS. PREFORMED TROUBLESHOOTING IN REF. WITH TSM 32-51-00-810-514-A. NO DEFECTS NOTED. OKAY FOR SERVICE.Aug 21, 2019 · N208HA · Airbus A321271N · Landing Gear Steering SystemSDR HALA2019070100338Smoke Warning · false activationLAVATORY SMOKE ECAM IN-FLIGHT, PAX SUSPECTED OF SMOKING IN LAV D. CHECKED LAV D SMOKE DETECTOR & WASTE BIN FIRE EX, NO FAULTS FOUND. PERFORMED CIDS SDF1 LAV SMOKE WARN TEST NO FAULTS. OK FOR SVC. REF AMM 26-17-00Jun 30, 2019 · N208HA · Airbus A321271N · Smoke DetectionSDR HALA2019050400214Smoke Warning · false activationLAV C SMOKE WARNING WENT OFF FOR SEVERAL SECONDS AND FA'S VERIFIED OPS NORMAL WITH NO SMELL. T/S PER TSM 26-16-17-00-810-812-A. OPS CKS GOOD, OK TO CONTINUE.May 1, 2019 · N208HA · Airbus A321271N · Smoke DetectionSDR HALA2019042500201Outflow Valve · faultedATB - VENT SKIN VALVE FAULT. // FOUND MAIN SKIN AIR OUTLET VALVE IN PARTIALLY OPEN POSITION, MANUALLY OPENED VALVE TO FULL OPEN. ACCOMPLISHED AEVC TEST TWICE, BOTH PASSED. VALVE OPS OK.Apr 24, 2019 · N208HA · Airbus A321271N · Pressure Regulator/Outflow ValveSDR HALA2019020500045Smoke Warning · false activationDURING FLIGHT LAV SMOKE WARNING, FA PANEL INDICATED LAV 1, NO SMOKE FOUND.// NO SMOKE DETECTED, NO SMOKE INDICATED. OK FOR SERVICE PER AMM26-17-01.Feb 4, 2019 · N208HA · Airbus A321271N · Smoke DetectionSDR HALA2018121700656Igniter · malfunctionedETOPS SIGNIFICANT SYSTEM - BTB ENG 2 IGN A INOP. PERFORMED OPERATIONAL CHECK OF #2 ENGINE IGNITER "A" OPS CK NORMAL ON GROUND. OK TO CONTINUE. REF AMM 74-00-00 PB 501.Dec 14, 2018 · N208HA · Airbus A321271N · Spark Plug/IgniterSDR HALA2018111400581Fire Loop · faultedETOPS SIGNIFICANT SYSTEM - ATB - DUE TO ENG. 2 LOOP "A" FAULT. // REMOVED AND REPLACED PYLON FIRE - DETECTOR RAMP ASSEMBLY PER AMM 26-12-16. EMPLOYEE# 3752 (11/14/18). OPERATIONAL CHECK PENDING. OPS CHECK GOOD PER AMM 26-12-00-710-002, FAULT WENT AWAY AND NO DNov 13, 2018 · N208HA · Airbus A321271N · Fire Detection
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