N220HA

Service difficulty reports · 34

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 = 'N220HA' 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 HALA20251020323Skin · dentedETOPS - NR 2 ENGINE INLET DENT OUT OF LIMITS. REMOVED AND REPLACE NR 2 ENGINE INLET COWL PER AMM 71-61-10. RAN ENGINE PERFOM ANTI ICE LEAK CHECK PER AMM 30-31-00.LEAK CHECK OK OK ,NO DEFECT NOTED OK TO CONTINUE FOR SERVICE.Oct 17, 2025 · N220HA · Airbus A321271N · Engine Air Intake SystemSDR HALA20251013313Fire Loop · faultedETOPS - ENG 2 FIRE LOOP A FAULT. REMOVED & REPLACED LOOP A FIRE HARNESS PER AMM 26-12-61. OPERATIONAL CHECK OK.Oct 10, 2025 · N220HA · Airbus A321271N · Fire DetectionSDR 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 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 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 HALA20240620164Sensor · faultedETOPS - ENG2 OIL SENSOR FAULT ECAM CAME ON DURING ENGINE 2 START AND WENT AWAY JUST BEFORE COMPLETING ENGINE 2 START. DUE TO REPEAT WRITE- UP OF ENG 2 OIL SENSOR FAULT NEED TO REPLACE PHMU. FOUND INTERNAL FAULT/ SNSR INTERFACE FAIL CODE 773101. REOMVED AND REPJun 18, 2024 · N220HA · Airbus A321271N · Engine Oil PressureSDR HALA20240617161Clevis · faultedETOPS - ENG 1 BLEED FAULT AFTER ENG START. REMOVED AND REPLACED CLEVIS AND SCREW PIN OF ELECTROPNEUMATIC ACTUATOR ON ENG1 PERFORMED OPS TEST OF BMC 1 TEST PASSED. PERFORMED ENG RUN OF ENG 1 NO ECAM MESSAGES ENG RUN GOOD OK TO CONTINUE PER AMM 36-11-504-400-802Jun 16, 2024 · N220HA · Airbus A321271N · Pneumatic Distribution SystemSDR HALA20240520138Fire Loop · faultedETOPS - BTB ENG 1 FIRE LOOP A FAULT ILLUMINATED RIGHT BEFORE T.O. LOW SPEED ABORT. PERFORMED ENG #1 LOOP A WIRE CHK, CONTINUITY CHK OK. NO SHORTS TO GND. BITE CHK OF FDU #1 LAST LEG REPORT FOUND 26-12-00 CHK FDU ENG 1 CHAN B SUPPLY, 26-12-00 CHK FDU ENG 1 LOOPMay 19, 2024 · N220HA · Airbus A321271N · Fire DetectionSDR HALA20240517134Wire Harness · faultedETOPS - ENG 1 FIRE LOOP A FAULT. REMOVED AND REPLACED ENG 1 FIRELOOP A HARNESS (4165KS) PER AMM 26-12-400-802-A. OPS TEST AND BITE TEST GOOD. OK FOR SVC.May 16, 2024 · N220HA · Airbus A321271N · Fire Protection System WiringSDR HALA20240422106Fire Loop · faultedETOPS - ENGINE 2 FIRE LOOP B FAULT. CHECK WIRES FROM ENG 2 FDU PLUG B, J AND K SHORTING TO GROUND PER AWM 26-12-08. DISCONNECTED 41WD2 & 42WD2 FROM (4WD2) PYLON DETECTOR. CONTINUITY & INSULATION CHECK OF 4WD2 GOOD. FOUND 41WD2 & 42WD2 INTERMITTENT SHORTING TO Apr 19, 2024 · N220HA · Airbus A321271N · Fire DetectionSDR HALA20240422105Fire Loop · faultedETOPS - ENGINE 2 FIRE LOOP A FAULT. CHECK ENGINE WIRE FROM FDU2 "A" PLUG J AND K SHORTING TO GROUND. REMOVED WIRES 2612-277 AND 2612-276 FROM TERMINAL BLOCK 450VT2. SHORT TO GROUND STILL PRESENT. RECONNECTED WIRE 2612-277 AND 2612-276 TO TERMINAL BLOCK 450VT2 Apr 19, 2024 · N220HA · Airbus A321271N · Fire DetectionSDR HALA20240422104Fire Loop · faultedETOPS - ENGINE 1 FIRE LOOP A FAULT. T/S ENG 1 CHECK WIRE FROM FDU 1 LOOP A, J AND K SHORTING TO GROUND. PER AWM 26-12-05. FOUND WNVRN12 (4181KS) INTERMITTENT. REMOVED LOOP A FIRE DETECTOR CABLES PER AMM 26-12-61.(3752). CONTINUE ON LOG PG # 1047623 ITEM 2. INApr 19, 2024 · N220HA · Airbus A321271N · Fire DetectionSDR HALA20240417102Wire · corrodedETOPS - FOUND CORROSION AND NICK ON ENG 1 FIRE LOOP A HARDWIRE (4182KS). REMOVED & REPLACED ENG 1 LOOP A ASSY. PER AMM 26-12-61-400-807-A. OPERATIONAL CHECK OK PER AMM 26-12-00Apr 16, 2024 · N220HA · Airbus A321271N · Fire Protection System WiringSDR HALA20240417101Wire · shortedETOPS - ENG 1 FIRE LOOP B FAULT. FOUND WIRE HARNESS (41WD1) SHORTING TO GND 3.9M OHMS. FOUND DETECTOR (4WD1) SHORTING TO GND 5.2M OHMS. REMOVED AND REPLACED HARDWIRE (41WD1) PER WDM 26-12-07. REMOVED AND REPLACED ENG 1 PLYON LOOP B (4WD1) PER AMM 26-12-16-000-Apr 16, 2024 · N220HA · Airbus A321271N · Fire Protection System WiringSDR HALA20240417100Fire Loop · shortedETOPS - ENG 1 FIRE LOOP A FAULT. FOUND WIRE HARNESS (4165KS) SHORTING TO GND 1.8M OHMS. FOUND WIRE HARNESS (4181KS WHT) SHORTING TO GND 1.2M OHMS. REMOVED AND REPLACED WIRE HARNESS. WDM 71-51-75 PAGE 3. PENDING OPS CHECK. PER AMM 26-12-61 & 26-12-61 FOR 4181KSApr 16, 2024 · N220HA · Airbus A321271N · Fire DetectionSDR HALA20240417099Wire Harness · shortedETOPS - ENG 2 FIRE LOOP A FAULT. REMOVED AND REPLACED ENG 2 FIRE LOOP A, WNVRN12 (4181KS) PER WDM 71-51-75. PENDING OPS CHECK. OPS CHECK FAILED. FOUND WIRE HARNESS LOOP A ( 31WD2 & 32WD2) SHORTING TO GND. REMOVED & REPLACED 31WD2 & 32WD2 PER AMM 26-12-36. OPERApr 16, 2024 · N220HA · Airbus A321271N · Fire Protection System WiringSDR HALA20240415096Fire Loop · faultedETOPS - AFTER HPR ENG 2 FIRE LOOP B FAULT. FOUND PYLON RAMP ASSY NO GOOD AND 4002WD2 ELEMENT SHORTING TO GROUND. NEED TO BE REPLACED. REMOVED & REPLACED AGB 4002WD2 DETECTOR PER AMM 26-12-17. REMOVED AND REPLACED #2 ENGINE PYLON FIRE-DETECTOR RAMP ASSEMBLY PERApr 14, 2024 · N220HA · Airbus A321271N · Fire DetectionSDR HALA20240415095Fire Loop · faultedETOPS - ENG2 FIRELOOP A FAULT. REMOVED AND REPLACED ENG2 LOOP A FIRE HARNESS (4165KS) PER AMM 26-12-61. BITE TEST GOOD.Apr 13, 2024 · N220HA · Airbus A321271N · Fire DetectionSDR HALA20240415094Control Unit · faultedETOPS - FUEL OVERFLOW PROT FAULT. FUEL IDG 1 COOL FAULT. (POSSIBLE FUEL LEVEL SENSE CONTROL UNIT 1). REMOVED & REPLACED FLSCU1. CONDITION SAME. REINSTALLED ORIGINAL COMPUTER. NEED FURTHER TROUBLESHOOTING/WIRE CHECKS PER TSM 28-46-00-810-812-A. REPLACED OVApr 13, 2024 · N220HA · Airbus A321271N · Fuel Indicating SystemSDR HALA20240415093Fire Loop · faultedETOPS - ENG 1 LOOP A FAULT. REMOVED AND REPLACED ENG #1 AGB LOOP A DETECTOR (4002WD1) OER AMM 26-12-17. OPS CHECK GOOD. OK FOR SVCApr 13, 2024 · N220HA · Airbus A321271N · Fire DetectionSDR HALA20240412092Accumulator · rupturedETOPS - DURING SYSTEM ACCUMULATOR SERVICEING FOUND GREEN SYSTEM ACCUMULATOR (1070GM) RUPTURE DAIAPHRAM. INOP. REPLACED GREEN HYDRAULIC SYS ACCUM & GAGE REF. AMM 29-11-42. OPS CHECK LEAK CHECK GOOD. OK FOR SVC.Apr 11, 2024 · N220HA · Airbus A321271N · Hydraulic Indicating SystemSDR HALA20240410089Duct · damagedETOPS - #2 ENG PYLON ECS INTERFACE DUCT PN 636D0005-527 DAMAGED. INSTALLED #2 ENG ECS INTERFACE DUCT PER AMM 36-11-49. 17934 OPS LEAK CHK PENDING. LEAK CK COVERED IN CARD 321-72-HWI-02.Apr 9, 2024 · N220HA · Airbus A321271N · Pneumatic SystemSDR HALA2023031400042Blade · damagedETOPS - DMI# 206651 ENG #1 BLADE TIP 17 MISSING POLYURETHANE COATING. ENG CHANGED REF CARD 321-72-HWI-02 MIC UPDATED PLACARD REMOVED. ORIGINAL SUBMISSION DATE: 3/15/2023.Mar 13, 2023 · N220HA · Airbus A321271N · Turbine Engine Air Inlet SectionSDR HALA2023030900036Decoder/Encoder · faultyATB - TOILETS NOT FLUSHING IN FLIGHT. WASTE SENSOR SHOWS FULL. REPLACED REF AMM 38-31-63. COND SAME. SWAPPED BACK. REPLACED DEU B (300RH7) REF AMM 23-73-47. TOILET CHECKS GOOD. OK FOR SERVICE.Mar 8, 2023 · N220HA · Airbus A321271N · Waste Disposal SystemSDR HALA2022072500135None · noneATB - ECAM AIRBORNE AIR ENG 1 BLEED FAULT // INSPECTION OF ENG 1 FAN AIR VALVE C/O IAW AMM 36-11-54. FOUND ROD ASSY & SCREW DAMAGED, ITEM 10 & 30 OF IPC 36-11-54-02. R&R ENG 'FAN AIR VALVE' PER AMM 36-11-54-00-803-A & 3611-54-400-803-A AND PERFORMED ENG RUN IAJul 23, 2022 · N220HA · Airbus A321271N · Pneumatic SystemSDR HALA2022031600078None · noneETOPS - WHILE TROUBLESHOOTING DMI # 204842 (REF. LOGPAGE 873976) FOUND #2 ENGINE HPV PYLON SENSE LINE CROSS THREADED & SEIZED ON ECS MID Y DUCT ADAPTER BLEED AIR LEAKING FROM SENSE LINE B NUT. // REPLACED HPV PYLON SENSE LINE AND ADAPTER TO ECS Y DUCT. REF AMMMar 15, 2022 · N220HA · Airbus A321271N · Pneumatic Distribution SystemSDR HALA2021101200136Fire Loop · false indicationETOPS - ENG 1 LOOP A FAULT // T/S IAW TSM 26-12-00-803-A. R&R ENG 1 PYLON LOOP A FIRE DETECTOR WITH OPS CHECK GOOD AND NO FAULTS NOTED. A/C OF TO CONTINUE. R&R IAW AMM 26-12-16-00-802A.Oct 8, 2021 · N220HA · Airbus A321271N · Fire DetectionSDR HALA2021072900090Igniter · failedETOPS - WHILE TAXING IN AFTER LANDING APU ABORTED ITS START ECAM MESSAGE APU FAULT // REMOVED AND INSTALLED EGNITER PLUG IAW 49-11-41, REMOVED AND INSTALLED ELECTRICAL LEAD IAW 49-11-43 , REMOVED AND INSTALLED IGNITION UNIT 49-41-39 PERFORMED OPERATION TEST OJul 30, 2021 · N220HA · Airbus A321271N · APU Start/Ignition SystemSDR HALA2021042600051Oil System · contaminatedETOPS - ENG #1 OIL CHIP DETECT. PERFORMED TSM 79-35-00-810-808-A, FOUND NO CONTAMINATION ON CHIP DETECTORS. PER POWERPLANT ENGINEERING REPLACED OIL FILTER ELEMENT PER AMM 79-21-06-960-801-A AND REPLACED ENGINE NR1 OIL PER AMM 79-00-00-610-802-A. PERFORMED ENApr 25, 2021 · N220HA · Airbus A321271N · Turbine Engine Oil SystemSDR HALA2021040500041Screw · failedETOPS - SCREW SNAPPED IN LH ENG OIL CONTROL MODULE // REMOVED STRIPPED FASTENER AND HELICOIL, REPLACED PER AIRBUS 321 AMM 70-24-00-910-803-AApr 4, 2021 · N220HA · Airbus A321271N · Engine Oil System (Airframe Furnished)SDR HALA2020123100231Battery · defectiveEMERGENCY EQUIPMENT ON SERVICE CHECK CARD ITEM 10, OPERATIONAL CHECK OF EMERGENCY LIGHTS, TEST SHOWS FAULT MESSAGE: 256241- ESCAPE SLIDE LIGHT/ EPSU (13WL) AFT L- SCOURCE: CIDS 1-CLASS 1. REPLACED BATTERY IN FIN 13WL EPSU, PER AMM 33-51-38. CONDITION SAME. Dec 30, 2020 · N220HA · Airbus A321271N · Emergency LightingSDR HALA2019111900491Smoke Warning · false activationSMOKE LAVATORY SMOKE ON POST FLIGHT REPORT. // PERFORMED T/S IAW TSM 26-17-00-810-804-A. NO FAULTS DETECTED. OK FOR SERVICE.Nov 18, 2019 · N220HA · Airbus A321271N · Smoke DetectionSDR HALA2019110200465Life Raft · low pressureSUP - LIFE RAFT RESERVOIR PRESSURE AT 2650 PSI, FERRY FLIGHT REQUIRED. // REMOVED AND REPLACED LIFE RAFT PER AMM 25-66-41. SECURITY CHECK GOODNov 2, 2019 · N220HA · Airbus A321271N · Life RaftSDR HALA2019090300360Eec · malfunctionedETOPS SIGNIFICANT SYSTEM - ENG 2 FADEC SYS FAULT. REMOVED AND REPLACED EEC ENG 2 IAW AMM 73-21-01 PB 401. OPS CHECK NORMAL. NO FAULTS NOTED AT THIS TIME. A/C OK FOR SERVICE.Aug 29, 2019 · N220HA · Airbus A321271N · Fuel Control/Turbine Engines
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