# Service difficulty reports: N226HA A list on [N226HA](https://openairdocs.org/aircraft/N226HA.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR ASAA2026010262645](https://openairdocs.org/sdr/ASAA2026010262645.md): Smoke Warning · false activation · Jan 2, 2026 · N226HA · Airbus A321271NX · Smoke Detection > SMOKE LAVATORY SMOKE 1 HOUR PRIOR TO LANDING. NO SIGN OF SMOKE OR FIRE IN ANY LAVATORY. GROUNDED - YES. RESET CIDS SDF AND PERFORMED OPS TEST OF ALL LAVATORY SMOKE DETECTION SYSTEMS PER AMM 26-17-00. OPS TEST OK. NO FAULTS NOTED. OK FOR SVC. - [SDR HALA20251015319](https://openairdocs.org/sdr/HALA20251015319.md): Rod · damaged · Oct 14, 2025 · N226HA · Airbus A321271N · Pneumatic Distribution System > ETOPS - RETURN TO GATE AFTER ENG. START DUE TO ENG.1 BLEED FAULT. FOUND FAN AIR VALVE ACTUATOR ROD DAMAGED. REMOVED AND REPLACED ACTUATOR ROD PER AMM 36-11-54-400-803-A. OPS CHECK OF FAN AIR VALVE ACTUATION GOOD W/IDLE RUN. NO FAULTS NOTED. OK FOR SVC. - [SDR HALA20250812245](https://openairdocs.org/sdr/HALA20250812245.md): Control Valve · faulted · Aug 11, 2025 · N226HA · Airbus A321271N · Cabin Temperature Control System > DIV - 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. PER - [SDR HALA20250602157](https://openairdocs.org/sdr/HALA20250602157.md): Igniter · faulted · May 30, 2025 · N226HA · Airbus A321271N · APU Start/Ignition System > ETOPS - APU AUTO SHUT DOWN TWICE CALLED MX, SHUT DOWN THRID TIME ALSO NOTICED FUEL SLOWLY DRIPPING FROM APU DRAIN MAST. REMOVED AND REPLACD APU IGNTIER PLUG PER AMM 49-41-41 AND APU IGNITION UNIT PER AMM 49-41-38. OPS AND LEAK CHK GOOD. OK FOR SVC - [SDR HALA20250317016](https://openairdocs.org/sdr/HALA20250317016.md): Skin · corroded · Mar 14, 2025 · N226HA · Airbus A321271N · Ailerons > CORROSION FOUND ON RHW AILERON AT UPPER EXTERNAL SKIN NEAR TRAILING EDGE AREA. PERFORMED REPAIR IAW RI-HAL-57-023. DAMAGE IS RAISED TO SPEAR DUE TO NO ADL OR REPAIR. SEE SPEAR REF NO. N226HA/B4836/SPEAR001. SEE SJC NR 8027 AND NR 20005, 20006. SILVER DOT APPLI - [SDR HALA20250317015](https://openairdocs.org/sdr/HALA20250317015.md): Skin · corroded · Mar 14, 2025 · N226HA · Airbus A321271N · Wing, Plate/Skin > CORROSION FOUND ON LHW LOWER SURFACE OUTBOARD SIDE OF PYLON BETWEEN RIBS 8 AND 9. PERFORMED DAMAGE EVALUATION IAW A321N SRM 57-21-11-283-014 FIG 001 SHT 1 REV 35 DTD 01NOV24. REWORK EXTENDS OVER FASTENER HEAD, CONTACT AIRBUS. PERFORMED REPAIR IAW RI-HAL-57-022 - [SDR HALA20250204049](https://openairdocs.org/sdr/HALA20250204049.md): Fire Loop · shorted · Feb 3, 2025 · N226HA · Airbus A321271N · Fire Detection > ETOPS - ENG 1 FIRE LOOP A APPEARED DURING CLIMB AND ONCE IN FLIGHT. FOUND SHORT TO GROUND ON #1 ENGINE LOOP A HARNESS (4165KS) REMOVED & REPLACED HARNESS PER AMM 26-12-61. FDU 1 TEST OK, OK FOR SERVICE. - [SDR HALA20250127038](https://openairdocs.org/sdr/HALA20250127038.md): Fire Loop · faulted · Jan 24, 2025 · N226HA · Airbus A321271N · Fire Detection > ETOPS - DURING CLIMB, WE GOT ECAM ENG 2 FIRE LOOP A FAULT TWICE. BOTH TIMES LASTED UNDER A MINUTE AND CLEARED ON ITS OWN. PERFORMED RESISTANCE TEST PER AMM 26-12-00-810-805-A. FOUND PINS J&K 1.490O, INSULATION RES. PIN J-GRD-0.00MO PINS K TO GRD - 0.00MO. REMO - [SDR HALA20250124033](https://openairdocs.org/sdr/HALA20250124033.md): Overheat Loop · faulted · Jan 23, 2025 · N226HA · Airbus A321271N · Overheat Detection > ETOPS - INFO TO MAINT: DURING CLIMB, WE GOT ECAM ENG 2 FIRE LOOP A FAULT TWICE. BOTH TIMES LASTED UNDER A MINUTE AND CLEARED ON ITS OWN. PERFORMED RESISTANCE TEST PER AMM 26-12-00-810-805-A. FOUND PINS J&K 1.490O, INSULATION RES. PIN J-GRD-0.00MO PINS K TO GRD - [SDR HALA20241216366](https://openairdocs.org/sdr/HALA20241216366.md): Fire Loop · faulted · Dec 15, 2024 · N226HA · Airbus A321271N · Fire Detection > ETOPS - ENG 2 FIRE LOOP B FAULT. REMOVED AND REPLACED #2 ENG AGB FIURE DETECTOR B PER AMM 26-12-17-000-802-A & 26-12-17-400-802-A FAULT CLEARED AND BITE TEST PASS PER 26-12-00-710-002 AC OKAY TO CONTINUE - [SDR HALA20241125332](https://openairdocs.org/sdr/HALA20241125332.md): Oil System · leaking · Nov 24, 2024 · N226HA · Airbus A321271N · Turbine Engine Oil System > ATB - ENG 1 OIL DISCREASE DURING FLIGHT. PERFORMED INSP OF THE NO. 4 BEARING SCAVENGE OIL TUBE ASSY ( LR111) PER 772-21-01-31. REMOVED AND REPLACED OIL FILTER AND SERVICED SYSTEM PER AMM 79-21-06. PERFORMED HIGH POWER ENG RUN PER AMM 71-00-00-720-816-A. NO LEA - [SDR HALA20240913045](https://openairdocs.org/sdr/HALA20240913045.md): Smoke Detector · no discrepancy · Sep 12, 2024 · N226HA · Airbus A321271N · Smoke Detection > INFO TO MX INFLIGHT LAVATORY SMOKE ECAM MSG. NO FIRE OR SMOKE NOTED UPON INSPECTION SUSPECTED PAX VAPING. INFO NOTED BY MX, PERFORMED BITE TEST OF LAV SMOKE WARN TESTS OK, NO DEFECTS NOTED A/C OK TO CONT. REF TSM 26-17-00-710-11--A0 - [SDR HALA20240814224](https://openairdocs.org/sdr/HALA20240814224.md): Pump · low pressure · Aug 13, 2024 · N226HA · Airbus A321271N · Hydraulic Pump (Electric/Engine), Main > ETOPS - MULTIPLE HYD Y ENG 2 PUMP LO PR SPURIOUS ALERTS. REMOVED AND REPLACED ENG2 PUMP PRESSURE SWITCH PER AMM 29-13-17. LEAK CK AND OPS CHECK GOOD OK FOR SVC. - [SDR HALA20240509129](https://openairdocs.org/sdr/HALA20240509129.md): Fuel Line · leaking · May 8, 2024 · N226HA · Airbus A321271N · APU Engine Fuel and Control > ETOPS - APU FUEL LINE LEAKING NEAR AFT LOWER AREA OF APU. PN:3889352-1. IPC 49-21-84-30A ITEM #400. REPLACED APU ACTUATOR SUPPLY PIPE PN:3883952-1 PER AMM 49-32-11 & 49-23-51. OPS CHECK & LEAK CHECK OF OF APU OK. - [SDR HALA20240506123](https://openairdocs.org/sdr/HALA20240506123.md): Filter · missing · May 5, 2024 · N226HA · Airbus A321271N · Hydraulic System, Main > ETOPS - FOUND #1 GREEN HYD CASE DRAIN FILTER ASSY MISSING. INSTALLED #1 GREEEN HYD CASE DRAIN FILTER ASSY PER AMM 29-11-43-803-A. PENDING OPS AND LEAK. OPS & LEAK CHECK OK. OK FOR SVC. - [SDR HALA20240506122](https://openairdocs.org/sdr/HALA20240506122.md): Wire Harness · missing · May 4, 2024 · N226HA · Airbus A321271N · Fire Protection System Wiring > ETOPS - ENGINE 2 ESN P770479 MISSING A LOOP HARNESS 4165KS AND MISSING A LOOP ELECTRIC RAIL ASSEMBLY. INSTALLED ENGINE 2 A LOOP ELECTRIC RAMP ASSY PER AMM 26-12-61. OPS CK GOOD. - [SDR HALA20221229321](https://openairdocs.org/sdr/HALA20221229321.md): Seal · not reported · Dec 28, 2022 · N226HA · Airbus A321271N · Turbine Section > ETOPS-#2 ENG #3 BEARING AFT SEAL NESTING. - [SDR HALA2022090100254](https://openairdocs.org/sdr/HALA2022090100254.md): None · none · Aug 31, 2022 · N226HA · Airbus A321271N · Oxygen System > ETOPS - ECAM: ANTI ICE ENG 1 SYS FAULT, ENG 1 A-ICE MONG FAULT ILLUMINATED IN DESCENT 1-2 MINUTES // REMOVED AND REPLACED NAI PRESSURE TRANSDUCER (4002DN) REF AMM 30-21-23. OPS TEST GOOD. NO FAULTS NOTED. OK FOR SERVICE. - [SDR HALA2022071400130](https://openairdocs.org/sdr/HALA2022071400130.md): Wire Harness · failed · Jul 14, 2022 · N226HA · Airbus A321271N · Fuel Divider > ETOPS - ENG 2 FADEC SYS FAULT ALERT IN CRUISE. REMOVED AND REPLACED WO3 EEC WIRING HARNESS PER AMM 73-21-63. OPS CHECK GOOD. OK FOR SERVICE - [SDR HALA2022052300103](https://openairdocs.org/sdr/HALA2022052300103.md): None · none · May 18, 2022 · N226HA · Airbus A300* · Powerplant System > ETOPS - #1 ENGINE HIGH VIB - ENGINE REPLACED PER ENGINEERING REQUEST // REMOVED AND REPLACED #1 ENGINE PER HAL TASKCARD J321-72-WHI-02 - [SDR HALA2022031500077](https://openairdocs.org/sdr/HALA2022031500077.md): None · none · Mar 14, 2022 · N226HA · Airbus A321271N · Fire Detection > ETOPS - DMI # 204854 ENG 2 FIRE LOOP A FAULT ( ENGINE FIRE DETECTION SYSTEMS LOOP A (EXCEPT FOR ER OPERATIONS BEYOND 120 MINUTES, ONE MAY BE INOPERATIVE ON EACH ENGINE PROVIDED: ASSOCIATED LOOP B IS OPERATIVE / THE ENGINE FIRE TEST IS PERFORMED BEFORE EACH DE - [SDR HALA2021031800037](https://openairdocs.org/sdr/HALA2021031800037.md): Power Supply · inoperative · Mar 17, 2021 · N226HA · Airbus A321271N · Emergency Lighting > EMER EQ - FOUND EMEREGENCY LIGHT SWITCH IN THE ARM POSIOTION WITH NO POWER TO AIRCRAFT. NUMERIOUS EMR LIGHTS THROUGHOUT CABIN INOP. // REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (EPSU) BATTERIES PER AMM 33-51-38. BITE TESE PASSED. OPS CHK GOOD. OK FOR SE - [SDR HALA2021020800013](https://openairdocs.org/sdr/HALA2021020800013.md): Balance Weight · out of balance · Feb 5, 2021 · N226HA · Airbus A321271N · Turbine Engine Air Inlet Section > ETOPS - #2 N1, HIGH VIBRATION DURING FUNCTION TEST. AMM 71-00-00-710-807-A // REMOVED AND INSTALLED FAN TRIM BALANCE (CA) WEIGHTS AT LOCATIONS 11,13,15 AND 19 AND C2 WEIGHT AT LOCATION 17 (5897) FUNCTION TEST (FAN TRIM BALANCE) PENDING. PERFORMED #2 ENG FUNCT - [SDR HALA2021011900006](https://openairdocs.org/sdr/HALA2021011900006.md): Flow Divider · loose · Jan 18, 2021 · N226HA · Airbus A321271N · Engine Fuel Distribution > ETOPS, NR 2 ENGINE HAS FUEL LEAK. FOUND FUEL LINE FROM FLOW DIVIDER LOOSE, TIGHTENED LINE. GROUND RUN AND LEAK CHECK OK. OK FOR SERVICE. - [SDR HALA2021011200004](https://openairdocs.org/sdr/HALA2021011200004.md): Sensor · defective · Jan 9, 2021 · N226HA · Airbus A321271N · Pneumatic Distribution System > ETOPS, AIR BLEED CLASS 2 ON ECAM PAGE. REMOVED & REPLACED DELTA PRESSURE SENSOR (18HA2), PER AMM 36-11-18. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'N226HA' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N226HA/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.