# Service difficulty reports: N227HA

A list on [N227HA](https://openairdocs.org/aircraft/N227HA.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR ASAA2026062765513](https://openairdocs.org/sdr/ASAA2026062765513.md): Battery · unserviceable · Jun 27, 2026 · N227HA · Airbus A321271N · Emergency Lighting
  > EPSU BAT (15WL) FAIL. GROUNDED - YES. REMOVED AND REPLACED EPSU BATTERY (15WL) IAW AMM 33-51-38. BITE TEST OK. OK FOR SBC..
- [SDR HALA20251002298](https://openairdocs.org/sdr/HALA20251002298.md): Igniter · damaged · Oct 1, 2025 · N227HA · Airbus A321271N · Spark Plug/Igniter
  > ETOPS - 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.
- [SDR HALA20250509026](https://openairdocs.org/sdr/HALA20250509026.md): Smoke Detector · false activation · May 6, 2025 · N227HA · Airbus A321271N · Fire Detection
  > SMOKE LAVATORY SMOKE LAV D. FA REPORTED ALL CLEAR. PERFORMED OPERATIONAL CHECK OF THE LAV SMOKE DETECTION PER AMM 26-17-00-710-001-A. OPS CHECK GOOD. NO FAULTS NOTED. A/C OK TO CONTINUE
- [SDR HALA20250314011](https://openairdocs.org/sdr/HALA20250314011.md): Radome · damaged · Mar 12, 2025 · N227HA · Airbus A321271N · Aerodynamic Fairings
  > POSSIBLE BIRD STRIKE DESCENDING BETWEEN 6-5000 FEET. REMOVED & REPLACED RADOME PER AMM 53-15-11. OK FOR SERVICE.
- [SDR HALA20250115020](https://openairdocs.org/sdr/HALA20250115020.md): B-Nut · damaged · Jan 14, 2025 · N227HA · Airbus A321271N · Engine Fuel and Control
  > ETOPS - WHILE PERFORMING E1128-321-73-019 FOUND AS11 TUBE B-NUT CROSS THREADED ON #2 ENGINE BURNER PRESSURE (PB) SENSOR. REMOVED & REPLACED AS11 TUBE PER AMM 73-21-23.
- [SDR HALA20241230386](https://openairdocs.org/sdr/HALA20241230386.md): Ignition Sys · malfunctioned · Dec 28, 2024 · N227HA · Airbus A321271N · APU Start/Ignition System
  > ETOPS - ECAM APU AUTO SHUTDOWN ON START ATTEMPT 3 UNSUCCESSFUL START ATTEMPTS. REMOVED AND REPLACED IGNITION UNIT PER A321 AMM 49-41-38 ECB TEST OK OPS CHECK NORMAL A/C OK FOR SERVICE
- [SDR HALA20241226380](https://openairdocs.org/sdr/HALA20241226380.md): Bolt · broken · Dec 25, 2024 · N227HA · Airbus A321271N · Pneumatic Distribution System
  > ETOPS - ECAM AIR ENG 2 BLEED FAULT ON REVERSE THRUST SELECTION ON LANDING. FOUND FAN AIR VALVE ACTUATOR ROD BOLT BROKEN, REPLACED BOLT IN REFERENCE TO AMM 36-11-54-400-802-A, ACCOMPLISHED ENG RUN CHECK PER AMM 71-00-00-860-823-A, NO DEFECTS NOTED ON GROUND, AL
- [SDR HALA20241216367](https://openairdocs.org/sdr/HALA20241216367.md): Regulator Valve · faulted · Dec 14, 2024 · N227HA · Airbus A321271N · Pneumatic Distribution System
  > ETOPS - AIR ENG 2 ABNORM PR ON THRUST LVR ADVANCE ON TO W/ RTO SYSTEM RESET SUCCESSFUL. FOUND PRESSURE REGULATING VALVE (PRV) FAULTING. REMOVED AND REPLACED PRV PER AMM 36-11-52-000-802-A/400-802-A. OPS AND LEAK CHECK GOOD. OK FOR SVC.
- [SDR HALA20241212362](https://openairdocs.org/sdr/HALA20241212362.md): Bleed Valve · faulted · Dec 11, 2024 · N227HA · Airbus A321271N · Compressor Bleed Valve
  > DIV - AIR ENG 2 BLEED FAULT DURING CLIMB. ACCOMPLISHED GVI OF #2 ENG BLEED VALVES. FOUND FAV ACTUATRO ROD BROKEN. REMOVED FAV PER AMM 36-11-54. INSTALLED FAN AIR VALVE ON ENG 2 PER AMM 36-11-54. OPS/BITE/LEAK CHECK GOOD.
- [SDR HALA20241028301](https://openairdocs.org/sdr/HALA20241028301.md): Seal · damaged · Oct 26, 2024 · N227HA · Airbus A321271N · Engine Thrust Reverser
  > ETOPS - DURING VISUAL INSPECTION OF THE THRUST REVERSERS FIRE SEAL AND VAPOR BARRIER SEALS T/C: 321-783200-W3-1, FOUND 2 FIRE SEALS DAMAGED. REMOVED AND REPLACED BOTH FIRE SEALS PER IPC: 78-32-05-75 ITEM NUMBER 240, 350. OK TO CONTINUE SERVICE.
- [SDR HALA20240722195](https://openairdocs.org/sdr/HALA20240722195.md): Clamp · leaking · Jul 17, 2024 · N227HA · Airbus A321271N · Cabin Cooling System
  > ETOPS - DURING TAXI IN, APU BLEED SELECTED ON TO CONFIRM PACKS 10 MINS AFTER SELECTING ON, OBSERVED AN INTENSE BURING ASPHALT/CHEMICAL ODOR IDENTICAL TO PREVIOUS TEST FLIGHTS. REMOVED #2 RT OZONE FILTER IAW AMM 21-51-41 TO FOM FOUND CONTAMINATED. INSTALLED #2
- [SDR HALA20240716193](https://openairdocs.org/sdr/HALA20240716193.md): Duct · contaminated · Jul 15, 2024 · N227HA · Airbus A321271N · Pneumatic System
  > ATB - AFTER TAKEOFF PRIOR TO THRUST REDUCTION, BURNING ELECTRICAL AND CHEMICAL SMELL OBSERVED IN THE COCKPIT. TAKEOFF THRUST WAS TOGA. PERFORMED DECONTAINATION OF THE BLEED AIR DUCTS LEVEL C AMM 36-10-00-615-806-A. NO BURNING SMELL WHEN PACKS 1 AND 2 ON AND OF
- [SDR HALA20240510023](https://openairdocs.org/sdr/HALA20240510023.md): Smoke Detector · inoperative · May 9, 2024 · N227HA · Airbus A321271N · Smoke Detection
  > LAV E SMOKE DETECTOR INOP. REMOVED AND REPLACED SMOKE DETECTOR AT LAV E PER AMM 26-17-15-400-807-A.OPS CHECK GOOD OK FOR SERVICE.
- [SDR HALA20240311064](https://openairdocs.org/sdr/HALA20240311064.md): Warning Light · illuminated · Mar 9, 2024 · N227HA · Airbus A321271N · AC Generator-Alternator
  > ETOPS-ON ARRIVAL DESENDING THRU 12,000 ECAM GEN 2 FAULT. COMPLETE ECAM ACTIONS GEN 2 FAULT STILL ILLUMINATED. STARTED APU. REMOVED AND REPLACED RH IDG IAW AMM 24-21-51-400-803-A UP TO AND INCLUDING STAEP 4. A. (15) (H). 12570/25041, 03/08/24.. NEED TO CONTINUE
- [SDR HALA20240212040](https://openairdocs.org/sdr/HALA20240212040.md): Line · punctured · Feb 11, 2024 · N227HA · Airbus A321271N · Hydraulic System, Main
  > ETOPS - #1 ENGINE EDP SUCTION LINE FOUND TO HAVE PUNCTURE/LEAKING. REMOVED AND REPLACED #1 ENGINE EDP SUCTION LINE PER AMM 29-11-51-400. LEAK CHECKED, OPS CHECKED. NO DEFECTS NOTED. OK FOR SERVICE.
- [SDR HALA20240125029](https://openairdocs.org/sdr/HALA20240125029.md): Sensor · faulted · Jan 24, 2024 · N227HA · Airbus A321271N · Engine Oil System (Airframe Furnished)
  > ETOPS - ENG 1 N1 AND N2 VIB DISPLAY LOST FOR 30 MIN IN FLT, CAME BACK. (SEEMED TO CORRESPOND WITH ENG I OIL SENSOR FAULT ECAM, WHICH IS MEL'D) REMOVED PHMU PER AMM 77-31-01-000-801-AAND INSTALLED PER AMM 77-31-0-400-801-A. RAN EEC OPERATION TEST PER TASK 7 3-2
- [SDR HALA20231109242](https://openairdocs.org/sdr/HALA20231109242.md): Unknown · unknown · Nov 9, 2023 · N227HA · Airbus A321271N · Fuel Controlling System
  > ETOPS - AFTER BOTH ENG STARTS (2&1) GOT ECAM: ENG 2 EIU FAULT. DID QRH RESET PROCEDURE ECAM CLRD. OPS NORM. ACCOMPLISHED BITE TEST OF EIU 1 & 2 PER AMM 73-25-34. NO FAULTS FOUND. OK TO CONTINUE SERVICE. REMOVED AND REPLACED (6KS) SWITCH PER AWM 73-25-34 AS P
- [SDR HALA20231016224](https://openairdocs.org/sdr/HALA20231016224.md): Eiu · faulty · Oct 15, 2023 · N227HA · Airbus A321271N · Fuel Controlling System
  > ETOPS - RECIEVED FAULT MESSAGE EIU2-008-ENGINE START FAULT. REMOVED AND REPLACED EIU-2 PER AMM 73-25-34 OPS AND SECURITY CHECK GOOD OK FOR SERVICE
- [SDR HALA20240712189](https://openairdocs.org/sdr/HALA20240712189.md): Brake Assy · unknown · Jul 11, 2023 · N227HA · Airbus A321271N · Landing Gear Brake System
  > AFTER TOUCHDOWN, LOSS OF BRAKES WITH AUTOBRAKES ON LOW. PERFORM TSM 32-42-00-810-919-A, NO FAULTS PRESENT. PERFORM AMM TASK 32-42-00-710-001-A, ALL RESULTS AS INDICATED IN REFERENCE. OK TO CONTINUE SERVICE.
- [SDR HALA2023020600002](https://openairdocs.org/sdr/HALA2023020600002.md): Not Reported · not reported · Feb 5, 2023 · N227HA · Airbus A321271N · Fire Protection System
  > LAV SMOKE WARNING IN FLIGHT. PERFORMED LAVATORY SMOKE TEST IAW TSM 26-17-00-810-804-A. TEST PASSED, OPS CHECK GOOD. NO DEFECTS NOTED. A/C OK TO CONTINUE.
- [SDR HALA2022030400067](https://openairdocs.org/sdr/HALA2022030400067.md): None · none · Mar 3, 2022 · N227HA · Airbus A321271N · APU Start/Ignition System
  > ETOPS - APU WILL NOT START // REMOVED AND REPLACED EXCITER-IGNITION PER AMM 49-41-38 OPS TEST OK. OK FOR SERVICE
- [SDR HALA2021080300093](https://openairdocs.org/sdr/HALA2021080300093.md): Fire Loop · faulted · Aug 2, 2021 · N227HA · Airbus A321271N · Fire Detection
  > ETOPS - ENG 2 FIRE LOOP B FAULT DISPLAYED NUMEROUS TIMES DURING CRUISE // PERFORMED TSM 26-12-00-810-806-A. MEASURE OHMS 1472 OHMS, VISUAL INSP TERMINAL BLOCK 2WD-D (450VT2). NO DEFECTS NOTED. REMOVED AND REPLACED FIRE LOOP B AT PYLON & REMOVED AND REPLACED FI
- [SDR HALA2021072900091](https://openairdocs.org/sdr/HALA2021072900091.md): Wire Harness · malfunctioned · Jul 29, 2021 · N227HA · Airbus A321271N · Fire Protection System Wiring
  > ETOPS - ENG 2 FIRE LOOP B FAULT CAME ON FOR 30 SECONDS. T/S PER A321 TSM 26-12-00-810-806-A. PERFORMED OP TEST ENG FIRE & OVERHEAT DET & SAME ALL TEST OK. PERFORMED GVI OF ENG 2 FIRE DET SYS IAW ESPM CH 20 & ENG 2. NEED HARNESS FIN 4166KS (DL304822). REMO
- [SDR HALA2020113000214](https://openairdocs.org/sdr/HALA2020113000214.md): Anti-Ice Valve · defective · Nov 27, 2020 · N227HA · Airbus A321271N · Engine Anti-Icing System
  > ETOPS-ANTI-ICE ENGINE 2 VALVE CLOSED. ECAM AND OVERHEAD AMBER FAULT. FAULT DID NOT CLEAR. REMOVED AND REPLACED ENGINE 2 UPPER ANTI-ICE VALVE, PER AMM 30-21-51. OPERATIONS CHECK GOOD. SECURITY AND CONDITION CHECK OK. MESSAGE CLEARED, NO FAULTS NOTED. A/C
- [SDR HALA2020031100059](https://openairdocs.org/sdr/HALA2020031100059.md): Eec · malfunctioned · Mar 10, 2020 · N227HA · Airbus A321271N · Fuel Control/Turbine Engines
  > ETOPS SIGNIFICANT SYSTEM - BTB - ECAM: ENG 2 FADEC SYS FAULT FOLLOWED BY ENG 2 MINOR FAULT OIL CHIP DETECTED. // INSTALLED NEW PHMU ON #2 ENG, CONDITION SAME. RE-INSTALLED ORIGINAL PHMU PER AMM 77-31-01. REMOVED AND REPLACED #2 EEC PER AMM 73-21-01. LAND TEST
- [SDR HALA2019122300527](https://openairdocs.org/sdr/HALA2019122300527.md): Unknown · odor · Dec 23, 2019 · N227HA · Airbus A321271N · Air Distribution System
  > AT 1250Z A GARBAGE TYPE ODOR STARTED IN THE CABIN AND INCREASED FOR THE NEXT TEN MINUTES. ONE PASSENGER FELT ILL, AT FIRST, THE SMELL WAS IN CABIN. IT LATER DISAPPEARED. NOTED BY MX. OK TO CONTINUE.

## 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 = 'N227HA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N227HA/reports

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