# Service difficulty reports: N220HA

A list on [N220HA](https://openairdocs.org/aircraft/N220HA.md).

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

- [SDR HALA20251020323](https://openairdocs.org/sdr/HALA20251020323.md): Skin · dented · Oct 17, 2025 · N220HA · Airbus A321271N · Engine Air Intake System
  > ETOPS - 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.
- [SDR HALA20251013313](https://openairdocs.org/sdr/HALA20251013313.md): Fire Loop · faulted · Oct 10, 2025 · N220HA · Airbus A321271N · Fire Detection
  > ETOPS - ENG 2 FIRE LOOP A FAULT. REMOVED & REPLACED LOOP A FIRE HARNESS PER AMM 26-12-61. OPERATIONAL CHECK OK.
- [SDR HALA20251003301](https://openairdocs.org/sdr/HALA20251003301.md): Button · cracked · Oct 2, 2025 · N220HA · Airbus A321271N · Indicating/Recording System
  > ETOPS - CAPTAIN FD PUSH BUTTON, ON GLARESHIELD CRACKED. REMOVED AND REPLACED FCU PER AMM 22-81-12. OPS CHECK GOOD. NO DEFECTS NOTED. OK TO CONTINUE
- [SDR HALA20250829264](https://openairdocs.org/sdr/HALA20250829264.md): Fuel Cap · missing · Aug 28, 2025 · N220HA · Airbus A321271N · Fuel Storage
  > ETOPS - DURING WALKAROUND FOUND RIGHT WING MISSING FUEL CAP. REPLACED RIGHT WING FUEL COUPLING PER AMM 28-25-41. OK FOR SVC.
- [SDR HALA20250818250](https://openairdocs.org/sdr/HALA20250818250.md): Jumper · worn · Aug 15, 2025 · N220HA · Airbus A321271N · Nacelle/Pylon System Wiring
  > ETOPS - 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
- [SDR HALA20240620164](https://openairdocs.org/sdr/HALA20240620164.md): Sensor · faulted · Jun 18, 2024 · N220HA · Airbus A321271N · Engine Oil Pressure
  > ETOPS - 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 REP
- [SDR HALA20240617161](https://openairdocs.org/sdr/HALA20240617161.md): Clevis · faulted · Jun 16, 2024 · N220HA · Airbus A321271N · Pneumatic Distribution System
  > ETOPS - 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 36-11-504-400-802
- [SDR HALA20240520138](https://openairdocs.org/sdr/HALA20240520138.md): Fire Loop · faulted · May 19, 2024 · N220HA · Airbus A321271N · Fire Detection
  > ETOPS - 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 LOOP
- [SDR HALA20240517134](https://openairdocs.org/sdr/HALA20240517134.md): Wire Harness · faulted · May 16, 2024 · N220HA · Airbus A321271N · Fire Protection System Wiring
  > ETOPS - 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.
- [SDR HALA20240422106](https://openairdocs.org/sdr/HALA20240422106.md): Fire Loop · faulted · Apr 19, 2024 · N220HA · Airbus A321271N · Fire Detection
  > ETOPS - 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
- [SDR HALA20240422105](https://openairdocs.org/sdr/HALA20240422105.md): Fire Loop · faulted · Apr 19, 2024 · N220HA · Airbus A321271N · Fire Detection
  > ETOPS - 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
- [SDR HALA20240422104](https://openairdocs.org/sdr/HALA20240422104.md): Fire Loop · faulted · Apr 19, 2024 · N220HA · Airbus A321271N · Fire Detection
  > ETOPS - 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. IN
- [SDR HALA20240417102](https://openairdocs.org/sdr/HALA20240417102.md): Wire · corroded · Apr 16, 2024 · N220HA · Airbus A321271N · Fire Protection System Wiring
  > ETOPS - 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 26-12-00
- [SDR HALA20240417101](https://openairdocs.org/sdr/HALA20240417101.md): Wire · shorted · Apr 16, 2024 · N220HA · Airbus A321271N · Fire Protection System Wiring
  > ETOPS - 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-
- [SDR HALA20240417100](https://openairdocs.org/sdr/HALA20240417100.md): Fire Loop · shorted · Apr 16, 2024 · N220HA · Airbus A321271N · Fire Detection
  > ETOPS - 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 4181KS
- [SDR HALA20240417099](https://openairdocs.org/sdr/HALA20240417099.md): Wire Harness · shorted · Apr 16, 2024 · N220HA · Airbus A321271N · Fire Protection System Wiring
  > ETOPS - 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. OPER
- [SDR HALA20240415096](https://openairdocs.org/sdr/HALA20240415096.md): Fire Loop · faulted · Apr 14, 2024 · N220HA · Airbus A321271N · Fire Detection
  > ETOPS - 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 PER
- [SDR HALA20240415095](https://openairdocs.org/sdr/HALA20240415095.md): Fire Loop · faulted · Apr 13, 2024 · N220HA · Airbus A321271N · Fire Detection
  > ETOPS - ENG2 FIRELOOP A FAULT. REMOVED AND REPLACED ENG2 LOOP A FIRE HARNESS (4165KS) PER AMM 26-12-61. BITE TEST GOOD.
- [SDR HALA20240415094](https://openairdocs.org/sdr/HALA20240415094.md): Control Unit · faulted · Apr 13, 2024 · N220HA · Airbus A321271N · Fuel Indicating System
  > ETOPS - 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 OV
- [SDR HALA20240415093](https://openairdocs.org/sdr/HALA20240415093.md): Fire Loop · faulted · Apr 13, 2024 · N220HA · Airbus A321271N · Fire Detection
  > ETOPS - 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 SVC
- [SDR HALA20240412092](https://openairdocs.org/sdr/HALA20240412092.md): Accumulator · ruptured · Apr 11, 2024 · N220HA · Airbus A321271N · Hydraulic Indicating System
  > ETOPS - 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.
- [SDR HALA20240410089](https://openairdocs.org/sdr/HALA20240410089.md): Duct · damaged · Apr 9, 2024 · N220HA · Airbus A321271N · Pneumatic System
  > ETOPS - #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.
- [SDR HALA2023031400042](https://openairdocs.org/sdr/HALA2023031400042.md): Blade · damaged · Mar 13, 2023 · N220HA · Airbus A321271N · Turbine Engine Air Inlet Section
  > ETOPS - 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.
- [SDR HALA2023030900036](https://openairdocs.org/sdr/HALA2023030900036.md): Decoder/Encoder · faulty · Mar 8, 2023 · N220HA · Airbus A321271N · Waste Disposal System
  > ATB - 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.
- [SDR HALA2022072500135](https://openairdocs.org/sdr/HALA2022072500135.md): None · none · Jul 23, 2022 · N220HA · Airbus A321271N · Pneumatic System
  > ATB - 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 IA
- [SDR HALA2022031600078](https://openairdocs.org/sdr/HALA2022031600078.md): None · none · Mar 15, 2022 · N220HA · Airbus A321271N · Pneumatic Distribution System
  > ETOPS - 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 AMM
- [SDR HALA2021101200136](https://openairdocs.org/sdr/HALA2021101200136.md): Fire Loop · false indication · Oct 8, 2021 · N220HA · Airbus A321271N · Fire Detection
  > ETOPS - 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.
- [SDR HALA2021072900090](https://openairdocs.org/sdr/HALA2021072900090.md): Igniter · failed · Jul 30, 2021 · N220HA · Airbus A321271N · APU Start/Ignition System
  > ETOPS - 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 O
- [SDR HALA2021042600051](https://openairdocs.org/sdr/HALA2021042600051.md): Oil System · contaminated · Apr 25, 2021 · N220HA · Airbus A321271N · Turbine Engine Oil System
  > ETOPS - 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 EN
- [SDR HALA2021040500041](https://openairdocs.org/sdr/HALA2021040500041.md): Screw · failed · Apr 4, 2021 · N220HA · Airbus A321271N · Engine Oil System (Airframe Furnished)
  > ETOPS - SCREW SNAPPED IN LH ENG OIL CONTROL MODULE // REMOVED STRIPPED FASTENER AND HELICOIL, REPLACED PER AIRBUS 321 AMM 70-24-00-910-803-A
- [SDR HALA2020123100231](https://openairdocs.org/sdr/HALA2020123100231.md): Battery · defective · Dec 30, 2020 · N220HA · Airbus A321271N · Emergency Lighting
  > EMERGENCY 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.
- [SDR HALA2019111900491](https://openairdocs.org/sdr/HALA2019111900491.md): Smoke Warning · false activation · Nov 18, 2019 · N220HA · Airbus A321271N · Smoke Detection
  > SMOKE LAVATORY SMOKE ON POST FLIGHT REPORT. // PERFORMED T/S IAW TSM 26-17-00-810-804-A. NO FAULTS DETECTED. OK FOR SERVICE.
- [SDR HALA2019110200465](https://openairdocs.org/sdr/HALA2019110200465.md): Life Raft · low pressure · Nov 2, 2019 · N220HA · Airbus A321271N · Life Raft
  > SUP - LIFE RAFT RESERVOIR PRESSURE AT 2650 PSI, FERRY FLIGHT REQUIRED. // REMOVED AND REPLACED LIFE RAFT PER AMM 25-66-41. SECURITY CHECK GOOD
- [SDR HALA2019090300360](https://openairdocs.org/sdr/HALA2019090300360.md): Eec · malfunctioned · Aug 29, 2019 · N220HA · Airbus A321271N · Fuel Control/Turbine Engines
  > ETOPS 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.

## 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 = 'N220HA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N220HA/reports

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