# Service difficulty reports: N215HA

A list on [N215HA](https://openairdocs.org/aircraft/N215HA.md).

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

- [SDR HALA20250819254](https://openairdocs.org/sdr/HALA20250819254.md): Igniter · faulted · Aug 18, 2025 · N215HA · Airbus A321271N · Spark Plug/Igniter
  > ETOPS - ENG 1 A ING ECAM ON ENGINE START UP. REMOVED AND REPLACED LOWER IGNITER PLUG. PER AMM 74-21-01. OPS TEST BAD. FURTHER T/S REQUIRED. REMOVED AND REPLACED EXCITER PER AMM 74-11-01. OPS CHECK NORMAL. OK FOR SERVICE.
- [SDR HALA20250804238](https://openairdocs.org/sdr/HALA20250804238.md): Wire Harness · faulted · Aug 4, 2025 · N215HA · Airbus A321271N · Engine Fuel System Wiring
  > ETOPS - ENG 1 MINOR FAULT AFTER START. FOUND WC08 HARNESS WIRE SHOWING. REMOVED AND REPLACED PER AMM 73-21-68. PERFROMED IDLE ENGINE RUN. OPS GOOD.
- [SDR HALA20250122028](https://openairdocs.org/sdr/HALA20250122028.md): Wire Harness · chafed · Jan 21, 2025 · N215HA · Airbus A321271N · Fire Protection System Wiring
  > ETOPS - INFO TO MX: ENG 1 FIRE LOOP A FAULT ECAM APPEARED AND DISAPPEARED MULTIPLE TIMES DURING FLIGHT. WHILE CHECKING INSULATION RESISTANCE AT FDU 1 LOOP A CONNECTOR PIN J-GRD & SHAKING LOOP A HARNESS 4165KS GOT A FLUCTUATION IN RESISTANCE FROM <100MOHMS TO 4
- [SDR HALA20241226378](https://openairdocs.org/sdr/HALA20241226378.md): Elec Connector · damaged · Dec 25, 2024 · N215HA · Airbus A321271N · Hydraulic Power System Wiring
  > ETOPS - BTB- HYD G ENG 1 PUMP LO PR. REPLACED CONTACTS IN CONNECTOR 1074GK-A PER ESPM 20-44-13. REMOVED AND REPLACED ENG HYD PUMP SWITCH PER TSM 29-11-00-810-804-A AND AMM 29-11-17. LEAK CHECK GOOD. OPS CHECK GOOD. RAND ENG 1 3 TIMES WITH CREW. CYCLED #1 ENG H
- [SDR HALA20241226379](https://openairdocs.org/sdr/HALA20241226379.md): Pump · low pressure · Dec 24, 2024 · N215HA · Airbus A321271N · Hydraulic Pump (Electric/Engine), Main
  > ATB - HYD G ENG 1 PUMP LO PR. REMOVED AND REPLACED #1 ENG GREEN EDP PER AMM 29-11-51. OPS & LEAK CHECK OK. HYD INDICATION OK & NO FAULT NOTED. PERFORMED TSM 29-11-00-810-804-A UP TO STEP 4.A. PRESSURE CHECK OK, MORE THAN 1812 PSI. NEED TO CONTINUE WIRING CHEC
- [SDR HALA20241223376](https://openairdocs.org/sdr/HALA20241223376.md): Oil System · leaking · Dec 22, 2024 · N215HA · Airbus A321271N · Turbine Engine Oil System
  > IFSD / DIV - DURING CLIMB, ADV APPEARED W/FLASHING ZERO OIL QUANTITY. EVENTUALLY LOW OIL PRESSURE AND ECAM DROVE US TO SHUT DOWN ENG #1. AIR DIVERSION TO HNL. REMOVED #1 GREEN HYD EDP PER AMM 29-11-51. FOUND TORN SPLINE SEAL. NEED TO REPLACE SPLINE SEAL AND FL
- [SDR HALA20241112070](https://openairdocs.org/sdr/HALA20241112070.md): Unknown · odor · Nov 10, 2024 · N215HA · Airbus A321271N · Air Distribution System
  > ATB-FUME EVENT CABIN CREW NOTIFIED US SHORTLY AFTER TO OF "BURNING POPCORN" SMELL NEAR 3R DOOR. SMELL MOVED FWD TO ROWS 11-27. CONSTANT, NOT DISSAPATING FOR CLIMB, CRUISE, OR DESCENT. APU BLEED USED @ 10K TO LANDING. SMELL DISSAPATED. PERFORMED DUAL ENG WASH P
- [SDR HALA20240925168](https://openairdocs.org/sdr/HALA20240925168.md): Fire Loop · faulted · Sep 24, 2024 · N215HA · Airbus A321271N · Fire Detection
  > ETOPS - ENG1 FIRELOOP B FAULT. ENG 1 REPLACED AGB LOOP B 4002WD2 PER AMM 26-12-17 OPS CHECK OK
- [SDR HALA20240815226](https://openairdocs.org/sdr/HALA20240815226.md): Filter · unknown · Aug 14, 2024 · N215HA · Airbus A321271N · APU Oil System
  > ETOPS - APU AUTO SHUTDOWN AT GATE. REMOVED AND REPLACED APU OIL FILTER AND GEN SCAVENGE FILTER PER AMM 49-91-41-200.OPS/LEAK CHECK GOOD. OK FOR SERVICE.
- [SDR HALA20240705180](https://openairdocs.org/sdr/HALA20240705180.md): Master Switch · faulted · Jul 3, 2024 · N215HA · Airbus A321271N · Airborne Auxiliary Power Unit (APU) System
  > DMI 209186 - APU MASTER S/W INTERMIT HAVE TO TAP ( MASTER SWITCH ON LIGHT). REPLACED APU MASTER SWITCH 14KD PER ESPM 20-45-11 OPS CHECK APU PER AMM 49-00-00 OK
- [SDR HALA20240701174](https://openairdocs.org/sdr/HALA20240701174.md): Wire · detached · Jun 28, 2024 · N215HA · Airbus A321271N · Hydraulic Power System Wiring
  > ETOPS - DURING PDSC FOUND GREEN EDP ENG 1 INDICATING ON WHEN OFF. FOUND BLUE WIRE AT CONNECTOR 1074GK-A SHEARED, RE-PINNED PER ESPM 20-48-24. ALSO FOUND INTERNAL LEAKAGE OF PRESSURE SWITCH. REMOVED AND REPLACED PRESSURE SWITCH REF AMM 29-11-17. OPS AND LEAK CH
- [SDR HALA20240313065](https://openairdocs.org/sdr/HALA20240313065.md): Probe · faulted · Mar 12, 2024 · N215HA · Airbus A321271N · Fuel Quantity Sensor
  > ETOPS - 1600LBS OF FUEL DISSAPEARED FROM FOB BEFORE PUSHBACK. REMOVED AND REPLACED RH WING FUEL PROBES 27QT2 AND 28QT2 PER AMM 28-42-15. PENDING 640BB FUEL PANEL INSTALL AND OPS CHECK. INSTALLED FUEL PANEL OPS, LEAK, AND BITE CHECKS GOOD PER AMM 28-42-15
- [SDR HALA20240306062](https://openairdocs.org/sdr/HALA20240306062.md): Packing · leaking · Mar 3, 2024 · N215HA · Airbus A321271N · Hydraulic System, Main
  > ETOPS - DURING DESCENT HYD G RSVR LO LVL L/G GRAVITY EXTENSION COMPLETED. FOUND PRESSURE SWITCH PACKING LEAKING. REMOVED AND REPLACED PRESSURE SWITCH PACKING PER AMM 29-11-17. LEAK CHECK GOOD. OK FOR SERVICE.
- [SDR HALA20240229055](https://openairdocs.org/sdr/HALA20240229055.md): Tube · leaking · Feb 28, 2024 · N215HA · Airbus A321271N · Engine Oil Distribution (Airframe Furnished)
  > ATB - #1 ENG OIL QTY DROPPED TO ZERO. UPON INSEPCTION NOTICED THE OIL PRESSURE TUBE FROM ENGINE AIR/OIL HEAT EXCHANGER WITH EVIDENCE OF OIL SEEPAGE. REFER PIPC 79-21-49-08 SHEET 2 OF 5 ITEM #20. ALL BOLTS FOR OIL PRESSURE TUBE SECURE AND TORQUED IAW AMM 79-21-
- [SDR HALA20240108006](https://openairdocs.org/sdr/HALA20240108006.md): Unknown · unknown · Jan 5, 2024 · N215HA · Airbus A321271N · Engine (Turbine/Turboprop)
  > DURING THRUST LEVER ADVANCEMENT, ENG 1 STALL MESSAGE APPEARED. MESSAGE CLEARED ITSELF WITHIN 2 SECONDS WHILE BRINGING THRUST LEVERS TO IDLE. PER INDICATED ENG 1 STALL MESSAGE. PILOT NOTED ALL ENGINE INDICATIONS NORMAL. POWER LEVER NOT AT TAKEOFF POWER @ EVENT
- [SDR HALA2023083100186](https://openairdocs.org/sdr/HALA2023083100186.md): Unknown · unknown · Aug 26, 2023 · N215HA · Airbus A321271N · Fire Detection
  > ETOPS - ENG 1 FIRE LOOP A FAULT ECAM CAME ON DURING DEPARTURE. REMOVED AND REPLACED # 1 ENG FIRE DETECTOR ELEMENT IAW AMM 26-12-17-000-802-A. OPS CHECK NORMAL IAW 26-11-00.
- [SDR HALA2023061600126](https://openairdocs.org/sdr/HALA2023061600126.md): Unknown · unknown · Jun 15, 2023 · N215HA · Airbus A321271N · Fire Detection
  > ETOPS - ON A/C WAKE-UP, ENG 1 FIRE LOOP B FAULT. REMOVED AND REPLACED AGB FIRE LOOP B PER AMM 26-12-17. OPS TEST GOOD. SECURITY CHECK GOOD. OK FOR SERVICE.
- [SDR HALA2022121600310](https://openairdocs.org/sdr/HALA2022121600310.md): Fire Loop · faulted · Dec 15, 2022 · N215HA · Airbus A321271N · Fire Detection
  > ETOPS, NR 2 ENGINE FIRE LOOP B ILLUMINATED IN CRUISE. PERFORMED TSM 26-12-00-810-861-A FOR ENG 2 LOOP B AGB LOSS. R & R ENG 2 FIRE LOOP B AND BITE TESTED OKAY IAW AMM 26-12-17 PB401. A/C OK FOR SERVICE.
- [SDR HALA2022110400283](https://openairdocs.org/sdr/HALA2022110400283.md): Fire Loop · faulted · Nov 3, 2022 · N215HA · Airbus A321271N · Fire Detection
  > ETOPS - ECAM ENG 1 FIRE LOOP A FAULT. PERFORMED TSM 26-12 -00-810-857-A. 'LOSS OF DETECTION BY ENG 2 LOOP A CORE.' FOUND LOOP A CORE FIRE DETECTOR RESISTANCE VALUES OUT OF SPECIFIED LIMITS. REMOVED AND REPLACED ENG 2 LOOP A CORE LOOP PER AMM 26-12-17. OPS CHEC
- [SDR HALA2022091200259](https://openairdocs.org/sdr/HALA2022091200259.md): None · none · Sep 10, 2022 · N215HA · Airbus A300* · Engine Oil System (Airframe Furnished)
  > ETOPS-DURING LANDING PILOT NOTED LOSING OIL QUAINTY ON # 2 ENG. FOUND # 2 ENG STARTER DUCT TWISTED, REMOVED ANF REPLACED ENG STARTER PER AMM 80-11-03. FOUND CHIPS AND METALS ON STARTER CHIP DETECTOR REMOVED AND REPLACED PER AMM 80-11-01 AND REMOVED AND REPLACE
- [SDR HALA2022081100141](https://openairdocs.org/sdr/HALA2022081100141.md): None · none · Aug 10, 2022 · N215HA · Airbus A321271N · Pneumatic System
  > BTB - L BLEED AIR FAULT - ABNORMAL PRESSURE // REMOVED AND INSTALLED HP BLEED VALVE IAW AMM 36-11-51. REMOVED AND INSTALLED OVERPRESSURE VALVE IAW AMM 36-11-53. OPS CHECK GOOG, BITE TEST OAK. PERFORMED IDLE ON BOTH ENGINES NO FAULTS NOTED OK FOR SERVICE
- [SDR HALA2022031000073](https://openairdocs.org/sdr/HALA2022031000073.md): None · none · Mar 9, 2022 · N215HA · Airbus A321271N · Auto Flight System
  > ETOPS - FO CONSTRAINT BUTTON CRACKED // REMOVED AND REPLACED FLIGHT CONTROL UNIT PER AMM 22-81-12. AFS TEST GOOD. LAND CAT 3 TEST GOOD. OK FOR SVC.
- [SDR HALA2021102500143](https://openairdocs.org/sdr/HALA2021102500143.md): None · none · Oct 21, 2021 · N215HA · Airbus A321271N · Airborne Auxiliary Power Unit (APU) System
  > ETOPS - 2 APU AUTO SHUTDOWNS // REMOVED AND REPLACED APU IGNITION UNIT PER AMM 49-41-38.PERFORMED APU GRD. SCAN NO FAULTS AND TEST PER AMM 49-00-00.STARTED APU NORMALLY OPS CK. GOOD.SECURED APU ACCESS DOORS PER AMM 49-00-00 P/N OFF:3888058-7 S/N OFF 180016 P/
- [SDR HALA2021031800036](https://openairdocs.org/sdr/HALA2021031800036.md): B-Nut · loose · Mar 17, 2021 · N215HA · Airbus A321271N · Pneumatic Distribution System
  > ETOPS - ECAM:AIR ENG 1 BLEED FAULT DURING LANDING ROLLOUT. // FAULT CODE 361151, PERFORMED TSM 36-11-00-810-975-A. INSPECTED SENSE LINES, FOUND LOOSE B-NUT, TORQUED. PERFORMED LEAK CHECK PER AMM 36-22-00-790-802, AND TEST NO. 1- PNEUMATIC LEAK TEST PER AMM 71-
- [SDR HALA2020060500121](https://openairdocs.org/sdr/HALA2020060500121.md): Valve · malfunctioned · Jun 4, 2020 · N215HA · Airbus A321271N · Engine Cooling System
  > ETOPS SIGNIFICANT SYSTEM. ENG 1 TURB COOL FAULT. PERFORMED DRY MOTOR OF ENG NR 1 PER AMM 73-21-00-710-809-A. PER MOC NEED TO CHANGE ACC VALVE. REMOVED AND REPLACED NR 1 ENG ACC VALVE PER AMM 75-24-01-400-801-A. PENDING OPS CHECK. OPS AND LEAK CHECK GOOD
- [SDR HALA2020020500029](https://openairdocs.org/sdr/HALA2020020500029.md): Display · abnormal · Feb 5, 2020 · N215HA · Airbus A321271N · Weather Radar System
  > ETOPS SIGNIFICANT SYSTEM - WX RADAR DISPLAY ERROR, 60 DEGREE LEFT, OA MONITOR. // PERFORMED BITE TEST OF WEATHER RADAR SYSTEM PER AMM 34-41-00-740-002-A. NO FAULTS DISPLAY TEST PATTERN OPERATING NORMALLY, OK FOR SERVICE.
- [SDR HALA2019091700377](https://openairdocs.org/sdr/HALA2019091700377.md): Engine · leaking · Sep 15, 2019 · N215HA · Airbus A321271N · Turbine Engine Compressor Section
  > ECAM ENG. 1 CHIP DETECTED AFTER LANDING, STRANGE ODOR. DURING BOROSCOPE FOUND OIL LEAKING AT HPC STAGE 2. // ACCOMPLISHED #1 ENGINE CHANGE PER J321-72-HWI 02. OPS AND LEAK CHECK GOOD. VERIFICATION FLIGHT FOR #1 ENGINE CHANGES COMPLETED SATISFACTORY.
- [SDR HALA2019081900345](https://openairdocs.org/sdr/HALA2019081900345.md): Unknown · odor · Aug 17, 2019 · N215HA · Airbus A321271N · Air Distribution System
  > F/A REPORT CHEMICAL SMELL IN ALL LAVATORIES // INSPECTED ALL LAVS NO CHEMICAL SMELL NOTED. OK TO CONTINUE.
- [SDR HALA2019071500353](https://openairdocs.org/sdr/HALA2019071500353.md): Fire Loop · faulted · Jul 11, 2019 · N215HA · Airbus A321271N · Fire Detection
  > ETOPS SIGNIFICANT SYSTEM - ENGINE #1 FIRE LOOP B FAULT. FOUND #1 ENG PYLON FIRE DETECTOR LOOP B INSULATION CHECK FAILED. REPLACED LOOP B PYLON FIRE DETECTOR PER AMM 26-12-16-400-803. REINSTALLED PYLON FIRE-DETECTOR RAMP ASSY PER AMM 26-12-16-400-802. OPS CHK
- [SDR HALA2019070200344](https://openairdocs.org/sdr/HALA2019070200344.md): Warning System · false activation · Jul 1, 2019 · N215HA · Airbus A321271N · Fire Detection
  > ENG1 FIRE LOOP A FAULT ECAM CAME ON TWICE ON CLIMB OUT THEN DISAPPEARED. PERFORMED OPS TEST OF THE ENGINE FIRE AND OVERHEAT DETECTION WITH MCDU CFDS PER MM 26-12-00-710-002-A. OPS TEST OK. NO DEFECTS NOTED. OK TO CONTINUE.
- [SDR HALA2019070200343](https://openairdocs.org/sdr/HALA2019070200343.md): Fire Warning · false activation · Jun 30, 2019 · N215HA · Airbus A321271N · Fire Detection
  > ENG 1 FIRE LOOP A FAULT CAME ON MOMENTARILY TWICE AT CRUISE. FDU1 RESET. NO FAULTS, TEST PASSED.
- [SDR HALA2019050900241](https://openairdocs.org/sdr/HALA2019050900241.md): Relay · faulty · May 9, 2019 · N215HA · Airbus A321271N · AC Power Distribution System
  > ETOPS SIGNIFICANT SYSTEM - DURING EMER GEN TEST ECAM MESSAGE ELEC AC ESS BUS FAULT ON ECAM. FOLLOWED TSM 24-50-00-810-804-A. RELAY 12XE REPLACED AS REQUIRED. OPS CHECKS GOOD. OK FOR SVC.
- [SDR HALA2018120430625](https://openairdocs.org/sdr/HALA2018120430625.md): Warning Message · false activation · Dec 1, 2018 · N215HA · Airbus A321271N · Smoke Detection
  > SMOKE LAV RED ECAM IN CRUISE FL 330 (2-3 SEC) WENT OUT BY ITSELF. F/A DID CABIN WALK THROUGH. NO SIGNS OF SMOKE.// CHECK ALL LAV TRASH EXT BOTTLE WITHIN LIMIT. OPS CHK ALL TOILETS OK. PERFORMED LAV SMOKE TEST PER AMM 26-17-00-710-001-A. NO FAULTS. NO SMELL NOT
- [SDR HALA2018112000600](https://openairdocs.org/sdr/HALA2018112000600.md): Oil System · pressure loss · Nov 19, 2018 · N215HA · Airbus A321271N · Engine Oil Indicating System
  > OPEN - ETOPS SIGNIFICANT SYSTEM - AIRCRAFT DIVERTED TO NEAREST AIRPORT, DUE TO #2 ENG OIL PRESS LOSS IN FLIGHT. ENGINE WAS SHUTDOWN IN FLIGHT. // REMOVED AND REPLACED #2 ENGINE. OPS AND LEAK CHECK OK. OK FOR SERVICE. VERIFICATION FLIGHT COMPLETED SATISFACTORY.
- [SDR HALA2018101800523](https://openairdocs.org/sdr/HALA2018101800523.md): Fire Loop · defective · Oct 17, 2018 · N215HA · Airbus A321271N · Fire Detection
  > ETOPS SIGNIFICANT SYSTEM. ENG 1 LOOP A FAULT ON PDC. PERFORMED TSM 26-12-00-810-851-A. DURING FDU1 TEST, CHECK ENG 1 FIRE LOOP A CORE. RESISTANCE OF 4001WD1 DET-FIRE CORE VENT LOOP A, OUT OF LIMITS. REPLACED LOOP DETECTOR PER AMM 26-12-17. OPS CHECK BITE CHECK
- [SDR HALA2018092500435](https://openairdocs.org/sdr/HALA2018092500435.md): Mmr · malfunctioned · Sep 24, 2018 · N215HA · Airbus A321271N · HF Communications System
  > ETOPS SIGNIFICANT SYSTEM, HF DATA LINK INTERMITTENT. RESET MMR AND ATSU C/B AS REQUIRED. OPS CHECK GOOD.
- [SDR HALA2018092500433](https://openairdocs.org/sdr/HALA2018092500433.md): Monitor · faulty · Sep 24, 2018 · N215HA · Airbus A321271N · Engine Oil Indicating System
  > ETOPS SIGNIFICANT SYSTEM, ENG 1 OIL CHIP DETECTED. TROUBLESHOOT PER TSM 79-35-00-810-808-A PER STEP 8(A) REPLACED OIL DEBRIS MONITOR IAW AMM 79-35-21. RAN NR 1 ENGINE AND PERFORMED TEST NO 3 PER AMM 71-00-00-720-811-A AND TEST NO 6 PER AMM 73-21-00-710-807-A
- [SDR HALA2018092500431](https://openairdocs.org/sdr/HALA2018092500431.md): Warning System · false activation · Sep 24, 2018 · N215HA · Airbus A321271N · Engine Oil Indicating System
  > ETOPS SIGNIFICANT SYSTEM - ENG 1 OIL CHIP DETECTED ECAM ON TAXI. INSPECTED NR 1 ENG OIL CHIP DETECTORS PER AMM 79-00-00-281-802A. NO CHIPS NOTED. INSPECTED NR 1 ENG OIL FILTER ELEMENT PER AMM 79-00-00-210-809A. NO CONTAMINATION NOTED. RAN ENGINE NO LEAK NOTED.

## 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 = 'N215HA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N215HA/reports

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