# Service difficulty reports: N217HA

A list on [N217HA](https://openairdocs.org/aircraft/N217HA.md).

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

Page 1 of 2 · 68 reports

- [SDR HALA20250929292](https://openairdocs.org/sdr/HALA20250929292.md): Coupling · faulted · Sep 26, 2025 · N217HA · Airbus A321271N · Fuel Storage
  > ETOPS - FUEL LEAKING FROM HOSE NOZZLE WHEN CONNECTED TO REFUEL/DEFUEL COUPLING. AIRCRAFT WONT TAKE FUEL. REMOVED AND REPLACED REFUEL/DEFUEL COUPLING ELEMENT ASSY PER AMM 28-25-41, OPS CHECK AND LEAK CHECK GOOD. A/C OK FOR SERVICE.
- [SDR HALA20250904048](https://openairdocs.org/sdr/HALA20250904048.md): Not Reported · not reported · Sep 2, 2025 · N217HA · Airbus A321271N · Standard Practices/Structures
  > TOW BAR SNAPPED ON PUSH. AWAITING FULL RESOLUTION.
- [SDR HALA20250804239](https://openairdocs.org/sdr/HALA20250804239.md): Fadec · faulted · Aug 1, 2025 · N217HA · Airbus A321271N · Fuel Controlling System
  > ETOPS - ENG 2 FADEC SYS FAULT ON ECAM. REMOVED AND REPLACED ENG2 EEC PER AMM 73-21-01, OPS CHECK GOOD NO FAULT NOTED ON ECAM. A/C OK FOR SERVICE
- [SDR HALA20250514134](https://openairdocs.org/sdr/HALA20250514134.md): Sensor · faulted · May 13, 2025 · N217HA · Airbus A321271N · Cabin Temperature Control System
  > ETOPS - AIR PACK 2 REGUL FAULT IN CRUISE. AMBER XX C SENSOR ON BLEED PAGE. PERFORMED A320 FIM TASK 21-61-00-810-A. REMOVED AND REPLACED P2 COMP TEMP SENSOR PER A320 AMM 21-61-11. OPS CHK GOOD. OK FOR SVC.
- [SDR HALA20250407101](https://openairdocs.org/sdr/HALA20250407101.md): Switch · broken · Apr 4, 2025 · N217HA · Airbus A321271N · Weather Radar System
  > ETOPS - INFO TO MAINTENANCE: RADAR "SYS SWITCH DETENT IS BROKEN ALLOWING IT TO BE BUMPED TO THE ON POSITION, WHICH CAN CAUSE A HAZARD AT THE GATE. REMOVED AND REPLACED WXR CONTROL UNIT. BITE TEST PER 34-41-00. TEST OK, NO FAULTS NOTED. OK FOR SERVICE.
- [SDR HALA20250303010](https://openairdocs.org/sdr/HALA20250303010.md): Oil System · overserviced · Feb 28, 2025 · N217HA · Airbus A321271N · Turbine Engine Oil System
  > WEAK DIRTY SOCKS SMELL THROUGHOUT CABIN AND COCKPIT. STRONGER IN BACK OF PLANE. STARTED UNDER 5000'. TURNED ON APU BLEED AND SMELL DISAPATED. DURING ETOPS PDSC NOTICED #2 ENG OIL OVERSERVICED. REMOVED 2 QRTS. PERFORMED TSM 71-00-00-810-847-A. NO SMELLS NOTED.
- [SDR HALA20250226072](https://openairdocs.org/sdr/HALA20250226072.md): Pressure Sensor · faulted · Feb 25, 2025 · N217HA · Airbus A321271N · Engine Oil Pressure
  > ETOPS - FOUND OIL PRESSURE DIFFERENTIAL SENSOR BAD PER TASKCARD 321-730000-WI-1 W/O 335093 FIN- 4077KS. REMOVED AND REPLACED OIL PRESSURE DIFFERENTIAL SENSOR PER AMM 79-33-23. OPS AND SECURITY CHECK GOD. BITE AND LEAK CHECK GOOD.
- [SDR HALA20250210005](https://openairdocs.org/sdr/HALA20250210005.md): Tailpipe · fire · Feb 6, 2025 · N217HA · Airbus A321271N · Engine (Turbine/Turboprop)
  > UPON GATE ARRIVAL. REPORTED A SMALL ENGINE FIRE ON ENGINE 2 TAIL CONE- EXTINGUISHED ITSELF. PERFORMED VISUAL INSPECTION OF ENGINE AFTER FIRE NO FAULTS NOTED. PERFORMED IDLE RUN OF ENGINE2 PER AMM 71-00-00-710-806-A IDLE RUN GOOD A/C OK FOR SVC.
- [SDR HALA20240830248](https://openairdocs.org/sdr/HALA20240830248.md): Fcu · faulted · Aug 30, 2024 · N217HA · Airbus A321271N · APU Engine Fuel and Control
  > ETOPS - APU AUTO SHUT DOWN. FOLLOWED TSM 49-00-81-810-835-A AND REPLACED FCU AS PER AMM 49-32-11. OPERATION AND LEAK CHECK NORMAL. AIRCRAFT OK FOR SERVICE
- [SDR HALA20240830247](https://openairdocs.org/sdr/HALA20240830247.md): Pressure Switch · faulted · Aug 30, 2024 · N217HA · Airbus A321271N · APU Oil System
  > ETOPS - APU STATUS MESSAGE (LOW OIL PRESSURE). FOLLOWED TSM 49-00-81-810-868-A AND REPLACED OIL PRESSURE SWITCH AS PER AMM 49-94-14. OPERATIONAL CHECK NORMAL. AIRCRAFT OK FOR SERVICE.
- [SDR HALA20240605155](https://openairdocs.org/sdr/HALA20240605155.md): Switch · inoperative · Jun 4, 2024 · N217HA · Airbus A321271N · Hydraulic System, Main
  > ETOPS - FOUND BLUE HYD OVRD PUSHBUTTON SWITCH INOP DURING TASK CARD. REMOVED AND REPLACED SWITCH PER ASM 29-12-01. OPS CHECK GOOD. OK FOR SERVICE
- [SDR HALA20240308013](https://openairdocs.org/sdr/HALA20240308013.md): Brake Assy · chattering · Mar 7, 2024 · N217HA · Airbus A321271N · Landing Gear Brake System
  > TAXI IN BELOW 6 KTS, FELT BRAKE CHATTER USING LEFT BRAKE PEDAL ONLY. CHECKED L/H MLG BRAKES PER AMM 32-42-00-710-001-A, 32-43-00-710-001-A, 32-44-00-710-002-A. OPS CHECK GOOD. RAISED GEAR & SPUN WHEELS. NO GRABBING. NO FAULTS ON PFR. OK FOR SERVICE.
- [SDR HALA20240226052](https://openairdocs.org/sdr/HALA20240226052.md): Sensor · faulted · Feb 25, 2024 · N217HA · Airbus A321271N · Engine Oil Indicating System
  > ETOPS - ECAM ENG2 OIL SENSOR FAULT. REMOVED AND REPLACED PHMU PER AMM 77-31-01. AND TROUBLESHOT PER TSM 79-35-00-810-806-A. OPS CHECK GOOD. NO FAULTS NOTED OK FOR SERVICE.
- [SDR HALA20231124254](https://openairdocs.org/sdr/HALA20231124254.md): Overheat Sensor · faulty · Nov 22, 2023 · N217HA · Airbus A321271N · Overheat Detection
  > ETOPS - ENGINE 2 LOOP A FAULT ON ECAM FOUND DURING PDC WALKAROUND. PERFORMED TSM 26-12-00-710-002 FOUND LOOP 4002WD1 SHORTING. REMOVED & REPLACED ENG 2 LOOP A 4002WD1 IAW AMM 26-12-17 PB401. FDU TEST OKAY. NO FAULTS NOTED. A/C OK TO CONTINUE. MOC NOTIFIED.
- [SDR HALA20231019231](https://openairdocs.org/sdr/HALA20231019231.md): Unknown · unknown · Oct 18, 2023 · N217HA · Airbus A321271N · Airspeed/Mach Indicator
  > ATB - AIR TURN BACK DUE TO UNRELIABLE AIRSPEED - BUG IN PITOT TUBE. FOUND BUG IN F/O PITOT PROBE (9DA2) CLEANED AND FLUSHED PITOT PROBE PER AMM 34-10-00-170-004-A. OK FOR SERVICE.
- [SDR HALA20240712188](https://openairdocs.org/sdr/HALA20240712188.md): Exciter · faulted · Jul 11, 2023 · N217HA · Airbus A321271N · APU Start/Ignition System
  > ETOPS - APU AUTO SHUTDOWN 2X ON TAXI IN TO GATE. REMOVED AND REPLACED APU EXCITER PER AMM 49-41-38. OPS AND SECURITY CHECK GOOD.
- [SDR HALA2023041300085](https://openairdocs.org/sdr/HALA2023041300085.md): Unknown · unknown · Apr 13, 2023 · N217HA · Airbus A321271N · Engine Start Valves/Controls
  > ATB - AFTER REACHING CRUISE ALT FL340 ENG 1 START VALVE FAULT ECAM. VERIFIED START VALVE POS CLOSED, MOVED FREELY (REF TSM 80-11-00-810-828-A) REMOVED AND REPLACED #1 STARTER PER AMM 80-AA-01. LEAK CHECK AND OPS CHECK GOOD.
- [SDR HALA2023041300087](https://openairdocs.org/sdr/HALA2023041300087.md): Unknown · unknown · Apr 10, 2023 · N217HA · Airbus A321271N · Turbine Engine Air Inlet Section
  > ETOPS - #1 ENGINE FAN BLADE NICK. BLEND #1 ENG #17 BLADE. ALSO INSPECT AND CLEAN WITHIN LIMITS. PRATT AND WITHNEY 72-11-03. OK FOR SVC.
- [SDR HALA2023041700088](https://openairdocs.org/sdr/HALA2023041700088.md): Unknown · unknown · Apr 4, 2023 · N217HA · Airbus A321271N · Drag Control System
  > SUPPLEMENTAL SUBMISSION TO HALA2023040500079. UPDATED WITH RESOLUTION. DIV - SPOILER 1 FAULT - IN FLIGHT UNABLE TO RESET. DIV TO OAK. SPOILER ACTUATOR DEACTUATED. OK TO CONTINUE. UPDATED MIC SHEET AND INSTALLED PLACARD. REMOVED AND REPLACED SPOILER SERVO CONT
- [SDR HALA2023040500079](https://openairdocs.org/sdr/HALA2023040500079.md): Unknown · unknown · Apr 4, 2023 · N217HA · Airbus A321271N · Drag Control System
  > DIV - SPOILER 1 FAULT - IN FLIGHT UNABLE TO RESET. DIV TO OAK. DEFERED PER MEL 27-64-01A. SPOILER ACTUATOR DEACTUATED. OK TO CONTINUE. UPDATED MIC SHEET AND INSTALLED PLACARD.
- [SDR HALA2023033100072](https://openairdocs.org/sdr/HALA2023033100072.md): Unknown · unknown · Mar 24, 2023 · N217HA · Airbus A330243 · Engine Indicating System
  > SUPPLEMENTAL SUBMISSION TO HALA2023032400060. RESOLUTION UPDATED. ETOPS - BLOCK TURN BACK, ENG 1 EGT OVERLIMIT. PER ENGINEERING. PERFORMED TSM 71-00-00-810-885-A STEPS 4.A(3) & (4). NO FAULTS NOTED. PERFORMED TSM 71-00-00-810-861-A STEP 4.A(15) & (21). REMOVE
- [SDR HALA2023032400060](https://openairdocs.org/sdr/HALA2023032400060.md): Unknown · unknown · Mar 24, 2023 · N217HA · Airbus A321271N · Engine (Turbine/Turboprop)
  > ETOPS - BLOCK TURN BACK, ENG 1 EGT OVERLIMIT. AWAITING RESOLUTION
- [SDR HALA2023032100009](https://openairdocs.org/sdr/HALA2023032100009.md): Unknown · unknown · Mar 21, 2023 · N217HA · Airbus A321271N · Engine Exhaust System
  > REPORTED #1 ENGINE TAILPIPE FIRE. ACCOMPLISHED AMM 72-00-00-210-817-A. VISUAL INSPECTION OF ENG AFTER FIRE NO DEFECTA NOTED.
- [SDR HALA2023032100053](https://openairdocs.org/sdr/HALA2023032100053.md): Unknown · unknown · Mar 21, 2023 · N217HA · Airbus A321271N · Smoke Detection
  > ETOPS - #1 ENG CORE FIRE LOOP CLIP BROKEN (PN 636-5712-505) ON RAIL ASSY RH SIDE. REPLACED #1 ENG FIRE LOOP A RAIL ASSY PER AMM 26-12-61. OPS CHK OK. (PN 636-5712-505.
- [SDR HALA2023032100052](https://openairdocs.org/sdr/HALA2023032100052.md): Pump · faulty · Mar 21, 2023 · N217HA · Airbus A321271N · Fuel Control/Turbine Engines
  > ETOPS - ENGINE 1 START FAULT ENGINE 1 EGT OVERLIMIT HUNG START, EMGINE STALL. PERFORMED TSM 71-00-00-810-861-A, REMOVED AND REPLACED IFPC PER AMM 73-11-01-000-801-A AND 73-11-01-400-801-A. LEAK AND OPS TESTS GOOD, OK FOR SVC.
- [SDR HALA2023022400005](https://openairdocs.org/sdr/HALA2023022400005.md): None · none · Feb 23, 2023 · N217HA · Airbus A321271N · Fire Protection System
  > AT CRUZ FL350. ECAM MASTER WARN LAV SMOKE. FA'S REPORTED LAV E WEREINDICATION WAS GENERATED. PAX IN LAV SAID WAS NOT SMOKE/VAPING. LAV INSP NORMAL. INSPECTED LAV E SMOKE DETECTOR FOR CONDITION. SEAT INTACKED AND TAMPERING. PERFORMED SMOKE DETECTOR TEST IN REF/
- [SDR HALA2023011700007](https://openairdocs.org/sdr/HALA2023011700007.md): Outflow Valve · faulted · Jan 15, 2023 · N217HA · Airbus A321271N · Pressure Regulator/Outflow Valve
  > ETOPS - VENT AVIONICS SYS FAULT. SKIN AIR OUTLET VALVE ON ECAM. REMOVED & REPLACED SKIN AIR OUTLET VALVE PER AMM 21-26-53-400-001-A01. OPS CHECK GOOD. OK FOR SVC. PN/SN OFF: VFT300B00 / 042607159, PN/SN ON: VFT300B00 / 2279
- [SDR HALA2022110800288](https://openairdocs.org/sdr/HALA2022110800288.md): Fire Loop · shorted · Nov 7, 2022 · N217HA · Airbus A321271N · Fire Detection
  > PILOT REPORTS ENG 2 FIRE LOOP A FAULT. REMOVED AND REPLACED ENG 2 LOOP PER AMM 26-12-17. OPS CHECK GOOD OK TO CONTINUE SERVICE.
- [SDR HALA2022110200282](https://openairdocs.org/sdr/HALA2022110200282.md): Fadec · faulted · Nov 1, 2022 · N217HA · Airbus A321271N · Fuel Controlling System
  > ETOPS-DURING ENGINE START ECAM "ENG 2 FADEC SYS FAULT" RESET IN ACCORDANCE WITH HAL MX ENG 2 FADEC REMAINED. TWO ENGINE STARTS ATTEMPTED PER MOC DURING TAXI ENG 1 STALL FOLLOWED BY ENG 1 FAIL. ACTIONED ECAM AND TAXIED TO GATE. PER TSM 73-21-00-810-878-A REMOV
- [SDR HALA2022110100003](https://openairdocs.org/sdr/HALA2022110100003.md): Fire Loop · loose · Oct 31, 2022 · N217HA · Airbus A321271N · Fire Detection
  > BTB ENG 2 FIRE LOOP FAULT A. OPEN COWL ENG 2. FOUND 2 OPEN LOOP CLAMPS, SECURED CLAMPS. DID BITE TEST PER AMM 26-12-00-710-002. NO FAULTS NOTED. OK TO CONTINUE.
- [SDR HALA2022101900274](https://openairdocs.org/sdr/HALA2022101900274.md): Buffer Valve · used · Oct 12, 2022 · N217HA · Airbus A321271N · Compressor Bleed Governor
  > SUPPLEMENTAL INFORMATION (THIS SUBMISSION IS FOR TYPO CORRECTION OF HALA2022101800274 - TYPO CORRECTION TO BLOCK 2.J FLIGHT NUMBER, 3.A AIRCRAFT SERIAL NUMBER, TOTAL TIME, AND TOTAL CYCLE, 5.E PARTS CONDITION) - PERFORMED TSM 71-00-00-810-854-APAR, 4.A(1)TO (
- [SDR HALA2022101400274](https://openairdocs.org/sdr/HALA2022101400274.md): Valve · faulted · Oct 12, 2022 · N217HA · Airbus A321271N · Engine Bleed Air System
  > ETOPS, CREW REPORTS #1 ENG STALL, RETURN TO BLOCK, MAINTENANCE COMPLETED BORESCOPE INSPECTION, NO DEFECT NOTED, ENGINE KEEPS STALLING DURING RUNS. PERFORMED TSM 71-00-00-810-854-APAR, 4.A (1) TO (3) STEP, PERFORMED BORESCOPE INSP OF HPC & LPC PER STEP 4.A (
- [SDR HALA2022081600145](https://openairdocs.org/sdr/HALA2022081600145.md): None · none · Aug 17, 2022 · N217HA · Airbus A300* · Engine (Turbine/Turboprop)
  > ETOPS - FUEL LEAK FOUND AT ENG 1 FUEL DRAIN MAST. REMOVED AND REPLACED ENG #1 LOW PRESSURE COMPRESSOR BLEED VALVE PER AMM 75-32-01-00-00-801-A & AMM 75-32-01-400-801-A. PERFORMED ENGINE IDLE RUN PER AMM 71-00-720. NO LEAKS FOUND. A/C OK TO CONTINUE
- [SDR HALA2022061300112](https://openairdocs.org/sdr/HALA2022061300112.md): None · none · Jun 10, 2022 · N217HA · Airbus A321271N · Compressor Bleed Valve
  > ETOPS - ECAM ENG 2 AIR SYS FAULT DESCENDING THROUGH 12,000' // REMOVED AND REPLACED #2 ENGINE BUFFER AIR VALVE PER AMM 75-26-04, PERFORMED TEST 3 IDLE RUN PER AMM 71-00-00, NO DEFECTS NOTED, SYSTEM CHECKED NORMAL. OK FOR SERVICE.
- [SDR HALA2022021500044](https://openairdocs.org/sdr/HALA2022021500044.md): None · none · Feb 14, 2022 · N217HA · Airbus A321271N · Engine Oil System (Airframe Furnished)
  > ETOPS - IN FLIGHT ECAM "ENG 2 AIR SYS FAULT". WOULD APPEAR THEN CLEAR ITSELF SEVERAL TIME.// REMOVED AND REPLACED LPC BUFFER AIR VALVE. PER AM M75-26-00 PB 400 CONFIG 00. OPS AND LEAK CHECK GOOD. OK FOR SERVICE.
- [SDR HALA2022020100035](https://openairdocs.org/sdr/HALA2022020100035.md): None · none · Jan 31, 2022 · N217HA · Airbus A321271N · Air Conditioning System
  > BTB - CAN NOT CONTROL FWD CABIN HEAT ACFT RETURNING TO THE GATE. COND TRIM AIR SYSTEM FAULT FWD CABIN TRIM VALVE ECAM // REMOVED AND REPLACED FWD CABIN TRIM VALVE (12HK) PER AMM 21-63-51. OPS CHECK GOOD, RAN BOTH ENGINES AT IDLE FOR FIVE MINUTES, NO FAULTS NO
- [SDR HALA2021112400172](https://openairdocs.org/sdr/HALA2021112400172.md): None · none · Nov 22, 2021 · N217HA · Airbus A321271N · Hydraulic Power Accumulator, Main
  > ETOPS - #1 ENG HYD PUMP LINE FOUND DAMAGED // REPLACED SUCTION LINE REF AMM 29-11-49. LEAK CHECK GOOD.
- [SDR HALA2021110100148](https://openairdocs.org/sdr/HALA2021110100148.md): Unknown · odor · Oct 28, 2021 · N217HA · Airbus A321271N · Air Distribution System
  > FAS REPORTED NOTICEABLE "DIRTY SOCK" SMELL IN FORWARD CABIN FROM 15 MINS OUT TO LANDING // PERFORMED TSM 05-50-00-810-831-A. ISOLATED BOTH PACKS WITH ENG 1, ENG 2, AND APU. UNABLE TO DUPLICATE ODOR IN CABIN. NO DEFECTS NOTED. OK FOR SVC.
- [SDR HALA2021101800140](https://openairdocs.org/sdr/HALA2021101800140.md): None · none · Oct 17, 2021 · N217HA · Airbus A321271N · Passenger Compartment Lighting
  > EMER EQ - EXIT SIGN @ DOOR 3 CENTER DOES NOT ILLUMINATE. // RELAMPED EXIT SIGN AT DOOR 3 CENTER. OPS CHECK GOOD. OK FOR SERVICE.
- [SDR HALA2021101500138](https://openairdocs.org/sdr/HALA2021101500138.md): None · none · Oct 14, 2021 · N217HA · Airbus A321271N · APU Start/Ignition System
  > ETOPS - APU AUTO SHUTDOWN // REMOVED AND REPLACED EXCITER-IGNITION PER AMM 49-41-38 OPS CHECK GOOD. NO FAULTS NOTED.
- [SDR HALA2021092000119](https://openairdocs.org/sdr/HALA2021092000119.md): Fuel Filter · degraded · Sep 18, 2021 · N217HA · Airbus A321271N · Engine Fuel Distribution
  > ETOPS - INFO TO MX:ON CLIMB OUT MOMENTARY ECAM ENG 2 FUEL FILTER DEGRADE APPEAR FOR A FEW SECONDS THEN CLEARED ITSELF // PERFORM T/S PER TSM 73-11-00-810-826-A. REPLACED FUEL FILTER PER AMM REF 73-11-06-400-801-A. PERFORM GRD ENG RUN #2 ENG., OPS CHECK GOOD. N
- [SDR HALA2021041300047](https://openairdocs.org/sdr/HALA2021041300047.md): Life Raft · expired · Apr 11, 2021 · N217HA · Airbus A321271N · Life Raft
  > EMER EQ - LIFE RAFT IN AFT CEILING CONTAINER EXPIRED PER HALENGINEERING AND HAL901. NEDDS REPLACEMENT // REPLACED LIFE RAFT IN AFT CEILING CONTAINER WITH SERVICEABLE PART PER AMM 25-66-41. SECURITY CHECK OK. HAL 901 INSTALLED PER GMM VOL.2. OK FOR SERVICE.
- [SDR HALA2020080500168](https://openairdocs.org/sdr/HALA2020080500168.md): Pitot Head · damaged · Aug 4, 2020 · N217HA · Airbus A321271N · Pitot/Static System
  > DURING PITOT STATIC TEST, FOUND PITOT PROBE 1 (9DA1) BURNED. REMOVED AND REPLACED PITOT PROBE 1 (9DA1) PER AMM 34-11-15. OPS TESTED GOOD.
- [SDR HALA2020060600122](https://openairdocs.org/sdr/HALA2020060600122.md): Flap · punctured · Jun 5, 2020 · N217HA · Airbus A321271N · Trailing Edge Flaps
  > OPEN - ON MX WALK AROUND PUNCTURE DAMAGE ON LT IB FLAP 32" FROM OUTB EDGE AND 0.5" FWD OF TE. LT INBOARD FLAP TAB HAS BEEN REPAIRED PER E105-C30022-TER, OK TO CLOSE OK FOR SERVICE.
- [SDR HALA2020011700016](https://openairdocs.org/sdr/HALA2020011700016.md): Engine · vibration · Jan 17, 2020 · N217HA · Airbus A321271N · Engine (Turbine/Turboprop)
  > ATB, NR 2 ENGINE. HIGH VIBRATION. IFSD. REMOVED AND REPLACED THE NR 2 ENGINE.
- [SDR HALA2019122600528](https://openairdocs.org/sdr/HALA2019122600528.md): Warning Message · false activation · Dec 24, 2019 · N217HA · Airbus A321271N · Fire Detection
  > DURING DESENT THROUGH 12500, THE NR 1 ENGINE FIRE LOOP, A FAULT APPEARED ON ECAM WITH NO ASSOCITED CAUTION ALERT MASSAGE LASTED APPROX 2 MIN ON ECAM//T/S REF TSM 26-12-00-810-825-A, PERFORMED VI IAW AMM 26-12-00-200-802, VERFIED ALL CONNECTIONS TIGHT AND SECU
- [SDR HALA2019122300526](https://openairdocs.org/sdr/HALA2019122300526.md): Warning Message · false activation · Dec 21, 2019 · N217HA · Airbus A321271N · Fire Detection
  > NR 1 ENGINE FIRE LOOP -A- FAULTED ECAM DURING APPROACH. TROUBLESHOT IAW TAM 26-12-00-810-851-A, POST SB 26-1112. DETECTOR CONFIRMED AND NO FAULTS NOTED ON OPERATIONAL TEST, VISUAL INSPECTION OF DETECTORS AND HARNESS FOUND NO DEFECTS NOTED, RESTIANCE CHE
- [SDR HALA2019121700520](https://openairdocs.org/sdr/HALA2019121700520.md): Fire Detector · malfunctioned · Dec 16, 2019 · N217HA · Airbus A321271N · Fire Detection
  > ETOPS SIGNIFICANT SYSTEM - ENG 1 FIRE LOOP A FAULT ON DESCENT INTO HNL. // REMOVED ENG 1 FDU 1 FOR TROUBLESHOOTING. REINSTALLED SAME. OPS CHK PENDING. CB'S Q38, Q39, A06, A07 PULLED + COLLARED. OPS CHK PENDING. FOUND HARDWARE NOT SECURED ON FIRE DETECTOR LOOP
- [SDR HALA2019121700519](https://openairdocs.org/sdr/HALA2019121700519.md): Fire Loop · faulted · Dec 15, 2019 · N217HA · Airbus A321271N · Fire Detection
  > ETOPS SIGNIFICANT SYSTEM - ENG 1 FIRE LOOP A FAULT, REPEAT WRITE-UP // T/S PER TSM 26-12-00-810-803-A. REMOVED AND REPLACED #1 ENGINE LOOP A AFT DETECTOR PER AMM 26-12-17-000-803-A. OPS CHECK GOOD. NO DEFECTS NOTED.
- [SDR HALA2019121700518](https://openairdocs.org/sdr/HALA2019121700518.md): Connector · loose · Dec 15, 2019 · N217HA · Airbus A321271N · Fire Protection System Wiring
  > ETOPS SIGNIFICANT SYSTEM - ENG 1 FIRE LOOP A FAULT, REPEAT WRITE-UP // INSPECTED ENG 1 FIRE LOOP, FOUND LOOSE CONNECTOR @ ENG 1 FIRE LOOP. RE-TORQUED CONNECTOR AS REQUIRED. PERFORMED FDU BITE CHECKED, PER AMM 26-12-00. TEST PASSED NO FAULTS NOTED. OK TO CONTIN

Next page: https://openairdocs.org/aircraft/N217HA/reports.md?page=2

## 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 = 'N217HA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N217HA/reports

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