# Service difficulty reports: N208HA

A list on [N208HA](https://openairdocs.org/aircraft/N208HA.md).

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

- [SDR ASAA2026100867315](https://openairdocs.org/sdr/ASAA2026100867315.md): Arming Lever · dirty · Oct 8, 2026 · N208HA · Airbus A321271N · Service Doors
  > 4R DOOR SLIDE LEVER DOES NOT ARM. GROUNDED - YES. FOUND DEBRIS SMALL EXITPLACARD IN GIRT BAR LATCH, REWMOVED DEBRIS DOOR SRMED NORMALLY AND REINSATLLED EXIT SIGN AS REQUIRED AC OKAY TO CONTINUE.
- [SDR ASAA2026052865025](https://openairdocs.org/sdr/ASAA2026052865025.md): Pressure Switch · unserviceable · May 28, 2026 · N208HA · Airbus A321271NX · Hydraulic System, Main
  > ATB: ENG #1 HYD GREEN LO PRESSURE. GROUNDED - YES. REPLACED#1 ENG PUMP PRESSURE SWITCH (FIN 1074GK) PER AMM 29-11-17. 17261 05/29/26 PENDING WIRING, OPS & LEAK CHECK. PENDING WIRING, OPS && LEAK CHECK. REPAIRED WIRING TO 1074GK PER ESPM 20-53-22 OPS CHECK PEND
- [SDR HALA20250813246](https://openairdocs.org/sdr/HALA20250813246.md): Cabin Pressure · malfunctioned · Aug 12, 2025 · N208HA · Airbus A321271N · Cabin Pressure Control System
  > DIV - AVIONICS DOOR OPEN IN FLIGHT MESSAGE A/C NOT PRESSURIZING NORMALLY. PERFORMED VISUAL INSPECTION OF AVIONICS DOOR. PERFORMED PRESSURIZATION TEST FOR AIR LEAKS PER AMM 05-53-00. NO DEFECTS NOTED. OK TO CONTINUE.
- [SDR HALA20250728235](https://openairdocs.org/sdr/HALA20250728235.md): Fuel Sys · leaking · Jul 26, 2025 · N208HA · Airbus A321271N · Fuel Storage
  > ETOPS - FUEL LEAK COMING OUT LH AND RH WING DRY BAY WEEP HOLES. REPAIRED BOTH LEFT & RIGHT WING DRY BAY FUEL LEAKS IN ACCORDANCE WITH SRM 51-76-12. PERFORMED LEAK TEST PER AMM 28-11-00. NO LEAKS NOTED.
- [SDR HALA20250606163](https://openairdocs.org/sdr/HALA20250606163.md): Igniter · failed · Jun 5, 2025 · N208HA · Airbus A321271N · Spark Plug/Igniter
  > ETOPS - ENG 2 IGN A FAULT DURING START. REMOVED AND REPLACED IGN A IGNITER PLUG ON ENG 2 PER AMM 74-21-01. OPS CHECK GOOD. NO DEFECTS NOTED. OK FOR SERVICE
- [SDR HALA20250529154](https://openairdocs.org/sdr/HALA20250529154.md): Display · faulted · May 27, 2025 · N208HA · Airbus A321271N · Fuel Indicating System
  > ETOPS - MCDU'S DON'T MATCH WHEN IT COMES TO FUEL PREDICTION, TIME PREDICTION, AND VERTICAL PATH ERROR. FO'S MCDU APPEARS TO SHOW TIME: 4 MINUTES EARLIER, FUEL BURN: 400 MORE POUNDS, ABOVE DESCENT PATH: 400 FEET. REMOVED AND REPLACED FQIC PER AMM 28-42-34-04. N
- [SDR HALA20250527150](https://openairdocs.org/sdr/HALA20250527150.md): Valve · faulted · May 25, 2025 · N208HA · Airbus A321271N · Engine Bleed Air System
  > ATB DUE TO ECAM ENG 2 BLEED FAULT. REMOVED AND REPLACED #2 ENGINE FAN AIR VALVE PER AMM 36-11-54. BITE TEST OF LEFT ENGINE BLEED SYSTEM GOOD. PERFORMED IDLE RUN OF #2 ENGINE. ALL CHECKS GOOD. OK TO CONTINUE
- [SDR HALA20250416108](https://openairdocs.org/sdr/HALA20250416108.md): Igniter · failed · Apr 15, 2025 · N208HA · Airbus A321271N · APU Start/Ignition System
  > ETOPS-BTB: APU FAIL. REPLACED APU IGNITOR PLUG AND LEAD REF AMM 49-41-41 AND 49-41-43, OPS TEST NORMAL. OK FOR SVC.
- [SDR HALA20250210058](https://openairdocs.org/sdr/HALA20250210058.md): Switch · faulted · Feb 7, 2025 · N208HA · Airbus A321271N · APU Oil System
  > ETOPS - BEFORE TOW OPERATIONS, ATTEMPTED TO START APU, "APU AUTO SHUT SHUTDOWN" MESSAGE SHOWN ON ECAM. APU GRANDSCAN CONFIRMS "OIL FILTER SWITCHES" FAULT. CLEAN CONNECTORS P5 & P9 IAW TSM 49-90-00-810-812-A. APU START NOT SUCCESSFUL. REMOVED & INSPECTED PRESSU
- [SDR HALA20241230385](https://openairdocs.org/sdr/HALA20241230385.md): Oil Filter · clogged · Dec 28, 2024 · N208HA · Airbus A321271N · APU Oil System
  > ETOPS - FOUND APU OIL FILTERS CLOGGED. REMOVED AND REPLACED APU OIL FILTERS PER AMM 49-91-41-200-002-A. LEAK AND OPS CHECK GOOD. OK FOR SERVICE.
- [SDR HALA20241227382](https://openairdocs.org/sdr/HALA20241227382.md): Control Valve · faulted · Dec 26, 2024 · N208HA · Airbus A321271N · Cabin Cooling System
  > ETOPS - PACK 2 FAULT PRIOR TO DEPARTURE. REMOVED AND REPLACED PACK 2 FLOW CONTROL VALVE PER AMM 21-51-51. OPS CHECK / LEAK CHECK OK.
- [SDR HALA20241202345](https://openairdocs.org/sdr/HALA20241202345.md): Connector · damaged · Dec 1, 2024 · N208HA · Airbus A321271N · APU System Wiring
  > ETOPS - APU FAULT ON TAXI OUT BTB. ITEM ALREADY ON DMI, REPLACED AND RESECURED PINS/ JUMP CONNECTORS PER AMM 49-16-00-003-A OPS CHK OF APU GOOD OK TO REMAIN ON DMI.
- [SDR HALA20241023295](https://openairdocs.org/sdr/HALA20241023295.md): Packing · leaking · Oct 22, 2024 · N208HA · Airbus A321271N · Engine (Turbine/Turboprop)
  > ETOPS - #1 ENG OIL NEAR FAN BLADES (OIL BLADES). REMOVED AND REPLACED #1 ENG FAN SHAFT COVER PACKING IDLE POWER TEST GOOD. LK CK GOOD. OK FOR SERVICE IAW AMM 72-15-00-960-801-A
- [SDR HALA20240725197](https://openairdocs.org/sdr/HALA20240725197.md): Filter · faulted · Jul 24, 2024 · N208HA · Airbus A321271N · APU Oil System
  > ETOPS - APU AUTO SHUTDOWN TWICE DURING PREFLIGHT. PERFORMED BITE TEST, FAULTED GEN SCAV AND LUBE FILTERS. REMOVED AND REPLACED BOTH FILTERS IN REF W/ AMM 49-91-41-200-002-A. APU OPS CHECK GOOD. LEAK CHECK GOOD. NO LEAK NOTED. OK FOR SVC.
- [SDR HALA20240703178](https://openairdocs.org/sdr/HALA20240703178.md): Apu · shutdown · Jul 2, 2024 · N208HA · Airbus A321271N · Airborne Auxiliary Power Unit (APU) System
  > ETOPS - APU: AUTO SHUT DOWN ON TAXI IN 3X ATTEMPTS FAILED. REMOVED & REPLACED WIRING FROM APU STARTER MOTOR + TERMINAL LUG TO 7120VC PIN 1. WIRES X011A20, X011B14, X011C14 PER ESPM 20-33-11. REMOVED & REPLACED APU STARTER MOTOR CLUTCH PER AMM 49-42-52. PERFORM
- [SDR HALA20240327077](https://openairdocs.org/sdr/HALA20240327077.md): Packing · leaking · Mar 26, 2024 · N208HA · Airbus A321271N · Hydraulic System, Main
  > ETOPS - HYD LEAK COMING FROM LH AFT DRAIN MAST. REMOVED AND REPLACED PACKING ON # 1 ENG HYD PUMP PRESSURE SWITCH PER AMM 29-11-17, OPS AND LEAK CHECK OKAY.
- [SDR HALA20240207039](https://openairdocs.org/sdr/HALA20240207039.md): Plug · missing · Feb 6, 2024 · N208HA · Airbus A321271N · Turbine Engine Oil System
  > ETOPS - SAW A FEW DROPS OF OIL UNDER #1 ENGINE FAN COWL. FOUND LP05 OIL MANIFOLD DRAIN PLUG MISSING SCREW REF PIPC 79-21-49-01 ITEM 320 & 140 & 150. INSTALLED MISSING BOLT P/N: ST2601-06. NO LEAKS NOTED OK FOR SERVICE.
- [SDR HALA20240131005](https://openairdocs.org/sdr/HALA20240131005.md): Battery Pack · inoperative · Jan 30, 2024 · N208HA · Airbus A321271N · Emergency Lighting
  > FOUND EMER LT/EPSU (12WL) INOP DURING SERVICE CHECK. REMOVED AND REPLACED EPSU BATTERYPER AMM 33-51-38. BITE TEST GOOD. OK FOR SERVICE
- [SDR HALA20231223284](https://openairdocs.org/sdr/HALA20231223284.md): Unknown · unknown · Dec 22, 2023 · N208HA · Airbus A321271N · Hydraulic Pump (Electric/Engine), Main
  > ETOPS - HYDRAULIC OIL LEAKING FROM RH ENGINE. REMOVED AND REPLACED O RING SEAL IN COUPLING HALFT FROM YELLOW HYDRAULIC SYSTEM PER AMM 29-13-39. LEAK CHECK WITH DRY MOTOR OF ENGINE PER AMM 71-00-00-860-817A GOOD. NO FAULTS. OK FOR SERVICE
- [SDR HALA20231124255](https://openairdocs.org/sdr/HALA20231124255.md): Unknown · unknown · Nov 22, 2023 · N208HA · Airbus A321271N · Communications System
  > ETOPS - 1L DOOR HANDSET UNREADABLE ON INTERCOMAND PA. REMOVED AND REPLACED 1L DOOR HANDSET. OPS CHECK GOOD. OK FOR SERVICE PER AMM 23-73-44.
- [SDR HALA20240520137](https://openairdocs.org/sdr/HALA20240520137.md): Fire Loop · faulted · May 18, 2023 · N208HA · Airbus A321271N · Fire Detection
  > ETOPS - ENG 2 FIRE LOOP A FAULT ON ECAM PAGE. REMOVED AND REPLACED FIRE DETECTOR ELECTRICAL LOOP A PER AMM 26-12-61-000-807-A. OPS CHECK GOOD. OK FOR SERVICE.
- [SDR HALA2023041300086](https://openairdocs.org/sdr/HALA2023041300086.md): Unknown · unknown · Apr 10, 2023 · N208HA · Airbus A321271N · Engine Start Valves/Controls
  > SUPPLEMENTAL SUBMISSION TO HALA2023041300086. CORRECTION FROM REGISTRATION # 217HA TO 208HA. 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
- [SDR HALA2023032800067](https://openairdocs.org/sdr/HALA2023032800067.md): Unknown · unknown · Mar 27, 2023 · N208HA · Airbus A321271N · Pneumatic System
  > ETOPS - DUIRNG T/C 321-72-HWI-03 LEAK CHECK FOUND PRV MUSCLE TUBE CRACKED AND LEAKING BLEED AIR. REMOVED AND REPLACED PRV MUSCLE TUBE IAW AMM 36-11-52-000-802-A. AND 36-11-52-400-802-A. OPS CK GOOD. LEAK TEST GOOD. OK TO CONTINUE.
- [SDR HALA2023032200055](https://openairdocs.org/sdr/HALA2023032200055.md): Fan · faulty · Mar 22, 2023 · N208HA · Airbus A321271N · Air Distribution Fan
  > SUPPLEMENTAL TO HALA2023032000051. UPDATED WITH RESOLUTION. ETOPS - DMI# 206665 VENT EXTRACT FAULT. (CREW PLACARD). REMOVED AND INSTALLED VENT EXTRACT FAN PER AMM 21-26-51-00. PERFORMED OPERATIONAL TEST OF VENTILATION SYSTEM PER AMM 21-26-00-710-001-A. OPS CHE
- [SDR HALA2023032000051](https://openairdocs.org/sdr/HALA2023032000051.md): Unknown · unknown · Mar 17, 2023 · N208HA · Airbus A321271N · Air Conditioning System
  > ETOPS - DMI# 206665 VENT EXTRACT FAULT. (CREW PLACARD). AWAITING RESOLUTION.
- [SDR HALA2023031600043](https://openairdocs.org/sdr/HALA2023031600043.md): Unknown · unknown · Mar 15, 2023 · N208HA · Airbus A321271N · Fire Detection
  > ETOPS - DMI# 206657 ENG 1 FIRE LOOP B FAULT IN CRUISE ( ENGINE FIRE DETECTION SYSTEMS LOOP B (EXCEPT FOR ER OPERATIONS BEYOND 120 MINUTES, ONE MAY BE PROVIDED: ASSOCIATED LOOP A IS OPERATIVE / THE ENGINE FIRE TEST IS PERFORMED BEFORE EACH DEPARTURE)) TROUBLE
- [SDR HALA202303060032](https://openairdocs.org/sdr/HALA202303060032.md): Computer · faulted · Mar 3, 2023 · N208HA · Airbus A321271N · Air Conditioning System
  > ETOPS - AVNCS SYS FAULT DURING PREFLIGHT. FOUND INLET BYPASS V (16HQ) FAULT. DEFERRED PER MEL 21-26-03. REF TSM 21-26-00-810-806-A, CHSNGED INLET BYPASS VALVE (16HQ), CONDITION SAME. REMOVED & REPLACED AEVC COMPUTER. BITE CHECK GOOD, NO FAULTS NOTED. PLACARD R
- [SDR HALA2022090600255](https://openairdocs.org/sdr/HALA2022090600255.md): None · none · Sep 3, 2022 · N208HA · Airbus A321271N · Pneumatic System
  > ETOPS - APU LEAK DETECT FAULT ON ECAM. PERFORMED TSM 36-22-00-810-876-A. FOUND ELEMENT SESOR (15HF) SHORTED TO GRN. REMOVED AND REPLACED OVHT SENS ELEMENT (15HF) PER AMM 36-22-17-400-001 BITE TESET GOOD. OK FOR SVC.
- [SDR HALA2022080300138](https://openairdocs.org/sdr/HALA2022080300138.md): None · none · Aug 2, 2022 · N208HA · Airbus A300* · Manifold Pressure (MP) Indicating
  > ETOPS - AT 8000' "ENG 2 FADEC SYS FAULT THRUST LEVER 2 NOT ABOVE IDLE" THRUST LEVERS WERE IN CL DETENT // PERFORMED INSPECTION OF ENG #2 EEC AND N2 SPEED TRANSDUCER HARNESS & CONNECTIONS PER TSM 77-11-00. CHECKS OK. REMOVED & REPLACED ENG #2 N2 SPEED TRANSDUCE
- [SDR HALA2022030200061](https://openairdocs.org/sdr/HALA2022030200061.md): None · none · Mar 1, 2022 · N208HA · Airbus A321271N · Fire Detection
  > ETOPS - STATUS MSG, ENG # 1 FIRE LOOP A FAULT // RESET FDU 1 C/B'S PER AMM 26-12-34, AS PRECAUTIONARY REMOVED AND REPLACED FDU 1 CAS6465, RAN # 1 ENG AT IDLE FOR FIVE MINUTES NO FAULTS NOTED, OPS CHECK GOOD, OK FOR SERVICE
- [SDR HALA2022020400039](https://openairdocs.org/sdr/HALA2022020400039.md): Computer · faulted · Feb 3, 2022 · N208HA · Airbus A321271N · Leading Edge Slat Control System
  > BTB 2 - SELECTING FLAPS 1 ECAM F/CTL FLAPS FAULT // PERFORMED BITE OF SFCC PER AMM 27-54-00. FAULTING SFCC2 22CV. REMOVED AND REPLACED SFCC2 PER AMM 27-51-34, OPS CHECK GOOD. OK FOR SVC
- [SDR HALA2022020400038](https://openairdocs.org/sdr/HALA2022020400038.md): None · none · Feb 3, 2022 · N208HA · Airbus A321271N · Indicating/Recording System
  > BTB 1 - SPEED LIMIT DISPLAYED ON BOTH PFD’S FD+SPD LIM RED INDICATIONS // RE-SET A/C TO NORMAL CONDITIONS. BOTH PFD FD AND SPD LIM INDICATIONS ARE ABSENT. INDICATIONS READING NORMAL.
- [SDR HALA2022011100010](https://openairdocs.org/sdr/HALA2022011100010.md): Skin · damaged · Jan 10, 2022 · N208HA · Airbus A321271N · Fuselage Structure (General)
  > DURING PDC FOUND BOTTOM TAIL AREA FUSELAGE SKIN DAMAGE AND AFT GALLEY DRAIN MAST DAMAGE. DAMAGE AREA: FRAME 61-70, STRINGER 42LH - 40 RH. 176" LONG 22" WIDE // REPAIRED DAMAGE TO BOTTOM TAIL AREA AT FRAME 61-70 STRINGER 42LH-40RH AS PER AIRBUS WOTD: M-308924-E
- [SDR HALA2021090600107](https://openairdocs.org/sdr/HALA2021090600107.md): Clamp · loose · Sep 6, 2021 · N208HA · Airbus A321271N · Fire Detection
  > ETOPS - ENG 1 FIRE LOOP A FAULT DURING TOW UP, FAULTING ENG 1 LOOP A CORE AND AGB LOOPS FOUND LOOSE CLAMP AND WIRE ON LOOP A HI TEMP WIRE HARNESS. SECURED CLAMP AND ADJUSTED SLACK ON HARNESS REPLACED ENG 1 LOOP A CORE DETECTOR PER AMM 26-12-17. ALL OPS CHECK G
- [SDR HALA2021072200087](https://openairdocs.org/sdr/HALA2021072200087.md): Fire Loop · malfunctioned · Jul 22, 2021 · N208HA · Airbus A321271N · Fire Detection
  > ETOPS - ENG2 FIRE LOOP A. PERFORMED TSM26-12-00-810-825-A & TSM 26-12-00-810-914-A. REPLACED ENG2 FIRE LOOP A PER AMM26-12-16-400-803-A AND INSTALLED PYLON FIRE DETECTOR IAW AMM 26-12-16-400-802-A. SECURITY CHECKED GOOD. RAMP ASSY.AMM26-12-00-710-001.SECUR
- [SDR HALA2021061400070](https://openairdocs.org/sdr/HALA2021061400070.md): Fire Loop · faulted · Jun 13, 2021 · N208HA · Airbus A321271N · Fire Detection
  > ETOPS - PASSING FLI 80 "ENG 2 FIRE LOOP B FAULT" MSG. MSG CLEARED AFTER APPROX 5 MINS. REPEAT WRITE UP. FOUND ENG 2 LOOP B INTERMITTENT. PERFORMED CONTINUITY CHECK PER TSM 26-12-00. NO FAULT NOTED. PRECAUTIONARY ACTION, REMOVED AND REPLACED FWD FIRE LOOP ASSY
- [SDR HALA2021060700084](https://openairdocs.org/sdr/HALA2021060700084.md): Fire Loop · faulted · Jun 6, 2021 · N208HA · Airbus A321271N · Fire Detection
  > ETOPS - ECAM ENG2 FIRE LOOP A FAULT, REMOVED AND REPLACED FIRE DETECTOR ENG 2 LOOP A PYLON IAW AMM 26-12-16 OPS CHECK OK NO FAULTS NOTED.
- [SDR HALA2021032800038](https://openairdocs.org/sdr/HALA2021032800038.md): Fire Loop · broken · Mar 28, 2021 · N208HA · Airbus A321271N · Fire Detection
  > ETOPS - #2 FIRE LOOP A FAULT // FOUND ENGINE 2 PYLON DETECTOR LOOP A (3WD2) BROKEN. REMOVED PYLON FIRE-DETECTOR RAMP ASSY PER A321 AMM 26-12-16-000-802-A. 21402. 3/29/21.
- [SDR HALA2020022700044](https://openairdocs.org/sdr/HALA2020022700044.md): Chip Detector · false indication · Feb 26, 2020 · N208HA · Airbus A321271N · Turbine Engine Oil System
  > ETOPS SIGNIFICANT SYSTEM- AFTER LANDING: ECAM ENG 1 OIL CHIP DETECTED. // PERFORMED TSM 79-35-00-810-808-A "CHIP DETECTED ALERT BY ODM" NO METAL DEBRI FOUND. OK TO CONTINUE. REMOVED AND REPLACED OIL FILTER PER AMM 79-21-06-960-801-A. PERFORMED IDLE RUN LEAK CH
- [SDR HALA2020021000920](https://openairdocs.org/sdr/HALA2020021000920.md): Fire Loop · faulted · Jan 29, 2020 · N208HA · Airbus A321271N · Fire Detection
  > SUP - ECAM: ENG. 2 FIRE LOOP A FAULT ON CLIMB. // REPLACED FIRE LOOP A DETECTOR PER AMM 26-12-16, FUNCTIONAL CHECK OK. OK FOR SERVICE.
- [SDR HALA20200130020](https://openairdocs.org/sdr/HALA20200130020.md): Warning Light · false activation · Jan 29, 2020 · N208HA · Airbus A321271N · Fire Detection
  > ETOPS: ECAM - ENG 2 FIRE LOOP A FAULT ON CLIMB. REPLACED FIRE LOOP A DETECTOR PER AMM 26-12-16, FUNCTIONAL CHECKED OK.
- [SDR HALA2020010600001](https://openairdocs.org/sdr/HALA2020010600001.md): Warning System · false activation · Jan 6, 2020 · N208HA · Airbus A321271N · Engine Start Valves/Controls
  > ETOPS SIGNIFICANT SYSTEM - AFTER GO AROUND ECAM "ENG 1 START VALVE FAULT. START VALVE NOT CLOSED" COMPLIED WITH ECAM ACTIONS. // PERF EEC OPS TEST NO.6 PER AMM 73-21-00-710-807-A. NO DEFECTS NOTED.
- [SDR HALA2019092320382](https://openairdocs.org/sdr/HALA2019092320382.md): Start Valve · open · Sep 22, 2019 · N208HA · Airbus A321271N · Engine Start Valves/Controls
  > ETOPS SIGNIFICANT SYSTEM - ENGINE 2 START VALVE FAULT, VALVE NOT CLOSED. REMOVED AND REPLACED STARTER ON ENGINE 2, PER AMM 80-11-01. OPS CHECK GOOD. OK TO CONTINUE.
- [SDR HALA2019082200350](https://openairdocs.org/sdr/HALA2019082200350.md): Fault Message · false activation · Aug 21, 2019 · N208HA · Airbus A321271N · Landing Gear Steering System
  > ATO - BRAKE SYSTEM 2 FAULT CAME ON @ TAKEOFF POWER. ABORTED TAKEOFF RESET A/SKID AND N/W STEG. RESET SUCCESSFUL. NO INBOUND FAULTS. PREFORMED TROUBLESHOOTING IN REF. WITH TSM 32-51-00-810-514-A. NO DEFECTS NOTED. OKAY FOR SERVICE.
- [SDR HALA2019070100338](https://openairdocs.org/sdr/HALA2019070100338.md): Smoke Warning · false activation · Jun 30, 2019 · N208HA · Airbus A321271N · Smoke Detection
  > LAVATORY SMOKE ECAM IN-FLIGHT, PAX SUSPECTED OF SMOKING IN LAV D. CHECKED LAV D SMOKE DETECTOR & WASTE BIN FIRE EX, NO FAULTS FOUND. PERFORMED CIDS SDF1 LAV SMOKE WARN TEST NO FAULTS. OK FOR SVC. REF AMM 26-17-00
- [SDR HALA2019050400214](https://openairdocs.org/sdr/HALA2019050400214.md): Smoke Warning · false activation · May 1, 2019 · N208HA · Airbus A321271N · Smoke Detection
  > LAV C SMOKE WARNING WENT OFF FOR SEVERAL SECONDS AND FA'S VERIFIED OPS NORMAL WITH NO SMELL. T/S PER TSM 26-16-17-00-810-812-A. OPS CKS GOOD, OK TO CONTINUE.
- [SDR HALA2019042500201](https://openairdocs.org/sdr/HALA2019042500201.md): Outflow Valve · faulted · Apr 24, 2019 · N208HA · Airbus A321271N · Pressure Regulator/Outflow Valve
  > ATB - VENT SKIN VALVE FAULT. // FOUND MAIN SKIN AIR OUTLET VALVE IN PARTIALLY OPEN POSITION, MANUALLY OPENED VALVE TO FULL OPEN. ACCOMPLISHED AEVC TEST TWICE, BOTH PASSED. VALVE OPS OK.
- [SDR HALA2019020500045](https://openairdocs.org/sdr/HALA2019020500045.md): Smoke Warning · false activation · Feb 4, 2019 · N208HA · Airbus A321271N · Smoke Detection
  > DURING FLIGHT LAV SMOKE WARNING, FA PANEL INDICATED LAV 1, NO SMOKE FOUND.// NO SMOKE DETECTED, NO SMOKE INDICATED. OK FOR SERVICE PER AMM26-17-01.
- [SDR HALA2018121700656](https://openairdocs.org/sdr/HALA2018121700656.md): Igniter · malfunctioned · Dec 14, 2018 · N208HA · Airbus A321271N · Spark Plug/Igniter
  > ETOPS SIGNIFICANT SYSTEM - BTB ENG 2 IGN A INOP. PERFORMED OPERATIONAL CHECK OF #2 ENGINE IGNITER "A" OPS CK NORMAL ON GROUND. OK TO CONTINUE. REF AMM 74-00-00 PB 501.
- [SDR HALA2018111400581](https://openairdocs.org/sdr/HALA2018111400581.md): Fire Loop · faulted · Nov 13, 2018 · N208HA · Airbus A321271N · Fire Detection
  > ETOPS SIGNIFICANT SYSTEM - ATB - DUE TO ENG. 2 LOOP "A" FAULT. // REMOVED AND REPLACED PYLON FIRE - DETECTOR RAMP ASSEMBLY PER AMM 26-12-16. EMPLOYEE# 3752 (11/14/18). OPERATIONAL CHECK PENDING. OPS CHECK GOOD PER AMM 26-12-00-710-002, FAULT WENT AWAY AND NO D

## 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 = 'N208HA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N208HA/reports

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