# Service difficulty reports: N216HA

A list on [N216HA](https://openairdocs.org/aircraft/N216HA.md).

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

- [SDR ASAA2026092166991](https://openairdocs.org/sdr/ASAA2026092166991.md): Outflow Valve · malfunctioned · Sep 21, 2026 · N216HA · Airbus A321271N · Pressure Regulator/Outflow Valve
  > ATB, AIRCRAFT UNABLE TO PRESSURIZE. ACCOMPLISHED BY VENT AVNCS SYS FAULT ECAM. ECAM ACTIONS COMPLETE HOWEVER STILL UNABLE TO PRESSURIZE. GROUNDED - YES. VERIFIED SKIN AIR OUTLET VALVE WAS SLIGHTLY OPEN. REAPPLIED MEL 21-26-04. VERIFIED MAIN FLAP CLOSED AND INT
- [SDR ASAA2026082366480](https://openairdocs.org/sdr/ASAA2026082366480.md): None · none · Aug 23, 2026 · N216HA · Airbus A321271NX · Standard Practices/Structures
  > LAV SMOKE ECAM, RAN ECAM ACTION. GROUNDED - YES. FLT CREW REPORTED PASSENGER CAUGHT SMOKING. NO FAULTS NOTED. INDICATIONS NORMAL. AMM 26-17-00.
- [SDR ASAA2025112061797](https://openairdocs.org/sdr/ASAA2025112061797.md): Battery · faulted · Nov 20, 2025 · N216HA · Airbus A321271N · Emergency Lighting
  > WHILE PER TASK CARD I321-7DAY-CHECK. FOUND 11WL & 13WL EPSU BATTERY FAULT. GROUNDED - YES. REMOVED AND REPLACED 11WL AND 13WL EPSU BATTERY IAW AMM 33-51-38. OPS GOOD. OK FOR SERVICE.
- [SDR HALA20251017321](https://openairdocs.org/sdr/HALA20251017321.md): Pump · failed · Oct 16, 2025 · N216HA · Airbus A321271N · Hydraulic Pump (Electric/Engine), Main
  > ETOPS - Y ENG 2 PUMP INOP. REMOVED AND REPLACED NR 2 ENG. DRIVEN HYD. PUMP CONDITION SAME. ACCOMP. TEST OF PTU W/ENG. PUMPS PER AMM 29-23-00-710-004-A. ALL ENG.DRIVEN HYD PUMPS,ELECT HYD. PUMPS & PTU OPS NORMAL OK FOR SERVICE. SECURED NR 2 ENG.COWLINGS. P/N OF
- [SDR HALA20251008308](https://openairdocs.org/sdr/HALA20251008308.md): Fire Loop · faulted · Oct 7, 2025 · N216HA · Airbus A321271N · Fire Detection
  > ETOPS - IN FLIGHT, ENG 1 FIRE LOOP B FAULT. REMOVED AND REPLACED #1 ENG PYLON FIRE DETECTOR RAMP ASSY PER AMM 26-12-16. OPS CHECK GOOD. OK FOR SERVICE.
- [SDR HALA20251001295](https://openairdocs.org/sdr/HALA20251001295.md): Sensor · faulted · Sep 30, 2025 · N216HA · Airbus A321271N · Engine Oil Pressure
  > ETOPS - ENG2 OIL SENSOR FAULT MESSAGE FLASHED SPORADICALLY DURING CRUISE. REPLACED PHMU PER AMM 77-31-01 ON RH ENGINE. PERFORMED IDLE AND OPS CHECK. OPS CHECK GOOD. OK TO CONTINUE.
- [SDR HALA20250618185](https://openairdocs.org/sdr/HALA20250618185.md): Line · damaged · Jun 17, 2025 · N216HA · Airbus A321271N · Compressor Bleed Valve
  > ETOPS - DURING ENGINE HARNESS REPLACEMENT FOUND HPC BLEED VALVE SOLENOID LINE DAMAGED. REMOVED 7 REPLACED HPC BVS LINE PER AMM 75-32-02-400-801A. LEAK CK GOOD. OK FOR SVC.
- [SDR HALA20250618186](https://openairdocs.org/sdr/HALA20250618186.md): Wire · damaged · Jun 16, 2025 · N216HA · Airbus A321271N · Engine Fuel System Wiring
  > ETOPS - DURING FOM FOUND WIRE DAMAGE ON #2 ENG N2 SENSOR O/B 4065KS-J64. FOUND WIRE BUNDLE DAMAGE ON #2 ENG BY TACC (FLAGGED) 4055KS-J31. REMOVED & REPLACED WIRE HARNESS W03 ON ENG #2 PER AMM 73-21-63. EEC OPS CK GOOD. OK FOR SVC
- [SDR HALA20250617033](https://openairdocs.org/sdr/HALA20250617033.md): Starter · leaking · Jun 15, 2025 · N216HA · Airbus A321271N · Engine Starter
  > EMERGENCY DECLARED. LOW OIL ENG #1 0.0 DECREASING FROM 18.0. AT SHUTDOWN ENG 1 QT 3.5. PILOT NOTED DURING EVENT OIL PSI 152 AND NO INFLIGHT SHUT DOWN PERFORMED. FOUND ENG STARTER LEAKING. REMOVED AND REPLACED PER AMM 80-11-01. LEAK AND OPS CHECK GOOD. ENGINE O
- [SDR HALA20250610174](https://openairdocs.org/sdr/HALA20250610174.md): Valve · faulted · Jun 9, 2025 · N216HA · Airbus A321271N · Engine Bleed Air System
  > ATB - AIR ENG BLEED 2 FAULT ECAM DURING CLIMBOUT @ MCT POWER PER WONT CLIMB PROC. UNABLE TTO RESET W/ ECAM OVERHEAT NOTED. T/S REMOVED & REPLACED #2 ENGINE FAN AIR VALVE IAW AMM 36-11-54-400-803-A.
- [SDR HALA20250423114](https://openairdocs.org/sdr/HALA20250423114.md): Display · intermittent · Apr 22, 2025 · N216HA · Airbus A321271N · Central Display
  > ETOPS-CAPTAIN'S MCDU 3L BUTTON WORKS ONLY INTERMITTENTLY. REMOVED AND REPLACED CAPT'S MCDU PER AMM 22-82-12. OPS CHECK GOOD, OK TO CONT. SERVICE.
- [SDR HALA20241126337](https://openairdocs.org/sdr/HALA20241126337.md): Fuel Filter · clogged · Nov 25, 2024 · N216HA · Airbus A321271N · Engine Fuel Distribution
  > ETOPS - INFO TO MX ON DEPARTURE CLIMB ENG 2 AMBER CLOG ANNUNCIATOR ILLUMINATED ON ENG SD PAGE. MESSAGE CLEARED AFTER A FEW MINS. PERFORMED TSM 73-11-00-810-822-A. REMOVED AND REPLAACED FUEL FILTER. FADEC SYSTEM IDLE TEST OK. NO LEAKS NOTED. OK FOR SVC.
- [SDR HALA20241104065](https://openairdocs.org/sdr/HALA20241104065.md): Smoke Detector · no discrepancy · Nov 1, 2024 · N216HA · Airbus A321271N · Smoke Detection
  > LAV SMOKE ECAM IN FLIGHT. ECAM CLEARED ITSELF AFTER 3 SECONDS, FA'S INVESTIGATED AND FOUND NO SOURCE OF FIRE. SUSPECT PAX VAPING. PERFORMED TSM 36-17-00-810-804-A NO DETECTORS FAULTING. NO FAULTS ON POST FLIGHT REPORT CLEANED DUST FROM ALL 4 LAVS. OK FOR SERVI
- [SDR HALA20241023296](https://openairdocs.org/sdr/HALA20241023296.md): Connector · inoperative · Oct 22, 2024 · N216HA · Airbus A321271N · Hydraulic Power System Wiring
  > ETOPS - BTB. HYD G ENG 1 PUMP LO PR INDICATION 8X ON TAXI OUT. HYD PAGE PUMP LOW PRESSURE PTU OPERATING SHOWING AMBER AND GREEN INDICATIONS ENG 1 PUMP FAULT LIGHT ON OFF THROUGH INDICATIONS. REMOVED AND REPLACED PRESSURE SWITCH PART #450-1-3100-00 AND ELECTRIC
- [SDR HALA20241015049](https://openairdocs.org/sdr/HALA20241015049.md): Latch · fod · Oct 13, 2024 · N216HA · Airbus A321271N · Escape Slide
  > 4R DOOR DISARMED DURING FLIGHT. WOULD NOT REARM. PERFORMED PRESSURIZATION CHECK WITH 4R DOOR ARMED. FOUND ARM/DISARM LEVER NOT FLUSH. FOUND SLIDE LOCK/LATCH BLOCKED WITH DEBRIS. RMEOVED DEBRIS. OPS CHECK OK. OK FOR SVC.
- [SDR HALA20240918259](https://openairdocs.org/sdr/HALA20240918259.md): Pressure Switch · loose · Sep 17, 2024 · N216HA · Airbus A330243 · Hydraulic Pump (Electric/Engine), Main
  > ETOPS-ECAM HYD G ENG 1 PUMP LO PR TURNED OFF ENG 1 PUMP AS INSTRUCTED BY ECAM. PERFORMED TSM 29-11-00-810-804-A, FOUND PRESSURE SWITCH LOOSE. REMOVED AND REPLACED ENG 1 PUMP PRESSURE SWITCH (1047GK) PER AMM 29-11-17. OPS CHECK AND LEAK CHECK GOOD, NO FAULT NOT
- [SDR HALA20240405086](https://openairdocs.org/sdr/HALA20240405086.md): Seal · leaking · Apr 4, 2024 · N216HA · Airbus A321271N · Engine (Turbine/Turboprop)
  > ETOPS - DURING WALK AROUND, FOUND OIL SEEPING FROM EN1 S/N: P770687 INLET CONE. UPON INSPECTION, FOUND OIL INSIDE INLET CONE. REMOVED & REPLACED FAN SHAFT COVER SEAL PER AMM 72-15-00-960-801-A. NO LEAKS NOTED POST IDLE RUN. OK FOR SERVICE.
- [SDR HALA20240311063](https://openairdocs.org/sdr/HALA20240311063.md): Selector · failed · Mar 9, 2024 · N216HA · Airbus A321271N · Cabin Temperature Control System
  > ETOPS-FORWARD TRIM AIR VALVE NOT RESPONDING APPROPIATELY TO SWITCH POSITION. TEMP IN CABIN HOT WITH FULL COLD SET. PREVIOUSLY WRITTEN UP, NO CHANGE. REMOVED AND REPLACED TEMPERATURE SELECTOR PER AMM 21-63-11-000-001-A (21315 3/8/24. PENDING OPS CHECK. PERFORME
- [SDR HALA20240311013](https://openairdocs.org/sdr/HALA20240311013.md): Connector · dirty · Mar 8, 2024 · N216HA · Airbus A321271N · Light System Wiring
  > AFT EXIT SIGN BURNT OUT AIRCRAFT LEFT SIDE. CLEANED AFT EXIT SIGN CONNECTORS. OPS CHECKED PER AMM 33-51-00 CHECK GOOD OK FOR SERVICE.
- [SDR HALA2026090300194](https://openairdocs.org/sdr/HALA2026090300194.md): Skin · corroded · Feb 13, 2024 · N216HA · Airbus A321271N · Wing, Plate/Skin
  > DURING PERFORMING A 3 YEAR CHECK AT SIAEP, AN OF INSPECTION AS PER B321-ZL-500-02-1, CORROSION WAS FOUND ON THE LT WING BOTTOM SKIN PANEL 2 BETWEEN RIBS 24-25. AFTER DAMAGE ASSESSMENT AS PER SRM 57-21-11-283-014, CONTACT WITH AIRBUS IS REQUIRED SINCE THE BLEND
- [SDR HALA2023072100155](https://openairdocs.org/sdr/HALA2023072100155.md): Pump · faulty · Jul 20, 2023 · N216HA · Airbus A321271N · Hydraulic Pump (Electric/Engine), Main
  > ETOPS - ENG #2 HYDRAULIC DRIPPING, 1 DRIP PER SECOND. REMOVED AND REPLACED ENG#2 HYD PUMP IAW AMM 29-13-51-000-806-A. ACCOMPLISHED ENG #2 IDLE RUN, NO LEAKS NOTED. AIRCRAFT OK FOR SERVICE.
- [SDR HALA2023051900111](https://openairdocs.org/sdr/HALA2023051900111.md): Unknown · unknown · May 18, 2023 · N216HA · Airbus A321271N · Fire Protection System
  > ETOPS - INFO TO MTX: ON CLIMB OUT MOMENTARY ECAM OF: ENG 1 FIRE LOOP A FAULT. CLEARED ITSELF UP AS WE BEGAN ECAM ACTIONS. INSTALLED NEW #1 ENG FIRE ELEC HARNESS ASSY. PER AMM TASK 26-12-61, OPS TEST OK.
- [SDR HALA2023051000024](https://openairdocs.org/sdr/HALA2023051000024.md): Unknown · unknown · May 9, 2023 · N216HA · Airbus A321271N · Fire Detection
  > INFO TO MX: DURING CRUISE BRIEF ECAM (2X) ENG.1 FIRE LOOP A FAULT. ECAMS CLEARED AFTER APPROX 3 SECS. NOTED BY MAINTENANCE. PERFORMED OPERATIONAL TEST OF THE ENG. FIRE AND OVERHEAT DETECTION TEST I.A.W. AMM 26-12-00-710-002-B. TEST O.K.
- [SDR HALA2023041300084](https://openairdocs.org/sdr/HALA2023041300084.md): Unknown · unknown · Apr 12, 2023 · N216HA · Airbus A321271N · Aircraft Fuel System
  > ATB - RIGHT WING FUEL AND TEMP INDICATIONS AMBER XX'S, FOB AMBER XX'S. ATTEMPTED QRH RESET WITH MX VIA SATCOM - UNSUCCESSFUL. REMOVED & REPLACED R WING TANK FUEL PROBES 30QT2 & 59QT2 PER AMM 28-42-15 R TANK INDICATION & FOB INDICATION & TEMP INDICATION SHOW NO
- [SDR HALA2023011900010](https://openairdocs.org/sdr/HALA2023011900010.md): Wire Harness · out of limits · Jan 18, 2023 · N216HA · Airbus A321271N · Fire Protection System Wiring
  > ETOPS-ENG B FIRE LOOP ON ECAM. CHECKED RESISTANCE BETWEEN PINS J-K AT FDU 2 LOOP B. FOUND RESISTANCE FLUCTUATING FRANTICALLY OUT OF LIMITS WHILE TAPPING HARNESS 4166KS. REMOVED & REPLACED HARNESS 4166KS PER AMM 26-12-62. RESISTANCE STAYED SOLID AT 1.5K OHMS. E
- [SDR HALA2023010300001](https://openairdocs.org/sdr/HALA2023010300001.md): Deu · faulted · Dec 31, 2022 · N216HA · Airbus A321271N · Waste Disposal System
  > ETOPS - ALL LAVATORIES NOT WORKING IN FLIGHT, HEADING BACK TO LAX. PERFORMED CIDS POWER UPTEST AND FAULTED 300RH8. REMOVED AND REPLACED DEU-B 300RH8 IAW AMM 23-73-47 PB 401, OPS CHECK OF ALL LAV AS OKAY. AC OK TO CONTINUE. ORIG SUB DATE: 1/3/2023
- [SDR HALA2022112100297](https://openairdocs.org/sdr/HALA2022112100297.md): Hpc · used · Nov 20, 2022 · N216HA · Airbus A321271N · Compressor Bleed Governor
  > ETOPS-DURING PDC FOUND #2 ENG LEAKING FUEL AT HPC PRIMARY STATOR VANE ACTUATOR. REMOVED AND REPLACED #2 ENG HPC PRIMARY STATOR VANE PER AMM 75-31-02-400-801-A. MECH 16488 / 21800. PENDING IDLE RUN / LEAK CHECK. COMPLETED IDLE RUN & LEAK CHECK PER AMM 71-00-00-
- [SDR HALA2022102200278](https://openairdocs.org/sdr/HALA2022102200278.md): Igniter · failed · Oct 22, 2022 · N216HA · Airbus A321271N · APU Start/Ignition System
  > ETOPS - APU AUTOSHUTDOWN - TRIED A SECOND TIME WITH ANOTHER AUTOSHUTDOWN. REMOVED AND REPLACED IGNITER AS PER AMM 49-41-41-400-0041-A, ALSO REMOVED AND REPLACED EXITER BOX AS PER AMM 49-41-38-400-003-A, PERFORMED OPS CHECK NORMAL. APU VERIFICATION FLIGHT FOR
- [SDR HALA2022102000277](https://openairdocs.org/sdr/HALA2022102000277.md): Sensor · faulted · Oct 19, 2022 · N216HA · Airbus A321271N · Pneumatic Distribution System
  > AIR ENG 1 HP VALVE FAULT. REPLACED PACK INLET PRESS SENSOR (LH) FIN (23HB1) PER AMM 21-51-13. LEAK CHECK OK. OPS PENDING 10-19-22 16801... REMOVED AND REPLACED #1 ENG HPV PER AMM 36-11-51. OPS AND LEAK CHECK PENDING 7880 10/18/22.. CONT ON LOG #895086 ITEM 1.
- [SDR HALA2022081200142](https://openairdocs.org/sdr/HALA2022081200142.md): None · none · Aug 11, 2022 · N216HA · Airbus A321271N · Fire Protection System
  > ETOPS - ENG 2 FIRE LOOP B FAULT DURING CLIMB @ 16000' PRIOR TO ETOPS ENTRY // REMOVED & REPLACED ENG 2 FIRE LOOP B AGB PER AMM 26-12-17. OPS TEST OF ENG FIRE & OVERHEAT DETECTION GOOD PER AMM 26-12-00. OK FOR SERVICE.
- [SDR HALA2022013100033](https://openairdocs.org/sdr/HALA2022013100033.md): Unknown · odor · Jan 28, 2022 · N216HA · Airbus A321271N · Air Distribution System
  > ON APPROACH STRONG SOCK SMELL LEVELING OFF @ 4000 IN COCKPIT AND FWD CABIN. PERSISTING THROUGH ENG SHUTDOWN // PERFORMED #1 & #2 ENG IDLE RUN PER AMM 71-00-00-860-823-A.OPERATIONAL CHECK OF #1 & #2 PACK PER AMM 21-51-00-710-002-A. NO SMELL NOTED. OK FOR SVC.
- [SDR HALA2022011200012](https://openairdocs.org/sdr/HALA2022011200012.md): Oil System · overserviced · Jan 11, 2022 · N216HA · Airbus A321271N · Turbine Engine Oil System
  > INFO TO MX ON DESCENT PASSING 5000' FAINT WET SOCK SMELL THROUGH AIR GASPRES. WENT AWAY AFTER A FEW MIN. FOUND ENG 1 OVER SERVICED BY APPROX 3 QTS. REMOVED EXCESS OIL FROM TANK. OPERATED ENG @ IDLE FOR FOR APPROX 5 MIN. NO SMELL. OK FOR SVC.
- [SDR HALA2021112200168](https://openairdocs.org/sdr/HALA2021112200168.md): None · none · Nov 19, 2021 · N216HA · Airbus A321271N · APU Start/Ignition System
  > ETOPS - APU SHUTDOWN PRIOR TO A/C REPOSITIONING // PERFORMED TSM 49-00-81-810-825-A NEED TO REPLACE IGNITION EXCITER PER PARAGRAGH 4A2A REMOVED AND REPLACED IGNITION EXCITER PER AMM 49-41-38. ALL CHECKS GOOD.
- [SDR HALA2021102500145](https://openairdocs.org/sdr/HALA2021102500145.md): Unknown · odor · Oct 22, 2021 · N216HA · Airbus A321271N · Air Distribution System
  > IMMEDIATELY AFTER ENGINE START (LIGHT) AND AFTER INITIATING DESCENT (STRONG) DIRTY SOCK SMELL IN COCKPIT. PERFORMED TROUBLESHOOTING OF ENGINES AFTER SMOKE/OIL FUMES IN THE CABIN PER TSM 71-00-00-810-847-A. RAN BOTH ENGINES 1&2 AND OPERATED ALL PAX SYSTEMS. N
- [SDR HALA2021040600044](https://openairdocs.org/sdr/HALA2021040600044.md): Battery · defective · Apr 5, 2021 · N216HA · Airbus A321271N · Emergency Lighting
  > EMER EQ - EPSU BATTERIES 11WL AND 13WL FAULTING // REMOVED AND REPLACED EPSU BATTERIES AT 11WL AND 13WL PER AMM 33-51-38-400-002-A. OK FOR SVC.
- [SDR HALA2019070800350](https://openairdocs.org/sdr/HALA2019070800350.md): Warning System · false activation · Jul 6, 2019 · N216HA · Airbus A321271N · Ignition System
  > ETOPS SIGNIFICANT SYSTEM - ENG 2 IGN B ECAM WENT THRU THE ALT START PROCEDURES. THE ECAM WENT AWAY (STATUS) AFTER ENGINE SHUTDOWN AT DESTINATION. PERFORMED OPS TEST OF THE ENG 2 IGN A+B PER AMM 74-00-00-710-802-A, OPS NORMAL. NO CURRENT FAULT DISPLAYED, OK FO
- [SDR HALA2019032500142](https://openairdocs.org/sdr/HALA2019032500142.md): Transducer · defective · Mar 22, 2019 · N216HA · Airbus A321271N · Elevator Control System
  > ATB - "F/CTL ELEV SERVO FAULT" ILLUMINATED ON CLIMB OUT. PERFORMED OPS TEST OF SIDE STICK ASSY PER AMM 27-96-00-710-020-A. PERFORMED WIRING CHK OF POS RVDT MON SIGNAL FROM ELAC 1 MON PART TO FIRST TERMINAL BLOCK REF 27-93-07. SWAP ELAC 1 AND ELAC 2 NO HELP SWA
- [SDR HALA2018121000636](https://openairdocs.org/sdr/HALA2018121000636.md): Transceiver · malfunctioned · Dec 9, 2018 · N216HA · Airbus A321271N · Weather Radar System
  > ETOPS SIGNIFICANT SYSTEM - CAPTAIN'S SIDE ND FLICKERS BETWEEN WX + TERRAIN WHEN TERRAIN SELECTED. // DURING T/S FOUND FLICKERING ONLY OCCURS WHILE WXR 2 IS ON. REMOVED AND REPLACED #2 WXR TRANSCEIVER IAW AMM 34-41-33 PB 401 CONF 01 OPS TEST GOOD, FLICKERING BE
- [SDR HALA2018121000637](https://openairdocs.org/sdr/HALA2018121000637.md): Transceiver · malfunctioned · Dec 8, 2018 · N216HA · Airbus A321271N · Weather Radar System
  > ETOPS SIGNIFICANT SYSTEM - WX + T + H AND TERR FLASH CONTINUOUSLY WHEN TERR ON ND IS SELECTED ON CA'S SIDE ND.// FOUND DEFECT ASSOCIATED WITH #2 RADAR SYS. RE-RACKED #2 WEATHER RADAR TRANSCEIVER "15Q2" DEFECT CLEARED. OPS CHECK GOOD. OK TO SERVICE
- [SDR HALA2018110100557](https://openairdocs.org/sdr/HALA2018110100557.md): Carbon Seal · missing · Oct 31, 2018 · N216HA · Airbus A321271N · Engine (Turbine/Turboprop)
  > ETOPS SIGNIFICANT SYSTEM - DURING BOROSCOPE INSPECTION OF #1 ENG FOUND AFT #3 BRG DRY FACE CARBON SEAL MISSING.// REPLACED #1 ENGINE PER TASK CARD J321-72-HWI -02. ALL REQUIRED TESTS CHECK OK. OK FOR SERVICE. ENGINE: IAE, PW1133G-JM.
- [SDR HALA2018103100554](https://openairdocs.org/sdr/HALA2018103100554.md): Control Valve · unknown · Oct 30, 2018 · N216HA · Airbus A321271N · Cabin Cooling System
  > ATB AT 8,000 ECAM, AIR FAULT PACK 2. REMOVED AND REPLACED PACK FLOW CONTROL VALVE PER AMM 21-51-51-400-001-A AND PERFORMED OPS TEST OF FLOW CONTROL AND INDICATING SYSTEM PER AMM 21-51-00-710-002-A. OPS CHECK GOOD OK FOR SERVICE.
- [SDR HALA2018102600546](https://openairdocs.org/sdr/HALA2018102600546.md): Warning System · false activation · Oct 25, 2018 · N216HA · Airbus A321271N · Door Warning System
  > ATB - AFT CARGO DOOR OPEN IN FLIGHT. INSPECTED DOOR, VERIFIED AFT CARGO DOOR CLOSED AND LOCKED PER AMM 52-70-00. PRESSURE CHECK OF AFT CARGO DOOR OK PER AMM 05-53-00-780-001-A. PERFORMED OVERWEIGHT LANDING INSPECTION PER AMM 05-51-11-200-004-B. NO DAMAGE NOTED
- [SDR HALA2018101600502](https://openairdocs.org/sdr/HALA2018101600502.md): Pressure Sensor · faulty · Oct 15, 2018 · N216HA · Airbus A321271N · Engine Oil Pressure
  > ETOPS SIGNIFICANT SYSTEM - ENGINE 1 OIL FILTER DEGRADE. (OIL FILTER DEGRADE CAUTION ON ECAM. REMOVED & REPLACED NR 1 OIL FILTER & NR 1 OIL FILTER DIFFERENTIAL PRESS SENSOR. ENG NR 1 OIL FILTER DEGRADE MESSAGE DID NOT RETURN. A/C IS OK FOR CONTINUE SERVICE.
- [SDR HALA2018101200492](https://openairdocs.org/sdr/HALA2018101200492.md): Proximity Switch · malfunctioned · Oct 11, 2018 · N216HA · Airbus A321271N · Door Warning System
  > OPEN - ATB - AFT CARGO OPEN WARNING IN CLIMB OUT 2500FT. ECAM DOOR PAGE INDICATIONS CARGO DOOR, (INDICATIONS MAY BE INOPERATIVE PROVIDED A VISUAL CHECK IS MADE BEFORE EACH DEPARTURE TO CONFIRM THAT DOORS ARE CLOSED AND LOCKED). SUP - ATB - PERFORMED ALTERNATI

## 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 = 'N216HA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N216HA/reports

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