# Service difficulty reports: N188US

A list on [N188US](https://openairdocs.org/aircraft/N188US.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 6 · 285 reports

- [SDR AALA202609142372](https://openairdocs.org/sdr/AALA202609142372.md): Bottle · low pressure · Sep 10, 2026 · N188US · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: L4 DOOR ACCUMULATOR LOW. MAINTENANCE SERVICED ACCUMULATOR PER AMM 52-10-00.
- [SDR AALA202609142429](https://openairdocs.org/sdr/AALA202609142429.md): Bottle · low pressure · Sep 10, 2026 · N188US · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: L1 DOOR ACCUMULATOR LOW. MAINTENANCE SERVICED ACCUMULATOR PER AMM 52-10-00.
- [SDR AALA202607158540](https://openairdocs.org/sdr/AALA202607158540.md): Bottle · low pressure · Jul 12, 2026 · N188US · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: L4 DOOR DAMPER PRESSURE BELOW LIMIT. MAINTENANCE SERVICED L4 DOOR DAMPER PRESSURE TO SERVICEABLE LIMIT IAW JC 26L80052001.
- [SDR AALA202607155214](https://openairdocs.org/sdr/AALA202607155214.md): Bottle · low pressure · Jul 12, 2026 · N188US · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: L1 DOOR DAMPER PRESSURE BELOW LIMIT. MAINTENANCE SERVICED L1 DOOR DAMPER PRESSURE TO SERVICEABLE LIMIT IAW JC 26L80052001.
- [SDR AALA202605181529](https://openairdocs.org/sdr/AALA202605181529.md): Bottle · low pressure · May 17, 2026 · N188US · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER JOB CARD 26L80052001.
- [SDR AALA202605081023](https://openairdocs.org/sdr/AALA202605081023.md): Bottle · low pressure · May 6, 2026 · N188US · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
- [SDR AALA202605087719](https://openairdocs.org/sdr/AALA202605087719.md): Bottle · low pressure · May 6, 2026 · N188US · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: L4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
- [SDR AALA202604249265](https://openairdocs.org/sdr/AALA202604249265.md): Control Unit · faulty · Apr 23, 2026 · N188US · Airbus A321211 · Landing Gear Brake System
  > AIRCRAFT WAS NOT GROUNDED: FLIGHT CREW REPORTED THAT THE BRAKES VERY SLOW TO RESPOND EVEN WITH MODERATE PEDAL PRESSURE. WHEN INCREASING PRESSURE BEYOND NORMAL PEDAL INPUT BRAKES WILL SURGE. MAINTENANCE REPLACED BCSU PER AMM 32-42-34 AND ACCOMPLISHED A SATISFAC
- [SDR AALA202604085177](https://openairdocs.org/sdr/AALA202604085177.md): Bottle · low pressure · Apr 6, 2026 · N188US · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: L4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
- [SDR AALA202604083003](https://openairdocs.org/sdr/AALA202604083003.md): Bottle · low pressure · Apr 6, 2026 · N188US · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
- [SDR AALA202601215415](https://openairdocs.org/sdr/AALA202601215415.md): Bottle · low pressure · Jan 19, 2026 · N188US · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
- [SDR AALA202512177857](https://openairdocs.org/sdr/AALA202512177857.md): Deu · faulted · Dec 15, 2025 · N188US · Airbus A321211 · Emergency Equipment
  > AIRCRAFT IN BASE MAINTENANCE: DOOR 3L EVACUATION LIGHT ALWAYS ILLUMINATED. MAINTENANCE FOUND A FAULT MESSAGE FOR DECODER / ENCODER UNIT B 300RH4 (DEU) WAS DISPLAYED ON THE FLIGHT ATTENDANTS PANEL AND REPLACED THE DEU PER AMM 23-73-47. A SATISFACTORY OPERATIONA
- [SDR AALA202512160632](https://openairdocs.org/sdr/AALA202512160632.md): Bottle · low pressure · Dec 15, 2025 · N188US · Airbus A321211 · Emergency Exits
  > AIRCRAFT IN BASE MAINTENANCE: L2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
- [SDR AALA202512168253](https://openairdocs.org/sdr/AALA202512168253.md): Bottle · low pressure · Dec 15, 2025 · N188US · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
- [SDR AALA202512165479](https://openairdocs.org/sdr/AALA202512165479.md): Battery · no test · Dec 14, 2025 · N188US · Airbus A321211 · Emergency Lighting
  > AIRCRAFT IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY UNIT 13WL AND BATTERY ARE INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY UNIT 13WL (AALA202512159172) AND BATTERY (AALA202512165479) PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO
- [SDR AALA202512169172](https://openairdocs.org/sdr/AALA202512169172.md): Power Supply · no test · Dec 14, 2025 · N188US · Airbus A321211 · Emergency Lighting
  > AIRCRAFT IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY UNIT 13WL AND BATTERY ARE INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY UNIT 13WL (AALA202512159172) AND BATTERY (AALA202512165479) PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO
- [SDR AALA202512151139](https://openairdocs.org/sdr/AALA202512151139.md): Bottle · no test · Dec 11, 2025 · N188US · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 832 DAMPER AND EMERGENCY OPERATION CYLINDER FAILS THE DAMPING FUNCTION TEST. REPLACED DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-13-14.
- [SDR AALA202512081989](https://openairdocs.org/sdr/AALA202512081989.md): Bottle · no test · Dec 5, 2025 · N188US · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 831 DAMPER AND EMERGENCY OPERATION CYLINDER FAILS THE DAMPING FUNCTIONAL TEST. REPLACED DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-111-14.
- [SDR AALA202511280829](https://openairdocs.org/sdr/AALA202511280829.md): Fitting · cracked · Nov 25, 2025 · N188US · Airbus A321211 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED CENTER FUSELAGE PRESSURE DECK RIGHT HAND CORNER FITTING AT FR 36 AND -Y1292. REPLACED CORNER FITTING PER EA 368568.
- [SDR AALA202511280666](https://openairdocs.org/sdr/AALA202511280666.md): Fitting · cracked · Nov 25, 2025 · N188US · Airbus A321211 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED CENTER FUSELAGE PRESSURE DECK LEFT HAND CORNER FITTING AT FR 36 AND +Y1292. REPLACED CORNER FITTING PER EA 368568.
- [SDR AALA202511250158](https://openairdocs.org/sdr/AALA202511250158.md): Door Sill · corroded · Nov 24, 2025 · N188US · Airbus A321211 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL AT FR 66 AND S23R. REPLACED LOWER SILL PER SRM 51-42-11.
- [SDR AALA202512152228](https://openairdocs.org/sdr/AALA202512152228.md): Elec Connector · broken · Nov 23, 2025 · N188US · Airbus A321211 · Equipment/Furnishings Wiring
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT-HAND AFT EMERGENCY EXIT DOOR 844 INFLATION RESERVOIR HAS BROKEN ELECTRICAL CONNECTOR. MAINTENANCE REPLACED INFLATION RESERVOIR PER AMM 25-62-49.
- [SDR AALA202512028896](https://openairdocs.org/sdr/AALA202512028896.md): Bottle · no test · Nov 23, 2025 · N188US · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: AFT RIGHT PASSENGER / CREW DOOR 842 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER DOES NOT PASS THE DAMPING FUNCTION TEST. REPLACED DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-13-14.
- [SDR AALA202511203069](https://openairdocs.org/sdr/AALA202511203069.md): Bottle · no test · Nov 19, 2025 · N188US · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 841 DAMPER AND EMERGENCY OPERATION CYLINDER DOES NOT PASS THE OPERATIONAL TEST OF THE DAMPING FUNCTION. MAINTENANCE REPLACED DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-11-14. A SATISFACTORY OPERATIONA
- [SDR AALA202511134290](https://openairdocs.org/sdr/AALA202511134290.md): Splice · corroded · Oct 30, 2025 · N188US · Airbus A321211 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER, CREW DOOR CUTOUT LOWER SILL UPPER INBOARD SPLICE AT FR 66 AND S23L. REPLACED SPLICE PER SRM 51-42-11.
- [SDR AALA202511131224](https://openairdocs.org/sdr/AALA202511131224.md): Splice · corroded · Oct 30, 2025 · N188US · Airbus A321211 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUTOUT LOWER SILL UPPER OUTBOARD SPLICE AT FR 66 AND S23L. REPLACED SPLICE PER SRM 51-42-11.
- [SDR AALA202510249633](https://openairdocs.org/sdr/AALA202510249633.md): Fitting · none · Oct 21, 2025 · N188US · Airbus A321211 · Standard Practices/Structures
  > AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK CENTER WINDSHIELD FRAMING THE LEFT CONTINUITY FITTING BETWEEN AT FR 2 AND Y0 MUST BE REPLACED PER INSTRUCTIONS OUTLINED IN EO 5319Y017-002. REPLACED CONTINUITY FITTING
- [SDR AALA202510235597](https://openairdocs.org/sdr/AALA202510235597.md): Bellcrank · out of adjust · Oct 20, 2025 · N188US · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 842 TORSION BAR BELLCRANK COMPENSATION MECHANISM OUT OF ADJUSTMENT. MAINTENANCE ADJUSTED TORSION BAR BELLCRANK COMPENSATION MECHANISM PER AMM 52-13-21.
- [SDR AALA202512045135](https://openairdocs.org/sdr/AALA202512045135.md): Stringer · corroded · Oct 17, 2025 · N188US · Airbus A321211 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER BETWEEN FR 55 AND FR 56 AT S43L. REPAIRED STRINGER PER EA 203929A.
- [SDR AALA202510249828](https://openairdocs.org/sdr/AALA202510249828.md): Sleeve · worn · Oct 11, 2025 · N188US · Airbus A321211 · Nacelle/Pylon, Main Frame
  > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND PYLON AFT ATTACH FITTING UPPER SLEEVE WORN. REPLACED SLEEVE PER TASK CARD 26C41554028.
- [SDR AALA202511065247](https://openairdocs.org/sdr/AALA202511065247.md): Lug · worn · Oct 10, 2025 · N188US · Airbus A321211 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ELEVATOR #4 HINGE FITTING TAB LUG WORN. REPLACED TAB LUG PER SRM 55-26-41-300-002 AND CMM 55-21-15.
- [SDR AALA202510208403](https://openairdocs.org/sdr/AALA202510208403.md): Bellcrank · out of adjust · Oct 6, 2025 · N188US · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 831 TORSION BAR BELLCRANK COMPENSATION MECHANISM IS OUT OF ADJUSTMENT. ADJUSTED TORSION BAR BELLCRANK COMPENSATION MECHANISM PER AMM 52-11-21.
- [SDR AALA202510202922](https://openairdocs.org/sdr/AALA202510202922.md): Bellcrank · out of adjust · Oct 6, 2025 · N188US · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 841 TORSION BAR BELLCRANK COMPENSATION MECHANISM IS OUT OF ADJUSTMENT. ADJUSTED TORSION BAR BELLCRANK COMPENSATION MECHANISM PER AMM 52-11-21.
- [SDR AALA202511057065](https://openairdocs.org/sdr/AALA202511057065.md): Seat Track · corroded · Oct 3, 2025 · N188US · Airbus A321211 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MAIN CABIN FLOOR SEAT TRACK BETWEEN FR 47.1-AND FR 47.2 AT +Y1292. REPLACED SEAT TRACK PER SRM 51-72-11.
- [SDR AALA202511174602](https://openairdocs.org/sdr/AALA202511174602.md): Shear Plate · cracked · Oct 2, 2025 · N188US · Airbus A321211 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-72-11.
- [SDR AALA202511176520](https://openairdocs.org/sdr/AALA202511176520.md): Shear Plate · cracked · Oct 2, 2025 · N188US · Airbus A321211 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-72-11.
- [SDR AALA202511143211](https://openairdocs.org/sdr/AALA202511143211.md): Hinge Fitting · excess play · Oct 2, 2025 · N188US · Airbus A321211 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #6 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202511145292](https://openairdocs.org/sdr/AALA202511145292.md): Hinge Fitting · excess play · Oct 2, 2025 · N188US · Airbus A321211 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #3 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202511146056](https://openairdocs.org/sdr/AALA202511146056.md): Hinge Fitting · excess play · Oct 2, 2025 · N188US · Airbus A321211 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #2 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202511149445](https://openairdocs.org/sdr/AALA202511149445.md): Hinge Fitting · excess play · Oct 2, 2025 · N188US · Airbus A321211 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #5 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202511145057](https://openairdocs.org/sdr/AALA202511145057.md): Hinge Fitting · excess play · Oct 2, 2025 · N188US · Airbus A321211 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #4 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202511146732](https://openairdocs.org/sdr/AALA202511146732.md): Hinge Fitting · excess play · Oct 2, 2025 · N188US · Airbus A321211 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #1 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202511137693](https://openairdocs.org/sdr/AALA202511137693.md): Door Sill · corroded · Oct 2, 2025 · N188US · Airbus A321211 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER, CREW DOOR CUTOUT LOWER SILL AT FR 68 AND S23R. REPLACED LOWER SILL PER SRM 51-42-11.
- [SDR AALA202511135553](https://openairdocs.org/sdr/AALA202511135553.md): Door Sill · corroded · Oct 2, 2025 · N188US · Airbus A321211 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER, CREW DOOR CUTOUT LOWER SILL AT FR 66 AND S23L. REPLACED LOWER SILL PER SRM 51-42-11.
- [SDR AALA202511121943](https://openairdocs.org/sdr/AALA202511121943.md): Cleat · corroded · Oct 2, 2025 · N188US · Airbus A321211 · Fuselage Main, Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT CLEAT AT FR 32, AT S40R. REPLACED CLEAT PER SRM 51-72-11.
- [SDR AALA202511069514](https://openairdocs.org/sdr/AALA202511069514.md): Hinge Fitting · excess play · Oct 2, 2025 · N188US · Airbus A321211 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #1 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202511067821](https://openairdocs.org/sdr/AALA202511067821.md): Hinge Fitting · excess play · Oct 2, 2025 · N188US · Airbus A321211 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #4 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202511069118](https://openairdocs.org/sdr/AALA202511069118.md): Hinge Fitting · excess play · Oct 2, 2025 · N188US · Airbus A321211 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #6 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202511068495](https://openairdocs.org/sdr/AALA202511068495.md): Hinge Fitting · excess play · Oct 2, 2025 · N188US · Airbus A321211 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #3 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202511061949](https://openairdocs.org/sdr/AALA202511061949.md): Hinge Fitting · excess play · Oct 2, 2025 · N188US · Airbus A321211 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #5 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Next page: https://openairdocs.org/aircraft/N188US/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 = 'N188US' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N188US/reports

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