# Service difficulty reports: N191UW

A list on [N191UW](https://openairdocs.org/aircraft/N191UW.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 · 283 reports

- [SDR AALA202610136650](https://openairdocs.org/sdr/AALA202610136650.md): Arming Lever · loose · Oct 11, 2026 · N191UW · Airbus A321211 · Emergency Exits
  > AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTED DOOR 2R ARMED LEVER LOOSE. MAINTENANCE SECURED DOOR 2R ARMED LEVER PER AMM 52-22-00.
- [SDR AALA202609185949](https://openairdocs.org/sdr/AALA202609185949.md): Ground Wire · broken · Sep 18, 2026 · N191UW · Airbus A321211 · Light System Wiring
  > AIRCRAFT WAS GROUNDED: WHILE CHECKING EMERGENCY LIGHTING FOR PERIODIC SERVICE CHECK FOUND SEATS 14 AND 15 SEAT MOUNT LIGHT INOPERATIVE - MAINTENANCE FOUND A BROKEN GROUND AT PLUG LOCATION 7260VC5-A AND REPAIRED PER ESPM 20-56-21. LIGHT OPS CHECK GOOD. OK FOR S
- [SDR AALA202609060309](https://openairdocs.org/sdr/AALA202609060309.md): Arming Lever · loose · Sep 4, 2026 · N191UW · Airbus A321211 · Emergency Exits
  > AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS ARM AND DISARM LEVER IS LOOSE ON DOOR 2R - MAINTENANCE READJUSTED THE ARM AND DIARM LEVER PER AMM 20-21-00
- [SDR AALA202608065760](https://openairdocs.org/sdr/AALA202608065760.md): Flashlight · no test · Aug 4, 2026 · N191UW · Airbus A321211 · Emergency Equipment
  > AIRCRAFT WAS NOT GROUNDED: FA L1 DOOR FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED FLASHLIGHT PER AMM 25-64-00.
- [SDR AALA202607216951](https://openairdocs.org/sdr/AALA202607216951.md): Handle · loose · Jul 18, 2026 · N191UW · Airbus A321211 · Emergency Exits
  > AIRCRAFT WAS NOT GROUNDED: DOOR 2R ARMED LEVER LOOSE. MAINTENANCE TIGHTENED HANDLE PER AMM 20-21-00 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
- [SDR AALA202606254961](https://openairdocs.org/sdr/AALA202606254961.md): Lever · loose · Jun 22, 2026 · N191UW · Airbus A321211 · Emergency Exits
  > AIRCRAFT WAS NOT GROUNDED: DOOR 2R ARMING LEVER LOOSE. MAINTENANCE RESECURED R2 DOOR ARMING LEVER HARDWARE PER AMM 52-20-00 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO ISSUES NOTED.
- [SDR AALA202605272826](https://openairdocs.org/sdr/AALA202605272826.md): Oven · dirty · May 23, 2026 · N191UW · Airbus A321211 · Buffet/Galleys
  > AIRCRAFT WAS NOT GROUNDED: NR 2 OVEN HAS BURNING SMELL WHEN TURNED ON. MAINTENANCE SCRUBBED, SANITIZED AND DISINFECTED THE FORWARD GALLY OVEN #2 PER CMM 25-33-01. A SATISFACTORY OPERATIONAL CHECK OF THE OVEN WAS ACCOMPLISHED WITH NO BURNING SMELL DETECTED.
- [SDR AALA202605012089](https://openairdocs.org/sdr/AALA202605012089.md): Strut · out of adjust · Apr 29, 2026 · N191UW · Airbus A321211 · Trailing Edge Flaps
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED INTO DFW DUE TO THE FLIGHT CREW REPORTING THAT DURING APPROACH A FLIGHT CONTROL FLAPS LOCKED - ALIGNMENT FAULT ECAM DISPLAYED, DURING EXTENSION FROM FLAPS 1 TO FLAPS 2. SLATS INDICATED FULLY EXTENDED AT 2, FLAPS
- [SDR AALA202602164902](https://openairdocs.org/sdr/AALA202602164902.md): Warning Message · illuminated · Feb 15, 2026 · N191UW · Airbus A321211 · Central Warning
  > AIRCRAFT WAS NOT GROUNDED: AN EMERGENCY WAS DECLARED INBOUND INTO PHX DUE TO THE FLIGHT CREW REPORTING THAT DURING DESCENT THAT A FLIGHT CONTROL SPEED BRAKE NR 3 & 4 FAULT DISPLAYED. MAINTENANCE TROUBLESHOT PER TSM 27-60-00-810-801-A AND REPORTED THAT ALL FAUL
- [SDR AALA202602105353](https://openairdocs.org/sdr/AALA202602105353.md): Handle · loose · Feb 9, 2026 · N191UW · Airbus A321211 · Emergency Exits
  > AIRCRAFT WAS NOT GROUNDED: DOOR 2R ARM/DISARM HANDLE IS LOOSE. MAINTENANCE RESECURED R2 DOOR ARMING LEVER HANDLE PER AMM 52-10-00.
- [SDR AALA202601125153](https://openairdocs.org/sdr/AALA202601125153.md): Union · sheared · Jan 10, 2026 · N191UW · Airbus A321211 · Hydraulic System, Main
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED ON FINAL APPROACH INTO DFW DUE TO THE FLIGHT CREW REPORTING THAT AFTER LOWERING THE GEAR A YELLOW HYDRAULIC SYSTEM RESERVOIR LOW LEVEL ECAM MESSAGE DISPLAYED AND THAT ALL HYDRAULIC FLUID WAS LOST FOR THE YELLOW
- [SDR AALA202510274921](https://openairdocs.org/sdr/AALA202510274921.md): Transceiver · inoperative · Oct 24, 2025 · N191UW · Airbus A321211 · Weather Radar System
  > AIRCRAFT IN BASE MAINTENANCE: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW DUE TO THE FLIGHT CREW REPORTING THAT THE RADAR NOT WORKING IN AIR. IT SHOWED GROUND CLUTTER BUT NO RADAR RETURN WITH STORMS IN FRONT OF US. RADAR LOOKED PIXILATED LIKE IT
- [SDR AALA202510064455](https://openairdocs.org/sdr/AALA202510064455.md): Accumulator · low pressure · Oct 3, 2025 · N191UW · Airbus A321211 · Service Doors
  > AIRCRAFT WAS NOT GROUNDED: FOUND R4 DOOR ACCUMULATOR PRESSURE LOW PER PS CHECK. MAINTENANCE SERVICED R4 DOOR ACCU. TO PROPER LEVEL REF AMM 52-10-00.
- [SDR AALA202510066934](https://openairdocs.org/sdr/AALA202510066934.md): Accumulator · low pressure · Oct 3, 2025 · N191UW · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: FOUND L4 DOOR ACCUMULATOR PRESSURE LOW PER PS CHECK. MAINTENANCE SERVICED L4 DOOR ACCU. TO PROPER LEVEL REF AMM 52-10-00.
- [SDR AALA202510063790](https://openairdocs.org/sdr/AALA202510063790.md): Accumulator · low pressure · Oct 3, 2025 · N191UW · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: FOUND L1 DOOR ACCUMULATOR PRESSURE LOW PER PS CHECK. MAINTENANCE SERVICED L1 DOOR ACCU. TO PROPER LEVEL REF AMM 52-10-00.
- [SDR AALA202505191162](https://openairdocs.org/sdr/AALA202505191162.md): Fitting · sticking · May 18, 2025 · N191UW · Airbus A321211 · Emergency Equipment
  > AIRCRAFT WAS NOT GROUNDED: DOOR 4R ARMING LEVER IS HARD TO ARM AND DISARM. MAINTENANCE CLEANED DEBRIS AND LUBRICATED GIRT FITTINGS PER AMM 52-10-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
- [SDR AALA202504096933](https://openairdocs.org/sdr/AALA202504096933.md): Light · no test · Apr 8, 2025 · N191UW · Airbus A321211 · Emergency Lighting
  > AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 832 SLIDE FAILED EMERGENCY LIGHTING SYSTEM TEST. REPLACED SLIDE ASSEMBLY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM PER TASK CARD 26L00025010.
- [SDR AALA202502289544](https://openairdocs.org/sdr/AALA202502289544.md): Fitting · worn · Feb 24, 2025 · N191UW · Airbus A321211 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT AFT PASSENGER / CREW DOOR CUTOUT LOWER SILL AFT CORNER SHAPE FITTING HAS ELONGATED FASTENER HOLES AT FR 68 AND S23R. REPLACED CORNER SHAPE FITTING PER SRM 51-42-11.
- [SDR AALA202503055779](https://openairdocs.org/sdr/AALA202503055779.md): Bolt · corroded · Feb 21, 2025 · N191UW · Airbus A321211 · Leading Edge Devices
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #7 LOWER BOLT AT RIB 14. REPLACED BOLT PER AMM 27-84-65.
- [SDR AALA202502041102](https://openairdocs.org/sdr/AALA202502041102.md): Hinge Fitting · excess play · Jan 31, 2025 · N191UW · 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 AALA202502020519](https://openairdocs.org/sdr/AALA202502020519.md): Hinge Fitting · excess play · Jan 30, 2025 · N191UW · 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 AALA202502017111](https://openairdocs.org/sdr/AALA202502017111.md): Hinge Fitting · excess play · Jan 30, 2025 · N191UW · 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 AALA202502018644](https://openairdocs.org/sdr/AALA202502018644.md): Hinge Fitting · excess play · Jan 30, 2025 · N191UW · 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 AALA202502018949](https://openairdocs.org/sdr/AALA202502018949.md): Hinge Fitting · excess play · Jan 30, 2025 · N191UW · 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 AALA202502019453](https://openairdocs.org/sdr/AALA202502019453.md): Hinge Fitting · excess play · Jan 30, 2025 · N191UW · 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 AALA202502034711](https://openairdocs.org/sdr/AALA202502034711.md): Cleat · corroded · Jan 29, 2025 · N191UW · Airbus A321211 · Fuselage Main, Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT CLEAT AT FR 32 BETWEEN S39R AND S40R. REPLACED CLEAT PER SRM 51-72-11.
- [SDR AALA202502020443](https://openairdocs.org/sdr/AALA202502020443.md): Hinge Fitting · excess play · Jan 25, 2025 · N191UW · 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 AALA202502023374](https://openairdocs.org/sdr/AALA202502023374.md): Hinge Fitting · excess play · Jan 25, 2025 · N191UW · 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 AALA202502026249](https://openairdocs.org/sdr/AALA202502026249.md): Hinge Fitting · excess play · Jan 25, 2025 · N191UW · 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.
- [SDR AALA202502027500](https://openairdocs.org/sdr/AALA202502027500.md): Hinge Fitting · excess play · Jan 25, 2025 · N191UW · 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 AALA202502029166](https://openairdocs.org/sdr/AALA202502029166.md): Hinge Fitting · excess play · Jan 25, 2025 · N191UW · Airbus A321211 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #2 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202502020499](https://openairdocs.org/sdr/AALA202502020499.md): Hinge Fitting · excess play · Jan 25, 2025 · N191UW · 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 AALA202504082887](https://openairdocs.org/sdr/AALA202504082887.md): Skin Panel · corroded · Jan 22, 2025 · N191UW · Airbus A321211 · Wing, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN PANEL #2 LOWER SURFACE AT RIB 14. REPAIRED SKIN PANEL PER EA 362006.
- [SDR AALA202504082364](https://openairdocs.org/sdr/AALA202504082364.md): Skin Panel · corroded · Jan 22, 2025 · N191UW · Airbus A321211 · Wing, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN PANEL #2 LOWER SURFACE AT RIB 7. REPAIRED SKIN PANEL PER EA 362006.
- [SDR AALA202504080175](https://openairdocs.org/sdr/AALA202504080175.md): Skin Panel · corroded · Jan 22, 2025 · N191UW · Airbus A321211 · Wing, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN PANEL #2 LOWER SURFACE AT RIB 10. REPAIRED SKIN PANEL PER EA 362006.
- [SDR AALA202503268689](https://openairdocs.org/sdr/AALA202503268689.md): Pressure Deck · cracked · Jan 19, 2025 · N191UW · Airbus A321211 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED CENTER FUSELAGE PRESSURE DECK MEMEBRANE OPEN HOLES AT FR 36 AND +Y1292. REPAIRED PRESSURE DECK MEMBRANE PER EA 361440.
- [SDR AALA202504015227](https://openairdocs.org/sdr/AALA202504015227.md): Shear Plate · cracked · Jan 16, 2025 · N191UW · 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 AALA202503033063](https://openairdocs.org/sdr/AALA202503033063.md): Door Sill · corroded · Jan 16, 2025 · N191UW · Airbus A321211 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUT OUT LOWER SILL BETWEEN FR 66 AND FR 68 AT S23R. REPLACED LOWER SILL PER SRM 51-42-11.
- [SDR AALA202502242494](https://openairdocs.org/sdr/AALA202502242494.md): Fitting · corroded · Jan 16, 2025 · N191UW · Airbus A321211 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL CENTER SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23R. REPLACED CENTER SHAPE FITTING PER SRM 51-42-11.
- [SDR AALA202502114505](https://openairdocs.org/sdr/AALA202502114505.md): Floor Support · corroded · Jan 15, 2025 · N191UW · Airbus A321211 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM BETWEEN FR 12 AND FR 16 AT +Y503.2. REPLACED FLOOR BEAM PER SRM 51-42-11.
- [SDR AALA202502023446](https://openairdocs.org/sdr/AALA202502023446.md): Cleat · corroded · Jan 13, 2025 · N191UW · Airbus A321211 · Fuselage Main, Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT CLEAT AT FR 35.6 BETWEEN S40R AND S41R. REPLACED CLEAT PER SRM 51-42-11.
- [SDR AALA202501315906](https://openairdocs.org/sdr/AALA202501315906.md): Cleat · corroded · Jan 13, 2025 · N191UW · Airbus A321211 · Fuselage Main, Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT CLEAT AT FR 32 BETWEEN S42R AND S43R. REPLACED CLEAT PER SRM 51-42-11.
- [SDR AALA202501310007](https://openairdocs.org/sdr/AALA202501310007.md): Cleat · corroded · Jan 13, 2025 · N191UW · Airbus A321211 · Fuselage Main, Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT CLEAT AT FR 35.4 BETWEEN S40R AND S41R. REPLACED CLEAT PER SRM 51-42-11.
- [SDR AALA202501318942](https://openairdocs.org/sdr/AALA202501318942.md): Cleat · corroded · Jan 13, 2025 · N191UW · Airbus A321211 · Fuselage Main, Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT CLEAT AT FR 35.3 BETWEEN S40R AND S41R. REPLACED CLEAT PER SRM 51-42-11.
- [SDR AALA202501243484](https://openairdocs.org/sdr/AALA202501243484.md): Cleat · corroded · Jan 13, 2025 · N191UW · Airbus A321211 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT CLEAT AT FR 35.5 BETWEEN S40R AND S41R. REPLACED CLEAT PER SRM 51-42-11.
- [SDR AALA202501248505](https://openairdocs.org/sdr/AALA202501248505.md): Cleat · corroded · Jan 13, 2025 · N191UW · Airbus A321211 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT CLEAT AT FR 35.3 BETWEEN S41R AND S42R. REPLACED CLEAT PER SRM 51-42-11.
- [SDR AALA202501237591](https://openairdocs.org/sdr/AALA202501237591.md): Cleat · corroded · Jan 13, 2025 · N191UW · Airbus A321211 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT CLEAT AT FR 29 BETWEEN S42R AND S43R. REPLACED CLEAT PER SRM 51-42-11.
- [SDR AALA202504044249](https://openairdocs.org/sdr/AALA202504044249.md): Fitting · worn · Jan 12, 2025 · N191UW · Airbus A321211 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: AFT AVIONIC COMPARTMENT RACK 80VU RIGHT HAND LATERAL FITTING WORN BETWEEN FR 23 AND FR 24 AT S32R. REPLACED RIGHT HAND LATERAL FITTING PER EA 361842.
- [SDR AALA202504065050](https://openairdocs.org/sdr/AALA202504065050.md): Fitting · worn · Jan 11, 2025 · N191UW · Airbus A321211 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: AFT AVIONIC COMPARTMENT RACK 80VU LEFT HAND LATERAL FITTING WORN BETWEEN FR 23 AND FR 24 AT S32L. REPLACED LEFT HAND LATERAL FITTING PER EA 361842.
- [SDR AALA202408214363](https://openairdocs.org/sdr/AALA202408214363.md): Handle · loose · Aug 20, 2024 · N191UW · Airbus A321211 · Emergency Exits
  > AIRCRAFT WAS NOT GROUNDED: 2R DOOR ENTRY DOOR HANDLE LOOSE. RESECURED EMERGENCY CONTROL HANDLE

Next page: https://openairdocs.org/aircraft/N191UW/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 = 'N191UW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N191UW/reports

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