# Service difficulty reports: N181UW

A list on [N181UW](https://openairdocs.org/aircraft/N181UW.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 8 · 362 reports

- [SDR AALA202610060329](https://openairdocs.org/sdr/AALA202610060329.md): Bottle · low pressure · Oct 2, 2026 · N181UW · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: CIDS CAUTION LIGHT RED - MAINTENANCE SERVICED THE MID LEFT DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00 WHICH CLEARED THE CAUTION RED LIGHT
- [SDR AALA202609140895](https://openairdocs.org/sdr/AALA202609140895.md): Bottle · low pressure · Sep 8, 2026 · N181UW · Airbus A321211 · Emergency Exits
  > AIRCRAFT WAS NOT GROUNDED: CIDS LIGHT ON FLIGHT ATTENDANTS FORWARD PANEL - MAINTENANCE FOUND BOTTLE DOOR MID LEFT INDICATION ON THE CIDS PANEL AND SERVICED THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-22-00 WHICH EXTINGUISHED THE FAULT LIGHT ON
- [SDR AALA202607275470](https://openairdocs.org/sdr/AALA202607275470.md): Arming Lever · sticking · Jul 24, 2026 · N181UW · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: DOOR 4R ARMING LEVER HARD TO PUSH DOWN. MAINTENANCE CHECKED DOOR ARMING LEVER FOR ANY RESISTANCE AND LUBRICATED THE DOOR ARMING DISARMING MECHANISM PER AMM 12-22-52. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
- [SDR AALA202607226996](https://openairdocs.org/sdr/AALA202607226996.md): Bottle · low pressure · Jul 21, 2026 · N181UW · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT WAS GROUNDED: CIDS PANEL CAUTION LIGHT ON. MAINTENANCE SERVICED THE L2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
- [SDR AALA202607063707](https://openairdocs.org/sdr/AALA202607063707.md): Elec Connector · loose · Jul 1, 2026 · N181UW · Airbus A321211 · Light System Wiring
  > AIRCRAFT WAS NOT GROUNDED: OVERHEAD EMERGENCY LIGHT AT ROW 28 INOPERATIVE. MAINTENANCE FOUND CONNECTORS LOOSE, RESECURED CONNECTORS AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM PER AMM 33-51-00 WITH NO ISSUES NOTED.
- [SDR AALA202606120059](https://openairdocs.org/sdr/AALA202606120059.md): Flashlight · not seated · Jun 10, 2026 · N181UW · Airbus A321211 · Emergency Equipment
  > AIRCRAFT WAS NOT GROUNDED: ONE FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT IS NOT BLINKING RED LIGHT, NEAREST THE CABIN DOOR 1L. MAINTENNACE RESEATED FORWARD OUTBOARD FLASHLIGHT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-65-00.
- [SDR AALA202604205497](https://openairdocs.org/sdr/AALA202604205497.md): Arming Lever · loose · Apr 15, 2026 · N181UW · Airbus A321211 · Emergency Exits
  > AIRCRAFT WAS NOT GROUNDED: DOOR 3R ARMING LEVER LOOSE. MAINTENANCE TIGHTENED LEVER AS REQUIRED.
- [SDR AALA202604201095](https://openairdocs.org/sdr/AALA202604201095.md): Bottle · low pressure · Apr 15, 2026 · N181UW · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: CIDS CAUTION ON FLIGHT ATTENDANTS PANEL. MAINTENANCE SERVICED L2 EMERGENCY EXIT DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER WORK CARD 26L80052003,
- [SDR AALA202603046214](https://openairdocs.org/sdr/AALA202603046214.md): Fitting · lack of lube · Mar 3, 2026 · N181UW · Airbus A321211 · Emergency Equipment
  > AIRCRAFT WAS NOT GROUNDED: L4 ARMING DOOR LEVER DOES NOT STAY DISARMED (UP). SLOWLY FALLS DOWN. MAINTENANCE REPOSITIONED GIRT BAR INTO FLOOR FITTING & LUBRICATED FLOOR FITTINGS IAW AMM 25-62-44. A SATISFACTORY OPS CHECK OF THE L4 DOOR ARMING SYSTEM ACCOMPLIS
- [SDR AALA202512161290](https://openairdocs.org/sdr/AALA202512161290.md): Bottle · low pressure · Dec 13, 2025 · N181UW · Airbus A321211 · Door Warning System
  > AIRCRAFT WAS GROUNDED: CIDS CAUTION LIGHT ILLUMINATED. MAINTENANCE FOUND L2 EMERGENCY PASSENGER DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW AND SERVICED IT PER AMM 52-10-00.
- [SDR AALA202507107202](https://openairdocs.org/sdr/AALA202507107202.md): Power Supply · no test · Jul 9, 2025 · N181UW · Airbus A321211 · Emergency Lighting
  > AIRCRAFT IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY UNIT 14WL INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY UNIT 14WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.
- [SDR AALA202507096888](https://openairdocs.org/sdr/AALA202507096888.md): Bottle · no test · Jul 8, 2025 · N181UW · Airbus A321211 · Emergency Exits
  > AIRCRAFT IN BASE MAINTENANCE: EMERGENCY EXIT DOOR 844, DOOR DAMPER AND EMERGENCY OPERATION CYLINDER STRIKER LEVER MECHANISM DOES NOT WORK CORRECTLY. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-22-14/
- [SDR AALA202507084547](https://openairdocs.org/sdr/AALA202507084547.md): Mount · worn · Jul 5, 2025 · N181UW · Airbus A321211 · Wing Main, Frame Structure
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT WING TRAILING EDGE PANEL #3 LOWER SURFACE PYLON MOUNTING PLATE SYSTEM FEED THRU HOLES WORN BETWEEN RIB 7 AND RIB 8. REPLACED MOUNTING PLATE PER SRM 57-21-11-300-005.
- [SDR AALA202506278091](https://openairdocs.org/sdr/AALA202506278091.md): Plug · missing · Jun 26, 2025 · N181UW · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 831 (L1) DOOR DAMPER AND EMERGENCY OPERATION CYLINDER GAGE MISSING PLUG. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-11-14.
- [SDR AALA202506236106](https://openairdocs.org/sdr/AALA202506236106.md): Plate · cracked · Jun 17, 2025 · N181UW · Airbus A321211 · Fuselage Main, Keel
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED KEEL BEAM RIGHT HAND SIDE LOWER HOLES OF PLATE CONNECTING IN MAIN WHEEL WELL AT FR 42 AND X18992.7. REPLACED PLATE PER SRM 651-72-11.
- [SDR AALA202506111653](https://openairdocs.org/sdr/AALA202506111653.md): Attach Fitting · worn · Jun 8, 2025 · N181UW · Airbus A321211 · Nacelle/Pylon, Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND PYLON INBOARD MIDDLE ATTACHMENT FITTING FOR THE THRUST REVERSER BEARING HAS MIGRATED. REPLACED FITTING PER AMM 54-57-17.
- [SDR AALA202506119868](https://openairdocs.org/sdr/AALA202506119868.md): Attach Fitting · worn · Jun 8, 2025 · N181UW · Airbus A321211 · Nacelle/Pylon, Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND PYLON INBOARD AFT ATTACHMENT FITTING FOR THE THRUST REVERSER BEARING HAS MIGRATED. REPLACED FITTING PER AMM 54-57-17.
- [SDR AALA202506113846](https://openairdocs.org/sdr/AALA202506113846.md): Attach Fitting · worn · Jun 8, 2025 · N181UW · Airbus A321211 · Nacelle/Pylon, Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND PYLON OUTBOARD MIDDLE ATTACHMENT FITTING FOR THE THRUST REVERSER BEARING HAS MIGRATED. REPLACED FITTING PER AMM 54-57-17.
- [SDR AALA202506114229](https://openairdocs.org/sdr/AALA202506114229.md): Attach Fitting · worn · Jun 8, 2025 · N181UW · Airbus A321211 · Nacelle/Pylon, Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND PYLON OUTBOARD AFT ATTACHMENT FITTING FOR THE THRUST REVERSER BEARING HAS MIGRATED. REPLACED FITTING PER AMM 54-57-17.
- [SDR AALA202506118617](https://openairdocs.org/sdr/AALA202506118617.md): Attach Fitting · worn · Jun 8, 2025 · N181UW · Airbus A321211 · Engine Thrust Reverser
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND PYLON INBOARD AFT ATTACHMENT FITTING FOR THE THRUST REVERSER BEARING HAS MIGRATED. REPLACED FITTING PER AMM 54-57-17.
- [SDR AALA202507084130](https://openairdocs.org/sdr/AALA202507084130.md): Mount · worn · Jun 4, 2025 · N181UW · Airbus A321211 · Wing Main, Frame Structure
  > AIRCRAFT IN BASE MAINTENANCE: LEFT WING TRAILING EDGE PANEL #3 LOWER SURFACE PYLON MOUNTING PLATE SYSTEM FEED THRU HOLES WORN BETWEEN RIB 7 AND RIB 8. REPLACED MOUNTING PLATE PER SRM 57-21-11-300-005.
- [SDR AALA202505308843](https://openairdocs.org/sdr/AALA202505308843.md): Coupling · corroded · May 27, 2025 · N181UW · Airbus A321211 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON UPPER OUTBOARD SPLICE COUPLING AT FR 66 AND S23R. REPLACED SPLICE COUPLING PER SRM 51-72-11.
- [SDR AALA202505216669](https://openairdocs.org/sdr/AALA202505216669.md): Bolt · corroded · May 19, 2025 · N181UW · Airbus A321211 · Leading Edge Devices
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE #9 SLAT TRACK FORWARD BOLT AT WS 10204 AND RIB 19. REPLACED BOLT PER TASK CARD 26C61057005.
- [SDR AALA202505216765](https://openairdocs.org/sdr/AALA202505216765.md): Bolt · corroded · May 17, 2025 · N181UW · Airbus A321211 · Leading Edge Devices
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE #3 SLAT TRACK UPPER BOLT AT WS 2580 AND RIB 5. REPLACED BOLT PER TASK CARD 26C61057005.
- [SDR AALA202505213617](https://openairdocs.org/sdr/AALA202505213617.md): Bolt · corroded · May 17, 2025 · N181UW · Airbus A321211 · Leading Edge Devices
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE #4 SLAT TRACK UPPER BOLT AT WS 3059 AND RIB 6. REPLACED BOLT PER TASK CARD 26C61057005.
- [SDR AALA202506064967](https://openairdocs.org/sdr/AALA202506064967.md): Seat Track · corroded · May 10, 2025 · N181UW · Airbus A321211 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION PASSENGER CABIN FLOOR SEAT TRACK BETWEEN FR 56 AND FR 57 AT +Y1292. REPLACED SEAT TRACK PER SRM 51-42-11.
- [SDR AALA202506278578](https://openairdocs.org/sdr/AALA202506278578.md): Skin Panel · corroded · May 9, 2025 · N181UW · Airbus A321211 · Fuselage Main, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON UPPER FUSELAGE EXTERNAL SKIN PANEL BETWEEN FR 69 AND FR 70, BETWEEN S1L AND S2L. REPAIRED SKIN PANEL PER EA 365391.
- [SDR AALA202506036187](https://openairdocs.org/sdr/AALA202506036187.md): Fitting · cracked · May 6, 2025 · N181UW · Airbus A321211 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT FR 20 RIGHT AT THE #7 DOOR STOP FITTING AREA. REPLACED INTERCOSTAL FITTING PER SRM 51-42-11.
- [SDR AALA202506022759](https://openairdocs.org/sdr/AALA202506022759.md): Seat Track · corroded · May 6, 2025 · N181UW · Airbus A321211 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR SEAT TRACK AT FR 20 AND -Y765. REPLACED SEAT TRACK PER SRM 51-72-11.
- [SDR AALA202505283576](https://openairdocs.org/sdr/AALA202505283576.md): Fitting · cracked · May 6, 2025 · N181UW · Airbus A321211 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT FR 16 LEFT BETWEEN Z1051 AND Z1330 AT THE #7 DOOR STOP FITTING. REPLACED INTERCOSTAL FITTING PER SRM 51-72-11.
- [SDR AALA202507085382](https://openairdocs.org/sdr/AALA202507085382.md): Shear Plate · cracked · May 5, 2025 · N181UW · 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 51-42-11.
- [SDR AALA202506138809](https://openairdocs.org/sdr/AALA202506138809.md): Shear Plate · cracked · May 5, 2025 · N181UW · 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 AALA202506026226](https://openairdocs.org/sdr/AALA202506026226.md): Door Sill · corroded · May 5, 2025 · N181UW · Airbus A321211 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT PASSENGER / CREW DOOR CUTOUT LOWER SILL BETWEEN FR 66 AND FR 68 AT S23L. REPLACED LOWER SILL PER SRM 51-72-11.
- [SDR AALA202506020760](https://openairdocs.org/sdr/AALA202506020760.md): Door Sill · corroded · May 5, 2025 · N181UW · Airbus A321211 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT AFT PASSENGER / CREW DOOR CUTOUT LOWER SILL BETWEEN FR 66 AND FR 68 AT S23R. REPLACED LOWER SILL PER SRM 51-72-11.
- [SDR AALA202505302377](https://openairdocs.org/sdr/AALA202505302377.md): Fitting · corroded · May 5, 2025 · N181UW · Airbus A321211 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT PASSENGER / CREW DOOR CUTOUT LOWER SILL CENTER SHAPE FITTING BETWEEN FR 66 AND FRF 68 AT S23L. REPLACED CENTER SHAPE FITTING PER SRM 51-72-11.
- [SDR AALA202505289476](https://openairdocs.org/sdr/AALA202505289476.md): Hinge Arm · excess play · May 5, 2025 · N181UW · Airbus A321211 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR 3 HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42.
- [SDR AALA202505284805](https://openairdocs.org/sdr/AALA202505284805.md): Hinge Arm · excess play · May 5, 2025 · N181UW · Airbus A321211 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR 2 HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42.
- [SDR AALA202505281437](https://openairdocs.org/sdr/AALA202505281437.md): Hinge Arm · excess play · May 5, 2025 · N181UW · Airbus A321211 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR 1 HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42.
- [SDR AALA202505280311](https://openairdocs.org/sdr/AALA202505280311.md): Fitting · corroded · May 5, 2025 · N181UW · Airbus A321211 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT HAND PASSENGER / CREW DOOR CUTOUT LOWER SILL CENTER SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23R. REPLACED CENTER SHAPE FITTING PER ARM 51-72-11.
- [SDR AALA202505284473](https://openairdocs.org/sdr/AALA202505284473.md): Hinge Arm · excess play · May 5, 2025 · N181UW · Airbus A321211 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR 6 HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42.
- [SDR AALA202505286599](https://openairdocs.org/sdr/AALA202505286599.md): Hinge Arm · excess play · May 5, 2025 · N181UW · Airbus A321211 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR 5 HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42.
- [SDR AALA202505282080](https://openairdocs.org/sdr/AALA202505282080.md): Hinge Arm · excess play · May 5, 2025 · N181UW · Airbus A321211 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR 4 HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42.
- [SDR AALA202505281264](https://openairdocs.org/sdr/AALA202505281264.md): Hinge Fitting · worn · May 3, 2025 · N181UW · Airbus A321211 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #5 HINGE ARM END FITTING WORN. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202507156297](https://openairdocs.org/sdr/AALA202507156297.md): Skin Panel · corroded · May 2, 2025 · N181UW · Airbus A321211 · Wing, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TOP SKIN PANEL LOWER SURFACE AT RIB 10 AND THE REAR SPAR AREA. REPAIRED SKIN PANEL PER EA 365112.
- [SDR AALA202507154771](https://openairdocs.org/sdr/AALA202507154771.md): Skin Panel · corroded · May 2, 2025 · N181UW · Airbus A321211 · Wing, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TOP SKIN PANEL LOWER SURFACE AT RIB 15 AND THE REAR SPAR AREA. REPAIRED SKIN PANEL PER EA 365112.
- [SDR AALA202506303132](https://openairdocs.org/sdr/AALA202506303132.md): Hinge Fitting · cracked · May 2, 2025 · N181UW · Airbus A321211 · Landing Gear Doors
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND MAIN LANDING GEAR DOOR FORWARD HINGE FITTING, FORWARD LUG WEB CRACKED ON THE KEEL BEAM BETWEEN FR 42 AND FR 43 AT S36R. REPLACED HINGE FITTING PER EA 364701.
- [SDR AALA202505290838](https://openairdocs.org/sdr/AALA202505290838.md): Gusset · cracked · May 2, 2025 · N181UW · Airbus A321211 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED GUSSET PLATE AT FR 68 AND S14R. REPLACED GUSSET PLATE PER SRM 51-42-11.
- [SDR AALA202506258758](https://openairdocs.org/sdr/AALA202506258758.md): Support Angle · corroded · Apr 30, 2025 · N181UW · Airbus A321211 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SUPPORT STRUCTURE ANGLE FOR EMERGENCY EXIT DOOR ESCAPE SLIDE ENCLOSURE ATTACHMENT BETWEEN FR 35.1 AND FR 35.2A AT S24R.
- [SDR AALA202507168706](https://openairdocs.org/sdr/AALA202507168706.md): Skin Panel · corroded · Apr 27, 2025 · N181UW · Airbus A321211 · Wing, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE TOP SKIN SKIN PANEL UPPER SURFACE BETWEEN RIB 5 AND RIB 6 AT STRINGER 17. REPAIRED SKIN PANEL PER EA 365114.
- [SDR AALA202507159555](https://openairdocs.org/sdr/AALA202507159555.md): Skin Panel · corroded · Apr 27, 2025 · N181UW · Airbus A321211 · Wing, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TOP SKIN PANEL UPPER SURFACE AT RIB 19 AND THE FRONT SPAR AREA. REPAIRED SKIN PANEL PER EA 365114.

Next page: https://openairdocs.org/aircraft/N181UW/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 = 'N181UW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N181UW/reports

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