# Service difficulty reports: N180US A list on [N180US](https://openairdocs.org/aircraft/N180US.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 7 · 334 reports - [SDR AALA202609233062](https://openairdocs.org/sdr/AALA202609233062.md): Sensor · fault message · Sep 22, 2026 · N180US · Airbus A321211 · Landing Gear Position and Warning > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED INBOUND INTO BOS DUE TO THE FLIGHT CREW REPORTING THAT AT LANDING GEAR EXTENSION NOSE STEERING WHEEL FAULT DISPLAYED AND THE FLIGHT CREW PERFORMED A GO AROUND TO RUN THE CHECK LIST - THE FLIGHT CREW REPORTED THA - [SDR AALA202607241419](https://openairdocs.org/sdr/AALA202607241419.md): Arming Lever · loose · Jul 21, 2026 · N180US · Airbus A321211 · Emergency Exits > AIRCRAFT WAS NOT GROUNDED: 3L DOOR ARMING LEVER/HANDLE LOOSE. MAINTENANCE TIGHTENED 3L ARMING LEVER. - [SDR AALA202605270195](https://openairdocs.org/sdr/AALA202605270195.md): Bottle · low pressure · May 25, 2026 · N180US · Airbus A321211 · Emergency Exits > AIRCRAFT WAS NOT GROUNDED: L3 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00. - [SDR AALA202603192077](https://openairdocs.org/sdr/AALA202603192077.md): Wire · loose · Mar 18, 2026 · N180US · Airbus A321211 · Light System Wiring > AIRCRAFT WAS NOT GROUNDED: SEAT ROW 23 CEILING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND ONE OF THE WIRE LEADS LOOSE, RE-INSTALLED WIRE LEAD ON ROW 23 CEILING EMERGENCY LIGHT PER AMM 33-51-11 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO ISSUE - [SDR AALA202602023277](https://openairdocs.org/sdr/AALA202602023277.md): Flashlight · no test · Jan 30, 2026 · N180US · Airbus A321211 · Emergency Equipment > AIRCRAFT WAS NOT GROUNDED: FORWARD OUTBOARD FLASHLIGHT AT 1L FLIGHT ATTENDANTS JUMPSEAT IS INOPERATIVE. MAINTENANCE REPLACED FLASHLIGHT PER AMM 25-65-00. - [SDR AALA202512264537](https://openairdocs.org/sdr/AALA202512264537.md): Battery · no test · Dec 23, 2025 · N180US · Airbus A321211 · Emergency Lighting > AIRCRAFT WAS GROUNDED: BATTERY FAULT MESSAGE FOR EMERGENCY POWER SUPPLY UNIT FORWARD LEFT DISPLAYED DURING SYSTEM TEST. REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38. - [SDR AALA202512260408](https://openairdocs.org/sdr/AALA202512260408.md): Battery · no test · Dec 23, 2025 · N180US · Airbus A321211 · Emergency Lighting > AIRCRAFT WAS GROUNDED: BATTERY FAULT MESSAGE FOR EMERGENCY POWER SUPPLY UNIT MID RIGHT DISPLAYED DURING SYSTEM TEST. REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38. - [SDR AALA202512040901](https://openairdocs.org/sdr/AALA202512040901.md): Sensor · false indication · Dec 1, 2025 · N180US · Airbus A321211 · Fuel Indicating System > AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED FUEL RIGHT WING TANK OVERFLOW ECAM MESSAGE ON DESCENT. MAINTENANCE REPLACED RIGHT WING SURGE TANK OVERFLOW SENSOR 28QJ2 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 28-46-16. - [SDR AALA202508290228](https://openairdocs.org/sdr/AALA202508290228.md): Handle · loose · Aug 26, 2025 · N180US · Airbus A321211 · Emergency Exits > AIRCRAFT WAS NOT GROUNDED: 3L DOOR DISARM HANDLE IS VERY LOOSE. MAINTENANCE RESECURED ARM/DISARM LEVER PER AMM 52-10-00. - [SDR AALA202507142632](https://openairdocs.org/sdr/AALA202507142632.md): Terminal · disconnected · Jul 11, 2025 · N180US · Airbus A321211 · Electrical Power System Wiring > AIRCRAFT IN BASE MAINTENANCE: EVACUATION SIGNALING SYSTEM RESET SWITCH FOR THE R2 DOOR IS INOPERATIVE. MAINTENANCE FOUND TERMINAL 1 ON PUSH BUTTON SWITCH 2064VU4 DISCONNECTED AND WAS RECONNECTED PER ASM 23-73-27 AND AWM 23-73-54 A SATISFACTORY OPERATIONAL CHE - [SDR AALA202507111793](https://openairdocs.org/sdr/AALA202507111793.md): Slide · deformed · Jul 10, 2025 · N180US · Airbus A321211 · Escape Slide > AIRCRAFT IN BASE MAINTENANCE: PASSENGER CREW DOOR 831 ESCAPE SLIDE IS DEFORMED. REPLACED ESCAPE SLIDE PER TASK CARD 26L00025010. - [SDR AALA202507085370](https://openairdocs.org/sdr/AALA202507085370.md): Fitting · none · Jul 5, 2025 · N180US · Airbus A321211 · Fuselage Main, Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED AT FR 16 AND DOOR STOP FITTING #1 THE INTERCOSTAL FITTING REQUIRES REPLACEMENT PER THE REPAIR INSTRUCTIONS OUTLINED ON EA 365203. REPLACED INTERCOSTAL FITTING PER EA 365203. - [SDR AALA202506309135](https://openairdocs.org/sdr/AALA202506309135.md): Frame · cracked · Jun 28, 2025 · N180US · Airbus A321211 · Fuselage Main, Frame > AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AFT FACE WEB JOINT TO THE DOOR FRAME AT FR 68 AND S8R. REPAIRED FRAME PER SRM 51-41-12-300-012. - [SDR AALA202506309130](https://openairdocs.org/sdr/AALA202506309130.md): Web · cracked · Jun 18, 2025 · N180US · Airbus A321211 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CRACKED REINFORCEMENT WEB FASTENER HOLE BETWEEN FR 67 AND FR 68 AT S8R. REPLACED REINFORCEMENT WEB PER SRM 51-42-11. - [SDR AALA202506172741](https://openairdocs.org/sdr/AALA202506172741.md): Bottle · leaking · Jun 16, 2025 · N180US · Airbus A321211 · Passenger/Crew Doors > AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 842 DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. REPLACED DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-13-14. - [SDR AALA202506172830](https://openairdocs.org/sdr/AALA202506172830.md): Bottle · leaking · Jun 16, 2025 · N180US · Airbus A321211 · Passenger/Crew Doors > AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 831 DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. REPLACED DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-11-14. - [SDR AALA202506065462](https://openairdocs.org/sdr/AALA202506065462.md): Floorbeam · corroded · Jun 5, 2025 · N180US · Airbus A321211 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM AT FR 16 AND +Y765. REPLACED FLOOR BEAM PER SRM 51-42-11. - [SDR AALA202506236678](https://openairdocs.org/sdr/AALA202506236678.md): Fitting · corroded · May 26, 2025 · N180US · Airbus A321211 · Nacelle/Pylon, Main Frame > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 5. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-001. - [SDR AALA202505307099](https://openairdocs.org/sdr/AALA202505307099.md): Hinge Fitting · excess play · May 26, 2025 · N180US · Airbus A321211 · Nacelle/Pylon Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND PYLON OUTBOARD SIDE, CENTER HINGE ATTACHMENT FITTING FOR THE THRUST REVERSER HAS EXCESSIVE PLAY. REPLACED ATTACHMENT FITTING PER AMM 54-57-17. - [SDR AALA202506172871](https://openairdocs.org/sdr/AALA202506172871.md): Fitting · cracked · May 18, 2025 · N180US · Airbus A321211 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT FR 16 BETWEEN S10L AND S11L AT THE #7 DOOR STOP FITTING AREA. REPLACED INTERCOSTAL FITTING PER SRM 51-72-11. - [SDR AALA202507094182](https://openairdocs.org/sdr/AALA202507094182.md): Frame · cracked · May 17, 2025 · N180US · Airbus A321211 · Fuselage Main, Frame > AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AFT FACE WEB JOINT TO THE DOOR FRAME AT FR 68 BETWEEN S8L AND S9L. REPAIRED FRAME PER EA 365394. - [SDR AALA202507102478](https://openairdocs.org/sdr/AALA202507102478.md): Pressure Deck · cracked · May 13, 2025 · N180US · 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 364983 - [SDR AALA202506174493](https://openairdocs.org/sdr/AALA202506174493.md): Door Sill · corroded · May 13, 2025 · N180US · Airbus A321211 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL AT FR 68 AND S23R. REPAIRED LOWER SILL PER SRM 53-41-14-300-001. - [SDR AALA202506135748](https://openairdocs.org/sdr/AALA202506135748.md): Door Sill · corroded · May 13, 2025 · N180US · Airbus A321211 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT PASSENGER / CREW DOOR CUTOUT LOWER SILL AT FR 68 AND S23L. REPLACED LOWER SILL PER SRM 53-41-14-300-001. - [SDR AALA2025060200013](https://openairdocs.org/sdr/AALA2025060200013.md): Hinge Fitting · excess play · May 12, 2025 · N180US · 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 AALA202505208237](https://openairdocs.org/sdr/AALA202505208237.md): Hinge Fitting · excess play · May 12, 2025 · N180US · 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 AALA202505198169](https://openairdocs.org/sdr/AALA202505198169.md): Hinge Fitting · excess play · May 12, 2025 · N180US · 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 AALA202507081602](https://openairdocs.org/sdr/AALA202507081602.md): Shear Plate · cracked · May 11, 2025 · N180US · 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 AALA202506236667](https://openairdocs.org/sdr/AALA202506236667.md): Shear Plate · cracked · May 11, 2025 · N180US · 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 51-42-11. - [SDR AALA202506114813](https://openairdocs.org/sdr/AALA202506114813.md): Floorbeam · corroded · May 11, 2025 · N180US · Airbus A321211 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CORROSION AFT CABIN FLOOR BEAM AT FR 70 AND +Y160. REPLACED FLOOR BEAM PER SRM 51-72-11. - [SDR AALA202506115420](https://openairdocs.org/sdr/AALA202506115420.md): Floorbeam · corroded · May 11, 2025 · N180US · Airbus A321211 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CORROSION AFT CABIN FLOOR BEAM AT FR 70 AND +Y765. REPLACED FLOOR BEAM PER SRM 51-72-11. - [SDR AALA202506116834](https://openairdocs.org/sdr/AALA202506116834.md): Floorbeam · corroded · May 11, 2025 · N180US · Airbus A321211 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CORROSION AFT CABIN FLOOR BEAM AT FR 70 AND -Y160. REPLACED FLOOR BEAM PER SRM 51-72-11. - [SDR AALA202506118157](https://openairdocs.org/sdr/AALA202506118157.md): Attach Fitting · excess play · May 10, 2025 · N180US · Airbus A321211 · Engine Thrust Reverser > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND PYLON OUTBOARD MIDDLE ATTACHMENT FITTING FOR THE THRUST REVERSER HAS EXCESSIVE PLAY IN THE BEARING AREA. REPLACED FITTING PER AMM 54-57-17. - [SDR AALA202506118242](https://openairdocs.org/sdr/AALA202506118242.md): Attach Fitting · excess play · May 10, 2025 · N180US · Airbus A321211 · Engine Thrust Reverser > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND PYLON OUTBOARD AFT ATTACHMENT FITTING FOR THE THRUST REVERSER HAS EXCESSIVE PLAY IN THE BEARING AREA. REPLACED FITTING PER AMM 54-57-17. - [SDR AALA202506114899](https://openairdocs.org/sdr/AALA202506114899.md): Attach Fitting · excess play · May 10, 2025 · N180US · Airbus A321211 · Engine Thrust Reverser > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND PYLON INBOARD MIDDLE ATTACHMENT FITTING FOR THE THRUST REVERSER HAS EXCESSIVE PLAY IN THE BEARING AREA. REPLACED FITTING PER AMM 54-57-17. - [SDR AALA202506110311](https://openairdocs.org/sdr/AALA202506110311.md): Attach Fitting · excess play · May 10, 2025 · N180US · Airbus A321211 · Nacelle/Pylon, Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND PYLON INBOARD AFT ATTACHMENT FITTING FOR THE THRUST REVERSER HAS EXCESSIVE PLAY IN THE BEARING AREA. REPLACED FITTING PER AMM 54-57-17. - [SDR AALA202505301884](https://openairdocs.org/sdr/AALA202505301884.md): Hinge Fitting · excess play · May 10, 2025 · N180US · Airbus A321211 · Nacelle/Pylon Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND PYLON INBOARD SIDE, CENTER HINGE ATTACHMENT FITTING FOR THE THRUST REVERSER HAS EXCESSIVE PLAY. REPLACED ATTACHMENT FITTING PER AMM 54-57-17. - [SDR AALA202505304747](https://openairdocs.org/sdr/AALA202505304747.md): Hinge Fitting · excess play · May 10, 2025 · N180US · Airbus A321211 · Nacelle/Pylon Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND PYLON INBOARD SIDE, AFT HINGE ATTACHMENT FITTING FOR THE THRUST REVERSER HAS EXCESSIVE PLAY. REPLACED ATTACHMENT FITTING PER AMM 54-57-17. - [SDR AALA202505309436](https://openairdocs.org/sdr/AALA202505309436.md): Hinge Fitting · excess play · May 10, 2025 · N180US · Airbus A321211 · Nacelle/Pylon Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND PYLON OUTBOARD SIDE, AFT HINGE ATTACHMENT FITTING FOR THE THRUST REVERSER HAS EXCESSIVE PLAY. REPLACED ATTACHMENT FITTING PER AMM 54-57-17. - [SDR AALA202506308568](https://openairdocs.org/sdr/AALA202506308568.md): Plate · worn · May 5, 2025 · N180US · Airbus A321211 · Wing Main, Frame Structure > AIRCRAFT IN BASE MAINTENANCE: LEFT WING SKIN PANEL #3 LOWER SURFACE PYLON SYSTEMS MOUNTING PLATE WORN BETWEEN RIBS 7 AND 8. REPLACED MOUNTING PLATE PER SRM 57-21-11-300-005. - [SDR AALA202507088577](https://openairdocs.org/sdr/AALA202507088577.md): Fitting · cracked · May 2, 2025 · N180US · Airbus A321211 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING CRACKED AT FR 4 AND Y0. REPLACED CONTINUITY FITTING PER EA 365054. - [SDR AALA202507086944](https://openairdocs.org/sdr/AALA202507086944.md): Fitting · cracked · May 2, 2025 · N180US · Airbus A321211 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING RIGHT HAND CONTINUITY FITTING CRACKED AT FR 4 AND Y0. REPLACED CONTINUITY FITTING PER EO 5319Y017-002. - [SDR AALA202507123917](https://openairdocs.org/sdr/AALA202507123917.md): Frame · cracked · Apr 23, 2025 · N180US · Airbus A321211 · Fuselage Main, Frame > AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME FASTENER HOLE AT DOUBLE JOGGLE AREA, FR 16 RIGHT AND DOOR STOP #7. REPAIRED FRAME PER EA 364655. - [SDR AALA202503200993](https://openairdocs.org/sdr/AALA202503200993.md): Lever · loose · Mar 20, 2025 · N180US · Airbus A321211 · Emergency Exits > AIRCRAFT WAS NOT GROUNDED: 3L ARMING LEVER IS LOOSE. MAINTENANCE RESECURED LEVER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-22-22. - [SDR AALA202502171198](https://openairdocs.org/sdr/AALA202502171198.md): Girt Bar · sticking · Feb 14, 2025 · N180US · Airbus A321211 · Emergency Equipment > AIRCRAFT WAS NOT GROUNDED: L1 DOOR IS DIFFICULT TO ARM AND DISARM. CLEANED AND LUBRICATED GIRT BAR MECHANISM PER AMM 12-20-52. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED. - [SDR AALA202501109775](https://openairdocs.org/sdr/AALA202501109775.md): Bottle · low pressure · Jan 9, 2025 · N180US · Airbus A321211 · Emergency Equipment > AIRCRAFT WAS NOT GROUNDED: MAINTENANCE FOUND THE FLIGHT ATTENDANTS PANEL HAD A CAUTION LIGHT ILLMINATED AND A FAULT MESSAGE FOR DOOR BOTTLE EXIT LEFT. MAINTENANCE FOUND THE L3 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW AND SERVICED IT PER AMM 52 - [SDR AALA202501097149](https://openairdocs.org/sdr/AALA202501097149.md): Bottle · low pressure · Jan 8, 2025 · N180US · Airbus A321211 · Emergency Exits > AIRCRAFT WAS GROUNDED: L2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED L2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-22-00. - [SDR AALA202411254855](https://openairdocs.org/sdr/AALA202411254855.md): Battery · no test · Nov 23, 2024 · N180US · Airbus A321211 · Emergency Lighting > AIRCRAFT WAS NOT GROUNDED: DURING EMERGENCY LIGHTS TEST PORTION OF R3 DOOR SLIDE INSTALLATION, EMERGENCY POWER SUPPLY UNIT BATTERY AT DOOR 1L IS FAULTING. REMOVED AND REPLACED DOOR 1L EMERGENCY POWER SUPPLY UNIT BATTERY. - [SDR AALA202409209360](https://openairdocs.org/sdr/AALA202409209360.md): Bottle · low pressure · Sep 19, 2024 · N180US · Airbus A321211 · Emergency Equipment > AIRCRAFT WAS NOT GROUNDED: DURING PS CHECK, FOUND L3 EMERGENCY EXIT DOOR DAMPER PRESSURE IS IN THE YELLOW BAND. REQUIRED SERVICING. SERVICED L3 EMERGENCY EXIT DOOR DAMPER. - [SDR AALA202409203666](https://openairdocs.org/sdr/AALA202409203666.md): Bottle · low pressure · Sep 19, 2024 · N180US · Airbus A321211 · Emergency Equipment > AIRCRAFT WAS NOT GROUNDED: DURING PS CHECK, FOUND L1 DOOR EMERGENCY CYLINDER PRESSURE LOW AS 1500 PSI. REQUIRED SERVICING. SERVICED L1 DOOR EMERGENCY CYLINDER. Next page: https://openairdocs.org/aircraft/N180US/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 = 'N180US' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N180US/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.