# Service difficulty reports: N178US A list on [N178US](https://openairdocs.org/aircraft/N178US.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 · 346 reports - [SDR AALA202605189307](https://openairdocs.org/sdr/AALA202605189307.md): Cids · false activation · May 16, 2026 · N178US · Airbus A321211 · Emergency Equipment > AIRCRAFT WAS NOT GROUNDED: EVACUATION COMMAND AUDITABLE GOING OFF WHEN AIRCRAFT IS POWERED UP. MAINTENANCE REPLACED CIDS DIRECTOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 23-73-34. - [SDR AALA202603021170](https://openairdocs.org/sdr/AALA202603021170.md): Door · damaged · Feb 28, 2026 · N178US · Airbus A321211 · Fixed Inner Doors > AIRCRAFT WAS NOT GROUNDED: MID LAVATORY DOOR STUCK CLOSED. MAINTENANCE FOUND THE DOOR UPPER TRIM WAS DAMAGED AND REPLACED THE DOOR PER AMM 25-45-19-400. - [SDR AALA202601120052](https://openairdocs.org/sdr/AALA202601120052.md): Filter · dirty · Jan 9, 2026 · N178US · Airbus A321211 · Smoke Detection > AIRCRAFT WAS NOT GROUNDED: MID LAVATORY FIRE WARNING WENT OFF IN AIR: NO WARNING IN FLIGHT DECK. MAINTENANCE FOUND ALL LAVATORY SMOKE DETECTORS FILTER SUPER DIRTY, CLEANED ALL LAVATORY SMOKE DETECTOR FILTERS AND ACCOMPLISHED A SATISACTORY OPERATIONAL CHECK PER - [SDR AALA202601065111](https://openairdocs.org/sdr/AALA202601065111.md): Smoke Detector · false activation · Jan 5, 2026 · N178US · Airbus A321211 · Smoke Detection > AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTED THAT AFT RIGHT LAVATORY SMOKE ALARM STARTED TO BEEP ONCE EVERY TWO SECONDS AND THE LIGHT CAME ON. NO INDICATIONS ON THE FLIGHT DECK. THE LAVATORY WAS EMPTY. AFTER ABOUT 5 MINUTES THE BEEPING STOPPED AND THE - [SDR AALA202601042359](https://openairdocs.org/sdr/AALA202601042359.md): Smoke Detector · false activation · Jan 2, 2026 · N178US · Airbus A321211 · Smoke Detection > AIRCRAFT WAS NOT GROUNDED: FLIGHT CREW REPORTED THAT THE FORWARD LAVATORY SMOKE DETECTION CHIME ALERTED SMOKE WHILE PASSENGER WAS ALLEGEDLY VAPING. THE MID AND AFT RIGHT SMOKE DETECTION CHIME WENT OFF SIMULTANEOUSLY WITH FORWARD LAVATORY BUT NO PASSENGERS WERE - [SDR AALA202509122653](https://openairdocs.org/sdr/AALA202509122653.md): Latch · out of adjust · Sep 11, 2025 · N178US · Airbus A321211 · Fixed Inner Doors > AIRCRAFT WAS NOT GROUNDED: THE FLIGHT DECK DOOR WILL NOT OPEN WITH HANDLE ON THE DOOR FROM INSIDE OF THE FLIGHT DECK IT ONLY OPEN WITH FLIGHT DECK DOOR SWITCH. MAINTENANCE ADJUSTED TOP LATCH MECHANISM PER AMM 52-51-21. - [SDR AALA202509118803](https://openairdocs.org/sdr/AALA202509118803.md): Striker · faulted · Sep 8, 2025 · N178US · Airbus A321211 · Fixed Inner Doors > AIRCRAFT WAS NOT GROUNDED: THE FLIGHT DECK DOOR WILL NOT OPEN WITH HANDLE ON THE DOOR FROM INSIDE OF THE FLIGHT DECK, IT WILL ONLY OPEN WITH FLIGHT DECK DOOR SWITCH. MAINTENANCE FOUND A FAULT MESSAGE FOR THE BOTTOM STRIKER DUE TO PIN #6 BEING DAMAGED AND REPLA - [SDR AALA202509024893](https://openairdocs.org/sdr/AALA202509024893.md): Power Supply · no test · Aug 25, 2025 · N178US · Airbus A321211 · Emergency Lighting > AIRCRAFT IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY UNIT 10WL DOES NOT PASS SYSTEM TEST. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 10WL (AALA202509028249) AND BATTERY (AALA202509025754) PER AMM 33-51-38. MAINTENANCE ALSO REPLACED PASSENGER / CREW DOOR - [SDR AALA202509025754](https://openairdocs.org/sdr/AALA202509025754.md): Battery · no test · Aug 25, 2025 · N178US · Airbus A321211 · Emergency Lighting > AIRCRAFT IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY UNIT 10WL DOES NOT PASS SYSTEM TEST. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 10WL (AALA202509028249) AND BATTERY (AALA202509025754) PER AMM 33-51-38. MAINTENANCE ALSO REPLACED PASSENGER / CREW DOOR - [SDR AALA202509028249](https://openairdocs.org/sdr/AALA202509028249.md): Power Supply · no test · Aug 25, 2025 · N178US · Airbus A321211 · Emergency Lighting > AIRCRAFT IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY UNIT 10WL DOES NOT PASS SYSTEM TEST. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 10WL (AALA202509028249) AND BATTERY (AALA202509025754) PER AMM 33-51-38. MAINTENANCE ALSO REPLACED PASSENGER / CREW DOOR - [SDR AALA202508292226](https://openairdocs.org/sdr/AALA202508292226.md): Switch · inoperative · Aug 20, 2025 · N178US · Airbus A321211 · Emergency Equipment > AIRCRAFT IN BASE MAINTENANCE: R2 DOOR FLIGHT ATTENDANTS PANEL EVACUATION PUSH BUTTON IS INOPERATIVE. REPLACED FLIGHT ATTENDANTS PANEL 126RH AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 23-73-13. - [SDR AALA202506306755](https://openairdocs.org/sdr/AALA202506306755.md): Hinge Fitting · worn · Jun 28, 2025 · N178US · Airbus A321211 · Nacelle/Pylon, Main Frame > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND PYLON OUTBOARD SIDE FORWARD HINGE FITTING FOR FAN COWL MOUNTING IS WORN, REPLACED HINGE FITTING PER SRM 51-42-11. - [SDR AALA202507163315](https://openairdocs.org/sdr/AALA202507163315.md): Fitting · cracked · Jun 26, 2025 · N178US · Airbus A321211 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACKED CENTER FUSELAGE PRESSURE DECK CORNER FITTING AT FR 36 AND -Y1525.34. REPLACED CORNER FITTING PER SRM 51-42-11. - [SDR AALA202507155201](https://openairdocs.org/sdr/AALA202507155201.md): Fitting · cracked · Jun 26, 2025 · N178US · Airbus A321211 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACKED CENTER FUSELAGE PRESSURE DECK CORNER FITTING AT FR 36 AND +Y1525.34. REPLACED PRESSURE DECK CORNER FITTING PER SRM 51-42-11. - [SDR AALA202506232325](https://openairdocs.org/sdr/AALA202506232325.md): Hinge Fitting · worn · Jun 15, 2025 · N178US · Airbus A321211 · Fuselage, Door Hinge > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND MAIN LANDING GEAR DOOR FORWARD HINGE FITTING BEARING IS LOOSE. REPLACED HINGE FITTING PER CMM 52-81-18. - [SDR AALA202507158289](https://openairdocs.org/sdr/AALA202507158289.md): Fitting · cracked · Jun 12, 2025 · N178US · Airbus A321211 · Fuselage Main, Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT FR 16 BETWEEN S10R AND 11R AT THE # 7 DOOR STOP. REPLACED INTERCOSTAL FITTING PER SRM 51-42-11. - [SDR AALA202506064276](https://openairdocs.org/sdr/AALA202506064276.md): Hinge Fitting · excess play · Jun 5, 2025 · N178US · Airbus A321211 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #6 HINGE ARM FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42. - [SDR AALA202506060564](https://openairdocs.org/sdr/AALA202506060564.md): Hinge Fitting · excess play · Jun 5, 2025 · N178US · Airbus A321211 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #4 HINGE ARM FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM FITTING PER AMM 55-16-42. - [SDR AALA202506060755](https://openairdocs.org/sdr/AALA202506060755.md): Hinge Fitting · excess play · Jun 5, 2025 · N178US · Airbus A321211 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #1 HINGE ARM FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM FITTING PER AMM 55-16-42. - [SDR AALA202507099109](https://openairdocs.org/sdr/AALA202507099109.md): Attach Fitting · worn · Jun 4, 2025 · N178US · Airbus A321211 · Nacelle/Pylon, Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: LEFT 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 AALA202505303952](https://openairdocs.org/sdr/AALA202505303952.md): Bolt · corroded · May 29, 2025 · N178US · Airbus A321211 · Leading Edge Devices > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #12 UPPER AFT BOLT AT RIB 26. REPLACED BOLT PER AMM 27-84-67. - [SDR AALA202505307533](https://openairdocs.org/sdr/AALA202505307533.md): Hinge Fitting · excess play · May 29, 2025 · N178US · 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 AALA202507084013](https://openairdocs.org/sdr/AALA202507084013.md): Fitting · no discrepancy · May 28, 2025 · N178US · Airbus A321211 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK CENTER WINDSHIELD FRAMING THE RIGHT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 2 AT Y0 MUST BE REPLACED PER INSTRUCTIONS OUTLINED IN EO 5319Y017-002 REPLACED RIGHT HAN - [SDR AALA202506185973](https://openairdocs.org/sdr/AALA202506185973.md): Hinge Fitting · excess play · May 22, 2025 · N178US · Airbus A321211 · Nacelle/Pylon, Main Frame > 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 AALA202506182161](https://openairdocs.org/sdr/AALA202506182161.md): Hinge Fitting · excess play · May 22, 2025 · N178US · Airbus A321211 · Nacelle/Pylon, Main Frame > 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 AALA202506174888](https://openairdocs.org/sdr/AALA202506174888.md): Bearing · excess play · May 22, 2025 · N178US · Airbus A321211 · Nacelle/Pylon, Main Frame > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND PYLON INBOARD SIDE AFT ATTACH FITTING BEARING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER AMM 54-57-17. - [SDR AALA202506068323](https://openairdocs.org/sdr/AALA202506068323.md): Attach Fitting · excess play · May 22, 2025 · N178US · Airbus A321211 · Nacelle/Pylon, Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: LEFT 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 AALA202506069947](https://openairdocs.org/sdr/AALA202506069947.md): Attach Fitting · excess play · May 22, 2025 · N178US · Airbus A321211 · Nacelle/Pylon, Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: LEFT 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 AALA202506062811](https://openairdocs.org/sdr/AALA202506062811.md): Attach Fitting · excess play · May 22, 2025 · N178US · Airbus A321211 · Nacelle/Pylon, Attach Fittings > 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 AALA202508124169](https://openairdocs.org/sdr/AALA202508124169.md): Pressure Deck · cracked · May 21, 2025 · N178US · 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 365069. - [SDR AALA202508129808](https://openairdocs.org/sdr/AALA202508129808.md): Pressure Deck · cracked · May 21, 2025 · N178US · 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 365069. - [SDR AALA202505289300](https://openairdocs.org/sdr/AALA202505289300.md): Hinge Fitting · excess play · May 21, 2025 · N178US · 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 AALA202505285872](https://openairdocs.org/sdr/AALA202505285872.md): Hinge Fitting · excess play · May 21, 2025 · N178US · 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 AALA202505289195](https://openairdocs.org/sdr/AALA202505289195.md): Hinge Fitting · excess play · May 21, 2025 · N178US · 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 AALA202505289641](https://openairdocs.org/sdr/AALA202505289641.md): Hinge Fitting · excess play · May 21, 2025 · N178US · 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 AALA202505281706](https://openairdocs.org/sdr/AALA202505281706.md): Hinge Fitting · excess play · May 21, 2025 · N178US · 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 AALA202505287637](https://openairdocs.org/sdr/AALA202505287637.md): Hinge Fitting · excess play · May 21, 2025 · N178US · 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 AALA202506037446](https://openairdocs.org/sdr/AALA202506037446.md): Bolt · corroded · May 20, 2025 · N178US · Airbus A321211 · Leading Edge Devices > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #1 FORWARD MIDDLE BOLT AT RIB 2. REPLACED BOLT PER AMM 27-84-63. - [SDR AALA202507174351](https://openairdocs.org/sdr/AALA202507174351.md): Access Panel · corroded · May 19, 2025 · N178US · Airbus A321211 · Wing, Plate/Skin > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING FUEL TANK ACCESS PANEL / DOOR 540 BB. REPLACED ACCESS PANEL / DOOR PER SRM 51-72-11. - [SDR AALA202506231855](https://openairdocs.org/sdr/AALA202506231855.md): Handle · cracked · May 19, 2025 · N178US · Airbus A321211 · Flight Compartment Windows > AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK LEFT HAND SLIDING WINDOW HANDLE CRACKED. REPLACED HANDLE PER CMM 56-12-12 AND AMM 56-12-11. - [SDR AALA202506234623](https://openairdocs.org/sdr/AALA202506234623.md): Handle · cracked · May 19, 2025 · N178US · Airbus A321211 · Flight Compartment Windows > AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK RIGHT HAND SLIDING WINDOW HANDLE CRACKED. REPLACED HANDLE PER CMM 56-12-12 AND AMM 56-12-11. - [SDR AALA202506061907](https://openairdocs.org/sdr/AALA202506061907.md): Support Bracket · broken · May 19, 2025 · N178US · Airbus A321211 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: AFT CARGO COMPARTMENT PRESSURE BULKHEAD SUPPORT ANGLE BROKEN AT FR 46 LEFT. REPLACED SUPPORT BRACKET PER SRM 51-72-11. - [SDR AALA202506234546](https://openairdocs.org/sdr/AALA202506234546.md): Floorbeam · corroded · May 17, 2025 · N178US · Airbus A321211 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM AT FR 16 AND +Y1292. REPLACED FLOOR BEAM PER SRM 51-42-11. - [SDR AALA202508189263](https://openairdocs.org/sdr/AALA202508189263.md): Shear Plate · cracked · May 16, 2025 · N178US · 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 AALA202508146193](https://openairdocs.org/sdr/AALA202508146193.md): Shear Plate · cracked · May 16, 2025 · N178US · 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 AALA202507102347](https://openairdocs.org/sdr/AALA202507102347.md): Floor Support · corroded · May 16, 2025 · N178US · Airbus A321211 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM BETWEEN FR 65 AND FR 66 AT -Y465. REPLACED BEAM PER SRM 51-72-11. - [SDR AALA202507089013](https://openairdocs.org/sdr/AALA202507089013.md): Floorbeam · cracked · May 16, 2025 · N178US · Airbus A321211 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR CROSSBEAM SPLICE AT FR 66 AND S23L. REPLACED SPLICE PER SRM 51-42-11. - [SDR AALA202506305185](https://openairdocs.org/sdr/AALA202506305185.md): Floorbeam · corroded · May 16, 2025 · N178US · Airbus A321211 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM AT FR 70 AND -Y160.5. REPLACED FLOOR BEAM PER SRM 51-42-11. - [SDR AALA202506244723](https://openairdocs.org/sdr/AALA202506244723.md): Door Sill · corroded · May 16, 2025 · N178US · Airbus A321211 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUTOUT LOWER SILL AT FR 67 AND S23L. REPAIRED LOWER SILL PER SRM 53-41-14-300-001. - [SDR AALA202506242743](https://openairdocs.org/sdr/AALA202506242743.md): Floorbeam · corroded · May 16, 2025 · N178US · Airbus A321211 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOORBEAM AT FR 69 AND +Y765. REPLACED FLOORBEAM PER SRM 51-72-11. Next page: https://openairdocs.org/aircraft/N178US/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 = 'N178US' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N178US/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.