# Service difficulty reports: N170US A list on [N170US](https://openairdocs.org/aircraft/N170US.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 · 310 reports - [SDR AALA202610083301](https://openairdocs.org/sdr/AALA202610083301.md): Arming Lever · loose · Oct 6, 2026 · N170US · Airbus A321211 · Emergency Exits > AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS DOOR 3L ARMING LEVER LOOSE. MAINTENANCE SECURED LOOSE FLAP ON 3L DOOR ARM LEVER. - [SDR AALA202607286048](https://openairdocs.org/sdr/AALA202607286048.md): Switch · illuminated · Jul 25, 2026 · N170US · Airbus A321211 · Hydraulic Indicating System > AIRCRAFT WAS NOT GROUNDED: AN EMERGENCY WAS DECLARED INTO CLT DUE TO THE FLIGHT CREW REPORTING THAT AFTER DEPARTURE ECAM: YELLOW RESERVOIR LOW LEVEL. THE FLIGHT CREW FOLLOWED ECAM PROCEDURE AND TURNED OFF PTU AND YELLOW ENGINE 2 HYDRAULIC PUMP. THE GREEN AND B - [SDR AALA202603257177](https://openairdocs.org/sdr/AALA202603257177.md): Flashlight · misinstalled · Mar 23, 2026 · N170US · Airbus A321211 · Emergency Equipment > AIRCRAFT WAS NOT GROUNDED: 1L OUTBOARD FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT INSTALLED WRONG. UNABLE TO COMPLETE PREFLIGHT CHECK. MAINTENANCE REMOVED AND INSTALLED FLASHLIGHT CORRECTLY PER AMM 25-65-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO - [SDR AALA202603175106](https://openairdocs.org/sdr/AALA202603175106.md): Door · out of adjust · Mar 16, 2026 · N170US · Airbus A321211 · Fixed Inner Doors > AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS SOMETHING IS JAMMING THE MID LAVATORY DOOR WHICH IS VERY HARD TOO OPEN / CLOSE RESULTING IN PEOPLE KEEP GETTING STUCK. MAINTENANCE ADJUSTED THE MID LAVATORY DOOR PER CMM 25-43-25 AND ACCOMPLISHED A SATISFACTO - [SDR AALA202512269197](https://openairdocs.org/sdr/AALA202512269197.md): Actuator Valve · warning message · Dec 23, 2025 · N170US · Airbus A321211 · Fuel Transfer Valve > AIRCRAFT WAS NOT GROUNDED: CENTER FUEL TANK RIGHT TRANSFER VALVE FAULT ECAM MESSAGE DISPLAYED IN FLIGHT. MAINTENANCE REPLACED RIGHT ACTUATOR VALVE 12QL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 28-26-51. - [SDR AALA202512264720](https://openairdocs.org/sdr/AALA202512264720.md): Flashlight · misinstalled · Dec 21, 2025 · N170US · Airbus A321211 · Emergency Equipment > AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT UNDER JUMPSEAT AT DOOR 4R IS ON AND WON'T TURN OFF. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY AND STOWED THE FLASHLIGHT PROPERLY IN HOLDER. - [SDR AALA202512157629](https://openairdocs.org/sdr/AALA202512157629.md): Lever · loose · Dec 12, 2025 · N170US · Airbus A321211 · Passenger/Crew Doors > AIRCRAFT WAS NOT GROUNDED: ARMING LEVER ON DOOR 4L IS NON-FUNCTIONAL. MAINTENANCE TIGHTENED ARMING LEVER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-20-00. - [SDR AALA202511260049](https://openairdocs.org/sdr/AALA202511260049.md): Bottle · low pressure · Nov 26, 2025 · N170US · Airbus A321211 · Emergency Exits > AIRCRAFT WAS GROUNDED: R2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00. - [SDR AALA202511266192](https://openairdocs.org/sdr/AALA202511266192.md): Bottle · low pressure · Nov 26, 2025 · N170US · Airbus A321211 · Passenger/Crew Doors > AIRCRAFT WAS GROUNDED: L4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00. - [SDR AALA202511264782](https://openairdocs.org/sdr/AALA202511264782.md): Bottle · low pressure · Nov 26, 2025 · N170US · Airbus A321211 · Passenger/Crew Doors > AIRCRAFT WAS GROUNDED: R1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00. - [SDR AALA202511260077](https://openairdocs.org/sdr/AALA202511260077.md): Bottle · low pressure · Nov 26, 2025 · N170US · Airbus A321211 · Emergency Exits > AIRCRAFT WAS GROUNDED: L2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00. - [SDR AALA202511268923](https://openairdocs.org/sdr/AALA202511268923.md): Lamp · inoperative · Nov 26, 2025 · N170US · Airbus A321211 · Emergency Lighting > AIRCRAFT WAS GROUNDED: EMERGENCY LIGHT DOES NOT ILLUMINATE IN FORWARD LAVATORY. REPLAMPED FORWARD LAVATORY EMERGENCY LIGHT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-24-12 - [SDR AALA202509021576](https://openairdocs.org/sdr/AALA202509021576.md): Lever · loose · Sep 1, 2025 · N170US · Airbus A321211 · Emergency Exits > AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS 3L DOOR ARM/DISARM LEVER LOOSE. MAINTENANCE TIGHTENED ARM/DISARM LEVER PER AMM 52-00-00. - [SDR AALA202508252756](https://openairdocs.org/sdr/AALA202508252756.md): Lock · jammed · Aug 21, 2025 · N170US · Airbus A321211 · Fixed Inner Doors > AIRCRAFT WAS NOT GROUNDED: LAVATORY E LOCK JAMMED. AND THE DOOR WAS REMOVED TO FREE PASSENGER. MAINTENANCE REPLACED DOOR LOCK ASSEMBLY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-45-21. - [SDR AALA202507316212](https://openairdocs.org/sdr/AALA202507316212.md): Priority Valve · leaking · Jul 30, 2025 · N170US · Airbus A321211 · Hydraulic System, Main > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO CLT DUE TO THE FLIGHT CREW REPORTING TJHAT A GREEN HYDRAULIC SYSTEM ENGINE #1 PUMP LOW PRESSURE ECAM MESSAGE DISPLAYED FOLLOWED BY A COMPLETE LOSS OF THE GREEN HYDRAULIC SYSTEM. THE - [SDR AALA202507210878](https://openairdocs.org/sdr/AALA202507210878.md): Lever · loose · Jul 21, 2025 · N170US · Airbus A321211 · Service Doors > AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTED THE HANDLE ON THE ARMING LEVER ON THE 1R DOOR IS FUNCTIONAL BUT LOOSE. MAINTENANCE TIGHTENED LOOSE THROUGH BOLT AND NUT OF ARM PLATE ON DOOR ARMING LEVER PER AMM 25-23-46. - [SDR AALA202505059058](https://openairdocs.org/sdr/AALA202505059058.md): Skin Panel · corroded · May 4, 2025 · N170US · Airbus A321211 · Wing, Plate/Skin > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE AT WS 3758 AND RIB 7. REPAIRED SKIN PANEL PER EA 362466. - [SDR AALA202505026913](https://openairdocs.org/sdr/AALA202505026913.md): Fitting · none · Apr 30, 2025 · N170US · Airbus A321211 · Landing Gear Doors > AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE RIGHT HAND MAIN LANDING GEAR DOOR FORWARD ACTUATOR FITTING, THE AFT FITTING MUST BE REPLACED PER THE INSTRUCTIONS ON EA 362968. MAINTENANCE REPLACED THE AFT FITTING PER EA 362968. - [SDR AALA202505029764](https://openairdocs.org/sdr/AALA202505029764.md): Fitting · cracked · Apr 30, 2025 · N170US · Airbus A321211 · Landing Gear Doors > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND MAIN LANDING GEAR DOOR FORWARD ACTUATOR FITTING FASTENER HOLE CRACKED ON THE KEEL BEAM BETWEEN FR 42 AND FR 43 AT KEEL BEAM RIB W10. REPLACED FITTING PER EA 362968. - [SDR AALA202504174149](https://openairdocs.org/sdr/AALA202504174149.md): Sleeve · worn · Apr 15, 2025 · N170US · Airbus A321211 · Nacelle/Pylon, Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND PYLON AFT ATTACH FITTING LOWER SLEEVE HAS WORN THREADS. REPLACED SLEEVE PER AMM 54-51-17 AND TASK CARD 26L40054002. - [SDR AALA202504016210](https://openairdocs.org/sdr/AALA202504016210.md): Hinge Arm · excess play · Mar 31, 2025 · N170US · 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 AALA202503146951](https://openairdocs.org/sdr/AALA202503146951.md): Shear Tie · corroded · Mar 12, 2025 · N170US · Airbus A321211 · Fuselage Internal Mounting Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT SHEAR TIE / CLEAT AT FR 33 BETWEEN S41R AND S42R. REPLACED SHEAR TIE / CLEAT PER SRM 51-42-11. - [SDR AALA202503122005](https://openairdocs.org/sdr/AALA202503122005.md): Floorbeam · corroded · Mar 9, 2025 · N170US · 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 AALA202503122763](https://openairdocs.org/sdr/AALA202503122763.md): Attach Fitting · corroded · Mar 8, 2025 · N170US · Airbus A321211 · Nacelle/Pylon, Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON OUTBOARD FACE OF THE RIGHT HAND SIDE FORWARD PYLON ATTACH FITTING (SHACKLE) AT PYLON STATION 6793 / RIB 4. REPLACED PYLON ATTACH FITTING PER TASK CARD 26L40054002. - [SDR AALA202503126313](https://openairdocs.org/sdr/AALA202503126313.md): Floorbeam · corroded · Mar 8, 2025 · N170US · Airbus A321211 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM AT FR 68 AND +Y765. REPLACED FLOOR BEAM PER SRM 51-42-11. - [SDR AALA202503072380](https://openairdocs.org/sdr/AALA202503072380.md): Bolt · corroded · Mar 6, 2025 · N170US · Airbus A321211 · Leading Edge Devices > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #2 ATTACHMENT BOLT AT WS 1406 AND RIB 3. REPLACED BOLT PER TASK CARD 26C61057005. - [SDR AALA202503147454](https://openairdocs.org/sdr/AALA202503147454.md): Bolt · corroded · Mar 3, 2025 · N170US · Airbus A321211 · Leading Edge Devices > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK 1 MID FORWARD BOLT AT WS 700 AND RIB 2. REPLACED BOLT PER TASK CARD 26C61057005. - [SDR AALA202503056654](https://openairdocs.org/sdr/AALA202503056654.md): Shear Plate · cracked · Mar 3, 2025 · N170US · 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 AALA202503220681](https://openairdocs.org/sdr/AALA202503220681.md): Fitting · corroded · Feb 25, 2025 · N170US · 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 AALA202503204834](https://openairdocs.org/sdr/AALA202503204834.md): Fitting · corroded · Feb 25, 2025 · N170US · Airbus A321211 · Nacelle/Pylon Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 5. REPLACED SPIGOT FITTING PER SRM 54-51-12. - [SDR AALA202503122408](https://openairdocs.org/sdr/AALA202503122408.md): Attach Fitting · corroded · Feb 24, 2025 · N170US · Airbus A321211 · Nacelle/Pylon, Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON OUTBOARD FACE OF THE FORWARD LEFT HAND SIDE PYLON ATTACH FITTING (SHACKLE) AT PYLON STATION 6793 / RIB 4. REPLACED PYLON ATTACH FITTING PER TASK CARD 26L40054002. - [SDR AALA202505026225](https://openairdocs.org/sdr/AALA202505026225.md): Hinge Fitting · cracked · Feb 21, 2025 · N170US · Airbus A321211 · Fuselage, Door Hinge > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND MAIN LANDING GEAR DOOR FORWARD HINGE FITTING FORWARD LUG, FORWARD FACE LOWER CORNER WEB CRACKED ON THE KEEL BEAM BETWEEN FR 42 AND FR 43 AT RIB W10. REPLACED HINGE FITTING PER EA 362968. - [SDR AALA202503124256](https://openairdocs.org/sdr/AALA202503124256.md): Shear Tie · corroded · Feb 20, 2025 · N170US · Airbus A321211 · Fuselage Internal Mounting Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT SHEAR TIE AT FR 32 BETWEEN S40R AND S41R. REPLACED SHEAR TIE PER SRM 51-42-11. - [SDR AALA202503234995](https://openairdocs.org/sdr/AALA202503234995.md): Shear Tie · corroded · Feb 19, 2025 · N170US · Airbus A321211 · Fuselage Internal Mounting Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT SHEAR TIE AT FR 30 BETWEEN S40R AND S41R. REPLACED SHEAR TIE PER SRM 51-42-11 AND 51-72-11. - [SDR AALA202503220337](https://openairdocs.org/sdr/AALA202503220337.md): Shear Tie · corroded · Feb 19, 2025 · N170US · Airbus A321211 · Fuselage Internal Mounting Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT SHEAR TIE / CLEAT AT FR 31 BETWEEN S40R AND S41R. REPLACED SHEAR TIE / CLEAT PER SRM 51-42-11. - [SDR AALA202503176660](https://openairdocs.org/sdr/AALA202503176660.md): Shear Tie · corroded · Feb 19, 2025 · N170US · Airbus A321211 · Fuselage Internal Mounting Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT SHEAR TIE / CLEAT AT FR 35.2, BETWEEN S40R AND S41R. REPLACED SHEAR TIE / CLEAT PER SRM 51-42-11. - [SDR AALA202503177397](https://openairdocs.org/sdr/AALA202503177397.md): Floorbeam · corroded · Feb 19, 2025 · N170US · Airbus A321211 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM AT FR 16 AND +Y503.2. REPLACED FLOOR BEAM PER SRM 51-42-11. - [SDR AALA202503177462](https://openairdocs.org/sdr/AALA202503177462.md): Shear Tie · corroded · Feb 19, 2025 · N170US · Airbus A321211 · Fuselage Internal Mounting Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT SHEAR TIE / CLEAT AT FR 35.4, BETWEEN S40R AND S41R. REPLACED SHEAR TIE / CLEAT PER SRM 51-42-11. - [SDR AALA202503173346](https://openairdocs.org/sdr/AALA202503173346.md): Shear Tie · corroded · Feb 19, 2025 · N170US · Airbus A321211 · Fuselage Internal Mounting Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT SHEAR TIE /CLEAT AT FR 35.2 BETWEEN S41R AND S42R. REPLACED SHEAR TIE / CLEAT PER SRM 51-42-11. - [SDR AALA202503146089](https://openairdocs.org/sdr/AALA202503146089.md): Shear Tie · corroded · Feb 19, 2025 · N170US · Airbus A321211 · Fuselage Internal Mounting Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT SHEAR TIE / CLEAT AT FR 35.4 BETWEEN S41R AND S42R. REPLACED SHEAR TIE / CLEAT PER SRM 51-42-11. - [SDR AALA202503122227](https://openairdocs.org/sdr/AALA202503122227.md): Shear Restraint · corroded · Feb 19, 2025 · N170US · Airbus A321211 · Fuselage Internal Mounting Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT SHEAR TIE AT FR 33 BETWEEN S40R AND S41R. REPLACED SHEAR TIE PER SRM 51-42-11. - [SDR AALA202505056630](https://openairdocs.org/sdr/AALA202505056630.md): Skin Panel · corroded · Feb 17, 2025 · N170US · Airbus A321211 · Wing, Plate/Skin > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TOP SKIN PANEL LOWER SURFACE AT WMRX4567.249 AND RIB 14. REPAIRED SKIN PANEL PER EA 362466. - [SDR AALA202505059092](https://openairdocs.org/sdr/AALA202505059092.md): Skin Panel · corroded · Feb 17, 2025 · N170US · Airbus A321211 · Wing, Plate/Skin > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TOP SKIN PANEL LOWER SURFACE AT WMRX5097.109 AND RIB 15. REPAIRED SKIN PANEL PER EA 362466. - [SDR AALA202505057776](https://openairdocs.org/sdr/AALA202505057776.md): Skin Panel · corroded · Feb 17, 2025 · N170US · Airbus A321211 · Wing, Plate/Skin > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TOP SKIN PANEL LOWER SURFACE AT WS 3758 AND RIB 7. REPAIRED SKIN PANEL PER EA 362689. - [SDR AALA202505025944](https://openairdocs.org/sdr/AALA202505025944.md): Frame · cracked · Feb 17, 2025 · N170US · Airbus A321211 · Fuselage Main, Frame > AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME UPPER DOUBLE JOGGLE AREA FASTENER HOLE AT FR 16 AND S10R. REPAIRED FRAME PER EA 362408. - [SDR AALA202504104506](https://openairdocs.org/sdr/AALA202504104506.md): Fitting · cracked · Feb 17, 2025 · N170US · Airbus A321211 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT FR 16 RIGHT AND #7 DOOR STOP FITTING. REPLACED INTERCOSTAL FITTING PER SRM 51-42-11. - [SDR AALA202503126493](https://openairdocs.org/sdr/AALA202503126493.md): Hinge Arm · excess play · Feb 17, 2025 · N170US · 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 AALA202503123403](https://openairdocs.org/sdr/AALA202503123403.md): Hinge Arm · excess play · Feb 17, 2025 · N170US · 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 AALA202503121907](https://openairdocs.org/sdr/AALA202503121907.md): Hinge Arm · excess play · Feb 17, 2025 · N170US · 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 AALA202503129824](https://openairdocs.org/sdr/AALA202503129824.md): Hinge Arm · excess play · Feb 17, 2025 · N170US · 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. Next page: https://openairdocs.org/aircraft/N170US/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 = 'N170US' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N170US/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.