# Service difficulty reports: N234WN A list on [N234WN](https://openairdocs.org/aircraft/N234WN.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 · 287 reports - [SDR SWAA2026072118406](https://openairdocs.org/sdr/SWAA2026072118406.md): Handle · cracked · Jul 17, 2026 · N234WN · Boeing 7377H4 · Emergency Exits > RIGHT OVER-WING EXIT DOOR LIFT HANDLE ATTACH HOUSING HAS A CRACK PROTRUDING FROM THE FWD NUT PLATE. REMOVED AND REPLACED RIGHT O/W EXIT DOOR LIFT HANDLE HOUSING PER AMM 52-22-51. - [SDR SWAA2026072150153](https://openairdocs.org/sdr/SWAA2026072150153.md): Battery Pack · no test · Jul 17, 2026 · N234WN · Boeing 7377H4 · Emergency Lighting > AFT RT EMERGENCY BATTERY PACK M1672 FAILED CAPACITY CHECK. R & R EMERGENCY BATTERY PACK PER AMM 33-51-06. - [SDR SWAA2026021069152](https://openairdocs.org/sdr/SWAA2026021069152.md): Slide · dislodged · Feb 8, 2026 · N234WN · Boeing 7377H4 · Escape Slide > R1 DOOR SLIDE PARTIALLY FELL FROM HOUSING. REMOVED AND REINSTALLED THE SLIDE IAW MT 725-61-06. - [SDR SWAA2026020667279](https://openairdocs.org/sdr/SWAA2026020667279.md): Fuse · failed · Feb 3, 2026 · N234WN · Boeing 7377H4 · Emergency Lighting > RIGHT OVERWING EMERGENCY EXIT WINDOW LIGHT INOPERATIVE. REMOVED AND REPLACED FUSE TO RIGHT OVERWING EMERGENCY EXIT WINDOW LIGHT, OPS CHECKED GOOD IAW AMM 33-22-00. - [SDR SWAA2025120132373](https://openairdocs.org/sdr/SWAA2025120132373.md): Floorbeam · cracked · Nov 6, 2025 · N234WN · Boeing 7377H4 · Fuselage Main, Floor Beam > CRACKED FLOORBEAM ANGLE BS 695, LBL24.75. REPLACED FLOORBEAM ANGLE IAW SRM 51-40-02, SRM 51-10-02, AND DWG 273A9110, SHEET 6, REV A. - [SDR SWAA2025120130501](https://openairdocs.org/sdr/SWAA2025120130501.md): Intercostal · corroded · Oct 31, 2025 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORRODED INTERCOSTAL FL SEAL, BS 1016, BETWEEN LBL10 - LBL 8.39. REPLACED INTERCOSTAL FL SEAL AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, AND DWG 148A0922, SHEET 20, REV -. - [SDR SWAA2025120130272](https://openairdocs.org/sdr/SWAA2025120130272.md): Stringer · corroded · Oct 30, 2025 · N234WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer > CORROSION ON STRINGER 25R, BETWEEN BS 360 - 380, WL156 IN E & E BAY. PERFORMED PERMANENT REPAIR ON THE STRINGER IAW SRM 53-00-03-2R-1, REPAIR 1. - [SDR SWAA2025120130273](https://openairdocs.org/sdr/SWAA2025120130273.md): Angle · corroded · Oct 30, 2025 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORRODED ANGLE, BETWEEN BS 351.2 - 360, S28L, WL 148.8. REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, AND DWG 140A9101, SHEET 23, SHEET 26, REV -. - [SDR SWAA2025120129789](https://openairdocs.org/sdr/SWAA2025120129789.md): Panel · damaged · Oct 29, 2025 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > ELONGATED HOLE ON BULKHEAD PANEL 141JW. FABRICATED A NEW BULKHEAD PANEL IAW AMM 25-52-01-201-801, STEP 1 F, AND DWG 453A2510, SHEET 4, REV-. - [SDR SWAA2025120129910](https://openairdocs.org/sdr/SWAA2025120129910.md): Scuff Plate · cracked · Oct 29, 2025 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED CENTER SCUFF PLATE IN THE FWD CARGO BAY. REPAIRED CENTER SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, AND BAC 5975. - [SDR SWAA2025120129911](https://openairdocs.org/sdr/SWAA2025120129911.md): Floor Support · cracked · Oct 29, 2025 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED FLOOR ANGLE, BS 291.5 - 294.5, STRINGER 17R. REPLACED THE FLOOR ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, AND DWG 141A8310, SHEET 25, REV. - [SDR SWAA2025120129794](https://openairdocs.org/sdr/SWAA2025120129794.md): Nut Plate · cracked · Oct 29, 2025 · N234WN · Boeing 7377H4 · Wing, Attach Fittings > CRACKED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE, SS 508 RT WING. REPLACED RAIL NUT PLATES IAW SRM 51-10-02, PARAGRAPH 9, AND SRM 51-40-02. - [SDR SWAA2025120129898](https://openairdocs.org/sdr/SWAA2025120129898.md): Rib · cracked · Oct 29, 2025 · N234WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib > CRACKED LEADING EDGE RIB ACCESS PANEL 331B HSS 95.96 ON THE LT HORIZONTAL STAB LEADING EDGE. REPLACED THE LEADING EDGE RIB ACCESS PANEL IAW SRM 51-10-02, SRM 51-40-02, AND DWG 186A1001, SHEET 10. - [SDR SWAA2025120129790](https://openairdocs.org/sdr/SWAA2025120129790.md): Rib · cracked · Oct 29, 2025 · N234WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib > CRACKED RIB HSS 95.96 ACCESS PANEL 341B ON LEADING EDGE OF THE RT HORIZONTAL STAB. REPLACED RIB AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 186A1001, REV A.. - [SDR SWAA2025120129792](https://openairdocs.org/sdr/SWAA2025120129792.md): Rib · cracked · Oct 29, 2025 · N234WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib > CRACKED RIB ON THE LE, HSS 105.26 ACCESS PANEL 341B. REPLACED THE RIB AND FASTENERS ON THE LEADING EDGE ACCESS PANEL IAW 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 186A1001, REV A. - [SDR SWAA2025120129899](https://openairdocs.org/sdr/SWAA2025120129899.md): Rib · cracked · Oct 29, 2025 · N234WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib > CRACKED LEADING EDGE RIB ACCESS PANEL 331B, LE HSS 105.26. REPLACED RIB AND FASTENERS ON LEADING EDGE ACCESS PANEL 331B IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 186A1001, REV A. - [SDR SWAA2025120129913](https://openairdocs.org/sdr/SWAA2025120129913.md): Tie Clip · cracked · Oct 29, 2025 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED TIE CLIP, BS 277, S10R. REPLACED THE TIE CLIP AND FASTENERS IAW SRM 51-10-02 ITEM 9, AND DWG 141A1110, SHEET 18, REV-, AND DWG 141A8380, SHEET 21, REV-. - [SDR SWAA2025120129912](https://openairdocs.org/sdr/SWAA2025120129912.md): Frame · cracked · Oct 29, 2025 · N234WN · Boeing 7377H4 · Fuselage Main, Frame > CRACKED FRAME, BS 312, S5L - 6L IN THE PASSENGER CABIN. PERFORMED REPAIR ON THE FRAME IAW EA M-22-153-01244. - [SDR SWAA2025120129793](https://openairdocs.org/sdr/SWAA2025120129793.md): Nut Plate · cracked · Oct 29, 2025 · N234WN · Boeing 7377H4 · Wing, Attach Fittings > CRACK ON RAIL NUT PLATES LOCATED OFSS 483 INTERNAL CAVITY LEADING EDGE AT RT WING. REPLACED RAIL NUT PLATES AND FASTENERS IAW SRM 51-10-02 AND SRM 51-40-02. - [SDR SWAA2025120129542](https://openairdocs.org/sdr/SWAA2025120129542.md): Support Angle · cracked · Oct 28, 2025 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED SUPPORT ANGLE, BS 500D, STRINGER 28R IN THE FWD CARGO BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, SRM 51-10-02, PARAGRAPH 9, & DRAWING 143A7902, SHEET 126, REV A. - [SDR SWAA2025120129539](https://openairdocs.org/sdr/SWAA2025120129539.md): Stringer · cracked · Oct 28, 2025 · N234WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer > CRACKED STRINGER 23L, BS 540 IN THE FWD CARGO BAY. REPAIRED THE STRINGER IAW SRM 53-00-03-2R-1, REPAIR 1. - [SDR SWAA2025120129388](https://openairdocs.org/sdr/SWAA2025120129388.md): Fitting · damaged · Oct 28, 2025 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > ELONGATED HOLES ON FITTING, BS 1016. REPLACED THE FITTING IAW SRM 51-10-02, ITEM 9, SRM-51-40-02-0G, AND DWG 148A2230, SHEET 8, REV C. - [SDR SWAA2025120129127](https://openairdocs.org/sdr/SWAA2025120129127.md): Angle · cracked · Oct 28, 2025 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED ANGLE, LOCATED BS 500C AT LEVEL S26R IN FWD CARGO COMPARTMENT. THE CRACKED ANGLE WAS RESOLVED ON ANOTHER FAULT TTG8Q015ZPF7. - [SDR SWAA2025120129129](https://openairdocs.org/sdr/SWAA2025120129129.md): Support · corroded · Oct 27, 2025 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION SUPPORT ZEE LOCATED BS 500A TO BS 500D, LBL 24 AND WL156 AT FWD CARGO COMPARTMENT. REPLACED SUPPORT ZEE AND FASTENERS LOCATED BS 480 TO BS 500D, LBL24 AND WL156 AT FWD CARGO COMPARTMENT IAW SRM 51-40-02, SRM 51-10-02 ITEM 9, SRM 53-00-53-2R-6, REP - [SDR SWAA2025120129121](https://openairdocs.org/sdr/SWAA2025120129121.md): Support · corroded · Oct 27, 2025 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON SUPPORT ZEE LOCATED BTW BS 727B TO BS 767, RBL22 AND WL156 AT AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE LOCATED BTW BS 727B TO BS 767, RBL22 AND WL156 AT AFT CARGO COMPARTMENT IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 146A7500 SHEET 85 REV - [SDR SWAA2025120129120](https://openairdocs.org/sdr/SWAA2025120129120.md): Shield · corroded · Oct 27, 2025 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORRODED SHIELD BETWEEN BS 767 - 787, RBL 22, WL 156. REPLACED WITH A NEW SHIELD IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 146A0081, SHEET 31, REV -. - [SDR SWAA2025120129119](https://openairdocs.org/sdr/SWAA2025120129119.md): Support · corroded · Oct 27, 2025 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION SUPPORT ZEE LOCATED BTW BS 727C - 807, LBL 22, WL156 IN THE AFT CARGO BAY. REPLACED SUPPORT ZEE IAW SRM 51-40-02; SRM 51-10-02, PARAGRAPH 9, SRM 53-00-53-2R-6, REPAIR 6, PARAGRAPH 4, AND DRAWING 146A7500, SHEET 85, REV A. - [SDR SWAA2025120129116](https://openairdocs.org/sdr/SWAA2025120129116.md): Support Channel · cracked · Oct 27, 2025 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED SUPPORT CHANNEL, BS 727, STRINGER 27R IN THE AFT CARGO BAY. REPLACED THE SUPPORT CHANNEL IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 144A2600, SHEET 566, REV -. - [SDR SWAA2025120129117](https://openairdocs.org/sdr/SWAA2025120129117.md): Cargo Track · cracked · Oct 27, 2025 · N234WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings > CRACKED TRACK RBBL 13.84, BS 727E. PERFORMED PERMANENT REPAIR ON TRACK, BS 727D+12 AND BS 727E+8. IAW SRM 53-00-53-2R-3, REPAIR 3, PARAGRAPH 4. - [SDR SWAA2025120129014](https://openairdocs.org/sdr/SWAA2025120129014.md): Pin · corroded · Oct 27, 2025 · N234WN · Boeing 7377H4 · Horizontal Stabilizer Structure > CORROSION ON THE PIN ATTACHED TO THE REAR RT STABILIZER LOWER POSITION. REPLACED PIN IAW AMM 27-41-11-000-801, AND 27-41-11-401-801. - [SDR SWAA2025120129112](https://openairdocs.org/sdr/SWAA2025120129112.md): Angle · cracked · Oct 27, 2025 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED ANGLE, BS 907 PLUS 7 INCHES, S26R. REPLACED THE ANGLE IAW SRM 51-10-02, PARAGRAPH 9, AND DRAWING 147A7221, SHEET 24, REV -. - [SDR SWAA2025120129118](https://openairdocs.org/sdr/SWAA2025120129118.md): Angle · cracked · Oct 27, 2025 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED ANGLE, BS 907 PLUS 11 INCHES, S26R. REPLACED ANGLE LOCATED BS 907 PLUS 11 INCHES, S26R IAW SRM 51-10-02, PARAGRAPH 9, AND DRAWING 147A7221, SHEET 24, REV -. - [SDR SWAA2025120129125](https://openairdocs.org/sdr/SWAA2025120129125.md): Angle · cracked · Oct 27, 2025 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED ANGLE, BS 500B, S26R IN THE FWD CARGO COMPARTMENT. REPLACED ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 6, REV D. - [SDR SWAA2025120129126](https://openairdocs.org/sdr/SWAA2025120129126.md): Angle · cracked · Oct 27, 2025 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED ANGLE, BS 500C AFT POSITION AT S26L IN THE FWD CARGO COMPARTMENT. REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 143A7505, SHEET 9, REV A. - [SDR SWAA2025120129122](https://openairdocs.org/sdr/SWAA2025120129122.md): Sill Drain · corroded · Oct 27, 2025 · N234WN · Boeing 7377H4 · Fuselage Main, Structure > CORROSION ON LOWER SILL LOCATED BTW BS794.3 AND BS847 RBL26 AND WL 156 AFT CARGO COMPARTMENT. REPLACED LOWER SILL LOCATED BTW BS794.3 AND BS847 RBL26 AND WL156 AFT CARGO COMPARTMENT IAW SRM 51-10-02; SRM 51-40-02 AND DWG 146A8340 SHEET 28 REV -. - [SDR SWAA2025120129124](https://openairdocs.org/sdr/SWAA2025120129124.md): Support Angle · corroded · Oct 27, 2025 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION SUPPORT ANGLE LOCATED BS 727D, LBL 27, AND WL 155 AT AFT CARGO COMPARTMENT. REPLACED SUPPORT ANGLE, IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, DWG 146A1220, SHEET 52, REV -. - [SDR SWAA2025120128825](https://openairdocs.org/sdr/SWAA2025120128825.md): Bracket · cracked · Oct 26, 2025 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK BRACKET LOCATED BS 540 PLUS 4 INCHES, LBL 8 AT AIR CONDITIONING BAY. REPLACED THE BRACKET AT AIR CONDITIONING BAY IAW SRM 51-40-02-0G-0, DUE TO ALLOWABLE DAMAGE NOT FOUND SRM 53-40-71-1A-1. CRACK MEASUREMENT: 0.400 IN. - [SDR SWAA2025120128162](https://openairdocs.org/sdr/SWAA2025120128162.md): Pressure Deck · cracked · Oct 25, 2025 · N234WN · Boeing 7377H4 · Fuselage Main, Structure > CRACK INDICATION ON THE HORIZONTAL PRESSURE DECK WEB, LBL 40, BS 663. PERFORMED A PERMANENT REPAIR ON HORIZONTAL PRESSURE DECK WEB IAW SRM 53-40-51-2R-2, REPAIR 2. - [SDR SWAA2025120128551](https://openairdocs.org/sdr/SWAA2025120128551.md): Rib · cracked · Oct 25, 2025 · N234WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib > CRACKED INSPAR RIB, HSS 120.30 AND 17 INCHES FROM FRONT SPAR IN THE RT HORIZONTAL STAB. PERFORMED A PERMANENT REPAIR ON INSPAR RIB IAW SRM 55-10-09-2R-4, REPAIR 4. - [SDR SWAA2025120128163](https://openairdocs.org/sdr/SWAA2025120128163.md): Stub Frame · cracked · Oct 25, 2025 · N234WN · Boeing 7377H4 · Fuselage Main, Frame > ONE CRACK INDICATION ON STUB FRAME, BS 294.5 BETWEEN S8 --9, CRACK LENGTH 1.4 INCH. REPLACED STUB FRAME IAW SRM 51-40-02, DWG 141A8370, SHEET 9, REV D, SHEET 10, REV-. - [SDR SWAA2025120128159](https://openairdocs.org/sdr/SWAA2025120128159.md): Panel · cracked · Oct 24, 2025 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED BULKHEAD PANEL 142MW. FABRICATED A NEW BULKHEAD PANEL IAW AMM 25-52-01-201-801, STEP 1 F, AND DWG 453A2510, SHEET 6, REV A. - [SDR SWAA2025120127987](https://openairdocs.org/sdr/SWAA2025120127987.md): Floorbeam · cracked · Oct 24, 2025 · N234WN · Boeing 7377H4 · Fuselage Main, Floor Beam > CRACKED FLOORBEAM ANGLE, BS 695, LBL24.75. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-40-02 AND DWG 273A9110, SHEET 6, REV A, CORRECTED STEPS ARE DOCUMENTED ON FAULT TTG8Q018Q32G. - [SDR SWAA2025120127988](https://openairdocs.org/sdr/SWAA2025120127988.md): Angle · cracked · Oct 24, 2025 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED ANGLE, BS 500C, S26R IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 6, REV D. - [SDR SWAA2025120127592](https://openairdocs.org/sdr/SWAA2025120127592.md): Lens · broken · Oct 23, 2025 · N234WN · Boeing 7377H4 · Emergency Lighting > BROKEN LENS ON EMERGENCY LIGHT AT HEADER PANEL FWD RT SIDE. REPLACED THE LENS IAW SOPM 20-50-01, REV 39. - [SDR SWAA2025120127598](https://openairdocs.org/sdr/SWAA2025120127598.md): Scuff Plate · cracked · Oct 23, 2025 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED AFT CORNER SCUFF PLATE IN THE AFT CARGO BAY. REPAIRED THE AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975. - [SDR SWAA2025120127596](https://openairdocs.org/sdr/SWAA2025120127596.md): Scuff Plate · cracked · Oct 23, 2025 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK ON FWD CORNER SCUFF PLATE IN THE AFT CARGO BAY. REPAIRED FWD CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975. - [SDR SWAA2025120127597](https://openairdocs.org/sdr/SWAA2025120127597.md): Access Panel · elongated · Oct 23, 2025 · N234WN · Boeing 7377H4 · Wing, Plate/Skin > ELONGATED HOLE ON ACCESS PANEL 661BB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661BB IAW SRM 51-70-04-2R-10, REPAIR 10. - [SDR SWAA2025120126621](https://openairdocs.org/sdr/SWAA2025120126621.md): Scuff Plate · cracked · Oct 22, 2025 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED AFT CORNER SCUFF PLATE IN THE FWD CARGO BAY. REPAIRED THE AFT CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, AND BAC 5975. - [SDR SWAA2025120127122](https://openairdocs.org/sdr/SWAA2025120127122.md): Handle · deteriorated · Oct 22, 2025 · N234WN · Boeing 7377H4 · Passenger/Crew Doors > DETERIORATED ASSIST HANDLE NUT FWD ENTRY AND SERVICE DOORS. REPLACED THE ASSIST HANDLE NUTS IAW AMM 52-11-31-400-802, STEP 3.G (2). - [SDR SWAA2025120127124](https://openairdocs.org/sdr/SWAA2025120127124.md): Handle · deteriorated · Oct 22, 2025 · N234WN · Boeing 7377H4 · Passenger/Crew Doors > DETERIORATED ASSIST HANDLE NUT ON AFT ENTRY AND SERVICE DOORS. REPLACED ASSIST HANDLE NUT AFT ENTRY AND SERVICE DOORS IAW AMM 52-13-31-400-802, STEP 3.G (2), AND AMM 52-41-31-400-802, STEP 3.F (2). Next page: https://openairdocs.org/aircraft/N234WN/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 = 'N234WN' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N234WN/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.