N259WN

Service difficulty reports · 332

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N259WN' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWAA2026092314330Access Panel · crackedCRACKED ACCESS PANEL 524DB ON LEADING EDGE NR 2 SLAT, LT WING. REPLACED THE ACCESS PANEL 524DB IAW SRM 51-10-02, ITEM 9.Sep 19, 2026 · N259WN · Boeing 7377H4 · Leading Edge DevicesSDR SWAA2026092335082Web · crackedCRACKED WEB, BS 500B - 500C, LBL 21.80. REPLACED THE WEB AND FASTENERS, IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHT 81, REV-.Sep 11, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026092374661Fan Cowl · damagedELONGATED HOLE LOCATED ON OUTBOARD FAN COWL 0.500 INCH FROM FWD EDGE AND 3.375 INCH FROM LOWER EDGE AT ENGINE 1. EVALUATED HOLE LOCATED ON OTBD FAN COWL 0.500 INCH FROM FWD EDGE AND 3.375 INCH FROM LOWER EDGE AT ENGINE AND FOUND WITHIN LIMITS IAW CMM 71-13-3Sep 5, 2026 · N259WN · Boeing 7377H4 · Nacelle/Pylon, Main FrameSDR SWAA2026092313467Web · crackedWEB CRACKED AROUND FASTENER HOLE, BS 251+ 6 INCHES, RBL 5. PERFORMED A PERMANENT REPAIR BTWN BS 251 - 255, RBL 3.60 - 15.32 IAW SRM 51-40-02, & EA 26-153-02349.Aug 25, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026092129407Vapor Barrier · crackedCRACKED VAPOR BARRIER, BS 663.75, LBL 27. REPAIRED THE VAPOR BARRIER. THIS FAULT IS DOCUMENTED ON TTG8Q01DQ62J.Aug 24, 2026 · N259WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2026092188686Vapor Barrier · crackedCRACKED VAPOR BARRIER, BS 663.75, LBL 27. REPAIRED THE VAPOR BARRIER, FAULT IS DOCUMENTED ON TTG8Q01DQ62J.Aug 24, 2026 · N259WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2026092119869Vapor Barrier · crackedCRACKED VAPOR BARRIER BS 663.75 AND LBL 27 AT MAIN WHEEL WELL COMPARTMENT. REPAIRED VAPOR BARRIER BS 663.75 AND LBL 27 AT MAIN WHEEL WELL COMPARTMENT.Aug 24, 2026 · N259WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2026092176156Vapor Barrier · crackedCRACK 4 VAPOR BARRIER BS 663.75 AND LBL 27 AT MAIN WHEEL WELL . REPAIRED VAPOR BARRIER BS 663.75 AND LBL 27 AT MAIN WHEEL WELL.Aug 24, 2026 · N259WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2026092167858Vapor Barrier · crackedCRACKED VAPOR BARRIER, BS 663.75, LBL 27, IN THE MAIN WHEEL WELL. REPAIRED THE VAPOR BARRIER, FAULT DOCUMENTED ON TTG8Q01DQ62J.Aug 24, 2026 · N259WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2026092355100Bracket · damagedELONGATED HOLE ON BRACKET, LBL 10, BS 663. EVALUATED AND FABRICATED A NEW BRACKET IAW SRM 51-40-05, & DWG 287A4413, SHEET 66, REV-. THE BRACKET INSTALLATION WILL BE ACCOMPLISHED IAW TTG8Q01DQJAM STEP 23.Aug 23, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026092147085Support Frame · damagedELONGATED HOLE ON SUPPORT FRAME LOCATED ON VAPOR BARRIER LT SIDE BTWN BS 649 - 670, LBL 15 IN THE MAIN WHEEL WELL. EVALUATED & FABRICATED SUPPORT FRAME IAW SRM 51-40-05-0G-0, AND DWG 149A7214, SHEET 7 REV -. FRAME INSTALLATION WILL BE ACCOMPLISHED TTG8Q01DQAug 22, 2026 · N259WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026092343474Shear Angle · crackedCRACKED SHEAR ANGLE, BS 658 - BS638, LBL 40.875. FABRICATED & REPLACED THE SHEAR ANGLE & FASTENERS IAW SRM 51-10-02, ITEM 9, & DWG 110A0220, SHEET 2, REV-.Aug 21, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026092352715Bullnose · crackedLEFT WING, NR 2 KRUEGER FLAP, BULL NOSE CRACKED AT CENTER RIB. REMOVED AND REPLACED THE LT WING MID BULL NOSE KRUEGER FLAP NR 2 IAW CMM 57-56-44-NG.Aug 20, 2026 · N259WN · Boeing 7377H4 · Leading Edge DevicesSDR SWAA2026092374461Bracket · crackedCRACKED BRACKET ANGLE BTW BS 188 - 203, RBL 3, LOWER NOSE COMPARTMENT. REPLACED THE BRACKET ANGLE AND FASTENERS IAW SRM 51-40-02, AND DWG 141A9194, SHEET 4, REV D.Aug 20, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026092142001Floor Panel · delaminatedDELAMINATED FLOOR PANEL 241FF AT PASSENGER CABIN. REPAIRED FLOOR PANEL 241FF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-17-REPAIR 7Aug 19, 2026 · N259WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026092196832Floor Panel · debondedDEBONDED FLOOR PANEL 241DF IN THE PAX CABIN. REPAIRED FLOOR PANEL 241DF IAW SRM 53-00-50-2R-1, REPAIR 1.Aug 18, 2026 · N259WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026092169875Doubler · crackedCRACK ON DOUBLER LOCATED ON RBL 54.21 TO RBL 72 AT VAPOR BARRIER RH SIDE UPPER POSITION. EVALUATED AND FABRICATED DOUBLER LOCATED ON BS 663 RBL 54.21 TO RBL 72 AT VAPOR BARRIER RH SIDE UPPER POSITION I.A.W SRM 51-20-01-0G-0 DWG: 111A1521 SHEET: 5 REV: -.Aug 18, 2026 · N259WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2026092156695Doubler · damagedELONGATED HOLE ON DOUBLER ON VAPOR BARRIER, RT SIDE UPPER POSITION BTWN RBL 40 - 45 IN THE MAIN WHEEL WELL. EVALUATED & FABRICATED A DOUBLER IAW SRM 51-40-05, DWG 111A1511, SHEET 16, REV-, PL 11A1511, ITEM 16, REV B, & DWG 111A1151, SHEET 6, REV-.Aug 18, 2026 · N259WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2026092313059Nut Plate · crackedCRACKED NUT PLATE, OFSS 604, INTERNAL CAVITY LEADING EDGE, RT WING. REPLACED THE NUT PLATE BTWN OSS 362.51 - 384.24. IAW SRM 51-40-02, & DWG 112A4402, SHEET 14, REV-.Aug 17, 2026 · N259WN · Boeing 7377H4 · Wing, Attach FittingsSDR SWAA2026092332053Doubler · damagedELONGATE HOLE ON DOUBLER ON REAR SPAR, RT VAPOR BARRIER BS 663 BTWN RBL12 - 27. FABRICATED A DOUBLER, & LOCATED IAW DWG 111A1512, SHT 3, REV-.Aug 17, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026092106314Nut Plate · crackedCRACKED NUT PLATE, OFSS 404, INTERNAL CAVITY L/E OF LT WING. REPLACED THE NUT PLATE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 112A4402, SHEET 40, REV A.Aug 17, 2026 · N259WN · Boeing 7377H4 · Wing, Attach FittingsSDR SWAA2026092101997Support Frame · damagedELONGATE HOLE ON FRAME ON RT VAPOR BARRIER BTWN BS 655 - BS 693, RBL 12. EVALUATED & FABRICATED THE FRAME IAW SRM 51-40-05-0G-0, & DWG 149A7214, SHEET 7, REV -. DOUBLER INSTALLATION WILL BE ACCOMPLISHED TTG8Q01DQJAS.Aug 17, 2026 · N259WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026092127237Nut Plate · crackedCRACKED RAIL NUT PLATE LOC OFSS 570, INTERNAL CAVITY LEADING EDGE OF RT WING. REMOVED THE NUT PLATE IAW SRM 51-40-01 AND PERFORMED VISUAL INSPECTION ON ADJACENT AREAS AND DID NOT FIND OTHER DAMAGE. REPLACED THE NUT PLATE IAW SRM 51-40-01, SRM 51-40-02, SRM Aug 17, 2026 · N259WN · Boeing 7377H4 · Wing, Attach FittingsSDR SWAA2026092130117Nut Plate · crackedCRACKED RAIL NUT PLATE, OFSS 491 INTERNAL CAVITY LEADING EDGE IN THE RT WING. REPLACED RAIL NUT PLATE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 112A4402, SHEET 40, REV A.Aug 17, 2026 · N259WN · Boeing 7377H4 · Wing, Attach FittingsSDR SWAA2026092188030Nut Plate · crackedCRACKED RAIL NUT PLATE, OFSS 385 INTERNAL CAVITY LEADING EDGE OF THE LT WING. REPLACED THE RAIL NUT PLATE IAW SRM 51-40-02, AND DWG 112A4402, SHEET 40, REV A.Aug 17, 2026 · N259WN · Boeing 7377H4 · Leading Edge DevicesSDR SWAA2026092147620Nut Plate · crackedCRACKED RAIL NUT PLATE, OFSS 337 INTERNAL CAVITY LEADING EDGE OF LT WING. REPLACED THE NUT PLATE IAW SRM 51-40-02, AND DWG 112A4402, SHEET 40, REV A.Aug 17, 2026 · N259WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2026092127663Nut Plate · crackedCRACKED RAIL NUT PLATE, OFSS 588 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT PLATE IAW SRM 51-40-02-0G-0, & DWG 112A4402, SHEET 13, REV-.Aug 17, 2026 · N259WN · Boeing 7377H4 · Wing, Attach FittingsSDR SWAA2026092109501Nut Plate · crackedCRACK RAIL NUT PLATE LOC OFSS 449 INTERNAL CAVITY LEADING EDGE AT RT WING. REPLACED THE NUT PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG:112A4402, SHEET 40, REV A.Aug 17, 2026 · N259WN · Boeing 7377H4 · Wing, Attach FittingsSDR SWAA2026092186645Nut Plate · crackedCRACKED RAIL NUT PLATE LOC OFSS 491 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT PLATE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 112A4402, SHEET 40, REV A.Aug 17, 2026 · N259WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2026092309524Support · scratchedSCRIBE MARKS LOCATED ON SUPPORT ZEE BTW BS 400 - 488, LBL 21.8, IN THE FWD CARGO BAY. PERFORMED A PERMANENT REPAIR ON THE SUPPORT ZEE IAW SRM 53-00-53-2R-6, REPAIR 6.Aug 16, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026092374341Bracket · damagedELONGATE HOLE ON BRACKET ASSY LOCATED AT RT VAPOR BARRIER BS 663, RBL 31. EVALUATED & FABRICATED BRACKET ASSY IAW SRM 51-40-05-0G-0, & DWG 287A9112, SHEET 13, REV. A. FOR INSTALLATION OF THE BRACKET, SEE TTG8Q01DQJA.Aug 16, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026092192990Strap · missingMISSING STRAP ON LIFE LINE OF THE EMERGENCY DOORS LT & RT. INSTALLED THE STRAP ON LIFE LINE IAW SOPM 20-50-12, REV 56, & DWG 416A1500, REV-.Aug 16, 2026 · N259WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2026092135422Web · crackedCRACKED WEB LOCATED BTWN BS 500D - 520, STR 28L IN THE FWD CARGO BAY. REPLACED THE WEB AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7902, SHEET 126, REV A.Aug 16, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026092387797Support · damagedSCRIBE MARKS ON SUPPORT ZEE BTWN BS 727 - 847, LBL 21.80. REPLACED THE SUPPORT ZEE IAW SRM 51-40-02, AND DWG 146A7500, SHT 85, REV A.Aug 15, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026092397570Elec Connector · damagedCUT ON GALLEY 1 EMERGENCY EXIT LIGHT CABLE. REPLACED THE CONNECTOR ON WIRE W4142 D03658 IAW SWPM 20-30-12, AND PERFORMED EMERGENCY LIGHT OPS TEST IAW AMM 33-51-00-710-801.Aug 15, 2026 · N259WN · Boeing 7377H4 · Light System WiringSDR SWAA2026092376151Shield · corrodedCORRODED SHIELD WEB, BS 767 - 794.3, WL156, RBL 22. DRILLED DIAMETER FASTENERS HOLES (10 EA) TO ATTACH FLOOR PANEL TO SHIELD WEB. IAW SRM 51-40-05, & DWG 146A0081, SHT 46, REV -. DIAMETER HOLES IS 0.221 INCH.Aug 15, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026092372218Gusset · crackedCRACKED GUSSET, BS 500D, S19L. REPLACED THE GUSSET AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7902, SHEET 174, REV -.Aug 15, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026092345565Frame · dentedDENTED FRAME, BS 500B, STR 25L - 26L IN THE FWD CARGO BAY. MADE & DRILLED A REPAIR FOR FRAME BS 500B, STR 25L - 26L IAW SRM 53-30-07-2R-1, REPAIR 1, ALTERNATIVE 1.Aug 15, 2026 · N259WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2026092107956Hook · corrodedCORROSION ON LEFT EMERGENCY EXIT DOOR LIFE LINE HOOK. REPLACED THE LIFE LINE HOOK IAW AMM 25-61-10-000-802, AND AMM 25-61-10-400-802.Aug 15, 2026 · N259WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2026092107556Hook · corrodedCORROSION ON THE EMERGENCY EXIT DOOR LIFE LINE HOOK. REPLACED THE LIFE LINE HOOK IAW AMM 25-61-10-000-802, AND AMM 25-61-10-400-802 .Aug 15, 2026 · N259WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2026092109333Fastener · wornWORN HARDWARE ON GIRT BAR FITTING, AFT SERVICE & ENTRY DOORS. REPLACED THE HARDWARE IAW AMM 25-66-02-400-801.Aug 15, 2026 · N259WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2026092362109Support · corrodedCORRODED LOWER SILL BTWN BS 794.5 - 847, RBL 23, WL 156. REMOVED CORROSION AND EVALUATED REWORKED AREAS LOWER SILL IAW SRM 53-60-15-1A-1.Aug 14, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026092167397Vapor Barrier · crackedCRACKED VAPOR BARRIER, BS 663.75, LBL 27. REPAIRED THE VAPOR BARRIER IAW SRM 51-70-04-2R-10, REPAIR 10.Aug 14, 2026 · N259WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2026092181079Vapor Barrier · crackedCRACK VAPOR BARRIER BS 663.75 AND RBL 32 AT MAIN WHEEL WELL COMPARTMENT. REPAIRED VAPOR BARRIER BS 663.75 AND RBL 32 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.Aug 14, 2026 · N259WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2026092169457Crossbeam · crackedCRACKED FLOOR CROSSBEAM, BS 540, BTWN BL 0 - RBL 24.75. REPLACED THE CROSSBEAM IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 143A0060, SHEET 46, REV -.Aug 14, 2026 · N259WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026092105704Support Angle · crackedCRACKED SUPPORT ANGLE, BS 663.75, RBL 7. INSTALLED A PERMANENT REPAIR TO THE SUPPORT ANGLE IAW SRM 57-10-10-2R-5, REPAIR 5, AND DWG 111A100, SHEET 226, REV A.Aug 14, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026092132662Fastener · wornWORN HARDWARE ON GIRT BAR FITTING, FWD SERVICE & ENTRY DOORS. REPLACED THE HARDWARE IAW AMM 25-66-02-400-801.Aug 13, 2026 · N259WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2026092139517Strap · corrodedCORROSION STRAP RH SIDE LOCATED ON STR 25R BETWEEN BS 727 TO 727E AT AFT CARGO COMPARTMENT. EVALUATED CAPSTRIP LOC. ON RH SIDE STR 25R BETWEEN BS 727 TO BS 727E AT AFT CARGO COMPARTMENT AND NOT FOUND ALLOWABLE DAMAGE I.A.W B737-700 SRM 53-00-53-1A-2 CAPSTRIPAug 12, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026092146324Strap · corrodedCORRODED STRAP, BTWN BS 767 - 847, STR 25L IN THE AFT CARGO BAY. EVALUATED CORROSION ON CAPSTRIP & DID NOT FIND ALLOWABLE DAMAGE IAW SRM 53-00-53-1A-2. REPLACED THE CAPSTRIP (STRAP) IAW SRM 51-10-02-0G, STEP 9, AND DWG 453A2600, SHEET 92, REV A.Aug 12, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026092128302Strap · corrodedCORRODED STRAP, STRINGER 25L, BS 727 - 727E IN THE CARGO BAY. EVALUATED THE CAPSTRIP & DID NOT FIND ALLOWABLE DAMAGE IAW SRM 53-00-53-1A-2. REPLACED THE CAPSTRIP (STRAP) IAW SRM 51-10-02-0G-0, ITEM 9, & DWG 453A2600, SHEET 92, REV A.Aug 12, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
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