N925WN

Service difficulty reports · 252

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 = 'N925WN' 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 SWAA2026061596478Skin · crackedCRACK OF 0.25' APPROX ON FORWARD ENTRY DOOR INTERNAL SKIN, MIDDLE, AT BS 344 AND WL 237. REPAIRED IAW EA 26-152-01267 WITH INSPECTION THRESHOLD TRACKED IN EA 26-152-01267-DTI.May 7, 2026 · N925WN · Boeing 7377H4 · Passenger/Crew DoorsSDR SWAA2026061596314Support Plate · corrodedCORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES, BS 727B - 767, LBL 22, WL 156. REMOVED AND REPLACED THE AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT, BS 727 - 847, LBL 22, WL 156, IAW SRM 51-40-05-0G-0, SRM 51-May 7, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061596316Cargo Track · crackedAFT CARGO BAY CARGO TRACK IS CRACKED BS 767 - 747, RBL 13, WL 156. REPAIRED IAW EA 26-153-01273.May 7, 2026 · N925WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026061596315Sidewall Support · corrodedCORROSION AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT PLATE HAD MULTIPLE AREAS AROUND NUT PLATE HOLES, BS 727B - 767, RBL 22, WL 156. EVALUATED, REMOVED, LOCATED, DRILLED, AND INSTALLED A NEW FLOOR TO SIDEWALL SUPPORT BS 727 - 767, RBL 22, WL 156, IAW SRM 51May 7, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061596317Sidewall Support · corrodedCORROSION FWD CARGO BAY LT FLOOR TO SIDEWALL SUPPORT PLATE AT MULTIPLE AREAS AROUND NUT PLATE HOLES, BS 460 - 500B, LBL 22, WL 156. CORROSION ON FWD CARGO BAY LT FLOOR TO SIDEWALL SUPPORT PLATE, BS 396 - 500D, LBL 22, WL 156, FOUND TO BE OUT OF LIMITS. REMay 7, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061596457Splice Strap · corrodedCORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE, BS 727D+6, RBL 11.5, WL 156. CORROSION ON STRAP WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. RECEIVED A NEW CARGO BAY FLOOR SPLICE STRAP. THE NEW STRAP TO BE INSTALLEMay 7, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061596459Splice Strap · corrodedCORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE, BS 767+6, RBL 11.5, WL 156. CORROSION ON STRAP WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. RECEIVED NEW CARGO BAY FLOOR SPLICE STRAP, THE NEW STRAP TO BE INSTALLED ONMay 7, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061596479Floor Panel · debondedFLOOR PANEL 231ZF UPPER SKIN HAS A LARGE DEBONDED AREA NEAR AFT EDGE. FABRICATED A NEW 231ZF FLOOR PANEL ACCOMPLISHED IAW SRM 53-00-50-2R-0.May 7, 2026 · N925WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026061596480Floor Panel · debondedFLOOR PANEL 232SF UPPER SKIN HAS LARGE DEBONDED AREA NEAR AFT EDGE. FABRICATED A NEW 232SF FLOOR PANEL ACCOMPLISHED IAW SRM 53-00-50-2R-0.May 7, 2026 · N925WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026061596481Floor Panel · pulledFLOOR PANEL 241CF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPLACEMENT FLOOR PANEL 241CF WAS FABRICATED IAW SRM 53-00-50-2R-0.May 7, 2026 · N925WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026061596470Fastener · looseAFT ENTRY DOOR SLIDE COVER AFT GIRT BAR RETAINER FASTENERS ARE LOOSE. REMOVED AND REPLACED FASTENERS ON AFT ENTRY DOOR SLIDE COVER AFT GIRT BAR IAW SRM 51-40-02-0G-0 .May 7, 2026 · N925WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2026061596483Scuff Plate · crackedFWD SERVICE DOOR SCUFF PLATE CRACKED AT AFT EDGE. REMOVED THE COATINGS AND OTHER UNWANTED MATERIALS FROM THE SCUFF PLATE BEFORE WELDING IAW SRM 53-10-15-2R-2 STEP 4.B.(3). REFERRED TO SOPM 20-30-03, WELDED THE DAMAGED AREA ON SCUFF PLATE IAW SRM 53-10-15-2R-May 7, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061596087Former · crackedWING TO BODY FAIRING FORMER IS CRACKED BS 500D BETWEEN STRINGER 19 AND 20 L/H. REMOVED DAMAGED FAIRING FORMER AND INSTALLED NEW WING TO BODY FAIRING FORMER AT BS 500D BETWEEN STRINGER 19 AND 20 R/L PER SRM 51-40-02-0G-0; AND DWG 116A3010 REV: -.May 7, 2026 · N925WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2026061596085Scuff Plate · crackedAFT CARGO BAY AFT CORNER THRESHOLD IS CRACKED. AFT CARGO BAY CRACKED AFT CORNER SCUFF PLATE REPAIRED IAW SRM 53-60-15-2R-1.May 6, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061595776Skin · delaminatedLEFT INBD MAIN FLAP OTBD T/E DELAMINATED. REMOVED AND INSTALLED A NEW LT INBD MAIN FLAP OTBD T/E IPC 27-51-11-01B, ITEM 175 IAW AMM 20-50-11-910-801.May 6, 2026 · N925WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2026061595777Skin · delaminatedRT INBD MAIN FLAP OTBD T/E DELAMINATED. REMOVED AND REPLACED NEW RT INBD MAIN FLAP OTBD T/E IAW AMM 20-50-11-910-801, DWG 113A2100 REV A, AND DWG 113A2100 REV B.May 6, 2026 · N925WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2026022674378Seal · crackedLEFT STABILIZER TO BODY UPPER FRONT SPAR SLIDING SEAL CRACKED. REMOVED AND REPLACED THE LT STABILIZER UPPER SLIDING SEAL IAW AMM 53-31-31.Feb 26, 2026 · N925WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2026022674384Seal · crackedRIGHT STABILIZER-TO-BODY UPPER FRONT SPAR SLIDING SEAL CRACKED. R & R RT HORIZONTAL STAB FWD UPPER SLIDING SEAL IAW AMM 53-31-31.Feb 26, 2026 · N925WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2025121651835Girt Bar · bentFORWARD SERVICE DOOR. GIRT BAR BRACKET BENT. COMPLIED WITH EA M-23-125-01839. SECURED GIRT BAR CLIP.Dec 12, 2025 · N925WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2025121651802Fastener · missingFWD SERVICE DOOR SLIDE FWD GIRT BAR RETAINING CLIP IS MISSING A RIVET. INSTALLED ONE NEW FASTENER IN FWD SERVICE DOOR SLIDE FWD GIRT BAR RETAINING CLIP IAW IPC 25-66-00-01 & SRM 51-40-02.Dec 12, 2025 · N925WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2025120442316Smoke Detector · false activationFORWARD LAVATORY SMOKE DETECTOR WENT OFF AT 4000 FT ON APPROACH. PULLED THE CIRCUIT BREAKER TO SILENCE ALARM. R & R FWD LAVATORY SMOKE DETECTOR IAW 26-14-01. OPS CHECKED OK.Dec 3, 2025 · N925WN · Boeing 7377H4 · Smoke DetectionSDR SWAA2025110731533Fastener · missingWORKING M-23-125-01839-TLD, R1 DOOR GIRT BAR RETAINER CLIP MISSING FASTENERS. INSTALLED FASTENER ON R1 GIRT BAR RETAINER CLIP IAW SRM 51-40-02.Nov 4, 2025 · N925WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2025110531048Retainer · brokenR1 DOOR GIRT BAR RETENTION STOWAGE ANGLE FASTENER BROKE. C/W EA M-23-125-01839.Nov 2, 2025 · N925WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2025071791871Washer · looseDURING NOSE GEAR LUBRICATION ; EXCESSIVE PLAY FOUND ON NOSE LANDING GEAR RETRACT ACTUATOR AT UPPER & LOWER ATTACH POINTS. INSTALLED REQUIRED WASHERS IAW AMM 32-33-11. INSPECTED PER AMM 32-33-11-401-NG (NOSE GEAR RETRACT ACTUATOR - REMOVAL/INSTALLATION - PERJul 15, 2025 · N925WN · Boeing 7377H4 · Landing Gear ActuatorSDR SWAA2025062383699Floor Panel · crackedFWD CARGO FLOOR CRACK DAMAGE <[01]. REMOVED AND INSTALLED NEW FWD CARGO FLOOR PANEL IAW 25?52-10.Jun 20, 2025 · N925WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025060978989Girt Bar · out of adjustGIRT BAR SHIFTED IN SLIDE SLEEVE DURING OPENING FWD SERVICE DOOR.<[01] REPOSITIONED GIRT BAR IN SLIDE AT FWD SERVICE DOOR POSITION PER AMM25-66-01. INSPECTED FWD SERVICE DOOR ESCAPE SLIDE PER AMM25-66-01. OKAY FOR CONTINUED SERVICE.Jun 5, 2025 · N925WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2025042124208Light · detachedCENTER ISLE (CEILING) EMERGENCY EXIT LIGHT HANGING BY WIRES LOOSE. RESECURED LIGHT ASSY IAW B737 AMM 20-50-11-201-NG;[02] RESECURED LIGHT ASSY IAW B737 AMM 20-50-11-201-NGApr 13, 2025 · N925WN · Boeing 7377H4 · Emergency LightingSDR SWAA2024121675733Cover · brokenFO SIDE OVERWING EXIT ILLUMINATED SIGN COVER BROKEN AND FELL OFF PASSENGER BROKE IT OFF BY ACCIDENT<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-01-201-NG (EXIT SIGNS - MAINTENANCE PRACTICES - PERMANENT)]Dec 10, 2024 · N925WN · Boeing 7377H4 · Emergency LightingSDR SWAA2024112772218Lamp · inoperativeL/H EMERGENCY EXTERIOR ESCAPE HATCH LIGHT INOP SLIDE/OVERWING LIGHT<[01] 01 - REMOVED AND REPLACED PER L/H [AMM 33-51-04-960-801-NG (SLIDE/OVERWING LIGHT - LAMP REPLACEMENT - PERMANENT)]Nov 27, 2024 · N925WN · Boeing 7377H4 · Emergency LightingSDR SWAA2024061902864Lamp · inoperativeEMERGENCY EXIT EXTERIOR LIGHT OUT AT L2 DOOR<[01] RELAMPED L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT IAW AMM 33-51-04.Jun 18, 2024 · N925WN · Boeing 7377H4 · Emergency LightingSDR SWAA2024061398851Lamp · inoperativeMULTIPLE PAX EMERGENCY LIGHTS INOP. REPLACED OVERHEAD STORAGE BIN EMERGENCY LIGHT AT POS 13DEF R/H SIDE AS PER AMM 33-51-03-960-801. EMERGENCY LIGHTS TESTED NORMAL. INSP./ COMPLETED OF FAULT REPORTED AS 'MULTIPLE PAX EMERGENCY LIGHTS INOP. ' AND ONLY FOUND ONJun 6, 2024 · N925WN · Boeing 7377H4 · Emergency LightingSDR SWAA2024061391070Panel · crackedFOUND PANEL BRAKE CRACKED AT STA 537.45 BL 0 TO RBL 24.75 FOUND PANEL BREAK CRACKED AT MAIN CABIN STA 537.45 BL0 TO RBL 24.75<[01] REMOVED AND REPLACEDPANEL BRAKE AT STA 537 BL0 TO RBL24.75 PER SRM 51-40-02 AND DWG 143A5240;[02] CORRECTION: REMOVED AND REPLACEMay 29, 2024 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024061489549Attach Angle · crackedRIGHT VAPOR BARRIER UPPER ATTACH ANGLE CRACKED AT STA 663.75 AND RBL 9<[01] PERFORMED SME AUDIT OF ITEM AND INSPECTION OF WORKMANSHIP.;[02] CUT AND REMOVED CENTER WING REAR SPAR VAPOR BARRIER ATTACH ANGLE AT STA 663 RBL 20 TO RBL 6 PER SRM 57-10-10-2R-5; FABRIMay 24, 2024 · N925WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2024061489074Attach Angle · crackedRIGHT VAPOR BARRIER UPPER ATTACH ANGLE CRACKED AT STA 663.75 AND RBL 9<[01] THIS IS A DUPLICATE ITEM; WORK WILL BE ACCOMPLISHED ON TTG8Q00TJKQR;[02] VERIFIED STEP 1May 23, 2024 · N925WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2024061488336Skin · misrepairedREJECT...REPAIR ON TTG8Q00TAVDK INCORRECT REPAIR PARTS THICKNESS USED; RE-ACCOMPLISH REPAIR<[01] REMOVED PREVIOUS DOUBLER REPAIR 0.090' AND FILLER 0.071' AT LEFT HORIZONTAL STAB. LOWER SKIN STA. 193.90 PER REF SRM 51-40-02-0G-0.<BR>LOCATED AND DRILLED AND COUNMay 20, 2024 · N925WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2024061486697Floor Support · crackedFWD CABIN FLOOR SUPPORT INTERCOSTAL AT 294.5 TO 285 AT CENTERLINE IS CRACKED<[01] REMOVED AND REPLACED INTERRCOSTAL AT FWD CABIN FLOOR SUPPORT STA. 294.5 TO STA. 285.REF. SRM. 51-40-02-0G-0;[02] VERIFIED CORRECTIVE ACTION.May 16, 2024 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024061485701Channel · corrodedFORWARD CARGO COMPARTMENT FLOOR STRUCTURE RIGHT SIDE ''Z CHANNEL'' AROUND HOLES GAS EVIDENCE CORROSION BETWEEN STA 500 TO STA 500A ; WL 155.5; RBL-21.<[01] REMOVED AND REPLACED FWD CARGO Z CHANNEL (SHIELD) RT SIDE BETWEEN STA 500 AND STA 500A; REF SRM 51-40-02May 15, 2024 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024061485699Channel · corrodedFORWARD CARGO COMPARTMENT FLOOR STRUCTURE RIGHT SIDE ''Z CHANNEL'' AROUND HOLES GAS EVIDENCE CORROSION BETWEEN STA 500A TO STA 500B ; WL 155.5; RBL-21.<[01] FWD CARGO COMP FLOOR STRUCTURE RIGHT SIDE ' Z CHANNEL' FROM STA 500A TO STA 500D RBL 21 WL 155.1 WILL BMay 15, 2024 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024061485702Channel · corrodedFORWARD CARGO COMPARTMENT FLOOR STRUCTURE RIGHT SIDE ''Z CHANNEL'' AROUND HOLES GAS EVIDENCE CORROSION BETWEEN STA 500B TO STA 500C ; WL 155.5; RBL-21.<[01] REMOVED AND REPLACED FWD CARGO Z CHANNEL AT RT SIDE STA 500B TO 500C PER SRM 51-40-02-0G-0;[02] VERIFIEMay 15, 2024 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024061485947Shield · corrodedAFT CARGO COMPARTMENT SIDEPLATE SUPPORT ZEE HAS SURFACE CORROSION LOCATED AT S25R; RBL 20.0; IN BETWEEN STA 767 AND STA 787. AFT CARGO COMPARTMENT SIDEPLATE SUPPORT ZEE HAS SURFACE CORROSION LOCATED AT S25R RBL 21.0 IN BETWEEN STA 767 AND STA 787.<[01] REMOVEDMay 15, 2024 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024061385958Floor Panel · peelingCABIN FWD WET AREA FLOOR PANEL 222DF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-030<[01] RECEIVED NEW FLOOR PANEL 222DF; IT WILL BE INSTALLED ON TTG8Q00SCGXZ.;[02] VERIFIED STEP 1.May 15, 2024 · N925WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061385959Floor Panel · peelingCABIN FWD WET AREA FLOOR PANEL 222CF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-031<[01] FAULT WAS RAISED IN ERROR.May 15, 2024 · N925WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061385960Floor Panel · peelingCABIN FWD WET AREA FLOOR PANEL 221EF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-031<[01] RECEIVED NEW FLOOR PANEL 221EF; IT WILL BE INSTALLED ON TTG8Q00SCGY8.;[02] VERIFIED STEP 1.May 15, 2024 · N925WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061386167Floor Panel · peelingCABIN FWD WET AREA FLOOR PANEL 221DF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-033<[01] RECEIVED NEW FLOOR PANEL # 221DF; P/N:141A5810-235. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00SCGYA;[02] VERIFIED ON TASK CARD: TTG8Q00SCGYAMay 15, 2024 · N925WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061386175Floor Panel · peelingCABIN FWD WET AREA FLOOR PANEL 221AF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-036<[01] RECEIVED NEW FLOOR PANEL 221AF; IT WILL BE INSTALLED ON TTG8Q00SCGYG;[02] VERIFIED STEP1.May 15, 2024 · N925WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061386177Floor Panel · peelingCABIN FWD WET AREA FLOOR PANEL 221CF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-038<[01] RECEIVED REPAIRED FLOOR PANEL 221CF. <BR>P/N: 141A5810-9.<BR>PO: 2059779.<BR>PANEL WILL BE INSTALLED ON TTG8Q00SCGYC.;[02] VERIFIED STEP 1May 15, 2024 · N925WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061386173Floor Panel · peelingCABIN FWD WET AREA FLOOR PANEL 222AF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-040<[01] RECEIVED NEW FLOOR PANEL # 222AF; P/N:141A5810-769. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00SCGXL;[02] VERIFIED ON TASK CARD: TTG8Q00SCGXLMay 15, 2024 · N925WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061386180Floor Panel · peelingCABIN FWD WET AREA FLOOR PANEL 222BF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-042<[01] RECEIVED NEW FLOOR PANEL # 222BF; P/N:141A5810-464. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00SCGXJ;[02] VERIFIED ON TASK CARD: TTG8Q00SCGXJMay 15, 2024 · N925WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061386182Floor Panel · peelingFWD CABIN FLOOR PANEL 232AF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-044<[01] RECEIVED FWD CABIN FLOOR PANEL 232AF WILL BE INSTALL ON ITEM TTG8Q00SCGXR;[02] VERIFIED STEP 1May 15, 2024 · N925WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061386183Floor Panel · peelingFWD CABIN FLOOR PANEL 231AF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-045<[01] RECEIVED NEW FLOOR PANEL 231AF; IT WILL BE INSTALLED ON TTG8Q00SCGXX.;[02] VERIFIED STEP 1.May 15, 2024 · N925WN · Boeing 7377H4 · Fuselage Floor Panel
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