N235WN, cancelled Jun 5, 2026
Service difficulty reports · 280
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 = 'N235WN' AND deregistration_id = 'N235WN-2026-06-05' 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.
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 = 'N235WN' AND deregistration_id = 'N235WN-2026-06-05' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWAA2025120441472Battery · no testAFT RIGHT EMERGENCY LIGHTING BATTERY PACK FAILED A CAPACITY CHECK. REMOVED & REPLACED THE BATTERY IAW MM 33-51-06.SDR SWAA2025070387876Lamp · inoperativeFWD SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED IAW MM 33-51-04.SDR SWAA2025062785436Lamp · inoperativeLEFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] RELAMPED IAW AMM 33-51-03SDR SWAA2025041122644Handle · brokenF/O PILOT ASSIST HANDLE BROKEN<[01] R&R F/O SEAT ASSIST HANDLE PER AMM 20-50-11SDR SWAA2025020492495Cover · out of adjustPLASTIC EXIT ROW COVER FELL OFF AFTER LANDING<[01] RE-INSTALL PLASTIC EXIT ROW I.A.W AMM 11-32-01.SDR SWAA2024080822699Wire Harness · disconnectedRED BOX ON SHUTDOWN IN #2 ENG. EGT REDLINE LIMIT EXCEEDED ON TAKEOFF. DISCONNECTED A/T AND REDUCED THRUST; NO FURTHER INDICATIONS.<[01] T/S PER FIM 71-06 TASK 805 AND ACCOMPLISHED EA M-21-177-01860. FOUND CJ10 HARNESS; S3; AND S4 EGT PROBES FAILING RESISTANCE SDR SWAA2024080823958Probe · failedRED BOX ON SHUTDOWN IN #2 ENG. EGT REDLINE LIMIT EXCEEDED ON TAKEOFF. DISCONNECTED A/T AND REDUCED THRUST; NO FURTHER INDICATIONS.<[01] T/S PER FIM 71-06 TASK 805 AND ACCOMPLISHED EA M-21-177-01860. FOUND CJ10 HARNESS; S3; AND S4 EGT PROBES FAILING RESISTANCE SDR SWAA2024062505471Egt Indication · activatedON T/O #2 ENGINE EGT HAD AN EXCEEDENCE; EGT OF 960 FOR 5 SEC'S EGT GAUGE TURNED RED. PULLED POWER BACK & EGT RETURNED TO LIMITS. PER THE ENGINE EXCEEDENCE PAGE THE #2 ENGINE EXCEEDENCE WAS 958 DEGREES FOR 2 SECONDS & FOUND TO BE IN ZONE A ACCOMPLISHED A VISUALSDR SWAA2024061801469Handle · looseFWD ENTRY DOOR HANDLE RATTLES WHEN DOOR IS CLOSED<[01] RETIGHTEN FWD ENTRY DOOR HANDLE AS REQUIRED REF. AMM 52-11-31.SDR SWAA2024061801470Girt Bar · out of adjustFWD GALLEY SERVICE DOOR; SLIDE GIRT IS NOT PROPERLY PACKED<[01] REPACKED FWD SERVICE DOOR SLIDE GIRT PROPERLY REF. AMM 25-66-00.;[02] REPACKED FWD SERVICE DOOR SLIDE GIRT PROPERLY REF. AMM 25-66-01 AND MT 725-61-06.SDR SWAA2024011639815Light · inoperativeRIGHT HAND EMERGENCY EXIT GROUND ILLUMINATION LIGHT IS INOP<[01] RELAMPED R/H EMERGENCY EXIT GROUND ILLUMINATION LIGHT AND PERFORMED GOOD INSTALLATION TEST PER AMM 33-51-04-960-801;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLESDR SWAA2024011639220Battery Pack · inoperativeEMERGENCY EXIT LIGHTS ASSOCIATED WITH EMERGENCY BATTERY PACK M1669 INOP<[01] REPLACED EMERGENCY EXIT BATTERY PACK M1669 AND PERFORMED GOOD TEST PER AMM 33-51-06-960-806.;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR SWAA2024011639217Battery Pack · inoperativeMULTIPLE EMERGENCY EXIT LIGHTS ASSOCIATED WITH EMERGENCY BATTERY PACK M1674 INOP<[01] REPLACED BATTERY PACK M1674 AND PERFORMED GOOD TEST PER AMM 33-51-06-960-806.;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR SWAA2024011639219Light · inoperativeAFT SERVICE DOOR SLIDE LIGHT IS INOP<[01] RELAMPED AFT SERVICE DOOR SLIDE LIGHT AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-04-960-801.;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.<BR>JOB COMPLETE.SDR SWAA2024011737606Shield · corrodedPERFORM RII BUYBACK OF FWD CARGO AFT SHIELD HAS CORROSION AT BS 500+5 - 500+16; RBL 24; WL 208 [TTG8Q00QAH7R]<[01] UPDATED MEASUREMENTS;[02] PERFORMED RII BUYBACK OF FWD CARGO BAY AFT SHIELD INSTALLATION PER DGW#143A0080 AND SRM 51-40-02. VERIFIED MEASUREMENT SDR SWAA2024011636727Intercostal · corrodedCORROSION ON AFT CARGO BAY WEB AT BS 827-847 STRINGER 27 R/H<[01] REMOVED AND REPLACED ACB INTERCOSTAL FROM BS 827 TO BS 847 RBL 6 WL 156 IAW SRM 51-40-02-0G-0 AND DWG# 146A8130 AND DWG # 146A8131;[02] VERIFIED CORRECTIVE ACTION ITEMS; AND MEASUREMENT FIELDS CSDR SWAA2024011633879Scuff Plate · crackedAFT CARGO BAY FORWARD CORNER SCUFF PLATE IS CRACKED<[01] AFT CARGO BAY FORWARD CORNER SCUFF PLATE REPAIRED PER SRM 53-60-15-2R-1.;[02] CORRECTED MEASUREMENT LINE ITEM 3;[03] VERIFIED CORRECTIVE ACTION #1<BR>VERIFIED MEASUREMENTSSDR SWAA2024011633670Floor Panel · pulledFWD FLOOR PANEL 221CF UPPER SURFACE HAS PULLED STRAND OF FIBERGLASS.<[01] REPAIRED FWD FLOOR PANEL 221CF UPPER SURFACE PULLED STRAND OF FIBERGLASS IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1<BR>VERIFIED MEASUREMENTSSDR SWAA2024011633671Floor Panel · delaminatedFWD FLOOR PANEL 221CF LOWER SURFACE HAS AREAS OF DELAMINATION.<[01] REPAIRED FWD FLOOR PANEL 221CF LOWER SURFACE DELAMINATION IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1<BR>VERIFIED MEASUREMENTSSDR SWAA2024011633672Floor Panel · delaminatedFWD FLOOR PANEL 222AF UPPER SURFACE HAS AREAS OF DELAMINATION.<[01] REPAIRED FWD FLOOR PANEL 222AF UPPER SURFACE DELAMINATION IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1. JOB COMPLETE.SDR SWAA2024011633673Floor Panel · delaminatedFWD FLOOR PANEL 222AF LOWER SURFACE HAS AREAS OF DELAMINATION.<[01] REPAIRED FWD FLOOR PANEL 222AF LOWER SURFACE DELAMINATION IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1. JOB COMPLETE.SDR SWAA2024011633476Frame · crackedSTATION 312 FRAME IS CRACKED IN RADIUS ABOVE L1 DOOR CUT-OUT.<[01] THE UPPER CORD OF THE BS312 FRAME WAS REPAIRED PER REF EA M-22-153-01244;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLESDR SWAA2024011633439Support Angle · crackedLEFT WING; T/E COVE SEAL SUPPORT ANGLE CRACKED ABOVE #1 PYLON AFT TIP<[01] REMOVED AND REPLACED LEFT WING; T/E COVE SEAL SUPPORT ANGLE ABOVE #1 PYLON AFT TIP IAW SRM 51-40-02 AND AIPC 57-50-00-25.;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMESDR SWAA2024011633454Scuff Plate · crackedAFT CARGO DOOR AFT CORNER SCUFF PLATE IS CRACKED<[01] AFT CARGO DOOR AFT CORNER SCUFF PLATE REPAIRED PER SRM 53-60-15-2R-1.;[02] CORRECTED MEASUREMENT LINE ITEM 3;[03] VERIFIED CORRECTIVE ACTION #1<BR>VERIFIED MEASUREMENTSSDR SWAA2024011632520Floor Panel · pulledFLOOR PANEL 231FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231FF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] PANEL REPLACED. JOB COMPLETESDR SWAA2024011632521Floor Panel · pulledFLOOR PANEL 231MF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231MF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] PANEL REPLACED. JOB COMPLETESDR SWAA2024011632522Floor Panel · pulledFLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241UF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] PANEL REPLACED. JOB COMPLETESDR SWAA2024011632518Bracket · crackedPULLEY SUPPORT BEAM CRACKED ON L-BRACKET AT BS 697; LBL 0.5; WL 207. (MARKED)<[01] STEP 2 COMPLETE OK TO APPLY CONVERSION COAT AND PRIME;[02] STEP 3 COMPLETE;[03] REMOVED AND REPLACED L-BRACKET AT BS 697; LBL 0.5; WL 207 PER REF SRM 51-40-02 AND DWG NBR 273A91SDR SWAA2024011632253Flange · corrodedCORROSION ON FWD R/H MOP SILL VERTICAL FLANGE FROM STA 294 TO STA 330; RBL 54 TO RBL 59; WL 208.9.<[01] REMOVED AND REPLACED ON FWD R/H MOPSILL BS 260 TO BS 360 RBL 59 IAW SRM 51-40-02 AND DWG 141A8310;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASSDR SWAA2024011632251Floor Support · crackedCRACKED INTERCOSTAL AT STA 277+10; BL 0; WL 208.1.<[01] REMOVED AND REPLACED NEW INTERCOSTAL ITEM 141A5410-3 IAW SRM 51-40-02 AND DWG 141A5400;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2024011632393Scuff Plate · crackedFCB AFT CORNER SCUFF PLATE IS CRACKED<[01] APPLIED A CHEMICAL CONVERSION COATING TO THE BARE ALUMINUM SURFACES PER SOPM 20-43-03; TYPE 2; CLASS A OR C AND SRM 53-30-15-2R-1 AND APPLY TWO LAYERS OF BMS 10-11;TYPE 1 PRIMER TO THE INNER SURFACES OF THE CORNER SCUSDR SWAA2024011631806Floor Panel · pulledFWD FLOOR PANEL 221AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221AF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] PANEL REPLACED. JOB SDR SWAA2024011631807Floor Panel · pulledFWD FLOOR PANEL 221BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] PANEL REPLACED. JOB SDR SWAA2024011631815Floor Panel · pulledFWD FLOOR PANEL 221GF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221GF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE SDR SWAA2024011631812Floor Panel · pulledFWD FLOOR PANEL 222CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AREAS OF PULLED STRANDS ON UPPER SKIN OF FWD FLOOR PANEL 222CF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.SDR SWAA2024011631816Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 241DF HAS PULLED STRANDS.<[01] DUE TO EXTENT OF THE DAMAGE ON PASSENGER CABIN FLOOR PANEL 241DF FABRICATED NEW PANEL FROM BMS4-17 TYPE 6 LOT#1544951-1; LOCATED AND INSTALLED INSERTS USING BMS5-107 LOT#AK3BA2380A/A; CURED USING HEAT SDR SWAA2024011631820Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 241FF HAS PULLED STRANDS.<[01] VERIFIED STEP 1;2 AND THE MEASUREMENT TABLE.;[02] PASSENGER CABIN FLOOR PANEL 241FF WITH PULLED STRANDS WAS BEYOND ECONOMICAL REPAIR. PANEL WAS REPLACED BY FABRICATING A NEW ONE IAW SRM 53-00-50-2R-0 ASDR SWAA2024011631818Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 242CF HAS PULLED INSERT.<[01] VERIFIED STEP 1;2 AND THE MEASUREMENT TABLE.;[02] PASSENGER CABIN FLOOR PANEL 242CF WITH A PULLED INSERT WAS BEYOND ECONOMICAL REPAIR. PANEL WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0SDR SWAA2024011631821Floor Panel · pulledAFT FLOOR PANEL 241AAF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241AAF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS BEYOND ECONOMICAL REPAIR. A NEW PANEL WAS FABRICATED IAW SRM 53-00-50-2R-0 AND BOEING DWG 147A5810 ID: 0008.;[02] VERIFIED COSDR SWAA2024011631823Floor Panel · pulledAFT FLOOR PANEL 241ADF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ADF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.;[02] VERIFIED FLOOR PANEL 241ADF WAS REPAIRED PER SRM 53-00-50-2R-1.;[03] WORKSCOPE COMPLETE.SDR SWAA2024011631824Floor Panel · pulledAFT FLOOR PANEL 242TF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242TF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.;[02] VERIFIED FLOOR PANEL 242TF REPAIRED PER SRM 53-00-50-2R-1.;[03] WORKSCOPE COMPLETE.SDR SWAA2024011631827Floor Panel · pulledAFT FLOOR PANEL 242UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242UF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.;[02] VERIFIED FLOOR PANEL 242UF WAS REPAIRED PER SRM 53-00-50-2R-1.;[03] WORKSCOPE COMPLETESDR SWAA2024011631828Floor Panel · pulledAFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242VF UPPER SKIN; AREAS OF PULLED STRANDS; WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED FLOOR PANEL 242VF WAS REPAIRED IAW SRM 53-00-50-2R-1.SDR SWAA2024011632239Frame · corrodedAFT CABIN WET AREA FRAME HAS CORROSION AT FASTENER HOLE; BS 986; LBL 44; WL 208<[01] REMOVED AND REPLACED REPAIR PARTS PER SEM 51-40-02 AS SHOW IN SWA EA#1-753-32297 REV IR (ESR#23-02724);[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.SDR SWAA2024011632244Web · corrodedFWD CARGO DOOR CENTER THRESHOLD HAS CORROSION AT BS 440+10 - 480+4; RBL 28; WL 208<[01] REMOVED AND REPLACED THRESHOLD WEB AT FCB BS 440- 492.4; RBL 28; WL 156.IAW SRM 51-40-02.;[02] VERIFIED MEASUREMENTS FIELDSDR SWAA2024011632245Shield · corrodedFWD CARGO AFT SHIELD HAS CORROSION AT BS 500+5 - 500+16; RBL 24; WL 208<[01] REMOVED AND REPLACED AFT SHIELD;IAW DWG#143A0080 AND SRM 51-40-02.;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.SDR SWAA2024011632246Sidewall Support · corrodedAFT CARGO FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 767-727E; RBL 22; WL 156<[01] REMOVED AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02 AN DWG 146A7500.;[02] VERIFIED MEASUERMENT TABLE.;[03] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2024011632243Sidewall Support · corrodedAFT CARGO FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 727D - 744; LBL 22; WL 156<[01] CORRECTION TOM MEASUREMENT #1;[02] REMOVED AND REPLACED LH SIDEWALL SUPPORT FROM BS727 TO BS847;LBL22 WL156;IAW DGW#146A7500 REV A AND SRM 51-40-02.;[03] VERIFIED CORRECTIVSDR SWAA2024011632247Sidewall Support · corrodedAFT CARGO FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 747+9 - 787; LBL 22; WL 157<[01] THIS TASK CARD WILL BE COMPLETED WITH CARD #TTG8Q00QAFFY.;[02] VERIFIED ITEM 1 COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.SDR SWAA2024011632003Frame · corrodedFWD CABIN WET AREA FRAME HAS CORROSION AT FASTENER HOLES; BS 294.5; RBL 7; WL 208 CLARIFICATION THIS IS THE BS 294 FLOOR BEAM=FWD CABIN WET AREA FRAME HAS CORROSION AT FASTENER HOLES; BS 294.5; RBL 7; WL 208<[01] TASK CARD IS COMPLETE;[02] FWD CABIN WET AREA F
Back to N235WN, cancelled Jun 5, 2026