N409WN, cancelled Jun 5, 2026
Service difficulty reports · 284
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 = 'N409WN' AND deregistration_id = 'N409WN-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 = 'N409WN' AND deregistration_id = 'N409WN-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 SWAA2025063085224Floor Panel · splitFWD CARGO FLOOR PANEL SPLIT 4'' NEAR FWD EDGE. <[01] REMOVED AND REPLACED FWD CARGO FLOOR PANEL IAW B737 AMM 25-52-10.SDR SWAA2025060276751Slide · looseL 1 DOOR ESCAPE SLIDE FELL OUT OF SLIDE COMPARTMENT <[01]. INSTALLED FWD ENTRY ESCAPE SLIDE PER AMM 25-66-01 AND MT 725-61-06.SDR SWAA2024100141150Skin · cracked3/4' LONG CRACK FOUND ON RIB ;10' I/B & 2' FROM AFT SIDE OF PANEL 553BB<[01] REMOVED AND REPLACED L/H I/B TRAILING EDGE FLAP PER AMM 27-51-11 AND L/H I/B AFT FLAP PER AMM 27-51-12.SDR SWAA2024093040645Panel · crackedLH WING LOWER FIXED INBOARD TRAILING EDGE PANEL 551FB CRACK DAMAGE<[01] REMOVED PANEL 551FB PER SRM 51-40-02.;[02] LOCATED HOLES IN 551FB PER SRM 51-40-05.;[03] HOLES LOCATED IN NEW PANEL PER SRM 51-40-05;[04] INSTALLED 551FB PANEL PER M/M 57-15-00-400-801SDR SWAA2024092339358Tire · failedBLOWN TIRE ON TAKEOFF ROLL<[01] R/R #1 AND #2 MAIN GEAR WHEEL WHEEL ASSY PER M/M 32-45-11.SDR SWAA2024050983445Light · inoperativeL2 DOOR SLIDE EXTERIOR EMERGENCY LIGHT INOP<[01] R&R L2 DOOR SLIDE EXTERIOR EMERGENCY LIGHT PER AMM 33-51-04. OPS CHECK GOOD.SDR SWAA2024032567326Light · looseEMERGENCY EXIT SIGN IS LOOSE. OVERHEAD MID CABIN.<[01] REINSTALLED LIGHT PER SIPSDR SWAA2023102714313Slide · looseR1 DOOR SLIDE LOOKS LOOSE<[01] VERIFIED R1 DOOR SLIDE SECURITY PER AMM 25-66-01; NO DEFECTS NOTED.SDR SWAA2023101911680Light · inoperativeBOTH OVER WING EXIT SIDEWALL LIGHTS INOP<[01] RELAMPED L/H AND R/H OVERWING EXIT SIDEWALL EMERGENCY LIGHTS AND PERFORMED GOOD OPERATIONAL TEST PER AMM 33-51-01-960-801;[02] VERIFIED CORRECTIVE ACTION COMPLETESDR SWAA2023102011226Panel · out of positionRIGHT HORIZONTAL STAB PANEL 343AB SLIDE SEAL IS NOT PROPERLY IN SLIDE SEAL TRRACKS<[01] REMOVED AND PROPERLY REINSTALLED PANEL 343AB PER AMM 20-50-11-910-801<BR>CAL TOOL: ATS1731 DUE: 07/2024;[02] INSPECTED AND VERIFIED INSTALLATION. JOB COMPLETE.SDR SWAA2023101910226Light · inoperativeFOUND SEAT ROW 9 AND 11 ABC LEFT HAND EMERGENCY BIN LIGHTS INOP<[01] COMPLETED WORK STEP 1.;[02] CERTIFIED ACTION 2 STEP 2;[03] REPLACED LAMPS ON SEAT ROW 9 AND 11 ABC LEFT HAND EMERGENCY BIN LIGHTS AND CHECKED VOLTAGE ON BOTHS LIGHTS; STILL FAIL PER AMM 33-51SDR SWAA2023102007559Doubler · crackedEXTERNAL POWER DOOR CUTOUT DOUBLER HAS CRACKED FILLER (MIDDLE)<[01] REMOVED AND REPLACED DOUBLER AT EXTERNAL POWER DOOR CUTOUT BS 235; BETWEEN STR 22R AND STR 23R IAW SRM 53-10-15-2R-4 FIG 203.;[02] ACCOMPLISHED PERMANENT REPAIR AT EXTERNAL POWER DOOR CUTOUT BSDR SWAA2023101907153Frame · crackedCRACKED FRAME AT PASSENGER CABIN S-8L BS727D.<[01] UPDATED STEPS;[02] STEP 6 UPDATE;[03] CRACK NOTED WITHIN INSPECTION AREA. THIS CARD WILL BE ATTENDANT ON EA 1-A53-12114 CUST ID: TTG8Q00NTLYQSDR SWAA2023102306013Crease Beam · corrodedWING CENTER SECTION - CORROSION ON INNER CHORD BS 694+7 LBL 62.25 WL 208 (MARKED)<[01] REMOVED CORROSION ON INNER CHORD BS 694+7 LBL 62.25 WL 208 IN THE AREA OF 1'X1'X0.013'. FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13-1A-1;[02] REMOVED CORROSION ON INNER CHORDSDR SWAA2023102005996Seat Track · corrodedCORROSION AT PASSENGER CABIN SEAT-TRACK RBL-45 STA-500+6''<[01] VERIFIED STEP 2;[02] UPDATED STEP 1;[03] VERIFIED CORRECTIVE ACTION COMPLETESDR SWAA2023102005998Seat Track · corrodedCORROSION AT PASSENGER CABIN SEAT-TRACK RBL-45 STA-727B+5'' TO 727B+15''; STA-727D+10''; STA-807; STA-827; STA-846+12''; STA-867+5''<[01] VERIFIED STEPS 2;4;5;6;7;8;9;[02] UPDATED STEP 1;[03] VERIFIED CORRECTIVE ACTION COMPLETESDR SWAA2023102006016Channel · corrodedWING CENTER SECTION - CORROSION ON INNER CHORD BS 705 LBL 62.25 WL 208 (MARKED)<[01] REMOVED CORROSION ON INNER CHORD BS 705 LBL 62.25 WL 208 IN THE AREA OF 1'X1'X0.012'. FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13-1A-1;[02] REMOVED CORROSION ON INNER CHORD BS SDR SWAA2023102006012Support · crackedRIGHT WING T/E AFT PANEL SUPPORT FOR PANEL 661AB IS CRACKED AT I/B ENG<[01] NO ALLOWABLE DAMAGE LIMIT NOTED ON SRM; PART REPAIR BY REPLACEMENT OF PART PER SRM 51-10-02-0G-0 PARA 9.<BR><BR>REMOVED AND REPLACED RIGHT WING T/E AFT PANEL SUPPORT ASSY FOR PANEL 661SDR SWAA2023102005991Web · corrodedFWD CARGO DOOR CUTOUT SURROUND AREA STRUCTURE; SOME CORROSION SPOTS BETWEEN STA 460 AND STA 480; RBL24 (THRESHOLD).<[01] UPDATED STEP 1 AND 2.;[02] UPDATED STEP 4;[03] CUSTOMER CARD COMPLETE AND VERIFIED MEASUREMENT TABLE.SDR SWAA2023101905617Flap · delaminatedRIGHT WING O/B AFT FLAP LOWER SURFACE AT I/B CORNER. DELAM APPROX 4'X5'<[01] R/W O/B AFT REPLACED ON FAULT #TTG8Q00NQHUR;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLESDR SWAA2023102005604Scuff Plate · crackedAFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED<[01] FAULT RESOLVED ON OTHER FAULT (FAULT WAS RESOLVED ON ANOTHER FAULT #TTG8Q00NQ15L;[02] VERIFIED CORRECTION ACTION ITEM 1; (FAULT WAS RESOLVED ON ANOTHER FAULT #TTG8Q00NQ15L.) THIS CARD COMPLETE.SDR SWAA2023101905296Pressure Deck · crackedCRACK FOUND ON HORIZONTAL PRESSURE DECK WEB STA 663 TO STA 675 LBL 30 TO LBL 45. MARKED LOCATION.<[01] HFEC INSPECTED CUT OUT EDGES IAW 737 NDTM PART 6; 51-00-00 PROCEDURE 23.<BR>NO CRACKS NOTED.<BR>EQUIP USED:<BR>-NORTEC 500D ID: IS000680 CAL DUE: 05/2024;[02SDR SWAA2023101905297Pressure Deck · crackedCRACK FOUND ON HORIZONTAL PRESSURE DECK WEB STA 663 TO STA 675 RBL 39 TO RBL 60. MARKED LOCATION.<[01] UPDATED MEASUREMENT TABLE;[02] STEP 11 PARTIAL UPDATE;[03] CRACK REPAIRED ON HORIZONTAL PRESSURE DECK WEB FROM BS663 - BS674; RBL31 - RBL63; WL202 WITH 1EA -SDR SWAA2023101905603Scuff Plate · crackedAFT CARGO BAY AFT CORNER SCUFF PLATE CRACKED<[01] WELDED CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 PARAGRAPH 4.B. (4) AND BAC 5975<BR>EQUIPMENT USED; WELDING MACHINE E10583 CALIBRATION DUE DATE 01/2024<BR><BR>SANDED THSDR SWAA2023102005073Doubler · crackedL/H WING LOWER SURFACE OF L/E SLAT NOSE SKIN AT ACTUATOR #2 HAS A SUSPECTED CRACK AT FASTENER (MARKED)<[01] UPDATED STEPS 2-4.;[02] REQ. HFEC FOR ALL INITIAL FASTENER HOLES IN THE NOSE SKIN AND THE UNDERLYING STRUCTURE FOR DAMAGE.;[03] VERIFIED STEP 7 IN PARTISDR SWAA2023062872042Slide · out of adjustOPS REPORTED SLIDE CAME OFF L1 DOOR.<[01] REPOSITIONED FWD L1 DOOR SLIDE PER AMM 25-66-01. C/W MT 725-61-06. A/C OK FOR SERVICE.SDR SWAA2023052552205Cover · looseCABIN EMERGENCY EXIT LIGHT COVER IS LOOSE AT 6ABC.<[01] SECURED CABIN EMERGENCY EXIT LIGHT COVER AT 6ABC PER AMM 33-51-03SDR SWAA2023021402208Slide · out of adjustAFT SERVICE DOOR SLIDE APPEARS TO BE COMING OUT<[01] RESECURRED SLIDE PER 25-66-00 CKS GOODSDR SWAA2023012794748Scuff Plate · crackedFWD CARGO DOOR LOWER MIDDLE THRESHOLD HAS CRACK MEASURING L=.25 LOCATED 14.5 AFT OF FWD EDGE<[01] REMOVED FWD CARGO DOOR LOWER SILL SCUFF PLATE AND BULLNOSE REF 737 AMM 53-11-02;[02] REPLACED 2EA NUT PLATES ON FWD CARGO DOOR LOWER SILL REF 737 SRM 51-40-02;[03SDR SWAA2023012694753Battery Pack · failedEMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY TEST AT LOCATIONS M1675; M1674; M1669; M1672; M1673; M1668. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS PER AMM 22-51-06.SDR SWAA2022112374008Floor Panel · delaminated193B PANEL HAS 15 HOLES WITH CRACKING OR DELAMINATION / [01] REMOVED AND REPLACED 193B PANEL I.A.W AMM 53-51-21.SDR SWAA2022111570452Retainer · dirtyFLIGHT ATTENDANT REPORTS FWD ENTRY DOOR GIRT BAR DIFFICULT TO MANIPULATE / [01] ADJUSTED GIRT BAR ON FWD ENTRY DOOR AND CLEANED RETAINING CLIPS. OPS CK?D GOOD PER M/M 25-66-01SDR SWAA2022101158146Megaphone · inoperativeAFT F/A MEGAPHONE INOP / [01] R&R AFT F/A MEGAPHONE REF AMM 25-64-00SDR SWAA2022061618464Slide · out of positionFORWARD SLIDE CAUGHT BETWEEN L1 DOOR & SLIDE COMPARTMENT / [01] REMOVED & REINSTALLED L1 DOOR SLIDE COMPARTMENT PER REF SIP. SLIDE COMPARTMENT REMAINED SEALED/SECURED. DID NOT OPEN SLIDE COMPARTMENT.SDR SWAA2021122050772Connector · disconnectedEXTERNAL EMERGENCY LIGHT OVERWING SCAPE R/H INOP. AMM 33-51-04-960-801 REPLACED BULB RIGHT OVERWING EMERGENCY LIGHT, NO HELP. AMM 33-51-06-960-806 USED A SERVICEABLE POWER SUPPLY AT LOCATION M1669, NO HELP. RECONNECTED ORIGINAL POWER SUPPLY. WD 33-51-13SDR SWAA2021122051002Light · missingEMERGENCY LIGHT LENS IS MISSING AT O/H BIN BULLNOSE ROW 13DEF ; / [01] INSTALLED NEW LIGHT LENS AT O/H BIN BULLNOSE ROW 13DEF IAW BOEING 737-700 AMM 33-51-03-960-801.; [02] VERIFIEDSDR SWAA2021122048830Panel · crackedDURANT OK TO CLOSE FOUND PANEL 651BB CRACKED AT INTERNAL SURFACE ; / [01] CLANER AND PREPAIRED FOR REPAIR FOUND PANEL 651 BB AS PER B737-700 SRM 51-70-04-2R-1; [02] CLEANED AND PREPPED FOR REPAIR NEEDED ON PANEL 651BB AS PER B737-700 SRM 51-70-04-2R-1; [03] VESDR SWAA2021122048831Skin · crackedCRACK FOUND AT LW #4 SLAT SKIN AT ACTUATOR FITTING ATTACHMENT 3RD 0/B AFT RIVET. CRACK LENGTH 0.0394' AT 1 O'CLOCK POSITION. ; CRACK FOUND AT LW #4 SLAT SKIN AT ACTUATOR FITTING ATTACHMENT 3RD 0B AFT RIVET. CRACK LENGTH 0.0394' AT 1 O'CLOCK POSITION. REMOVED SDR SWAA2021122047213Structure · crackedFOUND ANGLE CRACK AT AFT CARGO FLOOR STRUCTURE STA 867; LBL 10 ; / [01] REMOVED AND REPLACED ANGLE AT AFT CARGO FLOOR STRUCTURE STA 867;LBL 10 AS PER REF B737-700 SRM 51-40-02-0G-0.; [02] VERIFIED STEP 1.SDR SWAA2021122047019Stringer · corrodedAFT OF FWD CARGO COMP. STRINGER 23 R/H AT BULKHEAD STA 540 IS CORRODED ; / [01] REMOVED FASTENERS FROM STRINGER 26L AND STA 540 PER B737-700 SRM 51-40-02-0G-0; EVALUATED CORRODED AREA AND FOUND OUT OF LIMITS PER B737-700 SRM 53-00-03-1A-1 FIG 103; ORIGINAL MATSDR SWAA2021122046104None · brokenFOUND 1EACH CLIP ASSY BROKEN AT FWD CARGO COMP. AFT BULKHEAD L/H SIDE BY PANEL #121EW ; / [01] REMOVED AND REPLACED 1EA CLIP AT FWD CARGO COMP AFT BULKHEAD L/H SIDE AS REF. B737-700 SRM 51-40-02-0G-0; [02] VERIFIEDSDR SWAA2021122045776Seat Track · corrodedCAPTAIN AND 1ST OFFICER SEATS; ALL 04 FWD TRACKS HAVE CORROSION AT THE BASE. ; / [01] REMOVED CAPTAIN AND FIRST OFFICER SEATS ALL 4 FWD TRACKS; AS PER REF: 51-40-02-0G-0.; [02] VERIFIED STEP 1 AND OK TO INSTALL NEW TRACKS 4EA; [03] INSTALLED CAPTAIN AND FIRST SDR SWAA2021122045777Stringer · corrodedAFT OF FWD CARGO STRINGER 26 LH AT BULKHEAD 540 IS CORRODED ; / [01] REMOVED FASTENERS FROM STRINGER 26L AND STA 540 PER B737-700 SRM 51-40-02-0G-0; EVALUATED CORRODED AREA AND FOUND OUT OF LIMITS PER B737-700 SRM 53-00-03-1A-1 FIG 103; ORIGINAL MATERIAL .045'SDR SWAA2021122041576Floor Support · corrodedFWD CARGO FLOOR SUPPORT RIGHT SIDE AT STA 500 THRU 500A RBL 22'OF CENTER LINE IS CORRODED ; / [01] REMOVED CORROSION AT FWD CARGO;SIDE PLATE FLOOR SUPPORT R/SIDE;STA 500 THRU 500A;RBL 22'.PER B 737-700 SRM 51-10-02-0G.FOUND OUT OF LIMITS;CORROSION PASS THRU.PESDR SWAA2021122042001Intercostal · crackedFWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL CRACKED BETWEEN STA 277 AND 295.5 ; BL-0 MKD DOT ; / [01] REMOVED INTERCOSTAL AT FWD WET AREA;BET.STA 277 TO STA 295.5;BL 0.PER B 737-700 SRM 51-40-02-0G-0.; [02] LOCATED AND DRILL NEW PART.PER B 737-700 SRM 51-10-0SDR SWAA2021122042007Intercostal · crackedFWD CABIN WET AREA INTERCOSTAL SUPPORT CRACKED @ LBL 45 BETWEEN STA 312 AND 328 MKD DOTB ; / [01] REMOVED INTERCOSTAL FLOOR SUPPORT AT FWD WET AREA;STA 312 TO STA 328 LBL 45''PER B 737-700 SRM 51-40-02-0G-0; [02] LOCATED AND DRILL NEW PART;PER B 737-700 SRM 51SDR SWAA2021122041988None · crackedMAIN CABIN FLOOR CENTER WING SUPPORT BREAK CRACKED AT FASTENER TAIL BS 540, RBL 24. REMOVED FLOOR PANEL 231 UF AT MAIN CABIN IAW AMM 53-21-00-000-801. REMOVED SUPPORT BREAK IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW PART IAW ARM 51-10-02-0G-0. INSTALSDR SWAA2021111241546Channel · broken'U-CHANNEL' BROKEN JUST ABOVE RT RAM AIR INLET LIP PANEL ASSY. AT STA 540. REMOVED CLIP AT ABOVE RT RAM AIR INLET LIP PANEL ASSY STA 540 B737-700 SRM 51-40-02-0G-0 LOCATED HOLES AND NEW CLIP B 737-700 SRM 51-10-02-0G-0 CERTIFIED. VERIFIED STEP 1 AND 2. OK TO SDR SWAA2021111241545Angle · crackedLT FWD WING TO BODY FAIRING INTERNAL SUPPORT ANGLE CRACKED FOR ACCESS PANEL 191AL. REMOVED LT FWD WING TO BODY FAIRING INTERNAL SUPPOR ANGLE (END RIB) PER B737-700 SRM 51-40-02-0G-0 FOR ACCESS TO ATTCACH FAIRING PANEL #191AL VERIFIED STEP 1 LOCATED AND DRILLESDR SWAA2021111241551Structure · corrodedFLIGHT DECK FLOOR STRUCTURE HAS SURFACE CORROSION UNDER CAPTAIN'S SEAT TRACKS. CLEANED AREA AT FLIGHT DECK FLOOR STRUCTURE UNDER CAPITAN`S SEAT TRACKS AREA PER B737-700 SRM 51-10-02-0G-0 NO CORROSION FOUND ONLY DAMAGED PAINT. VERIFIED STEP 1. OK TO TREAT AND
Back to N409WN, cancelled Jun 5, 2026