N443WN
Service difficulty reports · 317
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 = 'N443WN' 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.
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 = 'N443WN' AND registry_match = 'registration' 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 SWAA2026101935111Lamp · inoperativeEMERGENCY LIGHT AT ROW 21DEF INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-03. OPS CHKD OKAY.SDR SWAA2026100588044Unknown · smokeSMALL PATCH OF VISIBLE WHITE SMOKE AND FUMES BTWN CA HEAD & IPAD. DID NOT CONTINUE AND NO OTHER INDICATIONS OF SMOKE OR FUMES THE REMAINER OF FLIGHT. DURATION WAS 1-2 SECS. PERFORMED SMOKE FUMES CONDITIONAL INSPECTION IAW FIM 21-00 TASK 806, NO DEFECTS NOTED. SDR SWAA2026100128693Engine · smokeNO LIGHT OFF NR 1 ENGINE USING RT IGNITION, AIRCRAFT BEHIND US INDICATED SMOKE COMING FROM NR 1 ENGINE. PERFORMED FIM TASK 80-06 TASK 804. NO RECENT FAULTS AND ON FAULT HISTORY ON ECC 1. PERFORMED IGN L & R AUDIBLE TEST. ENG 1 STARTED ON R IGN ON IDLE RUN. OPSSDR SWAA2026090858400Battery · inoperativeFWD MEGAPHONE WILL NOT WORK. IAW AMM 25-64-00 R & R THE BATTERY. OK FOR SERVICE.SDR SWAA2026052205502Lamp · inoperativeEMERGENCY LIGHT AT SEAT ROW 15ABC INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT ROW 15 ABC WDM 33-51-22. PERFORMED SATISFACTORY OPS CHECK IAW AMM 33-51-00-710-801.SDR SWAA2026052695211Skin · crackedFOUR CRACKS FOUND BETWEEN BS 727A - 727D APPROX. 3IN ABOVE STR14. FUSELAGE CRACK AT BS727A REF TTG8Q01BZCXU; FUSELAGE CRACKED AT BS727D REF TTG8Q01BZCYB; FUSELAGE CRACK AT BS 727B REF FOUR CRACKS FOUND BTWN BS727A-BS727-D APPROX. 3IN ABVE STR14. REPAIRED FUSESDR SWAA2026052694951Skin · crackedFUSELAGE HAS A .45 VERTICAL CRACK AT BS 727A; APPROX. 3 ABOVE STR 14R; VERIFIED WITH HFEC PER NDT PART 6; 51-00-00 PROCEDURE 23 AND FLUORESCENT PENETRANT INSPECTION PER SOPM 20-20-02. .26-153-01210SDR SWAA2026052694952Skin · crackedFUSELAGE HAS A .95 VERTICAL CRACK AT BS 727B; APPROX. 3 ABOVE STR 14R. VERIFIED WITH HFEC PER NDT PART 6; 51-00-00 PROCEDURE 23 AND FLUORESCENT PENETRANT INSPECTION PER SOPM 20-20-02. REFER TO FAULT TTG8Q01BZXU WHERE EA 26-153-01210 WAS ADDED AS A SUBTASK. SDR SWAA2026052694953Skin · crackedFUSELAGE HAS A .50 VERTICAL CRACK AT BS 727D APPROX. 3 ABOVE STR 14R; VERIFIED WITH HFEC PER NDT PART 6; 51-00-00 PROCEDURE 23 AND FLUORESCENT PENETRANT INSPECTION PER SOPM 20-20-02<[01] REFER TO FAULT TTG8Q01BZCYK WHERE EA 26-153-01211 WAS ADDED AS A SUBTASSDR SWAA2026052694954Skin · crackedFUSELAGE HAS A .72 VERTICAL CRACK AT BS 727E APPROX. 3 ABOVE STR 14R. VERIFIED WITH HFEC PER NDT PART6; 51-00-00 PROCEDURE 23 AND FLUORESCENT PENETRANT INSPECTION PER SOPM 20-20-02. C\W 26-153-01211.SDR SWAA2026052694660Skin · crackedSUSPECTED CRACK AT BS727A AND APPROX 3IN ABOVE S14R. REQUEST TO HAVE PAINT REMOVED TO VERIFY. REMOVED PAINT FROM BS727A APPROX 3 IN ABOVE STR14R<BR>REF AMM 51-21-11. COMPLIED WITH HFEC INSPECTION PER NDT PART 6, 51-00-00 PROCEDURE 23 AND FLUORESCENT PENETRASDR SWAA2026052694661Skin · crackedSUSPECTED CRACK AT BS727B AND APPROX 3IN ABOVE STR14R. REQUEST TO HAVE PAINT REMOVED TO VERIFY. REMOVED THE PAINT AT BS727B AND APPROX 3IN ABOVE STR14R REF AMM 51-21-11. COMPLIED WITH HFEC INSPECTION PER NDT PART 6; 51-00-00 PROCEDURE 23 AND FLUORESCENT PESDR SWAA2026052694663Skin · crackedSUSPECTED CRACK AT BS 727D AND APPROX 3IN ABOVE S14R. REMOVED THE PAINT AT BS727D AND APPROX 3IN ABOVE STR14R REF AMM 51-21-11. COMPLIED WITH HFEC INSPECTION PER NDT PART 6; 51-00-00 PROCEDURE 23 AND FLUORESCENT PENETRANT INSPECTION IAW AMM 70-40-01; VERIFIESDR SWAA2026052694664Skin · crackedSUSPECTED CRACK AT BS 727E AND APPROX 3IN ABOVE S14R. REQUEST TO HAVE PAINT REMOVED TO VERIFY. REMOVED THE PAINT AT BS727E AND APPROX. 3IN ABOVE STR14R REF AMM 51-21-11. COMPLIED WITH HFEC INSPECTION PER NDT PART 6; 51-00-00 PROCEDURE 23 AND FLUORESCENT PENESDR SWAA2026022673941Flashlight Assy · no testAFT LEFT FLASHLIGHT WILL NOT TEST. REMOVED AND REPLACED AFT LEFT EMERGENCY FLASHLIGHT, BATTERY, AND MOUNTING BRACKET. OPS CHECKED GOOD. ALL WORK PERFORMED IAW AMM 25-64-00.SDR SWAA2025070787513Battery Pack · inoperativeEMERGENCY EXIT BATTERY PACK M1670 WILL NOT CHARGE. REPLACED EMERGENCY BATTERY PACK M1670 AND ACCOMPLISHED OPS CHECK IAW AMM 33-51-960-805. TEST GOOD.SDR SWAA2025070778542Stringer · crackedREF. TTG8Q012Z7GR CRACK INDICATION NOTED AT STR. 1 BETWEEN 727A +10 AND 727A +12 (FWD OF WIFI DOUBLER) HIGHEST READING NOTED OF 67 % FSH WITH PAINT.<[01] DAMAGED AREA WAS REMOVED; VERIFIED; AND REPLACED I.A.W. SRM 51-10-02; B737 NDT PART 6; 51-00-00 PROC 23 ; SDR SWAA2025070778969Stringer · crackedCRACK INDICATION NOTED AT STR 1 BETWEEN 767+6 AND 767+8(AFT OF WIFI DOUBLER) HIGHEST READING NOTED OF 58% FSH WITH PAINT. REMOVED AND REPAIRED DAMAGE AT STR 1 BETWEEN STA 767 + 6' AND 767 + 8' I/A/W EA 25-153-015510-WIP 1 THRU WIP3 AND EA 25-153-01510. REMOSDR SWAA2025060977774Skin · crackedCRACK INDICATION NOTED AT STR 1 BETWEEN 727A+10 AND 727A+12(FWD OF WIFI DOUBLER). HIGHEST READING NOTED OF 67% FSH WITH PAINT. APPLIED PAINT STRIPPER TO DESIGNATED LOCATION IAW AMM 51-21-11. VERIFIED CRACK INDICATION WITH PAINT REMOVED PER 737 NDT MANUAL; PASDR SWAA2025060977775Skin · crackedCRACK INDICATION NOTED AT STR 1 BETWEEN 767+6 AND 767+8(AFT OF WIFI DOUBLER) HIGHEST READING NOTED OF 58% FSH WITH PAINT. APPLIED PAINT STRIPPER TO DESIGNATED LOCATION IAW AMM 51-21-11. VERIFIED CRACK INDICATION WITH PAINT REMOVED PER 737 NDT MANUAL; PART 4 SDR SWAA2025043064611Lamp · inoperativeR1 DOOR EMERGENCY EXIT SLIDE LIGHT INOP.<[01] RE-LAMPED SAID LIGHT ASSY PER AMM 33-51-04. OPS CHK OK.SDR SWAA2025042222843Shield · corrodedDOT A24-98 AFT PIT SHIELD FORWARD OF DOOR CUT-OUT CORRODED ON UPPER SURFACE NEAR FORWARD END. MARKED<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[02] VERIFIED STEP 1<BR>AUDISDR SWAA2025042220669Handle · looseL-1 DOOR INTERIOR AFT ASSIST HANDLE IS LOOSE.<[01] TIGHTEN L-1 DOOR INTERIOR AFT ASSIST HANDLE IAW AMM 25-21-31-420-802 ITEM B A-6;[02] C/W<BR>AUDIT C/WSDR SWAA2025042221138Filler · brokenEXTERNAL POWER DOOR MIDDLE LATCH CUTOUT HAS BROKEN FILLER SECTION FROM PREVIOUS REPAIR.<[01] 04 - REPAIRED PER [SRM 53-10-15-2R-4-A00964 (REPAIR 4 - ELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER - PERMANENT)];[02] COMPLETE<BR>AUDIT C/WSDR SWAA2025042220931Slide · out of adjustCUSTOMER REQUEST TF. L-2 DOOR SLIDE CONTACTS DOOR CUTOUT WHEN CLOSING<[01] FAULT WAS RESOLVED ON WORK CARD TTG8Q00ZMHEV;[02] FAULT WAS RESOLVED ON WORK CARD TTG8Q00ZMHEV.<BR>ADJUSMENT FOLD CLEAR CHECK GOOD;[03] REPOSITIONED FABRIC ATTACH TO THE GIRT BAR FOR L-SDR SWAA2025042219927Beam · crackedFWD SERVICE DOOR STRUCTURE BEAM 141A6536-14; #4 BEAM IS CRACKED IN RADIUS AT AFT HANDLE BOX MOUNT.<[01] REMOVED SERVICE DOOR BEAM #4 I/A/W SRM 51-40-02-0G-0 INSTALLED NEW FWD SERVICE DOOR BEAM #4 ON EA 5241-C-14093-NG STEP 2 I/A/W SRM 51-40-02-0G-0 AND BOEING SDR SWAA2025042220079Support · cracked(DOT 147-14) MAIN CABIN FLOOR SUPPORT EXPANSION BETWEEN BL 0 AND LBL 25 AT STA 540 HAS CRACK IN I/B SIDE <[01]. 04 - REPAIRED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]; [02] 01 - REMOVED AND REPLACED PESDR SWAA2025042220080Floorbeam · cracked(DOT 147-13) MAIN CABIN FLOOR SUPPORT EXPANSION BETWEEN BL 0 AND RBL 25 AT STA 540 HAS CRACK IN I/B SIDE<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[02] VERIFIED TASK COMPLSDR SWAA2025042220075Plate · crackedDOT#02 A-043 LH WING T/E WAFFLE PLATE CRACKED AT INBD FASTENER WS 302.50<[01] REMOVED AND REPLACED WAFFLE PLATE ON LH WING WS 302.50 I.A.W. SRM 51-40-02-0G-0 AND DWG 115A3712 REV:-;[02] VERIFIED ITEM 1<BR>C/WSDR SWAA2025042219649Bracket · crackedLEFT WING TRAILING EDGE; INBOARD OF DEFLECTION CONTROL RIB; WEB BULB SEAL RETAINER BRACKET CRACKED AT UPPER 2 EA. BOLTS.<[01] 04 - REPAIRED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[02] 01 - REMOVED ANSDR SWAA2025042219655Angle · cracked(A204 DOT 3) RH WING TRAILING EDGE CAVITY. 1 INCH INBOARD OF DEFLECTION CONTROL RIB. AND 24 INCHES FWD OF PANEL TRAILING EDGE. LATTERAL SUPPORT ANGLE IS CRACKED OUTBOARD FASTNER HOLE COMMON TO SKIN.<[01] REMOVED AND REPLACED LATTERAL SUPPORT ANGLE ON RH WING TSDR SWAA2025042219650Rib · cracked(A204 DOT 4) RH WING TRAILING EDGE CAVITY; 24 INCHES FORWARD OF PANEL TRAILING EDGE. ATTACH ANGLE COMMON TO DEFLECTION CONTROL RIB IS CRACKED AT LOWER OUTBOARD HOLE.<[01] 04 - REPAIRED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL SDR SWAA2025042219647Skin · cracked#2 SLAT; LOWER SKIN AT ACTUATOR ATTACHMENT; 2 RIVETS FOUND LOOSE WITH VISIBLE EVIDENCE OF SKIN CRACKS PROPOGATING FROM THE HOLES<[01] REPAIRED #2 SLAT; LOWER SKIN AT ACTUATOR ATTACHMENT IAW SRM 57-42-01-2R-8 AND SRM 51-40-02-0G-0;[02] AUDIT C/WSDR SWAA2025012087523Battery · no testAFT FA MEGAPHONE WILL NOT TEST<[01] REPLACED AFT FA FLASHLIGHT BATTERY PER AMM25-64-00SDR SWAA2024083031015Battery Pack · inoperativeL/H OVERWING EMER EXIT LIGHTS INOP<[01] REMOVED AND REPLACED LH OVERWING EMER EXIT LIGHTS BATTERY PACK M1668 AT STA 603 IAW AMM 33-51-06. OPS CHECK OKSDR SWAA2024082628295Battery Pack · failedM1675 BATTERY PACK FAILED CAPACITY CHECK.<[01] R&R M1675 BATTERY PACK REF AMM 33-51-06.SDR SWAA2024082628288Battery Pack · failedM1668; M1670; M1673; M1672; M1669; M1674 BATTERY PACKS FAILED CAPACITY CHECK.<[01] R&R BATTERY PACKS M1668; M1670; M1673; M1672; M1669; M1674 REF AMM 33-51-06.SDR SWAA2024082628294Bracket · looseFWD SERVICE DOOR (R1) FWD GIRT BAR HANGER BRACKET LOOSE ON SLIDE SHROUD<[01] SQUEEZED RIVETS FOR FWD SERVICE DOOR (R 1) FWD GIRT BAR HANGER BRACKET ON SLIDE SHROUD PER SRM 51-40-02SDR SWAA2024082628287Bracket · looseFWD ENTRY DOOR (L1) FWD GIRT BAR HANGER BRACKET LOOSE ON SLIDE SHROUD<[01] SQUEEZED RIVETS FOR FWD ENTRY DOOR (L1) FWD GIRT BAR HANGER BRACKET ON SLIDE SHROUD PER SRM 51-40-02.SDR SWAA2024082628296Doubler · missingPOWER RECEPTACLE CUT OUT; AFT DOUBLER MISSING HALF [TTG8Q00VCS16] RII REQUIRED<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]SDR SWAA2024080823954Light · brokenFWD ENTRY DOOR EMERGENCY EXIT LIGHT COVER BROKEN<[01] MADE TEMPORARY REPAIR PER EA M-21-133-00720. OK TO CONTINUE PER TLD M-21-133-00720. A/C OK FOR SERVICESDR SWAA2024040168733Lens · wrong partLOWER EXIT SIGN AT L1 DOOR MISSING DIRECTIONAL ARROW.<[01] R&R THE LOWER EXIT SIGN LENS AT L1 DOOR REF AMM 33-51-01.SDR SWAA2024040168727Lens · incorrectR1 DOOR LOWER EXIT SIGN IS NOT MULTI LINGUAL.<[01] R&R LOWER EXIT SIGN LENS AT R1 DOOR REF AMM 33-51-01.SDR SWAA2023121128623Seal · crackedRH HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL CRACKED.<[01] REMOVED AND REPLACED RH HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL. REF AMM 53-31-31SDR SWAA2023090898215Battery Pack · inoperative5 EMERGENCY LIGHTS INOP AT FWD GALLEY/CABIN<[01] SWAPPED BATTERY PACK M0174 AND M01675 IAW AMM 33-51-06. PROBLEM FOLLOWED. SUSPECT BAD BATTERY AND POWER SUPPLY. PARTS NIS UNTIL 0800;[02] REMOVED AND REPLACED FWD L/H EMER LIGHT BATTERY PACK REF AMM 33-51-06. OPSDR SWAA2023082893044Handle · looseCABIN R2 DOOR CLOSE ASSIST HANDLE IS LOOSE.<[01] SECURED CABIN R2 DOOR CLOSE ASSIST HANDLE IAW AMM 52-41-31.SDR SWAA2023061458214Slide · looseL1 DOOR SLIDE CAME OUT OF CONTAINER WHILE OPENING THE DOOR.<[01] C/W MT 725-61-06; REPACKED L1 DOOR SLIDE. AC OK FOR SERVICE.SDR SWAA2023041124439Handle · looseASSIST HANDLE ON L-2 DOOR LOOSE.<[01] ADJUSTED ASSIST HANDLE ON L2 DOOR AS PER REF 52-13-31-400-802;[02] VERIFIED ADJUSTMENT OF ASSIST HANDLE ON L2 DOOR AS PER REF 52-13-31-400-802.SDR SWAA2023041223900Slat · delaminatedSLAT #3 UPPER IB CORNER ON TE AREA IS DELAMINATED. .<[01] REMOVED DELAMINATED EXISTING FILLER REPAIR; AND PREPARED AREA FOR REBOUNDING NEW FILLER REPAIR ON L/W L/E #3 SLAT I/B CORNER T/E AS PER B737 SRM 57-42-01-2R-6. REBOUNDED FILLER REPAIR AS MARKED ON #3 L/SDR SWAA2023041222641Light · defectiveSEVERAL EMERGENCY EXIT LIGHTS DEFECTIVES THRU THE CABIN.<[01] PERFORMED EMERGENCY LIGHTS OPERATIONAL TEST AND FOUND NORMAL PER REF AMM 33-51-00-710-801;[02] VERIFIED STEP 1
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