N445WN
Service difficulty reports · 289
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 = 'N445WN' 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 = 'N445WN' 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 SWAA2024010422607Floor Support · crackedMAIN CABIN CENTER WING BOX FLOOR SUPPORT BREAK CRACKED AT STA 540 RBL-1 MKD DOT<[01] REMOVED AND REPLACED SUPPORT BREAK ASSY AT MAIN CABIN CENTER WING BOX STA 540 RBL-1 PER REF B737 SRM 51-40-02-0G-0 AND DWG 143A0060.;[02] VERIFIED ENTRY 1 AS WORK COMPLETED.SDR SWAA2024010525461Vapor Barrier · crackedCENTER WING REAR SPAR VAPOR BARRIER WEB L/H SIDE CRACKED AT STA 663.75 0/B MKD DOT<[01] ALL STEPS COMPLETED.;[02] REPAIRED DAMAGE AREAS AT CENTER WING REAR SPAR VAPORR BARRIER WEB L/H SIDE AS PER SRM 51-70-04-2R 10. MATERIAL USED EY 3804 A/B PO#2040614 PLUS BMSDR SWAA2024010526503Vapor Barrier · crackedCENTER WING REAR SPAR VAPOR BARRIER WEB SUPPORT STIFFENER CRACKED AT LOWER END STA 663.75 RBL 25 MKD DOT<[01] REMOVED AND REPLACED SUPPORT STIFFENER AT CENTER WING REAR SPAR VAPOR BARRIER WEB STA 663.75 RBL 25 AS PER B 737-700 SRM 51-40-02-0G-0 AND DWG# 111A10SDR SWAA2024010421859Floor Support · corrodedAFT CARGO FLOOR SUPPORT AT 767-787 24 INCHES RIGHT OF CENTER LINE IS CORRODED.<[01] REMOVED AND REPLACED FLOOR SUPPORT (SHIELD) AT AFT CARGO COMPT STA 767 TO STA 787 RBL 24 PER REF SRM 51-40-02-0G-0 AND DWG #146A0081;[02] FINAL INSPECTION; VERIFIED STEP #1.SDR SWAA2024010421860Channel · corrodedAFT CARGO RIGHT 'Z' CHANNEL IS CORRODED AT 767-727D<[01] REMOVED AND REPLACED R/H Z-CHANNEL AT AFT CARGO COMPT STA 727D+10 TO STA 767 RBL 21 PER REF SRM 51-40-02-0G-0 AND DWG #146A7500;[02] FINAL INSPECTION; VERIFIED STEP #1.SDR SWAA2024010421475Support · corrodedFWD CARGO FLOOR SUPPORT AT 500-500A 24 INCHES RIGHT OF CENTER LINE IS CORRODED<[01] REMOVED AND REPLACED FWD CARGO COMPT FLOOR SUPPORT (PN: 143A8126U31ATSMRO PO: 2012626) AT STA 500 TO STA 500A RBL 24 PER REF SRM 51-40-02-0G-0 AND DWG #143A8126;[02] FINAL INSPSDR SWAA2023091409218Rub Strip · out of adjustAFT SVC DOOR SLIDE COVER BUMPER TRIM END CAP MISSING. TAPE APPLIED TO TRIM. OK TO CONT ON MEL 25-10-01 SP1B. R&R END CAP AND RUBSTRIP IAW AMM 25-66-00.SDR SWAA2023091499956Cap · missingAFT SVC DOOR SLIDE COVER BUMPER TRIM END CAP MISSING. TAPE APPLIED TO TRIM. OK TO CONT ON MEL 25-10-01 SP1B. R & R END CAP AND RUBSTRIP IAW AMM 25-66-00.SDR SWAA2023091198605Slide · looseR1 DOOR SIDE CAME OFF DOOR AS IT WAS OPENING<[01] COMPLETED PART REMOVAL TRANSACTION.;[02] REMOVED AND INSTALL FWD SERVICE ESCAPE SLIDE PER AMM 25-66-01 MT 725-61-06. OPS CHECK GOOD.SDR SWAA2023051547654Floor Panel · crackedGROUND CREW REPORTS CRACK ON THE FLOOR OF THE FWD CARGO COMPARTMENT<[01] OK TO CONTINUE PER MEL 25-16-01 SP1B;[02] REPAIRED FWD CARGO COMPARTMENT FLOOR PANEL PER AMM 25-52-01.SDR SWAA2023013196148Panel · elongatedWING TO BODY FAIRING PANEL #193B HAS NUMEROUS ELONGATED HOLES.<[01] R&R PANEL 193B PER SRM 51-40-02-0G-0.SDR SWAA2022110267133Girt Bar · looseGIRT BAR RETAINING CLIP LOOSE; ON R1 DOOR / [01] SECURED GIRT BAR CLIP IAW S.I.P.SDR SWAA2022081140236Slide · out of positionL2 DOOR SLIDE DRAGGING ON THE FLOOR / [01] RE-PACK L2 DOOR SLIDE AS PER AMM 25-66-01SDR SWAA2022032184919Transmission · faultyFLAP T/E DISAGREE COMMANDED FLAPS 30; LEFT FLAP INDICATES 20 AND RIGHT FLAP INDICATES 25. / [01] FOUND BAD #2 FLAP TRANSMISSION.REMOVED AND REPLACED #2 FLAP TRANSMISSION IAW AMM 27-51-41 OPS AND RIG CHECK GOOD;[02] C/W INSPECTION.SDR SWAA2021112947022None · inoperativeSUPPLEMENTAL INFORMATION: L1 DOOR EXTERIOR EMERGENCY LIGHT INOP ; 2021-488120 / [01] REPLACED L1 DOOR EXTERIOR EMERGENCY LIGHT LAMP AND PERFORMED TEST IS OK IAW B737-700 AMM 33-51-04-960-801 .; [02] REPLACED L1 DOOR EXTERIOR EMERGENCY LIGHT LAMP AND PERFORMED SDR SWAA2021112439256None · crackedSUPPLEMENTAL INFORMATION: CRACK INDICATION ON INNER CHORD LOCATED BS 294.5 AND STR 17R AT FWD GALLEY AREA ; 2021-488094 / [01] REPLACED INNER CHORD LOCATED BETWEEN BS 271 TO BS 360 APROX STR 17R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DRSDR SWAA2021112438577Lens · brokenSUPPLEMENTAL INFORMATION: BROKEN EMERGENCY LIGHT LENS LOCATED ON OVERHEAD STOWAGE BIN RH SIDE AT PASSENGER CABIN (8 EA) ; 2021-488057 / [01] REMOVED AND INSTALLED EMERGENCY LIGHT LENS LOCATED ON OVER HEAD STOWAGE BIN RH SIDE AT PASSENGER CABIN (8 EA) IAW B737-SDR SWAA2021112438576None · brokenSUPPLEMENTAL INFORMATION: BROKEN EMERGENCY LIGHT LENS LOCATED ON OVERHEAD STOWAGE BIN LH SIDE AT PASSENGER CABIN (9 EA) ; 2021-488056 / [01] REMOVED AND INSTALLED EMERGENCY LIGHT LENS LOCATED ON OVERHEAD STOWAGE BIN LH SIDE AT PASSENGER CABIN (9 EA) IAW B737-7SDR SWAA2021112438138Lens · brokenSUPPLEMENTAL INFORMATION: BROKEN EMERGENCY EXIT LENS GALLEY 1 AT FWD GALLEY AND LAV (1 EA) ; 2021-487983 / [01] REPLACED EMERGENCY EXIT LENS GALLEY 1 AT FWD GALLEY AREA (1 EA) IAW AMM 33-51-01-960-802 STEP 3.C (10).; [02] TASK COMPLETED.SDR SWAA2021112438134Lens · brokenSUPPLEMENTAL INFORMATION: BROKEN EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA) ; 2021-488010 / [01] REPLACED EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA) IAW AMM 33-51-01-960-801 STEP 3.C (10).; [02] JOB COMPLETEDSDR SWAA2021112937828Bracket · crackedCRACK SUPPORT BRACKET LOCATED ORSS 268 TRAILING EDGE AT LT WING ; 2021-487894 / [01] REPLACED SUPPORT BRACKET LOCATED ORSS 268 TRAILING EDGE AT LT WING IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9; [02] CERTIFIED STEP 1 COMPLETE IAW B737-700 SRM 51-40-02 AND SDR SWAA2021112937829Support · crackedCRACK ANGLE SUPPORT LOCATED ORSS 268 TRAILING EDGE AT RT WING ; 2021-487895 / [01] REPLACED ANGLE SUPPORT LOCATED ORSS 268 TRAILING EDGE AT RT WING IAW B737-700 SRM 51-10-02 AND 51-40-02; [02] COMPLETE TASK CERTIFIEDSDR SWAA2021112938126Access Panel · crackedCRACK ACCESS PANEL 651FB ON SUPPORT AT RT WING ; 2021-487955 / [01] REPLACED ACCESS PANEL 651FB ON SUPPORT AT RT WING IAW B737-700 SRM 51-40-02-0G-0; [02] REPLACED ACCESS PANEL 651FB ON SUPPORT AT RT WING IAW B737-700 SRM 51-40-02-0G-0<BR>COMPLETED TASK.SDR SWAA2021112933846None · crackedSUPPLEMENTAL INFORMATION: CRACK INDICATION ON RADIUS OF THE LOWER BEAM 4 (141A6536-14) FWD SERVICE DOOR. CRACK LENGTH 0.560 INCH. ADD EO 5241-C-14093 OR 5241-C-14344. ; 2021-487819 / [01] REPLACED BEAM #4 AND FASTENERS LOCATED FWD SERVICE DOOR IAW B737-700 SRMSDR SWAA2021112937821Floor Panel · brokenBROKEN FLOOR PANEL 241ABF SLEEVE AT PASSENGER CABIN (10 EA) ; 2021-487856 / [01] REPLACED FLOOR PANEL 241ABF AT AFT PASSENGER CABIN IAW MT TTG8Q00712MR.; [02] REPLACED FLOOR PANEL 241ABF AT AFT PASSENGER CABIN AND DOCUMENTED ON MT TTG8Q00712MR.; [03] VERIFIED SDR SWAA2021112937823Floor Panel · corrodedCORROSION FLOOR PANEL 242VF ON SLEEVE AT PASSENGER CABIN (6 EA) ; 2021-487858 / [01] REPLACED FLOOR PANEL 242VF AT AFT PASSENGER CABIN IAW MT TTG8Q007131Q.; [02] REPLACED FLOOR PANEL 242VF AT AFT PASSENGER CABIN AND DOCUMENTED ON MT TTG8Q007131Q.; [03] VERIFIESDR SWAA2021112937824Floor Panel · delaminatedDELAMINATED FLOOR PANEL 242VF AT PASSENGER CABIN ; 2021-487859 / [01] REPLACED FLOOR PANEL 242VF AT AFT PASSENGER CABIN IAW AMM 53-21-00-400-801 AND INSTALLATION WILL BE DOCUMENTED ON MT TTG8Q001RHF6.; [02] VERIFIED TASK COMPLETESDR SWAA2021112937826Floor Panel · brokenBROKEN FLOOR PANEL 221DF AT PASSENGER CABIN ; 2021-487864 / [01] REPLACED FLOOR PANEL 221DF AT PASSENGER CABIN IAW AMM 53-21-00-400-801 AND INSTALLATION WILL BE DOCUMENTED ON MT TTG8Q001RCWX.; [02] COMPLETEDSDR SWAA2021112937827Floor Panel · corrodedCORROSION FLOOR PANEL 221DF ON SLEEVE AT PASSENGER CABIN (4 EA) ; 2021-487865 / [01] REPLACED FLOOR PANEL 221DF AT PASSENGER CABIN AND DOCUMENTED ON TTG8Q00716T0; [02] COMPLETEDSDR SWAA2021112942447Web · crackedCRACK INBOARD FAN COWL WEB INTERNAL AREA ON ENGINE 1 ; 2021-487849 / [01] REPLACED WEB LOCATED ON INBOARD FAN COWL INTERNAL AREA ON ENGINE 1 IAW GOODRICH AEROSTRUCTURES CMM 71-13-30 AND B737-700 SRM 51-10-02 AND SRM 51-40-02; [02] REPLACED WEB LOCATED ON INBOASDR SWAA2021112433845Beam · crackedCRACK INDICATION ON RADIUS OF UPPER BEAM 5, FWD SERVICE DOOR. CRACK LENGTH 0.750 INCH. REPLACED THE BEAM AND FASTENERS IAW SRM 51-10-02, SRM 51-40-02, & DWG 141A6516 REV-.SDR SWAA2021110137822Floor Panel · delaminatedDELAMINATED FLOOR PANEL 241ABF AT PASSENGER CABIN. REPLACED FLOOR PANEL 241ABF AT AFT PASSENGER CABIN IAW AMM 53-21-00-400-801 AND INSTALLATION WILL BE DOCUMENTED ON MT TTG8Q001RHF6. VERIFIED TASK COMPLETESDR SWAA2021110137667Floor Panel · missingMISSING FLOOR PANEL 241ABF INSERT AT PASSENGER CABIN (4 EA). REPLACED FLOOR PANEL 241ABF AT AFT PASSENGER CABIN IAW TTG8Q00712MR. REPLACED FLOOR PANEL 241ABF AT AFT PASSENGER CABIN AND DOCUMENTED ON TTG8Q00712MR. VERIFIED TASK COMPLETESDR SWAA2021112933840Stub Frame · crackedSUPPLEMENTAL INFORMATION: CRACK FWD SERVICE DOOR CUTOUT STUB FRAME LOCATED BS294.5 BETWEEN STR 7R AND STR 9R AT PASSENGER CABIN ; 2021-487807 / [01] REPLACED STUB FRAME LOCATED ON FWD SERVICE DOOR CUT OUT BS 294.5 BTW STR 7R AND STR 9R AT PASSENGER IAW B737-70SDR SWAA2021112933612Support Angle · crackedSUPPLEMENTAL INFORMATION: CRACK FWD SERVICE DOOR CUTOUT SUPPORT ANGLE LOCATED BETWEEN BS291.5 TO BS 294.5 AT STR 17R AT PASSENGER CABIN ; 2021-487792 / [01] FAULT RESOLVED ON OTHER FAULT; SEE TTG8Q0070KWP; FOR ANGLE REPLACEMENT; [02] FAULT RESOLVED ON OTHER FASDR SWAA2021112933611Frame · crackedSUPPLEMENTAL INFORMATION: CRACK FRAME ON BS 312 FWD UPPER CUT OUT ENTRY DOOR AT FWD GALLEY AREA ; 2021-487787 / [01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 21-JAN-22; [02] PERFORMED REPAIR ON FRAME BS 312 FWD UPPER CUT OUTSDR SWAA2021112933605Tie Clip · crackedSUPPLEMENTAL INFORMATION: CRACK TIE CLIP LOCATED BS 277 AND STR10R AT PASSENGER CABIN ; 2021-487784 / [01] REPLACED TIE CLIP LOCATED BS 277 AND STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02; B737-700 SRM 51-40-40-02 AND DRAWING # 141A1110 SHEET 18 REV-.;SDR SWAA2021112933839None · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 328 LBL44 FWD GALLEY AND LAV. REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE IAW SRM 51-10-02, SRM 51-40-02 AND DRAWING 141A5400 SHEET 26 REV -.SDR SWAA2021112933841Angle · crackedCRACK ANGLE LOCATED BETWEEN BS 380 AND BS 400 RBL10 AT PASSENGER CABIN ; 2021-487810 / [01] REPLACED ANGLE LOCATED BETWEEN BS 380 AND BS 400 RBL10 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; DWG 143A5400; SH 38; REV. A; AND SRM 51-40-02.; [02] CORRECTSDR SWAA2021112933842Angle · crackedCRACK ANGLE LOCATED BETWEEN BS 380 TO BS 400 BL0 AT PASSENGER CABIN ; 2021-487809 / [01] REPLACED ANGLE LOCATED BETWEEN BS 380 TO BS 400 BL0 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; DWG 143A5400; SH 38; REV. A; AND SRM 51-40-02; SEE INDIVIDUAL SIGNSDR SWAA2021112933835None · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 328 RBL30 FWD GALLEY AND LAV. REPLACED WEB IAW SRM 51-10-02, SRM 51-40-02 AND DRAWING 141A5400 SHEET 39 REV-.SDR SWAA2021112933834Angle · corrodedCORROSION ANGLE LOCATED BETWEEN BS 312 AND BS 344 AT LEVEL S-17L WL 208 AT PASSENGER CABIN ; 2021-487804 / [01] REPLACED ANGLE LOCATED BETWEEN BS 312 AND BS 344 AT LEVEL S-17L WL 208 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DRAWING 141A8110 SHEET 11 RESDR SWAA2021112933837Access Panel · delaminatedDELAMINATION ON FWD EDGE LOWER SURFACE OF ACCESS PANEL 193D LOWER FUSELAGE ; 2021-487813 / [01] TOOL USED: CALIPER P/N:500-464 S/N:B17030933 DUE DATE: 01-OCT-22; [02] HOT BONDER P/N HCS9200B-AV S/N 18196126 DUE DATE: 27-JAN-22.; [03] SCALE P/N SCA-301 S/N AE-4SDR SWAA2021112933838Access Panel · delaminatedDELAMINATED ACCESS PANEL 193AL BODY FAIRING AT FUSELAGE EXTERIOR ; 2021-487805 / [01] TOOL USED: CALIPER P/N: 500-197-30; S/N:A18229508; DUE DATE: 29-SEP-22.; [02] REPAIRED ACCESS PANEL 193AL BODY FAIRING AT FUSELAGE EXTERIOR AS PER B737-700 SRM 51-70-05-2R-6 SDR SWAA2021112933610Bracket · crackedCRACK FLOOR STRUCTURE SUPPORT ANGLE LOCATED BS867 AT LEVEL STR26L AT AFT CARGO COMPARTMENT ; 2021-487793 / [01] REPLACED SUPPORT BRACKET (ANGLE) AND FASTENERS LOCATED BS867 AT LEVEL STR26L AT AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02; DWG# 149A8102 SHSDR SWAA2021112933847Skin · crackedCRACK INDICATION FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 184.70; LOCATED 25.5 INCH FROM FRONT SPAR ON INBD SIDE OF RIB. CRACK LENGTH IS 0.750 INCH. ; 2021-487817 / [01] PERFORMED PERMANENT REPAIR ON LH HORIZONTAL STABILIZER LOWER IN-SPASDR SWAA2021112933844Skin · crackedCRACK INDICATION FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 184.70; LOCATED 9.5 INCH FROM FRONT SPAR ON INBD SIDE OF RIB. CRACK LENGTH IS 0.450 INCH. PERFORMED PERMANENT REPAIR ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 184.SDR SWAA2021112933836Access Panel · brokenBROKEN ACCESS PANEL 551DB LATCH SPRING LOC AT LT WING (1 EA) ; 2021-487812 / [01] REPLACED ACCESS PANEL 551 LATCH SPRING LOC AT LT WING 1EA IAW B737-700 SRM 51-40-02 -0G-0; [02] REPLACED ACCESS PANEL 551 DB LATCH SPRING LOC AT LT WING 1EA IAW B737-700 SRM 51-4SDR SWAA2021112933608Floorbeam · crackedCRACK FLOOR BEAM BS 294.5 AND RBL60 AT FWD GALLEY AREA ; 2021-487791 / [01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 210138503 DUE DATE: 05-MAR-22; [02] TOOL USED: EDDY CURRENT FLAW DETECTOR. PERFORMED REPAIR IAW SRM 53-10-51-2R-16 REPAIRSDR SWAA2021112933607Stub Frame · crackedCRACK FWD SERVICE DOOR CUTOUT STUB FRAME, BS 294.5, S17R. PERFORMED PERMANENT REPAIR ON STUB FRAME IAW SRM 53-10-15-2R-7, REPAIR 7.
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