N561WN
Service difficulty reports · 200
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 = 'N561WN' 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 = 'N561WN' 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 SWAA2023072559479Access Panel · crackedCRACK WEB LEADING EDGE ACCESS PANEL 341B LOC. STA 114.55 AT RT HORIZONTAL STABILIZER (1 EA) 2023-394553<[01] REPLACED WEB (RIB) LEADING EDGE ACCESS PANEL 341B LOC. STA 114.55 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 18SDR SWAA2023072570785Stiffener · brokenBROKEN SIDEWALL PANEL STIFFENER RT SIDE ON POSITION 242YEW AT PASSENGER CABIN (1 EA) 2023-394445<[01] REPLACED SIDEWALL PANEL STIFFENER RT SIDE ON POSITION 242YEW AT PASSENGER CABIN I.A.W. SOPM-20-50-12 REV. 56;[02] REPLACED SIDEWALL PANEL STIFFENER RT SIDE ONSDR SWAA2023072559480Slat · crackedCRACK ON LEADING EDGE LOWER SKIN SLAT 2 LOCATED SLAT STATION 322.71 AT LT WING 2023-394554<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[02] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N:N500X12SDR SWAA2023072559094Handle · brokenBROKEN SERVICE DOOR ASSY HANDLE NUT AT FWD GALLEY AREA (2 EA) 2023-394447<[01] REPLACED SERVICE DOOR ASSY HANDLE NUT AT FWD GALLEY AREA (2 EA) IAW B737-700 AMM 52-41-31-400-802 STEP 3. F ITEM (2);[02] CERTIFIED WORK PERFORMEDSDR SWAA2023072559100Support Angle · crackedCRACK SUPPORT ANGLE LOCATED BS695 AND RBL24.82 AT PASSENGER CABIN 2023-394466<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811019 DUE DATE: 25-JAN-24.;[02] REPLACED REPAIR SUPPORT ANGLE AND FASTENERS LOCATED BS695 AND RBL24.82 AT PASSENGER SDR SWAA2023072559101Support Angle · crackedCRACK SUPPORT ANGLE LOCATED BS695 AND LBL0.07 FWD SIDE AT PASSENGER CABIN 2023-394469<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112820025; DUE DATE: 01-FEB-2SDR SWAA2023072559097Pressure Deck · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB BTW RBL 40 TO RBL 50 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH APPROXIMATELY: 0.375 INCH. 2023-394451<[01] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 60009161631; DUE DATE: 31-JAN-24;[02] TOOLSDR SWAA2023072558931Access Panel · crackedCRACK ACCESS PANEL 661BB TRAILING EDGE AT RT WING 2023-394431<[01] TOOL USED: CALIPER P/N: 500-464 S/N: B17030933 DUE DATE: 17-OCT-23.;[02] TOOL USED HOT BONDER P/N HCS9200B-AV; S/N 18196021; DUE DATE: 24-JAN-24;[03] TOOL USED: SCALE P/N: SPC621 S/N: 834022548SDR SWAA2023051046553Radome · delaminatedPUNCTURE AND DELAMINATION<[01] FOUND RADOME PUNCTURE AND DELAMINATION; REMOVED AND REPLACED RADOME IAW AMM 53-52-00SDR SWAA2023041827588Radome · delaminatedFOUND HOLE IN CENTER OF RADOME WITH HONEYCOMB MISSING.<[01] DELAMINATION MEASUREMENT IS 1.0? L BY 0.90 H.;[02] COMPLIED WITH EA; TASK CARD # 23-153-01233SDR SWAA2022102765040Panel · crackedSUPPLEMENTAL INFORMATION: ELECTRICAL SERVICE PANEL PAST REPAIR AT LOWER CUTOUT AREA CRACKED / [01] REPAIRED ELECTRICAL SERVICE PANEL AT LOWER CUTOUT AREA IAW SRM 53-10-15-2R-4SDR SWAA2022060213285Light · inoperativeAFT SERVICE DOOR EMERGENCY EXIT LIGHTING MARKERS INOP / [01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IN AFT GALLEY LH CEILING PER AMM 33-51-06. OPS CHECK GOOD;[02] NOTE TO CHANGE INSTALLED BATCH NUMBER FROM 185926 TO 170893/211298.SDR SWAA2022032285285Plate · crackedR/H WING; WIGGLE PLATE BEHIND #2 ENG. IS CRACKED / [01] R&R RH WING; WIGGLE PLATE BEHIND #2 ENGINE IAW AMM 20-50-11 AND SRM 51-40-02.SDR SWAA2022032285286Tab · crackedR/H WING; FLAP ROLLER DEFLECTOR RIB ; UPPER TAB IS CRACKED / [01] ACCOMPLISHED REPAIR TO INBOARD FIXED TRAILING EDGE DEFLECTION CONTROL RIB UPPER TAB R/H WING PER SRM 57-51-02-2R-3 REPAIR 3. THIS IS A PERMANENT REPAIR NO FURTHER ACTION REQUIRED.SDR SWAA2021101228624Slide · missingCREW REPORTS FROWARD SERVICE DOOR EMERGENCY SLIDE FELL OUT ; / [01] REPACKED FS SLIDE PER MT725-61-06 AND AMM 25-66-01SDR SWAA2021100827412Girt Bar · out of adjustFA REPORTS FWD SERVICE DOOR GIRT BAR HARD TO INSERT AND RELEASE ; / [01] ADJUSTED GIRT BAR TENSION AS PER SIPSDR SWAA2021080900310Rub Strip · missingG-3 GALLEY LOWER COMPARTMENT RUB STRIP MISSING ; / [01] REMOVED RUB STRIP AT G-3 GALLEY FROM A/C 449 AND INSTALLED RUB STRIP AT G-3 GALLEY LOWER COMPARTMENT IN REF ENCORE CMM 25-31-04; [02] VERIFIEDSDR SWAA2021080598822Battery Pack · no testEMERGENCY LIGHTING BATTERY PACKS M1674 AND M1675 FAILED CAPACITY CHECK. ; / [01] REMOVED AND REPLACED BATTERIES PACK M1674 AND M1675 PER ACMM 33-51-06-960-805. GROUND TEST NORMAL.; [02] REMOVED AND REPLACED BATTERIES PACK M1674 AND M1675 PER ACMM 33-51-06-960-SDR SWAA2021080398824Battery Pack · no testEMERGENCY LIGHTING BATTERY PACK M1672 FAILED CAPACITY CHECK. ; / [01] REMOVED AND REPLACED BATTERY PACK M1672 PER ACMM 33-51-06-960-805. GROUND TEST NORMAL.; [02] REMOVED AND REPLACED BATTERY PACK M1672 PER ACMM 33-51-06-960-805. GROUND TEST NORMAL.; [03] VERISDR SWAA2021071995188Support · crackedAFT SUPPORT STRUCTURE TO PANEL 191AR HAS A CRACK . FAULT ACCOMPLISHED ON TASK TTG8Q005MC1R VERIFIED STEP 1.SDR SWAA2021080992262Web · crackedR/H HORIZONTAL STABILIZER L/E I/B PANEL 341A WEB CRACKED AND SEAL RETAINER IS BENT MKD DOT ; / [01] MEASUREMENTS; [02] REPAIRED R/H HORIZONTAL STABILIZER PANEL 341A SMALL .5 IN CRACK AND STRAITENED SEAL RETAINER AS PER B737 SRM 51-70-04-2R-10 MATERIALS USED POSDR SWAA2021080991783Nut Plate · brokenRIGHT WING FLAP TRACK # 6 FAIRING 642BB HAS 2EA BROKEN NUT PLATES @ FWD BULKHEAD MKD DOT ; / [01] REMOVED AND REPLACED BROKEN NUT PLATES AT RIGHT WING FLAP TRACK #6 IAW B737=7 SRM 51-40-02-0G-0; [02] VERIFIED STEP 1SDR SWAA2021080591774Bracket · crackedR-2 DOOR LOWER ACCESS PANEL # 844DZ HAS 2EA BRACKETS CRACKED MKD DOTS ; / [01] REMOVED 2EA BRACKETS FROM ACCESS PANEL 844DZ FOR R2 DOOR AS PER REF B737-7 SRM 51-40-02-0G-0 SECTION 4.; [02] VERIFIED REMOVAL OF 2 EA. BRACKETS FROM ACCESS PNL. 844DZ.; [03] LOCATESDR SWAA2021080591796Floor Panel · delaminatedAFT CABIN WET AREA FLOOR PANEL 241ZF TOP SURFACE DELAMINATED LAYERS ; / [01] REMOVED THE DAMAGED FACESHEET IN THE DAMAGED AREA AND PREPARED DAMAGED AREA TO APPLY THE REPAIR PLIES. REF B737-700 SRM 53-00-50-2R REPAIR 1.; [02] VERIFIED DAMAGE REMOVAL; [03] OK TOSDR SWAA2021080591801Floor Panel · delaminatedAFT CABIN FLOOR PANEL 242UF TOP SURFACE LAYERS DELAMINATED AT STA960 ; / [01] CLEANED DAMAGED AREA AND PREPARED FOR REPAIR AT PANEL 242UF AS PER B737-700 SRM 53-00-50-2R-1; [02] REPAIRED DAMAGED AREA AT PANEL 242UF AS PER B737-700 SRM 53-00-50-2R-1; [03] VERIFSDR SWAA2021080591804Floor Panel · delaminatedAFT CABIN FLOOR PANEL 241ABF TOP SURFACE LAYERS DELAMINATED AND NEED CLEANING ; / [01] CLEANED AT AFT CABIN FLOOR PANEL 241 ABF A PER B737 SRM 53-00-50 -2R-11; [02] VERIFIED STEP 1. OK TO APPLY REPAIR.; [03] REPAIRED AT AFT CABIN FLOOR PANEL 241ABF AS PER B 73SDR SWAA2021080591805Floor Panel · delaminatedAFT CABIN FLOOR PANEL 241XF TOP SURFACE LAYERS DELAMINATED STA 890 ; / [01] CLEANED AT AFT CABIN PANEL 241 XF AS PER B 53-00-50-2R-11; [02] VERIFIED STEP 1. OK TO APPLY REPAIR.; [03] REPAIRED AT AFT CABIN FLOOR PANEL 241 XF AS PER B737 SRM 53-00-50-2R-11; [04]SDR SWAA2021080591802Floor Panel · delaminatedAFT CABIN FLOOR PANEL 241ADF TOP LAYERS DELAMINATED STA 990 ; / [01] CLEANED AT AFT CABIN FLOOR PANEL 241 ADF SRM 53-00-50-2R-11; [02] VERIFIED STEP 1. OK TO APPLY REPAIR; [03] REPAIRED AT PANEL AFT CABIN FLOOR PANEL 241 ADF AS PER B 737 SRM 53-00-50-2R-11; [0SDR SWAA2021080591799Floor Panel · delaminatedMID CABIN FLOOR PANEL 241DF TOP LAYERS DELAMINATED STA 680 ; / [01] MEASUREMENTS; [02] CLEANED AND PREPARED PANEL 241DF FOR REPAIR AS PER B737 SRM 53-00-50-2R-1; [03] OK TO INSTALL<BR>AND VERIFIED STEP ONE AND TWO; [04] REPAIRED AT MID CABIN FLOOR PANEL241 DF SDR SWAA2021080591798Floor Panel · delaminatedAFT CABIN FLOOR PANEL 241YF TOP LAYERS DELAMINATED AT STA 890 ; / [01] CLEANED AT AFT CARGO FLOOR PANEL 241YF AS OR B 737 SRM. 53-00-50-2R-11; [02] VERIFIED STEP1. OK TO APPLY REPAIR; [03] REPAIRED AT AFT FLOOR PANEL 241YF AS PER B-737 SRM 53-00-50-2R-11; [04]SDR SWAA2021080591794Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 241AF TOP LAYERS DELAMINATED @ STA 960 ; / [01] MEASUREMENTS; [02] CLEANED AND PREPARED PANEL 241AF FOR REPAIR AS PER B737 SRM 53-00-50-2R-1; [03] OK TO INSTALL<BR>VERIFIED STEPS ONE AND TWO; [04] REPAIRED AT PANEL 241 AF AS PER B737-700SDR SWAA2021080591791Floor Panel · delaminatedFWD CABIN WET AREA FLOOR PANEL 221FF TOP SURFACE LAYERS DELAMINATED ; / [01] MEASUREMENTS; [02] CLEANED AND PREPARED PANEL 221FF FOR REPAIR AS PER B737 SRM 53-00-50-2R-1; [03] OK TO INSTALL<BR>VERIFIED STEPS ONE AND TWO; [04] REPAIRED AT PANEL 221FF AS PER B73SDR SWAA2021080591786Floor Panel · damagedFWD CABIN WET AREA FLOOR PANEL 222CF FWD I/B EDGE DAMAGED AT FASTENERS HOLES AND MISSING INSERTS ; PANEL NEED CLEANING ALSO . ; / [01] CLEANED AT PANEL 222CF AS PER B737 SRM 53-5-2R-1; [02] VERIFIED STEP #1.; [03] MEASUREMENTS; [04] REPAIRED PANEL AT TOP LAYERSDR SWAA2021080591795Floor Panel · delaminatedFWD CABIN R-1 DOOR ENTRY FLOOR PANEL 222BF TOP LAYERS SURFACE DELAMINATED ; / [01] CLEANED AT PANEL 222 BF AS PER B-737- 700 SRM 53-00-50-2R-1; [02] VERIFIED STEP #1.; [03] REPAIRED AT PANEL 222 BF AS PER B737 SRM 53-00-50-2R-1; [04] VERIFIED STEP #3.; [05] CLSDR SWAA2021080591790Floor Panel · delaminatedFWD CABIN FLOOR PANEL 231AF UPPER LAYERS DELAMINATED ; / [01] CLEANED PANEL 231AF AT AREA OF REPAIR AS PER B737-7 SRM 53-00-50-2R-1-A00939.; [02] VERIFIED STEP #1.; [03] REPAIRED AT PANEL 231AF AS PER B737 SRM 53-00-50-2R-1; [04] VERIFIED STEP #3.; [05] CLEANESDR SWAA2021080591789Floor Panel · delaminatedFWD CABIN WET AREA FLOOR PANEL # 221CF UPPER SURFACE DELAMINATED ; / [01] CLEANED AT FWD CABIN WET FOOD PANEL 221 CF AS PER B 737 SRM 53-00-50-2R-1; [02] VERIFIED STEP #1.; [03] REPAIRED AT PANEL 221CF AS PER B737 SRM 53-00-50-2R-1; [04] (RII) VERIFIED STEP #3SDR SWAA2021080591785Floor Panel · delaminatedFWD CABIN WET AREA FLOOR PANEL # 221EF UPPER LAYERS DELAMINATED ; / [01] CLEANED AT FDW CABIN FLOOR PANEL 221EF AS PER B737 SRM 53-00- 50 -2R-1; [02] VERIFIED STEP #1.; [03] REPAIRED AT PANEL 221EF AS PER B737 SRM 53-00-50-2R-1; [04] (RII) VERIFIED STEP #3.; [SDR SWAA2021080591800Floor Panel · delaminatedAFT CABIN FLOOR PANEL 242TF TOP LAYETS DELAMINATED AT STA 940 ; / [01] MEASUREMENTS; [02] CLEANED AND PREPARED PANEL 242TF FOR REPAIR AS PER B737 SRM 53-00-50-2R-1; [03] VERIFIED STEPS 1 & 2 <BR>OK TO INSTALL REPAIR; [04] INSTALLED REPAIR PLIES AT FLOOR PANEL SDR SWAA2021080591797Floor Panel · delaminatedAFT CABIN FLOOR PANEL TOP LAYERS DELAMINATED AT STA 1010 ; / [01] PREPARED DAMAGED AREA AND APLLIED REPAIR PLIES AT FLOOR PANEL 242 XF. REF B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [02] OK TO REPAIR; [03] INSTALLED REPAIR PLIES AT FLOOR PANEL 242 XF. REF B737-700SDR SWAA2021080591803Floor Panel · delaminatedAFT CABIN FLOOR PANEL 241AEF TOP LAYERS DELAMINATED AT STA 1010 ; / [01] MEASUREMENTS; [02] CLEANED AND PREPARED PANEL 241AEF FOR REPAIR AS PER B737 53-0-50-2R-1; [03] VERIFIED STEPS 1 & 2. <BR>OK TO INSTALL REPAIR; [04] REPAIRED PANEL 241EF AS PER B737 SRM 53SDR SWAA2021080991339Intercostal · crackedNO- 1 ENG I/B FAN COWL INNER INTERCOSTAL CRACKS @ ENG OIL ACCESS CUTOUT MKD DOT ; / [01] REMOVED AND REPLACED INNER INTERCOSTAL AT NO 1 ENGINE I/B FAN COWL AT ENG. OIL ACCESS CUTOUT. REF. BOEING 737-700 SRM 51-40-02-0G-0; [02] VERIFIED STEP 1SDR SWAA2021080591327Mount · crackedAFT CABIN L2 DOOR SLIDE PACK FWD MOUNT CRACKED @ CHOCK MOUNT BRACKETS. REMOVED AND REPLACED CHOCK MOUNT BRACKETS AT AFT CABIN L-2 DOOR SLIDE PACK FWD MOUNT P/N BACS14K2 PER B737-700 SRM 51-40-02-0G-0.SDR SWAA2021080990336Rib · crackedFOUND CRACK AT R/H HRZ STB.INSPAR #4 AT STB. STA 120.30 LOWER FLANGE ; / [01] REPAIR FOR CRACK FOUND AT LOWER FLANGE OF RT HORIZONTAL STAB RIB #4; WILL BE ACCOMPLISHED ON N/R REF TTG8Q005ME6A. GENERATED FOR THE REPAIR OF A CRACK ON STIFFENER #4. REPAIR REF; B7SDR SWAA2021080990345Angle · corrodedCORROSION. ** R/W REAR SPAR FIXED T/E LOWER SUPPORT ANGLE O/B OF FLAP TRACK # 8 ; / [01] REMOVER NUT PLATE FOR ACCESS AT R/W REAR SPAR FIXED T/E LOWER SUPPORT ANGLE IAW B737 SRM 51-40-02-0G -0.; [02] REMOVED CORROSION AT R/W REAR SPAR FIXED T/E LOWER SUPPORT ASDR SWAA2021080990344Angle · corrodedCORROSION. ** R/W REAR SPAR FIXED T/E LOWER SUPPORT ANGLE BETWEEN FLAP TRACK NO- 7 & 8 ; / [01] REMOVED NUT PLATE FOR ACCESS RE-WORK R/W REAR SPAR FIXED T/E LOWER SUPPORT ANGLE BETWEEN FLAP TRACK #7 AND 8 IAW B 737 SRM 51-40-02-0G-0.; [02] VERIFIED NUT PLATE RSDR SWAA2021080990339Fitting · crackedR/W FIXED T/E DEFLECTION CONTROL RIB PANEL VERTICAL SEAL FITTING CRACKED O/B SIDE UPPER MKD DOT ; / [01] REMOVED AND REPLACED RIGHT WING FIXED T/E DEFLECTION CONTROL RIB PANEL VERTICAL SEAL FITTING O/B UPPER SIDE IAW B 737-7 SRM 51-40-02-0G-0; [02] VERIFIED STSDR SWAA2021080590348Seat Track · damagedFLIGHT DECK FIRST OFFICER SEAT AFT O/B TRACK PIN HOLE IS ELONGATED ; / [01] REMOVED AND REPLACED O/B AFT FLIGHT DECK FIRST OFFICER'S SEAT TRACK PER BOEING 737-7 AAM 25-11-01-400-801-NG; [02] REMOVED AND REPLACED O/B AFT FLIGHT DECK FIRST OFFICER'S SEAT TRACK PSDR SWAA2021080990310Support Angle · crackedDORSAL FIN TERMINATION FITTINGS LOWER SECTION; SUPPORT ANGLE CRACKED 2EA PLACES BS 1016 RBL-11.5 AND LBL-11.5 MAD 126-20. ; / [01] PERFORMED HFEC INSP. ON SUSPECTED CRACK IAW B737 NDT PART 6; 51-00-00; PROCEDURE 23. CRACK CONFIRMED <BR>TOOL: NORTEC 600 B/C:166SDR SWAA2021080589700Support Angle · crackedSUPPORT ANGLE BETWEEN ACCESS PANELS 192E AND 192F CRACKED. REMOVED AND REPLACED SUPPORT ANGLE BETWEEN ACC. PANELS 192E TO 192F REF B-737-700-SRM 51-40-02-0G-0SDR SWAA2021080989261Nut Plate · damagedCABIN FLOOR WEB HAS SEVERAL NUT PLATES DAMAGED AT STA 1016; WL 208; LBL 45 TO RBL 45 ; / [01] INSTALLED NUT PLATES AT 13EA LOCATIONS AT STA 1016 BETWEEN LBL 45 AND RBL 45. AS PER B737-7 SRM 51-40-10-2R-0; [02] VERIFIED NUT PLATES INSTALLED
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