N485WN
Service difficulty reports · 330
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 = 'N485WN' 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 = 'N485WN' 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 SWAA2022072827078Baffle · crackedFWD CARGO COMPARTMENT BAFFLE LBL 24 CRACKED. STA 500-500A WL-156.4 / [01] REMOVED AND REPLACED BAFFLE AT STA 500-500A LBL 24 PER SRM 51-40-02-0G-0 AND DWG 143A7505;[02] VERIFIED 1SDR SWAA2022072826892Channel · crackedFOUND EXFOLIATION CORROSION AT AFT./ CARGO Z-CHANNEL AROUND FASTENER HOLES BETWEEN STA. 727E PLUS 4' BACK TO STA. 747 . LBL 21 ; WL 155. / [01] FABRICATED NEW Z CHANNEL SECTION FROM STA 727E TO STA 847 AT AFT CARGO COMPT LBL 21 WL 155 PER REF B737-700 SRM 53-0SDR SWAA2022072827079Shield · corroded*****CORROSION***** FWD CARGO COMPARTMENT RBL 24 AFT SHIELD HAS CORROSION. WL156.4 / [01] FOUND EXFOLIATING CORROSION AT PIECE; SHIELD FOUND OUT OF LIMIS AT FWD CARGO COMPT PER REF B737-7 SRM 51-10-02-0G-0.;[02] RECEIVED NEW SHIELD (P/N: 143A8126-31). REF TASKSDR SWAA2022072925540Stringer · out of toleranceWHILE PERFORMING A VISUAL INSPECTION ON TTG8Q00DAZFC STEP 8; FOUND 2EA FWD HOLES ON THE STRINGER WITHIN THE CUTOUT SECTION OF THE SKIN. LARGER THAN THE STANDARD SIZE / [01] FWD HOLE DIA. MEASURED: 0.200'; AFT HOLE DIA. MEASURED: 0.233'<BR><BR>TOOL USED B/C 174SDR SWAA2022072825539Fitting · crackedDURING REMOVAL OF FWD LT SIDE AIR SUPPLY ELBOW DUCT I/B OF KRUEGER FLAP FWD WTB SUPPORT STRUCTURE CRACKED. / [01] REMOVED IB FWD ANGLE AND IB FITTING OF FRONT SPAR TO GAIN ACCESS AS PER B737-700 SRM 51-40-02-0G-0;[02] REMOVED CRACKED FWD WTB FITTING LH WING IBSDR SWAA2022072825435Bracket · elongatedPANEL 651GB I/B AFT BRACKET ELONGATED HOLE / [01] REMOVED AND REPLACE BRACKET PER SRM 51-40-02-0G-0 AT PANEL 651GB;[02] VERIFIED 1SDR SWAA2022072824850Bracket · cracked#1 ENG OB FAN COWL AFT OPEN ROD RECEIVER BRACKET IS CRACKED / [01] INSTALLED RECEIVER /BRACKET IN ACCORDANCE TO REF51-40-02-0G.;[02] VERIFIED 1SDR SWAA2022072824337Panel · crackedRT WING LOWER MID SPAN T/E PANEL 661BB AT SEAL ATTACHMENT FLANGE HAS MULTIPLE FASTENER HOLES BULGING SOME WITH CRACKS AS VIEWED FROM INNER SKIN. / [01] PREPARED AREA FOR REPAIR MULTIPLE FASTERNER HOLES CRACKS AT RT WING LOWER PANEL #661BB AS PER B737 SRM 51-70SDR SWAA2022072823739Light · crackedEXIT SIGN AT FWD GALLEY G1 BASE IS CRACKED / [01] REMOVED AND REPLACED EXIT SIGN AT FWD GALLEY G1 BASE REF: 33-51-01-960-802.;[02] VERIFIED 1SDR SWAA2022072823738Floorbeam · corroded*CORROSION* AFT CABIN FLOORBEAM STA 986.5 LBL 47 TO LBL 48 WL 208.1 HAS CORROSION AROUND 1EA FASTENER HOLE / [01] REMOVED CORROSION ON FLOORBEAM STA 986.5 LBL 47 WL 208.1 AS PER B737-700 SRM 51-10-02-0G-0[21] REMOVED CORROSION ON FLOORBEAM STA 986.5 LBL 47 WL SDR SWAA2022072822773Floor Panel · corrodedAFT CABIN CENTER FLOOR PANEL 241AAF HAS 6EA CORRODED INSERTS AS MARKED. 124-038 / [01] PANEL IS OUT OF LIMIT AS PER B737 SRM 53-00-50-2R-1;[02] RECEIVED NEW PANEL 147A5810-8 PO#1772343;[03] REF. TASK CARD TTG8Q00CS130 FOR FLOOR PANEL INSTALLATION;[04] VERIFIEDSDR SWAA2022072822771Floor Panel · corrodedAFT CABIN FLOOR PANEL 242WF HAS 3EA CORRODED INSERTS ; 1EA MISSING INSERT ; AND IS DAMGED AS MARKED. 124-036 / [01] PANEL IS OUT OF LIMIT AS PER B737 SRM 53-00-50-2R-1;[02] RECEIVED NEW CABIN FLOOR PANEL 242WF (P/N: 147A5810-10). REF TASK CARD: TTG8Q00CS27C FOSDR SWAA2022072822770Floor Panel · corrodedAFT CABIN FLOOR PANEL 242VF HAS 3EA CORRODED INSERTS AS MARKED. 124-035 / [01] PANEL IS OUT OF LIMIT AS PER B737 SRM 53-00-50-2R-1;[02] RECEIVED NEW CABIN FLOOR PANEL 242VF (P/N: 147A5810-350). REF TASK CARD: TTG8Q00CS27E FOR PANEL INSTALLATION.;[03] VERIFIED SDR SWAA2022072822614Intercostal · crackedFWD CABIN BETWEEN STA 380 AND STA 400 INTERCOSTAL AT LBL 13 WL 208.1 IS CRACKED AS MARKED. 124-019 DOT 124-020 / [01] PLACED EWIZ PROTECTION UNDER MAIN CABIN FLOOR BETWEEN STA 380 AND STA 400 LBL 13 PER B737-700 AMM 20-60-07-913-801.;[02] VERIFIED 1;[03] REMOVSDR SWAA2022072822613Intercostal · crackedFWD CABIN BETWEEN STA 380 AND STA 400 INTERCOSTAL AT BL 0 WL 208.1 IS CRACKED AS MARKED. 124-019 / [01] PLACED EWIZ PROTECTION UNDER MAIN CABIN FLOOR BETWEEN STA 380 AND STA 400 BL 0 PER B737-700 AMM 20-60-07-913-801.;[02] VERIFIED 1;[03] REMOVED CRACKED INTERSDR SWAA2022072822615Intercostal · crackedFWD CABIN BETWEEN STA 380 AND STA 400 INTERCOSTAL AT RBL 8.5 WL 208.1 IS CRACKED AS MARKED. 124-021 / [01] PLACED EWIZ PROTECTION UNDER MAIN CABIN FLOOR BETWEEN STA 380 AND STA 400 RBL 8.5 PER B737-700 AMM 20-60-07-913-801.;[02] VERIFIED 1;[03] REMOVED CRACKEDSDR SWAA2022072822778Floor Panel · corrodedAFT CABIN FLOOR PANEL 242UF HAS 13 CORRODED INSERTS AS MARKED. 124-041 / [01] PANEL IS OUT OF LIMIT AS PER B737 SRM 53-00-50-2R-1;[02] VOID STEP 1. STEP WRITTEN IN ERROR.;[03] REMOVED AND REPLACED DAMAGED INSERTS AT FWD CABIN FLOOR PANEL 242UF AS PER BAC5085;[SDR SWAA2022072822779Floor Panel · corrodedAFT CABIN FLOOR PANEL 242TF HAS 5EA CORRODED INSERTS AND 1EA INSERT MISSING WITH HOLE BROKEN OUT AS MARKED. 124-042 / [01] PANEL IS OUT OF LIMIT AS PER B737 SRM 53-00-50-2R-1;[02] RECEIVED NEW PANEL AND INSTALL WITH CLOSING CARD TTG8Q00CS27J;[03] VERIFIED 1 & SDR SWAA2022072822898Floor Panel · corrodedAFT CABIN FLOOR PANEL 241ABF HAS 10EA CORRODED INSERTS AND 2EA BROKEN OUT INSERTS. 124-048 / [01] PANEL IS OUT OF LIMIT AS PER B737 SRM 53-00-50-2R-1;[02] RECEIVED NEW CABIN FLOOR PANEL 241ABF (P/N: 147A5810-88). REF TASK CARD: TTG8Q00CS12Y FOR PANEL INSTALLATSDR SWAA2022072822899Floor Panel · corrodedAFT CABIN FLOOR PANEL 241ADF HAS 15EA CORRODED INSERTS AND 2EA BROKEN OUT INSERTS. 124-049 / [01] PANEL IS OUT OF LIMIT AS PER B737 SRM 53-00-50-2R-1;[02] RECEIVED NEW PANEL AND INSTALLED UNDER CLOSING CARD TTG8Q00CS12U;[03] VERIFIED 1 & 2SDR SWAA2022072822897Floor Panel · corrodedAFT CABIN FLOOR PANEL 241ACF HAS 4EA CORRODED INSERTS AND 1EA BROKEN OUT INSERT. 124-050 / [01] PANEL IS OUT OF LIMIT AS PER B737 SRM 53-00-50-2R-1;[02] RECEIVED NEW CABIN FLOOR PANEL 241ACF (P/N: 147A5810-13). REF TASK CARD: TTG8Q00CS12W FOR PANEL INSTALLATIOSDR SWAA2022072822760Floor Panel · peelingFWD CABIN FLOOR PANEL 232AF HAS PEELED UPPER SURFACE FIBERS. 124-022 / [01] RECEIVED NEW FLOOR PANEL 232AF PO#1777513 P/N: 141A5810-167 REF. TASK CARD TTG8Q00CS14V FOR PANEL INSTALLATION;[02] VERIFIED STEP 1SDR SWAA2022072822758Floor Panel · deterioratedFWD CABIN FLOOR PANEL 231AF UPPER SURFACE LAYER IS DETERIORATING AND FIBERS ARE PEELED. 124-023 / [01] PREPARED AREA FOR REPAIR UPPER SURFACE LAYER IS DETERIORATING AND FIBERS ARE PEELED AT FWD CABIN FLOOR PANEL #231AF AS PER B737 SRM 53-00-50-2R-1;[02] VERIFISDR SWAA2022072822763Floor Panel · peelingAFT CABIN CENTER FLOOR PANEL 241UF HAS A MISSING INSERT AT CENTER AREA AS MARKED AND UPPER SURFACE FIBERS ARE PEELED. 124-025 / [01] FABRICATED PANEL #241UF AT AFT CABIN CENTER AS PER BOEING DWG 146A5810-54;[02] VERIFIED 1;[03] AFT CABIN CENTER FLOOR PANEL 241SDR SWAA2022072822764Floor Panel · corrodedAFT CABIN FLOOR PANEL 241AEF HAS 2EA CORRODED INERTS AS MARKED . 124-028 / [01] PANEL IS OUT OF LIMIT AS PER B737 SRM 53-00-50-2R-1;[02] RECEIVED NEW CABIN FLOOR PANEL 241AEF (P/N: 147A5810-351). REF TASK CARD: TTG8Q00CS12C FOR PANEL INSTALLATION.;[03] VERIFIESDR SWAA2022072822775Web · corroded*CORROSION* AFT CABIN LT SIDE FROM STA 1016 TO AFT PRESSURE BULKHEAD WL 208.1 FLOOR WEB HAS CORROSION AS MARKED. 124-029 / [01] REMOVED CORROSION AT AFT CABIN LT SIDE FROM STA 1016 TO AFT PRESSURE BULKHEAD WL 208.1 FLOOR WEB AS PER B737-700 SRM 51-10-02-0G-0. SDR SWAA2022072822765Strap · corroded*CORROSION* AFT CABIN STA 1016 TO STA 1016+13 FLOOR STRAP AT LBL 3 HAS CORROSION AS MARKED. 124-030 / [01] REMOVED CORROSION AT AFT CABIN STA 1016 TO STA 1016+13 FLOOR STRAP AT LBL 3 AS PER B737-700 SRM 51-10-02-0G-0. EVALUATED AREA; CORROSION PAS THRU;100% MASDR SWAA2022072822759Floor Panel · peelingMID CABIN FLOOR PANEL 241AF HAS UPPER SURFACE LAYER PEELED OFF AT LT O/B SIDE. 124-024 / [01] FABRICATED PANEL #241AF AT AFT CABIN CENTER AS PER BOEING DWG 144A5810-127;[02] FABRICATED PANEL #241AF AT MAIN CABIN CENTER AS PER BOEING DWG 144A5810-127;[03] VERIFSDR SWAA2022072822514Intercostal · crackedFWD CABIN BETWEEN STA 328 AND STA 344 LBL 46 WL 208.1 INTERCOSTAL IS CRACKED. 124-002 / [01] REMOVED INTERCOSTAL CRACKED PER SRM 51-40-02-0G-0 AT LBL 46 STA 328 T0 STA 344 WL 208.1;[02] LOCATED AND DRILLED NEW INTERCOSTAL AT STA 328 TO 344 LBL 46 PER SRM 51-40SDR SWAA2022072822517Floor Panel · brokenFWD CABIN FLOOR PANEL 221BF AFT O/B CORNER HAS A PIECE BROKEN OFF. 124-007 / [01] PANEL IS OUT OF LIMIT AS PER B737 SRM 53-00-50-2R-1;[02] RECEIVED NEW PANEL AND INSTALLED WITH CLOSING CARD TTG8Q00CS28U;[03] VERIFIED 1 & 2SDR SWAA2022072822612Retaining Clip · looseFOUND L-1 DOOR FWD RETAINER CLIP ATTACHING FASTENER BROKEN; RETAINER CLIP LOOSE. FOUND L-1 DOOR SLIDE FWD GIRT BAR RETAINER CLIP ATTACHING FASTENER BROKEN RETAINER CLIP LOOSE / [01] REMOVED AND REPLACED L-1 DOOR SLIDE FWD GIRT BAR RETAINER CLIP ATTACHING FASTESDR SWAA2022072822521Floor Panel · corrodedFWD CABIN FLOOR PANEL 221DF HAS 9EA CORRODED INSERTS AND UPPER SURFACE FIBER LAYER PEELED OFF AT I/B ENG AS MARKED. 124-008 / [01] PANEL IS OUT OF LIMIT AS PER B737 SRM 53-00-50-2R-1;[02] RECEIVED NEW CABIN FLOOR PANEL 221DF (P/N: 147A5810-59). REF TASK CARD: SDR SWAA2022072822524Intercostal · crackedFWD CABIN BETWEEN STA 294.5 AND STA 312 RBL 15 WL 208.1 INTERCOSTAL IS CRACKED AS MARKED. 124-011 / [01] PERFORMED HFEC INSP. ON FWD CABIN BETWEEN STA 294.5 AND STA 312 RBL 15 WL 208.1 INTERCOSTAL IAW B737 NDT PART 6 51-00-00 PROC. 23. CRACKS CONFIRMED. LENGTHSDR SWAA2022072822605Floor Panel · peelingCABIN FLOOR PANEL 222DF HAS PEELED UPPER SURFACE FIBERS. 124-012 / [01] PANEL IS OUT OF LIMIT AS PER B737 SRM 53-00-50-2R-1;[02] RECEIVED NEW CABIN FLOOR PANEL 222DF (P/N: 141A5810-1850. REF TASK CARD: TTG8Q00CS28A FOR PANEL INSTALLATION.;[03] VERIFIED STEP 1 SDR SWAA2022072822606Floor Panel · peelingFWD CABIN FLOOR PANEL 222CF HAS PEELED UPPER SURFACE FIBERS. 124-013 / [01] PANEL IS OUT OF LIMIT AS PER B737 SRM 53-00-50-2R-1;[02] NEW PANEL RECEIVED AND INSTALLED ON CLOSING CARD TTG8Q00CS28C;[03] VERIFIED 1 & 2SDR SWAA2022072822607Intercostal · crackedFWD CABIN BETWEEN STA 344 AND STA 360 INTERCOSTAL AT BL 0 WL 208.1 IS CRACKED AS MARKED. 124-014 / [01] PART REPLACED WITH NEW INTERCOSTAL P/N 141A5410U23 PER SRM 51-10-02-0G-0 PARAGRAPH 9 INSTALLATION WILL BE ACCOMPLISH ON TTG8Q00DDE9P;[02] VERIFIED 1SDR SWAA2022072822602Intercostal · crackedFWD CABIN BETWEEN STA 344 AND STA 360 INTERCOSTAL AT LBL 11 WL 208.1 IS CRACKED AS MARKED. 124-015 / [01] PART REPLACED WITH NEW INTERCOSTAL P/N 141A5410U148 PER SRM 51-10-02-0G-0 PARAGRAPH 9 INSTALLATION WILL BE ACCOMPLISH ON TTG8Q00DDE9P;[02] VERIFIED 1SDR SWAA2022072822608Floor Support · corroded*CORROSION* FWD CABIN FLOOR SUPPORT BEAM STA 344 HAS CORROSION AROUND HI-LOCK FASTENER AT BL 0 AND AROUND FASTENER HOLE AT LBL 9. 124-016 / [01] REMOVED CORROSION FROM FWD CABIN FLOOR SUPPORT BEAM STA 344 AROUND HI-LOCK FASTENER AND FASTENER HOLE LBL 9. PER SRSDR SWAA2022072827072Fastener · shearedSEE TASK TTG8Q001YGN6 : PAX CABIN SEAT TRACK AT RBL-24.75 AND STA 727B FASTENER LOCATION 'B' WITH SHEARED HEAD / [01] REMOVED AND REPLACED FASTENER AT RBL 24.75 STA 727B LOCATION 'B' PER EA-22-153-01872-WIP 1;[02] 'REPAIR ACCOMPLISHED PER EA 22-153-01872. REFESDR SWAA2022072826891Fastener · shearedSEE TASK TTG8Q001YGN6 : PAX CABIN SEAT TRACK AT LBL-45.5 AND STA 727B FASTENER LOCATION 'B' WITH SHEARED HEAD / [01] REMOVED AND REPLACED FASTENER AT LBL 45.5 STA 727B LOCATIO 'B' PER EA 22-153-01872-WIP1;[02] VERIFIED 1SDR SWAA2022072821729Stub Frame · crackedR-1 DOOR FWD FRAME UPPER STUB FRAME HAS A CRACK / [01] PLACED EWIS PROTECTION AROUND R-1 DOOR AREA PER B737-700 AMM 20-60-07-913-801.;[02] VARIFIED STEP 1;[03] APPLIED PAINT STRIPING TO OUTER FUSELAGE SKIN AT R-1 DOOR FWD FRAME PER B737-700 AMM 51-21-11-150-80SDR SWAA2022072820723Slide · out of positionL1 DOOR SLIDE ASSY LAP BRUSH THE CABIN FLOOR / [01] REPOSITIONED L-1 DOOR SLIDE ASSY LAP (SKIRT) IN REF TO MT 725-61-06. LAP (SKIRT) NO LONGER BRUSHES AGAINST CABIN FLOOR.;[02] [FINAL] VALIDATED STEP 1SDR SWAA2022072820717Vapor Barrier · crackedLEFT W/W VERTICAL VAPOR BARRIER CRACKED / [01] MEASUREMENTS;[02] CLEANED AND PREPARED DAMAGE AREA FOR REPAIR; STOP DRILL CRACKS; AND PERFORMED DRY OUT; FOUND NO WATER AS PER B737 SRM 51-70-04-2R-10;[03] VERIFIED STEP #1 AND #2;[04] OK TO INSTALL REPAIR;[05] RESDR SWAA2022012462366Panel · elongatedPANEL 194E HAS SEVERAL ELONGATED HOLES. / [01] R&R PANEL 194E PER AMM 53-51-21SDR SWAA2021122053483Angle · crackedSUPPLEMENTAL INFORMATION: BS 663; RBL 33; WL 194; .200' CRACK AT FASTENER HOLE ON 663 BULKHEAD TO CENTER WING BOX UPPER SKIN ATTACH ANGLE; END OF CRACK MARKED IN BLACK. ; / [01] CUT AND REMOVED DAMAGE IAW SRM 57-10-10-2R-6 REPAIR 6; [02] -1 FILLER MATERIAL VERSDR SWAA2021122053188Angle · crackedLT A/C BAY BS 663, LBL 8, LOWER FUEL TANK ANGLE COMMON THE VAPOR BARRIER IS CRACKED AT FASTENER JUST OUTBD OF LH KEELBEAM. REPLACEMENT ANGLE FABRICATED IAW W/O 43057-5000-0001. SPLICE ANGLE FABRICATED ON W/O 43057-5000-0002, REPLACEMENT ANGLE TO BE .063' 20SDR SWAA2021122052303Angle · crackedFOUND CRACK ON LOWER ATTACH ANGLE AT STA 663 FROM RBL 45-50. COMPLETED INSTALLATION OF REPAIR ANGLES IAW 21-157-03728-WIP1.SDR SWAA2021120249381Handle · brokenL1 DOOR ASSIST HANDLE BROKEN ; L1 DOOR ASSIST HANDLE ROKEN / [01] R&R L1 DOOR ASSIST HANDLE PER AMM 52-11-31SDR SWAA2021120249371Handle · missingFWD CARGO DOOR ASSIST LANYARD ASSY IS MISSING MULTIPLE COMPONENTS. ; FWD CARGO DOOR ASSIST LANYARD ASSY IS MISSING MLTIPLE COMPONENTS. / [01] R&R FWD CARGO DOOR ASSIST LANYARD ASSEMBLY PER AMM 52-31-00.SDR SWAA2021120249376Lanyard · missingAFT CARGO DOOR ASSIST LANYARD IS MISSING SOME COMPONENTS. / [01] R&R AFT CARGO DOOR ASSIST LANYARD ASSEMBLY PER AMM 52-31-00.
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