N210WN
Service difficulty reports · 268
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 = 'N210WN' 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 = 'N210WN' 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 SWAA2023022409284Intercostal · crackedFORWARD CARGO COMPARTMENT AIR CONDITIONING DISTRIBUTION BAY; FLOOR BEAM SUPPORT IS CRACKED. STATION 540 RIGHT OF BUTT LINE 0.<[01] REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02SDR SWAA2023022409283Intercostal · crackedFORWARD CARGO COMPARTMENT AIR CONDITIONING DISTRIBUTION BAY; FLOOR BEAM SUPPORT IS CRACKED. STATION 540 LEFT OF BUTT LINE 0.<[01] REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02SDR SWAA2022110166493Battery Pack · inoperativeSUPPLEMENTAL INFORMATION: PASSENGER CABIN SEVERAL EMERGENCY LIGHTS INOP. / [01] REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK AT POSITION M1672 AND RECONNECTED RIGHT FORWARD OVERWING EXIT SIGN AS PER REF B737 AMM 33-51-01-960-802; AMM 33-51-960-802. TEST SDR SWAA2022110166492Light · inoperativeR1 DOOR EMERGENCY EXTERIOR LIGHT INOP. / [01] RELAMPED R1 DOOR EMERGENCY EXTERIOR LIGHT AS PER REF B737 AMM 33-51-04-960-801. TEST OK.;[02] VERIFIED STEP 1.SDR SWAA2022110163276Scuff Plate · corrodedSCUFF PLATE FOUND CORRODED AT AFT CARGO FWD CUTOUT / [01] REMOVED AND REPLACED SCUFF PLATE AT AFT CARGO FWD CUTOUT AS PER B737-700 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1SDR SWAA2022110263272Fairing · crackedCRACK IN FLAP FAIRING 542BB LOWER AFT END. / [01] REMOVED AFT FLAP FAIRING END 542EB FOR COMP. REPAIR REF SRM 51-40-02.. BY ALEX # 17856;[02] VERIFIED 1;[03] PREPARED DAMAGED AREA AT FLAP FAIRING 542 BB ON LOWER SURFACE PER B737SRM<BR>51-70-04-2R-6;[04] VERIFISDR SWAA2022110259221Flap · delaminatedFOUND DELAMINATION (3' BY 3' APROX.) AT LH WING O/B AFT FLAP UPPER SURFACE LOCATED 1.0' FROM I/B EDGE AND 1.0' FROM T/E.NOTE: LOWER SURFACE HAS A PATCH. / [01] PERFORMED CUT OUT OF 3''X4'' AT LH WING O/B AFT FLAP UPPER SURFACE LOCATED 1.0' FROM I/B EDGE AND 1.SDR SWAA2022112173772Bracket · crackedL/T WING LOWER I/B T/E ACCESS PANEL # 551FB HAS 1 EA BRACKET CRACKED / [01] REMOVED AND REPLACED 1 EA. BRACKED PN. 287A9152-23 AT L/T WING LOWER I/B T/E ACCESS PANEL #551FB. REF. 51-40-02-0G-0-A00729.;[02] VERIFIED STEP 1 - REMOVED AND REPLACED BRACKETSDR SWAA2022110354879Structure · corrodedCORROSION SPOTS ON AFT WET AREA INNER CHORD UPPER SURFACE B.S.951-992.8 RBL. 45'-55' W.L. 208. (51-014) / [01] REMOVED CORROSION ON AFT WET AREA INNER CHORD UPPER SURFACE B.S 951-992.8 RBL 45'-55' WL 208 AS PER B737 SRM 51-10-02-0G-0-A00248;[02] VERIFIED STEP SDR SWAA2022110254871Strap · corrodedCORROSION SPOTS 0N AFT WET AREA FLOOR WEB AND STRAP B.S. 1016 TO AFT PRESSURE BLKHD. CENTER BL. TO LBL. 20' W.L. 208.(51-007) / [01] REMOVED LIGHT SURFACE CORROSION SPOTS ON AFT WET AREA FLOOR WEB AND STRAP B.S 1016 TO AFT PRESSURE BLKHD;[02] VERIFIED STEP #1.SDR SWAA2022110254874Floorbeam · corrodedCORROSION SPOTS ON AFT WET AREA FLOOR BEAM UPPER CAP B.S. 986.5 LBL 38'-44' W.L. 208.(51-010) / [01] FOUND AFT WET AREA FLOOR BEAM UPPER CAP B.S. 986.5 LBL. 38'-44' W.L.208. TO BE EXFOLIATED OUT OF LIMITS AS PER B737-700 SRM 53-70-51-1A-1;[02] CORRECTION: FOUNSDR SWAA2022110254875Support · corrodedCORROSION SPOTS ON AFT WET AREA FLOOR SUPPORT INNER CHORD UPPER SURFACE B.S 947.5 - 992.8 LBL. 45'-55' W.L. 208. (51-011) / [01] REMOVED CORROSION SPOTS ON AFT WET AREAS FLOOR SUPPORT INNER CHORD UPPER SURFACE B.S 947.5 -992.8 LBL. 45'-55' W.L. 208 AS PER B737SDR SWAA2022110254878Floorbeam · corrodedCORROSION SPOTS ON AFT WET AREA FLOOR BEAM UPPER CAP B.S. 986.5 RBL. 32'-45' W.L.208. (51-013) FOUND AFT WET AREA FLOOR BEAM UPPER CAP B.S. 986.5 RBL. 32'-45' W.L.208. TO BE EXFOLIATED OUT OF LIMITS IAW SRM 53-70-51-1A-1. AFT WET AREA REMOVED INTERCOSTAL AT SDR SWAA2022110152318Channel · corrodedAFT CARGO COMPARTMENT LEFT SIDE; FLOOR STRUCTURE 'Z CHANNEL'; AROUND HOLES HAS EVIDENCE CORROSION BETWEEN STA 727C TO 727D; WL 155.5; LBL-21. / [01] Z-CHANNEL (PN:146A7502-27) STA 727-847 REPLACED FOR WORK ACCOMPLISHED REFERENCE TASK CARD# TTG8Q00F6526;[02] VESDR SWAA2022110152330Channel · corrodedAFT CARGO COMPARTMENT LEFT SIDE; FLOOR STRUCTURE 'Z CHANNEL'; AROUND HOLES HAS EVIDENCE CORROSION BETWEEN STA 727D TO STA 727E; WL 155.5; LBL-21 / [01] Z-CHANNEL (PN:146A7502-27) STA 727-847 REPLACED FOR WORK ACCOMPLISHED REFERENCE TASK CARD# TTG8Q00F6526;[02]SDR SWAA2022110152331Channel · corrodedAFT CARGO COMPARTMENT LEFT SIDE; FLOOR STRUCTURE 'Z CHANNEL'; AROUND HOLES HAS EVIDENCE CORROSION BETWEEN STA 727E TO 747; WL 155.5; LBL-21 / [01] FOUND EXFOLIATED CORROSION AT AFT CARGO LH Z CHANNEL STA 727E TO 747 LBL21 OUT OF LIMITS PER REF SRM 51-10-02-0G-SDR SWAA2022110152332Channel · corrodedAFT CARGO COMPARTMENT LEFT SIDE; FLOOR STRUCTURE 'Z CHANNEL'; AROUND HOLES HAS EVIDENCE CORROSION BETWEEN STA 747 TO 767; WL 155.5; LBL-21 / [01] Z-CHANNEL (PN:146A7502-27) STA 727-847 REPLACED FOR WORK ACCOMPLISHED REFERENCE TASK CARD# TTG8Q00F6526;[02] VERIFSDR SWAA2022110152333Channel · corrodedAFT CARGO COMPARTMENT LEFT SIDE; FLOOR STRUCTURE 'Z CHANNEL'; AROUND HOLES HAS EVIDENCE CORROSION BETWEEN STA 767 TO 787; WL 155.5; LBL-21 / [01] Z-CHANNEL (PN:146A7502-27) STA 727-847 REPLACED FOR WORK ACCOMPLISHED REFERENCE TASK CARD# TTG8Q00F6526;[02] VERIFSDR SWAA2022110152334Channel · corrodedAFT CARGO COMPARTMENT LEFT SIDE; FLOOR STRUCTURE 'Z CHANNEL'; AROUND HOLES HAS EVIDENCE CORROSION BETWEEN STA 787 TO 807; WL 155.5; LBL-21 / [01] Z-CHANNEL (PN:146A7502-27) STA 727-847 REPLACED FOR WORK ACCOMPLISHED REFERENCE TASK CARD# TTG8Q00F6526;[02] VERIFSDR SWAA2022110152319Channel · corrodedAFT CARGO COMPARTMENT RIGHT SIDE; FLOOR STRUCTURE 'Z CHANNEL'; AROUND HOLES HAS EVIDENCE CORROSION BETWEEN STA 727B TO 727C; WL 155.5; RBL-21 / [01] Z-CHANNEL (PN:146A7502-51) STA 727-767 REPLACED FOR WORK ACCOMPLISHED REFERENCE TASK CARD# TTG8Q00F654H;[02] VESDR SWAA2022110152320Channel · corrodedAFT CARGO COMPARTMENT RIGHT SIDE; FLOOR STRUCTURE 'Z CHANNEL'; AROUND HOLES HAS EVIDENCE CORROSION BETWEEN STA 727C TO 727D; WL 155.5; RBL-21 / [01] Z-CHANNEL (PN:146A7502-51) STA 727-767 REPLACED FOR WORK ACCOMPLISHED REFERENCE TASK CARD# TTG8Q00F654H;[02] VESDR SWAA2022110152337Channel · corrodedAFT CARGO COMPARTMENT RIGHT SIDE; FLOOR STRUCTURE 'Z CHANNEL'; AROUND HOLES HAS EVIDENCE CORROSION BETWEEN STA 727D TO 727E; WL 155.5; RBL-21 / [01] Z-CHANNEL (PN:146A7502-51) STA 727-767 REPLACED FOR WORK ACCOMPLISHED REFERENCE TASK CARD# TTG8Q00F654H;[02] VESDR SWAA2022110152338Channel · corrodedAFT CARGO COMPARTMENT RIGHT SIDE; FLOOR STRUCTURE 'Z CHANNEL'; AROUND HOLES HAS EVIDENCE CORROSION BETWEEN STA 727E TO 747; WL 155.5; RBL-21 / [01] Z-CHANNEL (PN:146A7502-51) STA 727-767 REPLACED FOR WORK ACCOMPLISHED REFERENCE TASK CARD# TTG8Q00F654H;[02] VERSDR SWAA2022110152335Channel · corrodedAFT CARGO COMPARTMENT RIGHT SIDE; FLOOR STRUCTURE 'Z CHANNEL'; AROUND HOLES HAS EVIDENCE CORROSION BETWEEN STA 747 TO 767; WL 155.5; RBL-21 / [01] FOUND EXFOLIATED CORROSION AT <BR>AFT CARGO COMPARTMENT RIGHT SIDE; FLOOR STRUCTURE 'Z CHANNEL' STA 747 TO 767; WSDR SWAA2022110154873Strap · corrodedCORROSION SPOT ON AFT WET AREA LOWER SURFACE OF FLOOR SUPPORT AROUND FASTENER HOLE B.S. 1016 + 6' LBL 3' W.L. 208. (51-009) / [01] REMOVED STRAP CORRODED OUT LIMITE AT AFT WET AREA FLOOR SUPPORT CENTER AT B.S. 1016;[02] CORRECTION TO STEP 1: REMOVED STRAP CORRSDR SWAA2022110252307Intercostal · crackedFWD CABIN INTERCOSTAL BETWEEN STA 344 AND 360 LBL 11 WL 208.1 IS CRACKED. 124-012 / [01] PERFORMED HFEC INSPECTION PER B737 NDT PART 6 51-00-00 PROCEDURE 23; VERIFIED CRACK. CRACK LENGTH 0.750'. TOOL USED OLYMPUS NORTEC 600 B/C 172389; CAL DUE DATE 03/23.;[02]SDR SWAA2022110152296Intercostal · crackedFWD CABIN INTERCOSTAL BETWEEN STA 277 AND 294.5 BL-0 WL 208.1 IS CRACKED. 124-001 / [01] PERFORMED HFEC INSPECTION PER B737 NDT PART 6 51-00-00 PROCEDURE 23; VERIFIED CRACK. CRACK LENGTH 1.250'. TOOL USED OLYMPUS NORTEC 600 B/C 172389; CAL DUE DATE 03/23.;[02]SDR SWAA2022110152306Intercostal · crackedFWD CABIN INTERCOSTAL BETWEEN STA 344 AND 360 BL-0 WL 208.1 IS CRACKED. 124-011 / [01] PERFORMED HFEC INSPECTION PER B737 NDT PART 6 51-00-00 PROCEDURE 23; VERIFIED 2 CRACKS. CRACK LENGTHS ARE BOTH 0.750'. TOOL USED OLYMPUS NORTEC 600 B/C 172389; CAL DUE DATE SDR SWAA2022110152298Intercostal · crackedFWD CABIN INTERCOSTAL BETWEEN STA 328 AND 344 LBL 46 WL 208.1 IS CRACKED. 124-002 / [01] PERFORMED HFEC INSPECTION PER B737 NDT PART 6 51-00-00 PROCEDURE 23; VERIFIED CRACK. CRACK LENGTH 0.750'. TOOL USED OLYMPUS NORTEC 600 B/C 172389; CAL DUE DATE 03/23.;[02]SDR SWAA2022110152308Intercostal · crackedFWD CABIN INTERCOSTAL BETWEEN STA 344 AND 360 RBL 11 WL 208.1 IS CRACKED. 124-013 / [01] PERFORMED HFEC INSPECTION PER B737 NDT PART 6 51-00-00 PROCEDURE 23; VERIFIED CRACK. CRACK LENGTH 1.500'. TOOL USED OLYMPUS NORTEC 600 B/C 172389; CAL DUE DATE 03/23.;[02]SDR SWAA2022110152311Intercostal · crackedFWD CABIN INTERCOSTAL BETWEEN STA 380 AND 400 BL-0 WL 208.1 POSSIBLE CRACK AROUND CTR. FASTENER HOLE AS MARKED. 124-014 / [01] CRACK CONFIRMED IAW NDTM PART 6; 51-00-00 PROCEDURE 23. CRACK LENGTH : 0.250'<BR><BR>[NORTEC 600 ; B/C 166317 ; CALIB.DUE- 10/22];[02SDR SWAA2022110152312Intercostal · crackedFWD CABIN INTERCOSTAL BETWEEN STA 380 AND 400 LBL 13 WL 208.1 IS CRACKED. 124-015 / [01] CRACK CONFIRMED IAW NDTM PART 6; 51-00-00 PROCEDURE 23. CRACK LENGTH :0.500' <BR>[NORTEC 600 ; B/C 166317 ; CALIB.DUE- 10/22];[02] REMOVED UPPER ANGLE OF INTERCOSTAL BETWESDR SWAA2022110152309Intercostal · crackedFWD CABIN INTERCOSTAL BETWEEN STA 380 AND 400 RBL 8.5 WL 208.1 IS CRACKED. 124-016 / [01] CRACK CONFIRMED IAW NDTM PART 6; 51-00-00 PROCEDURE 23. CRACK LENGTH : 0.100'<BR>[NORTEC 600 ; B/C 166317 ; CALIB.DUE- 10/22];[02] REMOVED INERCOSTAL BETWEEN STA 380 TO SSDR SWAA2022110152327Channel · corrodedFWD CARGO COMPARTMENT RIGHT SIDE; FLOOR STRUCTURE 'Z CHANNEL'; AROUND HOLES HAS EVIDENCE CORROSION BETWEEN STA 500 TO 500A; WL 155.5; RBL-21. / [01] FOUND EXFOLIATED CORROSION OUT OF LIMITS AT FWD CARGO COMPARTMENT RIGHT SIDE; FLOOR STRUCTURE 'Z CHANNEL' BETWESDR SWAA2022102851674Light · missingG1 O/B EXIT SIGN COVER MISSING / [01] INSTALLED G1 O/B EXIT SIGN COVER PER CMM 25-31-03;[02] VERIFIED 1SDR SWAA2022110251248Flange · crackedFWD CABIN ABOVE L-1 DOOR UPPER SILL CUTOUT FWD FRAME FLANGE CUTOUT CRACKED @ STA 312 MKD DOT / [01] CLEANED AREA FOR EVALUATION AS PER SRM 51-10-02-0G-0;[02] PERFORMED HFEC INSP. AT FWD CABIN ABOVE L-1 DOOR UPPER SILL CUTOUT FWD FRAME FLANGE CUTOUT CRACKED @ SSDR SWAA2022110251247Seat Track · corrodedCORROSION MAIN CABIN SEAT TRACK EDGES & CROWN R/H O/B TRACK @ RBL 45.5 STA 706+5' MKD DOT / [01] REMOVED SURF. LIGHT CORROSION AT SEAT TRACK EDGES & CROWN R/H O/B TRACK STA. 706+5' RBL. 45.5' REF. SRM; 51-10-02;[02] VERIFIED STEP 1;[03] EVALUATED LIMITE AT MAISDR SWAA2022110349347Panel · delaminatedRT WING L/E PANEL 621QB IS DELAMINATED AS MARKLED. 124-006 / [01] PREPARED FOR REPAIR PANEL 621QB; AS PER B737-700 SRM 51-70-06-2R-6;[02] IN REF TO STEP 1; OK TO INSTALL REPAIR;[03] REPAIRED PANEL 621QB AS PER B737-700 SRM 51-70-06-2R-6 MATERIAL USED P/O# 1780SDR SWAA2022110349332Slat · delaminatedL/W MOVEABLE SLAT # 2 SLAT O/B MAIN TRACK L/E GAP FAIRING DISBONDED I/B EDGE MKD DOT / [01] PREPARED DAMAGED AREA TO APPLY REPAIR AT L\W #2SLAT ON MAIN TRACK L\E GAP FAIRING PER B737 SRM 51-70-06 2R-6;[02] VERIFIED STEP 1 - PREPARED DAMAGED AREA TO APPLY REPAISDR SWAA2022110347001Fitting · crackedRIGHT WING FIXED TRAILING EDGE DEFLECTION CONTROL RIB PANEL LOWER VERTICAL BULB SEAL FITTING CRACKED I/B SIDE / [01] REMOVED AND REPLACED BULB SEAL FITTING AT RT. WING T/E DEFECTION CONTROL RIB PANEL AS [PER B737-7 SRM 51-40-02-0G-0.;[02] VERIFIED 1SDR SWAA2022080235299Floor Panel · pulledCABIN FLOOR PANEL 231XF HAS PULLED FIBERS. / [01] EVALUATED AND FOUND DAMAGE TO UPPER SURFACE TO BE REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED UPPER SURFACE IAW SRM 53-00-50-2R-1 STEPS 3 A;C;E;F<BR>VERIFIED REPAIRSDR SWAA2022080235300Battery Pack · inoperativeEMERGENCY LIGHT BATTERY PACK M1674 WILL NOT HOLD A CHARGE / [01] REPLACED BATTERY PACK FOR M1674 IAW AMM 33-51-06-960-805. TESTS GOOD;[02] VERIFIED STEP 1 C/W; TEST PASSED; JOB COMPLETE; AUDIT C/WSDR SWAA2022080233814Stringer · crackedRIGHT WING UPPER SKIN AFT STRINGER END IS CRACKED BETWEEN RIB 19 AND 20. TRIMMED OUT CRACKED PORTION OF STRINGER END IAW SRM 51-10-02-0G. HFEC IAW NDT PART 6; 51-00-00 PROC 23 & 16; 53-30-00 PROC 5. NO DEFECTS NOTED. INSTALLED 3 EA. FASTNERS COMMON TO STRINGSDR SWAA2022080233815Stringer · crackedRIGHT WING UPPER SKIN AFT STRINGER END IS CRACKED BETWEEN RIB 21 AND 22. / [01] REMOVED 4 FASTENERS TO GAIN ACCESS I.A.W SRM 51-40-02-0G-0;[02] CUT OUT CRACKED AREA I.A.W SRM 51-10-02-0G-0;[03] VERIFIED ITEMS 1 AND 2;[04] HFEC IAW B737 NDT PART 6; 51-00-00 PROSDR SWAA2022080233084Floor Panel · delaminatedCABIN FLOOR PANEL 242BF IS SEPARATED ON THE EDGE. / [01] CABIN FLOOR PANEL 242BF REPAIRED ON NON-ROUTINE #TTG8Q00DROP7;[02] VERIFIED STEP 1SDR SWAA2022080232795Flap · debondedLH O/B AFT FLAP LOWER SKIN AT I/B CORNER HAS AN AREA OF DISBOND. / [01] BOND TEST IAW B737 NDT PART 4; 51-00-05. DISBONDED AREA MARKED IN BLACK. TOOL#40082; DUE 11OCT22;[02] EVALUATED AND FOUND DISBOND AS MARKED. FOUND TO BE REPAIRABLE IAW SRM 57-53-01-2R-4 STSDR SWAA2022080233081Floorboard · pulledFLOORBOARD 241AF HAS PULLED FIBERS. / [01] EVALUATED AND FOUND DAMAGE TO UPPER SURFACE TO BE REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED UPPER SURFACE IAW SRM 53-00-50-2R-1 STEPS 3 A;C;E;F<BR>VERIFIED REPAIR MATERISDR SWAA2022080233082Floor Panel · delaminatedCABIN FLOOR PANEL 241CF IS DELAMINATED. / [01] EVALUATED AND FOUND MISSING PLIES AT FWD EDGE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP 3 A; C; E-F.<BR><BR>VERIFIED MATSDR SWAA2022080233083Floor Panel · delaminatedCABIN FLOOR PANEL 242BF IS SEPARATED ON THE EDGE. / [01] EVALUATED DAMAGE; SKIN SEPARATION ON EDGE IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1.<BR><BR>VERIFIED REPAIR MATERIALS IAW B737 SRM 53-00-50-2R-1 TABLE 201; FIBERGLASS CLOTH BMS9-3 (A24484); POTTING COMPOUSDR SWAA2022080233085Floor Panel · delaminatedCABIN FLOOR PANEL 232SF IS SEPARATED ON THE EDGE. / [01] EVALUATED PANEL 232 SF AND FOUND DAMAGE TO CORE AT EDGE AT TWO CORNERS. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-10 PAR 1. CLEAN AND PREP FOR REPAIR. IAW B737-700 SRM 53-00-50-2R-10 PAR 3A-D.
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