N295WN
Service difficulty reports · 291
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 = 'N295WN' 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 = 'N295WN' 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 SWAA2024032165628Handle · looseAFT PASSENGER DOOR HANDLE LOOSE<[01] RE SECURED AFT PASSENGER DOOR HANDLE REF AMM 52-13-31.SDR SWAA2023062771240Battery Pack · inoperativeEMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1674 INOP<[01] REMOVED AND REPLACED M1674 BATTERY PACK WITH SERVICEABLE UNIT AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION #1.SDR SWAA2023062861125Light · damagedFWD LAV AFT WALL OUTBOARD LOWER EMERGENCY EXIT LIGHT ASSY IS DAMAGED.<[01] REMOVED AND REPLACED DAMAGED EMERGENCY EXIT LIGHT ASSEMBLY ON FWD LAV AFT WALL IAW AMM 33-51-01-960-802 3.C. (2-3)(5)(D)(6-7)(10) OPS CHECK GOOD;[02] VERIFIED CORRECTION ACTION ITEM 1.;SDR SWAA2023070355791Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK BS500C+9 LBL45 WL208.<[01] VERIFIED THAT SRM 53-00-52-1A-1 IS APPLICABLE.;[02] UPDATED MEASUREMENT TABLE.;[03] SEAT TRACK BEING REPLACED ON CUSTOMER CARD # TTG8Q00LF7RU. UPDATED MEASUREMENT TABLE.;[04] VERIFIED CORRECTIOSDR SWAA2023070355793Strap · corrodedCORROSION ON STRAP AT MID CABIN BS703 LBL65 WL203.<[01] REMOVED CORROSION ON MID CABIN AT BS 703; LBL 65; WL 203; IN <BR> AN AREA OF 0.6'X0.9'IAW SRM 51-10-02-0G-0;[02] UPDATED STEP 1;[03] INSPECTED AND VERIFIED CORRECTIVE ACTION 1.;[04] COMPLETED STEPS 2-4.;[SDR SWAA2023070355797Strap · corrodedCORROSION ON STRAP AT MID CABIN BS703 RBL67 WL203.<[01] REMOVED CORROSION ON MID CABIN AT BS 703; RBL 65; WL 203; IN <BR> AN AREA OF 0.5'X0.9'IAW SRM 51-10-02-0G-0;[02] REMOVED CORROSION ON MID CABIN AT BS 703; RBL 65; WL 203; IN <BR> AN AREA OF 0.5'X0.9' AND SDR SWAA2023070355799Strap · corrodedCORROSION ON STRAP AT MID CABIN BS708 RBL66 WL203.<[01] REMOVED CORROSION ON MID CABIN AT BS 708 RBL 65; WL 203; IN <BR> AN AREA OF 0.6'X1.1' AND 0.5'X0.8'IAW SRM 51-10-02-0G-0;[02] UPDATED STEP 1;[03] REMOVED CORROSION ON MID CABIN AT BS 708 RBL 65; WL 203; ISDR SWAA2023070355785Strap · corrodedCORROSION ON STRAP AT MID CABIN BS713 RBL66 WL203.<[01] REMOVED CORROSION ON MID CABIN AT BS 713 RBL 65; WL 203; IN<BR> AN AREA OF 0.5'X1.2'AND 0.5'X1'IAW SRM 51-10-02-0G-0;[02] UPDATED STEP 1;[03] INSPECTED AND VERIFIED CORRECTIVE ACTION 1.;[04] COMPLETED STESDR SWAA2023070355801Web · corrodedCORROSION ON WEB AT MID CABIN BS711 RBL64 WL203.<[01] REMOVED CORROSION ON MID CABIN WEB AT BS 711 RBL 64; WL 203; IN<BR> AN AREA OF 0.5'X0.8'IAW SRM 51-10-02-0G-0;[02] CORRECTED MEASUREMENT TABLE;[03] INSPECTED AND VERIFIED CORRECTIVE ACTION 1.;[04] COMPLETEDSDR SWAA2023070355795Strap · corrodedCORROSION ON STRAP AT MID CABIN BS707 LBL65 WL203.<[01] REMOVED CORROSION ON MID CABIN AT BS 707; LBL 65; WL 203; IN <BR> AN AREA OF 0.4'X1.7'IAW SRM 51-10-02-0G-0;[02] UPDATED STEP 1;[03] INSPECTED AND VERIFIED CORRECTIVE ACTION 1.;[04] COMPLETED STEPS 2;3;4.SDR SWAA2023070355803Panel · crackedCRACKED PANEL BREAK AT MID CABIN BS540 LBL1 WL208.<[01] REMOVED PANEL BREAK AT MID CABIN BS 540; LBL 1 TO LBL 45; WL 208 IAW SRM 51-40-02-0G-0.;[02] REMOVED PANEL BREAK AT MID CABIN BS 540; LBL 1 TO LBL 24; WL 208 IAW SRM 51-40-02-0G-0.<BR>LOCATED AND DRILLED SDR SWAA2023070355805Panel · crackedCRACKED PANEL BREAK AT MID CABIN BS540 RBL1 WL208.<[01] COMPLETED MEASUREMENT TABLE.<BR>REMOVED PANEL BREAK AT MID CABIN BS 540; RBL1 TO RBL 24; WL 208 IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW BREAK ASSY PANEL IAW SRM 51-40-05-0G-0.<BR>REQ. OK TO INSTALLSDR SWAA2023070355787Panel · crackedCRACKED PANEL BREAK AT MID CABIN BS540 LBL26 WL208.<[01] REMOVED PANEL BREAK AT MID CABIN BS 540 LBL 26 TO LBL 45; WL 208 IAW SRM 51-40-02-0G-0.;[02] VERIFIED CORRECTION ACTION ITEM1.;[03] LOCATED AND DRILLED NEW PANEL BREAK P/N 143A5240-32 AT MID CABIN BS 540SDR SWAA2023062955789Stringer · crackedCRACKED STRINGER CLIP AT PASSENGER CABIN BS727E S-5R.<[01] REMOVED STRINGER CLIP AT PASSENGER CABIN BS727E S-5R IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW STRINGER CLIP AT PASSENGER CABIN BS727E S-5R IAW SRM 51-40-05-0G-0 AND DWG 146A1112. OK TO INSTALSDR SWAA2023062955807Stringer · crackedCRACKED STRINGER CLIP AT PASSENGER CABIN BS727D S-6R.<[01] REMOVED STRINGER CLIP AT PASSENGER CABIN BS727D S-6R IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW STRINGER CLIP AT PASSENGER CABIN BS727D S-6R IAW SRM 51-40-05-0G-0 AND DWG 146A1111. OK TO INSTALSDR SWAA2023062955809Stringer · crackedCRACKED STRINGER CLIP AT PASSENGER CABIN BS727C S-5R.<[01] REMOVED STRINGER CLIP AT PASSENGER CABIN BS727C S-5R IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW STRINGER CLIP AT PASSENGER CABIN BS727C S-5R IAW SRM 51-40-05-0G-0 AND DWG 146A1103. OK TO INSTALSDR SWAA2023062955811Stringer · crackedCRACKED STRINGER CLIP AT PASSENGER CABIN BS727C S-6R.<[01] REMOVED STRINGER CLIP AT PASSENGER CABIN BS727C S-6R IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW STRINGER CLIP AT PASSENGER CABIN BS727C S-6R IAW SRM 51-40-05-0G-0 AND DWG 146A1103. OK TO INSTALSDR SWAA2023062955825Stinger · crackedCRACKED STRINGER CLIP AT PASSENGER CABIN BS727B S-6R.<[01] REMOVED STRINGER CLIP AT PASSENGER CABIN BS727B S-6R IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW STRINGER CLIP AT PASSENGER CABIN BS727B S-6R IAW SRM 51-40-05-0G-0 AND DWG 146A1102. OK TO INSTALSDR SWAA2023062955813Stringer · crackedCRACKED STRINGER CLIP AT PASSENGER CABIN BS727B S-7R.<[01] REMOVED STRINGER CLIP AT PASSENGER CABIN BS727B S-7R IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW STRINGER CLIP AT PASSENGER CABIN BS727B S-7R IAW SRM 51-40-05-0G-0 AND DWG 146A1102. OK TO INSTALSDR SWAA2023062955827Stringer · crackedCRACKED STRINGER CLIP AT PASSENGER CABIN BS747 S-6L.<[01] REMOVED STRINGER CLIP AT PASSENGER CABIN BS747 S-6L IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW STRINGER CLIP AT PASSENGER CABIN BS747 S-6L IAW SRM 51-40-05-0G-0 AND DWG 146A1131. OK TO INSTALL;[SDR SWAA2023062955815Stringer · crackedCRACKED STRINGER CLIP AT PASSENGER CABIN BS727E S-5L.<[01] REMOVED STRINGER CLIP AT PASSENGER CABIN BS727E S-5L IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW STRINGER CLIP AT PASSENGER CABIN BS727E S-5L IAW SRM 51-40-05-0G-0 AND DWG 146A1112. OK TO INSTALSDR SWAA2023062955817Stringer · crackedCRACKED STRINGER CLIP AT PASSENGER CABIN BS727E S-6L.<[01] REMOVED STRINGER CLIP AT PASSENGER CABIN BS727E S-6L IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW STRINGER CLIP AT PASSENGER CABIN BS727E S-6L IAW SRM 51-40-05-0G-0 AND DWG 146A1112. OK TO INSTALSDR SWAA2023062955829Stringer · crackedCRACKED STRINGER CLIP AT PASSENGER CABIN BS727E S-7L.<[01] REMOVED STRINGER CLIP AT PASSENGER CABIN BS727E S-7L IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW STRINGER CLIP AT PASSENGER CABIN BS727E S-7L IAW SRM 51-40-05-0G-0 AND DWG 146A1112. OK TO INSTALSDR SWAA2023062955819Stringer · crackedCRACKED STRINGER CLIP AT PASSENGER CABIN BS727D S-6L.<[01] REMOVED STRINGER CLIP AT PASSENGER CABIN BS727D S-6L IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW STRINGER CLIP AT PASSENGER CABIN BS727D S-6L IAW SRM 51-40-05-0G-0 AND DWG 146A1111. OK TO INSTALSDR SWAA2023062955831Stringer · crackedCRACKED STRINGER CLIP AT PASSENGER CABIN BS727D S-7L.<[01] REMOVED STRINGER CLIP AT PASSENGER CABIN BS727D S-7L IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW STRINGER CLIP AT PASSENGER CABIN BS727D S-7L IAW SRM 51-40-05-0G-0 AND DWG 146A1111. OK TO INSTALSDR SWAA2023062955821Stringer · crackedCRACKED STRINGER CLIP AT PASSENGER CABIN BS727C S-6L.<[01] REMOVED STRINGER CLIP AT PASSENGER CABIN BS727C S-6L IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW STRINGER CLIP AT PASSENGER CABIN BS727C S-6L IAW SRM 51-40-05-0G-0 AND DWG 146A1103. OK TO INSTALSDR SWAA2023062955833Stringer · crackedCRACKED STRINGER CLIP AT PASSENGER CABIN BS727C S-5L.<[01] REMOVED STRINGER CLIP AT PASSENGER CABIN BS727C S-5L IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW STRINGER CLIP AT PASSENGER CABIN BS727C S-5L IAW SRM 51-40-05-0G-0 AND DWG 146A1103. OK TO INSTALSDR SWAA2023062955823Stringer · crackedCRACKED STRINGER CLIP AT PASSENGER CABIN BS727B S-7L.<[01] REMOVED STRINGER CLIP AT PASSENGER CABIN BS727B S-7L IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW STRINGER CLIP AT PASSENGER CABIN BS727B S-7L IAW SRM 51-40-05-0G-0 AND DWG 146A1102. OK TO INSTALSDR SWAA2023062955771Stub Frame · crackedBS 294 STUB FRAME CRACKED AT RBL 65 WL 208 (MARKED)<TRIMMED DAMAGED PART OF THE STUB FRAME INNER CHORD I.A.W SRM 53-10-15-2R-7 REPAIR 7 PAR 4.D FIGURE 202;[05] REQUEST D.V.I I.A.W SRM 53-10-15-2R-7 REPAIR 7 PAR 4.G CRACK INDICATION NOTED WITHIN HOLE. MARKED LOSDR SWAA2023062955767Intercostal · crackedCRACKED INTERCOSTAL AT FWD CABIN BS295.5 S-16L WL216.<[01] NO ALLOWABLE LIMITS FOUND; SRM 51-10-02-0G-0 PAR 9.R REPLACEMENT OF THE PART IS APPLICABLE;[02] REMOVED INTERCOSTAL AND DRILLED NEW I.A.W SRM 51-40-05-0G-0;SRM 51-40-02-0G-0 AND BOEING DWG 141A8180 OK SDR SWAA2023062655773Frame · crackedPASSENGER CABIN FED UPPER FRAME CRACKED BS 312 STR 5L. MARKED<[01] REQUEST NDI TO VERIFY CRACK LENGTH ON PASSENGER CABIN FED UPPER FRAME AT BS312 STR 5L.;[02] ACCOMPLISHED HFEC SURFACE SCAN ON UPPER FRAME IAW 737 NDTM PART 6 CHAPTER 51-00-00 PROCEDURE 23. VERISDR SWAA2023062655772Frame · crackedPASSENGER CABIN FED UPPER FRAME CRACKED BS 312 STR 5L. MARKED<SDR SWAA2023062655770Stub Frame · crackedBS 294 STUB FRAME CRACKED AT RBL 65 WL 208 (MARKED)<[01] VERIFIED APPLICABILITTY OF SRM 53-10-15-2R-7 REPAIR 7;[02] RENOVED AND DISCHARGED 141A8312-3 CLIP I.A.W SRM 53-10-15-2R-7 REPAIR 7 PAR 4.B;[03] VERIFIED CORRECTIVE ACTION STEPS 1 AND 2.SDR SWAA2023062655766Intercostal · crackedCRACKED INTERCOSTAL AT FWD CABIN BS295.5 S-16L WL216.<SDR SWAA2023070355710Beam · corrodedCORROSION ON PASSENGER CABIN FLOOR BEAM AT BS 986; RBL 20 - RBL 24 AND LBL 44; WL 208.<[01] NO LIMITS FOUND FOR PREVIOUS REPAIR A REVIEW OF AIRCRAFT MAINTENANCE RECORDS CONFIRMS THAT AS PER NRC N215090 THE PREVIOUSLY INSTALLED REPAIR IS DOCUMENTED AS BEING ACCSDR SWAA2023070355711Beam · corrodedCORROSION ON PASSENGER CABIN FLOOR BEAM AT BS 986; RBL 20 - RBL 24 AND LBL 44; WL 208.<[01] NO LIMITS FOUND FOR PREVIOUS REPAIR A REVIEW OF AIRCRAFT MAINTENANCE RECORDS CONFIRMS THAT AS PER NRC N215090 THE PREVIOUSLY INSTALLED REPAIR IS DOCUMENTED AS BEING ACCSDR SWAA2023070355719Web · corrodedCORROSION ON PASSENGER CABIN FLOOR SHEAR WEB AT BS 1016+9; LBL 20 - LBL 29; WL 208.<[01] NO ALLOWABLE LIMITS FOUND;REMOVED DAMAGE ON PASSENGER CABIN FLOOR SHEAR WEB AT BS 1016+9; LBL 20 - LBL 29; WL 208 9.5'X2' AREA I.A.W SRM 51-10-02-0G-0;[02] REQUEST HFEC TOSDR SWAA2023070355725Strap · corrodedCORROSION ON PASSENGER CABIN FLOOR STRAP AT BS 1016+12; RBL 18; WL 208.<[01] NO ALLOWABLE LIMITS FOUND; REMOVE AND REPLACE THE PART IS APPLICABLE I.A.W SRM 51-10-02-0G-0 PAR 9.C;[02] VERIFIED CORRECTION ACTION ITEM 1; AND MEASUREMENT TABLE; DAMAGE OUT OF LIMITSDR SWAA2023070355724Strap · corrodedCORROSION ON PASSENGER CABIN FLOOR STRAP AT BS 1016+12; RBL 18; WL 208.<[01] NO ALLOWABLE LIMITS FOUND; REMOVE AND REPLACE THE PART IS APPLICABLE I.A.W SRM 51-10-02-0G-0 PAR 9.CSDR SWAA2023070355718Web · corrodedCORROSION ON PASSENGER CABIN FLOOR SHEAR WEB AT BS 1016+9; LBL 20 - LBL 29; WL 208.<[01] NO ALLOWABLE LIMITS FOUND;REMOVED DAMAGE ON PASSENGER CABIN FLOOR SHEAR WEB AT BS 1016+9; LBL 20 - LBL 29; WL 208 9.5'X2' AREA I.A.W SRM 51-10-02-0G-0;[02] REQUEST HFEC TOSDR SWAA2023062955743Floor Support · crackedPASSENGER CABIN FLOOR SUPPORT BS 927-947; BL 0; WL 208 IS CRACKED.<[01] NO ALLOWABLE LIMITS FOUND ON SRM ;REPLACEMENT OF THE PART IS APPLICABLE I.A.W SRM 51-10-02-0G-0 PAR 9.C;[02] REMOVED PASSENGER CABIN FLOOR SUPPORT BS 927-947; BL 0; WL 208 IAW SRM 51-40-02SDR SWAA2023062955749Seat Track · elongatedPASSENGER CABIN SEAT TRACK BS 923; RBL 25 TRACK OUTBOARD FLANGE; WL 208 HAS ELONGATED HOLE.<[01] NO SRM ENTRIES FOUND REPLACEMENT OF THE PART IS APPLICABLE PER SRM 51-10-02-0G-0 PAR 9.C;[02] REMOVED PASSENGER CABIN SEAT TRACK SECTION BS887-BS927; RBL 25; WL 20SDR SWAA2023062955755Seat Track · elongatedPASSENGER CABIN SEAT TRACK BS 923; RBL 45 TRACK INBOARD FLANGE; WL 208 HAS ELONGATED HOLE.<[01] NO SRM ENTRIES FOUND REPLACEMENT OF THE PART IS APPLICABLE PER SRM 51-10-02-0G-0 PAR 9.C;[02] REMOVED PASSENGER CABIN SEAT TRACK SECTION BS887-BS927; RBL 25; WL 208SDR SWAA2023070355252Attach Angle · corrodedCORROSION AFT CARGO BAY ATTACH ANGLE UNDER SHIELD HAS MULTIPLE AREAS UNDER NUT PLATES BS767 TO BS787 RBL21 WL156<[01] CORROSION ON ANGLE WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2023070354817Stringer · corrodedCORROSION ON STRINGER S-26R FROM STA 520+18 TO STA 540.<[01] CORROSION FOUND OUT OF LIMITS ON STRINGER S-26R BS 535 SKIN ATTACHMENT FLANGE 100% OF MATERIAL THICKNESS LOSS L=1' X W=0.75' IAW SRM 53-00-03-1A-1.;[02] VERIFIED APPLICABILITY OF SRM 53-00-03-2R-1 RESDR SWAA2023070355251Shield · corrodedCORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION 1;[03] UPDATE TO CORRECTSDR SWAA2023070355253Angle · corrodedCORROSION AFT CARGO BAY ATTACH ANGLE UNDER SHIELD HAS MULTIPLE AREAS UNDER NUT PLATES BS767 TO BS787 RBL21 WL156<[01] CORROSION ON ANGLE WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION 1;[03] UPDATE TO CORRESDR SWAA2023070355299Door · corrodedCORROSION ON FWD ENTRY DOOR MOPSILL BS 300-312; LBL 65; WL 208.<[01] VERIFIED APPLICABILITY OF SRM 53-10-15-1A-1; REMOVED CORROSION OF FWD ENTRY DOOR MOPSILL BS 300-312; LBL 65; WL 208 AND FOUND OUT OF LIMITS; MATERIAL THICKNESS 0.090' REMOVED MATERIAL 0.020' SDR SWAA2023070355250Shield · corrodedCORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2023070355025Skin · crackedRH HORIZONTAL STABILIZER LOWER SKIN (INSPECTION OF SKIN PANEL OUTBOARD OF SB 737-55-1096) .5' CRACK FOUND 26.8' FROM FWD SIDE AT STA 187.70<[01] REMOVED PANEL 341BZ IAW SOPM 20-50-01 TO ACCESS REPAIR.;[02] REQUEST HFEC INSPECTION TO MARK END OF CRACK.;[03] ACC
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