N252WN
Service difficulty reports · 323
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 = 'N252WN' 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 = 'N252WN' 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 SWAA2024072402671Floor Panel · pulledPANEL 241CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED REPLACEMENT PANEL 241CF IAW SRM 53-00-50-2R-0 ALONG WITH BOEING DRAWING 144A5810 SHEET 0130.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024072402679Floor Panel · pulledPANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED REPLACEMENT PANEL 241DF IAW SRM 53-00-50-2R-0 ALONG WITH BOEING DRAWING 144A5810 SHEET 0009.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024072402672Floor Panel · pulledPANEL 241FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED A NEW FLOOR PANEL USING BMS4-23TYII LOT 1553922-1 AND BMS5-107A ADHESIVE; CURED THE ADHESIVE; UNDER A HEAT LAMP USING THERMOMETER CAL ID: ATS2402 CAL DUE: 08/2024 TO VERIFY TEMPERATURES DURINGSDR SWAA2024072402673Floor Panel · pulledPANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED A NEW FLOOR PANEL USING BMS4-23TYII LOT 1553922-1 AND BMS5-107A ADHESIVE; CURED THE ADHESIVE; UNDER A HEAT LAMP USING THERMOMETER CAL ID: ATS2402 CAL DUE: 08/2024 TO VERIFY TEMPERATURES DURINGSDR SWAA2024072402674Floor Panel · pulledPANEL 242CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] TRIMMED SHAPE FOR NEW FLOOR PANEL FROM BMS4-17TYVI LOT 1553922-1; LOCATED INSERT HOLES AND UP-SIZED INSERTS HOLES; ALL THE WORK WAS PERFORMED IAW SRM 53-00-50-2R-0 PARAGRAPH 1.A AND PARAGRAPH 4.A; TABLE SDR SWAA2024072402675Floor Panel · pulledPANEL 242DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED A NEW FLOOR PANEL USING BMS4-17TYVI LOT 155754-1 AND BMS5-107 ADHESIVE LOT AK3BA2380A-A; CURED ADHESIVE; UNDER A HEAT LAMP USING THERMOMETER; CAL ID: ATS2402 CAL DUE: 08/2024 TO MONITOR THE TESDR SWAA2024072402944Web · crackedRIGHT WING; TRANSVERSE WEB IS CRACKED ON O/B UPPER LEG AT O/B RIVET<[01] REMOVED AND REPLACED RIGHT WING TRANSVERSE WEB ON O/B UPPER LEG IAW SRM 51-40-02 AND DWG# 115A6200 REV B.SDR SWAA2024072403073Seal · crackedRT. STAB PANEL 343AT SHARK FIN CRACKED.<[01] REMOVED AND REPLACED R/H STAB PANEL 343AT SLIDE SEAL (SHARK FIN) IAW SRM 51-40-02-0G-O STEP 4 AND MM 20-50-11-910-801; TABLE 204.<BR>SCREWGUN<BR>ATS2427<BR>CAL DUE 9-24;[02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2024072403069Plate · crackedRIGHT WING; T/E WAFFLE PLATE IS CRACKED AT I/B ATTACH RIVET 10-INCH I/B OF #6 FLAP TRACK<[01] REMOVED AND REPLACED RIGHT WING T/E WAFFLE LOCATED 10' I/B OF #6 FLAP TRACK IAW SRM 51-40-02 AND AIPC 57-50-00-22A.;[02] VERIFIED CORRECTION ACTION ITEM 1; MEASUREMENSDR SWAA2024072403070Attach Angle · crackedRIGHT WING; TRANSVERSE WEB O/B ATTACH ANGLE IS CRACKED AT UPPER ATTACH POINT ON PROGRAM ROLLER SUPPORT FITTING<[01] REMOVED AND REPLACED RT WING TRANSVERSE WEB O/B ATTACH ANGLE;IAW SRM 51-40-02 AND DWG# 115A6200 REV B.SDR SWAA2024072402665Panel · pulledR/W T/E PANEL 661BB HAS SEVERAL PULLED FASTENER HOLES ON AFT END (MARKED)<[01] R/W T/E PANEL 661BB PULLED FASTENER HOLES REPAIRED IAW SRM 51-70-04-2R-9;[02] JOB COMPLETE.SDR SWAA2024072402666Panel · pulledR/W T/E PANEL 661CB HAS SEVERAL PULLED FASTENER HOLES ON AFT END (MARKED)<[01] R/W T/E PANEL 661CB PULLED FASTENER HOLES REPAIRED IAW SRM 51-70-04-2R-9;[02] JOB COMPLETE.SDR SWAA2024052186915Battery Pack · inoperative14A EMERGENCY LIGHT INOP<[01] R&R?D M1673 POWER SUPPLY AND BATTERY; R&R?D M1670 POWER SUPPLY AND BATTERY; AND R&R?D M1668 BATTERY REF AMM 33-51-06. REFERENCE TTG8Q00RQXJV FOR PART INSTALLATION. REPLACED SPLICE SM8 AT CONNECTOR D10712 REF WDM 33-51-11-1 AND SWPSDR SWAA2024052186916Ground Wire · broken20A EMERGENCY LIGHT INOP<[01] FOUND GROUND WIRE BROKEN AT GROUND BLOCK GD3764-DC FOR CONNECTOR D11338 REF WDM 33-51-14.;[02] REPAIRED BROKEN WIRE AT GROUND BLOCK GD3764-DC PER SWPM 20-10-04SDR SWAA2024052186682Battery Pack · no testM1671 FAILED MV EMERGENCY LIGHT CHECK<[01] R/R M1671 BATTERY PACK PER AMM 33-51-06 NO FIX NOTED;[02] R/R M1671 BATTERY PACK PER AMM 33-51-06 NO FIX NOTEDSDR SWAA2024052186914Battery Pack · inoperativeEMERGENCY LIGHT AT 23A INOP<[01] R&R?D M1673 POWER SUPPLY AND BATTERY; R&R?D M1670 POWER SUPPLY AND BATTERY; AND R&R?D M1668 BATTERY REF AMM 33-51-06. REFERENCE TTG8Q00RQXJV FOR PART INSTALLATION. REPLACED SPLICE SM8 AT CONNECTOR D10712 REF WDM 33-51-11-1 AND SDR SWAA2024052186679Battery Pack · no testM1673 FAILED MV EMERGENCY LIGHT CHECK<[01] R/R M1673 BATTERY PACK PER AMM 33-51-06SDR SWAA2024052186680Battery Pack · no testM1672 FAILED MV EMERGENCY LIGHT CHECK<[01] R/R M1672 BATTERY PACK PER AMM 33-51-06 NO FIX NOTEDSDR SWAA2024052186681Battery Pack · no testM1669 FAILED MV EMERGENCY LIGHT CHECK<[01] R/R M1669 BATTERY PACK PER AMM 33-51-06SDR SWAA2023090697242Handle · looseR-2 DOOR SURROUND ASSIST HANDLE IS LOOSE. SECURED R-2 DOOR SURROUND ASSIST HANDLE IAW AMM 25-21-420-801 STEP 3.B.(5).SDR SWAA2023091196738Floor Panel · debondedMID CABIN FLOOR PANEL 242AF UPPER SURFACE HAS SKIN TO CORE DISBOND IN CENTER OF PANEL.<[01] ACCOMPLISHED UT IAW B737 NDT PART 4 51-00-05. NO FURTHER DISBOND NOTED. TOOL# 40082 DUE 10OCT23.<BR>ACCOMPLISHED UT IAW B737 NDT PART 4 51-00-03. WATER INTRUSION NOTED SDR SWAA2023091396179Bracket · crackedRIGHT HAND STA 663 GROUD DISCONNECT BRACKET IS CRACKED<[01] VERIFIED NEW BRACKET AS PART # 276A9183-2 I.A.W BOEING DWG 111A1001<BR><BR>DRILLED NEW BRACKET I.A.W SRM 51-40-05-0G-0 AND BOEING DWG 111A1001;[02] A TAG # FOR BRACKET A201950;[03] INSTALLED BRACKET ISDR SWAA2023091395380Vapor Barrier · crackedRIGHT HAND STA 663 VAPOR BARRIER WEB IS CRACKED AT EXISTING REPAIR AT APPROX RBL 55; W/L 155 - 160<[01] RECEIVED NEW VAPOR BARRIER WEB; PN 111A1151Y10 ATAG WN34763 TO REPLACE CRACKED VAPOR BARRIER WEB IAW BOEING DWG 111A1001 ID:0378 REV A;[02] UPDATED PARTS INSDR SWAA2023091395384Attach Angle · crackedCRACK FOUND ON VAPOR BARRIER UPPER ATTACH ANGLE AT STA 663 RBL 8 (WL 167)<[01] ACCOMPLISHED CRACK CHECK OF OPEN HOLES AND CUT EDGES IAW B737 NDT P6 51-00-00 P16 AND P23 TOOL 36285 DUE 16DEC23 NO CRACKS NOTED;[02] REMOVED DAMAGED VAPOR BARRIER ATTACH ANGLE AT 6SDR SWAA2023091395385Attach Angle · crackedCRACK FOUND ON VAPOR BARRIER UPPER ATTACH ANGLE AT STA 663 LBL 8 (WL 167)<[01] ACCOMPLISHED OPEN HOLE CRACK CHECK IAW B737 NDT P6 51-00-00 P16 AND SURFACE HFEC IAW B737 NDT P23 NO CRACKS NOTED<BR><BR>TOOL 44291 DUE 03NOV23;[02] REMOVED DAMAGE VAPOR BARRIER ATTSDR SWAA2023090695673Floor Panel · pulledMID CABIN FLOOR PANEL 241BF HAS PULLED COMPOSITE FIBERS ON UPPER SURFCE. CLEANED FLOORBOARD IAW SRM 53-0-50-2R-0 REPAIR GENERAL PARAGRAPH 5 A (1). ACCOMPLISHED UT IAW NDT PART 4 51-00-05. NO DISBOND NOTED. ACCOMPLISHED UT IAW NDT PART 4 51-00-03. NO WATER ISDR SWAA2023090695674Floor Panel · pulledDOT A24-23 MID CABIN FLOOR PANEL 241AF HAS PULLED COMPOSITE FIBERS ON UPPER SURFCE.<[01] EVALUATED AND FOUND MULTIPLE AREAS OF DAMAGE TO UPPER SURFACE TO BE BER. REPLACE FLOOR PANEL IAW SRM 53-00-50-2R-0 REPAIR GENERAL PARAGRAPH 4 A.<BR>VERIFIED MATERIALS AS FSDR SWAA2023090695671Floor Panel · pulledMID CABIN FLOOR PANEL 242AF HAS PULLED COMPOSITE FIBERS ON UPPER SURFCE. CLEANED FLOORBOARD IAW SRM 53-0-50-2R-0 REPAIR GENERAL PARAGRAPH 5 A (1). ACCOMPLISHED UT IAW NDT PART 4 51-00-05. NO DISBOND NOTED. ACCOMPLISHED UT IAW NDT PART 4 51-00-03. NO WATER SDR SWAA2023090695672Floor Panel · pulledMID CABIN FLOOR PANEL 231XF HAS PULLED COMPOSITE FIBERS ON UPPER SURFCE. EVALUATED & FOUND MULTIPLE AREAS OF DAMAGE TO UPPER SURFACE TO BE BER. REPLACE FLOOR PANEL IAW SRM 53-00-50-2R-0 REPAIR GENERAL PARAGRAPH 4 A. FABRICATED A NEW FLOORBOARD FROM SAMPLE BOSDR SWAA2023032720606Light · brokenROW 12 CENTER AISLE EMERGENCY EXIT SIGNE BROKEN AND HANGING FROM POWER WIRES<[01] REPLACED CENTER AISLE EMERGENCY EXIT LIGHT HOUSING IAW AMM 33-51-01. OPS CHECK GOODSDR SWAA2022102563387Light · inoperativeL2 DOOR EMERGENCY SLIDE LIGHT INOP / [01] REMOVED AND REPLACED L2 DOOR EMERGENCY SIDE LIGHT PER AMM 33-51-04. OPS CHECK IS GOOD AT THIS TIME.SDR SWAA2022090649594None · inoperativeWORK LIGHT INOP; AFT ENTRY DOOR. WORK LIGHT INOP AFT ENTRY DOOR.<[01] RELAMPED WORK LIGHT AT AFT ENTRY DOOR IAW AMM 33-26-01SDR SWAA2022071929942Cover · missingEMERGENCY EXIT ROW PLACARD LIGHT COVER MISSING ROW 12 F/O SIDE. / [01] C/W EA M 21-133-00720.SDR SWAA2022070717594Strap · corrodedCORROSION STRAP LOCATED BETWEEN BS 727D TO BS727E AND RBL 21.0 TO LBL 21.0 WL 156 AFT CARGO COMPARTMENT 2022-316938 / [01] REPLACED STRAP LOCATED BETWEEN BS 727D TO BS727E AND RBL 21.0 TO LBL 21.0 WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-SDR SWAA2022070717599Support · corrodedCORROSION SUPPORT ZEE LOCATED BETWEEN 727E TO BS767 RBL 21.0 WL 156 AFT CARGO COMPARTMENT 2022-316939 / [01] PERFORMED PERMANENT REPAIR SUPPORT ZEE LOCATED BETWEEN 727E TO BS767 RBL 21.0 WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-6 REPAIR 6;[02]SDR SWAA2022070717595Support · corrodedCORROSION SUPPORT ZEE LOCATED BETWEEN BS 727E TO BS 787 LBL 21 WL 156 AFT CARGO COMPARTMENT 2022-316945 / [01] PERFORMED PERMANENT REPAIR IAW B737-700 SRM 53-00-53-2R-6 FIGURE 203 REPAIR 6 LOC BETWEEN BS 727 TO BS 787 LBL 21 WL 156 AFT CARGO COMPARTMENT SEE INSDR SWAA2022070717596Intercostal · corrodedCORROSION WEB - INTERCOSTAL LOCATEDBETWEEN BS 767 TO BS 794.3 WL 156 AFT CARGO COMPARTMENT 2022-316949 / [01] REPLACED WEB-INTERCOSTAL LOCATED BETWEEN BS 767 TO BS 794.3 WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 146A0081 REV SDR SWAA2022070717598Rib · crackedCRACK DORSAL FIN RIB #8 AT VERTICAL STABILIZER 2022-316969 / [01] REPLACED RIB #8 AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 174A0101 SHEET: 5 REV: B<BR> SEE INDIVIDUAL SIGN-OFFS BELOW;[02] REPLACED RIB #8 AT VERTICAL STABILISDR SWAA2022070717390Track · crackedCRACK TRACK RBBL 13.84 LOCATED BS 767 AFT CARGO COMPARTMENT 2022-316931 / [01] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; CAL DUE DATE: 03-DEC-22;[02] TOOL EDDY CURRENT USED P/N: NORTEC 600D S/N: 210138203 AND DUE DATE: 11-APR-23.;[03] PERFORMSDR SWAA2022070717383Track · crackedCRACK TRACK LBBL 17.24 LOCATED BS 727E AFT CARGO COMPARTMENT 2022-316934 / [01] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; CAL DUE DATE: 03-DEC-22;[02] TOOL EDDY CURRENT USED P/N: NORTEC 600D S/N: 210138203 AND DUE DATE: 11-APR-23.;[03] REPAIRSDR SWAA2022070717391Angle · crackedCRACK ANGLE LOCATED BETWEEN BS 907 TO BS 927 AND BETWEEN STR 26R TO STR 28R AFT CARGO COMPARTMENT 2022-316950 / [01] REPLACED STIFFENER LOCATED BETWEEN BS 907 TO BS 927 AND BETWEEN STR 26R TO STR 28R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DSDR SWAA2022070717392Angle · crackedCRACK ANGLE - SUPPORT LOCATED BS727 RBL3 AFT CARGO COMPARTMENT 2022-316947 / [01] REPLACED ANGLE SUPPORT LOCATED BS727 RBL 3 AFT CARGO COMPARTMENT IAW SRM B737-700 51-40-02 AND DRAWING 144A2600 SH 566 REV - DUE TO ALLOWABLE DAMAGE NOT FOUND IN SRM B737-700 MEASDR SWAA2022070717385Seat Track · corrodedCORROSION SEAT TRACK LOCATED BS639 TO BS663.75 AT RBL45.5 AND WL208.1 AT PASSENGER CABIN 2022-316952 / [01] REMOVED CORROSION LOCATED ON SEAT TRACK AT LEVEL BS649 RBL 45.5 AND WL 208.1 AT PASSENGER CABIN AND EVALUATED REWORKED AREA WAS FOUND WITHIN ALLOWABLE DSDR SWAA2022070117386Stringer · crackedCRACK STRINGER 23L LOCATED BS540 AT FWD CARGO COMPARTMENT 2022-316955 / [01] EQUIPMENT P/N 45MG; S/N 130066701; DUE DATE 08-APR-23 WAS USED.;[02] TOOL USED EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600D S/N: 60007161486; DUE DATE: 06-DEC-22.;[03] TOOLS USED: TEMPSDR SWAA2022070117387Stringer · crackedCRACK STRINGER 24L LOCATED BS540 AT FWD CARGO COMPARTMENT 2022-316956 / [01] EQUIPMENT P/N 45MG; S/N 130066701; DUE DATE 08-APR-23 WAS USED.;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLESDR SWAA2022070117389Stringer · crackedCRACK STRINGER 26L LOCATED BS540 AT FWD CARGO COMPARTMENT 2022-316957 / [01] EQUIPMENT P/N 45MG; S/N 130066701; DUE DATE 08-APR-23 WAS USED.;[02] TOOL USED EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600D S/N: 60007161486; DUE DATE: 06-DEC-22.;[03] TOOLS USED: TEMPSDR SWAA2022070716916Vapor Barrier · crackedCUSTOMER REQUEST CRACK VAPOR VARRIER BS 663 RBL 53 AT MAIN WHEEL WELL COMPARTME 2022-316890 / [01] TOOL USED CALIPER P/N 700-113-10; S/N 0023208; DUE DATE: 23-FEB-23.;[02] PERFORMED AN INTERIM REPAIR ON VAPOR BARRIER BS 663 AND RBL 53 AT MAIN WHEEL WELL COMPARSDR SWAA2022070716912Vapor Barrier · crackedCUSTOMER REQUEST CRACK VAPOR VARRIER BS 663 RBL 34 AT MAIN WHEEL WELL COMPARTME 2022-316891 / [01] TOOL USED CALIPER P/N 700-113-10; S/N 0023208; DUE DATE: 23-FEB-23.;[02] PERFORMED AN INTERIM REPAIR ON VAPOR BARRIER BS 663 RBL 34 AT MAIN WHEEL WELL COMPARTMENSDR SWAA2022070116917Battery Pack · inoperativeINOP BATTERY PACK ON AFT LOWERED CEILING PANEL 2 EA 2022-316545 / [01] REPLACED BATTERY PACK ON AFT LOWERED CEILING PANEL 2 EA IAW B737-700 AMM 33-51-06-960-805 AND OPERATIONAL TEST IS OK;[02] REPLACED BATTERY PACK ON AFT LOWERED CEILING PANEL 2 EA IAW B737-70SDR SWAA2022063016924Intercostal · elongatedELONGATED HOLE WEB-INTERCOSTAL LOCATED BETWEEN BS492.4 TO BS500A AND STR26R AT LEVEL FLOOR STRUCTURE FWD CARGO COMPARTMENT 2022-316906 / [01] REPLACED WEB INTERCOSTAL LOCATED BETWEEN BS492.4 TO BS500A AND STR26R AT LEVEL FLOOR STRUCTURE FWD CARGO COMPARTMENT I
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