N203WN
Service difficulty reports · 295
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 = 'N203WN' 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 = 'N203WN' 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 SWAA2022111557730Floor Panel · crackedCABIN FLOOR PANEL HAS CRACK ON LWR SURFACE AND HOLE ON UPPER SURFACE 221DF. RECEIVED A NEW FLOOR PANEL AND WILL BE INSTALLED ON ROUTINE T/C: TTG8Q00E8D9T.SDR SWAA2022111557745Floor Panel · peelingAFT CABIN FLOOR PANEL 241ZF HAS PEELED UPPER SURFACE FIBERS. RECEIVED A NEW FLOOR PANEL AND WILL BE INSTALL ON T/C TTG8Q00E8D0Q.SDR SWAA2022111557752Floor Panel · peelingAFT CABIN FLOOR PANEL 241UF HAS PEELED UPPER SURFACE FIBERS. RECEIVED A NEW FLOOR PANEL AND WILL BE INSTALLED ON ROUTINE T/C TTG8Q00ED7AU.SDR SWAA2022111557755Floor Panel · peelingAFT CABIN FLOOR PANEL 241DF HAS PEELED UPPER SURFACE FIBERS. RECEIVED A NEW FLOOR PANEL AND WILL BE INSTALLED ON ROUTINE T/C TTG8Q00E8D03.SDR SWAA2022111557756Floor Panel · peelingMID CABIN FLOOR PANEL 231DF HAS PEELED UPPER SURFACE FIBERS. RECEIVED NEW PANEL AND WILL BE INSTALLED ON ROUTINE T/C TTG8Q00ED7BS.SDR SWAA2022111557716Floor Panel · corrodedCABIN FLOOR PANEL HAS CORROSION SPOTS BS 312-328 LBL 11. 8-66. RE-INSPECTED AREA FOUND PANEL BREAK OUT OF LIMITS. REMOVED CABIN FLOOR PANEL BREAK AT IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED THE NEW FLOOR PANEL BREAK IAW SRM 51-40-05-0G-0. INSTALLED THE NSDR SWAA2022111557728Floor Panel · crackedCABIN FLOOR PNL 241AEF HAS CRACK ON LWR SURFACE. 8-71. FLOOR PANEL WILL BE INSTALLED ON ROUTINE T/C TTG8Q00E8D0C.SDR SWAA2022111557751Channel · corrodedAFT CARGO FLOOR SIDEPLATE RBL-21 AT ABOUT STA 727B+9' AND ABOUT WL-156 WITH CORROSION AROUND FASTENER HOLE. CHANNEL SECTION 727-767. REPLACED IAW TASKCARD #TTG8Q00F9U30.SDR SWAA2022110157725Intercostal · crackedCABIN FLOOR INTERCOSTAL BS 380-400 CRACKED AT 2ND FROM AFT SCREW HOLE RBL 9. 8-74 / [01] REMOVED UPPER ANGLE FROM INSTERCOSTAL AT STA 380-400; RBL 9 AS PER B 737-700 SRM 51-40-02-0G-0.;[02] RECEIVED; LOCATED AND DRILLED NEW UPPER ANGLE FROM INSTERCOSTAL AT STASDR SWAA2022110157726Angle · crackedCABIN FLOOR INTERCOSTAL UPPER ANGLE BS 380-400 CRACKED AT 2ND FROM AFT SCREW HOLE BL 0. 8-75 / [01] REMOVED UPPER ANGLE AT STA 380 TO 400 AS PER B737-700 SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW UPPER ANGLE AT STA 380 TO 400 AS PER B737-700 SRM 51-40-05SDR SWAA2022110157727Angle · crackedCABIN FLOOR INTERCOSTAL UPPER ANGLE BS 380-400 CRACKED AT 2ND FROM AFT SCREW HOLE LBL 13. 8-76 / [01] REMOVED CRACKED UPPER ANGLE FROM STA 380 TO STA 400; LBL 13 AS PER B737-700 SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW UPPER ANGLE FROM STA 380 TO STA 40SDR SWAA2022110157720Bracket · corrodedCABIN FLOOR STRUCTURAL MOUNT BRACKET FOR SLIDE GIRT LATCH CORRODED BS 312 LBL 60. 8-66 / [01] REMOVED AND REPLACED SLIDE GIRT LATCH BRACKET AT BS 312 LBL 60.;[02] AT STEP 1 SRM 51-40-02-0G-0;[03] VERIFIED 1-2.SDR SWAA2022110157721Bracket · corrodedCABIN FLOOR STRUCTURAL MOUNT BRACKET FOR SLIDE GIRT LATCH CORRODED BS 344 LBL 62. 8-67 / [01] REMOVED AND REPLACED SLIDE GIRT LATCH BRACKET AT CABIN FLOOR STRUCTURAL BS 344 LBL 62. AS PER B737 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1SDR SWAA2022111557389Floorbeam · corroded*CORROSION* AFT CABIN FLOOR BEAM STA 986.5 BL-0 TO RBL 45 WL 208.1 HAS CORROSION AS MARKED. 124-055 / [01] AFT CABIN FLOOR BEAM STA 986.5 BL-0 TO RBL 45 WL 208.1 FOUND EXFOLIATED CORROSION OUT OF LIMITS AS PER B737 -700 SRM 53-70-51-1A-1.;[02] VERIFIED STEP #1SDR SWAA2022111557390Floorbeam · corroded*CORROSION* AFT CABIN FLOOR BEAM STA 986.5 BL-0 TO LBL 45 WL 208.1 HAS CORROSION AS MARKED. 124-056 / [01] AFT CABIN FLOOR BEAM STA 986.5 BL 0 TO LBL 45 WL 208.1 FOUND EXFOLIATED AND OUT OF LIMITS AT PER SRM 53-70-51-1A-1.;[02] REMOVED EXFOLIATED EXISTING REPASDR SWAA2022111557408Intercostal · crackedINTERCOASTAL CRACKED AT RBL WATERLINE 208.1, BETWEEN BS 294.5 & 312. REMOVED INTERCOSTAL IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED THE NEW INTERCOSTAL IAW SRM 51-40-05-0G-0. REMOVED AND INSTALLED THE NEW INTERCOSTAL IAW SRM 51-40-02-0G-0, & DWG 141A5400.SDR SWAA2022111557357Seat Track · chafedLEFT CABIN SEAT TRACK LBL 45.5' HAS CHAFE AREA ON EDGE BS 520. LEFT CABIN SEAT TRACK LBL 45.5 CHAFE AREA ON EDGE BS 520 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A-1. LOCATED AND DRILLED NEW SEAT TRACK AND NEW SPLICE CHANNEL IAW SRM 53-00-52-2R-4. INSTASDR SWAA2022111557395Floor Panel · peelingAFT CABIN FLOOR PANEL 242UF HAS PEELED UPPER SURFACE FIBERS. RECEIVED A NEW FLOOR PANEL AND WILL BE INSTALL ON FAULT TTG8Q00E8D8P.SDR SWAA2022111557398Floor Panel · bulgedAFT CABIN FLOOR PANEL 241ABF IS BULGING ON UNDERSIDE OF INSERT. RECEIVED A NEW FLOOR PANEL 241ABF AND WILL BE INSTALL ON TTG8Q00E8D0J.SDR SWAA2022111557407Floor Panel · peelingAFT CABIN FLOOR PANEL 241ABF HAS PEELED UPPER SURFACE FIBERS. THE FLOOR PANEL WILL BE REPLACED USING TTG8Q00F9C2C.SDR SWAA2022111557386Gusset · crackedFWD CARGO, BS 500D, S19L GUSSET CRACKED. REMOVED GUSSET IAW SRM 51-40-02-0G-0. LOCATED & DRILLED A NEW GUSSET IAW SRM 51-40-05-0G-0. APPLIED ALODINE AND PRIMED DRILLED HOLES ON GUSSET IAW SRM 51-20-01-0G-0, AND AMM 51-21-72-370-801. INSTALLED THE NEW GUSSETSDR SWAA2022111557399Floor Support · crackedCRACKED FLOOR SUPPORT BETWEEN BS 277 & 294.5, BL 0, WL 208.1 REMOVED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0. LOCATED & DRILLED THE NEW FLOOR SUPPORT IAW SRM 51-40-05-0G-0. INSTALLED THE NEW FLOOR SUPPORT IAW SRM 51-40-02-0G-0, & DWG141A5400.SDR SWAA2022111557351Seat Track · corrodedLEFT CABIN SEAT TRACK, LBL 45.5' HAS CORROSION BS 540. REPAIRED IAW T/C TTG8Q00F8V9M.SDR SWAA2022111557372Structure · corrodedCORROSION ON RT CABIN INNER CHORD BS 312-328 RBL 60. R1 DOOR LOWER INNER CHORD CORROSION IS FOUND OUT OF LIMITS IAW SRM 51-10-02-0G-0. REMOVED LOWER INNER CHORD AT R1 DOOR IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED THE NEW CABIN INNER CHORD IAW SRM 51-40-05SDR SWAA2022111556898Panel · delaminatedLEFT WING LOWER L/E PANEL 521DB CORNER EDGES DELAMINATED. PERFORMED VISUAL AND TAP TEST INSPECTION ON PANEL AND FOUND NO ENTRY OF WATER, OIL, FUEL, OR OTHER UNWANTED MATERIAL IAW NDTM 51-05-01. PREPARED PANEL IAW SRM 51-70-04-2R-13, PARA 4.C, & SRM 51-70-0SDR SWAA2022111556897Panel · delaminatedLEFT WING LOWER L/E PANEL #521KB CORNER EDGES DELAMINATED. PREPARED AREA FOR REPAIR EDGES DELAMINATED IAW SRM 51-70-04-2R-13. REPAIRED AREA AT LEFT WING LOWER L/E PANEL IAW SRM 51-70-04-2R-13.SDR SWAA2022111556899Panel · delaminatedLEFT WING LOWER L/E PANEL 521WB, CORNER EDGES DELAMINATED. PREPARED FOR REPAIR PANEL521 WB IAW SRM 51-70-06-2R-6. REPAIRED PANEL 521 WB IAW SRM 51-70-06-2R-6.SDR SWAA2022111556894Strap · cracked0.375' CRACK EXTENDING FORWARD OF FASTENER ON R1 BEAR STRAP INT. SIDE. SEE FIG. 4 SHEET 1 AT THE TYPICAL CRACK LOCATION. TASK NUMBER 5313-I-15021-NG. 0.375 & 34, CRACK EXTENDING FORWARD OF FASTENER ON R1 BEAR STRAP INT SIDE. ASK NUMBER 5313-I-15021-NG. REMOVSDR SWAA2022111556915Web · damagedFWD CARGO DOOR SILL WEB HAS AN ELONGATED FASTENER HOLE AT BS 460+13, RBL 29, WL 156. FOUND OUT OF LIMITS IAW SRM 53-30-15-1A-1. LOCATED AND DRILLED A NEW FWD CARGO DOOR SILL WEB IAW SRM 51-40-05-0G-0. TREATED AND PRIMED THE NEW WEB LOCATED AND DRILLED IAW ASDR SWAA2022111556895Scuff Plate · crackedFWD CARGO COMPARTMENT FWD CORNER SCUFF PLATE CRACKED. WELDING REPAIR IAW SRM 53-30-15-2R-1AND SOPM 20-20-02 . SCUFF PLATE WILL BE INSTALL ON T/C TTG8Q004EWZ3.SDR SWAA2022111555580Floor Splice · brokenAFT CARGO LT SIDE FLOOR CAP STRIP SPLICE AT APPROX. STA 767 IS BROKEN. INSTALLED ON ROUTINE T/C TTG8Q004E3DG.SDR SWAA2022071930046Floor Panel · crackedFWD CARGO BAY AFT FLOOR PANEL HAS MULTIPLE CRACKS THAT ARE OUT OF LIMITS. / [01] R+R FLOOR PANEL PER AMM 25-52-10.SDR SWAA2022062718354Support · brokenRIGHT SIDE EMERGENCY EXIT WINDOW REVEAL SUPPORT ASSEMBLY IS BROKEN / [01] REMOVED AND REPLACED R/H EMERGENCY EXIT WINDOW REVEAL SUPPORT ASSEMBLY IAW SOPM 20-50-12 PG31 STEP AX;[02] VERIFIED STEP 1; JOB COMPLETE; AUDIT C/WSDR SWAA2022062718132Attach Angle · crackedFOUND CRACK IN A/C BAY ON LOWER ATTACH ANGLE WL 172 AT STA 663 LBL 8 / [01] APPLIED EWIS PROTECTION TO REPAIR AREA IAW AMM 20-60-07;[02] REMOVED ALL FASTENERS AND TRIMMED OUT DAMAGED SECTION OF ANGLE IAW SRM 57-10-10-2R-5;[03] PERFORMED DETAILED VISUAL INSPECTSDR SWAA2022062718133Angle · crackedFOUND CRACK IN A/C BAY ON LOWER ATTACH ANGLE WL 172 AT STA 663 RBL 40 / [01] APPLIED EWIS PROTECTION TO REPAIR AREA IAW AMM 20-60-07;[02] DISPLACED OTBD U CHANNEL SUPPORT AND PANEL SUPPORT TO FOM IAW SRM 57-10-10-2R-5;[03] REMOVED ALL FASTENERS AND TRIMMED OUTSDR SWAA2022050904883Slide · out of positionFWD ENTRY DOOR SLIDE NOT SECURED / [01] RE-SECURED FWD PAX L1 DOOR SLIDE; IAW AMM 25-66-01-400-804. AC OK FOR SERVICE.SDR SWAA2022041994555Scuff Plate · pulledAFT CARGO CENTER SCUFF PLATE (AFT OF BULL NOSE) HAS PULLED THROUGH SCREW HOLES / [01] R & R AFT CARGO ENTER SCUFF PLATE PER AMM 25-52-10.SDR SWAA2021101127201Intercostal · crackedFWD CARGO AFT DISTRIBUTION BAY AT BS540 CABIN FLOOR BOARD INTERCOSTAL RIGHT OF CENTER IS CRACKED ; / [01] R&R FWD CARGO AFT DISTRIBUTION BAY CABIN FLOOR BOARD INTERCOSTAL AT BS540 RIGHT OF CENTER PER SRM 51-40-02.SDR SWAA2021101127200Intercostal · crackedFWD CARGO AFT DISTRIBUTION BAY AT BS540 CABIN FLOOR BOARD INTERCOSTAL LEFT OF CENTER IS CRACKED ; / [01] R&R FWD CARGO AFT DISTRIBUTION BAY CABIN FLOOR BOARD INTERCOSTAL AT BS540 LEFT OF CENTER PER SRM 51-40-02.SDR SWAA2021100827206None · failedEMERGENCY LIGHT BATTERY CHARGER FAILED TEST AT POSITION M1669 ; / [01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY CHARGER AND BATTERY PACK AT POSITION M1669 PER AMM 33-51-06 AND ENG DWG 3500005SDR SWAA2021100828151Battery Pack · failedEMERGENCY LIGHT BATTERY CHARGER FAILED TEST AT POSITION M1669 ; / [01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY CHARGER AND BATTERY PACK AT POSITION M1669 PER AMM 33-51-06 AND ENG DWG 3500005SDR SWAA2020121736832Lamp · inoperativeLT AFT EMERGENCY LIGHT ON BELLY OF AIRCRAFT INOPERABLE. RELAMPED LT AFT EMERGENCY LIGHT, PER AMM 33-51-04.SDR SWAA2020113031460Rib · crackedCRACK INSPAR RIB 129.5 LOCATED AT 34 INCH FROM FRONT SPAR LT HORIZONTAL STAB. REPAIRED INSPAR RIB 129.5 LOCATED AT 34 INCH FROM FRONT SPART LT HORIZONTAL STAB, IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4.SDR SWAA2021052530352Gusset · crackedCRACK GUSSET LOCATED BS 500D AT STR 19R FWD CARGO COMPARTMENT / REPLACED GUSSET LOCATED ON BS 500D AT STR 19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG #143A7902 SHEET 174 REV-SDR SWAA2021052530353Gusset · crackedCRACK GUSSET LOCATED BS 500D AT STR 19L FWD CARGO COMPARTMENT / REPLACED GUSSET LOC BS500D AT STR 19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DWG #143A7902; SHEET 174 REV-SDR SWAA2021021132673Strap · corrodedCORROSION STRAP LOCATED AFT OF BS 767 BETWEEN RBL 21 TO LBL21 AND AFT CARGO COMPARTMENT WL 157.5 / REPLACED STRAP P/N:146A9401-4 LOCATED AFT OF BS 5767 BETWEEN RBL 21 TO LBL 21 AND WL 254.5 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. MEASURE OF CORROSISDR SWAA2021021132002Intercostal · corrodedCORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS 767 TO BS 787 STR 25 RBL 21.84 AFT CARGO COMPARTMENT WL 259.1 / REPLACED INTERCOSTAL WEB LOCATED BETWEEN BS767 TO BS787 STR 25 RBL 21.84 AFT CARGO COMPARMTMENT WL 259.1 IAW SRM B737-700 51-40-02 AND DWG 146A0081 SSDR SWAA2021021131459Strap · corrodedCORROSION STRAP LOCATED ON BS 887 BETWEEN RBL 21 TO LBL 21 AND WL 155.5 AFT CARGO COMPARTMENT / REPLACED STRAP LOC ON BS 887 BTW RBL 21 TO LBL 21 AND WL 155.5 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02SDR SWAA2021021131458Support · corrodedCORROSION SUPPORT ZEE LOCATED BETWEEN BS 727B TO BS 767 STR 25 AND RBL 2 1.84 AFT CARGO COMPARTMENT WL 259.1 / REPLACED SUPPORT ZEE LOC BTW BS 727 TO BS 767 STR 25R AND RBI 21.84 AFT CARGO COMPARTMENT IAW B737- 700 SRM 51-40-02 AND DWG 146A7500 REV BSDR SWAA2020113032672Frame · crackedCRACK INDICATION ON FRAME LOCATED ON BS 907 BETWEEN STR 8L TO STR 9L AT PASSENGER CABIN. PERFORMED PERMANENT REPAIR ON FRAME BS 907 BETWEEN S-18L TO S-9L, IAW E/A SWA NR 20-153-02361 REV IR AND AEROMAN EA NR 53-0761-20 REVISION NR 0 AND PART NR 1 DUE DATE NOT
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