N231WN
Service difficulty reports · 263
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 = 'N231WN' 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 = 'N231WN' 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 SWAA2023112820379Battery Pack · inoperativeSEVERAL EXTERNAL AND INTERNAL EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY PACKS AT M01670; M01672; M01668 POSITIONS. PERFORMED OPERATIONAL TEST FOUND NORMAL PER REF. AMM 33-51-00-710-801.;[02] VERIFIED STEP 1.;[03] VERIFIED STEP:2SDR SWAA2023112825528Battery Pack · inoperativeSEVERAL EXTERNAL AND INTERNAL EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY PACKS AT M01670; M01672; M01668 POSITIONS. PERFORMED OPERATIONAL TEST FOUND NORMAL PER REF. AMM 33-51-00-710-801.;[02] VERIFIED STEP 1.;[03] VERIFIED STEP:2SDR SWAA2023112825529Battery Pack · inoperativeSEVERAL EXTERNAL AND INTERNAL EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY PACKS AT M01670; M01672; M01668 POSITIONS. PERFORMED OPERATIONAL TEST FOUND NORMAL PER REF. AMM 33-51-00-710-801.;[02] VERIFIED STEP 1.;[03] VERIFIED STEP:2SDR SWAA2023113016004Rib · crackedLEFT HORIZONTAL STABILIZER IN SPAR RIB ASSY. #3 (STB STA 111.10); STIFFENER #3 AT LOWER AREA CRACK NOTED.<[01] INSTALL NEW REPAIR PARTS.;[02] REMOVED CRACK DAMAGE AND ACCOMPLISHED REPAIR AT LEFT HORIZONTAL STABILIZER IN SPAR RIB ASSY. #3 (STB STA 111.10); STIFSDR SWAA2023112815320Floor Support · crackedFWD WET CABIN WET AREA FLOOR SUPPORT INTERCOSTAL CRACKED AT LBL-46 BETWEEN STA 312 AND 328<[01] REMOVED AND REPLACED FLOOR SUPPORT INTERCOSTAL AT FWD CABIN WET AREA; LBL-46 BTW STA 312 AND STA 328 AS PER B737-700 SRM 51-40-02-0G-0; DWG# 141A5400.;[02] FINAL INSDR SWAA2023112213248Floor Panel · crackedPANEL 212BW HAS CRACK IN COMPOSITE CORNER ALREADY MARKED<[01] PREPARED FOR REPAIR PANEL 212BW; AS PER AMM 25-00-00-300-802-NG ;.REPAIRED PANEL 212BW AS PER AMM 25-00-00-300-802-NG; MATERIAL USED PO.2004901 AND PO.147381;[02] VERIFIED FINAL STEP 1SDR SWAA2023113012410Sidewall Panel · crackedFWD CABIN WET AREA L/H SIDEWALL FOUND S-15L CRACKED AFT OF STA 294.5 MKD DOT<[01] 'THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-00-03-2R-1 REPAIR 1 AND EA 23-153-03207.';[02] VERIFIED STEP 1.SDR SWAA2023112912164Shield · crackedAPU COMPARTMENT; UPPER HEAT SHIELD P/N 16H40198-19 FOUND CRACKED.<[01] PART RECEIVED; INSTALLATION OF APU UPPER HEAT SHIELD WILL BE ACCOMPLISHED ON TASK CARD: TTG8Q0024ACU;[02] VERIFIED STEP 1.SDR SWAA2023112212414Fitting · crackedRIGHT WING REAR SPAR FIXED T/E LOWER ATTACHED WIGGLE FITTING CRACKE AND SHEARED RIVETS @ ORSS 261 O/B OF FLAP TRACK NO- 6 MKD DOT<[01] REMOVED RIGHT WING REAR SPAR FIXED T/E LOWER ATTACHED WIGGLE FITTING AS PER SRM 51-40-02-0G-0.<BR>LOCATED AND DRILLED NEW LOWSDR SWAA2023112212166Access Panel · bulgedLOWER FWD KEEL BEAM ACCESS PANEL # 192E HAS BULGING/CRACKED FASTENER HOLES<[01] APPLIED REPAIR AT PANEL #192E PER B737 SRM 51-70-04-2R-9 PARAGRAPH 4.K ; 4.M AND B737 SRM 51-70-04-2R-0 PARAGRAPH 4.L.7 & 4.N.2 MATERIAL USED RESIN 9390 PO#1791128 ; FIBEGLASS PO#1SDR SWAA2023112812044Floor Support · corrodedSTA 294.5 AND 312CORROSION ** FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL UPPER CAP @ LBL 11 BETWEEN<[01] CLEANED AND RE-INSPECTED FLOOR SUPPORT INTERCOSTAL UPPER SURFACE AT FWD CABIN WET AREA AT STA 294.5; LBL 11; NO CORROSION SPOT FOUND; ONLY PRIMER AND OLDSDR SWAA2023112812038Floor Support · crackedFWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL CRACKED @ RBL 30 BETWEEN STA 312 AND 328<[01] REMOVED AND REPLACED FLOOR SUPPORT INTERCOSTAL AT FWD CABIN WET AREA BTW STA 312 AND STA 328; RBL 30 AS PER B737-700 SRM 51-40-02-0G-0; DWG# 141A5400.;[02] VERIFIED STEPSDR SWAA2023112812045Floor Support · crackedFWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL UPPER CAP CRACKED @ BL-0 BETWEEN STA 344 AND STA 360 MKD DOT<[01] REMOVED AND REPLACED DAMAGE INTERCOSTAL AT FWD CABIN BL-0 BETWEEN BS344 AND BS360 PER INSTRUCTIONS ON ATTACHED EA 23-153-03182.;[02] FINAL INSPECTIONSDR SWAA2023112812046Intercostal · crackedFWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL UPPER CAP CRACKED @ FASTENER'S HLOE RBL-12 BETWEEN STA 344 AND STA 360 MKD DOT<[01] REMOVED AND REPLACED FLOOR SUPPORT INTERCOSTAL AT FWD CABIN WET AREA BTW STA 344 AND STA 360; RBL 12 AS PER B737-700 SRM 51-40-02-0SDR SWAA2023112812161Floor Panel · delaminatedFWD WET AREA LH PASSENGER CABIN FLOOR ACCESS PANEL #222DF; UPPER SURFACE DELAMUNATED.<[01] THIS WORK WAS ACCOMPLISHED ON FAULT # TTG8Q00P25PQ;[02] FINAL INSPECTION; VERIFIED STEP #1.SDR SWAA2023112211779Fitting · corrodedCORROSION AT FWD ENTRY L-1 DOOR LOWER SILL FWD AND AFT ESCAPE SLIDE LATCH MOUNT FITTINGS<[01] REMOVED AND REPLACED FWD AND AFT ESCAPE SLIDE LATCH MOUNT FITTING (TIE DOWN ASSY) AT L-1 DOOR LOWER SILL AS PER B737-700 SRM 51-40-02-0G-0; SRM 51-40-04-0G-0.;[02] VESDR SWAA2023113011775Rib · crackedLEFT HORIZONTAL STABILIZER INSPAR RIB ASSY. #3 (STB STA 111.10); STFFENER #4 AT LOWER AREA CRACK NOTED.<[01] REMOVED CRACK DAMAGE AND ACCOMPLISHED REPAIR AT LEFT HORIZONTAL STABILIZER INSPAR RIB ASSY. #3 (STB STA 111.10); STIFFENER #4 AT LOWER AREA AS PER SRM SDR SWAA2023113014029Angle · crackedCENTER WING REAR SPAR VAPOR BARRIER WEB UPPER SUPPORT FITTING AT STA 663; IMPROPERLY BUCKED RIVETS FOUND ON EXISTING REPAIR.<[01] REMOVED DAMAGE RIVETS AT CENTER WING REAR SPAR VAPOR BARRIER UPPER SUPPORT ANGLE EXISTING REPAIR FROM RBL5 TO RBL27; PERFORMED HFESDR SWAA2023112911771Floorbeam · corrodedCORROSION AT FWD CABIN WET AREA FLOOR SUPPORT BEAM UPPER CAP LBL 15 STA 312 MKD DOT<[01] ACCOMPLISHED PERMANENT REPAIR PARTS AT STA 312 UPPER CHORD BETWEEN LBL 4 AND LBL 25.5 REF B737-700 SRM 53-10-51-2R-15 TABLE 201 FIG 204.;[02] RII-VERIFIED PERMANENT REPAIRSDR SWAA2023112911599Web · corrodedCORROSION AFT CABIN WET AREA FLOOR WEB STA 1016 TO STA 1021 BL0 TO LBL 33 WL 208.1 MKD DOT<[01] REMOVED EXFOLIATED FLOOR WEB AT AFT CABIN WET AREA STA 1016 TO STA 1021 BL0 TO LBL 33 WL 208.1 PER B737-700 SRM 51-40-02-0G-0. COMPLETED INSTALLATION OF NEW FLOOR WSDR SWAA2023112811590Floor Support · crackedCABIN FLOOR SUPPORT INTERCOSTAL IS CRACKED AT B/S 294.5-277 ON CENTER LINE<[01] REMOVED AND REPLACED FLOOR SUPPORT INTERCOSTAL AT FWD CABIN WET AREA BTW STA 277 TO STA 294.5; ON CENTER LINE AS PER B737-700 SRM 51-40-02-0G-0; DWG# 141A5400.;[02] VERIFIED STEP:1SDR SWAA2023112811388Scuff Plate · crackedAFT CARGO COMPARTMENT DOOR CUTOUT AFT SCUFF PLATE FOUND CRACKED.<[01] AFT CARGO COMPARTMENT DOOR CUTOUT AFT SCUFF PLATE SENT OUT TO OUTSIDE VENDOR J.L. WELDING AND ACCOMPLISHED WELD REPAIR AS PER SRM 53-30-15-2R-1 AND BAC5975.;[02] VERIFIED STEP 1.SDR SWAA2023112811390Web · corrodedCORROSION ** AFT WET AREA FLOOR WEB AT STA 1016; LBL 8.<[01] FAULT TO BE RESOLVED ON NR #TTG8Q00P27WE.;[02] FINAL INSPECTION; FAULT TO BE RESOLVED ON NR #TTG8Q00P27WE.SDR SWAA2023112811392Strap · corrodedCORROSION ** AFT WET AREA FLOOR STRAP AT STA 1021+2; LBL 3.<[01] (FINAL) REMOVED EXFOLIATED FLOOR STRAP AT WET AREA STA 1021+2; LBL 3 PER B737-700 SRM 51-40-02-0G-0. INSTALLED NEW FLOOR STRAP AT STA 1021+2 LBL 3 PER B737-700 SRM 51-40-02-0G-0 AND DWG#: 147A560SDR SWAA2023112811595Floor Panel · corrodedCORROSION AFT CABIN WET AREA SMALL FLOOR PANEL # 242XF DAMAGED R/H STA 1016 MKD DOT<[01] RECEIVED NEW PANEL 242XF. PANEL WILL BE INSTALLED ON ROUTINE CARD TTG8Q00NPRUH.;[02] VERIFIED STEP 1.SDR SWAA2023112811769Floor Support · crackedFWD WET CABIN WET AREA FLOOR SUPPORT INTERCOSTAL CRACKED AT BL-0 BETWEEN STA 277 AND STA 294.5<[01] INTERCOSTAL REPLACEMENT WAS ACCOMPLISHED ON FAULT TTG8Q00P2E4P.;[02] CORRECTING STEP 1 INTERCOSTAL REPLACEMENT WAS ACCOMPLISHED ON FAULT TTG8Q00P26JU.;[03] VERISDR SWAA2023112811772Floor Support · crackedFWD WET CABIN WET AREA FLOOR SUPPORT INTERCOSTAL CRACKED AT BL-0 BETWEEN STA 277 AND STA<[01] INTERCOSTAL REPLACEMENT WAS ACCOMPLISHED ON FAULT TTG8Q00P26JU.;[02] VERIFIED STEP:1SDR SWAA2023112811773Floor Support · crackedFWD WET CABIN WET AREA FLOOR SUPPORT INTERCOSTAL CRACKED AT BL-46 BETWEEN STA 328 AND 344 CORRECTION OF LOCATION LBL 46<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN BETWEEN STA 328 AND STA 344 LBL 46 REF B737-700 SRM 51-40-02-0G-0 AND DWG# 141A5400.;[02SDR SWAA2023112811583Floor Panel · corrodedCABIN FLOOR PANEL 221BF HAS CORRODED INSERTS.<[01] RECEIVED NEW FLOOR PANEL 221BF FROM OUTSIDE VENDOR(AMI); PO#2042489; THIS PANEL WILL BE INSTALL ON FAULT TTG8Q00FYEHJ;[02] FINAL INSPECTION; VERIFIED STEP #1. PANEL WILL BE INSTALLED ON FAULT TTG8Q00FYEHJ.SDR SWAA2023112811584Floor Panel · corrodedCABIN FLOOR PANEL 221DF HAS CORRODED INSERTS.<[01] RECEIVED NEW FLOOR PANEL 221DF FROM OUTSIDE VENDOR(AMI); PO#2042489; THIS PANEL WILL BE INSTALL ON FAULT #TTG8Q00FYEH5;[02] FINAL INSPECTION; VERIFIED STEP #1. PANEL WILL BE INSTALLED ON FAULT #TTG8Q00FYEH5.SDR SWAA2023112811585Floor Panel · corrodedCABIN FLOOR PANEL 221CF HAS CORRODED INSERTS.<[01] RECEIVED NEW FLOOR PANEL 221CF FROM OUTSIDE VENDOR(AMI) PO#2042484; THIS PANEL WILL BE INSTALL ON FAULT #TTG8Q00FYEHA;[02] FINAL INSPECTION; VERIFIED STEP #1. PANEL WILL BE INSTALL ON FAULT #TTG8Q00FYEHA.SDR SWAA2023112811588Floor Panel · corrodedCABIN FLOOR PANEL 222DF HAS CORRODED INSERTS.<[01] RECEIVED NEW FLOOR PANEL 221DF FROM OUTSIDE VENDOR(AMI); PO#2042489; THIS PANEL WILL BE INSTALL ON FAULT TTG8Q00FYEH5;[02] CORRECTING STEP 1 <BR>RECEIVED NEW FLOOR PANEL 221DF FROM OUTSIDE VENDOR(AMI); PO#2042SDR SWAA2023112811592Web · corrodedCORROSION AFT CABIN WET AREA FLOOR WEB STRAP STA 1016 RBL 4 WL 208.1 MKD DOT<[01] AFT CABIN WET AREA FLOOR WEB STRAP STA 1016 RBL 4 WL 208.1 FOUND EXFOLIATED AND OUT OF LIMITS. REMOVED AND REPLACED WEB STRAP AS PER B737-700 SRM 51-40-05-0G-0; SRM 51-40-02-0G-0SDR SWAA2023113011382Rib · crackedNO-2 PYLON AFT LOWER FIXED FAIRING INTERNAL AFT RIB CRACKED MKD DOT<[01] REMOVED AND REPLACED NEW EDGE ASSY PER SRM 51-40-02-0G-0;[02] VERIFIED STEP 1; EDGE ASSY REPLACED AT #2 PYLON AFT FIXED FAIRING;[03] CORRECTING STEP 1: REMOVED AND REPLACED AFT EDGE ASSY SDR SWAA2023113011128Fitting · crackedL/W REAR SPAR FIXED T/E LOWER WIGGLE FITTING CRACKED ABOVE FLAP TRACK NO-3 FWD OUB.MKD DOT<[01] REMOVED AND REPLACED LOWER WIGGLE PLATE ASSY AT L/W REAR SPAR FIXED T/E ABOVE FLAP TRACK NO-3 FWD OUB AS PER B737-700 SRM 51-40-02-0G-0.;[02] FINAL INSPECTION; VERISDR SWAA2023113011137Panel · corrodedCORROSION AT R/W FIXED L/E FRONT SPAR FUELING STATION QTY GAUGES SUPPRT PANEL MKD DOT<[01] REFUELING STATION QTY GAUGES SUPPORT PANEL WILL BE REPLACED ON CARD # TTG8Q00NZZCQ.;[02] FINAL INSPECTION; REFUELING STATION QTY GAUGES SUPPORT PANEL WILL BE REPLACED ONSDR SWAA2023112811380Frame · crackedFWD CABIN WET FUS FRAME CUTOUT RADIUS CRACKED ABOVE L-1 DOOR CUTOUT FWD STA 312 MKD DOT<[01] ACCOMPLISHED REPAIR OF CRACK AT FWD CABIN FRAME BS 312 BETWEEN S-5L AND S-6L PER INSTRUCTIONS ON ATTACHED EA M-22-153-01244.;[02] (RII) FINAL INSPECTION; VERIFIED STEPSDR SWAA2023113010495Retainer · crackedL/W REAR SPAR FIXED T/ E DEFLECTION CONTROL RIB PANEL VERTICAL BULB SEAL RETAINER CRACKED MKD DOT<[01] REMOVED AND REPLACED SEAL RETAINER AT LT WING REAR SPAR FIXED T/E DEFLECTION CONTROL RIB VERTICAL PANEL PER REF B737 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1SDR SWAA2023082392023Girt Bar · out of adjustSWA - REPAIR - NG DOOR SLIDE COVER GIRT BAR RETAINER CLIP MISSING FASTENERS - PERMANENT)<[01] REPLACED FASTENER PER SRM 51-40-02;[02] REPLACED FASTENER PER SRM 51-40-02SDR SWAA2023081689209Fastener · looseF/A REPORT GERT BAR LATCH ON MAIN CABIN DOOR IS LOOSE<[01] OK TO CONTINUE PER TLD<BR>COMPLIED WITH A SAFETY WIRE SECURITY PER EA M23-125-01839.SDR SWAA2023071177256Slide · out of adjustR1 DOOR SLIDE DISLODGED<[01] COMPLIED WITH SLIDE MT 725-61-06. A/C OK FOR SERVICESDR SWAA2023030109448Battery Pack · inoperativeLEFT AFT EMERGENCY LIGHT BATTERY PACK IS INOP BATTERY PACK M1673<[01] REMOVE AND REPLACED LEFT AFT EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06-960-805. OPS CHECK GOOD;[02] VERIFIED STEP 1SDR SWAA2023030105305Angle · crackedCRACK FOUND AT NUTPLATE HOLE INBD SIDE OF DRAIN ON VERTICAL PRESSURE WEB LOWER ATTACH ANGLE STA 663 RBL 35<[01] CUT AND REMOVED DAMAGED SECTION OF ATTACH ANGLE IAW SRM 57-10-10-2R-6 SECTION 4.C;[02] ACCOMPLISHED HFEC IAW B737 NDT PART 6 51-00-00 PROCEDURE 23. SDR SWAA2023030103310Floor Panel · pulledDOT A24-1 CENTER CABIN FLOOR PANEL 241AF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND DAMAGE 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 3A;SDR SWAA2023030103322Floor Panel · pulledDOT A24-2 CENTER CABIN FLOOR PANEL 231XF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND DAMAGE 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 3A;SDR SWAA2023030103311Floor Panel · pulledDOT A24-3 CENTER CABIN FLOOR PANEL 241BF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED DAMAGE; TOP SIDE OF PANEL IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1 REPAIR 1; TAP TEST GOOD NO DELAMINATION NOTED. <BR><BR>VERIFIED REPAIR MATERIALS IAW B737 SSDR SWAA2023030103323Floor Panel · pulledDOT A24-4 CENTER CABIN FLOOR PANEL 241CF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND MISSING FIBERS ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM SDR SWAA2023030103314Floor Panel · pulledDOT A24-10 CENTER CABIN FLOOR PANEL 231ZF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED PANEL 231ZF AND FOUND PULLED FIBERS AND DENTS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP FOR REPAIR. IAWSDR SWAA2023030103315Floor Panel · pulledDOT A24-11 CENTER CABIN FLOOR PANEL 232RF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] WORK ACCOMPLISHED ON W.O.#TTG8Q00HU0UH;[02] VERIFIED STEP 1SDR SWAA2023030103316Floor Panel · pulledDOT A24-12 CENTER CABIN FLOOR PANEL 231YF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND MULTIPLE PLIES ON UPPER SURFACE FULL LENGTH OF BOARD. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANE
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