N240WN
Service difficulty reports · 359
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 = 'N240WN' 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 = 'N240WN' 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 SWAA2023041926192Floor Panel · pulledDOT A24-4 MID CABIN FLOOR PANEL 241AF 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 SRM SDR SWAA2023041926196Floor Panel · pulledDOT A24-5 MID CABIN FLOOR PANEL 241BF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED PANEL 241BF AND FOUND AREA OF PULLED FIBERS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1. CLEAN AND PREP. IAW B737-700 SRM 53-00-50-2SDR SWAA2023041926201Floor Panel · pulledDOT A24-1 MID CABIN FLOOR PANEL 242BF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] FOUND PULLED FIBERS ON 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 STSDR SWAA2023032420511Slide · lowLEFT AFT SLIDE LOW PSI<[01] R&R AFT ENTRY DOOR ESCAPE SLIDE PER MT 725-240-00-00SDR SWAA2023031414545Intercostal · crackedFWD MAIN CABIN FLOOR INTERCOSTAL AT BL 0; STA 538 CRACKED LOCATED IN FWD CARGO DISTRIBUTION BAY FWD MAIN CABIN FLOOR INTERCOSTAL AT BL 0 STA 538 CRACKED LOCATED IN FWD CARGO DISTRIBUTION BAY<[01] R/R CABIN FLOOR INTERCOSTAL AT BL 0; STA 538 REF SRM 51-40-02.SDR SWAA2022051005078Bracket · looseFA REPORTS RIGHT SIDE CLIP FOR GIRT BAR ON FWD SERVICE DOOR IS LOOSE / [01] REPLACED FWD SERVICE DOOR AFT CLIP FWD FASTENER SRM 51-40-02 AND MT 725-61-06SDR SWAA2022040790716Girt Bar · out of positionCUSTOMER WALK: L-2 DOOR GIRT BAR SKIRT DRAGS CATCHES CUT OUT. / [01] REPOSITIONED GIRT AT L-2 DOOR AS PER B737 AMM 26-66-01-400-803;[02] VERIFIED STEP 1SDR SWAA2022040789967Power Supply · inoperativeEMERGENCY LIGHT BATTERY PACK/POWER SUPPLY AT POSITION M1763 INOPERATIVE EMERGENCY LIGHT BATTERY PACK/POWER SUPPLY AT POSITION M1673 INOP / [01] REPLACED NEW BATTERY PACK AT POSITION M1673 AS PER B737 REF 33-51-06-960-805. TESTED FOUND NORMAL.;[02] VERIFIED STESDR SWAA2022040789645Lamp · inoperativeEMERGENCY LIGHT INOPERATIVE AT LOWER LEFT EXTERIOR AREA. / [01] ADJUSTED LAMP AT LOWER LEFT EXTERIOR EMERGENCY LIGHT. PERFORMED OPS CHECK; FOUND NORMAL AS PER B737 AMM 33-51-04-960-801.;[02] VERIFIED STEP 1SDR SWAA2022040889644Scuff Plate · corrodedAFT CARGO DOOR FWD SCUFF PLATE HAS CORROSION THAT IS OUT OF LIMITS / [01] REMOVED AND REPLACED FWD SCUFF PLATE AT AFT CARGO DOOR REF B737-700 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1SDR SWAA2022040884598Fitting · corrodedLT O/B DRAG LINK FOR REAR SPAR VERTICAL ATTACH HAS CORROSION ON AFT INNER LWR SIDE. / [01] REMOVED L/H O/B DRAG LINK AT VERT STAB REAR SPAR REF B737-700 SRM 51-40-02-OG-0;[02] VERIFIED STEP 1;[03] LOCATED AND DRILLED NEW O/B DRAG LINK FITTING AT L/H REAR SPAR SDR SWAA2022040784590Angle · crackedRIGHT WHEEL WELL FWD BULKHEAD RBL 5' VAPOR BARRIER HORIZONTAL ANGLE SECOND HOLE FROM I/B CRACKED / [01] PERFORMED HFEC IAW NDTM PART 6;51-00-00 PROCEDURE 23.<BR>CRACK CONFIRMED. CRACK LENGTH: 0.875';[02] FABRICATED NEW REPLACEMENT ANGLE FOR REPAIR ON RIGHT WHESDR SWAA2022040784591Doubler · crackedRIGHT WHEEL WELL FWD BULKHEAD WEB BY EXHAUST BETWEEN RBL 15' AND RBL 25' I/B HOLE CRACKED / [01] FABRICATED NEW RIGHT WHEEL WELL FWD BULKHEAD DOUBLER BY EXHAUST BETWEEN RBL 15 - RBL 25. IRW B737-700 SRM 51-30-01-0G-0 AND DWG # 111A1511;[02] LOCATED AND DRILLEDSDR SWAA2022040883671Web · corrodedFWD CARGO DOOR CUTOUT LOWER WEB UPPER SURFACE SEVERAL AREA WITH CORROSION / [01] REMOVED CORROSION AT FWD CARGO DOOR CUTOUT LOWER WEB UPPER SURFACE AS PER B737-7 SRM 51-10-02-0G-0;[02] ORIG. MAT. : 0.040'; MAT. REMOVED: 0.010'; REMAINING MAT. : 0.030'; FOUND OSDR SWAA2022040783675Gusset · crackedFWD CARGO COMP STA 500D STR 18R GUSSET CRACKED / [01] REMOVED DMG. GUSSET AT FWD CARGO COMP STA 500D STR 18R; AS PER B737-7 SRM 51-40-02-0G-0. & DWG. 143A9481.;[02] VERIFIED STEP 1 OK TO INSTALL NEW GUSSET;[03] INSTALLED NEW GUSSET AT FWD CARGO COMPT. STA. 500SDR SWAA2022040783676Gusset · crackedFWD CARGO COMP STA 500D STR 18L GUSSET CRACKED / [01] REMOVED CRACKED GUSSET AT FWD CARGO COMP STA 500D STR 18L; AS PER B737-7 SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1 OK TO INSTALL NEW GUSSET;[03] INSTALLED NEW GUSSET P/N:143A9481-6; AT FWD. CARGO COMPT. STA. SDR SWAA2022040883665Access Panel · elongatedLOWER FUSELAGE ACCESS PANEL 194E SEVERAL FASTENER HOLE ELONGATED / [01] ACCOMPLISHED VISUAL INSPECTION FOUND ALL HOLES DAMAGE AS PER B737 NTM 51-05-01 AND PREPARED AREA FOR DRY PROCCES AS PER B737 SRM 51-70-05-2R-0.;[02] VERIFIED STEP #1;[03] ACCOMPLISHED DRY SDR SWAA2022040883668Access Panel · elongatedLOWER FUSELAGE ACCESS PANEL 193D SEVERAL FASTENER HOLE ELONGATED / [01] PERFORMED VISUAL INSPECTION AT PANEL #193D FOUND ALL FASTENER HOLE DAMAGE AS PER BOEING 737 NTM 51-05-01 AND PREPARED PANEL FOR DRY-OUT PER BOEING 737 SRM 51-70-05-2R-0;[02] VERIFIED STEP SDR SWAA2022040883655Channel · corrodedAFT CARGO COMP BETWEEN STA 767 AND STA 847 LBL 21' ZEE CHANNEL UPPER SURFACE CORROSION / [01] REMOVED CORROSION AT AFT CARGO COMP BETWEEN STA767 AND STA 847 LBL 21' Z CHANNEL AS PER B 737 AMM-51-00-53-201-NG-01.;[02] VERIFIED STEP 1;[03] PERFOREMED UT THICKNESSDR SWAA2022040783653Bracket · crackedAFT CARGO COMP STA 867 LBL 11' BRACKET APPEARED CRACKED / [01] REMOVED BRACKET AT AFT CARGO COMPARTMENT STA 867 LBL 11' IAW B737 SRM 51-40-02-0G-0;[02] INSTALLED NEW BRACKET PN 149A8109U114 AT AFT CARGO COMP. STA 867 LBL 11' IAW B737 SRM 51-40-02-0G-0;[03] VERSDR SWAA2022040882682Access Panel · delaminatedR/W T/E ACCESS PANEL 661BB INNER SURFACE CRACKED / [01] CLEANED DAMAGE AREA FOR REPAIR ON ACCESS PANEL #661BB LOWER SKIN AS PER B737 SRM 51-70-05-2R-3;[02] PERFORMED DRY OUT ON DAMAGE AREA ON R/W T/E ACCESS PANEL 661BB ;FOUND NO WATER AS PER B737 SRM 51-70-05-SDR SWAA2022040782675Megaphone · inoperativeMEGAPHONE SW:03339 LOCATED AT AFT L/H WINDSCREEN IS INOP / [01] REMOVED MEGAPHONE S/N: 03339 LOCATED AT AFT L/H WINDSCREEN AND INSTALLED BN 195865 AS PER DWG: 25600001.;[02] VERIFIED STEP 1SDR SWAA2022040782813Strip · corrodedAFT CARGO COMP CAP STRIP LBL 21' BETWEEN STA 747 AND STA 847 CORRODED P/N 453A2611-4 / [01] RECEIVED SERVICEABLE CAPSTRIP P/N 453A2611-4. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q004E502SDR SWAA2022040782818Strip · corrodedAFT CARGO COMP CAP STRIP LBL 21' BETWEEN STA 727 D AND STA 747 CORRODED P/N 453A2611-10 / [01] RECEIVED SERVICEABLE CAPSTRIP P/N 453A2611-10. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q004E502SDR SWAA2022040782812Strip · corrodedAFT CARGO COMP CAP STRIP LBL 21' BETWEEN STA 727 AND STA 727D CORRODED P/N 453A2611-8 / [01] RECEIVED SERVICEABLE CAPSTRIP P/N 453A2611-8. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q004E502SDR SWAA2022040782817Strip · corrodedAFT CARGO COMP CAP STRIP RBL 21' BETWEEN STA 847 AND STA 947.5 CORRODED P/N 453A2611-3 / [01] RECEIVED SERVICEABLE CAPSTRIP P/N 453A2611-3. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q004E502SDR SWAA2022040782811Strip · corrodedAFT CARGO COMP CAP STRIP RBL 21' BETWEEN STA 727D AND STA 787 CORRODED P/N 453A2611-11 / [01] RECEIVED SERVICEABLE CAPSTRIP P/N 453A2611-11. INSTALLATION WILL BE ACCOMPLISHED ON T/C TTG8Q004E502;[02] VERIFIED STEP 1.SDR SWAA2022040782816Strip · corrodedAFT CARGO COMP CAP STRIP RBL 21' BETWEEN STA 727 AND STA 727D CORRODED P/N 453A2611-9 / [01] RECEIVED SERVICEABLE CAPSTRIP P/N 453A2611-9. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q004E502;[02] RECEIVED SERVICEABLE CAPSTRIP P/N 453A2611-9. INSTALLATISDR SWAA2022040782669Bracket · crackedFUSELAGE R/H STA 540 ACCESS THROUGH DOOR 192CR APU DUCT BRACKET CRACKED / [01] REMOVED CRACKED APU DUCT BRACKET AT FUS. R/H STA. 540; ACCESS THRU DOOR 192CR; AS PER B737-7 SRM 51-40-02-0G-0.;[02] INSTALLED NEW BRACKET P/N: 212A1116-1; PO #1762010; ISSUED TAG: SDR SWAA2022040784589Vapor Barrier · crackedRT SIDE VAPOR BARRIER AT STA 663 FOUND CRACKED / [01] PERFORMED VISUAL INSPECTION AND TAP TEST INSPECTION AT VAPOR BARRIER AT STA 663 FOUND CRACK 19'' OF LENGTH. REF B737-700 NDT PART 1 51-05-01PARAGRAPH 5.;[02] DRILLED STOP DRILL ON THE CRACK END. REF 57-10-1SDR SWAA2021040560469Handle · brokenCAPT ASSIST HANDLE BROKEN. OK TO CONT PER MEL 251001 SP1B TRACKING #74401 REMOVED & REPLACED CAPT ASSIST HANDLE REF. AMM 205011. NO DEFECTS NOTED. CL #74513SDR SWAA2021072639104Handle · brokenAFT CARGO DOOR HANDLE BROKEN / R&R AFT CARGO DOOR HANDLE IAW MM 52-31-14 P/N OFF C17333-1 P/N ON 103686-23.SDR SWAA2021082711686Bracket · crackedLEFT WING UPPER FIXED TRAILING EDGE; BEHIND #1 ENGINE AFT FAIRING; FLAP COVE SEAL RETAINER CRACKED. (MARKED) / REMOVED AND REPLACED BRACKET PER SOPM 20-50-01.SDR SWAA2020071499331Girt Bar · looseLEFT AFT GIRTBAR LOOSE. SECURED GIRT BAR AT AFT ENTRY DOOR PER SIP.SDR SWAA2021081077600Support Bracket · cracked#2 PYLON REMOVABLE FAIRING HAS CRACK AT THE AFT END WHERE ROD SUPPORT IS ATTACHED. MARKED / REMOVED AND REPLACED AFT FAIRING SUPPORT BRACKET ASSY PER SRM 51-40-02. SEE WIPS AND TASKS FOR INDIVIDUAL SIGN OFFS.SDR SWAA2020051877408Pressure Deck · crackedCABIN RT HORZ PRESSURE DECK BEADED WEB HAS CRACK AT STA 665 AT RBL 40.5 / REPAIRED RT PRESSURE DECK BEADED WEB PER SRM 53-40-51-2R-2 SEE WIP'S BELOW FOR ALL WORK ACCOMPLISHEDSDR SWAA2020051477409Beam · crackedFWD GALLEY DOOR #5 BEAM CRACKED IN RADIUS INNER SECTION / :INSTALLED NEW SERVICEABLE DOOR PER AMM 52-41-00 ; SEE SUBTASKS FOR INDIVIDUAL SIGNOFFS TAG NO: 664961 PN ON: 141A6516-14 SN ON: 000954 PN OFF: SN OFF: 001964SDR SWAA2020051477410Beam · crackedFWD GALLEY DOOR #4 BEAM CRACKED IN RADIUS INNER SECTION / DOOR REMOVED AND REPLACED ON NON ROUTINE G729482 TAG NO: 664961 PN ON: 141A6516-14M SN ON: 000954 PN OFF: SN OFF: BN001964SDR SWAA2020040134595Light · inoperativeEMERGENCY LIGHT (BULLNOSE AILE LIGHT) AT ROW 13 DEF INOP / REFERENCE A/L 0255905 R/R EMER LIGHT AT 13 DEF PER MM 33-51-03 CL # 35038SDR SWAA2020012210654Lamp · inoperativeEMERGENCY SLIDE LIGHT AFT OF AFT ENTRY DOOR INOP. RELAMPED LIGHT PER AMM.SDR SWAA2022032913532Panel · elongatedWING TO BODY FAIRING PANEL 193B HAS FASTENER HOLES ON THE PANEL ELONGATED; EGG-SHAPED AND DELAMINATED ON SOME OF THE HOLES. / REMOVED AND REPLACED WING TO BODY FAIRING PANEL AS REQUIRED PER B737 MM 53-51-21SDR SWAA2019062654141Lamp · inoperativeFORWARD R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. / RELAMPED LIGHT PER AMM.SDR SWAA2019062654117Lamp · inoperativeR/H OVERWING DOOR EMERGENCY EXIT EXTERIOR GROUND LIGHT INOP. RELAMPED LIGHT PER AMM.SDR SWAA2019051632744Battery · failedEMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1668. R&R BATTERY PER MM.SDR SWAA2019040131213Bracket · out of positionL1 DOOR GIRT BAR RETENTION BRACKET DID NOT SECURELY HOLD GIRT BAR. REPOSITIONED GIRT BAR BRACKET PER SIP.SDR SWAA2019021129463Light · unsecureEMERGENCY EXIT SIGN FELL DOWN MID CABIN. R&R LIGHT ASSEMBLY PER AMM.SDR SWAA2018073023903Sign · missingRT OVERWING EMERGENCY SMALL EXIT SIGN MISSING. INSTALLED SIGN PER MM.SDR SWAA2018052922247Control Unit · faultyAIR TURNBACK, YAW DAMPER, CA DUS AND CTR DU BLANKED, BOTH EEC'S ALT. CA VHF AND NAV RADIOS BLANK AND INOPERATIVE, ALTITUDE BLANK IN HUD, TR1 WOULD NOT DEPLOY ON LANDING, LNAV INOP. R&R STANDBY POWER CONTROL UNIT PER AMM.SDR SWAA2018052922246Control Unit · faultyAIR TURNBACK, YAW DAMPER, CA DUS AND CTR DU BLANKED, BOTH EEC'S ALT. CA VHF AND NAV RADIOS BLANK AND INOPERATIVE, ALTITUDE BLANK IN HUD, TR1 WOULD NOT DEPLOY ON LANDING, LNAV INOP. R&R DISPLAY ELECTRONIC UNIT PER MT.SDR SWAA2018051021850Battery · corrodedG1 GALLEY EMERGENCY EXIT SIGN INOP. R&R BATTERY PER MM.
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