N218WN
Service difficulty reports · 281
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 = 'N218WN' 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 = 'N218WN' 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 SWAA2024111858838Seal · crackedL/H HORIZONTAL STABILIZER UPPER FORWARD SLIDING SEAL IS CRACKED 4 PARALLEL TO SLIDING SEAL LEADING EDGE.<[01] R&RLH HORIZONTAL STABILIZER FRONT UPPER SLIDING SEAL REF. AMM 53-31-31.SDR SWAA2023102613754Hmu · slowNUMBER 1 ENGINE NOTICEABLY SLOW TO SPOOL UP WITH THROTTLES IN SAME POSITION. FMC COMMANDED TAKEOFF N1 SETTINGS APPROXIMATELY 1% DIFFERENT DURING TAKEOFF (#1=87.1; #2=86.3).<[01] REMOVED AND REPLACED #1 ENG HMU AND FUEL PUMP PER AMM 73-11-11;[02] COMPLIED WITH SDR SWAA2023102615188Pump · slowNUMBER 1 ENGINE NOTICEABLY SLOW TO SPOOL UP WITH THROTTLES IN SAME POSITION. FMC COMMANDED TAKEOFF N1 SETTINGS APPROXIMATELY 1% DIFFERENT DURING TAKEOFF (#1=87.1; #2=86.3).<[01] REMOVED AND REPLACED #1 ENG HMU AND FUEL PUMP PER AMM 73-11-11;[02] COMPLIED WITH SDR SWAA2023102312586Seat · faultyPASSENGER CABIN SEAT 11E RECLINES AND IS NOT SUPPOSED TO DUE TO IT BEING IN AN EMERGENCY EXIT ROW.<[01] LOCKED OUT PASSENGER CABIN SEAT 11E RECLINE PER CMM 25-21-42SDR SWAA2023071176869Unknown · unknownLEFT WING TANK SUSPECTED LEAKING QTY STARTED AT 8600LBS LOST 380LBS IN 5 MINUTES THEN STABILIZED AT 8200.<[01] PERFORMED FQIS BITE PER FIM 28-41 TASK 801; NO DEFECTS FOUND. PERFORMED COMPARISON CHECK OF FQIS SYSTEM TO FUEL STICKS PER AMM 28-41-00; STICKS AND QSDR SWAA2023030811465Battery Pack · failedSEVERAL EMERGENCY EXIT LIGHTS FAILED OPERATIONAL TEST IN THE CABIN.<[01] REMOVED AND REPLACED EMERGENCY BATTERY PACK AT POSITIONS: (M1669; M1670 AND M1672) PER REF. B737 AMM 33-51-06-960-805.;[02] PERFORMED EMERGENCY LIGHTS OPERATIONAL TEST PER REF B737 AMM 33SDR SWAA2023030805717Bracket · brokenR-2 DOOR FWD SLIDE MOUNT BRACKET BUMPER NUT BROKEN.<[01] REMOVED AND REPLACED R2 DOOR FWD SLIDE MOUNT BRACKET BUMPER NUT (SHOCKMOUNT) PER B737-700 SRM 51-40-02-0G-0.;[02] VERIFIED REPLACEMENT.SDR SWAA2023030804026Bracket · brokenR-1 DOOR AFT SLIDE MOUNTING BRACKET BUMPER BUT BROKEN.<[01] REMOVED AND REPLACED SHOCKMOUNT 1EA AT R-1 DOOR AFT SLIDE MOUNTING BRACKET.PER B 737-700 SRM 51-40-02-0G-0.;[02] VERIFIED 1.SDR SWAA2023030902654Angle · crackedCABIN FLOOR SUPPORT INTERCOSTAL AT 380-400 2'LEFT OF CENTER LINE IS CRACKED.<[01] INSTALLED EWIS PROTECTION AT ANGLE REPLACEMENT AREA PER B737-700 AMM 20-60-07-913-801.;[02] REMOVED CRACKED ANGLE AT FLOOR STRCTURE BET. STA 380 AND STA 400 BL0 PER B737-700 SRM SDR SWAA2023030901459Strap · corrodedCORROSION. AFT CARGO FLOOR SUPPORT TEE STRAP; AROUND FASTENERS STA 727D+5 BETWEEN LBL 21 AND RBL 21; WL 155.5<[01] FOUND DEEP COOROSION EXFOLIATION OUT OF LIMITS AT FLOOR SUPPORT TEE STRAP STA 727+5; BETWEEN LBL 21 AND RBL 21 AS PER REF SRM 53-00-53-1A-2;[02] SDR SWAA2023030800562Panel · missingEXIT SIGN COVER IS MISSING AT L/H SIDEWALL PANEL #9.<[01] REMOVED AND REPLACED EXIT SIGN COVER AT L/H SIDEWALL PANEL # 9. IAW B&37-700 AMM 33-51-01-960-802.;[02] VERIFIED STEP 1.SDR SWAA2023030800563Cover · missingEXIT SIGN COVER IS MISSING AT LAVATORY A.<[01] INSTALLED NEW EXIT SIGN COVER AT LAVATORY A IAW B737-700 AMM 33-51-01-960-801.;[02] VERIFIED INSTALLED SIGN COVER.SDR SWAA2023030999927Intercostal · crackedAFT PASSENGER COMPARTMENT FLOOR STRUCTURE - WET AREA INTERCOSTAL UPPER AREA;BL0 BETWEEN STA 927 TO STA 947 IS CRACKED<[01] REMOVED INTERCOSTAL AT AFT PASSENGER COMPARTMENT FLOOR STRUCTURE WET AREA INTERCOSTAL UPPER AREA BL0 BETWEEN STA. 927 TO STA 947;[02] VERSDR SWAA2023030900119Intercostal · crackedFWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL CRACKED @ BL-0 BETWEEN STA 340 AND 360 WL208.1 MKD DOT<[01] REMOVED CRACKED INTERCOSTAL BETWEEN STA 344 AND STA 360 BL0 PER B737-700 SRM 51-40-02-0G-0.;[02] THIS INTERCOSTAL HAS AN ANGLE FITTING REPAIR INSTALLED DUESDR SWAA2023030900386Floor Panel · peelingMAIN CABIN AFT WET AREA FLOOR PANEL #241ABF TOP SKIN FIBERGLASS PEELING OFF<[01] FABRICATED PASSENGER CABIN FLOOR PANEL #241ABF PER DRWG #147A5810 BY OUTSIDE VENDOR PO#2006646. THIS PANEL WILL BE INSTALLED ON FAULT #TTG8Q00GQ33Y PER B737-700 AMM 53-21-00-400-8SDR SWAA2023030900390Floor Panel · peelingMAIN CABIN FWD WET AREA FLOOR PANEL #221BF TOP SKIN FIBERGLASS PEELING OFF SEVERAL AREAS<[01] FABRICATED MAIN CABIN FLOOR PANEL #221BF BY OUTSIDE VWENDOR (AERO MARINE) WITH PO #2006745 REF. DRAWING 141A5810. PANEL 221BF BY OUTSIDE VENDOR;[02] VERIFIED STEP 1.SDR SWAA2023030900392Floor Panel · peelingMAIN CABIN FWD WET AREA FLOOR PANEL #221DF TOP SKIN FIBERGLASS PEELING OFF SEVERAL AREAS<[01] FABRICATED MAIN CABIN FLOOR PANEL #221DF BY OUTSIDE VWENDOR (AERO MARINE) WITH PO #2006750 REF. DRAWING 141A5810. PANEL 221DF WILL BE INSTALLED ON FAULT #TTG8Q00HPPNPSDR SWAA2023030800116Floor Panel · peelingMAIN CABIN AFT WET AREA FLOOR PANEL #242UF TOP SKIN FIBERGLASS PEELING OFF<[01] FABRICATED PASSENGER CABIN FLOOR PANEL #242UF PER DRWG #147A5810 BY OUTSIDE VENDOR PO#2006660. THIS PANEL WILL BE INSTALLED ON FAULT #TTG8Q00GQ3EY PER B737-700 AMM 53-21-00-400-801SDR SWAA2023030800117Floor Panel · peelingMAIN CABIN AFT WET AREA FLOOR PANEL #242TF TOP SKIN FIBERGLASS PEELING OFF<[01] FABRICATED PASSENGER CABIN FLOOR PANEL #242TF PER DRWG #147A5810 BY OUTSIDE VENDOR PO#2006738. THIS PANEL WILL BE INSTALLED ON FAULT #TTG8Q00GQ3F2 PER B737-700 AMM 53-21-00-400-801SDR SWAA2023030800394Floor Panel · peelingMAIN CABIN CENTER FLOOR PANEL #241KF TOP SKIN FIBERGLASS PEELING OFF SEVERAL AREAS<[01] PREPARED FOR REPAIR PANEL 241 KF; AS PER B737 SRM 53-00-50-2R-1;[02] VERIFIED STEP 1. OK TO APPLY REPAIR.;[03] REPAIRED PANEL 241KF AS PER B737 SRM 53-00-50-2R-1.MATERIAL USDR SWAA2023030899928Beam · corrodedAFT PASSENGER COMPARTMENT FLOOR STRUCTURE - WET AREA; FLOOR BEAM STA 986.5; RB2 45; FOUND CORROSION AROUND FASTENER HOLE.<[01] REMOVED NUTPLATE AT CABIN PASSENGER FLOOR STRUCTURE- WET AREA FLOOR BEAM STA 986.5; RBL 45 AS PER SRM 51-40-02-0G-0;[02] REMOVED CORRSDR SWAA2023030899929Beam · corrodedAFT PASSENGER COMPARTMENT FLOOR STRUCTURE - WET AREA; FLOOR BEAM STA 986.5; LBL 45; FOUND CORROSION AROUND FASTENER HOLE.<[01] REMOVED NUTPLATE AT CABIN PASSENGER FLOOR STRUCTURE- WET AREA FLOOR BEAM STA 986.5; LBL 45 AS PER SRM 51-40-02-0G-0;[16] FABRICATED RSDR SWAA2023030999442Angle · crackedFWD CARGO STA 500C LBL23 S-26L WL 156 - INTERCOSTAL ANGLE CLIP AT FWD SIDE OF FRAME IS CRACKED. 124-025<[01] REMOVED INTERCOSTAL ANGLE CLIP AT FWD SIDE OF FRAME AT FWD CARGO STA 500C LBL23 S26L WL 156 PER B737-700 SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEWSDR SWAA2023030999571Support · corrodedCORROSION AT R-2 DOOR LOWER SILL SCUFF PLATES SUPPORT INNER CHORD FROM STA 947.75 TO STA 992.8 MKD DOTS<[01] EVALUATED AREA. EXFOLIATED CORROSION PASS THROUGH AT R-2 DOOR LOWER SILL INNER CHORD FOUND OUT OF LIMITS AS PER REFERENCE SRM 53-70-15-1A-1.;[02] REMOVSDR SWAA2023030999441Tie Down · corroded*CORROSION* FWD CARGO TRACK TIE DOWN AT BOTTOM OF RECESS AS MARKED STA 400+2 RBL 14 BETWEEN S-26L AND S-27L WL 156. 124-024<[01] REMOVED CORROSION AT FWD CARGO TRACK TIE DOWN AT BOTTOM OF RECESS AS MARKED STA 400+2 RBL 14 BETWEEN S-26L AND S-27L WL 156. 124-02SDR SWAA2023030999440Tie Down · corroded*CORROSION* FWD CARGO TRACK TIE DOWN AT BOTTOM OF RECESS AS MARKED STA 400+2 LBL 18 BETWEEN S-26L AND S-27L WL 156. 124-023<[01] REMOVED CORROSION AT FWD CARGO TRACK TIE DOWN AT BOTTOM OF RECESS AS MARKED STA 400+2 LBL 18 BETWEEN S-26L AND S-27L WL 156. 124-02SDR SWAA2023030999438Tie Down · corroded*CORROSION* FWD CARGO TRACK TIE DOWN AT BOTTOM OF RECESS AS MARKED STA 480+19 LBL 18 BETWEEN S-26L AND S-27L WL 156. 124-021<[01] REMOVED CORROSION AT FWD CARGO TRACK TIE DOWN AT BOTTOM OF RECESS AS MARKED STA 480+19 LBL 18 BETWEEN S-26L AND S-27L WL 156. 124-SDR SWAA2023030999435Channel · corrodedCORROSION - FWD CARGO L/H SIDE 'Z' CHANNEL AT FASTENER HOLES STR 26L STA 460 TO 480 MKD<[01] ENTER IN ERROR - WRONG DESCRIPTION - SHOULD BE ' CORROSION';[02] CORRECTION ON STEP # 1 - SHOULD BE FOR FAULT #TTG8Q00HNHK1;[03] VERIFIED STEP 2;[04] REMOVED CORROSIONSDR SWAA2023030999425Fitting · crackedL/W REAR SPAR DEFLECTION CONTROL RIB T/E PANEL VERTICAL SEAL FITTING CRACKED @ FASTENER TAIL MKD DOT<[01] ENTER IN ERROR - DUPLICATE ITEM - THIS FAULT WILL BE ACCOMPLISHED ON FAULT #TTG8Q00HKJXV (TO BE REPLACE FITTING);[02] VERIFIED STEP 1SDR SWAA2023030997281Bracket · crackedR/W T/E DEFLECTION CONTROL PANEL O/B BRACKET CRACK.<[01] REMOVED CRACKED BRACKET AT R/W T/E DEFLECTION CONTROL PANEL O/B AREA PER B737-700 SRM 51-40-02-0G-0.;[02] VERIFIED STEP #1; REMOVAL.;[03] LOCATED AND DRILLED NEW BRACKET (CLIP) PER B737-700 SRM 51-10-02-SDR SWAA2023010587833Girt Bar · out of adjustFORWARD SERVICE DOOR GIRT BAR TOUCHES DOOR OPENING. VERIFIED FAULT. MEASURED GIRT BAR TO VERIFY AS CORRECT. VISUALLY VERIFIED OFFSET ON SLIDE BOX HOOKS, STOWAGE AS CORRECT POSITION AND OFFSET ON. ADJUSTED STOW HOOKS TO CLEAR DOOR OPENING DURING NORMAL OPS IASDR SWAA2022102861936Angle · crackedSTA 663 CENTER TANK LOWER ATTACH ANGLE COMMON TO VAPOR BARREIR IS CRACKED AT RBL 10 WL 170.85 / [01] ATTACH ANGLE BEEN REPAIRED ON N/R # TTG8Q00FJLLX I.A.W SRM 57-10-10-2R-5;[02] VERIFIED JOB COMPLETE; AUDIT C/WSDR SWAA2022102761933Floorboard · damagedDOT A-24-20 MID CABIN FLOOR BOARD 241BF HAS PULLED COMPOSITE FIBERS ON TOP SIDE OF PANEL. / [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 IAWSDR SWAA2022102761924Floorboard · damagedDOT A-24-21 MID CABIN FLOOR BOARD 241AF HAS PULLED COMPOSITE FIBERS ON TOP SIDE OF PANEL. / [01] EVALUATED AND FOUND PULLED FIBERS AND A PUNCTURE ON UPPER SURFACE ARE REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED UPPSDR SWAA2022102761926Floorboard · damagedDOT A-24-23 MID CABIN FLOOR BOARD 232SF HAS PULLED COMPOSITE FIBERS ON TOP SIDE OF PANEL. / [01] EVALUATED AND 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 IASDR SWAA2022102761927Floorboard · damagedDOT A-24-24 MID CABIN FLOOR BOARD 232RF HAS PULLED COMPOSITE FIBERS ON TOP SIDE OF PANEL. / [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>CLEANED; PREPPED; AND POTTED DASDR SWAA2022102761928Floorboard · damagedDOT A-24-26 MID CABIN FLOOR BOARD 231ZF HAS PULLED COMPOSITE FIBERS ON TOP SIDE OF PANEL. / [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>CLEANED; PREPPED; AND POTTED DASDR SWAA2022102761929Floorboard · damagedDOT A-24-28 MID CABIN FLOOR BOARD 231YF HAS PULLED COMPOSITE FIBERS ON TOP SIDE OF PANEL. / [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 IAWSDR SWAA2022102761930Floorboard · damagedDOT A-24-29 MID CABIN FLOOR BOARD 231XF HAS PULLED COMPOSITE FIBERS ON TOP SIDE OF PANEL. / [01] EVALUATED PANEL 231 XF AND FOUND PULLED FIBERS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP. IAW B737-700 SRM 53SDR SWAA2022102761931Floor Panel · damagedDOT A-24-30 MID CABIN FLOOR BOARD 242BF HAS PULLED COMPOSITE FIBERS ON TOP SIDE OF PANEL. / [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>CLEANED; PREPPED; AND POTTED DASDR SWAA2022102761932Floor Panel · damagedDOT A-24-31 MID CABIN FLOOR BOARD 242AF HAS PULLED COMPOSITE FIBERS ON TOP SIDE OF PANEL. / [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 IAWSDR SWAA2022102861078Flap · delaminatedR/H WING O/B AFT FLAP I/B LOWER CORNER DELAMINATED / REMOVED DELAMINATED LOWER SKIN 7.0 X 6.0. CLEANED AND PREP AREA FOR REPAIR. IAW B737-700 SRM 51-70-10-2R-0 PAR6;7. REV77;[04] INSPECTED THE FITMENT OF REPAIR PARTS. IAW B737-700 SRM 51-70-10-2R-0 PAR10.;[05]SDR SWAA2022102861077Attach Angle · crackedSTA 663 CENTER TANK LOWER ATTACH ANGLE COMMON TO VAPOR BARREIR IS CRACKED AT RBL 50; WL 170.85 / [01] VERIFIED PARTIALS FOR STEPS 2 - 4;[02] VERIFIED STEPS 1; 5; 7 AND 8;[03] STEP 9 C/W;[04] STEP 11 C/W;[05] REPAIR PARTS BEEN INSTALLED I.A.W SRM 57-1010-2R-5 NSDR SWAA2022101157870Battery Pack · faultyEMERGENCY LIGHTS ON BATTERY PACK M1670 GO ON BRIEFLY THEN EXTINGUISH / [01] REMOVED AND REPLACED POWER SUPPLY M1670 BATTERY PACK REF AMM 33-51-06.SDR SWAA2022071527804Transmitter · faultyON APPROACH WHEN SELECTING FLAPS FROM 15 TO 30 LEFT FLAP NEEDLE WENT TO 27 AND THE RIGHT STAYED AT 25. NO ADVERSE ROLL NOTED. FLAPS DID NOT RETRACT WHEN FLAP HANDLE RAISED. ALL OTHER INDICATIONS NORMAL. / [01] R&R R/H FLAP POSITION TRANSMITTER IAW AMM 27-58-01SDR SWAA2022011861292Battery Pack · inoperativeFWD SERVICE DOOR OUTER EMERGENCY LIGHT INOP ; / [01] R/R RH FWD EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06. OPS CHECKS GOOD.SDR SWAA2021121351212None · brokenSUPPLEMENTAL INFORMATION: AFT GALLEY OVERHEAD EXIT SIGN LENS RETAINING PIN BROKEN ; / [01] 21-133-03671 ISSUED.; [02] APPPLIED TAPE PER EA 21-133-03671-TLD 10 CYCLE PERMITSDR SWAA2021120850024Battery · inoperativeSUPPLEMENTAL INFORMATION: AFT FLESHLIGHT NOT WORKING ; / [01] INSTALLED NEW BATTERY AND INSP STICKER AS PER MM 25-64-00SDR SWAA2021041564165Light · inoperativeL/H WING TO BODY FILLET EMERGENCY LIGHT IS OUT / RELAMPED L/H WING TO BODY FILLET EMERGENCY LIGHT PER M/M 33-51-04 OPS CKS NORMALSDR SWAA2021041564166Light · inoperativeR/H WING TO BODY FILLET EMERGENCY LIGHT IS OUT / RELAMPED R/H WING TO BODY FILLET EMERGENCY LIGHT PER M/M 33-51-04 OPS CKS NORMAL
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