N220WN
Service difficulty reports · 358
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 = 'N220WN' 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 = 'N220WN' 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 SWAA2024100444599Battery Pack · failedEMX BATTERY PACK M01673 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX BATTERY PACK M01673 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]SDR SWAA2024100444596Battery Pack · failedEMX BATTERY PACK M01674 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX BATTERY PACK M01674 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]SDR SWAA2024061802401Handle · looseMAIN CABIN DOOR WHITE HANDLE SUPER LOOSE<[01] RE SECURED MAIN CABIN DOOR WHITE HANDLE REF SIP ; NO DEFECTS NOTED.SDR SWAA2024031964998Handle · out of adjustFWD SVC DOOR PANEL WHERE DOOR HANDLE ATTACHES TO THE DOOR ( INTERIOR)<[01] RESECURED FWD SVC DOOR PANEL IAW AMM 52-41-31.SDR SWAA2024021251214Transmitter · faultyON APPROACH THE T/E FLAPS STOPPED AT >10<15 WIHT FLAPS 15 SELECTED<[01] R&R FLAP POSITION TRANSMITTER IAW AMM 27-58-01. OP CHECK GOODSDR SWAA2023090697165Handle · looseL1 DOOR ASSIST HANDLE LOOSE.<[01] L1 DOOR ASSIST HANDLE TIGHTENED PER 52-11-31SDR SWAA2023041426327Seat · out of adjustRH PASSENGER CABIN SEATS 11DEF RECLINES. 'EMERGENCY EXIT ROW'<[01] ADJUSTED RECLINE TO COMPLETE STOP AS PER DRAWING 25220031(NOTE 52);[02] ADJUSTED RECLINE TO COMPLETE STOP AS PER B/E AEROSPACE CMM 25-23-46;[03] VERIFIED STEPS 1 AND 2.SDR SWAA2023041325320Light · inoperativeSEVERAL PASSENGER INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOPERATIVE.<[01] RE-LAMPED SEVERAL PASSENGER INTERIOR AND EXTERIOR EMERGENCY LIGHTS AND PERFORMED EMERGENCY LIGHTS - OPERATIONAL TEST AS PER B737 AMM 33-51-00-710-801. TEST OK.;[02] VERIFIED STEP 1.SDR SWAA2023041724491Scuff Plate · crackedAFT CARGO DOOR SCUFF PLATE AFT CORNER CRACKED<[01] ACCOMPLISHED REPAIR AT AFT CARGO DOOR SCUFF PLATE AFT CORNER PER B737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975 BY OUTSIDE VENDOR PO#413980. THIS SCUFF PLATE WILL BE INSTALLED ON FAULT #TTG8Q00JDXNP.;[02] VESDR SWAA2023041423725Panel · corrodedFWD CARGO COMP. BULKHEAD PANEL 121HW HAS CORROSION.<[01] VERIFIED STEPS ACCOMPLISHED.SDR SWAA2023041722651Angle · crackedRT WING DEFLECTION PANEL; VERTICAL WEB TO DEFLECTION RIB ATTACH CLIP ANGLE CRACKED.<[01] VERIFIED.SDR SWAA2023041721247Floor Panel · peelingMAIN CABIN FWD WET AREA FLOOR PANEL #221FF LARGE AREA TOP SKIN FIBERGLASS PEELING OFF<[01] REPLACED MAIN CABIN FLOOR PANEL #221FF REF. B737-700 AMM 53-21-00-400-801. THIS PANEL WILL BE INSTALL ON FAULT #TTG8Q00HHHPE;[02] VERIFIED STEP 1SDR SWAA2023041720584Angle · crackedFLOOR SUPPORT BETWEEN STA. 500D AND STA. 520; BL-0 UPPER ANGLE CRACKED.<[01] INSTALLED EWIS PROTECCION AT MAIN CABIN CENTER DRY AREA BETW. STA 500D THRU 520 FOR SHEETMETAL ANGLE REPLACEMENT PER B737-700 AMM 20-60-07-913-801;[02] VERIFIED STEP 1.;[03] INSTALLEDSDR SWAA2023041417489Cover · missingEXIT SING COVER IS MISSING AT R/H SIDEWALL PANEL # 10.<[01] INSTALLED EXIT SING COVER AT R/H SIDEWALL PANEL # 10 IAW B737-700- AMM 33-51-01-96-801.;[02] VERIFIED STEP #1.SDR SWAA2023041717013Floor Panel · peelingMAIN CABIN FWD WET AREA FLOOR PANEL #222BF TOP SKIN WITH LARGE AREA FIBERGLASS PEELING OFF<[01] REPLACED MAIN CABIN FLOOR PANEL #222BF WITH A NEW PANEL REF.B73<BR>7-700 AMM 53-21-00-400-801. FLOOR PANEL WILL BE INSTALL ON FAULT #TTG8Q00HHH8E;[02] VERIFIED STEPSDR SWAA2023041416240Strap · corroded***CORROSION*** AFT CARGO COMPARTMENT FLOOR SUPPORT STRAP AT STA 767+4 RBL:21; LBL:21; AND WL:150.8 CORRODED AT FASTENER HOLES (234-36) ***CORROSION*** AFT CARGO COMPARTMENT FLOOR SUPPORT STRAP AT STA 767+4 RBL:21 LBL:21 AND WL:155.5 CORRODED AT FASTENER HOLESSDR SWAA2023041715782Fitting · crackedDURING BUYBACK FOUND SUPPORT FITTING HAS 0.390' CRACK AT STR 16L BETWEEN STA 294.5 THRU 303.9 WL 208.1<[01] STARTED TO REMOVE FASTENERS AT SUPPORT FITTING LOCATED AT STR 16L BETWEEN STA 294.5 AND 303.9 WL 208.1 PER B737-700 SRM 51-40-02-0G-0;[02] REMOVED SUPPOSDR SWAA2023041715780Skin · bulgedLT WING LOWER MID SPAN T/E PANEL ASSEMBLY 561CB INNER SKIN SHOWS FASTENER HOLES BULGING AS MARKED. 124-014<[01] REPAIRED DAMAGED AREA AT LT WING LOWER MID SPAN T/E PANEL ASSEMBLY 561CB INNER SKIN. REF B737 SRM 51-70-04-2R-9 PARAGRAPH 4. MATERIAL USED GLASS FABSDR SWAA2023041715778Floor Panel · delaminatedPANEL 232QF DELAMINATED.<[01] REPLACED MAIN CABIN FLOOR PANEL #232QF REF. B737-700 AMM 53-21-00-400-801. FLOOR PANEL #232QF WILL BE INSTALL ON FAULT #TTG8Q00HHHG4;[02] VERIFIED.SDR SWAA2023041715771Bracket · crackedFWD CARGO STA 500C LBL 23.5 S-26L WL 156 INTERCOSTAL SUPPORT BRACKET ON AFT SIDE OF FRAME IS CRACKED 124-006<[01] REMOVED AND REPLACED INTERCOSTAL SUPPORT BRACKET AT FWD CARGO STA 500C LBL 23.5 S-26L WL 156 PER B737-700 SRM 51-40-02-0G-0 & DRAWING NO. 143A7505SDR SWAA2023041715779Angle · crackedINTERCOSTAL UPPER CHORD (ANGLE) AT BETWEEN STA 380 AND STA 400 BL 0; HAS CRACKS AT FASTENERS HOLES;<[01] REMOVED AND REPLACED INTERCOSTAL UPPER CHORD (ANGLE) BETWEEN STA 380 AND STA 400 BL 0 PER B737-700 SRM 51-40-02-0G-0 AND DRWG #143A5400.;[02] VERIFIED STEPSDR SWAA2023041714869Angle · crackedINTERCOSTAL UPPER CHORD (ANGLE) AT BETWEEN STA 380 AND STA 400 RBL 10; HAS CRACKS AT FASTENERS HOLES;<[01] REMOVED AND REPLACED INTERCOSTAL UPPER CHORD (ANGLE) BETWEEN STA 380 AND STA 400 RBL 10 PER B737-700 SRM 51-40-02-0G-0 AND DRWG #143A5400.;[02] VERIFIED SDR SWAA2023041714870Frame · crackedFUSELAGE FRAME STA 312 BETWEEN S-5L AND S-6L CRACK AT EDGE.<[01] REPAIRED FRAME AT STA 312 BETWEEN STR 5L AND 6L EDGE AREA PER EA M-22-153-01244 ON FAULT #TTG8Q00JRCWL.;[02] VERIFIED 1.SDR SWAA2023041415024Seat Track · corrodedCABIN SEAT TRACK AT STA 380 LBL 44.50 SPOT OF CORROSION. CORRECTION FAULT. CABIN SEAT TRACK AT STA 380 LBL 45.5 SPOT OF CORROSION.<[01] REMOVED CORROSION AT CABIN SEAT TRACK AT STA 380; LBL 45.5 AS PER SRM 51-10-02-0G-0;[02] VERIFIED STEP 1.;[03] EVALUATED REWSDR SWAA2023041714392Floor Panel · missingMAIN CABIN L/H SIDE FLOOR PANEL #221BF MISSING MATERIAL AT O/B CORNER<[01] FABRICATED MAIN CABIN FWD WET AREA FLOOR PANEL #221BF BY OUTSIDE VENDOR (AERO MARINE) WITH P.O #2011815 REF. DRAWING #141A5810. THIS PANEL WILL BE INSTALL ON FAULT #TTG8Q00HHHPN;[02] VESDR SWAA2023041714395Floor Panel · peelingMAIN CABIN CENTER AREA BETW. STA 727B THRU 727E FLOOR PANEL #241KF TOP SKIN PEELING OFF SOME AREAS<[01] REMOVED FLOOR PANEL # 241KF IAW B737-700 AMM 53-21-00-000-801.;[02] REMOVED THE DAMAGED FACESHEET AND PREPARED DAMAGED AREA AT MAIN CABIN CENTER AREA BETW SSDR SWAA2023041714414Floor Panel · peelingMAIN CABIN AFT AREA BETW. STA 827 THRU 887 FLOOR PANEL #241UF TOP SKIN PEELING OFF SOME AREAS<[01] REMOVED THE FACESHEET AND PREPARED DAMAGED AREA AT MAIN CABIN CENTER AREA BETW STA 727B TRUR 727E FLOOR PANEL #241KF REF: B 737 SRM 53-00-50-2R-1 PARAGRAPH 3;[02SDR SWAA2023041714714Intercostal · crackedFOUND A CRACK AT STA 328 TO 312 RBL 30 WL 208.1 INTERCOSTAL<[01] OK TO INSTALL NEW INTERCOSTAL.SDR SWAA2023041714419Structure · corrodedCORROSION SPOTS AT LOWER MAIN SILL ASSY L2 DOOR INNER CHORD<[01] FOUND DEEP CORROSION EXFOLIATION AT L2 DOOR LOWER SILL INNER CHORD BETWEEN STA 951 AND STA 986. FOUND OUT OF LIMITS AS PER SRM 53-70-15-1A-1;[02] STARTED L2 DOOR LOWER SILL INNER CHORD REMOVAL ASSDR SWAA2023041714708Angle · corrodedCORROSION ** BETWEEN STA 306.9 AND STA 312 AT ANGLE INNER BEAM WL 208<[01] INSTALLED EWIS PROTECTION AT L1 DOOR LOWER SILL INNER CHORD AREA PER B737-700 AMM 20-60-07-913-801.;[02] EVALUATED CORROSION AND FOUND OUT OF LIMITS PER B737-700 SRM 53-10-15-1A-1; CORRSDR SWAA2023041714709Frame · corrodedCORROSION** AT LOWER SIDE FRAME STA 303.9; LBL 64; WL 208.1 CORROSION** AT LOWER SIDE FRAME STA 303.9 LBL64 WL 208.1<[01] REMOVED CORROSION AT LOWER SIDE FRAME AT FRAME STA 306.9 LBL 64 PER B737-700 SRM 51-10-02-0G-0;[02] PERFORMED VISUALLY INSPECTION AT FRAMESDR SWAA2023041714711Beam · corrodedCORROSION AT STA 312 LBL 50 TOP SIDE OF FLOOR BEAM WL 208.1<[01] REMOVED CORROSION AT STA 312 LBL 50 TOP SIDE OF FLOOR BEAM PER B737-700 SRM 51-10-02-0G-0.;[02] VERIFIED STEP 1.;[03] ACCOMPLISHED REPAIR AT MAIN CABIN FLOOR BEAM STA 312 LBL 50 PER EA #23-153-00SDR SWAA2023041714717Intercostal · corrodedCORROSION AT STA 312 TO 294.5 LBL 10; WL 208.1; LAVATORY BASE SUPPORT INTERCOSTAL<[01] REMOVED AND REPLACED INTERCOSTAL BETWEEN STA 294.5 AND STA 312 LBL 10 PER B737-700 SRM 51-40-02-0G-0 AND DRWG #141A5600.;[02] VERIFIED REPLACEMENT OF INTERCOSTAL BETWEEN STASDR SWAA2023041714415Skin · corrodedFUSELAGE SKIN EXTERNAL SPOT OF CORROSION AT STA 747+10 BETWEEN S1 AND S-2R (ON SKIN AND AROUND OF ADJACENT RIVETS)<[01] C/W INSTRUCTIONSSDR SWAA2023041714399Web · corrodedCORROSION FOUND AT AFT WET AREA UNDER PANEL 242VF FROM STA 986.5 TO 1006; RBL 24 TO RBL 25; WL 208.1<[01] AFTER INSPECTION OF FLOOR STRUCTURE UNDER PANEL 242VF. FOUND CORROSION AT WEB BETWEEN STA 986.5 AND STA 1006; RBL 38. FOUND OUT OF LIMITS. NO DAMAGE IS PESDR SWAA2023041714225Beam · corrodedCORROSION AROUND FASTENER HOLES AT STA 986.5; FROM RBL 44 TO LBL44; WL 208.1<[01] FOUND DEEP CORROSION EXFOLIATION OF SEVERAL FASTENER HOLES UPPER AND LOWER FLANGE AT FLOOR BEAM STA 986.5 BETWEEN LBL-40 AND RBL-40. 100% MATERIAL LOST. OUT OF LIMITS AS PER SRM SDR SWAA2023041714212Floor Panel · peelingMAIN CABIN FWD WET AREA FLOOR PANEL #221EF TOP SKIN LARGE AREA FIBERGLASS PEELING OFF<[01] REPLACED MAIN CABIN FLOOR PANEL #221EF WITH A NEW PANEL REF.B73<BR>7-700 AMM 53-21-00-400-801. FLOOR PANEL WILL BE INSTALL ON FAULT #TTG8Q00HHHPG;[02] VERIFIED STEP 1SDR SWAA2023041714213Floor Panel · peelingMAIN CABIN CENTER FLOOR PANEL BETW. STA 480 THRU 500 231GF TOP SKIN PEELING OFF<[01] REMOVED THE DAMAGED FACESHEET AND PREPARED AREA AT MAIN CABIN CENTER AREA BETW. STA 480 THRU 500 FLOOR PANEL # 231GF REF : B 737 53-00-50-2R-1 PARAGRAPH 3;[02] VERIFIED STEP 1SDR SWAA2023041714214Floor Panel · peelingMAIN CABIN CENTER SECTION L/H SIDE FLOOR PANEL #231JF TOP FIBERGLASS SKIN PEELING OFR ON CENTER AREA BTW. STA 480 THRU 500<[01] PREPARED DAMAGED AREA FOR REPAIR; AT L/H SIDE FLOOR PANEL#231JF AS PER B737 SRM 53-00-50-2R-1;[02] REPAIRED DAMAGED AREA AT L/H SIDESDR SWAA2023041714219Panel · peelingMAIN CABIN FLOOR PANEL BETW. STA 500 THRU 520 #231KF TOP FIBERGLASS SKIN PEELING OFF SOME AREAS<[01] REMOVED THE DAMAGED FACESHEET AND PREPARED DAMAGED AREA AT MAIN CABIN FLOOR PANEL #231KF REF: B737 SRM 53-00-50-2R-1 PARAGRAPH 3;[02] VERIFIED STEP 1.;[03] APPSDR SWAA2023041714217Floor Panel · peelingMAIN CABIN CENTER FLOOR PANEL BETW. STA 420 THRU 480 #231DF TOP FIBERGLASS SKIN PEELING OFF ON SOME AREAS<[01] REMOVED THE DAMAGED FACESHEET AND PREPARED DAMAGED AREA AT MAIN CABIN CENTER FLOOR PANEL #231DF REF : B737 SRM 53-00-50-2R-1 PARAGRAPH 3;[02] VERIFIESDR SWAA2023041714223Intercostal · corrodedCORROSION AROUND FASTENER HOLE AT STA 986.5; RBL 45; WL 208.1<[01] JOB WAS ACCOMPLISHED ON ITEM TTG8Q00KBMYQ;[02] VERIFIED STEP 1.SDR SWAA2023041714224Intercostal · corrodedCORROSION AROUND FASTENER HOLE AT STA 986.5; LBL 45; WL 208.1<[01] JOB WAS ACCOMPLISHED ON ITEM TTG8Q00KBMYQ;[02] VERIFIED STEP 1.SDR SWAA2023041714215Web · corrodedFOUND SEVERAL SPOTS OF LIGHT SURFACE CORROSION AT AFT WET AREA FROM STA 1016+ UNDER FLOOR PANEL 241AEF. DOT 82-001 CORROSION AT FLOOR SURFACE FIXED SKIN FROM STA 1016 TO STA 1040 FROM LBL 0 TO LBL 40 WL 208.1.<[01] NO DAMAGE PERMITTED AT WEB AREA AS PER REFERESDR SWAA2023041714220Door · corrodedR2 DOOR LH SIDE INNER CORE HAS SEVERAL SPOTS OF CORROSION. DOT 82-006. CORROSION LOWER MAIN SILL ASSY INNER CHORD<[01] FOUND DEEP CORROSION EXFOLIATION AT R2 DOOR LOWER SILL INNER CHORD STA 980 APPROX. FOUND OUT OF LIMITS AS PER SRM 53-70-15-1A-1;[02] STARTED SDR SWAA2023041713702Plate · crackedAFTER REMOVED LEFT WING LOWER INBOARD FIXED TRALING EDGE PANEL #551GB FOUND GIGGLE PLATE AT INNER WING EDGE WITH CRACK<[01] REMOVED; REPLACED AND INSTALLED GIGGLE PLATE AT WING PANEL #551GB.SDR SWAA2023041713697Support · crackedAFTER REMOVED LEFT WING INBOARD LOWER TREALING EDGE PANEL 561AB; FOUND SUPPORT TO ATTACH PANEL WITH 0.500'CRACK AT END AREA<[01] REMOVED AND REPLACED SUPPORT.SDR SWAA2023012694558Seat Back · out of adjustSEATS BACKS 11DEF MOVE AFT ( IN FRONT OF EMERGENCY EXIT ROW ) SEATS BACKS 11DEF MOVE AFT ( IN FRONT OF EMERGENCY EXIT ROW ) NEEDS ADJUSTMENT<[01] ADJUSTED SEATS 11 DEF PER AMM 25-22-00 PER SEAT BACK LIMIT BREAK FORCE OVERSDR SWAA2023010386783Light · noneOVERWING EMERGENCY EXIT LIGHT INOP. FO SIDE. FO SIDE OVERWING EMERGENCY EXIT LIGHT OPS CHECKED GOOD PER AMM 33-51-01.SDR SWAA2022112974383Support · crackedDOT A24-100 LH WING L/E WING TO BODY FAIRING SUPPORT STRUCTURE CRACKED. LOCATED AT FWD LOWER CORNER OF PANEL 195AL. / [01] REMOVED DAMAGED ANGLE IAW SRM 51-40-02-0G-0.;[02] AUDIT C/W
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