N214WN
Service difficulty reports · 305
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 = 'N214WN' 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 = 'N214WN' 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 SWAA2023073183552Fairing · delaminatedFAIRING 194GR REQUIRE REPLACEMENT REF. TTG8Q00M0S0K FOR 194GR<[01] REMOVED AND REPLACED WING TO BODY FAIRING IAW AMM 53-51-21SDR SWAA2023073183554Fairing · delaminatedFAIRING 194CR REQUIRE REPLACEMENT REF FAULT TTG8Q00M0RW FOR 194CR<[01] REMOVED AND REPLACED FAIRING PANEL ASSY 194CR IAW AMM 53-51-21.SDR SWAA2023070675187Panel · delaminatedFOUND DELAMINATION ON PANEL 194FR<[01] SEE TASK 23-153-02086 FOR WORK PERFORMED.SDR SWAA2023070675186Panel · delaminatedFOUND DELAMINATION ON PANEL 194GR<[01] SEE TASK 23-153-02086 FOR WORK PERFORMED.SDR SWAA2023070675185Panel · delaminatedFOUND DELAMINATION ON PANEL 194CR<[01] COMPLIED WITH EA 23-153-02086.;[02] C/WSDR SWAA2023052451320Slide · inoperativeL1 DOOR PRESSURE INDICATOR IN RED<[01] REPLACED FWD ENTRY DOOR SLIDE AMM 25-66-01 AND MT 725-61-01FESDR SWAA2023051849725Handle · out of adjustPASSENGER CABIN- AFT SERVICE DOOR INSIDE DOOR HANDLE SHAFT COVER NOT SECURE.<[01] RE-SECURED PASSENGER CABIN- AFT SERVICE DOOR INSIDE DOOR HANDLE SHAFT COVER REF AMM 52-41-31.SDR SWAA2023020999259Fitting · looseCUSTOMER REQUEST: L1 DOOR GIRT BAR FITTING LOOSE<[01] L1 DOOR GIRT BAR FITTING TIGHTENED;[02] ADD TO STEP #1<BR>REFERENCE B737-700 AMM 25-66-01-000-804.;[03] VERIFIED STEPS 1 AND 2SDR SWAA2023020997982Flashlight · inoperativeAFT WINDSCREEN I/B FLASHLIGHT INOP<[01] REPLACED FLASHLIGHT BATTERY FOR PROPER FUNCTION AS PER AMM 25-64-00-900-806.;[02] VERIFIED STEP 1SDR SWAA2023020997586Light · inoperativePASSENGER CABIN OVERHEAD BIN EMERGENCY LIGHT AT ROW 9ABC INOP.<[01] RELAMPED PASSENGER CABIN OVERHEAD BIN EMERGENCY LIGHT AT ROW 9ABC AS PER REF B737 AMM 33-51-03-960-801. TEST OK.;[02] VERIFIED STEP 1.SDR SWAA2023020997587Light · inoperativeL2 DOOR EXTERIOR EMERGENCY LIGHT INOP.<[01] RELAMPED L2 DOOR EXTERIOR EMERGENCY LIGHT AS PER REF B737 AMM 33-51-04-960-801. TEST OK.;[02] VERIFIED STEP 1.SDR SWAA2023021395228Cowling · elongated# 2 ENGINE NOSE COWL INLET SKIN HAS ELONGATED FASTENER HOLE AT 9 O'CLOCK POSITION AND 7.5' AFT OF FORWARD EDGE OF SKIN.(51-021)<[01] #2 ENG INLET COWL TO BE REPLACED ON TASK CARD NUMBER TTG8Q00HG69C.;[02] VERIFIED STEP 1SDR SWAA2023021395227Cowling · elongated# 2 ENGINE NOSE COWL INLET SKIN ATTACH STRAP HAS ELONGATED FASTENER HOLE AT 9 O'CLOCK POSITION AND 6' AFT OF FORWARD EDGE OF STRAP. (51-022)<[01] #2 ENG INLET COWL TO BE REPLACED ON TASK CARD NUMBER TTG8Q00HG69C.;[02] VERIFIED STEP 1SDR SWAA2023021393542Fairing · elongatedFOUND ELONGATED HOLES ON SUPPORT FAIRING 642BB MIDDLE SEAL SECTION R/H SIDE<[01] PREPARED FOR REPAIR FAIRING 642 BB; AS PER B737 SRM 51-70-06-2R-9;[02] VERIFIED STEP 1.;[03] REPAIRED FAIRING 642BB AS PER B737 SRM 51-70-06-2R-9 MATERIAL USED PO.1800218 AND PO.1SDR SWAA2023021092941Bracket · crackedLEFT WING T/E ABOVE ACCESS PANEL 551GB SUPPORT BRACKET CRACK<[01] REMOVED BRACKET TO GAIN ACCESS TO THE CRACKED BRACKET SUPPORT PER SRM 51-40-02-0G-0;[02] REMOVED CRACKED SUPPORT BRACKET PER SRM 51-40-02-0G-0;[03] VERIFIED STEPS 1 AND 2;[04] INSTALLED NEW BRACSDR SWAA2023021092408Plate · corrodedEVIDENCE OF CORROSION ON LOWER FUSELAGE NO. 2 VHF ANTENNA MOUNTING PLATE<[01] REMOVED LOWER FUSELAGE NO. 2 VHF ANTENNA MOUNTING PLATE PER REF. SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1.;[03] LOCATED AND DRILL NEW LOWER FUSELAGE NO. 2 VHF ANTENNA MOUNTING PLATE PSDR SWAA2023021091524Panel · crackedVERTICAL FIN ACCESS PANEL 323BL SKIN SURFACE CRACKED.<[01] CUT OUT DAMAGE AREA AS MARKED ON TOP SURFACE OF ACCESS PANEL 323BL; NO CORE DAMAGE. PERFORMED DRY OUT; FOUND NO WATER REPAIR SIZE 1' DIA. PREPARED AREA FOR REPAIR ASPER B737 SRM 51-70-04-2R-1;[02] VERISDR SWAA2023021091527Door · out of adjustCUSTOMER REQUEST....L1 DOOR NEEDS RIG CHECK DOESN'T CLOSE EVENLY.<[01] ACCOMPLISHED L1 DOOR ADJUSTMENTS AS PER AMM 52-11-00-820-801 STEPS 2.H.(1) UP TO 2.H.(9). AND CHECKED SKIN CLEARANCE AND FLUSHNESS OK. ACCOMPLISHED FORWARD ENTRY DOOR SYSTEM TEST AS PER AMMSDR SWAA2023020991509Threshold · crackedITEM CABIN PASSENGER FLOOR STRUCTURE STA 303.9 LEFT WL 208.1 THRESHOLD INNER CORD HAS A CRACK<[01] REMOVED INNER CORD FROM STA. 277 TO 360 LBL 60' WL 208.1 AT CABIN PASSENGER FLOOR REF. B 737-700 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1;[03] LATE ENTRY INSTALLEDSDR SWAA2023021090420Channel · corrodedFWD CARGO FLOOR SUPPORT 24' LEFT OF CENTER LINE 'Z' CHANNEL AT B/S 400-420 HAS LIGHT CORROSION AROUND NUT PLATE HOLES.<[01] FWD CARGO L/H Z CHANNEL STA 400-STA 500D WILL BE REPLACED. FOR WORK ACCOMPLISHED REF TASKCARD#TTG8Q00H5X7Q;[02] VERIFIED CORRECT NONROUTSDR SWAA2023021090423Channel · corrodedFWD CARGO FLOOR SUPPORT 24' LEFT OF CENTER LINE 'Z' CHANNEL AT B/S 420-440 HAS LIGHT CORROSION AROUND NUT PLATE HOLES<[01] FWD CARGO L/H Z CHANNEL STA 400-STA 500D WILL BE REPLACED. FOR WORK ACCOMPLISHED REF TASKCARD#TTG8Q00H5X7Q;[02] VERIFIED CORRECT NONROUTISDR SWAA2023021090424Channel · corrodedFWD CARGO FLOOR SUPPORT 24' LEFT OF CENTER LINE 'Z' CHANNEL AT B/S 440-460 HAS LIGHT CORROSION AROUND NUT PLATE HOLES.<[01] FWD CARGO L/H Z CHANNEL STA 400-STA 500D WILL BE REPLACED. FOR WORK ACCOMPLISHED REF TASKCARD#TTG8Q00H5X7Q;[02] VERIFIED CORRECT NONROUTSDR SWAA2023021090425Channel · corrodedFWD CARGO FLOOR SUPPORT 24' LEFT OF CENTER LINE 'Z' CHANNEL AT B/S 460-480 HAS LIGHT CORROSION AROUND NUT PLATE HOLES<[01] FOUND EXFOLIATED CORROSION AND CRACK AT FWD CARGO FLOOR SUPPORT Z CHANNEL LBL 24 PER REF SRM 51-10-02-0G-0;[02] LOCATED AND DRILLED NEW ZSDR SWAA2023021090421Support · corrodedFWD CARGO FLOOR SUPPORT 24' LEFT OF CENTER LINE 'Z' CHANNEL AT B/S 500A-500B HAS LIGHT CORROSION AROUND NUT PLATE HOLES.<[01] FWD CARGO L/H Z CHANNEL STA 400-STA 500D WILL BE REPLACED. FOR WORK ACCOMPLISHED REF TASKCARD#TTG8Q00H5X7Q;[02] VERIFIED CORRECT NONROSDR SWAA2023021090422Support · corrodedFWD CARGO FLOOR SUPPORT 24' LEFT OF CENTER LINE 'Z' CHANNEL AT B/S 500B-500C HAS LIGHT CORROSION AROUND NUT PLATE HOLES<[01] FWD CARGO L/H Z CHANNEL STA 400-STA 500D WILL BE REPLACED. FOR WORK ACCOMPLISHED REF TASKCARD#TTG8Q00H5X7Q;[02] VERIFIED CORRECT NONROUSDR SWAA2023021390019Wedge · looseLEFT MAIN FLAP O/B T/E AREA COMPOSITE LOWER EDGE SECTION LOOSE DOT 48 EVALAUTED AREA O/B T/E LOWER SKIN SECTION DELAMINATED<[01] PERFORMED VISUAL INPECTION AND TAP TEST AT L\W MAIN FLAP O\B T\E WEDGE ON LOWER SURFACE FOUND DELAMINATION SIZE 30'X9.5' PER B737 NSDR SWAA2023021090018Intercostal · crackedCABIN FLOOR SUPPORT BETWEEN STA312-328 LBL 45.5 INTERCOSTAL CRACKED<[01] REMOVED CABIN FLOOR SUPPORT BETWEEN STA312-328 LBL 45.5 INTERCOSTAL CRACKED IN REF SRM 51-40-02-0G-0 AND FOUND OUT OF LIMITS IN REF SRM 51-10-02-0G-0;[02] LATE ENTRY :<BR>INSTALLED EWIS PSDR SWAA2023021089725Structure · crackedCABIN PASSENGER FLOOR STRUCTURE STA303.9 LEFT WL208 THRESHOLD INNER CORD HAS CRACK<[01] INSTALLED EWIS PROTECTION AT CABIN PASSENGER FLOOR STRUCTURE STA. 303.9 LEFT WL 208 THRESHOLD INNER CORD REF B 737-700 AMM 20-60-07-913-801;[02] REMOVED FASTENERS FOR ACCESSDR SWAA2023022004695Panel · crackedL/H WING FUEL ACCESS PANEL 532RB PLATE LOWER SURFACE CRACKED. (18-093)<[01] RECEIVED L/H WING NEW FUEL ACCESS PANEL #532RB WILL BE INSTALLED T/C TTG8Q00GDEB6;[02] VERIFIED STEP 1.SDR SWAA2023021088964Intercostal · crackedFWD CABIN FLOOR SUPPORT INTERCOSTAL IS CRACKED BETWEEN 344-360 AT CENTER LINE<[01] REMOVED FWD CABIN FLOOR SUPPORT INTERCOSTAL BETWEEN 344-360 AT CENTER LINE IN REF SRM 51-40-02-0G-0; FOUND OUT OF LIMITS IN REF SRM 51-10-02-0G-0;[02] LATE ENTRY :<BR>INSTALLED SDR SWAA2023021088971Beam · corrodedFLOOR BEAM 986.5 IS CORRODED ON TOP CAP 6 INCHES INBOARD OF R-2 DOOR SILL<[01] FOUND EXFOLIATE CORROSION AROUND FASTENER HOLE; OUT OF LIMITS PER SRM;53-70-51-1A-1;[02] REMOVED INTERCOSTAL BETWEEN STA. 986.5 AND STA. 1006 AND RBL 38; AND ATTACH ANGLES; PER REF SDR SWAA2023021088957Intercostal · crackedCABIN FLOOR SUPPORT INTERCOSTAL IS CRACKED BETWEEN 328-344 47' LEFT OF CENTER LINE<[01] REMOVED DAMAGED CABIN FLOOR SUPPORT INTERCOSTAL PER REF 51-40-02-0G-0.;[02] INSTALLED EWIS PROTECTION AT FWD CABIN STA 328-344 47' LEFT OF CENTER LINE PER REF AMM 20-60-07-SDR SWAA2023021088965Intercostal · crackedFWD CABIN FLOOR SUPPORT INTERCOSTAL IS CRACKED BETWEEN 344-360 12 INCHES LEFT OF CENTER LINE<[01] PLACED EWIS PROTECTION FROM STA 344-360.12 PER REF AMM 20-60-07-913-801;[02] REMOVED FOR ACCESS INTERCOSTAL STA 344-360 BL 0 PER REF SRM 51-40-02-0G-0;[03] REMOVESDR SWAA2023021088602Strip · elongatedAFT CARGO R/H FLOORS CAP STRIPS; HOLES ELONGATED<[01] RECEIVED NEW AFT CARGO R/H FLOORS CAP STRIPS; P/ 453A2611-11; -13;-9 AND- 1; NEW CAP STRIPS TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q004G38U;[02] VERIFIED STEP 1SDR SWAA2023021088608Strip · elongatedL/H AFT CARGO FLOORS CAP STRIPS WITH HOLES ELONGATED<[01] RECEIVED NEW AFT CARGO.; L/H FLOORS CAP STRIPS; P/N 453A2611-8;-10;-13; AND-2; NEW CAP STRIPS TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q004G38U;[02] VERIFIED STEP 1SDR SWAA2023021088961Support · corrodedCABIN FLOOR SUPPORT BETWEEN 294.5 - 312 10 INCHES LEFT OF CENTER LINE IS CORRODED<[01] INSTALLED EWIS PROTECTION AT CABIN FLOOR SUPPORT BETWEEN 294.5 - 312 10 INCHES LEFT OF CENTER LINE IN REF AMM 20-60-07-913-801;[18] VERIFIED STEPS 16 AND 17;[19] REMOVED ANDSDR SWAA2023021088968Bracket · crackedLEFT WING T/E BY DEFLECTOR PANEL SUPPORT BRACKET CRACKED DOT 39<[01] REMOVED SUPPORT BRACKET AT L/W T/E BY DEFLECTOR IN REF 51-40-02-0G-0;[02] LOCATED AND DRILLED SUPPORT BRACKET AT R/W T/E BY DEFLECTOR IN REF SRM 51-40-05-0G-0;[03] CORRECTION TO STEP #2:<BR>LSDR SWAA2023020988962Intercostal · crackedCABIN FLOOR SUPPORT INTERCOSTAL IS CRACKED BETWEEN 288-294.5 ON CENTER LINE<[01] REMOVED INTERCOSTAL CRACKED AT MAIN CABIN STA 288 TO STA 294.5 BL 0 PER SRM 51-40-02-0G-0;[02] VERIFIED STEP 1;[03] OK TO LOCATE AND DRILL HOLES;[04] LOCATE AND DRILLED NEW INTERCSDR SWAA2023022004684Panel · crackedFWD CARGO CO MPARTMENT PANEL 121YBC CRACKED<[01] RECEIVED NEW FWD CARGO COMPARTMENT CEILING. SHROUD PANEL P/N 221-11048-1A; NEW PANEL TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00GDE6Z.;[02] VERIFIED STEP 1.SDR SWAA2023021088163Floor Panel · peelingAFT CABIN FLOOR PANEL 241WF UPPER SKIN SURFACE PEELING. (18-041)<[01] MEASUREMENTS;[02] REPAIRED ALL DAMAGES AS MARKED ON TOP SURFACE OF MAIN CABIN FLOOR PANEL 241WF AS PER B737 SRM 51-70-04-2R-1. MATERIALS USED PO#1800218 AND PO#1690463;[03] PERFORMED TAP TESSDR SWAA2023021088160Floor Panel · peelingAFT CABIN FLOOR 242QF UPPER SKIN SURFACE PEELING.(18-046)<[01] REPAIRED DAMAGED AREA AS MARKED ON TOP SURFACE OF MAIN CABIN FLOOR PANEL #242QF AS PER B737 SRM 51-70-04-2R-1 MATERIAL USED PO#1778544 PO#1690463;[02] VERIFIED STEP 1.SDR SWAA2023021088162Floor Panel · peelingAFT CABIN FLOOR PANEL 241UF UPPER SKIN SURFACE PEELING. (18-043)<[01] PREPARED FLOOR PANEL #241UF AT DAMAGED AREA FOR REPAIR PER B737 SRM 53-00-50-2R-1;[02] VERIFIED STEP # 1;[03] OK TO INSTALL REPAIR.;[04] REPAIRED FLOOR PANEL #241UF AT DAMAGED AREA PER B737 SDR SWAA2023021088157Floor Panel · peelingAFT CABIN FLOOR PANEL 241WF UPPER SKIN SURFACE PEELING. (18-041)<[01] REPAIRED DISCREPANCY ON MAIN CABIN FLOOR PANEL 241WF ON NON ROUTINE #8706529 COPY ATTACHED;[02] CORRECTION STEP 1 REPAIRED DISCREPANCY ON MAIN CABIN FLOOR PANEL 241WF ON CUSTOMER BAR CODE TTSDR SWAA2023021088158Floor Panel · crackedAFT CABIN FLOOR PANEL 241WF CRACKED AROUND FASTENER HOLE. (18-042)<[01] REPAIRED DISCREPANCY ON MAIN CABIN FLOOR PANEL 241WF ON NON ROUTINE #8706529 COPY ATTACHED;[02] CORRECTION STEP 1 REPAIRED DISCREPANCY ON MAIN CABIN FLOOR PANEL 241WF ON CUSTOMER BAR CODE SDR SWAA2023021387673Bracket · crackedL/H WING L/E #1 SLAT I/B AUXILIARY TRACK LOWER I/B BRACKET CRACKED. (18-006)<[01] REMOVER BRACKET AT L/H WING L/E #1 SLAT I/B AUXILIARY TRACK LOWER I/B PER REF SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1;[03] OK TO INSTALL NEW BRACKET.;[04] REPLACED L/H WING L/E #SDR SWAA2023021087920Web · crackedCRACK ON HORIZONTAL PRESSURE DECK WEB AT STA 663; RBL 42; LENGTH 0.500'. CRACK ON HORIONTAL PRESSURE DECK WEB AT STA 663 RBL 42 LENGTH 0.500"<[01] FOR ACCESS TO PRESSURE DECK WEB REPAIR; INSTALLED EWIS PROTECTION TO ADJACENT AREA AT STA 663.75 AND STA 675 SDR SWAA2023021088120Floor Panel · delaminatedCABIN FLOOR PANEL 242CF LEFT FWD CORNER INTERNAL AREA COMPOSITE PANEL DELAMINATED<[01] REMOVED DELAMINATED FACESHEET PLIES AND PREPARED DAMAGED AREA TO APPLY THE GLASS FABRIC REPAIR PLIES; NO WATER NOTE ON REPAIR AREA; AT ACCESS FLOOR PANEL 242CF. REF B737 SRMSDR SWAA2023021088122Floor Panel · peelingCABIN FLOOR PANEL 241DF TOP SURFACE SEVERAL AREAS COMPOSITE PEELING<[01] REPAIRED DAMAGED AREA AT UPPER SURFACE ON ACCESS FLOOR PANEL 241 DF. REF B737 SRM 53-00-50-2R-1 REPAIR 1 PARAGRAPH 3. MATERIAL USED GLASS FABRIC PLIES PO#: 1690463 AND RESIN PO#: 1778544.SDR SWAA2023021088126Spar · crackedR/W FRONT SPAR INFERNAL UPPER CHORD FWD TIE-DOWN CLIP CRACKED ABOVE ACCESS PANEL621EB DEFUELING STATION MKD DOT<[01] REMOVED ACCESS PANEL # 621FB GAINED ACCESS TO REPAIR REF B 737-700 SRM 51-40-01;[02] PARTIAL REMOVED FASTENERS AT R/W UPPER CHORD FWD TIE DOWN SDR SWAA2023021088131Fitting · crackedR/W REAR SPAR T/E DEFLECTION CONTROL RIB PANEL VERTICAL BULB SEAL FITTING CRACKED INB MKD DOT<[01] REMOVED BUILD SEAL FITTING AT R/W REAR SPAR T/E DEFLECTION CONTROL IN REF SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED HOLES AT BULB SEAL FITTING R/W REAR SPAR T/E
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