N273WN
Service difficulty reports · 248
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 = 'N273WN' 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 = 'N273WN' 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 SWAA2026091403252Floor Panel · crackedRAMP REPORTS FORWARD CARGO FLOOR PANEL 120CF HAS CRACKS IN IT._ OK TO CONTINUE PER MEL 25-16-01 SP1B REMOVED CARGO FLOOR PANEL 120CF PER AMM 25-52-10 AND INSTALLED NUTPLATES PER EA M-21-153-00609. SEALANT REQURES CURE TIME. APPLIED CIC AND INSTALLED GEL TAPE PSDR SWAA2026061612168Cover · missingOVERWING EMERGENCY EXIT SIGN MISSING F.O SIDE. INSTALLED MISSING COVER IAW AMM 33-51-01SDR SWAA2026022674574Wedge · delaminatedLEFT WING INBOARD FLAP WEDGE APPEARS TO BE DELAMINATED. VERIFIED NEW REPLACEMENT WEDGE FIT CHECK GOOD IAW SRM 51-40-05. VERIFIED NEW REPLACEMENT WEDGE FIT. INSTALLED NEW FLAP WEDGE IAW AMM 27-51-12.SDR SWAA2026022673942Skin · delaminatedLEFT WING INBOARD FLAP APPEARS TO BE DELAMINATED. C/W EA 26-157-00528SDR SWAA2026012965235Slide · dislodgedAFT ENTRY L2 DOOR SLIDE DISLODGED. REMOVED & REPLACED IAW AMM 25-66-01-400-801-NG.SDR SWAA2025063085963Girt Bar · out of adjustFORWARD ENTRY DOOR GRIT BAR DIFFICULT TO INSERT INTO STOWAGE HOOKS<[01] ADJUSTED FWD ENTRY DOOR GIRT BAR PER AMM 25-66-01SDR SWAA2025061782283Fuel Filter · leakingENGINE #2 FUEL FILTER BYPASS LIGHT ILLUMINATED ON INITIAL CLIMB OUT; LIGHT EXTINGUISHED AT 9000 FEET. CONTRACT MX WAS DOING A RUN WITH THE CREW TO CHECK OUT THE BYPASS INDICATION IN THE PROCESS FOUND A BAD FUEL LEAK.. LIGHT DIDN'T COME BACK ON BUT WOULD REPLACSDR SWAA2024111449359Vapor Barrier · crackedCRACK VAPOR VARRIER LOCATED BS663.75 LBL47 AND WL168 AT MAIN WHEEL WELL COMPARTME 2024-634568 CRACK VAPOR BARRIER LOCATED BS663.75 LBL47 AND WL168 AT MAIN WHEEL WELL COMPARTME<[01] UT EQUIPMENT USED P/N: EPOCH 650; S/N 190984811; DUE DATE: 11-JAN-25;[02] TOOL SDR SWAA2024111448839Support Angle · crackedCRACK SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 BL0 AT PASSENGER CABIN 2024-634544<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 BL 0 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG 143A5400 SHEET: 92; RSDR SWAA2024111449007Angle · crackedCRACK ANGLE LOCATED BETWEEN BS663 AND LBL42 AT CENTER WING BOX 2024-634540<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 23 JAN 25.;[02] REPLACED ANGLE AND FASTENERS LOCATED BS 663 BTW LBL 5 TO LBL 70 AT CENTER WING BOX IAW BSDR SWAA2024111449009Angle · crackedCRACK ANGLE LOCATED BETWEEN BS663 AND LBL9 AT CENTER WING BOX 2024-634541<[01] REPLACEMENT ANGLE LOC. BS 663 AND BTW LBL 5 TO LBL 70 AT CENTER WING BOX WAS DOCUMENTED ON FAULT TTG8Q00WFAU7. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACEMENT ANGLE LOC. BS 663 ANDSDR SWAA2024111448838Support Angle · crackedCRACK SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 10 AT PASSENGER CABIN 2024-634542<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 RBL 10 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG 143A5400 SHEET 3SDR SWAA2024111448836Support Angle · crackedCRACK SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 41 AT PASSENGER CABIN 2024-634539<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 RBL 41 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG 143A5400 SHEET 3SDR SWAA2024111448784Support Angle · corrodedCORROSION SUPPORT ANGLE TRAILING EDGE LOCATED ORSS338 TO ORSS439 AT RT WING 2024-634508<[01] REPLACED SUPPORT ANGLE ON TRAILING EDGE LOCATED ORSS338 TO ORSS439 AT RT WING. IAW B737-700 SRM 51-40-02 AND DWG# 115A3700 SHEET 44 AND REV -.;[02] COMPLETEDSDR SWAA2024111448785Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED DEFLECTION CONTROL RIB ORSS271 APROX AT RT WING 2024-634509<[01] REPLACED ANGLE TRAILING EDGE LOCATED DEFLECTION CONTROL RIB ORSS271 APROX AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 115A2930 SHEET: 7 RESDR SWAA2024111448595Panel · corrodedCORROSION FUEL STATION PANEL LOCATED LEADING EDGE AT LEVEL OF S385 AT RT WING 2024-634505<[01] EQUIPMENT P/N 45MG; S/N 221861811; DUE DATE 30-NOV-24 WAS USED ON STEP 7 AND EQUIPMENT P/N PHASEC 3D; S/N 587435/07; DUE DATE 20-MAR-25 WAS USED ON STEP 8;[02] TASK SDR SWAA2024111448431Angle · crackedCRACK ANGLE LOCATED ARM SLAT 7 AT RT WING 2024-634490<[01] REPLACED ANGLE LOCATED ARM SLAT 7 AT RT WING IAW B737-700 SRM-51-10-02; CMM 57-43-02 AND MEASURE CRACK IS L:1.014 INCH. TOOL USE: DIGITAL CALIPER PN: 500-197-30 SN: B23357722 DUE DATE: 28-JAN-25;[02] RSDR SWAA2024111448083Support Angle · corrodedCORROSION SUPPORT ANGLE TRAILING EDGE LOCATED ORSS338 TO ORSS439 AT LT WING 2024-634422<[01] REPLACED SUPPORT ANGLE TRAILING EDGE LOCATED ORSS338 TO ORSS439 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 115A3700 SHEET: 43 REV A SEE INDIVIDSDR SWAA2024111448081Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED DEFLECTION CONTROL RIB IRSS271 APROX AT LT WING 2024-634426<[01] REPLACED BLADE XXX IAW B737-700 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 AND DWG 186A3005-4 SHEET:2 REV:B AND MEASURES OF CRACK IS :L= 0.176? INCHES TOOL USEDSDR SWAA2024111348078Intercostal · crackedCRACK FLOOR STRUCTURE WEB LOCATED BS 947.5 STRINGER 25R AT AFT CARGO COMPARTMENT 2024-634378<[01] REPLACED WEB-INTERCOSTAL AND FASTENER LOCATED BS 927 TO BS 947.5 STRINGER 25R AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9; AND DSDR SWAA2024111447725Frame · crackedCRACK FRAME ON BS 312 BETWEEN S-5L T S-6L FWD GALLEY AND LAV 2024-634332<[01] PERFORMED REPAIR ON FRAME BS 312 BETWEEN S-5L TO S-6L FWD GALLEY AND LAV IAW EA M-22-153-0124 ?SEE INDIVIDUAL SIGN OFF BELOW?.;[02] CERTIFIED CORRECTIVE ACTION STEP 1SDR SWAA2024111447726Web · crackedCRACK WEB LOCATED BS 294.5 TO BS 303.9 AND S-16L AT PASSENGER CABIN 2024-634334<[01] REPLACED WEB-INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AND S-16L AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02; DWG: 141A8180 SHEET:27 REV:C. SEE INDIVISDR SWAA2024111447724Angle · crackedCRACK ANGLE LOCATED BS 291.5 TO BS 294.5 AND S-17R AT FWD GALLEY AREA 2024-634333<[01] REPLACED ANGLE (CLIP) LOCATED BS 291.5 TO BS 294.5 AND STRINGER 17R AT FWD GALLEY AREA IAW B737-700 SRM-51-40-02-0G; SRM-51-10-02-0G-0 Ï¿½TEM 9 AND DWG:141A8310 SHEET:25 REVSDR SWAA2024111447921Strap · corrodedCORROSION ON STRAP LOCATED BETWEEN BS 787 AND BS 793.5; STRINGER 25; WL 156 AFT CARGO COMPARTMENT 2024-634339<[01] TOOL USED: MULTIMETER P/N: FLUKE-289 S/N:61180136 DUE DATE: 10-JUL-25; TOOL USED: THERMOMETER P/N: FLUKE 566 S/N: 65900104WS DUE DATE: 17-OCT-25 SDR SWAA2024111447922Angle · corrodedCORROSION ANGLE - SUPPORT LOCATED BETWEEN BS 767 AND BS 787; STRINGER 25R; WL 156 AFT CARGO COMPARTMENT 2024-634340<[01] REPLACED ANGLE - SUPPORT LOCATED BETWEEN BS 767 AND BS 787; STRINGER 25R; WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DWG 14SDR SWAA2024111447923Support · corrodedCORROSION SUPPORT ZEE LOCATED BETWEEN BS 727B AND BS 727D STRINGER 25L WL 156 AFT CARGO COMPARTMENT 2024-634341<[01] REPLACED SUPPORT ZEE; [2] SPLICE SIDE PLATE (3 E/A) AND FASTENERS LOCATED BETWEEN BS 727 TO BS 847 STRINGER 25L WL 156 AFT CARGO COMPARTMENT IASDR SWAA2024111347920Web · corrodedCORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS 767 AND BS 787; STRINGER 25R AFT CARGO COMPARTMENT 2024-634338 CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS 767 AND BS 787 STRINGER 25R WL 155.5 AFT CARGO COMPARTMENT<[01] REPLACED WEB - INTERCOSTAL AND FASTENERSDR SWAA2024111347630Girt Bar · out of adjustDETERIORATED HARDWARE ON GIRT BAR FITTING FWD ENTRY AND SERVICE DOOR A T PASSENGER CABIN 2024-634328<[01] REPLACED HARDWARE ON GIRT BAR FITTING FWD ENTRY AND SERVICE DOOR AT PASSENGER CABIN I.A.W B737-700 AMM 25-66-02-400-801 THE INSTALLATION WILL BE DOCUMENTESDR SWAA2024111447333Scuff Plate · crackedCRACK ON AFT CORNER SCUFF PLATE LOCATED ON FWD CARGO COMPARTMENT 2024-634300<[01] TOOL USED: RADIOMETER/PHOTOMETER; P/N: XRP-3000; S/N: 1998072; DUE DATE: 23-JAN-25;[02] REPAIRED BY WELDING AFT CORNER SCUFF PLATE LOCATED ON FWD CARGO COMPARTMENT IAW BOEING 737SDR SWAA2024111447334Scuff Plate · crackedCRACK ON FWD CORNER SCUFF PLATE LOCATED ON FWD CARGO COMPARTMENT 2024-634299<[01] TOOL USED: RADIOMETER/PHOTOMETER; P/N: XRP-3000; S/N: 1998072; DUE DATE: 23-JAN-25;[02] REPAIRED BY WELDING FWD CORNER SCUFF PLATE LOCATED ON FWD CARGO COMPARTMENT I. A. W. BOEINSDR SWAA2024111447516Intercostal · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS277 TO BS 294.5 AND BL 0 FWD GALLEY AND LAV 2024-634311<[01] REPLACED WEB AND FASTENERS BTW BS 270 TO BS 294.5 AT BL 0 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G AND DWG 141A540SDR SWAA2024111447629Vapor Barrier · crackedCRACK ON VAPOR BARRIER LOCATED BS 663.75 RBL 35 AT MAIN WHEEL WELL COMPARTMENT 2024-634324 CRACK ON VAPOR BARRIER LOCATED BS 663.75 RBL 35 WL 166 AT MAIN WHEEL WELL COMPARTMENT<[01] TOOL USED SCALE P/N CR5200 S/N 8343110774 DUE DATE 28-FEB-25;[02] TOOL USED HOSDR SWAA2024111447520Angle · crackedCRACK ANGLE LOCATED BS867 BETWEEN S-2R TO S-3R AT PASSENGER CABIN 2024-634319<[01] REPLACED ANGLE (BRACKET) AND FASTENERS LOCATED BS867 BETWEEN S-2R TO S-3R AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G AND DWG: 146A7901 SHEET:66 SDR SWAA2024111347517Intercostal · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND RBL 13 FWD GALLEY AND LAV 2024-634312 CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND RBL 11.05 FWD GALLEY AND LAV<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE AND FASSDR SWAA2024111347518Web · crackedCRACK WEB LOCATED BS 847 TO BS 867 AND LBL 23 UPPER POSITION AT AFT CARGO COMPARTMENT 2024-634313<[01] REPLACED WEB AND FASTENERS LOCATED BS 847 TO BS 867 AND LBL 23 UPPER POSITION AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG# 149SDR SWAA2024111346252Light · deterioratedDETERIORATED PHOTOLUMINESCENT STRIP (10 FT) AT PASSENGER CABIN 2024-634173<[01] REPLACED PHOTOLUMINESCENT STRIP (10 FT) AT PASSENGER CABIN I.A.W SOPM 20-50-12 REV. 56;[02] COMPLETED JOBSDR SWAA2024111446251Flap · debondedCUSTOMER REQUEST - DEBONDED EXTERNAL SKIN IB MAIN FLAP TRAILING EDGE WEDGE LOWER SURFACE AT RT WING 2024-634151<[01] TOOL USED; CALIPER PN: 8647A42; SN/ A22356048; DUE DATE: 25-JUL-25;[02] TOOL USED: ULTRASONIC FLAW DETECTOR; P/N: EPOCH 650; S/N: 190859705; DUSDR SWAA2024111446250Flap · debondedCUSTOMER REQUEST - DEBONDED EXTERNAL SKIN IB MAIN FLAP TRAILING EDGE WEDGE LOWER SURFACE AT LT WING 2024-634150<[01] TOOL USED; CALIPER PN: 8647A42; SN: A22356048; DUE DATE: 25-JUL-25.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV; S/N: 18185781; DUE DATE: 15-FESDR SWAA2024100344499Overheat Loop · false activationWHEEL WELL FIRE WARNIG INDICATION AFTER GEAR RETRACTION ON TAKEOFF<[01] OK TO CONTINUE PER MEL 26-4-01 SP 1 AND SP 3 C/W ATH 216807;[02] REMOVED AND REPLACED WHEEL WELL. OVERHEAT DETECTOR ELEMENT PER AMM 26-18-02SDR SWAA2024090534148Door · crackedRMLG MIDDLE DOOR CRACKED AT LWR FWD CUTOUT.<[01] OK TO CONTINUE SERVICE PER AUTH# 212644. REMOVED R/H MLG CTR & INNER DOOR. I.A.W. AMM 32-13-11SDR SWAA2024090433095Floor Panel · crackedFWD CARGO FLOOR PANEL 120CF CRACKED<[01] R&R CARGO PANEL PER AMM 25-52-10 AND ATTACHED EASDR SWAA2024051484690Girt Bar · damagedCREW REPORTS FWD SERVICE DOOR GIRT BAR (AFT) CLIP IS BENT<[01] STRAIGHTENED OUT FWD SERVICE DOOR GIRT BAR CLIP PER S.I.P.SDR SWAA2024050782990Girt Bar · looseFWD SERVICE DOOR AFT GIRT BAR CLIP IS LOOSE<[01] INSPECTED GIRT BAR AND CLIPS AT FWD SERVICE DOOR IAW AMM 25-66-01. ALL FASTENERS ARE INSTALLED AND GIRT BAR SECURITY IS SATISFACTORY. A/C OK FOR SERVICE.SDR SWAA2024020648522Battery Pack · inoperativeL/H EMERGENCY EXIT DOOR LIGHTS INOP<[01] REMOVED AND REPLACED EMERG BATTERY PACK<BR>PERFORMED OPS CHECK NO FAULTS NOTED <BR>IN REF TO AMM 33-51-06SDR SWAA2024010837173Panel · crackedPANEL 621PB CRACKED AT AFT INBD EDGE<[01] REMOVED PANEL 621PB FROM A/C TO FOM;[02] C/W EA 24-157-00026 AS REQ INSTALLED PANEL;[03] C/WSDR SWAA2024010437166Lens · out of adjustPASSENGER CABIN EMERGENCY EXIT LIGHT NOT SECURE AT 22FED.<[01] SECURED 22FED PASSENGER CABIN EMERGENCY EXIT LIGHT LENS ASSY IN REF AMM 33-51-03.SDR SWAA2023092704653Slide · dislodgedL1 DOOR SLIDE DISLODGED<[01] RE-PACKED SLIDE IAW AMM MT 725-61-06SDR SWAA2023050131235Battery Pack · inoperativeEMERGENCY EXIT LIGHT OVER AFT SERVICE DOOR AND LAST 4 CABIN LIGHTS CAME ON AND OFF DURING FLIGHT<[01] R&R LEFT AFT EMERG LIGHT BATTER AND CHARGER IRW AMM 33-51-06; OPS TEST GOODSDR SWAA2023012391039Shield · corrodedCORROSION ON SHIELD WEB LOCATED BTW BS 767 TO BS 787 RBL 21 AND WL 156.5 AT AFT CARGO COMPARTMENT 2022-701136<[01] REPLACED NEW SHIELD WEB AND FASTENERS LOCATED BTW BS 767 TO BS 787 RBL 21 AND WL 156.5 AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02 Ï¿½TEM SDR SWAA2023011990269Web · crackedCRACKED WEB, BS 500B - 500C, S25 - 26L IN THE FWD CARGO BAY. REPLACED THE WEB IAW SRM 51-10-02, AND DWG 143A7505, SHEET 81, REV-.
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