N287WN
Service difficulty reports · 245
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 = 'N287WN' 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 = 'N287WN' 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 SWAA2026073028065Cover · brokenEMERGENCY EXIT ROW LIGHT COVER LEFT SIDE BROKEN. R & R LT EX. ROW LIGHT ASSY IAW MM 33-51-01, OPS CHECK NORMAL.SDR SWAA2026061510784Balance Weight · corrodedRUDDER COUNTER BALANCE WEIGHT CORRODED AND ERODED. REPLACED THE RUDDER BALANCE WEIGHT IAW CMM 55-40-09.SDR SWAA2026061010781Battery Pack · no testAFT EMERGENCY EXIT BATTERY PACK M1674 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK PER AMM 33-51-06.SDR SWAA2026033083158Extinguisher · low pressureCOCKPIT FIRE EXTINGUISHER PRESSURE BELOW LIMITS<[01] R/R COCKPIT FIRE EXT. IAW AMM 26-26-01SDR SWAA2025110430971Girt Bar · out of adjustGIRT BAR ON L1 DOOR HARD TO GET ON AND OFF CLIPS. RESECURED GIRT BAR ON L1 DOOR PER AMM 25-66-01.SDR SWAA2025103030144Girt Bar · unsecureFAS REPORT L1 DOOR LEFT SIDE SLIDE GIRT BAR IS LOOSE. SECURED THE GIRT BAR TO CLIP IAW AMM 25-66-01. OPS CHKD GOOD.SDR SWAA2025040220175Handle · looseFLT ATT ASSIST HANDLE AFT OF L1 DOOR IS LOOSE 2025-168124 <[01]. CORRECTED INSTALL ASSIST HANDLE AFT OF L1 DOOR I.A.W AMM 25-21-25-420-801 STEP 3. B. (5); [02] INSTALL ASSIST HANDLE AFT OF L1 DOOR I.A.W AMM 25-21-25-420-801 STEP 3. B. (5).SDR SWAA2025040219535Support · corrodedFAULT RAISED TO CAPTURE MANDATORY MEASUREMENT OF CORROSION ON SUPPORT ZEE LOCATED BTW BS727E TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT ADDING RII LABOR ROW REMOVED BY ERROR ON FAULT TTG8Q00Z1GCE <[01]. REPLACED SUPPORT ZEE LOCATED ON BTW BS727 TO BS767 WSDR SWAA2025040704750Seat Track · crackedCUSTOMER REQUEST AAI INSPECTION REFERENCE V909529 - PASSENGER CABIN STA 727B LBL 45.5 IB SEAT TRACK FLANGE AFT FASTENER HOLE CRACKED. MISSING EA IDENTIFIER PER STEP 29 OF EA 130808. 2025-168072<[01] REPAIR SEAT TRACK FLANGE AFT FASTENER CORRECTLY MARKED LOC. OSDR SWAA2025040414253Seat Track · crackedCUSTOMER REQUEST AAI INSPECTION REFERENCE V909529 - PASSENGER CABIN STA 727B LBL 45.5 IB SEAT TRACK FLANGE AFT FASTENER HOLE CRACKED. MISSING EA IDENTIFIER PER STEP 29 OF EA 130808. 2025-168072 <[01]. REPAIR SEAT TRACK FLANGE AFT FASTENER CORRECTLY MARKED LOSDR SWAA2025040702662Skin · corrodedCORROSION ON WING CENTER SECTION UPPER SKIN LOC. AT STA 663.75 AND LBL 45.57 2025-168032<[01] TOOL USED ON STEP 4:EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:220272512; DUE DATE:05-FEB-26.;[02] TOOL USED ON STEP 5:EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600DSDR SWAA2025040214240Skin · corrodedCORROSION ON WING CENTER SECTION UPPER SKIN LOC. AT STA 663.75 AND LBL 45.57 2025-168032 <[01]. TOOL USED ON STEP 4: EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:220272512; DUE DATE:05-FEB-26.; [02] TOOL USED ON STEP 5: EDDY CURRENT FLAW DETECTOR P/N:NORTESDR SWAA2025040202312Bracket · crackedCRACK ON BRACKET STRUCTURE WING CENTER SECTION LOCATED BS540 AND BS578 AT LEVEL BL6 KEEL BEAM 2025-168021<[01]. REPLACED BRACKET LOCATED ON STRUCTURE WING CENTER SECTION BS540 AT LEVEL BL6 KEEL BEAM IAW B737 700 SRM 51-40-02-0G AND DWG 149A7701 SHEET 3 REV A.SDR SWAA2025040202176Plate · crackedCRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED IRSS215 AT RT WING 2025-168012 <[01]. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS215 AT RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2001 SHEET 45 REV-; AND EVALUATED CRACK AND NOT FOUND ALLOWABLE DAMASDR SWAA2025040201604Support · corrodedCORROSION ON SUPPORT ZEE LOCATED BTW BS727E TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT 2025-167994<[01] FABRICATED A NEW SUPPORT ZEE LOCATED ON BTW BS727 TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN OFF BELOSDR SWAA2025040201603Shield · corrodedCORROSION ON SHIELD LOCATED BTW BS767 TO BS794.3 WL156 AND RBL22 AT AFT CARGO COMPARTMENT 2025-167993<[01] REPLACED SHIELD LOCATED BTW BS767 TO BS794.3 WL156 AND RBL22 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND DRAWING 146A0081 SHEET 31SDR SWAA2025040114234Shield · corrodedCORROSION ON SHIELD LOCATED BTW BS767 TO BS794.3 WL156 AND RBL22 AT AFT CARGO COMPARTMENT 2025-167993<[01] REPLACED SHIELD LOCATED BTW BS767 TO BS794.3 WL156 AND RBL22 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND DRAWING 146A0081 SHEET 31SDR SWAA2025040114235Support · corrodedCORROSION ON SUPPORT ZEE LOCATED BTW BS727E TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT 2025-167994<[01] FABRICATED A NEW SUPPORT ZEE LOCATED ON BTW BS727 TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN OFF BELOSDR SWAA2025040201442Tie Clip · crackedCRACK TIE CLIP LOCATED BS277 AND STR10R PASSENGER CABIN 2025-167974 <[01]. REPLACED NEW TIE CLIP LOCATED BS277 AND STR10R PASSENGER CABIN IAW B737-700 SRM-51-40-03-0G-O AND DWG-141A1110 SHEET 17 REV - . SEE INDIVIDUAL SIGN OFF BELOW.; [02] CERTIFIED CORRECTIVESDR SWAA2025040201091Angle · crackedCRACK ANGLE BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB 2025-167865<[01] REPLACED ANGLE BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02;[02] REPLACED ANGLE BLADE ACCESS PANEL SDR SWAA2025040201093Access Panel · crackedCRACK ANGLE BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB 2025-167870<[01] REPLACED ANGLE BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02;[02] REPLACED ANGLE BLADE ACCESS PANEL SDR SWAA2025040700756Stub Frame · crackedCRACK STUB FRAME LOCATED STA 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2025-167697<[01] REPLACED STUB FRAME; SERATE PLATE (2 EA) AND LOWER REVEAL CORNER LOCATED BS 294.5 TO BS 296 BETWEEN STR14 R TO STR 17 R FWD GALLEY AREA B737-700 SRM 51-40-02 AND DWG 141A83SDR SWAA2025040700760Nut Plate · crackedCRACK RAIL NUT PLATE OFSS 449 OUTBOARD FIXED LEADING EDGE AT RT WING 2025-167717<[01] REPLACED RAIL NUT PLATE OFSS 449 OUTBOARD FIXED LEADING EDGE AT RT WING IAW B737-700 DWG 112A4402 SHEET 13 REV - AND SRM 51-40-02; SRM 51-10-02 SEE INDIVIDUAL SIGN OFF BELOW;SDR SWAA2025040700762Nut Plate · crackedCRACK RAIL NUT PLATE OFSS 371 FIXED LEADING EDGE AT LT WING 2025-167744<[01] REPLACED RAIL NUT PLATE OFSS 371 FIXED LEADING EDGE AT LT WING IAW B737-700 DWG 112A4402 SHEET 13 REV - AND SRM 51-40-02; SRM 51-10-02 SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETEDSDR SWAA2025040700763Nut Plate · crackedCRACK RAIL NUT PLATE OFSS 541 FIXED LEADING EDGE AT LT WING 2025-167738<[01] REPLACED RAIL NUT PLATE OFSS 541 FIXED LEADING EDGE AT LT WING IAW B737-700 DWG 112A4402 SHEET 13 REV - AND SRM 51-40-02; SRM 51-10-02 SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETEDSDR SWAA2025040700922Access Panel · crackedCRACK ON HOLES LOCATED ACCESS PANEL 661CB AT RT WING 2025-167784<[01] STEP 12 TOOL USED ULTRASONIC FLAW DETECTOR P/N: EPOCH 600; S/N: 120357005; CAL DUE DATE: 10-JUN-25;[02] TOOL USED: MULTIMETER P/N: FLUKE 87-V; S/N: 65700125; DUE DATE: 09-JAN-26. TOOL USED HSDR SWAA2025040700752Web · crackedCRACK WEB TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING 2025-167701<[01] REPLACED WEB LOC. ON TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 115A2512 SHEET 14 REV A. SEE INDIVIDUAL SIGN OFF SDR SWAA2025040700751Support Angle · crackedCRACK SUPPORT ANGLE FIXED TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT LT WING 2025-167645<[01] REPLACED FITTING LOCATED FIXED TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 115A2930 SHEETSDR SWAA2025040700754Angle · crackedCRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING 2025-167685<REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 6 SDR SWAA2025040200919Scuff Plate · crackedCRACK FWD SERVICE DOOR SCUFF PLATE AT PASSENGER CABIN 2025-167749 <[01]. TOOL USED: DIGITAL CALIPER P/N: 8647A42 S/N: B22440130 DUE DATE: 20-SEP-25; [02] STEP 4. TOOL USING RADIOMETER/PHOTOMETER P/N: XRP-3000; S/N: 1753759; DUE DATE: 30-JUN-25.; [03] REPAIREDSDR SWAA2025040200761Support · corrodedCORROSION ANGLE - SUPPORT LOCATED BTW STA 294.5 TO STA 312 RBL 56 AND WL 208.1 AT FWD GALLEY AREA 2025-167730 <[01]. REPLACED NEW ANGLE - SUPPORT LOCATED BTW STA 294.5 TO STA 312 RBL 56 AND WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 SEE INDIVIDUAL SSDR SWAA2025040214212Stub Frame · crackedCRACK STUB FRAME LOCATED STA 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2025-167697 <[01]. REPLACED STUB FRAME; SERATE PLATE (2 EA) AND LOWER REVEAL CORNER LOCATED BS 294.5 TO BS 296 BETWEEN STR14 R TO STR 17 R FWD GALLEY AREA B737-700 SRM 51-40-02 AND DWG 141ASDR SWAA2025040214217Access Panel · crackedCRACK ON HOLES LOCATED ACCESS PANEL 661CB AT RT WING 2025-167784<[01] STEP 12 TOOL USED ULTRASONIC FLAW DETECTOR P/N: EPOCH 600; S/N: 120357005; CAL DUE DATE: 10-JUN-25;[02] TOOL USED: MULTIMETER P/N: FLUKE 87-V; S/N: 65700125; DUE DATE: 09-JAN-26. TOOL USED HSDR SWAA2025040214210Web · crackedCRACK WEB TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING 2025-167701<[01] REPLACED WEB LOC. ON TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 115A2512 SHEET 14 REV A. SEE INDIVIDUAL SIGN OFF SDR SWAA2025040214211Angle · crackedCRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING 2025-167685<[01] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK ANGLE INBOARD AUXILIARY TRACK OF SLSDR SWAA2025040214209Fitting · crackedCRACK SUPPORT ANGLE FIXED TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT LT WING 2025-167645<[01] REPLACED FITTING LOCATED FIXED TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 115A2930 SHEETSDR SWAA2025040114213Nut Plate · crackedCRACK RAIL NUT PLATE OFSS 449 OUTBOARD FIXED LEADING EDGE AT RT WING 2025-167717<[01] REPLACED RAIL NUT PLATE OFSS 449 OUTBOARD FIXED LEADING EDGE AT RT WING IAW B737-700 DWG 112A4402 SHEET 13 REV - AND SRM 51-40-02; SRM 51-10-02 SEE INDIVIDUAL SIGN OFF BELOW;SDR SWAA2025040114215Nut Plate · crackedCRACK RAIL NUT PLATE OFSS 541 FIXED LEADING EDGE AT LT WING 2025-167738<[01] REPLACED RAIL NUT PLATE OFSS 541 FIXED LEADING EDGE AT LT WING IAW B737-700 DWG 112A4402 SHEET 13 REV - AND SRM 51-40-02; SRM 51-10-02 SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETEDSDR SWAA2025040114214Nut Plate · crackedCRACK RAIL NUT PLATE OFSS 371 FIXED LEADING EDGE AT LT WING 2025-167744<[01] REPLACED RAIL NUT PLATE OFSS 371 FIXED LEADING EDGE AT LT WING IAW B737-700 DWG 112A4402 SHEET 13 REV - AND SRM 51-40-02; SRM 51-10-02 SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETEDSDR SWAA2025040100755Floor Support · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 312 TO STA 328 AND RBL 31 FWD GALLEY AND LAV 2025-167681<[01] REPLACED WEB INTERCOSTAL WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 312 TO STA 328 AND RBL 31 FWD GALLEY AND LAV IAW B737-700 SRM 51-40SDR SWAA2025040100757Floor Support · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 277 TO STA 294.5 AND BL 0 FWD GALLEY AND LAV 2025-167675<[01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 277 TO STA 294.5 AND BL 0 FWD GALLEY AND LAV B737-700 SRM 51-40-02 AND DWG 141A5400 SSDR SWAA2025040100758Floor Support · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 312 TO STA 328 AND LBL 47 FWD GALLEY AND LAV 2025-167669<[01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 312 TO STA 328 AND LBL 47 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A54SDR SWAA2025040100759Floor Support · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 328 TO STA 344 AND LBL 47 FWD GALLEY AND LAV 2025-167671<[01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 328 TO STA 344 AND LBL 47 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A54SDR SWAA2025040700235Stub Frame · crackedCRACK INDICATION ON STUB FRAME LOCATED ON BS 294.5 BETWEEN STR-8 TO STR-9 IN FORWARD GALLEY DOOR RH SIDE; CRACK LENGTH 1.272 INCHES APPROX. 2025-167597<[01] REPLACED STUB FRAME LOC. ON BS 294.5 BTW S-7R TO S-9R AT FWD GALLEY DOOR AREA IAW B737-700 SRM 51-40-02SDR SWAA2025040700577Angle · crackedCRACK ANGLE ON INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING 2025-167631<[01] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK ANGLE INBOARD AUXILIARY TRACK OFSDR SWAA2025040700579Angle · crackedCRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING 2025-167634<[01] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK ANGLE INBOARD AUXILIARY TRACK OF SLSDR SWAA2025040214194Stub Frame · crackedCRACK INDICATION ON STUB FRAME LOCATED ON BS 294.5 BETWEEN STR-8 TO STR-9 IN FORWARD GALLEY DOOR RH SIDE; CRACK LENGTH 1.272 INCHES APPROX. 2025-167597 <[01]. REPLACED STUB FRAME LOC. ON BS 294.5 BTW S-7R TO S-9R AT FWD GALLEY DOOR AREA IAW B737-700 SRM 51-40SDR SWAA2025040214207Angle · crackedCRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING 2025-167634<[01] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK ANGLE INBOARD AUXILIARY TRACK OF SLSDR SWAA2025040214206Angle · crackedCRACK ANGLE ON INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING 2025-167631<[01] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK ANGLE INBOARD AUXILIARY TRACK OFSDR SWAA2025040400226Support Bracket · crackedCRACK SUPPORT BRACKET LOCATED STA 695 AT LEVEL LBL 24.75 AT PASSENGER CABIN 2025-167579 <[01]. TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 2
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