N939WN
Service difficulty reports · 200
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 = 'N939WN' 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 = 'N939WN' 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 SWAA2026081007254Girt Bar · unpackedFA REPORTS L1 GIRT BAR HARD TO RELEASE. REPACKED EXCESS GIRT MATERIAL AT BOTTOM OF SLIDE AMM 25-66-01. OP CHECK GOODSDR SWAA2026072304935Flashlight · inoperativeFWD ENTRY NR 1 EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FWD ENTRY NR 1 EMERGENCY FLASHLIGHT REF AMM 25-64-00.SDR SWAA2026061510979Seat · out of adjustPASSENGER CABIN SEAT 14B, WHICH IS IN AN EMERGENCY EXIT ROW, RECLINES AND SHOULDN`T. LOCKED OUT SEAT 14B RECLINE IAW CMM 25-21-45.SDR SWAA2026020566854Contact · dirtyAFT FA MEGAPHONE INOPERATIVE. CLEANED BATTERY CONTACTS AND ACCOMPLISHED MEGAPHONE OPS CHECK IAW AMM 25-64-00, CHECKED NORMAL.SDR SWAA2026011961926Seat · out of adjustPASSENGER CABIN EMERGENCY EXIT ROW SEAT 14B RECLINES. LOCKED OUT 14B SEAT RECLINE IAW CMM 25-21-42SDR SWAA2025120134400Fitting · crackedRIB FITTING IS CRACKED AT STAB BL 281.81 RH SIDE. PERFOMED REPAIR IAW SRM 55-10-90-2R-1-A01330, REPAIR 1.SDR SWAA2025090209425Seal · crackedLH HORIZONTAL STAB UPPER FWD SLIDER SEAL IS CRACKED. REMOVED AND REPLACED SEAL PER AMM 53-31-31.SDR SWAA2025090209426Seal · crackedRH HORIZONTAL STAB UPPER FWD SLIDER SEAL CRACKED. REMOVED AND REPLACED SEAL PER AMM 53-31-31.;[02] C/W INSPECTIONSDR SWAA2025040219829Web · crackedCRACK ON WEB LOCATED BTW BS440 TO BS BS460 AT LEVEL S-25L FWD CARGO COMPARTMENT 2025-203869<[01] FABRICATED WEB LOCATED BTW BS440 TO BS BS460 AT LEVEL S-25L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-05; SRM 51-20-01; SRM 51-30-01 AND DWG 143A7510 REV C. SEESDR SWAA2025040709653Angle · damagedELONGATED HOLE ANGLE LOCATE BETWEEN BS767 TO BS794.3 RBL21 AND WL156 AT AFT CARGO COMPARTMENT 2025-203852<[01] REPLACED ANGLE AND LOCATED BETWEEN BS767 TO BS794.3 RBL21 AND WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; AND SRM 51-10-02 ITEM 9 AND DSDR SWAA2025040706455Lens · misinstalledINCORRECTLY EMERGENCY LIGHT LENS GALLEY 1 AT FWD GALLEY AREA 2025-203843<[01] REPLACED EMERGENCY LIGHT LENS GALLEY AREA 1 AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-801 STEP 2.C.(1).(A)(2) AND (3).(4);[02] JOB COMPLETEDSDR SWAA2025040706454Lens · wrong partINCORRECTLY EMERGENCY LIGHT LENS GALLEY 4 AT AFT GALLEY AREA 2025-203844<[01] REPLACED EMERGENCY LIGHT LENS GALLEY 4 AT AFT GALLEY AREA IAW B737-700 AMM 33-51-01-960-801 STEP 2.C.(1).(A)(2) AND (3).(4);[02] JOB COMPLETEDSDR SWAA2025040705828Support · corrodedCORROSION SUPPORT ZEE LOCATED BETWEEN BS727 TO BS767 RBL21 AND WL156 AFT CARGO COMPARTMENT 2025-203782<SDR SWAA2025040715603Shield · corrodedCORROSION SHIELD WEB LOCATED BETWEEN BS767 TO BS794.3 RBL21 AND WL156 AT AFT CARGO COMPARTMENT 2025-203783<[01] REPLACED SHIELD WEB AND FASTENERS LOCATED BETWEEN BS767 TO BS794.3 RBL21 AND WL156 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02; SRM 51-10-0SDR SWAA2025040715604Support · corrodedCORROSION SUPPORT ZEE LOCATED BETWEEN BS727C TO BS807 LBL21 AND WL156 AFT CARGO COMPARTMENT 2025-203784<[01] REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 847 LBL 21 AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWSDR SWAA2025040705829Shield · corrodedCORROSION SHIELD WEB LOCATED BETWEEN BS767 TO BS794.3 RBL21 AND WL156 AT AFT CARGO COMPARTMENT 2025-203783<SDR SWAA2025040705827Support Angle · crackedCRACK ANGLE - SUPPORT LOCATED STA947.5 AND LBL11 AT AFT CARGO COMPARTMENT 2025-203797<[01] REPLACED ANGLE - SUPPORT LOCATED STA947.5 AND LBL11 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND SRM 51-40-02 AND DWG # 149A8103 SHEET 7 REV: SDR SWAA2025040715592Pressure Deck · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB LBL 30 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH 0.250 INCH APPROXIMATELY. ) 2025-203749<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138103; DUE DATE: 10-JUN-25.;[02] TOOL USED: SDR SWAA2025040705528Pressure Deck · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB RBL 41 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH 0.312 INCH APPROXIMATELY. ) 2025-203751<[01] ON STEP 6 AND 7: TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X12101V022240; DUE DATE: 28 MAR 25;[0SDR SWAA2025040705527Pressure Deck · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB LBL 30 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH 0.250 INCH APPROXIMATELY. ) 2025-203749<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138103; DUE DATE: 10-JUN-25.;[02] TOOL USED: SDR SWAA2025040705833Floorbeam · corrodedCORROSION ANGLE FLOOR STRUCTURE LOCATED STA947.5 AND RBL4 WL156 AT AFT CARGO COMPARTMENT 2025-203796<SDR SWAA2025040705681Floorbeam · crackedCRACK LOWER ANGLE FLOOR STRUCTURE BS 695 AND RBL 24.75 CENTER SECTION 2025-203648<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 29-JAN-26.SDR SWAA2025040705836Rib · crackedCRACK RIB 8 ON ACCESS PANEL 321A AT VERTICAL STABILIZER 2025-203809<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26.;[02] REPLACED RIB 8 AND FASTENERS LOCATED ON PANEL 312A AT VERTICAL STABILIZER IAW B737-700 SSDR SWAA2025040715599Angle · crackedCRACK LOWER ANGLE FLOOR STRUCTURE BS 695 AND RBL 24.75 CENTER SECTION 2025-203648<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 29-JAN-26.SDR SWAA2025040705830Support · corrodedCORROSION SUPPORT ZEE LOCATED BETWEEN BS727C TO BS807 LBL21 AND WL156 AFT CARGO COMPARTMENT 2025-203784<SDR SWAA2025040405831Track · crackedCRACK CARGO TRACK RBBL 13.84 LOCTAED BS727E AFT CARGO COMPARTMENT 2025-203785 <[01]. STEP 5 AND 6 TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 240497907; DUE DATE: 27-AUG-25; [02] INSTALLED PERMANENT REPAIR PARTS [1] TRACK EXTRUSION [2] TRACK SPLICE SDR SWAA2025040205832Cargo Track · crackedCRACK CARGO TRACK RBBL 13.84 LOCATED BS727C AFT CARGO COMPARTMENT 2025-203786<[01] STEP 4 TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 240497907; DUE DATE: 27-AUG-25;[02] STEP 5 TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 240497907; DUE DATESDR SWAA2025040205826Cargo Track · crackedCRACK CARGO TRACK LBBL 17.24 LOCATED BS727E AFT CARGO COMPARTMENT 2025-203789<[01] STEP 4 AND 5 TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 240497907; DUE DATE: 27-AUG-25;[02] REPAIRED CARGO TRACK LOCATED BS 727D + 13? TO BS 727E + 11? LBL 17.24 AT ASDR SWAA2025040215605Floor Support · corrodedCORROSION ANGLE FLOOR STRUCTURE LOCATED STA947.5 AND RBL4 WL156 AT AFT CARGO COMPARTMENT 2025-203796<[01] REPLACED ANGLE FLOOR STRUCTURE AND FASTENERS LOCATED STA947.5 AND RBL4 WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 ANSDR SWAA2025040215602Support · corrodedCORROSION SUPPORT ZEE LOCATED BETWEEN BS727 TO BS767 RBL21 AND WL156 AFT CARGO COMPARTMENT 2025-203782<[01] REPLACED SUPPORT ZEE AND FASTENERS LOCATED BETWEEN BS727 TO BS767 RBL21 AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND SSDR SWAA2025040705346Shield · damagedELONGATED HOLE ON SHIELD WEB LOCATED BETWEEN STA492.4 TO STA500A AND RBL21 AT FWD CARGO COMPARTMENT 2025-203697<[01] REPLACED SHIELD WEB LOCATED BTW BS 492.4 TO BS 500A AND RBL 21 AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 AND DWG # 143A0080; SHEET 33SDR SWAA2025040705507Flashlight · inoperativeINOP WINDSCREEN LT SIDE FLASH LIGHT ASSY AT AFT GALLEY AREA (1 EA) 2025-203706<[01] REPLACED WINDSCREEN LT SIDE FLASH LIGHT ASSY AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM 25-64-00-SWA-807 AND DWG 25600001 REV K;[02] CORRECTED ITEM 1 <BR><BR>REPLACED WINDSCREESDR SWAA2025040715570Stringer Clip · crackedCRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2025-203695<[01] REPLACED GUSSET AND FASTENERS LOCATED BS 500D AND STRINGER 19L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG # 143A7902; SHEET 209; REV -.<BR>SEESDR SWAA2025040705347Angle · crackedCRACK ANGLE - CLIP LOCATED STA440 AND STR26L FWD CARGO COMPARTMENT 2025-203694<SDR SWAA2025040705348Stringer Clip · crackedCRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2025-203695<SDR SWAA2025040715569Angle · crackedCRACK ANGLE - CLIP LOCATED STA440 AND STR26L FWD CARGO COMPARTMENT 2025-203694<[01] REPLACED ANGLE CLIP LOCATED BS 440 STRINGER 26L AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 AND DWG # 143A7505 SHEET 118. SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPLACED ASDR SWAA2025040715571Stringer · crackedCRACK STRINGER 23L LOCATED STA540 FWD CARGO COMPARTMENT 2025-203705<[01] TOOL USED ON STEP 6. ET EQUIPMENT: P/N: NORTEC 600D; S/N: 60007161486; CAL DUE DATE: 06-SEP-25;[02] REPAIRED STRINGER 23L LOCATED BS 500D PLUS 10 INCHES TO BS 540 IAW BOEING 737-700 SRM 5SDR SWAA2025040705506Stringer · crackedCRACK STRINGER 23L LOCATED STA540 FWD CARGO COMPARTMENT 2025-203705<[01] TOOL USED ON STEP 6. ET EQUIPMENT: P/N: NORTEC 600D; S/N: 60007161486; CAL DUE DATE: 06-SEP-25;[02] REPAIRED STRINGER 23L LOCATED BS 500D PLUS 10 INCHES TO BS 540 IAW BOEING 737-700 SRM 5SDR SWAA2025040415572Flashlight · inoperativeINOP WINDSCREEN LT SIDE FLASH LIGHT ASSY AT AFT GALLEY AREA (1 EA) 2025-203706 <[01]. REPLACED WINDSCREEN LT SIDE FLASH LIGHT ASSY AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM 25-64-00-SWA-807 AND DWG 25600001 REV K; [02] CORRECTED ITEM 1. REPLACED WINDSCREEN SDR SWAA2025040705002Stub Frame · crackedCRACK INDICATION ON STUB FRAME LOCATED ON BS 296.5 BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 0.375 IN. APROX.AT PASSENGER CABIN 2025-203649<[01] REPLACED STUB FRAME AND FASTENERS LOC. BETWEEN STR7R TO STR11R AT FWD GALLEY AREA IAW B737-700 SRM 51-1SDR SWAA2025040715564Stub Frame · crackedCRACK INDICATION ON STUB FRAME LOCATED ON BS 296.5 BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 0.375 IN. APROX.AT PASSENGER CABIN 2025-203649<[01] REPLACED STUB FRAME AND FASTENERS LOC. BETWEEN STR7R TO STR11R AT FWD GALLEY AREA IAW B737-700 SRM 51-1SDR SWAA2025040705001Floorbeam · crackedCRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN LBL 24.75 TO LBL 45.5 AT PASSENGER CABIN 2025-203646<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN LBL 24.75 TO LBL 45.5 AT PASSENGER CABIN B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02 AND DWG 1SDR SWAA2025040705003Floorbeam · crackedCRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN RBL 24.75 TO RBL 45.5 AT PASSENGER CABIN 2025-203647<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN RBL 24.75 TO RBL 45.5 AT PASSENGER CABIN. B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02 AND DWG SDR SWAA2025040715563Floorbeam · crackedCRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN 2025-203644<[01] REPLACED FLOOR STRUCTURE BRAKE PANEL AND FASTENERS LOCATED ON BS 540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM-51-40-02-0G; B737-700 SRM-SDR SWAA2025040715565Floorbeam · crackedCRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN RBL 24.75 TO RBL 45.5 AT PASSENGER CABIN 2025-203647<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN RBL 24.75 TO RBL 45.5 AT PASSENGER CABIN. B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02 AND DWG SDR SWAA2025040705197Support · crackedCRACK BLADE SUPPORT STRUCTURE OF THE ACCESS PANEL 333AT AT LT HORIZONTAL STABILIZER 2025-203656<[01] REPLEACED BLADE SUPPORT STRUCTURE OF THE ACCESS PANEL 333AT AT LT HORIZONTAL STABILIZER B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9;[02] CORREDTED STEP 1 REPSDR SWAA2025040404999Panel · crackedCRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN 2025-203644 <[01]. REPLACED FLOOR STRUCTURE BRAKE PANEL AND FASTENERS LOCATED ON BS 540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM-51-40-02-0G; B737-700 SSDR SWAA2025040405000Panel · crackedCRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 TO RBL 24.75 AT PASSENGER CABIN 2025-203645 <[01]. REPLACED FLOOR STRUCTURE BRAKE PANEL AND FASTENERS LOCATED ON BS 540 BETWEEN BL 0 TO RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM-51-40-02-0G; B737-700 SSDR SWAA2025040715555Access Panel · crackedCRACK ACCESS PANEL 191D AT LOWER FUSELAGE 2025-203626<[01] TOOL USED CALIPER PN: 8647A43; SN: B22440130; DUE DATE: 20/SEP/25.;[02] TOOL USED; HOT BONDER PN: HCS9200B; SN: 16122983; DUE DATE: 22-FEB-26.;[03] TOOL USED; SCALE PN: SCA-301; SN: AE-412135; DUE DATESDR SWAA2025040704618Access Panel · crackedCRACK ACCESS PANEL 191D AT LOWER FUSELAGE 2025-203626<[01] TOOL USED CALIPER PN: 8647A43; SN: B22440130; DUE DATE: 20/SEP/25.;[02] TOOL USED; HOT BONDER PN: HCS9200B; SN: 16122983; DUE DATE: 22-FEB-26.;[03] TOOL USED; SCALE PN: SCA-301; SN: AE-412135; DUE DATE
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