N410WN
Service difficulty reports · 325
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 = 'N410WN' 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 = 'N410WN' 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 SWAA2025070782676Skin · crackedCRACKED INDICATION LOCATED AT BS 767+12.5 STR 1 CHEM-MILL STEP. REPAIRED PER EA 25-153-01606 WITH AN INSPECTION THRESHOLD DEFINED IN 25-153-01606-DTI.SDR SWAA2025061681898Skin · crackedPOSSIBLE CRACK INDICATION LOCATED AT CHEM-MILL STEP BS 767+7.25 AT S-1. PERFORMED UTPA OF CRACK INDICATION AREA IAW B737 NDT PART 4; 53-30-07. FOUND SMALL RED DOT INDICATION ON S-SCAN DISPLAY WITH AN A-SCAN PERCENTAGE OF 74%. PERFORMED MFEC INSPECTION AT INDSDR SWAA2025060979528Seat · out of rigSEAT 11D RECLINE INTO THE EXIT ROW<[01] ADJUSTED SEAT 11D PER CMM 25-21-42. OPS CHECK GOOD.SDR SWAA2025041424272Angle · corrodedFWD CARGO PIT R/H FLOOR TO SIDEWALL ANGLE CORRODED AROUND FASTENER HOLES FROM STATION 500 TO 500A<[01] CORROSION IS OUT OF LIMITS DUE TO PROXIMITY TO A FASTENER HOLE PER SRM 53-30-15-1A-1 FIG. 103 DETAIL D;[02] CORRECTED STATION 500-500A;[03] REMOVED FWD CARGOSDR SWAA2025022498804Cover · looseF.A. REPORTS EMERGENCY EXIT LIGHT BY FWD. ENTRY DOOR COVER CAME OFF.<[01] RE-INSTALLED THE COVER FOR THE FWD ENTRY DOOR EMERGENCY EXIT SIGN PER A.M.M. S.I.P.SDR SWAA2025020392107Cover · missingAFT F/A REPORTS AFT SERVICE DOOR SLIDE PULL HANDLE COVER IS MISSING<[01]. REMOVED AFTER SERVICE DOOR SLIDE AND SECURED INFLATION COVER OVER PULL HANDLE PER STEP 12 OF MT 725-6106 AND AMM 25-66-01.SDR SWAA2024102851968Light · contaminatedROWS 16ABC -18ABC AISLE PHOTOLUMINESCENT STRIP HAS MOISTURE IN IT.<[01] R&R PASSENGER CABIN PHOTOLUMINESCENT STRIPS AT ROWS 16ABC -18ABC IAW AMM 25-27-31. PARTS USED WERE SHIPSET LEFTOVERS. NO P/N.SDR SWAA2024102851967Light · contaminatedROWS 12DEF- 14DEF AISLE PHOTOLUMINESCENT STRIP HAS MOISTURE IN IT.<[01] R&R PASSENGER CABIN PHOTOLUMINESCENT STRIPS AT ROWS 12DEF- 14DEF IAW AMM 25-27-31. PARTS USED WERE SHIPSET LEFTOVERS. NO P/N.SDR SWAA2024102851966Light · contaminatedROWS 1ABC; 21ABC; 24ABC AISLE PHOTOLUMINESCENT STRIPS HAS MOISTURE IN THEM.<[01] R&R PASSENGER CABIN PHOTOLUMINESCENT STRIPS AT ROWS 1ABC; 21ABC; 24ABC IAW AMM 25-27-31. PARTS USED WERE SHIPSET LEFTOVERS. NO P/N.SDR SWAA2024071813986Slide · out of positionFLIGHT ATTENDANT REPORTS AFT SERVICE DOOR GIRT BAR IS ANGLED BEHIND SLIDE. REPOSITIONED SLIDE PACK MATERIAL; GIRT BAR INSTALLS NORMALLY IAW AMM 25-66-01. A/C OK FOR SERVICE.SDR SWAA2024020849741Girt Bar · looseFLT ATT REPORTS; AFT ENTRY GIRT BAR LOOSE @ RETAINER.<[01] OPS CK?D GIRT BAR PER M/M 25-66-02SDR SWAA2023112824750Cover · damagedAFT ENTRY COVER PLATE FOR DOOR HANDLE IS MISSING INTERIOR DOOR HANDLE COVER PLATE<[01] OK TO CONTINUE PER MEL 25-10-01 SP1B AUTH# 167863. REPLACED AFT ENTRY DOOR HANDLE COVER PER SIP.SDR SWAA2023083191567Scuff Plate · crackedCRACK ON FWD ENTRY DOOR SCUFF PLATE AT FWD GALLEY AREA 2023-508553<[01] TOOL USED DIGITAL CALIPER P/N: 500-193-30; S/N: 0000291; DUE DATE: 12/OCT/23.;[02] TOOL USED: RADIOMETER PHOTOMETER P/N: XRP-3000; S/N: 1753759; CAL DUE DATE: 14-OCT-23;[03] REPAIRED FWD ESDR SWAA2023090190773Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED ON ACCESS PANEL 651GB AT RT WING 2023-508530<[01] REPLACED NEW SUPPORT ANGLE LOCATED ON ACCESS PANEL 651GB AT RT WING IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02;[02] REPLACED NEW SUPPORT ANGLE LOCATED ON ACCESS PANEL 651SDR SWAA2023090190020Angle · crackedCRACK INTERNAL AREA INBOARD TRAILING EDGE TEE ANGLE LOCATED IRSS 214 LT WING 2023-508516<[01] REPLACED TEE ANGLE ON INTERNAL AREA INBOARD TRAILING EDGE LOC. IRSS 214 LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 115A2001 REV: ?.;[02] TASK CARD COMPLESDR SWAA2023090189305Angle · crackedCRACK INBOARD TRAILING EDGE TEE ANGLE LOCATED ON IRSS 211 AT RT WING 2023-508488<[01] REPLACED ANGLE LOCATED ON IRSS 211 AT RT WING.IAW. B737-700 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 AND DWG 115A2001 SHEET 8 REV: . TOOL USED: ELECTRONIC CALIPER. P/N: 50SDR SWAA2023090193386Unknown · crackedCRACK ON LINK ASSY AT RAM AIR INLET MECHANISM RT SIDE (2 EA) 2023-508486<[01] REPLACED LINK ASSY AT RAM AIR INLET MECHANISM RT SIDE (2 EA) I.A.W B737-700 DWG 213A3130 SHEET 9 REV. A; SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 ITEM 9 AND AMM 20-50-11-910-801.<SDR SWAA2023090193387Inlet · crackedCRACK ON LINK ASSY AT RAM AIR INLET MECHANISM LT SIDE (2 EA) 2023-508485<[01] REPLACED LINK ASSY AT RAM AIR INLET MECHANISM LT SIDE (2 EA) I.A.W B737-700 DWG 213A3130 SHEET 9 REV. A; SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 ITEM 9 AND AMM 20-50-11-910-801.<SDR SWAA2023083189558Intercostal · crackedCRACK WEB - INTERCOSTAL LOCATED BETWEEN BS500D TO BS520 AT LEVEL STR28L FWD CARGO COMPARTMENT 2023-508493<[01] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BETWEEN BS500D TO BS520 AT LEVEL STR28L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-0SDR SWAA2023083195740Fastener · crackedCRACK WEB - INTERCOSTAL LOCATED BETWEEN BS500D TO BS520 AT LEVEL STR28L FWD CARGO COMPARTMENT 2023-508493<[01] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BETWEEN BS500D TO BS520 AT LEVEL STR28L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-0SDR SWAA2023083189557Angle · crackedCRACK SUPPORT ANGLE LOCATED BS867 AND BETWEEN STR2R/STR3R AT PASSENGER CABIN 2023-508498<[01] REPLACED SUPPORT ANGLE LOC. BS867 AND BETWEEN STR2R TO STR3R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 146A7901 REV. ?.;[02] CORRECTED STEP 1SDR SWAA2023083189555Stringer · corrodedCORROSION STRINGER 25R LOCATED BS540 AT FWD CARGO COMPARTMENT 2023-508487<[01] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 221860711; CAL DUE DATE: 07-NOV-23;[02] TOOL USED : EDDY CURRENT EQUIPMENT P/N NORTEC500D S/N 00X12101V022237 DUE DATE: 26-JAN-24.;[03] REPAIRSDR SWAA2023083189559Stringer · corrodedCORROSION STRINGER 27L LOCATED BS540 AT FWD CARGO COMPARTMENT 2023-508494<[01] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 221860711; CAL DUE DATE: 07-NOV-23;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATSDR SWAA2023083189556Stringer · corrodedCORROSION STRINGER 27R LOCATED BS540 AT FWD CARGO COMPARTMENT 2023-508495<[01] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 221860711; CAL DUE DATE: 07-NOV-23;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATSDR SWAA2023090189123Support Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 261 PLUS 11 INCHES; AT DEFLECTION RIB AREA; RT WING 2023-508464<[01] REPLACED ANGLE TRAILING EDGE ORSS 261 PLUS 11 INCHES; AT DEFLECTION RIB AREA; RT WING IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DRAWING 115A2930 SHEET 8 REV -;[02]SDR SWAA2023090189118Angle · crackedCRACK ANGLE FRONT SPAR WEB LOCATED BOOST PUMP BONDING STRAP AT IFSS 121 AT LT WING 2023-508460<[01] REPLACED ANGLE FRONT SPAR WEB LOCATED BOOST PUMP BONDING STRAP AT IFSS 121 AT LT WING IAW B737-700 SRM 51-10-02.SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACED ANGSDR SWAA2023090189122Web · crackedCRACK ANGLE FRONT SPAR WEB LOCATED BOOST PUMP BONDING STRAP AT IFSS 121 AT RT WING 2023-508461<[01] REPLACED ANGLE FRONT SPAR WEB LOCATED BOOST PUMP BONDING STRAP AT IFSS 121 AT RT WING IAW B737-700 SRM 51-10-02.SEE INDIVIDUAL SIGN OFFS BELOW;[02] JOB COMPLETESDR SWAA2023090188872Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS 261 PLUS 11 INCHES; DEFLECTION RIB AREA LT WING 2023-508425<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 261 PLUS 11 INCHES; DEFLECTION RIB AREA LT WING IAW B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02-0G Ï¿½TEM 9;[02] TSDR SWAA2023083188873Fitting · wornWEAR ON GIRT BAR FITTING HARDWARE AND PLATE ON FWD ENTRY DOOR AT FWD GALLEY AREA 2023-508422<[01] REPLACED GIRT BAR FITTING HARDWARE AND PLATE ON FWD ENTRY DOOR AT FWD GALLEY AREA IAW BOEING 737-700 AMM-25-66-02-400-801;[02] REPLACED GIRT BAR FITTING HARDWARE SDR SWAA2023083188874Fitting · wornWEAR ON GIRT BAR FITTING HARDWARE AND PLATE ON FWD SERVICE DOOR AT FWD GALLEY AREA 2023-508423<[01] REPLACED ON GIRT BAR FITTING HARDWARE AND PLATE ON FWD SERVICE DOOR AT FWD GALLEY ARE IAW BOEING 737-700 AMM-25-66-02-400-801;[02] REPLACED ON GIRT BAR FITTING SDR SWAA2023083188625Fitting · deterioratedDETERIORATED ENTRY DOOR HARDWARE AND PLATE GIRT BAR FITTING AT AFT GALLEY AREA 2023-508385<[01] REPLACED ENTRY DOOR HARDWARE AND PLATE GIRT BAR FITTING AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801.;[02] COMPLETED JOBSDR SWAA2023083188624Fitting · deterioratedDETERIORATED SERVICE DOOR HARDWARE AND PLATE GIRT BAR FITTING AT AFT GALLEY AREA 2023-508387<[01] REPLACED SERVICE DOOR HARDWARE AND PLATE GIRT BAR FITTING AT AFT GALLEY IAW B737-700 AMM 25-66-02-400-801.;[02] COMPLETED JOBSDR SWAA2023083188731Stiffener · crackedCRACK STIFFENER FLOOR STRUCTURE LOCATED BS540 BETWEEN BL0 TO RBL 24.75 CENTER SECTION 2023-508412<[01] REPLACED STIFFENER AND FASTENERS ON FLOOR STRUCTURE LOCATED BS540 BETWEEN BL0 TO RBL 24.75 CENTER SECTION IAW B737-700 SRM 51-40-02; SRM 51-40-02 AND DWG 143SDR SWAA2023083195741Fastener · crackedCRACK STIFFENER FLOOR STRUCTURE LOCATED BS540 BETWEEN BL0 TO RBL 24.75 CENTER SECTION 2023-508412<[01] REPLACED STIFFENER AND FASTENERS ON FLOOR STRUCTURE LOCATED BS540 BETWEEN BL0 TO RBL 24.75 CENTER SECTION IAW B737-700 SRM 51-40-02; SRM 51-40-02 AND DWG 143SDR SWAA2023083188732Stiffener · crackedCRACK STIFFENER FLOOR STRUCTURE LOCATED BS 540 BETWEEN BL0 TO LBL 24.75 CENTER SECTION 2023-508413<[01] REPLACED STIFFENER AND FASTENERS ON FLOOR STRUCTURE LOCATED BS 540 BETWEEN BL0 TO LBL 24.75 CENTER SECTION IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 1SDR SWAA2023083195742Fastener · crackedCRACK STIFFENER FLOOR STRUCTURE LOCATED BS 540 BETWEEN BL0 TO LBL 24.75 CENTER SECTION 2023-508413<[01] REPLACED STIFFENER AND FASTENERS ON FLOOR STRUCTURE LOCATED BS 540 BETWEEN BL0 TO LBL 24.75 CENTER SECTION IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 1SDR SWAA2023090188444Panel · crackedCRACK ACCESS PANEL 661BB AT RT WING 2023-508347<[01] TOOL USED: CALIPER P/N: 500-197-30; S/N: 15120589; DUE DATE: 13-FEB-24.;[02] TOOL USED: UT EQUIPMENT P/N: EPOCH 650; S/N: 190859705; CAL DUE DATE: 16-SEP-23;[03] TOOL USED: HOT BONDER: P/N:HCS9200B-AV S/N:18SDR SWAA2023090188445Panel · crackedCRACK ON BRACKET ACCESS PANEL 651FB AT RT WING 2023-508349<[01] REPLACED BRACKET ON ACCESS PANEL 651FB AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02.;[02] TASK CARD COMPLETEDSDR SWAA2023083188620Nut · deterioratedDETERIORATED ENTRY DOOR HANDLE NUT AT AFT GALLEY AREA (2 EA) 2023-508377<[01] REPLACED ENTRY DOOR LINING HANDLE NUT AT AFT GALLEY AREA IAW B737-700 AMM 25-21-25-420-801.;[02] REPLACED ENTRY DOOR LINING HANDLE NUT AT AFT GALLEY AREA IAW B737-700 AMM 25-21-25-42SDR SWAA2023083188622Nut · deterioratedDETERIORATED SERVICE DOOR HANDLE NUT AT AFT GALLEY AREA (2 EA) 2023-508376<[01] REPLACED SERVICE DOOR HANDLE NUT AT AFT GALLEY AREA IAW B737-700 AMM M 25-21-25-420-801;[02] CERTIFIED STEP 1 COMPLETESDR SWAA2023083188623Collar · missingMISSING AFT SERVICE DOOR HANDLE COLLAR AT AFT GALLEY AREA (2 EA) 2023-508378<[01] REPLACED AFT SERVICE DOOR HANDLE COLLAR AT AFT GALLEY AREA IAW B737-700 AMM 25-21-25-420-801 STEP 3. B. (5).;[02] REPLACED AFT SERVICE DOOR HANDLE COLLAR AT AFT GALLEY AREA IAW BSDR SWAA2023083188586Scuff Plate · crackedCRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT 2023-508354<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:A18229508;DUE DATE:30-OCT-23.;[02] REPAIRED SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BASDR SWAA2023083188582Access Panel · crackedCRACK ACCESS PANEL 324AL AT VERTICAL STABILIZER 2023-508338<[01] REPLACED RETAINER LOCATED ON ACCESS PANEL 324AL AT VERTICAL STABILIZER IAW. B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 172A6123 SHEET 1 REV: A;[02] CORRECTED STEP 1: REPLACED RETAINER LOCSDR SWAA2023083188583Access Panel · crackedCRACK ACCESS PANEL 323AL AT VERTICAL STABILIZER 2023-508333<[01] REPLACED RETAINER LOCATED ON ACCESS PANEL 323AL AT VERTICAL STABILIZER IAW. B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 172A6122 SHEET 1 REV: B;[02] CORRECTED STEP 1: REPLACED RETAINER LOCSDR SWAA2023090188256Flap · debondedCUSTOMER REQUEST - DEBONDED EXTERNAL SKIN OB AFT FLAP LOWER SURFACE IB AREA AT LT WING 2023-508262<[01] TOOL USED: CALIPER P/N:500-197-30 S/N:B20189416 DUE DATE: 19-DEC-23.;[02] TOOL USED BOND TESTING UNIT PN: BONDMASTER 600M; SN: 220052310; DUE DATE: 31 OCT 2SDR SWAA2023090188253Flap · debondedCUSTOMER REQUEST - DEBONDED EXTERNAL SKIN OB AFT FLAP UPPER SURFACE IB CORNER AT RT WING 2023-508263<[01] TOOL USED: CALIPER P/N:500-197-30 S/N:B20189416 DUE DATE: 19-DEC-23.;[02] TOOL USED: CALIPER P/N:500-464 S/N:B17030933 DUE DATE:17-OCT-23.;[03] TOOL USED SDR SWAA2023083187746Rib · crackedCRACK ON RIB LOCATED ON L/E STA 95.96 AT LEADING EDGE SKIN HORIZONTAL STABILIZER 2023-508215 (HORIZONTAL STABILIZER RH SIDE )<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 25 JAN 24.;[02] REPLACED RIB LOCATED ON STA 95.96 AT SDR SWAA2023083187747Light · deterioratedDETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (7 EA) 2023-508221<[01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (7 EA) IAW B737-700 AMM 33-51-15-000-802; AMM 33-51-15-400-802 AND DWG 33500007 REV 2.;[02] SDR SWAA2023080184004Slide · looseL1 EMERGENCY EXIT SLIDE LOOSE<[01] REPACKED F/E SLIDE IAW MT 725-61-06SDR SWAA2023070573640Bracket · out of adjustFLIGHT ATTENDANT REPORTS L1 GIRT BAR CLIPS LOOSE.<[01] ADJUSTED L1 GIRT BAR BRACKET TO FIRMLY SECURE GIRT BAR IN REF TO SIP. NO FURTHER DEFECTS NOTED.
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