N924WN
Service difficulty reports · 233
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 = 'N924WN' 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 = 'N924WN' 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 SWAA2024042567504Floor Support · crackedCRACKED FLOOR SUPPORT BS 328-344 LBL 47 WL 208.<[01] UPDATED STEPS 1 AND 2.;[02] VERIFIED;[03] COMPLETED STEPS 1 AND 2.SDR SWAA2024042567648Attach Angle · crackedCRACKED INTERCOSTAL LOWER ATTACH ANGLE STA 692; RBL 24; WL 204.<[01] REMOVED CRACK DAMAGED LOWER ATTACH ANGLE AT BS 692 RBL 24 WL 204 IAW SRM 51-40-02-0G-0;[02] FABRICATED NEW ATTACH ANGLE FOR BS 692 RBL 24 WL 204 FROM HFAB53-BR-012 (BAC1490-2782 7075 TO CLAD SDR SWAA2024042567644Floorbeam · crackedCRACKED BREAK PANEL STA 540; LBL 1; WL 207.<[01] REMOVED AND INSTALLED NEW BREAK PANEL LOT 1548854-1; PER SRM 51-40-02 AND DWG 143A0060.;[02] VERIFIED CORRECTIVE ACTION STEP 1. TASK CARD COMPLETE.SDR SWAA2024042567507Floorbeam · corrodedCORROSION AROUND FASTENER HOLE BS 986 BEAM RBL 44 WL 208.<[01] EVALUATED DAMAGE AND FOUND OUT ALLOWABLE DAMAGE LIMITS IAW SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1 PAR 4.D(2)(A) FIGURE 103/DETAIL E .<BR>PERFORMED REPAIR ON THE UPPER CHORD OF THE<BR>FLOOR BEAM AT STSDR SWAA2024042567667Seat Track · corrodedLH SECTION 3 OF LBL 45 SEAT TRACK HAS CORROSION ON CROWN BS 500C; WL 208<[01] FAULT WAS RESOLVED ON ANOTHER FAULT TTG8Q00SCLMFSDR SWAA2024042567281Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 222DF IS DELAMINATED<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED PASSENGER CABIN FLOOR PANEL 222DF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-51-21L ITEM 235.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024042567277Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 221FF IS DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 221FF WITH UPPER SKIN DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.SDR SWAA2024042567276Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 221EF IS DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 221EF WITH UPPER SKIN DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.SDR SWAA2024042567280Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 221DF IS DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 221DF WITH UPPER SKIN DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION. JOB SDR SWAA2024042567279Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 221CF IS DELAMINATED<[01] CABIN FLOOR PANEL 221CF DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.SDR SWAA2024042567278Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 221GF IS DELAMINATED. PASSENGER CABIN FLOOR PANEL 221GF WITH UPPER SKIN DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.SDR SWAA2024042567282Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 222CF IS DELAMINATED<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED PASSENGER CABIN FLOOR PANEL 222CF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-51-21L ITEM 275.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024042567283Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 231AF IS DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 231AF WITH UPPER SKIN DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.SDR SWAA2024042567284Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 231BF IS DELAMINATED<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED PASSENGER CABIN FLOOR PANEL 231BF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-51-21L ITEM 430.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024042567285Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 231CF IS DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 231CF WITH UPPER SKIN DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.SDR SWAA2024042567286Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 222BF IS DELAMINATED AND HAS BAD INSERTS. (MARKED) PASSENGER CABIN FLOOR PANEL 222BF IS DELAMINATED AND HAS BAD INSERTS.<[01] PASSENGER CABIN FLOOR PANEL 222BF WITH UPPER SKIN DELAMINATION AND BAD INSERTS WAS REPLACED WITH A SERVICESDR SWAA2024042567287Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 221AF IS DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 221AF WITH UPPER SKIN DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.SDR SWAA2024042567288Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 221BF IS DELAMINATED<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED PASSENGER CABIN FLOOR PANEL 221BF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-51-21L ITEM 95.;[02] VERIFIED CORRECTIVE ACTION STEP 1. TASK CARD COMPLETE.SDR SWAA2024042567379Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 232AF IS DELAMINATED<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED PASSENGER CABIN FLOOR PANEL 232AF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-51-21L ITEM 400.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024042567380Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 241AAF IS DELAMINATED.<[01] DUE TO EXTENT OF THE DAMAGE FABRICATED NEW PASSENGER CABIN FLOOR PANEL 241AAF IAW SRM 53-00-50-2R-1 PARA 1A(NOTE) AND BOEING DWG 147A5810-8.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024042567381Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 241ABF IS DELAMINATED.<[01] CABIN FLOOR PANEL 241ABF DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.SDR SWAA2024042567388Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 241YF IS DELAMINATED<[01] DELAMINATION ON PASSENGER CABIN FLOOR PANEL 241YF WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024042567382Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 241XF IS DELAMINATED<[01] CABIN FLOOR PANEL 241XF HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.SDR SWAA2024042567389Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 242UF IS DELAMINATED AND HAS BAD INSERTS MARKED<[01] DELAMINATION AND BAD INSERTS ON PASSENGER CABIN FLOOR PANEL 242UF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024042567383Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 242TF IS DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 242TF WITH UPPER SKIN DELAMINATION WAS REPAIRED PER SRM 53-00-50-2R-1.;[02] JOB COMPLETE.SDR SWAA2024042567384Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 242RF IS DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 242RF WITH UPPER SKIN DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.SDR SWAA2024042567385Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 242SF IS DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 242SF WITH UPPER SKIN DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.SDR SWAA2024042567390Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 241AEF IS DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 241AEF WITH UPPER SKIN DELAMINATION WAS REPAIRED PER SRM 53-00-50-2R-1.;[02] JOB COMPLETE.SDR SWAA2024042567386Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 242PF IS DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 242PF WITH UPPER SKIN DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.SDR SWAA2024042567391Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 242QF IS DELAMINATED<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED PASSENGER CABIN FLOOR PANEL 242QF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-51-63A ITEM 380.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024042567387Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 241UF IS DELAMINATED<[01] DUE TO EXCESSIVE DAMAGE; FLOOR PANEL 241UF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIEDSDR SWAA2024042566942Skin · corrodedCORROSION ON FUSELAGE CROWN SKIN FROM STA 1016+2 TO STA 1016+15; COMMON TO FASTENER HOLES AT BL 0; RBL 12; AND LBL 12.<[01] VERIFIED STEPS 1; 2; 5.;[02] REMOVED DAMAGE ON FUSELAGE CROWN SKIN FROM STA 1016+2 TO STA 1016+15; COMMON TO FASTENER HOLES AT BL 0; 10'SDR SWAA2024042567089Floorboard · delaminatedFLOORBOARD 241AF UPPER SURFACE DAMAGED. (DELAMINATED)<[01] FLOORBOARD 241AF WILL BE REPAIRED OR REPLACED ON FAULT TTG8Q00S9RVV;[02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2024042566571Stiffener · cracked2ND FWD STIFFENER CRACK AT LH HSTAB AT STAB STA 120.30<[01] OK TO INSTALL GIVEN;[02] OKAY TO CAP-SEAL GIVEN STEP # 2 COMPLETE.;[03] CAP SEALED FASTENERS AT LEFT HAND HORIZONTAL STABILIZER FRONT SPAR WEB AT STAB STA 111.10 - 136 IAW AMM 51-31-00-390-805.;[04] VSDR SWAA2024042566145Access Panel · debondedPANEL 191D OUTER SKIN HAS SMALL DISBOND. (MARKED)<[01] PANEL 191D OUTER SKIN SMALL DISBOND WAS REPAIRED IAW SRM 51-70-05-2R-2 AND SRM 51-70-05-2R-11.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.SDR SWAA2024022957487Handle · looseFWD ENTRY DOOR ASSIST HANDLE LOOSE<[01] RESECURED FWD ENTRY DOOR ASSIST HANDLE REF M/M 52-11-31SDR SWAA2023102714625Handle · looseCUSTOMER WALK - L1 DOOR ASSIST HANDLE (DOOR SIDE) LOOSE.<[01] RESECURED L-1 DOOR ASSIST HANDLE ( DOOR SIDE ) AS PER AMM 52-11-31-400-802.;[02] VERIFIED RESECURED L-1 DOOR ASSIST HANDLE ( DOOR SIDE )SDR SWAA2023102714624Handle · looseCUSTOMER WALK - R1 DOOR ASSIST HANDLE (DOOR SIDE) LOOSE.<[01] RESECURED R-1 DOOR ASSIST HANDLE.(DOOR SIDE )AS PER AMM 52-41-31-400-802.;[02] VERIFIED RESECURED R-1 DOOR ASSIST HANDLE.(DOOR SIDE )SDR SWAA2023102714622Battery Pack · inoperativeMAIN CABIN AFT ENTRY AREA SEVERAL EMERGENCY LIGHTS INOP<[01] REPLACED EMERGENCY BATTERY PACK AT POWER SUPPLY M1672 FOR MAIN CABIN AFT ENTRY INOP EMERGENCY LIGHTS AS PER REF AMM TASK 33-51-06-960-805. OPERATION TESTED NORMAL.;[02] VERIFIED REPLACED EMERGENCY BASDR SWAA2023102712959Vapor Barrier · elongatedREJECT - L/H VAPOR BARRIER WEB HAS MULTIPLE ELONGATED HOLES.<[01] COMPLETED INSTALLATION OF L/H VAPOR BARRIER WEB; ANGLES; SUPPORT STRUCTURES; BRACKETS AND STRAPS ON REFERENCE TO SRM 51-40-02-0G-0; DWG NO: 111A1000; 111A1001.;[02] SUMMARY: REMOVED & REINSTALLESDR SWAA2023102711891Stiffener · crackedLT HAND VAPOR BARRIER STIFFENER AT LBL 25' CRACKED.<[01] SUMMARY :REMOVED CRACKED STIFFENER AT LBL25' AS PER B 737 SRM 51-40-02-0G-0.LOCATED AND DRILLED NEW STIFFENER AS L/H VAPER BARRIER AT LBL 25' AS PER REF B/737 SRM 51-40-05-0G-0.INSTALLED NEW STIFFENERS ASDR SWAA2023102710639Vapor Barrier · crackedCENTER WING REAR SPAR VAPOR BARRIER CRACKED; APPROXIMATELY 19 INCHES LONG (EXCEEDING SRM LENGTH LIMIT).<[01] APPLIED REPAIR AT L\H VAPOR BARRIER REAR SIDE PER B737 SRM 57-10-10-2R-2;SRM 51-70-04-2R-10 AND SRM 51-70-04-2R-0 PARAGRAPH 4.N.2 AND PARAGRAPH 4.L.7 MSDR SWAA2023092704912Web · crackedCENTER WING REAR SPAR VAPOR WEB HAS AN APPROXIMATE 18 INCH CRACK BEGINNING INBOARD OF THE SYS.A HYD. PRESSURE MODULE INBOARD MOUNT AND EXTENDING APPROX. 6 INCHES TO LEFT OF LBL 45.64 STIFFENER.<[01] C/W EA 23-157-02932;[02] COMPLIED WITH EA 23-157-02932. ALSO SDR SWAA2023091198568Bulkhead · crackedL/H 663.75 LOWER BULKHEAD CRACKED. CRACKS STARTS APPROXIMATELY LBL 54.21 AND TRAVELS TO LBL 40.00. CRACK MEASURES AT 15 1/2 INCHES BEFORE IT GOES BEHIND THE HYDRAULIC MODULE BRACKET.<[01] ACCOMPLISHED PERMANENT REPAIR OF 4 INCHES OF CRACK IAW SRM 51-70-04-2R-1SDR SWAA2023081187391Control Module · warning messageAT ROTATION ALL ENG; APU & WHEEL WELL FIRE INDICATION ILLUMINATED WITH ASSOCIATED FIRE BELL<[01] R/R?D ENGINE AND APU FIRE OVERHEAT CONTROL MODULE (M279)AS PER EMM 26-10-01.ALL OPERATIONAL TESTS NORMAL. R/R?D ENGINE AND APU FIRE CONTROL PANEL (P8-1) AS PER AMMSDR SWAA2023081188070Control Module · faultedAT ROTATION ALL ENG; APU & WHEEL WELL FIRE INDICATION ILLUMINATED WITH ASSOCIATED FIRE BELL<[01] R/R?D ENGINE AND APU FIRE OVERHEAT CONTROL MODULE (M279)AS PER EMM 26-10-01.ALL OPERATIONAL TESTS NORMAL. R/R?D ENGINE AND APU FIRE CONTROL PANEL (P8-1) AS PER AMMSDR SWAA2023080986638Fire Detector · faultedAFTER TOUCHDOWN ALL FIRE INDICATIONS ILLUMINATED WITH ASSOCIATED FIRE BELL AND ANNUNCIATORS<[01] R&R ENG & APU FIRE DETECTION MODULE PER AMM 26-10-01<BR>OPS CHK NORMALSDR SWAA2023071979080Bulkhead · crackedL/H 663.75 LOWER BULKHEAD CRACKED. CRACKS STARTS APPROXIMATELY LBL 54.21 AND TRAVELS TO LBL 40.00. CRACK MEASURES AT 15 1/2 INCHES BEFORE IT GOES BEHIND THE HYDRAULIC MODULE BRACKET. ONCE CRACK GOES BEHIND HYDRAULIC MODULE BRACKET IT CAN NO LONGER BE MEASURED SDR SWAA2023070675800Cylinder · faultyDURING NORMAL GEAR EXTENSION; L/H GEAR RED INDICATION WHILE NOSE AND R/H GEAR GREEN; PERFORMED LOW PASS AND ATC CONFIRMED PARTIAL L/H GEAR EXTENSION. RAN QRH CHECKLIST; AND MANUALLY EXTENDED GEAR. DURING NORMAL GEAR EXTENSION L/H GEAR RED INDICATION WHILE NOSESDR SWAA2023070675923Regulator · faultyDURING NORMAL GEAR EXTENSION; L/H GEAR RED INDICATION WHILE NOSE AND R/H GEAR GREEN; PERFORMED LOW PASS AND ATC CONFIRMED PARTIAL L/H GEAR EXTENSION. RAN QRH CHECKLIST; AND MANUALLY EXTENDED GEAR. DURING NORMAL GEAR EXTENSION L/H GEAR RED INDICATION WHILE NOSE
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