N920WN
Service difficulty reports · 262
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 = 'N920WN' 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 = 'N920WN' 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 SWAA2024041876320Seal · crackedRIGHT HORIZONTAL STABILIZER UPPER FORWARD SLIDER CRACKED.<[01] R&R RH HORIZONTAL STAB UPPER FWD SLIDING SEAL REF. AMM 53-31-31.SDR SWAA2024041876321Seal · crackedLEFT HORIZONTAL STABILIZER UPPER FORWARD SLIDER CRACKED. REMOVED AND REPLACED PER [AMM 53-31-31-400-802-NG (STABILIZER-TO-BODY UPPER FRONT SPAR SLIDING SEAL INSTALLATION - PERMANENT).SDR SWAA2024041876315Handle · loosePASSENGER CABIN - R1 DOOR INTERIOR HANDLE LOOSE<[01] RE-SECURED FWD SERVICE DOOR (R1) INTERIOR HANDLE CAM HUB NUT PER AMM 52-41-31.SDR SWAA2024041071105Lens · unsecureEMERGENCY LIGHT LES AT 16DEF NOT SECURE<[01] RESECURE EMERGENCY LIGHT LEN AT 16DEF IN REF AMM-33-51-03-960-801;[02] VERIFIED CORRECTIVE ACTION.SDR SWAA2024041069804Sign · damagedAFT LOWER CEILING PANEL HOUSING ASSY-EXIT SIGN DAMAGED.<[01] REMOVED AND REPLACED AFT LOWER CEILING PANEL HOUSING ASSY-EXIT SIGN IN REF AMM-33-51-01-960-802;[02] VERIFIED STEP1SDR SWAA2024041070103Lamp · inoperative3 EA PAX CABIN EMERGENCY AREA LIGHTS R/H & L/H SIDE INOP<[01] CLEANING LAMP AND BULB BASE.;[02] VERIFIED STEP # 1SDR SWAA2024041065124Floorbeam · corrodedREMOVE CLIP AFT OF STA 986.5 FLOOR BEAM JUST BELOW OF R2 DOOR INNER CHORD. REINSTALL IT ONCE REPAIR IS COMPLETED<[01] REMOVED AND INSTALLED CLIP AFT OF STA 986.5 FLOOR BEAM JUST BELOW OF R2 DOOR INNER CHORD PER REF SRM 51-40-02-0G-0 AND DWG 147A5730.;[02] VERISDR SWAA2024041065014Cowling · cracked#2 ENGINE I/B FAN COWL LOWER FWD END CRACK<[01] ACCOMPLISHED REMOVAL; REPLACEMENT AND ADJUSTMENT OF #2 ENGINE I/B FAN COWL AS PER AMM 71-11-02-000-802-F00;71-11-02-400-802-F00 AND 71-11-03-820-001;[02] VERIFIED STEP 1 FINALSDR SWAA2024041063996Strap · damagedENGINE #1 UPPER OUTER INLET COWL STRAP P/N 314-2154-2 AT 3 O' CLOCK POSITION #3 HOLE FROM FWD END ELONGATED<[01] REMOVED AND PARTIALLY REPLACED STRAP AT ENGINE #1 UPPER OUTER INLET COWL AS PER SRM 51-40-020G-0 & CMM 71-11-22.;[02] CORRECTION TO STEP #1 <BR>STRSDR SWAA2024041062373Rib · crackedFOUND CRACK 3/4' ON VERTICAL DORSAL FIN AT FOWARD RIP; SEE DOT # 49<[01] REMOVED AND REPLACED FWD RIB AT VERTICAL DORSAL FIN REF SRM 51-40-02-0G-0;[02] VERIFIED CORRECTIVE ACTION.SDR SWAA2024041062371Intercostal · crackedL-1 DOOR CUTOUT INTERCOSTAL CRACK AT STR 16L STA 294.5<[01] REMOVED AND REPLACED INTERCOSTAL AT FWD CABIN STR 16 BETWEEN STA 294.5 REF. SRM 51-40-02-0G-0 AND DWG 141A8180;[02] VERIFIED STEP # 1SDR SWAA2024041061869Access Panel · crackedFUSELAGE ACCESS PANEL 191FL CRACK<[01] REPAIRED PANEL #191FL AT DAMAGED AREA PER B737 SRM 51-70-04-2R-1; B737 SRM 51-70-04-2R-0 PARAGRAPH 4.L.SDR SWAA2024041062212Skin · cracked#2 ENGINE O/B FAN COWL FWD LOWER END CRACK<[01] ACCOMPLISHED REPAIR- REPAIRED PER [SRM 54-20-01-2R-12-A01474 (REPAIR 12 - FAN COWL DOOR SKIN REPAIR AT FWD LATCH AREA - PERMANENT)];[02] VERIFIED FINAL STEP 1SDR SWAA2024041060934Angle · crackedCRACK FOUND AT FASTENER HOLE OF R/H VAPOR BARRIER UPPER SUPPORT ANGLE AT RBL 6.<[01] REMOVED AND REPLACED ANGLE P/N:111A1322-6 AT STA 663 VAPOR BARRIER BETWEEN RBL 6.15 TO RBL 63 PER REF SRM 51-40-02-0G-0; DWG#111A1001 AND DWG#111A7000.;[02] RII; VERIFIED STEPSDR SWAA2024041073044Support Angle · crackedCRACK FOUND AT FASTENER HOLE OF R/H VAPOR BARRIER UPPER SUPPORT ANGLE AND STIFFENER LAYER AT RBL 54.<[01] REPAIRED CRACK AT FASTENER HOLE OF RIGHT-HAND VAPOR BARRIER UPPER SUPPORT ANGLE AND STIFFENER LAYER AT RBL 54 REF 24-157-00665 WIP 1 AND WIP 2;[02] RII / SDR SWAA2024041060935Angle · crackedCRACK FOUND AT FASTENER HOLE OF R/H VAPOR BARRIER UPPER SUPPORT ANGLE AND STIFFENER LAYER AT RBL 54.<[01] REPAIRED CRACK AT FASTENER HOLE OF RIGHT-HAND VAPOR BARRIER UPPER SUPPORT ANGLE AND STIFFENER LAYER AT RBL 54 REF 24-157-00665 WIP 1 AND WIP 2;[02] RII / SDR SWAA2024041060773Door Frame · crackedFORWARD ENTRY DOOR CUTOUT STA 312 BETWEEN STR 5L AND STR 6L FRAME END CRACK<[01] ACCOMPLISHED FRAME REPAIR IN REF TTG8Q00S29RU.;[02] ACCOMPLISHED FRAME REPAIR IN REF TTG8Q00S29RU AND E/A M-22-153-01244 REV B.;[03] VERIFIED STEP 2SDR SWAA2024041060772Angle · crackedMAIN CABIN STA 540 LBL 1' FLOOR PANEL BREAK ANGLE CRACK<[01] REMOVED AND REPLACED MAIN CABIN STA 540 LBL 1' FLOOR PANEL BREAK ANGLE IN REF WITH SRM 51-40-02-0G-0;[02] CORRECTION TO STEP #1<BR>REMOVED AND REPLACED MAIN CABIN STA 540 LBL 1' FLOOR PANEL BREAK ANGSDR SWAA2024041060406Support Angle · corrodedAFT CARGO DOOR CUTOUT SUPPORT ANGLE UNDER FWD SHIELD BETWEEN STA 767-787 RBL 22' CORRODED<[01] REMOVED AND REPLACED AFT CARGO DOOR CUTOUT SUPPORT ANGLE UNDER FWD SHIELD STA AT 767 TO STA 787; RBL 22 PER REF SRM 51-40-02-0G-0 AND DWG #146A8123.;[02] VERIFIED STSDR SWAA2024041060936Channel · corrodedCARGO COMPARTMENT FROM ST 727 TO 787; R/H Z CHANNEL HAS LIGHT CORROSION AROUND NUT PLATES.<[01] REMOVED AND REPLACED RH Z-CHANNEL AT STA 727 TO 767 RBL 21 PER REF SRM 51-40-02-0G-0 AND DWG#146A7502.;[02] VERIFIED STEP 1.SDR SWAA2024041060405Bracket · crackedRIGHT WING LEADING EDGE ACCESS THROUGH PANEL 621GB FUEL METERING BRACKET CORRODED<[01] REMOVED REFUEL PANEL (P15) AS PER AMM 28-41-61-000-801; REMOVED AND REPLACED FUEL METERING BRACKET AS PER REF B737 SRM 51-40-02-0G-0 AND AIPC 28-21-51-05A; REMOVED AND REPLASDR SWAA2024041060407Support Bracket · crackedAFT CARGO COMPARTMENT FWD BULKHEAD STA 727 RBL 6'LOWER SUPPORT BRACKET CRACK<[01] REMOVED AND REPLACED SUPPORT BRACKET (PN: 144A9401U20ATSMRO PO: 2059779) AT AFT CARGO COMPT FWD BULKHEAD STA 727 RBL 6 PER REF SRM 51-40-02-0G-0 AND DWG #144A2600;[02] VERIFIED SSDR SWAA2024041060937Channel · corrodedCARGO COMPARTMENT FROM ST 727 TO 847; L/H Z CHANNEL HAS LIGHT CORROSION AROUND NUT PLATES.<[01] REMOVED AND REPLACED L/H Z-CHANNEL AT AFT CARGO COMPT STA 727 TO STA 847 PER REF SRM 51-40-02-0G-0 AND DWG #146A7500;[02] VERIFIED STEP 1SDR SWAA2024041060392Channel · corrodedCORROSION IN SEVERAL AREAS AT AFT CARGO LH Z-CHANNEL BETWEEN STA 727A & STA 727D. AFT CARGO FLOOR STRUCTURE<[01] WORK WAS ACCOMPLISHED ON TASK CARD TTG8Q00S14B0. REMOVED AND REPLACED.;[02] VERIFIED STEP 1SDR SWAA2024041060393Channel · corrodedCORROSION IN SEVERAL AREAS AT AFT CARGO FLOOR LH Z-CHANNEL BETWEEN STA 727D & STA 787.<[01] WORK WAS ACCOMPLISHED ON TASK CARD TTG8Q00S14B0. REMOVED AND REPLACED.;[02] VERIFIED STEP 1SDR SWAA2024041060401Floorbeam · corrodedMAIN CABIN AFT WET AREA EVIDENCE OF CORROSION UNDER PRIMER AT FLOOR BEAM UPPER SURFACE STA 986.5 LBL 5'<[01] CORRECTION STEP 3 REF IS SRM 53-70-51-1A-1;[02] ACCOMPLISHED REPAIR ON FLOOR BEAM STA 986.5 AS PER EA 24-153-00663 AND SRM 53-70-51-2R-4.;[03] VERIFIEDSDR SWAA2024041060208Angle · crackedMAIN CABIN INTERCOSTAL UPPER ANGLE BETWEEN STA 380-400 RBL 10' CRACK<[01] REMOVED AND REPLACED MAIN CABIN INTERCOSTAL UPPER ANGLE BETWEEN STA 380-400 RBL 10' IN REF WITH SRM 51-40-02-0G-0 AND DWG 143A5400;[02] VERIFIED STEP 1SDR SWAA2024041060389Channel · corrodedCORROSION IN SEVERAL AREAS AT AFT CARGO RH Z-CHANNEL BETWEEN STA 710 & STA 727D. AFT CARGO FLOOR STRUCTURE<[01] THIS JOB CARD WAS REFERED TO TASK CARD TTG8Q00S114AZ;[02] CORRECTION TO STEP 1: THIS JOB CARD WAS REFERED TO TASK CARD TTG8Q00S14AZ;[03] VERIFIED STSDR SWAA2024041060382Channel · corrodedCORROSION IN SEVERAL AREAS AT AFT CARGO RH Z-CHANNEL BETWEEN STA 727D & STA 747. AFT CARGO FLOOR STRUCTURE<[01] THIS JOB CARD WAS REFERED TO TASK CARD TTG8Q00S114AZ;[02] CORRECTION TO STEP 1: THIS JOB CARD WAS REFERED TO TASK CARD TTG8Q00S14AZ;[03] VERIFIED STSDR SWAA2024041060390Channel · corrodedCORROSION IN SEVERAL AREAS AT AFT CARGO RH Z-CHANNEL BETWEEN STA 747 & STA 767. AFT CARGO FLOOR STRUCTURE<[01] THIS JOB CARD WAS REFERED TO TASK CARD TTG8Q00S114AZ;[02] CORRECTION TO STEP 1: THIS JOB CARD WAS REFERED TO TASK CARD TTG8Q00S14AZ;[03] VERIFIED STESDR SWAA2024041060388Floorbeam · corrodedMAIN CABIN AFT WET AREA EVIDENCE OF CORROSION UNDER PRIMER AT FLOOR BEAM UPPER SURFACE STA 986.5 RBL 5'<[01] REMOVED CORROSION AT MAIN CABIN AFT WET AREA AT FLOOR BEAM UPPER SURFACE STA 986.5 RBL 5' SRM 51-10-02-0G-0<BR><BR>ORIGINAL MATERIAL 0.150'; REMAINING SDR SWAA2024041060399Floorbeam · corrodedMAIN CABIN AFT WET AREA CORROSION AT FLOOR BEAM UPPER SURFACE STA 986.5 RBL 40'- 44'<[01] REMOVED CORROSION AT MAIN AFT WET AREA FLOOR BEAM UPPER SURFACE STA 986.5 RBL 40'- 44' SRM 51-10-02-0G-0<BR><BR>ORIGINAL MATERIAL 0.150'; REMAINING MATERIAL 0.136'; REMOVSDR SWAA2024041059778Angle · crackedMAIN CABIN LEFT INNER CHORD CRACK AT STA 309<[01] REMOVED AND REPLACED INNER CHORD AT FWD MAIN CABIN L/H BETWEEN STA 270 TO STA 360 SRM 51-40-02-0G-0 AND DWG 141A8110;[02] VERIFIED STEP # 1SDR SWAA2024041059795Floorbeam · crackedMAIN CABIN FWD WET AREA CRACK AT FLOOR BEAM FASTENER HOLE STA 328 RBL 21'<[01] 04 - REPAIRED PER [EA EA-GENERAL (EA ATTACHED TO AN AIRCRAFT FAULT)]; REPAIR WAS ACCOMPLISHED PER EA # 24-153-00634.;[02] VERIFIED STEP 1SDR SWAA2024041059780Floor Panel · crackedMAIN CABIN FLOOR PANEL 221BF O/B FWD END CRACK<[01] RECEIVED MAIN CABIN FLOOR PANEL 221BF AND WIIL BE INSTALLED ON T/C TTG8Q00RKWCS;[02] VERIFIED STEP 1SDR SWAA2024041059786Floor Support · crackedMAIN CABIN INTERCOSTAL BETWEEN STA 328-344 LBL 46' CRACK<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN BETWEEN STA 328-344 LBL 46' AS PER SRM 51-40-02-0G-0 & DWG 141A5400.;[02] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN BETWEEN STA 328-344 LBL 46' ASSDR SWAA2024041059785Floor Support · crackedMAIN CABIN INTERCOSTAL BETWEEN STA 344-360 BL 0' CRACK<[01] REMOVED INTERCOSTAL AT MAIN CABIN BETWEEN STA 344-360 BL 0'AS PER SRM 51-40-02-0G-0; INSTALLED NEW INTERCOSTAL AT MAIN CABIN BETWEEN STA 344-360 BL 0' AS PER SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1;[0SDR SWAA2024041059794Floor Support · crackedMAIN CABIN INTERCOSTAL BETWEEN STA 312-328 RBL 30' CRACK<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN BETWEEN STA 312-328 RBL 30' AS PER SRM 51-40-02-0G-0 & DWG 141A5400.;[02] VERIFIED STEP 1SDR SWAA2024041059782Floor Support · corrodedMAIN CABIN FWD WET AREA CORROSION AT INTERCOSTAL UPPER SURFACE STA 294.5 +12' LBL 12'<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN STA 294.5 TO STA312 LBL 12' AS PER SRM 41-40-02-0G-0 & DWG 141A5600.;[02] CORRECTION TO STEP #1<BR>ORIGINAL MATERIAL 0.070SDR SWAA2024041060378Vapor Barrier · crackedCENTER SECTION REAR SPAR STA 663 VAPOR BARRIER WEB CRACK AT LOWER SECTION RBL 31.83<[01] APPLIED PERMANENTED REPAIR AT R\H VAPOR BARRIER ON BOTHS SIDE PER B737 SRM 51-70-04-2R-10 PARAGRAPH 4.F & B737 51-70-04-2R-0 PARAGRAPH.4-N.2 EQUIPMENT USED: HOT BONDER MACSDR SWAA2024041058938Pressure Deck · crackedCRACK FOUND AT HORIZONTAL PRESSURE DECK WEB STA 663 RBL 40. CRACK LENGTH : 0.343'<[01] INSTALLED WEB REPAIR AND DOUBLER AT STA 663 RBL 30 - RBL 60 REF SRM 53-40-51-2R-2 FIGURE 202 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1SDR SWAA2024041059433Access Panel · damagedLOWER FUSELAGE ACCESS PANEL # 194DL HAS ELONGATED FASTENER HOLES<[01] REPAIRED DAMAGED AREAS AT PNL #194DL PER B737 SRM 51-70-04-2R-9 PARAGRAPH 4.D-M; 51-70-04-2R-0 PARAGRAPH 4.N (2). MATERIALS USED PO#1473815; PO#1759622; PO#1775890. TOOL B/C #170006 CALIBRATSDR SWAA2024041059434Access Panel · crackedLOWER FUSELAGE ACCESS PANEL 194E HAS BULGING/CRACKED FASTENER HOLES<[01] REPAIRED PANEL #194E AT DAMAGED AREA PER B737 SRM 51-70-04-2R-9; B737 SRM 51-70-04-2R-0 PARAGRAPH 4.L.SDR SWAA2023101610669Battery Pack · inoperativeOVERWING EMERGENCY EXIT SIGN DAMAGED.<[01] R&R AFT EXIT SIGN LIGHT ASSY PER AMM 33-51-01. R&R AFT EMERGENCY BATTERY PACK PER AMM 33-51-06. OPS CHECK GOODSDR SWAA2023082994166Light · inoperativeFORWARD ENTRY DOOR LOWER INTERIOR EMERGENCY EXIT LIGHT ASSEMBLY REQUIRES REPLACEMENT.<[01] REMOVED & REPLACED FORWARD ENTRY DOOR LOWER INTERIOR EMERGENCY EXIT LIGHT ASSEMBLY; OPS CHECK GOOD; IAW AMM 33-51-01.SDR SWAA2023050242627Light · inoperativeRH OVER WING EXIT SIDEWALL LIGHT OUT<[01] REMOVED AND REPLACED WINDOW LIGHT AT RH OVERWING EXIT IAW AMM 33-21-00.SDR SWAA2022081742758Slide · out of positionFWD ENTRY SLIDE FLAP ON BOTTOM COME OUT. / [01] REATTACH FLAP VELCRO TO SLIDE HOUSING PER SIPSDR SWAA2022072835642Light · inoperativeEXTERIOR L1 DOOR EMER LIGHT INOP / [01] RELAMPED PER AMM 33-51-04SDR SWAA2022041490788Light · inoperativeEMERGENCY LIGHT INOP AT L/H OVERWING DOOR. / [01] REMOVED AND REPLACED LAMP AS PER BOEING 737 AMM 33-51-04-960-801.;[02] PERFORMED OPERATIONAL TEST AS PER BOEING 737 AMM 33-51-04-960-801. TEST FOUND NORMAL.;[03] VERIFIED STEP 1;2SDR SWAA2022041488889Channel · abnormalAFT CARGO L/H 'Z' CHANNEL HAS OVER SIZED HOLE AT BS 727C. / [01] REMOVED DAMAGED PART OF L/H 'Z' CHANNEL AS PER B737-700 SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW Z-CHANNEL IAW B 737 SRM 51-40-05-0G-0;[03] VERIFIED STEP 1 AND 2..O.K. TO TREAT AND PRIME..;
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