N929WN
Service difficulty reports · 267
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 = 'N929WN' 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 = 'N929WN' 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 SWAA2024061490964Floorbeam · defectiveDURING ACCOMPLISHMENT OF STA 986 FLOOR BEAM REPAIR FAULT TTG8Q00TDFQW REF: SRM 53-70-51-2R-4 DEVIATION IN FASTENERS HOLES LAYOUT AT RBL 22.5' FASTENERS NOT STAGGERED AS PER SRM LAYOUT.<[01] RECEIVED ENGINEERING APPROVAL FOR DEVIATION OF FASTENER HOLES LAYOUT ASDR SWAA2024061487475Shield · corroded**CORROSION** FWD CARGO R/H SIDE PLATE UPPER SURFACE BETWEEN STA 492 TO 500A RBL 21.80 HAS CORROSION AROUND FASTENERS HOLES MKD (107-005)<[01] (FINAL) REMOVED CORROSION AROUND FASTENER HOLES FROM FWD CARGO R/H SIDE PLATE UPPER SURFACE BETWEEN STA 492 TO STA 50SDR SWAA2024061886559Floorbeam · corrodedCORROSION ** AFT CABIN WET AREA FLOOR SUPPORT BEAM FASTENER HOLE FWD EDGE RBL 45 STA 986.5 MKD DOT<[01] REMOVED CORROSION ON FLOOR BEAM AT STA 986.5 RBL 45 AT FASTENER HOLE AS PER B 737 SRM 51-10-02-0G-0. EVALUATE DAMAGE: ORIGINAL MATERIAL 150'; MATERIAL LOST SDR SWAA2024061486387Floor Support · crackedMAIN CABIN FWD WET AREA UNDER PANEL 221DF BETWEEN STA 312 AND STA 328 APPROX. LBL 52 HAS INTERCOSTAL WITH POSSIBLE CRACK.<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN FWD WET AREA UNDER PANEL 221DF BETWEEN STA 312 AND STA 328 APPROX. LBL 52 PER B737-700SDR SWAA2024061486388Floor Support · crackedMAIN CABIN FWD WET AREA UNDER PANEL 221AF BETWEEN STA 285.62 AND STA 294.5 APPROX. RBL 5 HAS INTERCOSTAL WITH POSSIBLE CRACK.<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN FWD WET AREA UNDER FLOOR PANEL 221AF BETWEEN STA 285.62 AND STA 294.5 APPROX. RBL SDR SWAA2024061486379Floor Panel · corrodedMAIN CABIN FWD WET AREA PANEL 221CF WITH TWO FASTENER INSERT HOLES WITH SIGNS OF CORROSION PN: 141A5810-9<[01] FLOOR PANEL 221CF REPLACED ON NR TTG8Q00TD1ZK.;[02] QUALITY CONTROL PERFORMED A REVIEW OF THIS FAULT.<BR>C/W AUDIT PER 52.02.02SDR SWAA2024061486386Scuff Plate · corrodedMAIN CABIN FWD WET AREA AT L1 DOOR SCUFF PLATE LOWER STRUCTURE UNDER AFT DRAIN HOLE SHOW SIGNS OF CORROSION<[01] CLEANED AREA UNDER AFT DRAIN HOLE AT MAIN CABIN FWD WET AREA L-1 DOOR SCUFF PLATE LOWER STRUCTURE PER BOEING SOPM 20-30-03. NO COROSION NOTED. ONLYSDR SWAA2024061386561Floorbeam · crackedMAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK CRACKED AT STA 540 LBL 1 MKD DOT<[01] SUMMARY <BR>REMOVED MAIN CABIN FLOOR PANEL 231UF FOR ACCESS PER B737-700 SRM 51-40-02-0G-0.<BR>REMOVED FLOOR SUPPORT BREAK AT STA 540 LBL 1 AS PER B-737 SRM 51-40-02-0G-0LOCATESDR SWAA2024061386381Floor Panel · delaminatedMAIN CABIN FWD WET AREA PANEL 221GF WITH SEVERAL AREAS OF DELAMINATION ON TOP OF PANEL PN: 141A5810-181<[01] RECEIVED AND REPLACED PANEL 221GF AS PER SRM 53-00-50-2R-0. PANEL CLOSING WILL ACCOMPLISHED IN TASK CARD TTG8Q00SJK74.;[02] VERIFIED REPLACED.<BR>QUALISDR SWAA2024061386380Floor Panel · delaminatedMAIN CABIN FWD WET AREA PANEL 221EF WITH SEVERAL AREAS OF DELAMINATION ON TOP OF PANEL PN: 141A5810-249<[01] RECEIVED AND REPLACED PANEL 221EF AS PER SRM 53-00-50-2R-0. PANEL CLOSING WILL ACCOMPLISHED IN TASK CARD TTG8Q00SJK78.;[02] VERIFIED REPLACED;[03] VERISDR SWAA2024061386377Floor Panel · delaminatedMAIN CABIN FWD WET AREA PANEL 221CF WITH SEVERAL AREAS OF DELAMINATION ON TOP OF PANEL PN: 141A5810-9<[01] RECEIVED FLOOR PANEL 221CF P/N 141A5810-9 AND INSTALLED ON TASK CARD TTG8Q00SJK7C;[02] QUALITY CONTROL PERFORMED A REVIEW OF THIS FAULT.<BR>C/W AUDIT PERSDR SWAA2024061385993Scuff Plate · crackedAFT CARGO BAY AFT CARGO DOOR SCUFF PLATE CRACK.DOT 251-0015<[01] RECEIVED NEW SCUFF PLATE P/N 654A0004 PO# 2059779.LOCATED AND DRILL NEW SCUFF PLATE PER 51-40-05-0G-0.;[02] VERIFIED RECEIVED NEWSDR SWAA2024061385766Floor Panel · delaminatedCABIN FLOOR PANEL 231XF UPPER SKIN DELAMINATED AND TORN IN SEVERAL AREAS.<[01] RECEIVED AND REPLACED PANEL 231XF IAW SRM 53-00-50-2R-0.<BR>INSTALLATION WILL BE ACCOMPLISHED ON ITEM TTG8Q00SJKID;[02] VERIFIED STEP 1SDR SWAA2024061385768Floor Panel · delaminatedCABIN FLOOR PANEL 241UF UPPER SKIN DELAMINATED AND TORN IN SEVERAL AREAS<[01] RECEIVED AND REPLACED PANEL 241UF AS PER SRM 53-00-50-2R-0. PANEL CLOSING WILL ACCOMPLISHED IN TASK CARD TTG8Q00SJJZX.;[02] VERIFIED REPLACED.<BR>QUALITY CONTROL PERFORMED A REVIEW OSDR SWAA2024061485218Stiffener · crackedRH HORIZONTAL STABILIZER RIB #4 STIFFENER #3 LOWER SECTION CRACK<[01] SUMMARY<BR>REMOVED DAMAGE AT RIB #4 STIFFENER #3 AS PER B-737 SRM 55-10-09-2R-4.<BR>REMOVED CRACK ON #3 STIFFINER; AREA MARKED AS PER B-737 SRM 55-10-09-2R-4.<BR>LOCATED AND DRILLED REPAIR PSDR SWAA2024061384959Battery Pack · inoperativeMULTIPLE PAX EMERGENCY LIGHT BATTERIES INOP<[01] PERFORMED TROUBLESHOOTING AS PER B737 AMM 33-51-00-710-801 AND SSM 33-51-13. FOUND M1670 EMERGENCY EXIT LIGHT BATTERY PACK DEFECTIVE.<BR>PERFORMED POWER SUPPLY - BATTERY PACK REPLACEMENT AT POSITION M1670 AS PERSDR SWAA2024061384748Bulkhead · crackedFWD CARGO FWD BULKHEAD PANEL 121LW HAS CRACK. 8-14<[01] REPAIRED DAMAGE AREA AT FWD BULHEAD PANEL 121LW AS PER SRM 51-70-04-2R-1. MATERIAL EY3804 PO 1759622 PLUS BMS9-3-7781 PO 1738579 .RESTORED ORIGINAL FINISHED AT FWD BULKHEAD PANEL 121LW AS PER AMM 51-21-99SDR SWAA2024061384747Bulkhead · crackedFWD CARGO FWD BULKHEAD PANEL 121JW HAS CRACK. 8-13<[01] APPLIED REPAIR TO DAMAGED AREA AT FWD CARGO FWD BULKHEAD PANEL 121JW PER B737 AMM 25-00-00-300-801 AND SUBTASK 25-00-00-020-001 MATERIALS USED PO# 1690463 AND PO# 2039827.;[02] VERIFIED CORRECTIVE ACTION.SDR SWAA2024061484450Panel · corrodedREFUEL PANEL (P15) FACE PLATE HAS SIGN OF CORROSION AROUND FUEL QTY GAUGES.<[01] REMOVED REFUEL PANEL (P15) AS PER B737 AMM TASK 28-21-00-000-801.<BR>INSTALLED EWIS PROTECTION FOR MAINTENACE AS PER B737 AMM TASK 20-60-07-913-801.<BR>REPLACED FACEPLATE/BRACKET SDR SWAA2024061484572Skin · crackedCRACK FOUND AT RIGHT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90; 16' FROM FRONT SPAR; I/B ROW. LENGTH OF CRACK: 1'. CRACK FOUND AT RIGHT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90 16' FROM FRONT SPAR I/B ROW. LENGTH OF CRACK: 1'.<[01] COMPLETSDR SWAA2024042579186Lens · detachedMID CABIN OVERHEAD EMERGENCY MID CABIN OVERHEAD EMERGENCY LIGHT AFT LIGHT PANEL CAME OFF<[01] RESECURED MID CABIN OVERHEAD EMERGENCY LIGHT LENS IAN AMM 33-51-01SDR SWAA2024042578401Floor Panel · crackedFWD CARGO BIN AFT FLOOR PANEL HAS A CRACK.<[01] REPAIRED CARGO FLOOR PANEL PER AMM 25-52-01SDR SWAA2023110918524Battery Pack · inoperativeR/H OVERWING EMERGENCY EXIT LIGHT INOP / [01] R&R EMERGENCY LIGHT CHARGER ASSEMBLY AT POSITION M01669 PER AMM 33-51-06.SDR SWAA2023021401585Sign · out of adjustCENTER CEILING EXIT SIGN FELL OFF<[01] LP1878487 AP3230074 REATTACHED LENS REF AMM 33-51-01SDR SWAA2023020698180Girt Bar · out of adjustFWD ENTRY DOOR SLIDE GIRT REQUIRES ADJUSTMENT<[01] ADJUSTED FWD ENTRY SLIDE GIRT IAW SIPSDR SWAA2023020698181Girt Bar · out of adjustFWD SERVICE DOOR SLIDE GIRT REQUIRES ADJUSTMENT<[01] ADJUSTED FWD SERVICE DOOR SLIDE GIRT IAW SIPSDR SWAA2022080538789Light · inoperativeLH OVERWING EXIT DOOR INTERIOR LIGHT INOP / [01] RELAMPED LH OVERWING EXIT DOOR AND OPS CHECKED PER MM 33-21-00SDR SWAA2022062721395Handle · brokenL1 ENTRY DOOR ASSIST HANDLE BROKEN. / [01] REMOVED ASSIST HANDLE FROM FWD LAV AND INSTALLED ON L1 DOOR REF AMM 25-40-11. FWD LAV ASSIST HANDLE OK TO CONTINUE PER MEL 25-10-01. SP1B AUTH 72341;[02] INSTALLED ASSIST HANDLE PER CMM 25-42-60. THIS CLEARS MEL 25-10SDR SWAA2022062421107Cover · detachedOVERHEAD EMERGENCY EXIT SIGN AT EMERGENCY EXIT ROW COVER CAME OFF / [01] SECURED EMERGENCY EXIT SIGN PER AMM STANDARD INDUSTRY PRACTICESSDR SWAA2022071216884Light · inoperativeR/H OVERWING DOOR WINDOW LIGHT INOP. / [01] RE-LAMPED R/H OVERWING DOOR WINDOW LIGHT AND PERFORMED LAMP REPLACEMENT TEST AS PER B737 AMM 33-21-00-960-801. TEST OK.;[02] VERIFIED REPLACEMENTSDR SWAA2022061416886Light · inoperativeEXTERIOR EMERGENCY LIGHT AT R1 DOOR INOP. / [01] RE-LAMPED EXTERIOR EMERGENCY LIGHT AT R1 DOOR AND PERFORMED LAMP REPLACEMENT TEST AS PER B737 AMM 33-51-04-960-801. TEST OK.;[02] VERIFIED REPLACEMENTSDR SWAA2022061416885Lamp · inoperativeR/H AFT OVERWING EMERGENCY LIGHT INOP. / [01] RE-LAMPED R/H AFT OVERWING EMERGENCY LIGHT AND PERFORMED LAMP REPLACEMENT TEST AS PER B737 AMM 33-51-04-960-801. TEST OK.;[02] VERIFIED REPLACEMENTSDR SWAA2022061615686Stiffener · crackedSTA 663.5 VAPOR BARRIER LOWER SECTION FOUND STIFFENER CRACKED AT RBL 25'. / [01] STARTED TO REMOVED STIFFENER AT VAPOR BARRIER STA 663.5 RBL 25' AS PER SRM 51-40-02-0G-0.;[02] REMOVED STIFFENER AT VAPOR BARRIER STA 663.5 RBL 25' AS PER SRM 51-40-02-0G-0.;[03] SDR SWAA2022061413055Lens · missingAFT LAVATORY EXIT SIGN LEN MISSING / [01] INSTALLED AFT LAVATORY EXIT SIGN LENS REF. BOEING 737-700 AMM 33-51-01-960-802;[02] VERIFIED INSTALLATIONSDR SWAA2022061710917Skin · crackedCRACK FOUND AT LEFT HAND HORIZONTAL STABILIZER LOWER SKIN STAB STA 193.90 ; I/B ROW ; 16' FROM REAR SPAR. CRACK LENGTH 0.906' CRACK FOUND AT LEFT HAND HORIONTAL STABILIER LOWER SKIN STAB STA 193.90 I/B ROW 16' FROM REAR SPAR. CRACK LENGTH 0.906' / [01] REMOVEDSDR SWAA2022061612910Vapor Barrier · crackedRH VAPOR BARRIER CRACKED / [01] MEASUREMENTS;[02] CLEANED DAMAGE AREA OF R/H VAPOR BARRIER FOR REPAIR; STOP DRILL CRACK ; PERFORMED DRY OUT ;FOUND NO WATER AS PER B737 SRM 51-70-04-2R-10;[03] VERIFIED STEPS 1 AND 2. OK TO APPLY REPAIR.;[04] REPAIRED CRACK DAMASDR SWAA2021091316134Handle · brokenL1 DOOR WILL NOT OPEN CORRECTLY ASSIST HANDLE BROKEN ; L1 DOOR WILL NOT OPEN AND ASSIST HANDLE BROKEN / [01] REPLACED GUIDE ARM AND DOOR ASSIST HANDLE PER MM 52-11-21SDR SWAA2021031554613Roller · crackedAFT SERVICE DOOR GUIDE ROLLER CRACKED. / REMOVED AND REPLACED PER AMM 52-41-21.SDR SWAA2020070997892Light · inoperativeFWD SERVICE DOOR EMERGENCY EXIT LOCATOR SIGN HAS SEVERAL LIGHTS OUT. RELAMPED FWD SERVICE DOOR EMERGENCY EXIT LOCATOR SIGN AND PERFORMED GOOD FUNCTIONAL TEST AS PER AMM 33-51-01-960-801.SDR SWAA2020070997891Light · not seatedRT OVERWING ESCAPE GROUND EMERGENCY EXIT LIGHT L548 BULB IS OUT. RESEATED RT OVERWING ESCAPE GROUND EMERGENCY EXIT LIGHT L548 AND PERFORMED GOOD OPERATIONAL TEST PER AMM 33-51-04-960-801.SDR SWAA2020070997890Light · inoperativeEMERGENCY EXIT LIGHT L1189 FORWARD OF LT OWE HAS BULBS OUT. RELAMPED EMERGENCY EXIT LIGHT L1189 AND PERFORMED GOOD OPERATIONAL TEST PER AMM 33-51-01-960-801.SDR SWAA2021062497881Scuff Plate · crackedFWD CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED / LOCATED AND DRILLED NEW FWD CARGO BAY FWD CORNER SCUFF PLATE PO #784955/1 IAW SRM 51-40-05. OK TO INSTALL 88918C 29JUN20 INSP 86 29JUN20. INSTALLED FWD CARGO BAY FWD CORNER SCUFF PLATE IAW AMM 53-11-02-420-801SDR SWAA2021062497879Scuff Plate · brokenAFT CARGO DOOR SCUFF PLATE FWD CORNER HAS BROKEN FLANGE / LOCATED AND DRILLED NEW AFT CARGO DOOR SCUFF PLATE FWD CORNER IAW SRM 51-40-05. OK TO INSTALL 88928C 29JUN20 INSP 86 29JUN20. INSTALLED AFT CARGO DOOR SCUFF PLATE FWD CORNER IAW AMM 53-11-02-420-801SDR SWAA2020070893895Intercostal · corrodedCORROSION ON INTERCOSTAL AT PASSENGER CABIN BS 294 - BS312 LBL12 WL208. REMOVED & REPLACED INTERCOSTAL AT BS 294-312 LBL12 WL208 IAW SRM 51-40-02 & REF DWG 141A5600.SDR SWAA2020070997878Skin · gougedFUSELAGE SKIN HAS A GOUGE AT BS 847+6.5'; .8' BELOW S-1L. DAMAGE REPAIRED PER EA 20-153-00953 REV IR (ATS ER 20-02766 REV IR) REFER TO NRC U181821 FOR TRACKING.SDR SWAA2020070997877Skin · gougedFUSELAGE SKIN HAS A GOUGE AT BS 847+4.5' STR 1. FUSELAGE SKIN GOUGE AT BS 847+4; STR 1 WAS REPAIRED IAW ATS ER 20-02766 REV IR RATED 30JUN20 AND EA 20-153-00953 REV IR.SDR SWAA2020070992414Bulkhead · delaminatedBS 663 LOWER COMPOSITE BULKHEAD IS SEPARATING AT PREVIOUS REPAIR AT LBL 38; WL 150. BS 663 LOWER COMPOSITE BULKHEAD WAS REPAIRED IAW SRM 51-70-04-2R-10.SDR SWAA2020070992419Floor Panel · damagedFWD CABIN FLOOR PANEL 221AF HAS DAMAGE UPPER SURFACE SKIN. FWD CABIN FLOOR PANEL 221AF WITH DAMAGED UPPER SURFACE SKIN WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 51-10-02-0G-0 PARA 9A.(1).SDR SWAA2020070992422Floor Panel · damagedFWD CABIN FLOOR PANEL 221FF HAS DAMAGE UPPER SURFACE SKIN. FWD CABIN FLOOR PANEL 221FF WITH DAMAGED UPPER SURFACE SKIN WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 51-10-02-0G-0 PARA 9A.(1).SDR SWAA2020070992424Floor Panel · damagedFWD CABIN FLOOR PANEL 222DF HAS DAMAGED INSERTS ON THE FWD O/B EDGE. DUE TO THE EXTENT OF DAMAGE; REPLACED FLOOR PANEL 222DF WITH NEW PANEL IAW SRM 51-10-02-0G-0 PAR 9A(1) AND AIPC 53-21-51-21L.
Back to N929WN