N907WN
Service difficulty reports · 223
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 = 'N907WN' 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 = 'N907WN' 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 SWAA2025051269443Bolt · pulledL1 ENTRY DOOR ASSIST HANDLE BOLT PULLED OUT<[01] INSTALLED L1 ENTRY DOOR ASSIST HANDLE PER M/M 52-11-31SDR SWAA2024110155361Lens · brokenEMERGENCY EXIT SIGN AT LEFT OVER WING. EXIT FELL OFF<[01] HOUSING ASSAY. AFT LENS CLIP BROKEN. COMPLIED WITH EA M21-133-00720. SECURED LENS COVER WITH MYLAR TAPE.SDR SWAA2024110155362Sign · detachedAFT EXIT SIGN AE L2 DOOR FELL OFF<[01] REFER TO LOGPAGE 2586856 FOR CORRECT FAULT.SDR SWAA2024100444569Hook · looseFWD GALLEY SERVICE DOOR ; EMERGENCY ESCAPE SLIDE ; FWD GIRT BAR HOOK LOOSE .<[01] R&R RIVET IAW SRM 51-40-02.SDR SWAA2024062403233Battery Pack · no testLEFT HAND AFT GALLEY M1673 EMERGENCY BATTERY PACK WILL NOT CHARGE<[01] REPLACED LEFT HAND AFT GALLEY M1673 EMERGENCY BATTERY PACK AND ACCOMPLISHED INSTALLATION TEST IAW AMM 33-51-06-960-805. TEST GOOD.<BR><BR>ATAG:WN45285;[02] VERIFIED STEP 1<BR>AUDIT CWSDR SWAA2024062403234Battery Pack · inoperativeRIGHT HAND AFT GALLEY M1672 EMERGENCY BATTERY PACK WILL NOT CHARGE<[01] REPLACED RIGHT HAND AFT GALLEY M1672 EMERGENCY BATTERY PACK AND ACCOMPLISHED INSTALLATION TEST IAW AMM 33-51-06-960-805. TEST GOOD.<BR><BR>ATAG:WN45284;[02] VERIFIED STEP 1<BR>AUDIT CWSDR SWAA2024062500546Skin · delaminatedREMOVE/INSTALL LH T/E INBD MAIN FLAP (PN: 113A2100-61A; SN: T2242) WEDGE PANEL FOR DELAMINATION DAMAGE<[01] REMOVED AND REPLACED LH T/E INBD MAIN FLAP (PN: 113A2100-61A; SN: T2242) WEDGE PANEL;[02] REMOVED AND REPLACED LH T/E INBD MAIN FLAP OUTBOARD WEDGE PANESDR SWAA2024060798942Skin · delaminatedLH T/E INBD MAIN FLAP WEDGE PANEL DELAMINATION DAMAGE REF EA 21-157-01555. REMOVED AND REPLACED LH T/E INBD MAIN FLAP OUTBOARD WEDGE PANEL IAW SRM 51-40-02-0G-0 AND DWG 113A2100 REV A.SDR SWAA2024060798912Skin · delaminatedLEFT I/B MAIN FLAP DELAMINATED AT OB WEDGE PANEL. REMOVED LH IB MAIN FLAP OB WEDGE PANEL IAW CMM 57-53-05. RE-INSTALLED LT MAIN FLAP OUTBOARD WEDGE PANEL PER CMM 57-53-05 AND COMPLIED WITH TEMPORARY REPAIR OF DELAMINATED DAMAGE PER EA 21-157-01555 (REF TTG8QSDR SWAA2024060698913Skin · delaminatedLH OB TE FLAP DELAMINATED. ] R/R L/H O/B AFT FLAP PER AMM 21-51-22 STEPS F -F5G. REQUIRES OPS AND RIG CHECK PER SAME;[02] R/R L/H O/B AFT FLAP PER AMM 21-51-22 STEPS F -F5G.; COMPLETED OP`S AND RIG CHECKS PER AMM 27-51-22. NO DEFECTS NOTED.SDR SWAA2024060397447Panel · crackedRH WING UPPER FIXED TE PANEL 651ET LATERAL STIFFNER CRACKED 12.<[01] UPPER RIGHT WING PANEL (651CT) CRACK IS LOCATED IN THE RADIUS OF THE PANEL STIFFENER JUST FORWARD OF THE VISIBLE NUT PLATES AND IS APPROXIMATELY 12? IN LENGTH. REMOVED AND REPLACED WING PANESDR SWAA2024060497146Tire · blownMAIN TIRE #3 BLEW OUT DURING LANDING-LOSS OF A HYDRAULIC SYSTEM. REF. TTG8Q00TPFHB FOR NR 3 & 4. MLG TIRE R & R.SDR SWAA2024021250898Battery Pack · inoperativeEMERGENCY LIGHTS AT ROWS 9ABC;12ABC; FWD OF AFT CARGO AND ADJACENT SIDE ARE INOP.<[01] FOUND BATTERY PACK AT 17ABC DISCHARGED. R&R BATTERY PACK IAW AMM 33-51-06. OPS CK GOOD.SDR SWAA2023110816815Light · inoperativeR/H AFT EXTERNAL LOWER EMERGENCY LIGHT INOP 2023-637855<[01] R/H AFT EXTERNAL LOWER EMERGENCY LIGHT IAW B737-700 AMM 33-51-04-960-801. TEST IS OK;[02] CORRECTED STEP 1: REPLACED R/H AFT EXTERNAL LOWER EMERGENCY LIGHT IAW B737-700 AMM 33-51-04-960-801. TEST IS SDR SWAA2023110810151Plate · crackedCRACK PLATE LOCATED BS907 TO BS927 BETWEEN STR25R TO STR27R AT AFT CARGO COMPARTMENT (2 EA) 2023-637784<[01] REPLACED STIFFENER 2(E/A) AND FASTENERS LOC. BS907 TO BS927 BETWEEN STR25R TO STR27R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTSDR SWAA2023110810150Intercostal · crackedCRACK WEB - INTERCOSTAL LOCATED BS847 TO BS867 AT LEVEL LBL24 AT AFT CARGO COMPARTMENT 2023-637783<[01] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED BS847 TO BS867 AT LEVEL LBL24 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 ITEM 9 AND DWSDR SWAA2023110809826Intercostal · crackedCRACK ON UPPER ANGLE OF WEB INTERCOSTAL LOCATED ON FLOOR STRUCTURE BTW BS 380 TO BS 400 AND APROX BL0 ON PAX CABIN 2023-637759<[01] REPLACED UPPER ANGLE OF WEB INTERCOSTAL LOCATED ON FLOOR STRUCTURE BTW BS 380 TO BS 400 AND APROX BL0 ON PAX CABIN I.A.W B737-70SDR SWAA2023110809962Stringer · crackedCRACK STRINGER 25R LOCATED BS540 AT FWD CARGO COMPARTMENT 2023-637779<[01] TOOL USED: ULTRASONIC THICKNESS GAUGE; PN: 45MG; SN: 221861811; DUE DATE: 08-NOV-23;[02] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 220273012 AND DUE DATE: 17-DEC-23.;[03] TOOL SDR SWAA2023110909584Rib · crackedCRACK ACCESS PANEL 321A LOCATED RIB 8 AT VERTICAL STABILIZER 2023-637748 / [01] REPLACED RIB 8 LOC. ACCESS PANEL 321A AT VERTICAL STABILIZER IAW SRM B737-700 51-40-02; SRM 51-10-02 ITEM 9 AND DRAWING 174A0103 REV. - AND DRAWING 174A1008 REV:C. SEE INDIVIDUAL SSDR SWAA2023110909225Skin · crackedCRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.900 INCH. APPROX. 2023-637729 / [01] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 22027SDR SWAA2023110809222Access Panel · delaminatedDELAMINATED ACCESS PANEL 194DL WING TO BODY FAIRING AT FUSELAGE EXTERIOR 2023-637719<[01] TOOL USED CALIPER P/N: 700-113-10; S/N 0031753; DUE DATE: 27-NOV-23.;[02] TOOL USED: THERMAL CAMERA; P/N: FLIR-T530; S/N: 79316001; DUE DATE: 23 JAN 24.;[03] TOOL USED HOSDR SWAA2023110808771Floorbeam · crackedCRACK ANGLE FLOOR STRUCTURE BS695 AND RBL24.75 LOWER POSITION CENTER SECTION 2023-637667<[01] REPLACED ANGLE LOC. FLOOR STRUCTURE BS695 AND RBL24.75 LOWER POSITION CENTER SECTION IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 111A6000 SHEET: 304 REV:-<BR>SEE SDR SWAA2023110808772Floorbeam · crackedCRACK ANGLE FLOOR STRUCTURE BS540 AND BL0 TO LBL 24.75 CENTER SECTION 2023-637666<[01] REPLACED ANGLE FLOOR STRUCTURE BS540 AND BL0 TO LBL24.75 CENTER SECTION IAW SRM B737-700 51-40-02 AND SRM 51-10-02 ITEM 9;[02] CORRECTIVE ACTION CERTIFIEDSDR SWAA2023110808774Angle · crackedCRACK ANGLE FLOOR STRUCTURE BS540 AND RBL24.75 TO RBL 45.50 CENTER SECTION 2023-637668<[01] REPLACED ANGLE FLOOR STRUCTURE BS540 AND RBL24.75 TO RBL 45.50 CENTER SECTION IAW SRM B737-700 51-40-02 AND SRM 51-10-02 ITEM 9;[02] CERTIFIED WORK PERFORMED.SDR SWAA2023110808780Gusset · crackedCRACK GUSSET LOCATED BS 500D; STRINGER 19 L FWD CARGO COMPARTMENT 2023-637704<[01] REPLACED GUSSET AND FASTENERS LOCATED BS 500D; STRINGER 19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ; ITEM 9 ; SRM 51-40-02 AND DWG 143A7902 ; SHEET 209 ; REV-.<BR><BR>SSDR SWAA2023110808781Gusset · crackedCRACK GUSSET LOCATED BS 500D; STRINGER 19R FWD CARGO COMPARTMENT 2023-637705<[01] REPLACED GUSSET AND FASTENERS LOCATED BS 500D; STRINGER 19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ; ITEM 9 AND SRM 51-40-02 AND DWG 143A7902 ; SHEET 209 ; REV-.<BR><BR>SDR SWAA2023110808767Battery Pack · inoperativeINOP EMERGENCY BATTERY PACK ON STA 600 TO STA 620 LT SIDE AT PASSENGER CABIN 2023-637625<[01] REPLACED EMERGENCY BATTERY PACK ON STA 600 TO STA 620 LT SIDE AT PASSENGER CABIN IAW 737-700 AMM 33-51-06-960-805 OLD PART P/N D717-01-100SWA S/N 75500 NEW PART P/N ASDR SWAA2023110808766Battery Pack · inoperativeINOP EMERGENCY BATTERY PACK ON STA 600 TO STA 620 RT SIDE AT PASSENGER CABIN 2023-637624<[01] REPLACED EMERGENCY BATTERY PACK ON STA 600 TO STA 620 RT SIDE AT PASSENGER CABIN IAW 737-700 AMM 33-51-06-960-805 OLD PART P/N D717-01-100SWA S/N 220215 NEW PART P/N SDR SWAA2023110808769Hinge · corrodedCORROSION HINGE WASTE SERVICE DOOR 145AL AT FUSELAGE EXTERIOR (2 EA) 2023-637652<[01] REPLACED HINGE WASTE SERVICE DOOR 145AL AT FUSELAGE EXTERIOR (2 EA) IAW B737-700 SRM 51-40-02;[02] CORRECTED STEP 1 . REPLACED HINGE WASTE SERVICE DOOR 145AL AT FUSELAGE EXTESDR SWAA2023110808762Vapor Barrier · crackedCUSTOMER REQUEST - CRACK ON VAPOR BARRIER LOCATED BS663 RBL 27 RH SIDE WL 161 AT MAIN WHEEL WELL COMPARTMENT 2023-637618<[01] TOOL USED CALIPER PN:500-197-30 ; SN:B20189527 DUE DATE 26/DEC/23;[02] TOOL USED: HOT BONDER PN:HCS9200B-AV; SN:18196021 DUE DATE 24-JSDR SWAA2023050131371Girt Bar · out of adjustGIRT BAR NOT IN THE CORRECT POSITION<[01] NODEFECT NOTED PER AMM 25-66-01SDR SWAA2023042730885Light · inoperativeWINDOW LIGHT EMER. EXIT DOOR INOP EMERGENCY LIGHTS OPS GOOD<[01] AC OK TO CONTINUE PER MEL 33-2-03 SP1B AUTH#131432;[02] RE-LAMP WINDOW LIGTH EMER EXIT DOOR PER AMM 33-51-01. OPS CHECK GOOD.SDR SWAA2023041728125Battery Pack · inoperativeMULTIPLE INTERIOR EMERGENCY LIGHTS INOP<[01] R&R FWD R/H EMERGENCY LIGHT CHARGER ASSEMBLY AND BATTERY PACK PER AMM 33-51-06. OPS CHECK GOODSDR SWAA2022041192266Light · inoperativeFWD LH INTERIOR EMERGENCY LIGHTS INOP / [01] R&R FWD LH EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD.SDR SWAA2021121350529Threshold · crackedFWD CARGO; AFT CORNER THRESHOLD CRACKED, DRILLED UP NEW THRESHOLD AFT CORNER IAW SRM 51-40-02. INSTALLED FWD CARGO; AFT CORNER THRESHOLD PER AMM 53-11-02.SDR SWAA2021121049275None · inoperativeSUPPLEMENTAL INFORMATION: LEFT OVER WING EXIT LIGHT ABOVE DOOR WINDOW INOP ; / [01] REMOVED AND REPLACED BALLAST PER REF. SOPM 20-50-01 AND AMM 25-21-20 OPS CHECK GOOD PER REF. AMM 33-21-00.; [02] REMOVED AND REPLACED BALLAST PER REF. SOPM 20-50-01 AND AMM 25-SDR SWAA2021121348814Fairing · delaminated#8 FLAP AFT CANOE FAIRING IS DELAMINATED ON LOWER AFT END. ; / [01] REMOVED AND REPLACED #8 AFT CANOE FAIRING PER REF SRM 51-40-02; [02] INSPECTED WORK PERFORMEDSDR SWAA2021121345946None · crackedSUPPLEMENTAL INFORMATION: FWD CARGO COMPARTMENT L/H TRANSITION ANGLE CRACKED AND PUNCTURES STA. 500C+4. ; / [01] DAMAGE IS OUT OF LIMITS IAW SRM 53-30-53-1A-2.; [02] INSTALLED BONDING NUTPLATES TO ZEE ANGLE FROM STA 396 TO 500D PER SRM 51-40-10; [03] REPAIRED SDR SWAA2021121345735None · corrodedSUPPLEMENTAL INFORMATION: CORROSION FOUNDED ON FWD CARGO AFT R/H BULKHEAD TRANSICION ANGLE ; / [01] REMOVED CORROSION IAW SRM 51-10-02; AREA IS OUT OF LIMITS IAW SRM 53-30-80-1A-1.; [02] PART WILL BE INSTALLED ON FAULT TTG8Q004FUDH. 5330-E-16461-NG CPCP / AP MSDR SWAA2021121345734None · corrodedSUPPLEMENTAL INFORMATION: CORROSION FOUNDED ON FWD CARGO AFT L/H BULKHEAD TRANSICION ANGLE ; / [01] REMOVED CORROSION IAW SRM 51-10-02; AREA IS OUT OF LIMITS IAW SRM 53-30-80-1A-1.; [02] THIS PART WILL BE INSTALLED ON FAULT TTG8Q004FUDH. 5330-E-16461-NG CPCP/ASDR SWAA2021121344809Panel · crackedSUPPLEMENTAL INFORMATION: PANEL 561BB HAS SEVERAL FASTENER HOLES CRACKED ALONG TRAILING EDGE. ; / [01] C/W DAMAGE REMOVAL PER SRM 51-70-05 2R-9.; [02] VERIFIED CORRECTIVE ACTION 1; [03] FILLED FASTENER HOLES WITH CHOPPED FIBERS AND RESIN PER SRM 51-70-05-2R-9.SDR SWAA2021121344808Panel · crackedSUPPLEMENTAL INFORMATION: PANEL 561AB HAS SEVERAL FASTENER HOLES CRACKED ALONG TRAILING EDGE. ; / [01] C/W DAMAGE REMOVAL PER SRM 51-70-05 2R-9.; [02] VERIFIED CORRECTIVE ACTION 1; [03] FILLED FASTENER HOLES WITH CHOPPED FIBERS AND RESIN PER SRM 51-70-05-2R-9.SDR SWAA2021121344807None · crackedSUPPLEMENTAL INFORMATION: PANEL 661CB HAS SEVER FASTENER HOLES CRACKED ALONG THE TRAILING EDGE. ; / [01] C/W DAMAGE REMOVAL PER SRM 51-70-05 2R-9.; [02] VERIFIED CORRECTIVE ACTION 1; [03] FILLED FASTENER HOLES WITH CHOPPED FIBERS AND RESIN PER SRM 51-70-05-2R-SDR SWAA2021121344806Panel · crackedSUPPLEMENTAL INFORMATION: PANEL 661BB HAS SEVERAL FASTENER HOLES CRACKED ON TRAILING EDGE. ; / [01] C/W DAMAGE REMOVAL PER SRM 51-70-05 2R-9.; [02] VERIFIED CORRECTIVE ACTION 1; [03] FILLED FASTENER HOLES WITH CHOPPED FIBERS AND RESIN PER SRM 51-70-05-2R-9.; [SDR SWAA2021121344805Panel · crackedSUPPLEMENTAL INFORMATION: PANEL 561CB HAS SEVERAL FASTENER HOLES CRACKED ALONG TRAILING EDGE. ; / [01] C/W DAMAGE REMOVAL PER SRM 51-70-05 2R-9.; [02] VERIFIED CORRECTIVE ACTION 1; [03] FILLED FASTENER HOLES WITH CHOPPED FIBERS AND RESIN PER SRM 51-70-05-2R-9.SDR SWAA2021121344804Panel · crackedSUPPLEMENTAL INFORMATION: T/E PANEL 661AB HAS SEVERAL FASTENER HOLES CRACKED ON TRAILING EDGE ; / [01] C/W DAMAGE REMOVAL PER SRM 51-70-05-2R-9; [02] VERIFIED CORRECTIVE ACTION 1; [03] FILLED FASTENER HOLES WITH CHOPPED FIBERS AND RESIN PER SRM 51-70-05-2R-9.;SDR SWAA2021121344118None · crackedSUPPLEMENTAL INFORMATION: RH STAB #6 RIB HAS AN HFEC INDICATION OF A CRACK IN THE 4TH STIFFENER FROM THE FRONT ; / [01] DAMAGE IS LOCATED ON THE #6 RIB IN THE RH STABILIZER; [02] CUT OUT DAMAGE IAW SRM 55-10-09-2R-4.; [03] C/W NDT INSP OF CUT-OUT AND RIB SKIN SDR SWAA2021121344124Stiffener · crackedLEFT STABILIZER NR 5 RIB HAS AN HFEC INDICATION OF A CRACK IN THE 3RD STIFFENER FROM THE FRONT. ] CUT OUT DAMAGE IAW SRM 55-10-09-2R-4. COMPLIED WITH THE NDT OF DAMAGE REMOVED IN CORRECTIVE ACTION 1. FOUND FURTHER FLAWS OUTSIDE OF ORIGINAL CUT OUT IAW NDT MASDR SWAA2021111944125Structure · corrodedLIGHT SURFACE CORROSION ON UPPER SURFACE OF PANEL SUPPORT STRUCTURE AT STA 268.25 LBL 11 TO RBL 11 WL 207.5. MRKD ; LIGHT SRFACE CORROSION ON PPER SRFACE OF PANEL SPPORT STRCTRE AT STA 268.25 LBL 11 TO RBL 11 WL 207.5. REMOVED LIGHT POWDER AND SEALANT FOUND NOSDR SWAA000043632None · elongatedFORWARD CARGO FLOOR STRUCTURE R/H TRANSITION ANGLE STA. 400 RBL 24 HAS ELONGATED HOLE. (MARKED) ; / [01] DAMAGE IS OUT OF LIMITS IAW SRM 51-40-05.; [02] MATERIAL IDENTIFIED USE BAC1496-444 7075-T6 CLAD FORMED CHANNEL . LOCATED DRILLED UP TO HOLE SIZES PER SRM
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