N925WN
Service difficulty reports · 252
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 = 'N925WN' 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 = 'N925WN' 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 SWAA2024061386184Floor Panel · peelingFWD CABIN FLOOR PANEL 231BF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-046<[01] RECEIVED FWD CABIN FLOOR PANEL 231BF WILL BE INSTALL IN ITEM TTG8Q00SCGXV;[02] VERIFIED STEP 1SDR SWAA2024061386185Floor Panel · peelingFWD CABIN FLOOR PANEL 231CF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-047<[01] RECEIVED FWD CABIN FLOOR PANEL 231CF WILL BE INSTALL ON ITEM TTG8Q00SCGXT;[02] VERIFIED STEP 1SDR SWAA2024061386187Floor Panel · peelingAFT CABIN FLOOR PANEL 241UF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-048<[01] RECEIVED NEW FLOOR PANEL P/N 146A5810-470 PANEL # 241VF INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00SCGYQ;[02] RECEIVED NEW FLOOR PANEL P/N 146A5810-470 PANEL # 241UF INSSDR SWAA2024061385510Floor Panel · peelingCABIN CENTER SECTION FLOOR PANEL 241DF HAS PEELED UPPER SURFACE LAYER FIRBERS. 124-001<[01] RECEIVED NEW FLOOR PANEL 241DF; IT WILL BE INSTALLED ON TTG8Q00S5CRH.;[02] VERIFIED STEP 1.SDR SWAA2024061385513Floor Panel · peelingCABIN CENTER SECTION FLOOR PANEL 242DF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-002<[01] RECEIVED NEW FLOOR PANEL 242DF; IT WILL BE INSTALLED ON TTG8Q00S5CR7.;[02] VERIFIED STEP 1.SDR SWAA2024061385514Floor Panel · peelingCABIN CENTER SECTION FLOOR PANEL 232SF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-003<[01] RECEIVED CABIN CENTER SECTION FLOOR PANEL 232SF WILL BE INSTALLED ON ITEM TTG8Q00TBLTB;[02] RECEIVED CABIN CENTER SECTION FLOOR PANEL 232SF WILL BE INSTALLED ON ITEM TTGSDR SWAA2024061385517Floor Panel · peelingCABIN CENTER SECTION FLOOR PANEL 241FF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-004<[01] RECEIVED NEW FLOOR PANEL 241FF; IT WILL BE INSTALLED ON TTG8Q00S5CRD.;[02] VERIFIED STEP 1.SDR SWAA2024061385518Floor Panel · peelingCABIN CENTER SECTION FLOOR PANEL 241AF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-005<[01] RECEIVED NEW FLOOR PANEL 241AF; IT WILL BE INSTALLED ON TTG8Q00S5CRP.;[02] VERIFIED STEP 1SDR SWAA2024061385520Floor Panel · peelingCABIN CENTER SECTION FLOOR PANEL 231YF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-006<[01] RECEIVED NEW FLOOR PANEL 231YF; IT WILL BE INSTALLED ON TTG8Q00S5CS3.;[02] VERIFIED STEP 1.SDR SWAA2024061385522Floor Panel · peelingCABIN CENTER SECTION FLOOR PANEL 231XF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-007<[01] RECEIVED NEW FLOOR PANEL 231XF; IT WILL BE INSTALLED ON TTG8Q00S5CS5.;[02] VERIFIED STEP 1.SDR SWAA2024061385682Floor Panel · peelingAFT CABIN WET AREA FLOOR PANEL 241ADF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-012<[01] RECEIVED AFT CABIN FLOOR PANEL 241ADF WILL BE INSTALL ON ITEM TTG8Q00SCGYU;[02] RECEIVED AFT CABIN FLOOR PANEL 241ADF WILL BE INSTALL ON ITEM TTG8Q00SCGYW;[03] VERIFIED SSDR SWAA2024061385684Floor Panel · peelingAFT CABIN WET AREA FLOOR PANEL 241ACF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-015<[01] RECEIVED REPAIRED FLOOR PANEL 241ACF. <BR>P/N: 147A5810-13.<BR>PO: 2059779.<BR>PANEL WILL BE INSTALLED ON TTG8Q00SCGYY.;[02] VERIFIED STEP 1SDR SWAA2024061385685Floor Panel · peelingAFT CABIN WET AREA FLOOR PANEL 242VF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-016<[01] RECEIVED NEW FLOOR PANEL #242VF P/N:147A5810-350; INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00SCGZD.;[02] VERIFIED RECEIVED NEW FLOOR PANEL AND INSTALLATION WILLSDR SWAA2024061385687Floor Panel · peelingAFT CABIN WET AREA FLOOR PANEL 241ABF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-018<[01] RECEIVED REPAIRED FLOOR PANEL 241ABF. <BR>P/N: 147A5810-88.<BR>PO: 2059779.<BR>PANEL WILL BE INSTALLED ON TTG8Q00SCGZ1.;[02] VERIFIED STEP 1SDR SWAA2024061385688Floor Panel · peelingAFT CABIN WET AREA FLOOR PANEL 241AAF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-020<[01] RECEIVED NEW FLOOR PANEL # 241AAF P/N:147A5810-8; INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00SCGZ3.;[02] VERIFIED RECEIVED NEW FLOOR PANEL AND INSTALLATION WILSDR SWAA2024061385690Floor Panel · peelingAFT CABIN WET AREA FLOOR PANEL 242UF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-022<[01] RECEIVED NEW FLOOR PANEL # 242UF P/N: 147A5810-95; INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00SCGZF;[02] VERIFIED RECEIVED NEW FLOOR PANEL AND INSTALLATION WILLSDR SWAA2024061385692Floor Panel · peelingAFT CABIN WET AREA FLOOR PANEL 241XF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-025<[01] RECEIVED REPAIRED FLOOR PANEL 241ABF. <BR>P/N: 147A5810-100.<BR>PO: 2059779.<BR>PANEL WILL BE INSTALLED ON TTG8Q00SCGYJ.;[02] VERIFIED STEP 1SDR SWAA2024061385697Floor Panel · peelingAFT CABIN WET AREA FLOOR PANEL 241YF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-026<[01] RECEIVED REPAIRED FLOOR PANEL 241YF. <BR>P/N: 147A5810-77.<BR>PO: 2059779.<BR>PANEL WILL BE INSTALLED ON TTG8Q00SCGZ7.;[02] VERIFIED STEP 1SDR SWAA2024061385698Floor Panel · peelingAFT CABIN WET AREA FLOOR PANEL 241ZF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-027<[01] RECEIVED NEW FLOOR PANEL # 241ZF; P/N:147A5810-98; INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00SCGZ5.;[02] VERIFIED RECEIVED NEW FLOOR PANEL AND INSTALLATION WILSDR SWAA2024061385693Floor Panel · peelingAFT CABIN WET AREA FLOOR PANEL 242RF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-028<[01] RECEIVED NEW FLOOR PANEL # 242RF P/N:147A5810-2; INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00SCGZM.;[02] VERIFIED RECEIVED NEW FLOOR PANEL AND INSTALLATION WILL SDR SWAA2024061385694Floor Panel · peelingAFT CABIN WET AREA FLOOR PANEL 242SF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-029<[01] RECEIVED REPAIRED FLOOR PANEL 242SF. <BR>P/N: 147A5810-99.<BR>PO: 2059779.<BR>PANEL WILL BE INSTALLED ON TTG8Q00SCGZK.;[02] VERIFIED STEP 1SDR SWAA2024061385525Shim · damagedMAIN CABIN GIRT BAR FITTINGS SHIMS L1 R1 AND R2 L2 DAMAGED<[01] REPLACED MAIN CABIN GIRT BAR FITTINGS SHIMS L1 R1 AND R2 L2 AS PER AMM 25-66-02-400-801;[02] VERIFIED STEP 1.<BR>AUDIT C/W PER 52.02.02.SDR SWAA2024061484920Skin · crackedCRACK FOUND AT LEFT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90; 24' FROM FRONT SPAR; I/B ROW. CRACK LENGTH :0.531' CRACK FOUND AT LEFT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90 24' FROM FRONT SPAR I/B ROW. CRACK LENGTH :0.531'<[01] ACCOMPLISSDR SWAA2024061385206Scuff Plate · crackedR-1 DOOR SCUFF PLATE CRAKED AT AFT CORNER<[01] WELD REPAIRED SCUFFPLATE FOR R1 DOOR PER SRM53-10-15-2R-2; WORK ACCOMPLISHED BY J.L. WELDING; W/O# 16612; PO# 414702.<BR>SCUFFPLATE WILL BE INSTALLED ON (TTG8Q003GBLY);[02] VERIFIED STEP 1SDR SWAA2024061484912Panel · crackedFAIRING PANEL 191D HAS A CRACK ON BOLT HOLE 1 INCH FROM INNER LEFT EDGE AND 24 INCHES FROM INNER FWD EDGE.<[01] APPLIED REPAIR AT PANEL#191D PER B737 SRM 51-70-04-2R-0 PARAGRAPH(4;N) MATERIAL USED RESIN EA9390 PO#1791128 AND FIBER GLASS PO#1690463 TOOL USED TESDR SWAA2024061485675Panel · corrodedP15 REFUEL PANEL FACEPLATE HAS SPOTS OF CORROSION<[01] REMOVED THE REFUEL PANEL AS PER REFERENCE AMS 28-41-61-000-801; INSTALLED P15 REFUEL PANEL AS PER AMM 28-21-00-400-801; PERFORMED REFUEL PANEL INSTALLATION TEST AS PER AMM 28-21-00-400-801. TEST FOUND NORMSDR SWAA2024061484911Scuff Plate · crackedAFT CARGO; AFT SCUFF PLATE CORNER CRACK. P/N 146A8341-8<[01] RECEIVED SERVICEABLE AFT SCUFF PLATE P/N 146A8341-8 PO # 414679; WELDED BY JL WELDING INC; REF TASK CARD TTG8Q00C9FUA FOR AFT SCUFF PLATE INSTALLATION.;[02] VERIFIED STEP 1.SDR SWAA2024042377634Proximity Sensor · faultedLE FLAPS TRANSIT LIGHT REMAINED ILLUMINATED AFTER TAKEOFF FLAPS RETRACTION.<[01] R/R'D #3 LE FLAP EXT PROX SENSOR PER AMM 27-88-11. OPS CHECK GOOD.SDR SWAA2024032868384Light · inoperativePAX CABIN EMERGENCY EXIT LIGHT INOP @ 7ABC.<[01] REMOVED AND REPLACED PAX CABIN EMERGENCY EXIT LIGHT @7ABC. OPS CHECK GOOD. 33-51-03SDR SWAA2024032165896Gcu · inoperativeFL 410 #1 DRIVE AND SOURCE OFF LIGHT<[01] R/R #1 GCU REF AMM 24-21-81. RAN ENGINE AT IDLE PER AMM 71-00-00; OPS CK GOOD. SEE TTG8Q00S84GP FOR PART R/RSDR SWAA2024031262146Bracket · looseGIRT BAR FWD ENTRY DOOR SLIDE LOOSE BRACKET<[01] RE-SECURED SLIDE GIRT BAR ATTACHMENT BRACKET PER AMM 25-66-01SDR SWAA2024011640938Handle · brokenL2 DOOR ASSIST HANDLE BROKEN<[01] REMOVED AND REPLACED ASSIST HANDLE PER SIPSDR SWAA2023103015699Girt Bar · shearedAFT. ENTRY DOOR SLIDE GIRTH BAR AFT HOLDER SHEARED RIVITS<[01] R/R RIVITS PER SRM 51-40-02. C/W MT 725-61-06SDR SWAA2023092609219Pump · leakingLOSS OF SYSTEM HYDRAULIC B;2 LOW-PRESSURE LTS AND QUANTITY ZERO. REF #TTG8Q00NMN78 FOR JOB PERFORMED. R & R NR 2 ENG EDP PER AMM 29-11-11; R&R B SYS CASE DRAIN FILTERS PER AMM 29-11-41; R & R B HYD EMDP IAW AMM 29-11-21; R & R B SYS RETURN FILTER IAW AMM 29-SDR SWAA2023092804318Limiter · leakingFIRE DEPARTMENT REPORTED SMOKE FROM RIGHT MAIN LANDING GEAR<[01] REF TTG8Q00NN60N FOR THE JOB PERFORMED.;[02] REMOVED AND REPLACED TRAILING EDGE FLAP FLOW LIMITER REF AMM 27-51-67;[03] C/WSDR SWAA2023092604319Pump · leakingLOSS OF SYSTEM HYDRAULIC B;2 LOW-PRESSURE LTS AND QUANTITY ZERO. R&R #2 ENG EDP PER AMM 29-11-11; R&R B SYS CASE DRAIN FILTERS PER AMM 29-11-41; R&R ?B? HYD EMDP IAW AMM 29-11-21; R&R B SYS RETURN FILTER IAW AMM 29-11-61; R&R B SYS PRESSURE MODULE FILTER PER SDR SWAA2023080986923Seat · out of adjustSEAT 10A RECLINING BACK INTO EXIT ROW PER FA<[01] ADJUSTED HYDRO LOCK PER M/M25-22-00SDR SWAA2023071076837Pump · failedB HYD SYSTEM FAILURE<[01] REMOVED AND REPLACED #2 ENGINE DRIVE HYDRAULIC PUMP IAW MM 29-11-11<BR>REMOVED AND REPLACED B SYSTEM ELECTRIC HYDRAULIC PUMP IAW MM 29-11-21<BR>REMOVED AND REPLACED B SYSTEM HYDRAULIC FILTERS AND HYDRAULIC FUSE IAW MM 29-11-41<BR><BR>SDR SWAA2023071076919Pump · failedB HYD SYSTEM FAILURE<[01] REMOVED AND REPLACED #2 ENGINE DRIVE HYDRAULIC PUMP IAW MM 29-11-11<BR>REMOVED AND REPLACED B SYSTEM ELECTRIC HYDRAULIC PUMP IAW MM 29-11-21<BR>REMOVED AND REPLACED B SYSTEM HYDRAULIC FILTERS AND HYDRAULIC FUSE IAW MM 29-11-41<BR><BR>SDR SWAA2023071076920Filter · failedB HYD SYSTEM FAILURE<[01] REMOVED AND REPLACED #2 ENGINE DRIVE HYDRAULIC PUMP IAW MM 29-11-11<BR>REMOVED AND REPLACED B SYSTEM ELECTRIC HYDRAULIC PUMP IAW MM 29-11-21<BR>REMOVED AND REPLACED B SYSTEM HYDRAULIC FILTERS AND HYDRAULIC FUSE IAW MM 29-11-41<BR><BR>SDR SWAA2023071076921Fuse · failedB HYD SYSTEM FAILURE<[01] REMOVED AND REPLACED #2 ENGINE DRIVE HYDRAULIC PUMP IAW MM 29-11-11<BR>REMOVED AND REPLACED B SYSTEM ELECTRIC HYDRAULIC PUMP IAW MM 29-11-21<BR>REMOVED AND REPLACED B SYSTEM HYDRAULIC FILTERS AND HYDRAULIC FUSE IAW MM 29-11-41<BR><BR>SDR SWAA2023053153315Cover · out of positionFLIGHT ATTENDANT REPORTS AFT ENTRY EMERGENCY SLIDE MANUAL INFLATION HANDLE COVER OUT OF POSITION<[01] RE-SECURED AFT ENTRY SLIDE MANUAL HANDLE COVER PER SIPSDR SWAA2022091552444Panel · elongatedPANEL 193B PANEL HAS ELONGATED HOLES. / [01] REMOVED AND REPLACED PANEL 193B PER SRM 51-40-02.SDR SWAA2022052409808Light · inoperativeEXTERIOR EMERGENCY LIGHT L/H AFTER WING INOP. / [01] RELAMPED EXTERIOR EMERGENCY LIGHT L/H AFTER WING AS PER B737 AMM 33-51-04-960-801. TEST OK;[02] VERIFIED STEP 1.SDR SWAA2022052609549Scuff Plate · crackedAFT CARGO FWD SCUFF PLATE CORNER CRACKED. / [01] LOCATED AND DRILLED NEW FWD CORNER SCUFF PLATE AT AFT CARGO DOOR CUTOUT PER 737-700 SRM 51-40-05-0G-0.;[02] ACCOMPLISHED PARTS TRANSACTION;[03] C/WSDR SWAA2022052408175Vapor Barrier · crackedL/H STA 663 VAPOR BARRIER CRACK @ LBL 45 / [01] MEASUREMENTS;[02] CLEANED 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 AND OK TO INSTALL REPAIR;[04] REPAIRED BOTH SIDESSDR SWAA2022052405980Lens · brokenL/H SIDE EMERGENCY DOOR EXIT SIGN LENS BROKEN. / [01] REMOVED AND REPLACED L/H SIDE EMERGENCY DOOR EXIT SIGN LENS AS PER B737 AMM 33-51-01-960-801.;[02] VERIFIED STEP 1.SDR SWAA2022052605029Structure · corrodedAFT CARGO FLOOR STRUCTURE AT STA 847+12' AND RBL-21 WL 164 WITH CORROSION SPOT. (DOOR CUTOUT AFT SHIELD. (234-5). / [01] REMOVED CORROSION AFT CARGO FLOOR STRUCTURE AT STA 847 + 12' AND RBL 21 WL 164 DOOR CUT OUT AFF SHIELD IAW SRM 51-10-02-0G-0;[02] VERIFIED SDR SWAA2022052605034Structure · corrodedAFT CARGO FLOOR STRUCTURE AT STA 747+19 AND RBL -21 WL 155 HAS CORROSION AS MARKED. (234-9). / [01] REMOVED CORROSION AFT CARGO FLOOR STRUCTURE AT STA 747+9 AND RBL 21 WL 155 IAW B7737 SRM 51-10-02-0G -0.;[02] CORRECTION ERROR: STA 747 +19 AND RBL21 WL 155.;[0SDR SWAA2022052605031Channel · corrodedAFT CARGO LT Z CHANNEL AT STA 767+14' HAS CORROSION (234-10) REMOVED CORROSION AFT CARGO COMP LT Z CHANEL AT STA 767 +14' IAW B737 SRM51-10-02-0G-0. EVALUATION AREA :ORIGINAL MAT 0.040 .MAT LOSS 0.015.MAT REMAINING 0.025 .FOUND OUT LIMITS IAW B737 SRM 53-00-5
Back to N925WN