N215WN
Service difficulty reports · 291
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 = 'N215WN' 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 = 'N215WN' 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 SWAA2026080446798Starter · failedDURING PUSH BACK NR 2 ENG FAILED TO START. NO ROTATION. REMOVED AND REPLACED NR 2 ENGINE STARTER IAW AMM 80-11-01 OPS AND LEAK CHECKED GOOD.SDR SWAA2026021269236Isolator · crackedPASSENGER CABIN FORWARD GALLEY SERVICE DOOR FORWARD UPPER SLIDE ISOLATOR CRACKED. R & R UPPER SLIDE ISOLATOR IAW SRM 51-40-02.SDR SWAA2025122254056Slide · low pressureAFT SERVICE DOOR SLIDE LOW PRESSURE<[01] R&R AFT SERVICE ESCAPE SLIDE PER AMM 25-66-01; MT 725-61-06 REM/INSTLSDR SWAA2025100620121Lens · damagedAFT LAVATORY EMERGENCY EXIT SIGN HAS DAMAGED LENS. REMOVED AND REPLACED DAMAGED LENS FROM AFT LAV EMERGENCY EXIT SIGN AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-01-960-802.SDR SWAA2025090309867Handle · looseASSIST HANDLE ON FWD ENTRY DOOR LOOSE RE-SECURED FWD ENTRY DOOR ASSIST HANDLE PER AMM 52-11-31. RESECURED ASSIST HANDLE PER AMM 52-11-31.<BR><BR>3194309SDR SWAA2025072894222Fairing · damagedSTRUT FAIRING ON NR 2 ENGINE AT 3 O`CLOCK POSITION HAS ELONGATED HOLE. PARTIALLY INSTALLED STRUT FAIRING PANEL IAW AMM 73-21-06, FINISHED INSTALLING REMAINING 2 SCREWS COMMON TO STRUT FAIRING REF AMM 73-21-06.SDR SWAA2025062584647Girt Bar · out of positionFWD SERVICE DOOR GIRT BAR TO SLIDE IS OUT OF POSITION<[01] RESET GIRT BAR AS NEEDED PER SIPSDR SWAA2025060377055Holder · brokenFWD GALLEY EMERGENCY FLASHLIGHT HOLDER BROKEN <[01]. REPLACED BROKEN FLASHLIGHT HOLDER PER SRM 51-40-01 AND AMM 25-64-00.SDR SWAA2025022498262Lamp · inoperativeRH EMERGENCY EXIT WINDOW EXIT LIGHT BULB OUT <[01]. CORRECTLY INSTALLED RH EMERGENCY WINDOW EXIT LIGHT LAMP PER AMM 33-25-00-960-804;[02] VERIFIED CORRECTIVE ACTION #1.SDR SWAA2025022498258Battery Pack · inoperativeEMERGENCY LIGHT INSIDE CABIN ROW 12 ABC; 9 ABC ARE INOP <[01]. DURING TROUBLESHOOTING; DETERMINED THAT THIS DEFECT AND DEFECT TTG8Q00YW88E ARE BOTH CONTROLLED BY BATTERY CHARGER/POWER SUPPLY ASSEMBLY M1670 PER WDM 33-51-13. REPLACED BATTERY PACK/CHARGER ASSEMBSDR SWAA2025022499085Charger · inoperativeEMERGENCY LIGHT INSIDE CABIN ROW 12 ABC; 9 ABC ARE INOP <[01]. DURING TROUBLESHOOTING; DETERMINED THAT THIS DEFECT AND DEFECT TTG8Q00YW88E ARE BOTH CONTROLLED BY BATTERY CHARGER/POWER SUPPLY ASSEMBLY M1670 PER WDM 33-51-13. REPLACED BATTERY PACK/CHARGER ASSEMBSDR SWAA2025022498257Battery Pack · inoperativeAFT OF WING EMERGENCY SLIDE LIGHT BOTH LH AND RH SIDE ARE OUT <[01]. DURING TROUBLESHOOTING; DETERMINED THAT THIS DEFECT AND DEFECT TTG8Q00YW88S ARE BOTH CONTROLLED BY BATTERY CHARGER/POWER SUPPLY ASSEMBLY M1670 PER WDM 33-51-13. REPLACED BATTERY PACK/CHARGER SDR SWAA2025022499086Charger · inoperativeAFT OF WING EMERGENCY SLIDE LIGHT BOTH LH AND RH SIDE ARE OUT <[01]. DURING TROUBLESHOOTING; DETERMINED THAT THIS DEFECT AND DEFECT TTG8Q00YW88S ARE BOTH CONTROLLED BY BATTERY CHARGER/POWER SUPPLY ASSEMBLY M1670 PER WDM 33-51-13. REPLACED BATTERY PACK/CHARGERSDR SWAA2025022498256Light · disconnectedEMERGENCY EXIT LIGHT INOP AFT OF FED <[01]. CHECKED FOR GROUND AND POWER AT L731 (FORWARD ESCAPE SLIDE LIGHT); FOUND NEITHER GROUND OR VOLTAGE AY L731 LIGHT SOCKET PER WDM 33-51-12. FOUND INCOMPLETE CONNECTION AT D11074. RECONNECTED AND TESTED PER WDM 33-51-12SDR SWAA2025022497379Light · burned outEMERGENCY EXIT LIGHT SIDEWALL SIGN AT L/H OVERWING EXIT HAS BURNED OUT BULBS <[01]. RELAMPED EMERGENCY EXIT LIGHT AT L/H SIDEWALL OVERWING EXIT AND PERFORMED A SATISFACTORY TEST OF NEW LAMPS IAW AMM 33-51-01-960--801 STEPS 2.C.(1); (A); 1); 4); B); (C); (2)-(SDR SWAA2025022496769Battery Pack · inoperativeEMERGENCY LIGHTS FWD RIGHT OVERDOOR EXIT INOP L1067 <[01]. PER TROUBLESHOOTING PERFORMED GOOD CONTINUITY CHECK FROM CONNECTOR D10750 TO CONNECTOR D2968 IAW WDM 33-51-12; SWAP OF BATTERY PACKS BETWEEN M1675 AND M1674 PERFORMED; FAILURE CHANGED; BATTERY PACK M16SDR SWAA2025022494152Lens · damagedAFT LAVE 'B' EMERGENCY EXIT LIGHT LENS DAMAGED<[01] REMOVED AND REPLACED AFT LAVE 'B' EMERGENCY EXIT LIGHT LENS PER AMM 33-51-01-960-801;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR SWAA2025022493806Wire · brokenG-1 GALLEY MOUNTED EMERGENCY EXIT LIGHT WIRE BROKEN AT CONNECTOR<[01] DISCONNECTABLE SPLICE AT EMERGENCY EXIT LIGHT-FWD-FLOOR PROXIMITY G-1 GALLEY WAS REPLACED AND A SATISFACTORY OPERATIONAL TEST OF THE EMERGENCY LIGHTS WAS PERFORMED WITH NO DEFECTS FOUND IAW SDR SWAA2025022489513Baffle · crackedFWD CARGO BAY L/H BAFFLE CRACKED BS440 TO BS460 LBL22 WL156<[01] CORRECTION: FORWARD CARGO BAY L/H BAFFLE CRACKED BS440 TO BS460 LBL22 WL156 [TTG8Q00YBXHD].;[02] REMOVED DAMAGED BAFFLE AND INSTALLED NEW BAFFLE AS PER SRM 51-40-02-0G-0 AND DRAWING 143A7505 REV.SDR SWAA2025022588983Vapor Barrier · crackedSTIFFENER CRACKED COMMON TO VAPOR BARRIER BS663 LBL26 WL151 <[01]. REMOVED AND REPLACED NEW STIFFENER COMMON TO VAPOR BARRIER BS663 LBL26 WL151 IAW SRM 51-40-02-0G-0 AND DWG 111A1000 REV:-.SDR SWAA2025022488980Baffle · crackedFORWARD CARGO BAY BAFFLE IS CRACKED BS460 TO BS480 LBL25 WL156<[01] REMOVED DAMAGED BAFFLE AND INSTALLED NEW BAFFLE AS PER SRM 51-40-02-0G-0 AND DRAWING 143A7505 REV.-.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2025022588169Seat Track · corrodedCORROSION ON LBL 45 SEAT TRACK WELL AT STA 500A+8; WL 208.1. <[01] DISCREPANCY RECORD ON CCN TTG8Q00Y9RNQ REQUIRED REMOVED AND REPLACED THEREFORE CARD TO BE CLOSED AND ALL WORK DONE WAS RECORDED ON TTG8Q00Y9RNQ; [02] DISCREPANCY RECORD ON CCN TTG8Q00Y9RNQ REQUSDR SWAA2025022588170Seat Track · corrodedCORROSION ON LBL 24 SEAT TRACK WELL AT STA 500B+18; WL 208.1. <[01] DISCREPANCY RECORD ON CCN TTG8Q00Y9RP3 REQUIRED REMOVED AND REPLACED THEREFORE CARD TO BE CLOSED AND ALL WORK DONE WAS RECORDED ON TTG8Q00Y9RP3; [02] DISCREPANCY RECORD ON CCN TTG8Q00Y9RP3 REQSDR SWAA2025022488151Strap · corrodedCORROSION ON AFT CARGO BAY FLOOR T STRAP BS 727D+5 RBL 9 TO RBL 18 WL 156<[01] CORRECTION TO DISCREPANCY; SHOULD READ; CORROSION ON AFT CARGO BAY FLOOR T STRAP BS 727D+5 RBL 9 TO RBL 18 WL 156;[02] EVALUATED CORROSION FOUND TO BE OUT OF LIMITS; RECEIVED NEW STSDR SWAA2025022488150Strap · corrodedCORROSION ON AFT CARGO BAY FLOOR T STRAP BS 767+5 RBL 12 - TO RBL 19 WL 156<[01] EVALUATED CORROSION FOUND TO BE OUT OF LIMITS; RECEIVED NEW STRAP AND PAINTED WHITE ALL PER SRM 51-10-02; MM 51-21-73-370-804 AND ACO 5360-E-16462;[02] VERIFIED CORRECTIVE ACTION SDR SWAA2025022488537Attach Angle · corrodedCORROSION AFT CARGO BAY ATTACH ANGLE UNDER SHIELD HAS MULTIPLE AREAS UNDER NUT PLATES BS767 TO BS787 RBL21 WL156<[01] CORROSION ON AFT CARGO BAY ATTACH ANGLE UNDER SHIELD BS 767 TO 787 RBL 21 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SDR SWAA2025022488538Shield · corrodedCORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] CORROSION ON AFT CARGO BAY FWD SHIELD; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. REMOVED; REPLACED AND INSTALLED AFT CARGOSDR SWAA2025022488148Support Plate · corrodedCORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156<[01] CORROSION ON AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE; FOUND TO BE OUT LIMITS. REMOVE AND REPLACE L/H FLOOR TO SIDEWALL SDR SWAA2025022488149Support · corrodedCORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] DAMAGED ON R/H FLOOR TO SIDEWALL SUPPORT PLATE; FOUND TO BE OUT OF LIMITS. REMOVED; REPLACED AND INSTALLED NEW FLOOR TO SIDEWSDR SWAA2025022487908Threshold · crackedAFT CARGO BAY AFT CORNER THRESHOLD IS CRACKED <[01]. REPAIRED AFT CARGO BAY AFT CORNER THRESHOLD PER SRM 53-60-15-2R-1.SDR SWAA2025022487909Threshold · crackedAFT CARGO BAY FORWARD CORNER THRESHOLD IS CRACKED <[01]. REPAIRED AFT CARGO BAY FORWARD CORNER THRESHOLD PER SRM 53-60-15-2R-1.SDR SWAA2025022487794Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 242NF DELAMINATED. (CUSTOMER REQUEST)<[01] PASSENGER CABIN FLOOR PANEL 242NF WITH UPPER SKIN DELAMINATIONS 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 SWAA2025022487795Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 242MF DELAMINATED. (CUSTOMER REQUEST)<[01] PASSENGER CABIN FLOOR PANEL 242MF 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 SWAA2025022487797Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 241SF DELAMINATED. (CUSTOMER REQUEST)<[01] PASSENGER CABIN FLOOR PANEL 241SF 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 SWAA2025022487796Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 241RF DELAMINATED. (CUSTOMER REQUEST)<[01] PASSENGER CABIN FLOOR PANEL 241RF; WITH DELAMINATION; WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] JOB COMPLETE.SDR SWAA2025022487793Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 241TF DELAMINATED. (CUSTOMER REQUEST)<[01] PASSENGER CABIN FLOOR PANEL 241TF 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 SWAA2025022487628Floor Panel · delaminatedMAIN CABIN; FLOOR PANEL 241AAF TOP LAYER FIBER GLASS EXPOSED.<[01] 241AAF; WITH UPPER SURFACE DAMAGE; WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHESDR SWAA2025022586847Former · crackedWING TO BODY FAIRING FORMER IS CRACKED BS 500D BETWEEN STRINGER 19 AND 20 L/H <[01]. REMOVED DAMAGED FAIRING FORMER AND INSTALLED NEW FAIRING FORMER BS 500D BETWEEN STRINGER 19 AND 20 L/H IAW SRM 51-40-02-0G-0 AND DWG 116A3110 REV:- AND 116A3010 REV:-.; [02] VSDR SWAA2025022487207Stiffener · crackedSTIFFENER CRACKED AT BS 250 LBL 4 WL 208 <[01]. REMOVE AND REPLACED STIFFENER AT BS 250 LBL 4 WL 208 I.A.W SRM 51-10-02-0G-0; SRM 51-40-02-0G-0 AND BOEING DWG 141A5100 REV:SDR SWAA2025022586760Panel · crackedCRACKED PANEL BREAK BS 540 BL 0 - RBL 25 WL 207 (MARKED) <[01]. REPLACED CRACKED PANEL BREAK WITH NEW AT BS 540 BL 0 - RBL 25 WL 207. REMOVED PART AND FOUND NO ALLOWABLE LIMITS IAW SRM 51-10-02 STEP 9 AND SRM 51-40-02. LOCATED AND DRILLED NEW SERVICEABLE PART SDR SWAA2025022487904Floor Panel · delaminatedPANEL 241BF HAS BUBBLES; DENTS AND FRAYED ON TOP PLY FIBERGLASS (MARKED)<[01] PANEL 241BF WITH BUBBLES (DELAMINATION); DENTS AND FIBERGLASS STRAND FRAYING ON TOP PLY AS MARKED WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO SDR SWAA2025022586303Vapor Barrier · crackedL/H B.S. 663 VAPOR BARRIER IS CRACKED AT MID SPAN <[01]. L/H B.S. 663 VAPOR BARRIER DAMAGE AT MID SPAN HAS BEEN REPAIRED PER [SRM 51-70-04-2R-10-A00755 (REPAIR 10 - REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH IN SOLID LAMINATES - AIRFRAME - PERMANENT)] ATTACSDR SWAA2025022486038Door · corrodedLAV SERVICE DOOR IS CORRODED AT BONDING JUMPER ATTACH POINT <[01]. EVALUATED CORROSION ON LAV SERVICE DOOR; FOUND 0.040 REMOVED FROM ORIGINAL .100 IN A 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 52-40-01-1A-4;[02] REMOVED AND REPLACED DAMAGED LAV SERVICE DSDR SWAA2025022586024Skin · crackedRH WING #5 SLAT FOUND CRACK AT LEADING EDGE NOSE SKIN LOWER SURFACE FASTENER; MARKED <[01]. REPAIRED RH WING #5 SLAT AT LEADING EDGE NOSE SKIN LOWER SURFACE IAW SRM 51-40-02-0G-0 AND SRM 57-42-01-2R-8; REPAIR 8; FIG. 202.; [02] VERIFIED CORRECTIVE ACTION.SDR SWAA2025022586029Slat · crackedLH WING #2 SLAT FOUND CRACK AT LEADING EDGE NOSE SKIN LOWER SURFACE FASTENER; MARKED <[01]. REPAIRED LH WING #2 SLAT AT LEADING EDGE NOSE SKIN LOWER SURFACE IAW SRM 57-42-01-2R-8 REPAIR 8 ALTERNATIVE 1.; [02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2025022586030Slat · crackedLH WING #4 SLAT FOUND CRACK AT LEADING EDGE NOSE SKIN LOWER SURFACE FASTENER; MARKED <[01]. REPAIRED LH WING #4 SLAT AT LEADING EDGE NOSE SKIN LOWER SURFACE IAW SRM 57-42-01-2R-8.; [02] CORRECTED MEASUREMENT TABLE; [03] VERIFIED CORRECTIVE ACTION.SDR SWAA2024110455247Acm · seizedON CLIMB OUT F/A NOTICED SMOKE SMELL. NO SMOKE VISIBLE+ SMELL CLEARED AFTER A MINUTE. RAN PACKS FUL COLD BUT DUCT TEMP NEVER WENT BELOW 80 DEGREES. AFTER LANDING- DUCT TEMP RAN AWAY+RT PAC TRIP OFF LIGHT ILLUM TURNED RT PACK OFF FOR TAXI IN. PACK TRIP LT CLEARSDR SWAA2024091135478Charger · inoperative3 INTERIOR AND 1 EXTERIOR EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED CHARGER ASSEMBLY AND BATTERY PACK FWD OF LH EMERGENCY EXIT DOOR IAW AMM 33-51-06. OPS CHECK GOODSDR SWAA2023110316359Seal · cracked-LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED.<[01] REMOVED AND REPLACED LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM 53-31-31SDR SWAA2023072882803Panel · out of adjustRH WING INBOARD FIXED TRAILING EDGE UPPER PANEL IS OUT OF ADJUSTMENT.<[01] ADJUSTED PANEL REF AMM 57-50-01.;[02] REMOVED INSPECTION REQUIREMENTS. ADJUSTED PANEL REF AMM 57-50-01.
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