N209WN
Service difficulty reports · 296
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 = 'N209WN' 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 = 'N209WN' 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 SWAA2026101975253Battery Pack · no testAFT LEFT EMERGENCY BATTERY PACK M1673 FAILED CAPACITY CHECK. R & R THE BATTERY PACK IAW AMM 33-51-06.SDR SWAA2026101999157Battery Pack · no testAFT RT EMERGENCY BATTERY PACK M1672 FAILED A CAPACITY CHECK. R & R THE BATTERY PACK IAW AMM 33-51-06.SDR SWAA2026101923787Battery Pack · no testRT EMERGENCY EXIT BATTERY PACK M1669 FAILED A CAPACITY CHECK. R & R THE BATTERY PACK PER AMM 33-51-06 INSPECTION VERIFIED CORRECTIVE ACTION TAKEN IN STEP 1.SDR SWAA2026101914969Battery Pack · no testLEFT EMERGENCY EXIT BATTERY PACK M1668 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.SDR SWAA2026092855806Screw · missingSEAT 15F TRAY TABLE INOPERATIVE. INSTALLED MISSING SCREW IAW AMM SIPSDR SWAA2026090384922Sign · missingFWD ENTRY DOOR EMERGENCY EXIT SIGN MISSING. REPLACED THE FWD ENTRY DOOR EMERGENCY LIGHT ASSY IAW.AMM 33-51-04.SDR SWAA2026081016905Lens · missingCOVER FOR EMERGENCY LIGHT NEAR L1 DOOR MISSING. REPLACED MISSING EMERGENCY LENS AT L1 DOOR IAW MM 33-51-01.SDR SWAA2026072039827Sign · out of adjustFWD ENTRY DOOR EXIT SIGN FELL OFF. REINSTALLED FWD ENTRY EXIT SIGN LENS COVER IAW AMM 33-51-01.SDR SWAA2025122654860Seat Back · out of adjustSEAT BACK 11B RECLINES INTO EXIT ROW. ADJUSTED THE SEAT BACK IAW AMM 25-22-00.SDR SWAA2025101524300O-Ring · leakingHYDRAULIC SYSTEM A WENT DOWN TO 58 % IN FLIGHT. LOST 10 % DURING THE LEG. RETURNED TO NORMAL INDICATIONS AFTER LANDING. NOTED FLUID DRIPPING OUT OF HELL HOLE DRAINS AND AREA THICK WITH VAPOR. REPLACED O-RING FROM LEAKING UNION AT ELEVATOR FEEL COMPUTER ASSDR SWAA2025031204529B-Nut · looseEVIDENCE OF HYDRAULIC LEAK IN HELL HOLE <[01]. PERFORMED INSPECTION IN THE HELL HOLE FOUND HYDRAULIC LEAK FROM ELEVATOR FEEL COMPUTER AT B PRESSURE LINE FLARELES TUBING B- NUT WAS LOSE TIGHTENED PER AMM 20-10-51. AND HYDRAULIC LEAK CHECK DONE FOUND OK PER AMMSDR SWAA2025031103592Fitting · crackedLEFT ENGINE NACELLE AFT ATTACH POINT SUPPORT FITTING CRACKED.<[01] REMOVED AFT ATTACH POINT SUPPORT FITTING IAW SRM 51-40-02.;[02] REPLACED LEFT ENGINE AFT FAIRING AFT SUPPORT FITTING PER SRM 51-40-02 REINSTALLED LEFT ENGINE AFT FAIRING ASSEMBLY PER AMM 54-52-SDR SWAA2025021294193Battery Pack · failedEMERGENCY LIGHTS ASSOCIATED WITH M1674 FAIL TO LIGHT UP<[01] REMOVED AND REPLACED BATTERY PACK M1674. PERFORMED GOOD OP CHECK OF EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1674 PER AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2025021294194Battery Cable · failedEMERGENCY LIGHTS ASSOCIATED WITH M1675 FAIL TO LIGHT UP<[01] REMOVED AND REPLACED BATTERY PACK M1675. PERFORMED GOOD OP CHECK FOR LIGHTS ASSOCIATED TO BATTERY PACK M1675. PER AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2025021487993Rib · crackedCRACK ON RT HORIZ. STAB. LEADING EDGE RIB AT L/E STA. 86.66<[01] REMOVED AND REPLACED LE RIB AT L/E STA. 86.66 IAW SRM 51-40-02-0G-0.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2025021487992Rib · crackedCRACK ON RT HORIZ. STAB. LEADING EDGE RIB AT L/E STA. 95.96<[01] REMOVED AND REPLACED RIB AT R/H LE STAB STA 95.96 IAW SRM 51-40-02-0G-0 AND DWG. 186A1001-16.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2025021887822Floor Support · crackedBREAKER PANEL IS CRACKED AT BS 540 LBL 1 WL208 BREAKER PANEL IS CRACKED AT BS 540 RBL1 WL208<[01] REPLACED BREAKER PANEL AT BS 540 RBL1-RBL25 WL208 PER SRM 51-40-02 AND DWG#143A0060 ID:0036 REV:A;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABSDR SWAA2025021887321Stringer Clip · crackedCRACKED STRINGER CLIP S-8L BS 259.5 (MARKED)<[01] REMOVED CRACKED STRINGER CLIP S-8L BS 259.5 AND REPLACED WITH NEW FABRICATED STRINGER CLIP IAW SRM 51-40-02-0G-0.;[02] VERIFIED STEP 2;5 CORRECTION ACTION ITEM 1 MEASUREMENT FIELD COMPLETE; CARD COMPLETESDR SWAA2025021486195Rib · crackedL/H HORIZONTAL STAB #5 INSPAR RIB AT STAB STA 129.50 I/B LOWER FLANGE IS CRACKED AT FWD EDGE<[01] REPAIRED L/H HORIZONTAL STAB #5 INSPAR RIB AT STAB STA 129.50 I/B LOWER FLANGE IAW SRM 55-10-09-2R-5.;[02] VERIFIED CORRECTIVE ACTIONSDR SWAA2025021285467Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 241EF HAS DENTS AND DELAMINATION<[01] PASSENGER CABIN FLOOR PANEL 241EF WITH DENTS AND 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.SDR SWAA2025021085464Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 242AF HAS DELAMINATION<[01] ATTACHED (2EA) PLACARDS TO THE UPPER SURFACE USING BAC27DCA854 LOT # 1591209-1 IAW BOEING DWG: 144A5810 ID: 0189.<BR><BR>242AF FLOOR PANEL DELAMINATION DAMAGE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-1-A009SDR SWAA2025021085465Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 231XF HAS DELAMINATION<[01] PASSENGER CABIN FLOOR PANEL 231XF; WITH DELAMINATION; WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.SDR SWAA2025021085466Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 241DF HAS DELAMINATION<[01] PASSENGER CABIN FLOOR PANEL 241DF WITH DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.SDR SWAA2025021085468Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 241FF HAS DENTS AND DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 241FF WITH DENTS AND DELAMINATED WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.SDR SWAA2025021085469Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 242CF HAS DELAMINATION<[01] PASSENGER CABIN FLOOR PANEL 242CF WITH DELAMINATION WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0.;[02] JOB COMPLETE.SDR SWAA2025021085462Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 242DF HAS DELAMINATION<[01] PASSENGER CABIN FLOOR PANEL 242DF WITH DELAMINATION WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0.;[02] JOB COMPLETE.SDR SWAA2025021785215Scuff Plate · crackedFSD SCUFF PLATE; AFT EDGE IS CRACKED.<[01] REPAIRED FSD SCUFF PLATE PER SRM 53-10-15-2R-1 PARA 4.B.(3)-(6) AND (8). WILL BE REINSTALLED ON TASK TTG8Q003D32V STEP 10;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2025021884802Former · crackedR/H WING TO BODY FAIRING FORMER IS CRACKED BS 500D STRINGER 19 R/H<[01] FAIRING FORMER R/H IS CRACKED AT BS 500D IN L=2' NOT FOUND ALLOWABLE LIMITS ON SRM WILL BE REPAIRED BY REPLACEMENT OF PART PER SRM 51-10-02. PAR 9.;[02] VERIFIED CORRECTIVE ACTION 1;[03] RSDR SWAA2025021484913Skin · crackedCRACK ON RH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 184.70; 26.5' FROM FWD EDGE; 0.9' IN LENGTH (MARKED)<[01] ACCOMPLISHED REPAIR OF CRACK ON RH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 184.70; 26.5' FROM FWD EDGE<BR>PER SWA EA #25-155-00108;[02] VESDR SWAA2025021484804Nut Plate · damagedFWD SERVICE DOOR GIRT BAR FLOOR BRACKET SCREW NUT PLATE IS DAMAGED AT THE FWD SIDE FWD SCREW;<[01] REPLACED FWD SERVICE DOOR FWD GIRT BAR FLOOR BRACKET FWD SCREW NUT PLATE PER DWG#140A1005 ID:1 REV:J;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2025021884799Doubler · crackedEGPR SURROUND DOUBLER IS CRACKED BS233 WL175 8' ABOVE S-24R MARKED<[01] REPAIRED EGPR SURROUND DOUBLER AT BS233 WL175 8' ABOVE S-24R IAW SRM 53-10-15-2R-4 REPAIR 4 PARG 4(A-M) FIG. 204 SHT.(3-4);[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLSDR SWAA2025021784503Panel · debondedPANEL 192E INNER SKIN IS DISBONDED. (MARKED)<[01] PANEL 192E; INNER SKIN WITH DISBOND; WAS REPAIRED IAW SRM 51-70-05-2R-2.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2025021484800Stiffener · crackedLH HORIZONTAL STABILIZER #5 INSPAR RIB; AT STABILIZER STATION 129.50; 2ND VERTICAL STIFFENER IS CRACKED.<[01] REPAIRED LH HORIZONTAL STABILIZER #5 INSPAR RIB; AT STABILIZER STATION 129.50; 2ND VERTICAL STIFFENER IAW SRM 55-10-09-2R-4 REPAIR 4;[02] VERIFIED COMSDR SWAA2025021484801Stiffener · crackedRH HORIZONTAL STABILIZER #9 INSPAR RIB; AT STABILIZER STATION 166.30; 3RD VERTICAL STIFFENER IS CRACKED.<[01] REPAIRED RH HORIZONTAL STABILIZER #9 INSPAR RIB; AT STABILIZER STATION 166.30; 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4 REPAIR 4.;[02] VERIFIED COSDR SWAA2025021084496Sidewall Support · corrodedCORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156<[01] ' THE DAMAGE WAS REPAIRED PER SRM 53-00-53-2R-5 (REPAIR 5) AND EA M-22-153-01550'.;[02] COMPLETESDR SWAA2025021084497Sidewall Support · corrodedCORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] ' THE DAMAGE WAS REPAIRED PER SRM 53-00-53-2R-5 (REPAIR 5) AND EA M-22-153-01550'.;[02] COMPLETESDR SWAA2025021883828Skin · crackedCRACKED LOWER SURFACE OF THE LEADING-EDGE # 3 SLAT NOSE SKIN AT ACTUATOR RIBS - LEFT WING (MARKED)<[01] REPAIRED LOWER SURFACE OF THE LEADING-EDGE # 3 SLAT NOSE SKIN AT ACTUATOR RIBS - LEFT WING IAW SRM 57-42-01-2R-8.SDR SWAA2025021883831Skin · crackedCRACKED LOWER SURFACE OF THE LEADING-EDGE # 5 SLAT NOSE SKIN AT ACTUATOR RIBS - RIGHT WING (MARKED)<[01] REPAIRED LOWER SURFACE OF THE LEADING-EDGE #5 SLAT NOSE SKIN AT ACTUATOR RIBS - RIGHT WING IAW SRM 57-42-01-2R-8.;[02] VERIFIED CORRECTIVE ACTION 1;[03] VESDR SWAA2024071110882Isolation Mount · crackedAFT ENTRY DOOR FWD SLIDE MOUNT ISOLATOR CRACKED<[01] R&R AFT ENTRY DOOR FWD SLIDE MOUNT ISOLATOR IAW SRM 51-40-02.SDR SWAA2024071110875Isolation Mount · crackedFWD GALLEY SERVICE DOOR AFT SLIDE MOUNT ISOLATOR CRACKED<[01] R&R FWD GALLEY SERVICE DOOR AFT SLIDE MOUNT ISOLATOR IAW SRM 51-40-02.SDR SWAA2023062671226Bracket · crackedRIGHT WING UPPER PANEL SUPPORT FWD ATTACH POINT BRACKET IS CRACKED. (Z BRACKET)<[01] REMOVED AND REPLACED RIGHT WING UPPER PANEL SUPPORT FWD ATTACH POINT BRACKET PER SRM 51-40-02.SDR SWAA2023033021358Rib · crackedRIGHT WING UPPER INBOARD FIXED TRAILING EDGE SEAL RIB CRACKED AND BROKEN<[01] REMOVED AND REPLACED RIGHT WING UPPER INBOARD FIXED TRAILING EDGE SEAL RIB PER SRM 51-40-02SDR SWAA2023020698639Light · inoperativeRH INTERIOR EMERGENCY LIGHT INOP AT RH SEAT ROW 18.<[01] FOUND FUSE IN EMERGENCY LIGHT POWER SUPPLY M1672 THAT POWERS AISLE LIGHTS AT ROWS 16ABC AND 18ABC BLOWN. REPLACED FUSE AND LIGHTS WERE STILL INOP AND FOUND THE FUSE BLOWN AGAIN. REMOVED LAMPS FROM THE AFSDR SWAA2023020696817Bulb · inoperativeEMERGENCY EXIT LOCATOR LIGHT OVER FWD L/H DOOR HAS INOP BULBS<[01] RELAMPED AND PERFORMED GOOD INSTALLATION TEST OF FWD L/H DOOR'S EMERGENCY EXIT LOCATOR IAW AMM 33-51-01-960-801.<BR><BR>NO ADDITIONAL FAULTS OBSERVED.;[02] VERIFIED CORRECTIVE ACTION #1.SDR SWAA2023020696814Light · inoperativeEMERGENCY EXIT L/H FWD ENTRY DOOR SLIDE LIGHT INOP EMERGENCY EXIT L/H FWD ENTRY DOOR SLIDE LIGHT INOP (EXTERIOR LIGHT)<[01] RELAMPED AND PERFORMED GOOD INSTALLATION TEST OF L/H FWD DOOR'S EXTERIOR SLIDE LIGHT IAW AMM 33-51-04-960-801.<BR><BR>NO ADDITIONAL FAULSDR SWAA2023020795281Scuff Plate · crackedFORWARD CARGO COMPARTMENT AFT SCUFF PLATE IS CRACKED.<[01] WELDED CRACKED RADIUS OF FWD CARGO BAY AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-30-15-2R-1 PARAGRAPH 4.B. (2) AND (4)<BR>EQUIP USED. WELDING MACHINE E10583 CAL DUE DSDR SWAA2023020792786Intercostal · crackedCRACK ON PASSENGER CABIN FLOOR INTERCOSTAL AT BS 500D+10 BL 0.(MARKED)<[01] DAMAGE FOUND AT PASSENGER CABIN FLOOR INTERCOSTAL UPPER ANGLE FOUND TO BE OUT OFF LIMIT DUE TO NO LIMIT ON SRM PART WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-40-02-0G-0. PAR. 9C;[02] SDR SWAA2023020891365Panel · delaminatedPANEL 561BB DELAMINATED IN SEVERAL LOCATIONS ON OUTER SURFACE<[01] FOUND PANEL TO HAVE AREAS OF DISBOND. THESE AREAS OF DISBOND ARE BEYOND ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1 PARAGRAPH 4.A.(5)(A)<BR><BR>DAMAGED AREAS WILL BE REPAIRED IAW SRM 51-70-05-2R-1 ASDR SWAA2023020890443Support Bracket · crackedLEFT ECS BAY HAS CRACKED DUCT SUPPORT BRACKET (212A1116) ACCESS PANEL 192CL BS540+6 LBL8.<[01] REMOVED LEFT ECS BAY HAS CRACKED DUCT SUPPORT BRACKET BS540+6 LBL8 IAW AMM TASK 20-50-11-910-801.;[02] REPLACED AND INSTALLED NEW DUCT SUPPORT BRACKET (212A1116) ACCSDR SWAA2023020890447Support Bracket · crackedRIGHT ECS BAY HAS CRACKED DUCT SUPPORT BRACKET (212A1116) ACCESS PANEL 192CR BS540+6 RBL8.<[01] REMOVED RIGHT ECS BAY HAS CRACKED DUCT SUPPORT BRACKET BS540+6 RBL8 IAW AMM TASK 20-50-11-910-801.;[02] REPLACED AND INSTALLED NEW DUCT SUPPORT BRACKET (212A1116) A
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