N435WN
Service difficulty reports · 311
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 = 'N435WN' 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 = 'N435WN' 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 SWAA2026101596385Bulb · inoperativeEMERGENCY LIGHT AT SEAT 26ABC WAS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT BULB AT SEAT ROW 26ABC IAW AMM 33-51-03-960-801. OPS CHKD GOOD.SDR SWAA2026080515446Igniter · faultedABORTED NR 2 ENGINE START. IGNITION, RT N1, STALLED AT APPROX 9% TEMP 550. ENGINE STARTED OK WITH START SWITCH IN BOTH, OK TO CONTINUE IAW MEL 74-1-04, SP1. NR 2 ENG POWER SUPPLY CABLES SWAPPED AT IGNITION EXCITERS IAW MEL, R & R LT & RT IGNITER PLUGS ON NSDR SWAA2026072498626Cover · missingEMERGENCY EXIT LIGHT COVER MISSING ROW 14 LEFT SIDE OVER WING REPLACED LENS COVER PER AMM 33-51-01SDR SWAA2026051195709Yaw Damper · faultyAT FL400; CREW NOTED THAT YOKE WAS DISPLAYED TO RIGHT 3 UNITS; CORRECTED USING RUDDER TRIM. APPROX. 1 MINUTE LATER; CREW OBSERVED UNCOMMANDED RUDDER INPUT (SHARP YAW TO THE LEFT.) OCCURRED 3 TIMES. OCCURRED A TOTAL OF 3 TIMES IN FLIGHT.<[01] INTERROGATED #1 SMSDR SWAA2026051197274Sensor · faultyAT FL400; CREW NOTED THAT YOKE WAS DISPLAYED TO RIGHT 3 UNITS; CORRECTED USING RUDDER TRIM. APPROX. 1 MINUTE LATER; CREW OBSERVED UNCOMMANDED RUDDER INPUT (SHARP YAW TO THE LEFT.) OCCURRED 3 TIMES. OCCURRED A TOTAL OF 3 TIMES IN FLIGHT.<[01] INTERROGATED #1 SMSDR SWAA2026051197275Actuator · faultyAT FL400; CREW NOTED THAT YOKE WAS DISPLAYED TO RIGHT 3 UNITS; CORRECTED USING RUDDER TRIM. APPROX. 1 MINUTE LATER; CREW OBSERVED UNCOMMANDED RUDDER INPUT (SHARP YAW TO THE LEFT.) OCCURRED 3 TIMES. OCCURRED A TOTAL OF 3 TIMES IN FLIGHT. INTERROGATED #1 SMYD PSDR SWAA2026051197276Pcu · faultyAT FL400; CREW NOTED THAT YOKE WAS DISPLAYED TO RIGHT 3 UNITS; CORRECTED USING RUDDER TRIM. APPROX. 1 MINUTE LATER; CREW OBSERVED UNCOMMANDED RUDDER INPUT (SHARP YAW TO THE LEFT.) OCCURRED 3 TIMES. OCCURRED A TOTAL OF 3 TIMES IN FLIGHT. INTERROGATED #1 SMYD SDR SWAA2026022372928Skirt · out of positionFA STATES AFT ENTRY DOOR ESCAPE SLIDE SKIRT TOUCHES GROUND. REPOSITIONED SKIRT AT AFT ENTRY ESCAPE SLIDE. NO DEFECTS NOTED IAW MM 25-66-01.SDR SWAA2026021063490Pressure Blkhd · crackedDURING 5311-I-16524-NG (AD - INSP - FUSELAGE - INSPECTION OF BS 1016 AFT PRESSURE BULKHEAD CENTER DOME APEX - GROUP 2; INDICATION OF A CRACK (HFEC) AT BL0 RIGHT LOWER FASTENER. AFTER PAINT REMOVAL USING PART 6 51-00-00 PROCEDURE 23 INDICATION OF CRACK STILL SDR SWAA2025101624872Battery Pack · dischargedAFT GALLEY BOTH RH AND LH BATTERY PACK DEAD. R & R BOTH LT AND RT AFT GALLEY BATTERY PACK AS PER AMM 33-51-06.OPS CHECK GOOD.SDR SWAA2025090510739Lamp · inoperativeLEFT AFT ENTRY EXTERNAL EMERGENCY LIGHT INOP. REMOVED AND REPLACED LEFT AFT ENTRY EXTERNAL EMERGENCY LIGHT LAMP PER AMM 33-51-04. OPS CHECKED GOOD.SDR SWAA2025071188814Light · inoperativeCEILING LIGHTS INOP AT ROWS 2 & 24.SDR SWAA2025062083132Seat Back · out of adjustPASSENGER CABIN SEAT RECLINE IS NOT LOCKED OUT ON SEAT 11F AT R/H OVERWING EMERGENCY EXIT. LOCKED OUT SEAT 11B SEAT ACTUATOR RH EMERGENCY EXIT ROW REF CMM 25-21-42.SDR SWAA2025062382902Cabin Air Sys · odorEXPERIENCED STRONG ELECTRICAL BURNING ODOR UPON LANDING AND TAXIING TO GATE. NO VISIBLE SMOKE. <[01] CW COND. INSP PER AMM 05-51-56. NO ABNORMAL SMELLS NOTED.SDR SWAA2025050566945Fastener · looseAFT ENTRY DOOR EMERGENCY ESCAPE SLIDE BUSTLE ATTACH FASTENER IS LOOSE.<[01] CONFIRMED AFT ENTRY DOOR COVER FASTENERS SECURE PER AMM 20-50-11; AND INSTALLATION CORRECT PER AMM 25-66-01. ACFT OK FOR SERVICE.SDR SWAA2025033109403Battery Pack · inoperativeLIGHTS ASSOCIATED WITH M1674 BATTERY PACK INOP<[01] BATTERY PACK M1674 REPLACED AND RETESTED IAW AMM 33-51-06-960-805; NOT DEFECT NOTED.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.SDR SWAA2025033109401Bulb · inoperativeOVERHEAD EMERGENCY EXIT SIGN AT FWD SERVICE DOOR HAS INOP BULBS<[01] RELAMPED INOP BULBS IN OVERHEAD EMERGENCY EXIT SIGN AT FWD SERVICE DOOR AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-01-960-801.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.SDR SWAA2025033109402Bulb · inoperativeR/H OWE FWD LOCATOR SIGN HAS INOP BULBS<[01] RELAMPED INOP BULBS IN R/H OWE FWD LOCATOR SIGN AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-01-960-801.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.SDR SWAA2025033104830Floor Panel · delaminatedPASS CABIN FLOOR 231XF PREVIOUS REPAIR DELAMINATING<[01] PASS CABIN FLOOR 231XF; WITH PREVIOUS REPAIR DELAMINATION WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0 AND DRAWING 144A5810 ID:0126.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2025033104417Stiffener · corrodedCORROSION ON PRESSURE DECK STIFFENER AT STA 706+8; WL 200; RBL 62.<[01] REMOVAL OF CORROSION ON PRESSURE DECK STIFFENER AT STA 706+8; WL 200; RBL 62 ACCOMPLISHED ON WIP 1; EA 25-153-00668.;[02] REPAIRED PRESSURE DECK STIFFENER AT STA 706+8; WL 200; RBL 62 IAW SDR SWAA2025033104419Stiffener · corrodedCORROSION ON PRESSURE DECK STIFFENER AT STA 685+12; WL 200; RBL 63.<[01] REFER TO FAULT TTG8Q00Z7MFP WHERE EA 25-153-00668 WAS ADDED AS A SUBTASK.;[02] REMOVED CORROSION ON PRESSURE DECK STIFFENER AT STA 685+12; WL 200; RBL 63 REFER TO FAULT TTG8Q00Z7MFP WHERESDR SWAA2025033104418Stiffener · corrodedCORROSION ON PRESSURE DECK STIFFENER AT STA 685+1.5; WL 200; RBL 66.<[01] REFER TO FAULT TTG8Q00Z7MFP WHERE EA 25-153-00668 WAS ADDED AS A SUBTASK.;[02] REPAIRED PRESSURE DECK STIFFENER AT STA 685+1.5; WL 200; RBL 66 IAW EA 25-153-00668. REFERENCE FAULT TTG8Q0SDR SWAA2025033104420Stiffener · corrodedCORROSION ON PRESSURE DECK STIFFENER AT STA 708+2; FROM LBL 62 TO 70; WL 200.<[01] FABRICATED A NEW STIFFENER FROM 7075-T0 0.071' LOT 1523843-1 IAW SRM 51-30-01 AND DWG 144A7713 REV: B. REMOVED AND REPLACED THE CORROEDED STIFFENER ON PRESSURE DECK WITH THE STISDR SWAA2025033104421Stiffener · corrodedCORROSION ON PRESSURE DECK STIFFENER AT STA 706+8; FROM LBL 62 TO 70; WL 200.<[01] FABRICATED A NEW STIFFENER FROM 7075-T0 0.071' LOT 1523843-1 IAWSRM 51-30-01 AND DWG 144A7713 REV: B. REMOVED AND REPLACED THE CORROEDED STIFFENER ON THE PRESSURE DECK AT STA 70SDR SWAA2025033103823Skin · crackedCRACK ON LH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 18' FROM FWD EDGE; .3' IN LENGTH (MARKED)<[01] REPAIRED L/H HORIZONTAL STABILIZER SKIN AT STAB STA 193.9 IAW SRM 55-10-01-2R-11 REPAIR 11; FIG. 204; DETAIL B.;[02] TASK C/WSDR SWAA2025033103168Skin · debondedRIGHT O/B T/E AFT FLAP I/B CORNER LOWER SKIN AND UPPER SKIN HAVE DISBONDS. (MARKED)<[01] REMOVED AND REPLACED RIGHT O/B T/E AFT FLAP PER AMM 27-51-22-401;[02] COMPLETED ALL STEPSSDR SWAA2025033103167Skin · debondedLEFT I/B MAIN FLAP T/E LOWER SKIN IS DISBONDED. (MARKED)<[01] REMOVED AND REPLACED LEFT I/B MAIN FLAP T/E LOWER SKIN PER AMM 20-50-11-910-801 AND SRM 51-40-050G-0 AND BOEING DWG 113A2100 REV.: A.;[02] VERIFIED CORRECTIVE ACTION 1;[03] VERIFIED CARD COMPLETESDR SWAA2024101446860Handle · looseFWD SERVICE DOOR HANDLE CAM PLATE IS LOOSE<[01] SECURED HARDWARE TO FWD SERVICE DOOR HANDLE CAM PLATE IAW AMM 20-50-11.;[02] C/W INSPECTIONSDR SWAA2024080923898Scuff Plate · crackedON CLIMB THROUGH 7000FT ;LOUD CRACK FROM FWD R/H SIDE BEHIND COCKPIT. ON DECENT F/A REPORTED RUSHING AIR SOUND FROM FWD FWD SVC DOOR. A/C HELD PRESSURE. AFTER ARRIVAL FOUND FWD SVC DOOR HANDLE LOOSE<[01] REMOVED DOOR HANDLE TO FOM. IAW AMM 52-41-31;[02] FOUND SDR SWAA2024050281659Bracket · looseF/A REPORTS FWD GIRT BAR BRACKET NEEDS TO BE TIGHTENED.<[01] SECURED FWD ENTRY DOOR GIRT BAR BRACKET IAW AMM 25-66-02. OPS CHECK GOOD.SDR SWAA2023042530501Lens · missingROW 12 ABC EMERG. LT. OVERHEAD LENS MISSING<[01] INSTALLED LENS PER M/M 33-51-03SDR SWAA2023041928506Handle · looseCUSTOMER WALK R-2 AND L-1 DOOR ASSIST HANDLES ARE LOOSE.<[01] ADJUSTED R-2 AND L-1 DOOR ASSIST HANDLES. REF. BOEING 737-700 AMM 52-11-31-400-802.;[02] VERIFIED REPLACEMENTSDR SWAA2023041928505Light · inoperativeCUSTOMER REQUEST. R2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE.<[01] RELAMPED R2 DOOR EXTERIOR EMERGENCY LIGHT AS PER REF B737 AMM 33-51-04-960-801. TEST OK.;[02] VERIFIED REPLACEMENTSDR SWAA2023042028184Bracket · crackedL/H WING DEFLECTION CONTROL PANEL FWD SEAL BRACKET CRACK.<[01] CORRECTION FOR STEP #1 TO READ REMOVED LEFT WING DEFLECTION CONTROL PANEL FORWARD SEAL BRACKET AS PER B 737-700 SRM 51-40-02-0G-0;[02] *** ENTRY 1 WAS ENTERED IN ERROR ***;[03] REMOVED AND REPLACEDSDR SWAA2023042024890Girt Bar · draggingL2 DOOR SLIDE GIRT DRAGGING<[01] REPOSITIONED L2 DOOR SLIDE GIRT PER B737 AMM 25-66-01-400-803-NG;[02] VERIFIED STEP 1SDR SWAA2023042023391Panel · delaminatedPANEL 193AL HAS DELAMINATION AT ONE SIDE<[01] APPLIED THE GLASS FABRIC REPAIR PLIES AT DAMAGED AREA ON ACCESS PANEL 193AL. REF B737 SRM 51-70-04-2R-10 REPAIR 10 PARAGRAPH 4. MATERIAL USED GLASS FABRIC PLIES PO#:1690463 AND RESIN EY3804AB PO#: 1800550.;[02] VERSDR SWAA2023041923389Panel · delaminatedL/T WING I/B LOWER FAIRING ACEESS PANEL # 194CL HAS SEVERALS FASTENER HOLES BULGING/CRACKED<[01] PREPARED PANEL #194CL FOR REPAIR PER B737 SRM 51-70-06-2R-9 PARA 4.D<BR>APPLIED REPAIR IN DAMAGED AREA AT ACEESS PANEL # 194CL AROUND FASTENER HOLES. AS PER REF B7SDR SWAA2023042022885Panel · crackedLEFT WING LOWER MID T/E ACCESS PANEL # 561BB HAS BULGING/CRACKED AROUND FASTENER HOLES<[01] REPAIRED DAMAGED AREA AT LEFT WING LOWER MID T/E ACCESS PANEL # 561BB REF B737 SRM 51-70-04-2R-9-A00753 (REPAIR 9);[02] VERIFIED ALL STEPSSDR SWAA2023042022086Panel · crackedLEFT WING LOWER L/E ACCESS PANEL # 521UB CRACKED/EXPOSED COMPOSITE<[01] REMOVED DAMAGE AREA PANEL 521 UB. AS PER B737 SRM 51-70-06-2R-9 REPARED AREA AND FABRIC REPAIR PANEL 521UB ; AS PER B737 SRM 51-70-06-2R-9 REPAIRED PANEL 521UB; AS PER B737 SRM 51-70-06-2RSDR SWAA2023041920586Panel · elongatedLEFT VERTICAL STABILIZER ACCESS PANEL # 322A HAS 2 EA ELONGATED FASTENER HOLES<[01] RECEIVED; LOCATED AND DRILLED NEW L/E PANEL (322A) AT VERTICAL STABILIZER PER B737-700 PER SRM 51-40-05-0G-0.;[02] VERIFIED ALL STEPSSDR SWAA2023041922885Panel · crackedLEFT WING LOWER MID T/E ACCESS PANEL # 561BB HAS BULGING/CRACKED AROUND FASTENER HOLES<[01] REPAIRED DAMAGED AREA AT LEFT WING LOWER MID T/E ACCESS PANEL # 561BB REF B737 SRM 51-70-04-2R-9-A00753 (REPAIR 9);[02] VERIFIED ALL STEPSSDR SWAA2023041924744Panel · crackedLOWER FUSELAGE CENTER AFT ACCESS PANEL # 194E HAS SEVERAL FASTENER HOLES BULGING/CRACKED<[01] ACCOMPLISHED REPAIR OF PANEL 194E; REF: B737 SRM 51-70-06-2R-9;[02] VERIFIED REPAIRSDR SWAA2023042020454Panel · elongatedR/T HORIZONTAL STAB. UPPER ACCESS PANELN # 343AT HAS 2 EACH RUBBER SEALS WITH ELONGATED HOLES<[01] REMOVED AND REPLACED R/T HORIZONTAL STAB. UPPER ACCESS PANELN # 343AT SEAL AS PER 51-40-02-0G-0.;[02] VERIFIED STEP 1.SDR SWAA2023042020455Panel · elongatedLEFT HORIZONTAL STAB. T/E LOWER ACCESS PANEL # 333AB HAS RUBBER SEAL WITH ELONGATED HOLES<[01] REMOVED AND REPLACED LEFT HORIZONTAL STAB. T/E LOWER ACCESS PANEL # 333AB SEAL AS PER SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1.SDR SWAA2023042018867Angle · crackedR/H VAPOR BARRIER UPPER CHORD SUPPORT ANGLE CRACKED @ APPROXIMATELY RBL-7 STA 663.75 MKD DOT<[01] ACCOMPLISHED WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE REPAIR AT RBL 7 AR PER SRM 57-10-10-2R-5.;[02] VERIFIED ALL STEPS COMPLETEDSDR SWAA2023042018225Channel · corrodedCORROSION FOUND AFT CARGO LH ZEE CHANNEL FROM STA 727 TO STA 807 LBL 21 WL 155.5 HAS SPOTS OF CORROSION.<[01] REMOVED CORROSION AT AFT CARGO LH ZEE CHANNEL FROM STA 727 TO STA 807 AS PER B737-700 SRM 51-10-02-0G-0 FOUND EXFOLIATED CORROSION THROUGH OUT THE THISDR SWAA2023042018226Channel · corrodedCORROSION FOUND AFT CARGO RH ZEE CHANNEL FROM STA 727 TO STA 767 HAS SPOTS OF CORROSION RBL 21 WL 155.5.<[01] REMOVED CORROSION AT AFT CARGO RH ZEE CHANNEL FROM STA 727 TO STA 767 AS PER B737-700 SRM 51-10-02-0G-0 FOUND EXFOLIATED CORROSION THROUGH OUT THE THISDR SWAA2023042017019Bracket · crackedLEFT A/C BAY PNEUMATIC CROSS OVER DUCT MOUNTED ON KEEL BEAM CRACKED AT B.S. 546 LBL. 6'.(51-010) PNEUMATIC DUCT SUPPORT BRACKET CRACKED<[01] REMOVED AND REPLACED LEFT A/C BAY PNEUMATIC CROSS OVER DUCT SUPPORT BRACKET MOUNTED ON KEEL BEAM B.S. 546 LBL. 6' IN RESDR SWAA2023042017319Nut Plate · missingL2 DOOR FWD GIRT BAR FITTING LOWER BRACKET HAS FASTENERS MISSING<[01] REMOVED AND REPLACED MISSING NUT PLATE IN REFERENCE SRM 51-40-02-0G-0.;[02] VERIFIED INSTALLATION;[03] CORRECTION TO FAULT NAME: NUT PLATE MISSING; NOT FASTENERSDR SWAA2023042017018Bracket · crackedRIGHT A/C BAY PNEUMATIC CROSS OVER DUCT SUPPORT BRACKET MOUNTED ON KEEL BEAM CRACKED B.S. 546 RBL. 6'. (51-009)<[01] REMOVED AND REPLACED RIGHT A/C BAY PNEUMATIC CROSS OVER DUCT SUPPORT BRACKET MOUNTED ON KEEL BEAM B.S. 546 RBL. 6' IN REF B737 SRM 51-40-02-0G-
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