N420WN, cancelled Jun 5, 2026
Service difficulty reports · 341
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 = 'N420WN' AND deregistration_id = 'N420WN-2026-06-05' 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 = 'N420WN' AND deregistration_id = 'N420WN-2026-06-05' 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 SWAA2025040721053Web · crackedLEFT # 1 ENGINE INBD T/R FWD FRAME WEB CRACKED AT PLUNGER HOLE<[01] REMOVED AND REPLACED THRUST REVERSER HALF PER AMM 78-31-01. OPS AND LEAK CHECK GOOD REF AMM 78-31-01;[02] INSPECTION C/W REMOVED AND REPLACED THRUST REVERSER HALF PER AMM 78-31-01. OPS AND LEASDR SWAA2025013090970Floor Panel · crackedAFT CARGO COMPARTMENT FLOOR PANEL # 140BF HAS A 20 LONG CRACK.<[01]. REFERENCE: TTG8Q00YDWGQ M-22-125-02598 (CPCP/AD MOC- SWA? 737-700 ? OTHER ? AFT CARGO BILGE AREA RESTORATION AND FLOOR PANEL INSTALLATION);[02] REFERENCE: TTG8Q00YDWGQ M-22-125-02598SDR SWAA2024091135084Bracket · looseFWD GALLEY SERVICE DOOR GIRT BAR BRACKET LOOSE<[01] RESECURED GIRT BAR BRACKET PER SRM 51-40-02SDR SWAA2024072516218Slide · out of positionFWD CABIN DOOR SLIDE LOOSE L1 DOOR<[01] REPOSITIONRD FWD ENTRY SLIDE AS REQUIRED PER MT 725-61-06 AND AMM 25-66-01SDR SWAA2024062705501Retainer · looseFORWARD SERVICE DOOR GIRT BAR RETAINING CLIP LOOSE<[01] SECURED CLIP REF SIPSDR SWAA2024052388655Handle · out of adjustFA REPORTS AFT ENTRY SLIDE PULL HANDLE EXPOSED WHE SLIDE IS ARMED.<[01] RE-INSTALLED THE SLIDE AFT ENTRY; PER AMM 25-66-01. OPS CHECK GOOD.SDR SWAA2024042579190Light · missingEMER EXIT STRIP LIGHTING MISSING F/O SIDE AFT GALLEY TO LAST ROW SEATING<[01] REPLACED MISSING FLOOR PROXIMITY LIGHT STRIP SEGMENT PER AMM 33-51-15 AND DWG #33500007SDR SWAA2024042277390Slide · looseL1 DOOR SLIDE LOOSE.SDR SWAA2024041976940Slide · dislodgedAFT SERVICE DOOR AIRCRAFT RIGHT SLIDE PACK NOT FULLY IN BOX<[01] REPACKED AFT SERVICE DOOR EMERGENCY EVACUATION SLIDE IAW AMM 25-66-06SDR SWAA2024041273998Cover · looseFASTENER LOOSE ON AFT RIGHT SLIDE COVER<[01] SECURED FASTENER IAW SIPSDR SWAA2024041071932Slide · openLEFT FWD ENTRY DOOR SLIDE PARTIALLY OPEN ON ARRIVAL INTO DAL WHEN DOOR OPENED.<[01] REPACKED AND INSTALLED FWD ENTRY ESCAPE SLIDE PER AMM 25-66-01.SDR SWAA2023112925871Pushrod · failedAIRCRAFT RELEASED FOR FUNCTIONAL CHECK FLIGHT DUE TO ADJUSTMENT OF RIGHT HAND ELEVATOR PUSHROD. REF SA-M 192<[01] FCF FAILED REF. SAM 192. SEE LOG PAGE 2143849 FOR PITCH TRIM INFO. REGARDING THIS FCF.SDR SWAA2023112724590Control Unit · stiffDURING CLIMBOUT; F/O NOTICED AIRCRAFT STIFFNESS IN PITCH AXIS. A/P ALSO SLUGGISH IN PITCH AXIS. CAPT LANDED AND CONFIRMED STIFFNESS. NO OVERWEIGHT LANDING INSP REQ. LANDED 900 LBS OVER AND IT WAS A SMOOTH LANDING.<[01] REF NON ROUTINE TTG8Q00PV5V7; TTG8Q00PV5KSDR SWAA2023112725141Switch · stiffDURING CLIMBOUT; F/O NOTICED AIRCRAFT STIFFNESS IN PITCH AXIS. A/P ALSO SLUGGISH IN PITCH AXIS. CAPT LANDED AND CONFIRMED STIFFNESS. NO OVERWEIGHT LANDING INSP REQ. LANDED 900 LBS OVER AND IT WAS A SMOOTH LANDING.<[01] REF NON ROUTINE TTG8Q00PV5V7; TTG8Q00PV5KSDR SWAA2023112725142Bearing · stiffDURING CLIMBOUT; F/O NOTICED AIRCRAFT STIFFNESS IN PITCH AXIS. A/P ALSO SLUGGISH IN PITCH AXIS. CAPT LANDED AND CONFIRMED STIFFNESS. NO OVERWEIGHT LANDING INSP REQ. LANDED 900 LBS OVER AND IT WAS A SMOOTH LANDING.<[01] REF NON ROUTINE TTG8Q00PV5V7; TTG8Q00PV5KSDR SWAA2023111019439Door · deformed-EXTERNAL POWER DOOR DOESNT FIT CONTOUR OF THE PLANE.<[01] REMOVED AND REPLACED EXTERNAL POWER DOOR PER AMM 52-49-02SDR SWAA2023110919448Handle · out of adjustL-2 DOOR SLIDE COVER OVER MANUAL INFLATION HANDLE TUCKED INSIDE OF PACK. / [01] REPOSITIONED L-2 DOOR SLIDE COVER OVER MANUAL INFLATION HANDLE. REF 725-61-06 (REM/INST - SLIDE REMOVAL AND INSTALLATION) [TTG8Q00BEXCZ] FOR WORK PERFORMED.SDR SWAA2023110919447Handle · out of adjustL-1 DOOR SLIDE COVER OVER MANUAL INFLATION HANDLE TUCKED INSIDE OF PACK. / [01] L-1 DOOR SLIDE WAS CHANGED DUE TO SCHEDULED TIME CHANGE. REF 725-61-06-FE [TTG8Q00GQDFQ] FOR WORK PERFORMED.SDR SWAA2023091198766Cover · brokenEMERGENCY LIGHT COVER OVER SEAT 3D BROKEN<[01] RESECURED 3D EMERGENCY LIGHT COVER PER AMM 33-51-03SDR SWAA2023082993907Light · inoperativeLEFT OVERWING ; AFT ENTRY DOOR INDICATOR LIGHTS HAVE FIVE TOTAL INOPERATIVE LAMPS. LEFT OVERWING AFT ENTRY DOOR INDICATOR LIGHTS HAVE FIVE TOTAL INOPERATIVE LAMPS.<[01] RELAMPED LEFT OVERWING AND AFT ENTRY DOOR INDICATOR LIGHTS AND TESTED PER AMM 33-51-01-960-SDR SWAA2023082993906Light · inoperativeFORWARD ENTRY DOOR EMERGENCY AREA LIGHT HAS INOPERATIVE LIGHT.<[01] RELAMPED FORWARD ENTRY DOOR EMERGENCY AREA LIGHT AND TESTED PER AMM 33-51-01-960-801; NO DEFECTS NOTED.;[02] VERIFIED.SDR SWAA2023082993905Light · inoperativeRIGHT OVERWING SLIDE LIGHT DOES NOT ILLUMINATE.<[01] RELAMPED AND TESTED RIGHT OVERWING SLIDE LIGHT PER AMM 33-51-04-960-801; NO DEFECTS NOTED.;[02] VERIFIED.SDR SWAA2023082993904Light · inoperativeEMERGENCY BIN LIGHT AT SEAT 1L DOES NOT ILLUMINATE.<[01] RELAMPED SEAT 1L EMERGENCY BIN LIGHT AND TESTED PER AMM 33-51-03-960-801; NO DEFECTS NOTED.;[02] VERIFIED.SDR SWAA2023082992874Support · crackedBS 540 L/H RAM AIR INLET FAIRING SUPPORT P/N 149A7183-1 IS CRACKED<[01] UPDATED STEP 3. UPDATED MEASUREMENTS TABLE;[02] VERIFIED STEPS 1;2;3; IN PARTIAL OK TO INSTALL GIVEN.;[03] UPDATE STEP 1-2;[04] VERIFIED STEPS 1 IN PARTIAL OK TO INSTALL GIVEN; STEP 2 COMPSDR SWAA2023082992070Panel · elongatedR/W T/E PANEL 651GB 5EA I/B HOLES ARE ELONGATED. (MARKED)<[01] R/W T/E PANEL 651GB I/B AREA WITH 5 ELONGATED HOLES WERE REPAIRED IAW SRM 51-70-04-2R-9.;[02] VERIFIED JOB COMPLETE AND MEASUREMENT TABLE.SDR SWAA2023082490799Floor Panel · pulledPASSENGER FLOOR PANEL 241CF HAS NUMEROUS PULLED FIBER STRANDS.<[01] FABRICATED NEW FLOOR PANEL 241CF IAW SRM 53-00-50-2R-0 AND BDWG 144A5810-12.;[02] DAMAGED FLOOR BOARD WAS REPLACED WITH NEW FABRICATED FROM RAW STOCK IAW SRM 53-00-50-2R-0 AND DRAWING 144A5810SDR SWAA2023082490801Floor Panel · pulledPASSENGER FLOOR PANEL 241AF HAS NUMEROUS PULLED FIBER STRANDS.<[01] FABRICATION OF NEW FLOORBOARD 241AF HAS BEEN COMPLETED IAW SRM 53-00-50-2R-0.<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.;[02] ADDITION TO CORRECTIVE ACTION STEP 1; TO SAY; 'IAW SRM 53-00-50-2R-SDR SWAA2023082490800Floor Panel · pulledPASSENGER FLOOR PANEL 231ZF HAS NUMEROUS PULLED FIBER STRANDS.<[01] FABRICATED NEW FLOOR PANEL 231ZF IAW SRM 53-00-50-2R-0 AND BDWG 144A5810-11.;[02] VERIFIED MEASUREMENT TABLE;[03] DAMAGED FLOOR BOARD WAS REPLACED WITH NEW FABRICATED FROM RAW STOCK IAW SRM 53SDR SWAA2023082490802Floor Panel · pulledPASSENGER FLOOR PANEL 232RF HAS NUMEROUS PULLED FIBER STRANDS.<[01] FABRICATED NEW FLOOR PANEL 232RF IAW SRM 53-00-50-2R-0 AND BDWG 144A5810-4.;[02] DAMAGED FLOOR BOARD WAS REPLACED WITH NEW FABRICATED FROM RAW STOCK IAW SRM 53-00-50-2R-0 AND DRAWING 144A5810 SDR SWAA2023082490803Floor Panel · pulledPASSENGER FLOOR PANEL 232SF HAS NUMEROUS PULLED FIBER STRANDS.<[01] FABRICATED NEW FLOOR PANEL 232SF IAW SRM 53-00-50-2R-0 AND BDWG 144A5810-1.;[02] DAMAGED FLOOR BOARD WAS REPLACED WITH NEW FABRICATED FROM RAW STOCK IAW SRM 53-00-50-2R-0 AND DRAWING 144A5810 SDR SWAA2023082988451Retainer · crackedRIGHT WING T/E VERTICAL SEAL RETAINER IS CRACKED AT ORSS 268 JUST ABOVE AFT PYLON FAIRING TIP<[01] REMOVED AND REPLACED RIGHT WING T/E VERTICAL SEAL RETAINER IAW SRM 51-40-02 AND DWG NO. 115A2930;[02] CERTIFIED STEP 1 AND THE MEASUREMENT TABLE;[03] INSPECTED ASDR SWAA2023082988452Retainer · crackedLEFT WING T/E VERTICAL SEAL RETAINER IS CRACKED AT ORSS 268 JUST ABOVE AFT PYLON FAIRING TIP<[01] REMOVED AND REPLACED LEFT WING T/E VERTICAL SEAL RETAINER IAW SRM 51-40-02 AND DWG NO. 115A2930;[02] CERTIFIED STEP 1 AND THE MEASUREMENT TABLE;[03] INSPECTED ANDSDR SWAA2023082488272Skin · corrodedCORROSION ON FUSELAGE CROWN SKIN COMMON TO FASTENER ROWS LOCATED AT: BL 0; STA 1016+7 TO 1016+13; RBL & LBL 9; STA 1016+1 TO 1016+17; AND AT RBL & LBL 12 STA 1016+1 TO 1016+21.<[01] UPDATED STEPS 1-10;[02] UPDATED STEPS 1-10;[03] UPDATED STEP 2 AND 6;[04] ADDESDR SWAA2023082488450Plate · crackedRIGHT WING T/E LOWER WIGGLE PLATE CRACKED AT ORSS 260<[01] REMOVED CRACKED WIGGLE PLATE AT RIGHT WING T/E ORSS 260 AND BEGAN INSTALLATION OF NEW WIGGLE PLATE IAW SRM 51-40-02-0G-0;[02] COMPLETED INSTALLATION OF NEW WIGGLE PLATE; SEALANT AND RESTORATION OF PAINSDR SWAA2023082488449Plate · crackedLEFT WING T/E LOWER WIGGLE PLATE CRACKED AT ORSS 260<[01] REMOVED CRACKED WIGGLE PLATE ON L/W T/E AT ORSS 260 AND TEMPORARILY SECURED NEW WIGGLE PLATE IN PLACE WITH CLECOS IAW SRM 51-40-02-0G-0;[02] CONTINUED INSTALLATION OF NEW WIGGLE PLATE IAW SRM 51-40-02-0SDR SWAA2023082488453Support · crackedLEFT WING T/E PANEL SOPPORT IS CRACKED AT ORSS 278<[01] REMOVED AND REPLACED L/W T/E PANEL SUPPORT BRACKET IAW SRM 51-40-02-0G-0;[02] CERTIFIED STEP 1 AND MEASUREMENT TABLE;[03] VERIFIED MEASUREMENTS TABLE.<BR>VERIFIED CORRECTIVE ACTIONS 1 & 2. CARD COMPLETE.SDR SWAA2023082487783Floor Panel · delaminatedFLOOR PANEL 241SF UPPER SURFACE IS DELAMINATED.<[01] IDENTIFIED FLOOR PANEL 241SF IAW SRM 53-00-50-0I-1 FIG 5 TABLE 5 AND BOEING DWG 146A5810 ID:0102.<BR><BR>FOUND DELAMINATION DAMAGE TO UPPER SURFACE SKIN PLIES TO BE OUT OFF ALLOWABLE DAMAGE LIMITS IAW SRM 53SDR SWAA2023082487777Floor Panel · delaminatedFLOOR PANEL 241RF UPPER SURFACE IS DELAMINATED.<[01] IDENTIFIED FLOOR PANEL 241RF MATERIALS IAW SRM 53-00-50-0I-1 FIG 5 TABLE 5 AND BOEING DWG 146A5810 ID:0011.<BR><BR>FOUND DELAMINATION DAMAGE TO UPPER SURFACE SKIN PLIES TO BE OUT OF ALLOWABLE DAMAGE LIMITS ISDR SWAA2023082487776Seat Track · corrodedCORROSION ON LBL 44 PAX CABIN SEAT TRACK CROWN AT: STA 360+7; 360+10; 360+18 TO 380+4; 400+1 AND WELL AT: 360+9 TO 360+18. WL 208.4<[01] UPDATED STEP 2.;[02] CERTIFIED STEP 2;[03] UPDATED PARTIAL STEP 11 AND 12;[04] CERTIFIED CORRECTIVE ACTION 3;[05] STEP 13 CSDR SWAA2023082487785Seat Track · corrodedCORROSION ON PAX CABIN RBL 44 SEAT TRACK AT STA 578+1 (WELL); 663+17 TO 663+19 (WELL); 706+5 TO 706+8 (CROWN); 727+15 TO 727+17 (CROWN).<[01] VERIFIED APPLICABILITY FOR SRM 53-00-52-1A-1; ALLOWABLE DAMAGE 1.;[02] UPDATED STEP 2.SDR SWAA2023082487787Seat Track · corrodedCORROSION ON PAX CABIN RBL 24 SEAT TRACK WELL AT STA 727E+9; 827+1; 847+14; 867+5; WL 208.3<[01] PARTIAL ON STEPS 2 AND 3.;[02] ADDED TOOL INFORMATION ON STEP 2.;[03] PARTIAL UPDATE ON STEP 4;[04] UPDATED PARTS;[05] REPLACED SEAT TRACK AT STA 727B-887 RBL25 IASDR SWAA2023082487788Seat Track · corrodedCORROSION ON PAX CABIN RBL 44 SEAT TRACK AT: STA 727E+8 TO 727E+11 (CROWN); 827 TO 827+13 (WELL); 847+14 (WELL); 867+5 (CROWN).<[01] VERIFIED APPLICABILITY FOR SRM 53-00-52-1A-1; ALLOWABLE DAMAGE 1;[02] UPDATED STEP 2.;[03] REMOVED SEAT TRACK AT BS 727B-887; RSDR SWAA2023082987764Panel · debondedL/W L/E PANEL 521WB EDGE IS DISBONDED. (MARKED)<[01] REPAIRED L/W L/E PANEL 521WB DISBONED EDGE IAW SRM 51-70-05-2R-6.;[02] FINAL INSPECTION. JOB COMPLETE.SDR SWAA2023082487522Stringer · crackedAREA AFT OF FWD CARGO BAY STR. 25R IS CRACKED AT AFT FASTENER; BS 520+18<[01] UPDATED STEPS 1 TO 4.;[02] UPDATED STEP 5.;[03] UPDATED STEP 6.;[04] UPDATED STEP 7.;[05] PARTIAL UPDATE STEP 8;[06] PARTIAL UPDATE STEP 12;[07] STEP 11 COMPLETE; STEP 12 IN PARTIAL.SDR SWAA2023082487520Stiffener · crackedLEFT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 120.30; 4TH VERTICAL STIFFENER IS CRACKED.<[01] REMOVED PANEL 333CB FOR ACCESS IAW SOPM 20-50-01.;[02] REMOVED BALANCE BAY #2 ELEVATOR HINGE HALF IAW AMM 27-31-41-000-8012. F. (2).;[03] VALIDATESDR SWAA2023082487755Skin · crackedSTABILIZERS - LH HORIZONTAL STABILIZER LOWER SKIN - .4' CRACK FOUND TO BE AT RIB STA 184.70 AND 26' FROM FWD EDGE.<[01] UPDATED STEP 2-3;[02] UPDATED STEP 4. REPAIRED PER EA 23-155-02502 WITH REPETITIVE INSPECTION PROGRAM DEFINED IN EA 23-155-02502.SDR SWAA2023082487756Skin · crackedSTABILIZERS - LH HORIZONTAL STABILIZER LOWER SKIN - .4' CRACK FOUND TO BE AT RIB STA 193.90 AND 10' FROM FWD EDGE.<[01] UPDATED STEPS 3-4;[02] UPDATED STEPS 5-6;[03] UPDATED STEP 9.;[04] UPDATED STEP 9.;[05] VERIFIED STEP 9 COMPLETE.;[06] VERIFIED STEP 9 COMPLSDR SWAA2023082487750Panel · crackedAREA ABOVE WING BOX CENTER SECTION HAS A CRACKED BREAK PANEL I/B OF FASTENER; BS 540; RBL 1; WL 207<[01] UPDATED MEASUREMENT TABLE.;[02] COMPLETED STEPS 1 AND 2. PARTIAL UPDATED STEP 3.;[03] CONMPLETED STEP 3.;[04] REPLACED PANEL BREAK AT BS 540 RBL 1 PER SRM SDR SWAA2023082487751Panel · crackedAREA ABOVE WING BOX CENTER SECTION HAS A CRACKED BREAK PANEL I/B OF FASTENER; BS 540; LBL 1; WL 207<[01] COMPLETED STEPS 1 AND 2; PARTIAL UPDATED STEP 3. UPDATED MEASURENMENT TABLE.;[02] COMPLETED STEP 3.;[03] REPLACED PANEL BREAK AT BS 540 LBL 1 PER SRM 51-40SDR SWAA2023082987056Panel · elongatedWTB FAIRING 193AL HAS SEVERAL ELONGATED FASTENER HOLES<[01] UPDATED STEP 4 AND 5;[02] VERIFIED STEPS 1;2; IN PARTIAL.;[03] VERIFIED STEPS 4;5 COMPLETE.;[04] DUE TO EXTENT OF DAMAGE PANEL WAS REPLACED WITH A SERVICEABLE UNIT IAW SRM 51-10-02-0G-0 PAR 9.;[05] VE
Back to N420WN, cancelled Jun 5, 2026