N565WN, cancelled Apr 22, 2026
Service difficulty reports · 264
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 = 'N565WN' AND deregistration_id = 'N565WN-2026-04-22' 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 = 'N565WN' AND deregistration_id = 'N565WN-2026-04-22' 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 SWAA2025122955746Regulator · low pressureAT FL250 CABIN PRESSURE DROPPED TO -4000 PSI; ALT HORN SOUNDED. RAN QRH PRESSURE WAS CONTROLLED IN MANUAL. INSPECTED BOTH CARGO DOOR PRESSURE SEALS IAW MM 52-09-11, NO DEFECTS NOTED. PRESSURIZED ACFT TO 4.5 PSID, NO ABNORMAL LEAKS NOTED IAW MM 21-31-00. ASDR SWAA2025122956227Regulator · low pressureAT FL250 CABIN PRESSURE DROPPED TO -4000 PSI; ALT HORN SOUNDED. RAN QRH PRESSURE WAS CONTROLLED IN MANUAL. INSPECTED BOTH CARGO DOOR PRESSURE SEALS IAW MM 52-09-11, NO DEFECTS NOTED. PRESSURIZED ACFT TO 4.5 PSID, NO ABNORMAL LEAKS NOTED IAW MM 21-31-00. PESDR SWAA2025122956228Valve · low pressureAT FL250 CABIN PRESSURE DROPPED TO -4000 PSI, ALT HORN SOUNDED. RAN QRH PRESSURE WAS CONTROLLED IN MANUAL. INSPECTED BOTH CARGO DOOR PRESSURE SEALS IAW MM 52-09-11, NO DEFECTS NOTED. PRESSURIZED ACFT TO 4.5 PSID, NO ABNORMAL LEAKS NOTED IAW MM 21-31-00. SDR SWAA2025122956229Valve · low pressureAT FL250 CABIN PRESSURE DROPPED TO -4000 PSI; ALT HORN SOUNDED. RAN QRH PRESSURE WAS CONTROLLED IN MANUAL. INSPECTED BOTH CARGO DOOR PRESSURE SEALS IAW MM 52-09-11 NO DEFECTS NOTED. PRESSURIZED AIRCRAFT TO 4.5 PSID NO ABNORMAL LEAKS NOTED IAW MM 21-31-00. PSDR SWAA2025121651775Screw · missingLEFT OVERWING EMERGENCY EXIT DOOR HANDLE HOUSING MISSING SCREW LEFT OVERWING EMERGENCY EXIT DOOR HANDLE HOUSING MISSING SCREW. REPLACED LT OVERWING EMERGENCY EXIT DOOR HANDLE HOUSING SCREW IAW AMM 12-25-22.SDR SWAA2025090912957Fseu · faultedTRAILING EDGE FLAPS INOPERATIVE. FIM 27-59 TASK 808 CARRIED OUT. OHMED FOR CONTINUITY, SHORTS, INSULATION RESISTANCE & DAR TEST IAW WDM 27-53-21. NO FINDINGS. REPLACED FSEU IAW AMM 27-51-01. OPS CHECKED GOOD.SDR SWAA2025090210292Sensor · faultedAFTER PUTTING FLAP LEVER TO 5 THE FLAPS DID NOT EXTEND. WE NOTICED A VERY SMALL SPLIT IN THE TRAILING EDGE FLAPS. LE DEVICES WERE EXTENDED WITH THE ALTERNATE FLAP SWITCH PER QRH. THE LANDING WAS NORMAL AND UNEVENTFUL. R&R #8 FLAP SKEW SENSOR PER AMM 27-59-01.SDR SWAA2025081804438Flap System · faultedAS WE WERE ABOUT TO SELECT FLAPS 1 (210KTS) WE NOTICED THE FLAP GAUGE INDICATING ZERO - ONE ON RT SIDE. WHEN WE SELECTED F1 THE FLAPS/SLATS DID NOT EXTEND. SELECTED F5, SAME RESULT. RETURNED FLAP HANDLE TO ZERO CHECKED CIRCUIT BREAKERS, ALL IN, AND EXECUTSDR SWAA2025062785458Skirt · out of positionAFT ENTRY DOOR SLIDE EXCESSIVE FABRIC<[01] REPOSITIONED AFT ENTRY SKIRT SLIDE PER AMM 25-66-01 AND TASK MT 725-61-06.SDR SWAA2025050667536Sign · inoperativeCREW REPORTS OVER WING EMERGENCY EXIT INDICATOR LIGHT INOP. REMOVED AND REPLACED EXIT INDICATOR SIGN PER AMM 33-51-01.SDR SWAA2025022699482Lens · missingL/H OVER WING EMERGENCY EXIT LIGHT LENS COVER MISSING<[01] INSTALLED L/H OVER WING EMERGENCY EXIT LUGHT LENS COVER PER SIPSDR SWAA2025012789283Shroud · misinstalledFWD ENTRY DOOR SLIDE SHROUD NOT INSTALLED PROPERLY AT BOTTOM CENTER OF SHROUD<[01] INSTALLED CORRECTLY FWD ENTRY DOOR-SLIDE IAW AMM 25-66-01-400-801.;[02] INSTALLED CORRECTLY FWD ENTRY DOOR-SLIDE IAW AMM 25-66-01/401-MT 725-61-06.;[03] VERIFIED CORRECTIVE ACTISDR SWAA2025012788590Light · inoperativeEMERGENCY LIGHT L1065 INOP APROX STA 480 LEFT<[01] RELAMPED EMERGENCY LIGHT L1065 APROX STA 480 LEFT; PERFORMED GOOD TEST PER AMM 33-51-03-960-801;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.SDR SWAA2025012388436Elec Connector · disconnectedEMERGENCY EXIT CEILING LIGHT L1419 INOP.<[01] PERFORMED TROUBLESHOOTING FOUND CONNECTOR D40038J DISCONNECT. RECONNECTED CONNECTOR D40038P FOR THE EMERGENCY LIGHT L1419 PER SWPM 20-63-02. PERFORMED GOOD OPERATIONAL TEST PER AMM 33-51-00-710-801;[02] VERIFIED COSDR SWAA2025012385910Seat Track · crackedPASSENGER CABIN SEAT TRACK AFT FASTENER HEAD HAS A CRACK AT BS 727B; RBL 24.75. (MARKED)<[01] FINISHED PER EA-25-153-00101;[02] VERIFIED CORRECTIVE ACTION COMPLETESDR SWAA2025012884184Track · crackedRT HAND FWD UPPER TRACK ASSY FOR PANEL 343AT CRACKED.<[01] REMOVED AND REPLACED RT HAND FWD UPPER TRACK ASSY FOR PANEL 343AT IAW AMM 27-41-31-400-802.; [02] VERIFIED CORRECTIVE ACTION ENTRY 1.SDR SWAA2025012283949Scuff Plate · crackedFCB FWD CORNER SCUFF PLATE CRACKED<[01] REPAIRED IAW SRM 53-30-15-2R-1; NDI CRACK FREE; FCB FWD CORNER SCUFF PLATE;[02] VERIFIED ALL STEPS; CORRECTION ACTION ITEM 1; MEASUREMENT FIELD COMPLETE; CARD COMPLETE.SDR SWAA2025012283947Scuff Plate · crackedACB AFT CORNER SCUFF PLATE CRACKED<[01] VERIFIEDSDR SWAA2025012283948Scuff Plate · crackedACB FWD CORNER SCUFF PLATE CRACKED<[01] VERIFIEDSDR SWAA2025012283447Floorbeam · crackedBS540 FLOOR SUPPORT (PANEL BREAK) IS CRACKED RBL1; WL208<[01] REOMOVED AND REPLACED NEW FLOOR SUPPORT (PANEL BREAK) BS540 RBL1 TO RBL24 IAW SRM 51-40-02 AND DWG 143A0060 ID:0002 REV: B;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2025012283452Floorbeam · crackedBS540 FLOOR SUPPORT (PANEL BREAK) IS CRACKED LBL1; WL208<[01] REMOVED AND REPLACED FLOOR SUPPORT (PANEL BREAK) BS540 LBL1 TO LBL24 IAW SRM 51-40-02 AND DWG 143A0060 ID:0002 REV: B<BR>INSTALLED PANEL 231UF IAW AMM 53-21-00-400-801;[02] CORRECTIVE ACTION COMPLETSDR SWAA2025012083130Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 231XF HAS AREAS OF PULLED STRANDS<[01] PASSENGER CABIN FLOOR PANEL 231XF WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0; DWG 144A5810 ID:0007.;[02] VERSDR SWAA2025012083131Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 231YF HAS AREAS OF PULLED STRANDS<[01] PASSENGER CABIN FLOOR PANEL 231YF WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0; DWG 144A5810 ID:0017.;[02] VERSDR SWAA2025012083128Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 231ZF HAS AREAS OF PULLED STRANDS<[01] PASSENGER CABIN FLOOR PANEL 231ZF WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0; DWG 144A5810 ID:0020.;[02] VERSDR SWAA2025012083132Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 241BF HAS AREAS OF PULLED STRANDS<[01] PASSENGER CABIN FLOOR PANEL 241BF WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0; DWG 144A5810 ID:0018.;[02] VERSDR SWAA2025012083133Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 241DF HAS AREAS OF PULLED STRANDS<[01] PASSENGER CABIN FLOOR PANEL 241DF; WITH AREAS OF PULLED STRANDS; WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL; DUE TO THE EXTENT OF ALL OF THE DAMAGE; IAW SRM 53-00-50-2R-0.;[02] WORK COMPLSDR SWAA2025012083129Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 241EF HAS AREAS OF PULLED STRANDS<[01] FOUND DAMAGE TO PANEL 241EF BE BEYOND ECONOMICAL REPAIR; FABRICATED NEW FLOOR PANEL FROM BMS 4-17 TY 6 LOT 1583459-1; INSTALLED INSERTS WITH BMS 5-107 LOT AK4BA2601A/A; CURED INSERTS AND PART MSDR SWAA2025012083134Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 241FF HAS AREAS OF PULLED STRANDS<[01] FOUND DAMAGE TO PANEL 241FF BE BEYOND ECONOMICAL REPAIR; FABRICATED NEW FLOOR PANEL FROM BMS 4-17 TY 6 LOT 1583459-1; INSTALLED INSERTS WITH BMS 5-107 LOT AK4BA2601A/A; CURED INSERTS AND PART MSDR SWAA2024111960573Handle · brokenGRAB ASSIST HANDLE BROKEN FWD ENTRY DOOR<[01] RE SECURED PER SIP NO DEFECTS NOTED.SDR SWAA2024093041679Sign · detachedF/O SIDE EXIT SIGN AT FOOT LEVEL FELL OFF AND COULDNT BE REATTACHED<[01] RE-ATTACHED LIGHT LENS PER AMM 33-51-01SDR SWAA2024071612661Light · missingEMERGENCY EXIT LIGHT COVER MISSING F/O SIDE OVERWING EXIT LOWER LENS<[01] INSTALLED LIGHT COVER F/O SIDE EMERGENCY EXIT LIGHT PER AMM 33-51-04SDR SWAA2024042578757Cover · missingROW 12DEF EMERGENCY EXIT FWD LIGHT ASSY COVER IS MISSING<[01] INSTALLED EMERGENCY LIGHT LENS COVER AT ROW 12 DEF FWD LIGHT ASSY IAW AMM 33-51-01.SDR SWAA2023080284905Connector · faultyFLAP ASYMMETRY DISCOVERED DURING CRUISE BY SPLIT NEEDLES ON FLAP GAUGE. RT FLAP SHOWED FULL UP; LT FLAP WAS BETWEEN UP AND 1. VERIFIED ASYMMETRY BY CONFIGURING EARLY ON ARRIVAL. FLAPS DID NOT MOVE. PERFORMED A TRAILING FLAPS UP LANDING. VREF/VTARGET WAS 170/17SDR SWAA2023080284536Sensor · faultyFLAP ASYMMETRY DISCOVERED DURING CRUISE BY SPLIT NEEDLES ON FLAP GAUGE. RT FLAP SHOWED FULL UP; LT FLAP WAS BETWEEN UP AND 1. VERIFIED ASYMMETRY BY CONFIGURING EARLY ON ARRIVAL. FLAPS DID NOT MOVE. PERFORMED A TRAILING FLAPS UP LANDING. VREF/VTARGET WAS 170/17SDR SWAA2023073183616Sensor · dirtyAT CRUISE NOTICED A SMALL SPLIT ON THE FLAP GAUGE. RIGHT FLAP AT 0 LEFT FLAP AT .2. ON CONFIGURATION FOR LANDING FLAPS 1 SELECTED WITH NO MOVEMENT OF THE FLAPS. LED'S DID NOT MOVE EITHER. SAME WHEN FLAPS 5 WAS SELECTED. QRH WAS RUN WE LANDED WITH FULL LED'S ANSDR SWAA2023072481696Starter · leakingON DECENT #2 ENGINE OIL QTY DROPPED TO 21% ON DECENT #2 ENGINE OIL QTY DROPPED TO 21%.WHEN THRUST LEVER WAS MOVED FORWARD THE QTY DROPPED TO 19% WE KEPT THE #2 THRUST LEVER AT IDLE FOR THE REST OF THE DECENT & APPROACH. THE #2 OIL QTY REACHED 11% ON SHORT FINASDR SWAA2023071478500Sensor · fault messageSELECTED FLAPS 5; ONE FLAP STAYED AT ZERO; OTHER FLAP STOPPED AT LESS THEN 1.<[01] UPDATING PARTS TRANSACTION;[02] PERFORMED PARTS TRANSACTION ONLY;[03] FSEU FAULTED SKEW SENSOR 1. REPLACED SKEW SENSOR 1 REF. AMM 27-59-01. OPS CHECKS GOOD.SDR SWAA2023060556070Transmitter · faultyON APPROACH WITH FLAPS 5 SELECTED FLAPS LOCKED OUT BETWEEN 1 AND UP. SMOOTH NORMAL LANDING.<[01] R&R RH FLAP POSITION TRANSMITTER IAW AMM 27-58-01. OPS CHECK GOOD. NO DEFECTS NOTED.SDR SWAA2023051949416Strip · peelingRUDDER CONDUCTIVE FRAME PREVIOUS REPAIR SPLICE STRIP PEELED BACK; LH SIDE AT TE.<[01] INSTALLED NEW SPLICE STRIP AND VERIFIED CONDUCTIVITY LESS THAN 0.01 OHM IAW SRM 55-40-01-2R-2.;[02] NO CHANGE TO WEIGHT AND BALANCE. NO ADDITIONAL MATERIAL ADDED; MATERIAL INSDR SWAA2023050131165Wire · openMULTIPLE CABIN EMERGENCY LIGHT INOP<[01] FOUND CABIN EMERGENCY LIGHTS INOP AT 6C 8D 9C 12C 13D 18D. R/R POWER SUPPLY AND BATTERY PACK AT 7A ALONG THE SIDEWALL NEAR FLOOR; LIGHTS OPS GOOD AT 6C 8D 9C.<BR>SLAVED IN POWER SUPPLY AND BATTERY PACK AT 11A 12F 17A ALSDR SWAA2023021598916Connector · disconnectedAISLE LIGHT AT STA727E+13 RBL29 AND AFT SERVICE DOOR SLIDE LIGHT DO NOT ILLUMINATE DURING INSTALLATION TEST OF M1672 BATTERY<[01] **FOUND CONNECTOR D11336 DISCONNECTED. CONNECTED D11336 PER SWPM 20-61-28 AND PERFORMED GOOD TEST OF AISLE LIGHT AT 727E+13 RBL29 SDR SWAA2023021697987Floor Panel · damagedNEED TO RELOCATE FLOOR PANEL #241FF INSERT (1 EACH) DUE TO REPAIRED INSTALLED ON THE FLOORBEAM AT BS727+6 LBL 45.57.<[01] FABRICATED NEW FLOOR PANEL 241FF USING BMS 4-17TY6 LOT#1514505-1; INSTALLED ALL INSERTS EXCEPT P12 TO BE RELOCATED USING BMS 5-107 LOT#AK2SDR SWAA2023021598915Wire · pulled1 EACH WIRE IS PULLED OUT OF GROUND BLOCK BEHIND AFT LAV; JUST FWD OF BS 1006 ON L/H SIDEWALL<[01] RETERMINATED WIRE W3142-0451-18 TO GD3778 PER WDM 33-51-14.;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] RETERMINATED WIRE W3142-0451-18 TO GD3778 PER WDM 33-51-SDR SWAA2023021694367Baffle · crackedBAFFLE UNDER L/H FLOOR TO SIDEWALL SUPPORT BS 400-420 LBL 25 IS CRACKED<[01] REMOVED BAFFLE UNDER FLOOR TO SIDEWALL SUPPORT BS 400-420 LBL 25 PER SRM 51-40-02-0G-0.;[02] CRACK BAFFLE UNDER L/H FLOOR TO SIDEWALL SUPPORT BS 400-420 LBL 25 WITH NEXT DIMENSIONS L=SDR SWAA2023021693554Floor Panel · pulledFLOOR PANEL 242DF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] IDENTIFIED PANEL 242DF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 4; TABLE 4; AND DWG DOC: 144A5800 ID: 0004. <BR><BR>PANEL IS BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAR. 4.C. & FSDR SWAA2023021693555Floor Panel · pulledFLOOR PANEL 242CF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] IDENTIFIED PANEL 241CF MATERIAL IAW SRM 53-00-50-0I-1 FIG 4 TABLE 4 AND DWG: 144A5810 ID: 0019.<BR><BR>PANEL IS BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.C AND 4.F.<BR><BSDR SWAA2023021693552Floor Panel · pulledFLOOR PANEL 241FF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] PART/MATERIAL IDENTIFIED PER SRM 53-00-50-0I-1 FIG 4 TABLE 4 LOW TRAFFIC<BR>NUMEROUS PULLED STRANDS DENTS & HEAL STRIKES EXCEEDS ALLOWABLE DAMAGE LIMITS & IS BEYOND ECONOMICAL REPAIR . AS SDR SWAA2023021693547Floor Panel · debondedFLOOR PANEL 232RF UPPER SKIN PREVIOUS REPAIR IS DISBONDED. (MARKED)<[01] IDENTIFIED FLOOR PANEL 232RF MATERIAL IAW SRM 53-00-50-0I-1 FIG 4 TABLE 4<BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARA 4B<BR><BR>DUE TO EXTENT OF DASDR SWAA2023021693546Floor Panel · pulledFLOOR PANEL 231XF UPPER SURFACE HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] IDENTIFIED PANEL 231XF MATERIAL IAW SRM 53-00-50-0I-1 FIG 4 TABLE 4 AND DWG: 144A5810 ID: 0007.<BR><BR>PANEL IS BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.C AND 4.F.<BRSDR SWAA2023021691551Gusset · crackedCRACK ON FWD CARGO BAY GUSSET AT BS 500D STRINGER 19R.<[01] DAMAGE FOUND AT FWD CARGO BAY GUSSET BS 500D STR-19R FOUND TO BE OUT OF LIMIT DUE TO NO LIMTE ON SRM PARTS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR.9C;[02] VERIFIED CORRECTIVE ACTION
Back to N565WN, cancelled Apr 22, 2026