N953WN

Service difficulty reports · 221

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 = 'N953WN' 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.

SDR SWAA2026082402079Isolator · crackedAFT ENTRY DOOR UPPER FWD SLIDE MOUNT ISOLATOR CRACKED. R & R AFT ENTRY DOOR UPPER FWD SLIDE MOUNT ISOLATOR IAW SRM 51-40-02.Aug 19, 2026 · N953WN · Boeing 7377H4 · Escape SlideSDR SWAA2026082449279Isolator · crackedFWD SERVICE DOOR FWD LOWER SLIDE ISOLATOR IS CRACKED. R & R FWD SERVICE DOOR FWD LOWER SLIDE ISOLATOR IAW SRM 51-40-02.Aug 19, 2026 · N953WN · Boeing 7377H4 · Escape SlideSDR SWAA2026080470737Light · inoperativeTHE R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT IS INOPERATIVE. REPLACED THE R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT AND PERFORMED TEST IAW AMM 33-51-04-960-801. TESTED OK. TASK CARD COMPLETE.Aug 1, 2026 · N953WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026080565018Support · crackedCRACKED SUPPORT ZEE, BS 887 - 907, RBL 21 IN THE AFT CARGO BAY. REPLACED THE SUPPORT ZEE AND FASTENERS IAW SRM 51-40-02, & DWG 147A7500, SHEET 37, REV-.Jul 17, 2026 · N953WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026080527935Web · corrodedCORRODED SHIELD WEB, BS 767 - 794.3, WL 156, RBL 22 IN THE AFT CARGO BAY. REPLACED THE SHIELD WEB IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02, AND DWG 146A0081, SHEET 43, REV -.Jul 17, 2026 · N953WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026080568771Stringer Clip · corrodedCORRODED STRINGER CLIP BS 787, STR 26R, WL 152 IN THE AFT CARGO BAY. REPLACED THE STRINGER CLIP IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, AND DWG 146A1262, SHT 116, REV- .Jul 17, 2026 · N953WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026080501765Support · corrodedCORRODED SUPPORT ZEE, BS 500A - 500D, STR 26R, WL 156.5 IN THE FWD CARGO BAY. REPLACED THE SUPPORT ZEE & FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 143A7500 SHEET: 71 AND REV-.Jul 17, 2026 · N953WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026080541643Support · corrodedCORROSION SUPPORT ZEE BTWN BS 727B - 827, LBL 21, WL 156. ( 10 POINTS ) IN THE AFT CARGO BAY. INSTALLED SUPPORT ZEE AND FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 146A7500, SHT 137, REV-.Jul 17, 2026 · N953WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026080519768Angle · crackedCRACKED ANGLE BTWN BS 907 - 927, S25R - 27R IN THE AFT OF AFT CARGO BAY. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, AND DWG 147A7221, SHEET 28, REV -.Jul 17, 2026 · N953WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026080517633Support · corrodedCORRODED SUPPORT ZEE, BTW BS 727A - 767, RBL 21, WL 156 IN THE AFT CARGO BAY. REPLACED THE SUPPORT ZEE AND FASTENERS IAW SRM 51-40-02-0G-0, DWG 146A7500, SHEET 13, REV-, & DRAWING 146A7500, SHT 174, REV-.Jul 17, 2026 · N953WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026080551868Support Angle · corrodedCORROSION SUPPORT ANGLE, BS 500D, STR 26R - 26L AND WL 156.5 IN THE FWD CARGO BAY. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-10-02, ITEM 9, & DWG 143A7902, SHT 259, REV -.Jul 17, 2026 · N953WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026080501475Web · corrodedCORROSION SHIELD WEB BTWN BS 490 - 500A, STR 26R, WL 156.5 IN THE FWD CARGO BAY. REPLACED SHIELD WEB IAW SRM 51-40-02-0G-0, AND DWG 143A0080, SHT 41, REV-.Jul 17, 2026 · N953WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026080546647Web · corrodedCORRODED SHIELD WEB, BTW BS 847 TO 867, WL156, AND RBL 22 IN THE AFT CARGO BAY. REPLACED THE SHIELD WEB AND FASTENERS IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, AND DRAWING 146A0081, SHEET 43, REV- .Jul 17, 2026 · N953WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026080506407Cargo Track · corrodedCORROSION TRACK RBBL 13.84 BTW STA 787 TO STA 847 AND WL 155 (5 POINTS) AT AFT CARGO COMPARTMENT. REPLACED TRACK AND FASTENERS, RBL 13.84 BTW BS 767 - 887 AND WL 155 AT AFT CARGO BAY IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, AND DRAWING 146A7500, SHJul 17, 2026 · N953WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026080525167Web · corrodedCORROSION WEB BTW BS 747 TO 767, RBL 21, AND WL 156 AT AFT CARGO COMPARTMENT. REPLACED WEB BTW BS 747 TO 767 RBL 21 AND WL 156 AT AFT CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9 AND DWG 146A7502 SHEET: 49 REV -.Jul 17, 2026 · N953WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026080536416Isolation Mount · deterioratedDETERIORATE ISOLATION MOUNTS, UPPER POSITION ON THE RT EMERGENCY EXIT, (2EA). REPLACED THE ISOLATION MOUNTS IAW SRM-51-10-02, ITEM 9, AND DWG:144A8111, SHT 61, REV-.Jul 16, 2026 · N953WN · Boeing 7377H4 · Emergency ExitsSDR SWAA2026080591590Floor Panel · crackedCRACKED FLOOR PANEL 120BF IN THE FWD CARGO BAY. REPLACED FLOOR PANEL 120BF IAW SRM 51-10-02-0G-0, PARA 9, AND DWG 453A1610, SHT 7, REV C.Jul 16, 2026 · N953WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026080550087Isolator · deterioratedDETERIORATED MOUNT ISOLATOR UPPER POSITION AT EMERGENCY EXIT LT SIDE (2EA). REPLACED MOUNT ISOLATOR UPPER POSITION AT EMERGENCY EXIT LT SIDE (2EA) IAW SRM-51-10-02, ITEM 9, AND DWG 144A8111, SHEET 61, REV -.Jul 16, 2026 · N953WN · Boeing 7377H4 · Emergency ExitsSDR SWAA2026080446399Stringer · crackedCRACKED STRINGER 25R, BS 540, FWD CARGO BAY, REPAIRED THE STRINGER 25R, BETWEEN BS 500C - 540 IAW SRM 53-00-03-2R-1, REPAIR 1.Jul 16, 2026 · N953WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2026080585056Access Panel · crackedCRACKED LEADING EDGE RIB, ACCESS PANEL 331B HSS 114.55 LT HORIZONTAL STAB. REPLACED THE LEADING EDGE RIB ACCESS PANEL 331B IAW SRM 51-40-02-0G-0, AND DWG 186A1001, SHT 19, REV-.Jul 15, 2026 · N953WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2026080555591Angle · crackedCRACKED ANGLE, BS 867, S26L, AFT CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02, AND DRAWING 149A8102, REV A, SHT 19.Jul 15, 2026 · N953WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026080502837Crossbeam · crackedCRACKED BRAKE PANEL FLOOR STRUCTURE BS 540 BTW LBL 24.82 TO BL 0. REPLACED THE BRAKE PANEL AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, STEP 9, & DWG 143A0060, SHT 58, REV A.Jul 15, 2026 · N953WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026080558809Crossbeam · crackedCRACKED BRAKE PANEL FLOOR STRUCTURE BS540 AND BTW RBL24.82 TO BL0 AT PASSENGER CABIN. REPLACED BRAKE PANEL FLOOR STRUCTURE BS540 AND BTW RBL24.82 TO BL0 AT PASSENGER CABIN IAW SRM 51-40-02-0G-0 SRM 51-10-02-0G-0 ITEM 9 AND DWG:143A0060 SHEET:64 REV:- .Jul 15, 2026 · N953WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026080553996Frame · crackedCRACKED FRAME, BS 312, S5L & 6L IN THE FWD GALLEY AREA. REPAIRED FRAME IAW M-22-153-01244, SEE TTG8Q01D738K. COMPLETED TASK.Jul 14, 2026 · N953WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2026080502010Web · crackedCRACKED SUPPORT WEB, OTBD FAN COWL UPPER POSITION ON NR 2 ENGINE. REPLACED THE SUPPORT WEB AND FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, & 71-13-30.Jul 14, 2026 · N953WN · Boeing 7377H4 · Nacelle/Pylon Miscellaneous StructureSDR SWAA2026080535641Angle · crackedCRACKED ANGLE BS 400, STR 26L IN THE FWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, AND DWG 143A7505, SHEET 117, REV- .Jul 13, 2026 · N953WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026080527872Glowstrip · deterioratedDETERIORATED PHOTOLUMINESCENT STRIP ALONG PAX CABIN. REPLACED AND PHOTOLUMINESCENT STRIP ALONG PAX CABIN IAW AMM 33-51-15-400-802, STEP 1.E (1) (3) (5), & DWG 33500007, REV 2.Jul 11, 2026 · N953WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026080546983Access Panel · elongatedELONGATED HOLE ON ACCESS PANEL 561BB, LT WING. REPAIRED THE ACCESS PANEL 561BB IAW SRM 51-70-04-2R-9, REPAIR 9.Jul 11, 2026 · N953WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2026080575921Access Panel · damagedELONGATED HOLE ACCESS PANEL 661BB AT RT WING. REPAIRED ACCESS PANEL 661BB AT RT WING IAW SRM 51-70-04-2R-9, REPAIR 9.Jul 11, 2026 · N953WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2026080540700Skin · crackedCRACK LOWER SURFACE OF RT WING LEADING EDGE SLAT 7 NOSE SKIN AT ACTUATOR LOCATION AROUND THE FASTENER. PERFORMED A REPAIR ON LOWER SURFACE OF LEADING EDGE SLAT 7 NOSE SKIN IAW SRM 57-42-01-2R, REPAIR 8, & DWG 114A5020, REV A, SHEET 38.Jul 9, 2026 · N953WN · Boeing 7377H4 · Leading Edge DevicesSDR SWAA2026080580743Skin · crackedCRACKED LOWER SURFACE OF LEADING EDGE SLAT 6 NOSE SKIN AT THE ACTUATOR LOCATION. AROUND FASTENER. PERFORMED A REPAIR ON THE LOWER SURFACE OF LEADING EDGE SLAT 6 NOSE SKIN IAW SRM 51-40-02, AND SRM 57-42-01-2R-8, REPAIR 8, AND DWG 114A5030, REV A, SHEET 2.Jul 9, 2026 · N953WN · Boeing 7377H4 · Leading Edge DevicesSDR SWAA2025121551040Support Fitting · corrodedLEFT MAIN LANDING GEAR FWD TRUNNION SUPPORT FITTING, LOWER INBOARD LUG NR 4. OUTER FACE HAS EVIDENCE OF CORROSION. R & R LT MLG FWD TRUNNION SUPPORT FITTING; LOWER INBD LUG NR 4 PER EA. 1-A57-3246.Dec 9, 2025 · N953WN · Boeing 7377H4 · Wing, Landing Gear Attach FittingsSDR SWAA2025111734914Seal · crackedR/H HORIZONTAL UPPER SLIDER IS CRACKED. R & R STABILIZER-TO-BODY FRONT SPAR UPPER SLIDING SEAL PER M/M 53-31-31.Nov 14, 2025 · N953WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2025071590692Lens · brokenEXIT LIGHT COVER LENS BY L1 DOOR BROKEN. R&R EXIT LIGHT COVER LENS IAW AMM 33-51-02Jul 12, 2025 · N953WN · Boeing 7377H4 · Emergency LightingSDR SWAA2025021294868Slide · dislodgedFWD ENTRY DOOR SLIDE FELL OUT OF SLIDE COMPARTMENT<[01] 01 - REMOVED AND REPLACED PER [AMM 25-66-01-400-804-NG (ESCAPE SLIDE PACK INSTALLATION (UNSCHEDULED) - PERMANENT)]Feb 11, 2025 · N953WN · Boeing 7377H4 · Escape SlideSDR SWAA2025011385281Megaphone · looseAFT MEGAPHONE HANDLE LOOSE.<[01] REMOVED AND REPLACED AFT MEGAPHONE PER AMM25-64-00.Jan 12, 2025 · N953WN · Boeing 7377H4 · Cargo CompartmentsSDR SWAA2024110554600Fairing · crackedTHE #8 FLAP TRACK FWD FAIRING (644AB) HAS A CRACK ON LOWER SURFACE<[01] REPAIRED CRACK ON #8 FWD FAIRING 644AB IAW SRM 51-70-05-2R-2;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. WITH STEPS 1-7Oct 29, 2024 · N953WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2024110550016Stiffener · crackedVERTICAL STIFFENER IS CRACKED BS 663 LBL 26 WL 145<[01] CRACKED STIFFENER FOUND AT BS 663 LBL 26 WL 145; REMOVED AND INSTALLED NEW VERTICAL STIFFENER AT BS 663 LBL 26 WL 145 PER SRM 51-40-02-0G-0 AND DWG 111A1000 REV: A. FASTENERS COMMON TO VAPOR BARRIER WEB WOct 18, 2024 · N953WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024110549346Skate Angle · chafedCHAFED LH CROWN SKATE ANGLE AT BS1058 LBL11. WL308.5.<[01] REPAIRED LH CROWN SKATE ANGLE AT BS1058 LBL11. WL308.5 IAW SRM 53-80-71-2R-6.;[02] VERIFIED CORRECTIVE ACTIONOct 16, 2024 · N953WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2024110548973Rib · crackedR/H HORIZONTAL STABILIZER L/E 341B FIRST I/B RIB IS CRACKED (PANEL MARKED)<[01] REMOVED & REPLACED R/H HORIZONTAL STABILIZER L/E 341B FIRST I/B RIB I.A. W SRM 51-40-02 AND DWG 186A1301 LE STA 78.29;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.Oct 16, 2024 · N953WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2024110548977Attach Bracket · cracked651FB ATTACHING BRACKET (MARKED) IS CRACKED<[01] REMOVED AND REPLACED 651FB ATTACHING BRACKET; PER SRM 51-40-02-0G-0 AND BOEING DWG 115A2710 SHEET 2 REV.B;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETEOct 16, 2024 · N953WN · Boeing 7377H4 · Wing, Attach FittingsSDR SWAA2024110549477Web · crackedLT WING FIXED T/E PANEL LOWER WEB HAS CRACK JUST IB OF DEFLECTION RIB ORSS 279. MARKED<[01] REMOVED; REPLACED; AND INSTALLED A NEW LT WING FIXED T/E PANEL LOWER WEB ORSS 279 IAW SRM 51-40-02 AND BOEING DWG 115A2512 SH 4.;[02] VERIFIED CORRECTIVE ACTION COMPLETOct 16, 2024 · N953WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2024110548945Floor Panel · delaminatedCABIN FLOOR PANEL 241KF TOP SURFACE IS DELAMINATED.<[01] COMPLETE STEP 1;[02] FABRICATED NEW 241KF FLOOR PANEL USING BMS4-17 TY6 LOT # 1569956-1; LIGHTLY SANDED EDGES; LOCATED; DRILLED AND UPSIZED ALL (32EA) THROUGH INSERT LOCATIONS IAW SRM 53-00-50-2R-0 PAR. Oct 15, 2024 · N953WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024110548938Floor Panel · delaminatedCABIN FLOOR PANEL 241AF TOP SURFACE IS DELAMINATED.<[01] COMPLETE STEP 1;[02] FABRICATED NEW 241AF FLOOR PANEL USING BMS4-17 TY6 LOT # 1569956-1; LIGHTLY SANDED EDGES; LOCATED; DRILLED AND UPSIZED ALL (44EA) THROUGH INSERT LOCATIONS IAW SRM 53-00-50-2R-0 PAR. Oct 15, 2024 · N953WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024110548937Floor Panel · delaminatedCABIN FLOOR PANEL 231XF TOP SURFACE IS DELAMINATED.<[01] UPDATED STEP 1;[02] REINSTALLED NEW SERVICEABLE CABIN FLOOR PANEL 231XF PER AMM 53-21-00-400-801;[03] REMOVED & REPLACED NEW SERVICEABLE CABIN FLOOR PANEL 231XF PER AMM 53-21-00-400-801 & AMM 53-21-00-00Oct 15, 2024 · N953WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024110548972Stub Frame · cracked2EA CRACKS ON R1 DOOR STUB FRAME INNER SURFACE; ONE ABOVE SEAL DEPRESSOR BS295+4 WL266 L: 0.8'; ONE EXTENDING FROM AFT EDGE BS295+5 WL266 L: 0.2'<[01] DO NOT INSTALL NEW PART; SEE INCOMPLETE SUB-STEP 4 FOR 'FINISH COAT' APPLICATION.;[02] PARTIAL SUB-STEP 4 VEROct 15, 2024 · N953WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2024110548932Attach Angle · crackedB.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 8 W.L. 164.<[01] REMOVED; REPLACED; AND INSTALLED NEW B.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE PER SRM 51-40-02-0G-0; AND DWG 111A1000 REV:-.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.Oct 15, 2024 · N953WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2024110548943Attach Angle · crackedB.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 28 W.L. 164.<[01] CRACK FOUND TO BE OUT OF LIMITS AS PER SRM 57-10-10-1A-2. PART WILL BE REMOVED AND REPLACED ON FAULT TTG8Q00WF8Z9;[02] VERIFIED CORRECTIVE ACTIONOct 15, 2024 · N953WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2024110548568Skin · debondedPANEL 191D INNER SKIN HAS MULTIPLE DISBONDS. (MARKED)<[01] PANEL 191D WITH MULTIPLE DISBONDS ON INNER SKIN WAS REPAIRED IAW SRM 51-70-05-2R-2.Oct 15, 2024 · N953WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2024110548569Skin · debondedPANEL 191HL OUTER SKIN IS DISBONDED. (MARKED)<[01] DISBOND ON OUTER SKIN OF PANEL 191HL WAS REPAIRED IAW SRM 51-70-05-2R-2.Oct 15, 2024 · N953WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
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