N922WN

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 = 'N922WN' 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 SWAA2026080368997Battery Pack · no testLEFT EMERGENCY EXIT EMERGENCY LIGHT BATTERY PACK M1668 FAILED A CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.Jul 29, 2026 · N922WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026080310598Battery Pack · no testFWD LEFT ENTRY EMERGENCY BATTERY PACK M1675 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06 C/W INSPECTION.Jul 29, 2026 · N922WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026080319518Battery Pack · no testROW 20 ABC EMERGENCY BATTERY PACK M1670 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06 INSPECTION VERIFIED CORRECTIVE ACTION TAKEN IN STEP 1.Jul 29, 2026 · N922WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026061611648Girt Bar · out of adjustAFT SERVICE DOOR HAS A DAMAGED EVAC RELEASE STOP ON THE GIRT BAR. REMOVED AND REPLACED RELEASE STOP IAW AMM 25-66-00.Jun 12, 2026 · N922WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2026022372380Lamp · inoperativeLEFT OVERWING EXIT LIGHT IS HAS A BULB OUT. REMOVED AND REPLACED BOTTOM MOST LAMP IN THE LT OVERWING EXIT SIGN JUST FORWARD OF LT OVERWING EXIT AND PERFORMED SATISFACTORY OPERATIONAL TEST IAW AMM 33-51-01-960-801.Feb 20, 2026 · N922WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026022368081Scuff Plate · crackedAFT ENTRY DOOR LOWER CENTER SCUFF PLATE CRACKED. REMOVED ALL THE COATINGS AND OTHER UNWANTED MATERIALS FROM THE SCUFF PLATE BEFORE WELDING IAW SRM 53-10-15-2R-2 STEP 4.B.(3). REFERRED TO SOPM 20-30-03. REPAIRED BY FUSION WELD PROCESS THE SCUFF PLATE IAW SRM 5Feb 5, 2026 · N922WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026022368082Scuff Plate · crackedFWD GALLEY DOOR LOWER CENTER SCUFF PLATE CRACKED. REMOVED ALL THE COATINGS AND OTHER UNWANTED MATERIALS FROM THE SCUFF PLATE BEFORE WELDING IAW SRM 53-10-15-2R-2, STEP 4.B.(3). REFERRED TO SOPM 20-30-03. REPAIRED BY FUSION WELD PROCESS THE SCUFF PLATE IAW SRMFeb 5, 2026 · N922WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026022466142Skin · debondedLEFT WING OTBD AFT FLAP INBD AFT CORNER DISBONDED. REMOVED AND REPLACED THE LT WING OTBD AFT FLAP INBD IAW AMM 27-51-22-401.Jan 30, 2026 · N922WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2026022465349Retainer · crackedRIGHT WING AFT BULB SEAL RETAINER IS CRACKED AT THE TRANSVERSE WEB. REMOVED AND REPLACED THE AFT BULB SEAL RETAINER IAW SRM 51-40-02-OG-O.Jan 28, 2026 · N922WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2026022465014Stringer Clip · crackedCRACKED STRINGER CLIP, BS 727B, S9L. ACCOMPLISHED HFEC SURFACE SCAN OF THE STRINGER CLIP IAW NDTM, PART 6, CHAPTER 51-00-00, PROCEDURE 23. VERIFIED THE CRACK. REMOVED BS 727B; S-9L STRINGER CLIP IAW SRM 51-40-02, LOCATED AND DRILLED NEW STRINGER CLIP PER SRJan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026022465018Stringer Clip · crackedCRACKED STRINGER CLIP, BS 727C, S7L. ACCOMPLISHED HFEC SURFACE SCAN OF STRINGER CLIP AREA IAW NDTM, PART 6, CHAPTER 51-00-00, PROCEDURE 23. VERIFIED CRACKED. REMOVED BS 727C; S-7L STRINGER CLIP PER SRM 51-40-02. LOCATED AND DRILLED NEW STRINGER CLIP PER SJan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026022465019Stringer Clip · crackedCRACKED STRINGER CLIP, BS 727D, S7R. FABRICATED A NEW STRINGER CLIP IAW SRM 51-30-01 & DWG 143A1010-1 REV C. .APPLIED CHEMICAL CONVERSION COATING AND PRIMED IAW AMM 51-21-41-370-802, & AMM 51-21-72-370-804. REMOVED THE STRINGER CLIP IAW SRM 51-40-02. INSJan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026022465011Stringer Clip · crackedCRACKED STRINGER CLIP, BS 727C, S6L. ACCOMPLISH HFEC INSPECTION OF THE STRINGER CLIP AREA IAW NDTM, PART 6, CHAPTER 51-00-00, PROCEDURE 23. REMOVED THE BS 727C; STRINGER CLIP 6L IAW SRM 51-40-02, FABRICATED A NEW STRINGER CLIP IAW SRM 51-30-01, & DWG 143Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026022465020Stringer Clip · crackedCRACKED STRINGER CLIP, BS 727E, S5R, HFEC INSPECTED AREA IAW NDTM, PART 6; 51-00-00, PROCEDURE 23. CRACK NOTED. REMOVED THE STRINGER CLIP IAW SRM 51-40-02, LOCATED & DRILLED A NEW STRINGER CLIP IAW SRM 51-40-05, & DWG 146A1112, REV-. FABRICATED A NEW STJan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026022465021Stringer Clip · no discrepancyCRACKED STRINGER CLIP, BS 767, S7R. HFEC INSPECTED AREA IAW NDTM PART 6, 51-00-00, PROCEDURE 23. NO CRACKS NOTED.Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026022464680Former · crackedLEFT WING TO BODY FAIRING FORMER CRACKED, BS 500D BETWEEN STRINGER 19L & 20L. EVALUATED CRACK ON THE WING TO BODY FAIRING, FOUND TO BE OUT LIMITS AND WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02 PAR 9. REMOVED AND REPLACED THE WING TO BODY FAIRING FORMEJan 27, 2026 · N922WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2026022364652Floor Panel · pulledAFT FLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPLACEMENT AFT FLOOR PANEL 241UF WAS FABRICATED IAW SRM 53-00-50-2R-0.Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022364683Floor Panel · pulledAFT FLOOR PANEL 241XF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241XF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022364653Floor Panel · pulledAFT FLOOR PANEL 241YF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241YF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022364687Floor Panel · pulledAFT FLOOR PANEL 242TF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 242TF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022364657Floor Panel · pulledAFT FLOOR PANEL 242UF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 242UF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022364658Floor Panel · pulledAFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED UPPER SKIN PULLED STRANDS IAW SRM 53-00-50-2R-1-A00939, REPAIR 1.Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022364646Floor Panel · pulledFWD FLOOR PANEL 221BF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO EXTENT OF DAMAGE THE FLOOR PANEL 221BF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022364648Floor Panel · pulledFWD FLOOR PANEL 221DF UPPER SKIN HAS AREAS OF PULLED STRANDS. FWD FLOOR PANEL 221DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022364650Floor Panel · pulledFWD FLOOR PANEL 222BF UPPER SKIN HAS AREAS OF PULLED STRANDS. FWD FLOOR PANEL 222BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022364651Floor Panel · pulledFWD FLOOR PANEL 222CF UPPER SKIN HAS AREAS OF PULLED STRANDS. FWD FLOOR PANEL 222CF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022364656Floor Panel · pulledAFT FLOOR PANEL 241ACF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241ACF WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022365017Stringer Clip · crackedCRACKED STRINGER CLIP AT BS 727B, S5R. ACCOMPLISH HFEC INSPECTION ON THE STRINGER CLIP IAW NDTM, PART 6, CHAPTER 51-00-00 PROCEDURE 23. LOCATED AND DRILLED A NEW STRINGER CLIP IAW SRM 51-40-05, AND DWG 146A1102 REV-. FABRICATED A NEW STRINGER CLIP IAW SRJan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026022464636Floor Support · crackedCRACKED FLOOR SUPPORT, BS 380-400, LBL 1, WL 208. REMOVED, LOCATED, DRILLED, AND INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 143A5400, REV A.Jan 26, 2026 · N922WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026022464523Seat Track · corrodedFOUND CORROSION ON TOP & IN WELL OF PASSENGER CABIN SEAT TRACK LBL 45, BS 727C+13 - 787+6, BS 807+6, BS 847+7, BS 847+8, WL 208. REMOVED THE DAMAGED SEAT TRACK AND REPLACED WITH NEW IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, & DWG 146A5300, REV-.Jan 26, 2026 · N922WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026022464628Skin · crackedPOSSIBLE CRACK ON NR 4 SLAT NOSE SKIN AT ACTUATOR ATTACH FITTING. REPAIRED THE NR 4 SLAT NOSE SKIN IAW SRM 57-42-01-2R-8.Jan 26, 2026 · N922WN · Boeing 7377H4 · Leading Edge DevicesSDR SWAA2026022364644Floorbeam · corrodedCORROSION AROUND FASTENER HOLE AT BS 986, LBL 47, WL 208. REMOVED AND REPAIRED THE DAMAGE OF THE FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6, ALTERNATIVE 4.Jan 26, 2026 · N922WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2026022364679Support · corrodedCORROSION AROUND FASTENER HOLE, BS 986, RBL 47, WL 208. OPEN HOLE EXIST C/T INTERCOSTAL AND FLOOR PANEL SUPPORT AT BS 986 - 1006, WL 208 - WL 202 RBL38. REMOVE DAMAGED REPLACEMENT TEE ANGLE AND INSTALLED NEW REPLACEMENT -1 REPAIR IAW SRM 51-40-02-0G-0, SRM Jan 26, 2026 · N922WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026022364635Floor Support · crackedCRACKED FLOOR SUPPORT BS 380 - 400, RBL 39, WL 208. REMOVED, LOCATED, DRILLED, AND INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 143A5400, REV A.Jan 26, 2026 · N922WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026022364666Floor Support · crackedCRACKED FLOOR SUPPORT BS 380 - 400, RBL 8, WL 208. REMOVED, LOCATED, DRILLED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 143A5400, REV A.Jan 26, 2026 · N922WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026022364677Shield · corrodedCORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS 767+3 - 794, RBL 22, WL 156. REMOVED AND REPLACED AFT CARGO BAY FWD SHIELD BETWEEN BS 767 - 794, RBL 22, WL 156 IAW SRM 51-40-02, & DWG 146A0081, REV-.Jan 26, 2026 · N922WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026022364642Support · corrodedCORROSION AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS 727B - 767, LBL 22, WL156. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT BETWEEN BS 727+4 - 847, LBL 22, WL 156 IAW SRM 51-40-02, & DWG 146A7500, REV-.Jan 26, 2026 · N922WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026022364643Support · corrodedCORROSION AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS 727B - 767, RBL 22, WL 156. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT ACB BETWEEN BS 727+4 - 767, RBL 22, WL156 IAW SRM 51-40-02, DWG 146A7500, REVJan 26, 2026 · N922WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026022364634Floor Support · crackedCRACKED FLOOR SUPPORT BS 277 - 294, BL 0, WL 208. REMOVED, LOCATED, DRILLED, AND INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 141A5400, REV -.Jan 26, 2026 · N922WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026022364418Crossbeam · crackedCRACKED CROSSBEAM, PASSENGER CABIN, BS 540, LBL 2, WL 208. REMOVED AND REPLACED THE CROSSBEAM, BS 540, LBL 0.0 TO LBL 24.75 IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, AND DWG 143A0060, REV B;Jan 25, 2026 · N922WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026022364419Crossbeam · crackedCRACKED CROSSBEAM AT PASSENGER CABIN, BS 540; LBL 44, WL 208. REMOVED AND REPLACED CROSSBEAM, BS 540 LBL 24.75 - LBL 45.5 IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, AND DWG 143A0060, REV B.Jan 25, 2026 · N922WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026022364092Floor Panel · pulledCABIN FLOOR PANEL 231YF HAS PULLED STRANDS. FABRICATED A NEW 231YF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.Jan 23, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022364090Floor Panel · pulledCABIN FLOOR PANEL 231ZF HAS PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, DUE TO THE EXTENT OF ALL OF THE DAMAGE.Jan 23, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022364094Floor Panel · pulledCABIN FLOOR PANEL 241AF HAS PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.Jan 23, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022364095Floor Panel · pulledCABIN FLOOR PANEL 241BF HAS PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, AND DWG:144A5810 DUE TO AMOUNT OF ALL DAMAGE.Jan 23, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022364096Floor Panel · pulledCABIN FLOOR PANEL 242AF HAS PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.Jan 23, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022364098Floor Panel · pulledCABIN FLOOR PANEL 241DF HAS PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.Jan 23, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022364099Floor Panel · pulledCABIN FLOOR PANEL 241EF HAS PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, AND BDWG:144A5810, DUE TO AMOUNT OF ALL DAMAGE.Jan 23, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022364097Floor Panel · pulledCABIN FLOOR PANEL 242CF HAS PULLED STRANDS. THE FLOOR PANEL 242CF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0, & DWG 144A5810 ID:0125.Jan 23, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022364100Floor Panel · pulledCABIN FLOOR PANEL 242DF HAS PULLED STRANDS. THE FLOOR SUPPORT REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0, & DWG 144A5810 ID:0123.Jan 23, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor Panel
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