N909WN

Service difficulty reports · 329

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 = 'N909WN' 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 SWAA2025100107662Scuff Plate · crackedFCB FWD CORNER SCUFF PLATE IS CRACKED. WELDED THE FCB FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1594362-1 PER SRM 53-30-15-2R-1 STEP 4.B.(4).Aug 23, 2025 · N909WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025093007392Floor Panel · pulledFLOOR PANEL 231FF UPPER SKIN HAS AREAS OF PULLED STRANDS. FLOOR PANEL 231FF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL IAW SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.Aug 23, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093007393Floor Panel · pulledFLOOR PANEL 231JF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED NEW FLOOR PANEL IAW SRM 53-00-50-2R-0 PARA 1. A.Aug 23, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093007397Floor Panel · pulledFLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED A NEW FLOOR PANEL IAW SRM 53-00-50-2R-0 PARA 1. A.Aug 23, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093007398Floor Panel · pulledFLOOR PANEL 241VF UPPER SKIN HAS AREAS OF PULLED STRANDS. FLOOR PANEL 241VF WAS REPLACED WITTH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.Aug 23, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093007399Floor Panel · pulledFLOOR PANEL 242QF UPPER SKIN HAS AREAS OF PULLED STRANDS. FLOOR PANEL 242QF WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.Aug 23, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093007665Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAS PULLED STRANDS. FABRICATED NEW FLOOR PANEL IAW SRM 53-00-50-2R-0 PARA 1. A.Aug 23, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093007154Floor Panel · pulledFWD FLOOR PANEL 221GF UPPER SKIN HAS AREAS OF PULLED STRANDS. FWD FLOOR PANEL 221GF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.Aug 22, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093007148Floor Panel · pulledFWD FLOOR PANEL 222DF UPPER SKIN HAS AREAS OF PULLED STRANDS. FWD FLOOR PANEL 222DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.Aug 22, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093007153Floor Panel · pulledFWD FLOOR PANEL 221FF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FWD FLOOR PANEL 221FF WAS REPLACED WITH A SERVICEABLE FLOOR PANEL IAW SRM 51-10-02-0G-0, PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.Aug 22, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093007151Floor Panel · pulledFWD FLOOR PANEL 221BF UPPER SKIN HAS AREAS OF PULLED STRANDS. FWD FLOOR PANEL 221BF WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0, PARA 9.A.A DUE TO AMOUNT OF ALL DAMAGE.Aug 22, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093007152Floor Panel · pulledFWD FLOOR PANEL 221CF UPPER SKIN HAS AREAS OF PULLED STRANDS. FWD FLOOR PANEL 221CF WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0, PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.Aug 22, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093007145Floor Panel · pulledFWD FLOOR PANEL 221DF UPPER SKIN HAS AREAS OF PULLED STRANDS. FWD FLOOR PANEL 221DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.Aug 22, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093007146Floor Panel · pulledFWD FLOOR PANEL 221EF UPPER SKIN HAS AN AREA OF PULLED STRANDS. FWD FLOOR PANEL 221EF SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1-A00939.Aug 22, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093007147Floor Panel · pulledFWD FLOOR PANEL 222CF UPPER SKIN HAS AREAS OF PULLED STRANDS. FWD FLOOR PANEL WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G, PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.Aug 22, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025100107135Strap · corrodedCORROSION ON TENSION STRAP AT BS 1015 RBL3 AND BS 1016+13, RBL 3, WL 208. REMOVED AND REPLACED TENSION STRAP IAW SRM 51-40-02-0G-0 AND DWG 147A5730.Aug 21, 2025 · N909WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025100107136Shear Web · corrodedCORROSION ON LT SHEAR WEB AT BS 1016+14, LBL 12, WL 208. REPAIRED PER 25-153-02318-WIP1.Aug 21, 2025 · N909WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025100107137Shear Web · corrodedCORROSION ON RT SHEAR WEB AT BS 1016 RBL 1; WL 208. REPAIRED PER EA#25-153-02314.Aug 21, 2025 · N909WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025100107142Scuff Plate · crackedACD AFT CORNER SCUFF PLATE IS CRACKED PART WAS INSTALLED ON CUSTOMER CARD: TTG8Q01533B7;[02] WELDED THE ACD AFT CORNER SCUFF PLATE PER SRM 53-60-15-2R-1 STEP 4.B.(4). APPLIED CHEMICAL CONVERSION COATING AND TWO LAYERS OF BMS 10-11 TYPE I PRIMER ON ACB AFT CORAug 21, 2025 · N909WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025100107149Stub Frame · crackedCRACK ON FSD STUB FRAME AT BS300; .1' ABOVE SEAL DEPRESSOR; .2' LENGTH. NO ALLOWABLE DAMAGE FOUND AT SRM; UPPER STUB FRAME TO BE REPAIRABLE BY REPLACEMENT PER SRM 51-10-02; STEP 9. REMOVED FWD GALLEY DOOR UPPER STUB FRAME PER SRM 51-40-02; INSTALLED FWD GALLAug 21, 2025 · N909WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2025100107134Floorbeam · corrodedCORROSION ON BS986.5 FLOORBEAM AT NUTPLATE HOLE LBL41; WL208. DAMAGE FOUND AT BS-986.5; LBL-41; WL-208. WILL BE REPAIRED ON CUSTOMER CARD NO#TTG8Q014PYWD.Aug 21, 2025 · N909WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2025093006706Floor Panel · pulledAFT FLOOR PANEL 241XF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241XF UPPER SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1-A00939.Aug 21, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093006698Floor Panel · pulledAFT FLOOR PANEL 241YF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241YF SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1-A00939Aug 21, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093006699Floor Panel · pulledAFT FLOOR PANEL 241ZF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED PER SRM 53-00-50-2R-1.Aug 21, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093006700Floor Panel · pulledAFT FLOOR PANEL 241ABF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE AFT FLOOR PANEL 241ABF SKIN DAMAGE WAS REPAIRED IAW SRM 53-00-50-2R-1-A00939, REPAIR 1.Aug 21, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093006709Floor Panel · pulledAFT FLOOR PANEL 241ADF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241ADF SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1-A00939, REPAIR 1.Aug 21, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093006702Floor Panel · pulledAFT FLOOR PANEL 242TF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE AFT FLOOR PANEL 242TF UPPER SKIN WAS REPAIRED IAW SRM 53-00-50-2R-1.Aug 21, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093006703Floor Panel · pulledAFT FLOOR PANEL 242UF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE AFT FLOOR PANEL 242UF WAS REPAIRED IAW SRM 53-00-50-2R-1.Aug 21, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093006704Floor Panel · pulledAFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE AFT FLOOR PANEL 242VF WAS REPAIRED IAW SRM 53-00-50-2R-1-A00939, REPAIR 1.Aug 21, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093006710Floor Panel · crackedAFT FLOOR PANEL 242XF LOWER SKIN IS CRACKED. THE AFT FLOOR PANEL 242XF WAS REPLACED WITH A SERVICEABLE FLOOR PANEL IAW SRM 51-10-02-0G-0 PARA 9.A.1, DUE TO MOUNT OF DAMAGE.Aug 21, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093007138Floorbeam · corrodedCORROSION ON BS 986.5 FLOORBEAM AT NUTPLATE HOLE RBL 43, WL 208. REPAIRED THE FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6.Aug 21, 2025 · N909WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2025093006707Floor Panel · pulledAFT FLOOR PANEL 241AAF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATION OF NEW 241AAF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0-A00938.Aug 21, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093006708Floor Panel · pulledAFT FLOOR PANEL 241ACF UPPER SKIN HAS AREAS OF PULLED STRANDS. AREAS OF PULLED STRANDS ON AFT FLOOR PANEL 241ACF WERE REPAIRED IAW SRM 53-00-50-2R-1.Aug 21, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093006701Floor Panel · pulledAFT FLOOR PANEL 241AEF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT 241AEF SURFACE SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1-A00939, REPAIR 1.Aug 21, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093006350Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO THE EXTENT OF DAMAGE. REPLACED FLOOR PANEL 241AF WITH NEW PANEL IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-42A ITEM 75.Aug 20, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093006346Floor Panel · pulledFLOOR PANEL 231YF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPLACEMENT 231YF FLOORBOARD WAS FABRICATED IAW SRM 53-00-50-2R-0.Aug 20, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093006498Pressure Deck · crackedCRACK NOTED ON RT HORIZONTAL PRESSURE DECK WEB EDGE OF STIFFENER BS 663+10, RBL 41.5, L: 0.4'. INSTALLED A REPAIRBS 663- BS 706; RBL 24.5- RBL 45. WL 204 IAW SRM 53-40-51-2R-2, REPAIR 2, FIGURE 202.Aug 20, 2025 · N909WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2025093006351Floor Panel · pulledFLOOR PANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED FLOOR PANEL 242AF IAW SRM 53-00-50-2R-0 AND DWG 144A5810 0189.Aug 20, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093006347Floor Panel · pulledFLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPLACEMENT 231ZF FLOOR PANEL WAS FABRICATED IAW SRM 53-00-50-2R-0.Aug 20, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093006353Floor Panel · pulledFLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO EXTENT OF THE DAMAGE NEW 241BF FLOOR PANEL WAS FABRICATED IAW SRM 53-00-50-2R-0.Aug 20, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093006349Floor Panel · pulledFLOOR PANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO EXTENT OF THE DAMAGE NEW 232SF FLOOR PANEL WAS FABRICATED IAW SRM 53-00-50-2R-0.Aug 20, 2025 · N909WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025093016355Rib · looseLEFT WING DEFLECTION CONTROL RIB LOOSE. REPAIRED IAW SRM 57-51-02-2R-4; LT WING DEFLECTION CONTROL RIB.Aug 18, 2025 · N909WN · Boeing 7377H4 · Wing, Rib/BulkheadSDR SWAA2025093005270Lens · crackedCRACKED EXIT SIGN LENS AFT LT DOORWAY LINING. REPLACED THE EXIT SIGN LENS IAW AMM 33-51-01-960-801.Aug 17, 2025 · N909WN · Boeing 7377H4 · Emergency LightingSDR SWAA2025093005229Battery Pack · failedEMERGENCY EXIT LIGHT BATTERY PACK M1675 FAIED CAPACITANCE CHECK. REMOVED AND REPLACED SERVICEABLE EMERGENCY EXIT LIGHT BATTERY PACK M1675 IAW AMM 33-51-06-960-805. PERFORMED GOOD BATTERY PACK M1675 IAW AMM 33-51-06-960-805.Aug 16, 2025 · N909WN · Boeing 7377H4 · Emergency LightingSDR SWAA2025031204081Battery Pack · inoperativeEMERGENCY LIGHTS AROUND R/H OVER WING EXIT INOP <[01]. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1669 AT STA 603 RBL 67 IAW AMM 33-51-06.Mar 11, 2025 · N909WN · Boeing 7377H4 · Emergency LightingSDR SWAA2024091135496Light · inoperativeRH OVERWING DOOR EMERGENCY LIGHT INOP<[01] 01 - REMOVED AND REPLACED ;OPS OK; PER [AMM 33-51-04-960-801-NG (SLIDE/OVERWING LIGHT - LAMP REPLACEMENT - PERMANENT)]Sep 8, 2024 · N909WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023110811368Panel · crackedCRACK LEADING EDGE RIB ACCESS PANEL 331B LOCATED AT LE STA 105.26 AT LT HORIZONTAL STABILIZER 2023-635562<[01] REPLACED LEADING EDGE RIB (CHORD) AND FASTENERS IN ACCESS PANEL 331B LOCATED AT LE STA 105.26 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 POct 17, 2023 · N909WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2023110811366Panel · crackedCRACK LEADING EDGE RIB ACCESS PANEL 331B LOCATED AT LE STA 133.15 AT LT HORIZONTAL STABILIZER 2023-635563<[01] REPLACED RIB LOCATED LEADING EDGE RIB OF ACCESS PANEL 331B AT LE STA 133.15 AT LT HORIZONTAL STABILIZER I.A.W B737-700 SRM 51-40-02-0G-0; SRM 51-10-0Oct 17, 2023 · N909WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2023110711367Access Panel · crackedCRACK LEADING EDGE RIB ACCESS PANEL 331B LOCATED AT LE STA 95.96 AT LT HORIZONTAL STABILIZER 2023-635561<[01] REPLACED LEADING EDGE RIB ACCESS PANEL 331B LOCATED AT LE STA 95.96 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51Oct 17, 2023 · N909WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2023110710837Floor Panel · corrodedCORROSION FLOOR PANEL 221CF SLEEVES AT FWD GALLEY AREA (8 EA) 2023-635538<[01] REPLACED FLOOR PANEL 221CF SLEEVES AT FWD GALLEY AREA (9 EA) AND CURED EPOXY ADHESIVE ON SLEEVE OF FLOOR PANEL IAW B737-700 SRM 53-00-50-2R-0 REPAIR GENERAL PARAGRAPH 5S ITEM 1. APPOct 14, 2023 · N909WN · Boeing 7377H4 · Fuselage Floor Panel
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