N482WN

Service difficulty reports · 301

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 = 'N482WN'
  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 SWAA2026100741317Pump · low pressureENG 1 HYD PUMP LOW PRESSURE LIGHT CAME ON IN FLIGHT. HYDRAULIC SYSTEM A QTY: 13% PRESS: 3080.Oct 3, 2026 · N482WN · Boeing 7377H4 · Hydraulic Pump (Electric/Engine), MainSDR SWAA2026071420114Attach Bracket · crackedAFT ENTRY (L2) DOOR LOWER DOOR LINER ATTACHMENT PANEL BRACKET IS CRACKED. REMOVED AND REPLACED AFT ENTRY (L2) DOOR LOWER DOOR LINER ATTACHMENT PANEL BRACKET USING SRM 51-40-02Jul 10, 2026 · N482WN · Boeing 7377H4 · Passenger/Crew DoorsSDR SWAA2026071320213Battery Pack · failedFLIGHT DECK, BATTERY PACKS M1668 & M1675 EACH FAILED RESPECTIVE CAPACITY TESTS. R & R BATTERY PACKS M1668 & M1675 IAW AMM 33-51-06.Jul 10, 2026 · N482WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026071320978Battery Pack · no testFLIGHT DECK, BATTERY PACKS M1668 & M1675 EACH FAILED RESPECTIVE CAPACITY TESTS. R & R BATTERY PACKS M1668 & M1675 IAW AMM 33-51-06.Jul 10, 2026 · N482WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026071019308Sign · brokenCENTER CABIN CEILING OVER WING EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED IAW AMM 33-51-01-960-802-NG.Jul 7, 2026 · N482WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026061807884Strap · corrodedCORROSION ON RETAINER STRAP SEAL, SPOILER 1, LT WING. REPLACED RETAINER STRAP SEAL SPOILER 1 AT LT WING IAW SRM 51-40-02, DWG 115A3500, SHEET 22, REV A.May 30, 2026 · N482WN · Boeing 7377H4 · SpoilersSDR SWAA2026061707972Plate · crackedCRACKED OTBD TRAILING EDGE CORRUGATED PLATE ON ORSS 314, RT WING. REPLACED CORRUGATED PLATE LOCATED OTBD TRAILING EDGE ON ORSS 314 AT RT WING. IAW SRM 51-40-02-0G-0 AND DWG 115A3700, SHEET 32 REV-.May 30, 2026 · N482WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2026061707883Plate · crackedCRACKED CORRUGATED PLATE TRAILING EDGE LOCATED ON IRSS 261 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ON IRSS 261 AT LT WING IAW SRM 51-40-02-0G-0 AND DWG 115A2001 SHEET 26 REV-.May 30, 2026 · N482WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2026061707881Support Angle · crackedCRACKED OTBD TRAILING EDGE SUPPORT ANGLE ON ORSS 287 AT LT WING. REPLACED OTBD TE SUPPORT ANGLE AT ORSS 287, LT WING IAW SRM 51-40-02-0G-0, DWG 115A3700, SHEET 31, REV-, & DWG 115A3712, SHEET 12, REV- .May 30, 2026 · N482WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2026061707882Support Bracket · crackedCRACKED TRAILING EDGE SUPPORT BRACKET LOCATED ON IRSS 268 AT LT WING. REPLACED SUPPORT BRACKET LOCATED TRAILING EDGE IRSS 268 AT LT WING IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, AND DWG 115A2930, SHEET 7, REV -.May 30, 2026 · N482WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2026061707886Plate · crackedCRACKED INBD TRAILING EDGE CORRUGATED PLATE LOCATED ON IRSS 242 AT LT WING. REPLACED CORRUGATED PLATE LOCATED ON INBD TRAILING EDGE IRSS 242 AT LT WING IAW SRM 51-40-02-0G-0 AND DWG 115A2001, SHEET 30, REV A.May 30, 2026 · N482WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2026061807351Fitting · crackedREMOVE AND REPLACE SLAT 1 LT WING DUE TO SECONDARY FINDING: CRACK ON FITTING SLAT 1. REPLACED LEADING EDGE SLAT 1 IAW AMM 27-81-21-401. TESTED OK .May 28, 2026 · N482WN · Boeing 7377H4 · Leading Edge DevicesSDR SWAA2026061707339Rib · crackedCRACKED INSPAR RIB LOCATED STAB BS 129.50 AND 18 INCH FROM FRONT SPAR RT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON INSPAR RIB STA 129.50 AND 18 INCHS OF FRONT SPAR RT HORIZONTAL STABILIZER IAW SRM 55-10-09-2R-4 REPAIR 4.May 27, 2026 · N482WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2026061707340Support Angle · elongatedELONGATED HOLE ON SUPPORT ANGLE FOR ACCESS PANEL 551FB TRAILING EDGE AT LT WING. REPLACED SUPPORT ANGLE AND RE-INSTALLED BRACKET(2E/A) ACCESS PANEL 551FB TRAILING EDGE AT LT WING IAW SRM 51-10-02-OG-0, ITEM 9, SRM 51-40-02-OG-0, SRM 51-20-01-0G-0, AND DWG 11May 27, 2026 · N482WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2026061707341Support Angle · crackedCRACKED SUPPORT ANGLE, ACCESS PANEL 651GB AT RT WING. REPLACED SUPPORT ANGLE, ACCESS PANEL 651GB AT RT WING IAW SRM 51-40-02-0G-0 AND SRM 51-10-02 ITEM 9.May 27, 2026 · N482WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2026061706551Access Panel · damagedELONGATED HOLE ACCESS PANEL 661BB AT RT WING. REPAIRED THE ACCESS PANEL 661BB AT RT WING IAW SRM 51-70-04-2R-10, REPAIR 10.May 26, 2026 · N482WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2026061706765Scuff Plate · crackedCRACKED AFT CORNER SCUFF PLATE LOCATED AFT CARGO COMPARTMENT. REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.May 26, 2026 · N482WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061706766Scuff Plate · crackedCRACKED CENTER SCUFF PLATE LOCATED AFT CARGO COMPARTMENT. REPAIRED CENTER SCUFF PLATE LOCATED AFT CARGO COMPARTMENT IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.May 26, 2026 · N482WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061706552Access Panel · damagedELONGATED HOLE ON ACCESS PANEL 661CB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661CB TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-10, REPAIR 10.May 26, 2026 · N482WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2026061706548Access Panel · damagedELONGATED HOLE ACCESS PANEL 561AB AT LT WING. REPAIRED THE ACCESS PANEL 561AB AT LT WING IAW SRM 51-70-04-2R-10, REPAIR 10.May 26, 2026 · N482WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2026061706550Access Panel · damagedELONGATED HOLE ACCESS PANEL 561BB AT LT WING. REPAIRED THE ACCESS PANEL 561BB AT LT WING IAW SRM 51-70-04-2R-10, REPAIR 10.May 26, 2026 · N482WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2026061706219Skin · crackedCRACK AROUND FASTENER LOWER SURFACE LEADING EDGE SLAT NOSE SKIN AT THE ACTUATOR FITTING SLAT 7 AT RT WING. REPLACED SLAT NR 7 DUE TO SEVERAL CRACKS DAMAGE AT LOWER SKIN AND FITTING. REPLACED WITH FAULT TTG8Q01CFMD6.May 24, 2026 · N482WN · Boeing 7377H4 · Leading Edge DevicesSDR SWAA2026061706218Skin · crackedCRACK LOWER SURFACE OF LEADING EDGE SLAT 1 NOSE SKIN AT ACTUATOR LOC. AROUND FASTENER AT LT WING. REPLACED SLAT NR 1 DUE TO WAS FOUND SEVERAL CRACKS DAMAGE. FOR REPLACE SEE FAULT TTG8Q01CF1A3.May 24, 2026 · N482WN · Boeing 7377H4 · Leading Edge DevicesSDR SWAA2025121242831Tail Cone · delaminatedTHE FORWARD TAIL CONE FAIRING IS DELAMINATED WITH DAMAGE TO THE FACE SHEETS WITH FIBERS AND HONEYCOMB EXPOSED AND CONTAMINATED WITH HYDRAULIC FLUID. LOCATED BS 1192; 4' LEFT OF TOP. CRACK LENGTH, L=4' W=2.5'. THE TAIL CONE WAS REMOVED AND REPLACED WITH A NEDec 5, 2025 · N482WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2025121242832Tail Cone · delaminatedTHE FORWARD TAIL CONE FAIRING IS DELAMINATED WITH DAMAGE TO THE FACE SHEETS WITH FIBERS AND HONEYCOMB EXPOSED AND CONTAMINATED WITH HYDRAULIC FLUID. BS 1193.5; 24.5' RIGHT OF TOP. CRACK LENGTH, L=3' W=1.5'. THE TAIL CONE WAS REMOVED AND REPLACED WITH A NEW Dec 5, 2025 · N482WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2025121246031Tail Cone · delaminatedTHE FORWARD TAIL CONE FAIRING IS DELAMINATED WITH DAMAGE TO THE FACE SHEETS WITH FIBERS AND HONEYCOMB EXPOSED AND CONTAMINATED WITH HYDRAULIC FLUID. LOCATED BS 1192; 4 INCHES LT OF TOP. CRACK LENGTH, L=4' W=2.5'. TAIL CONE R & R WITH A NEW ONE.Dec 5, 2025 · N482WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2025121246032Tail Cone · delaminatedTHE FORWARD TAIL CONE FAIRING IS DELAMINATED WITH DAMAGE TO THE FACE SHEETS WITH FIBERS AND HONEYCOMB EXPOSED AND CONTAMINATED WITH HYDRAULIC FLUID, BS 1193.5; 24.5' RT OF TOP. CRACK LENGTH, L=3' W=1.5'. TAIL CONE R & R WITH A NEW ONE.Dec 5, 2025 · N482WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2025121242833Tail Cone · delaminatedTHE FORWARD TAIL CONE FAIRING IS DELAMINATED, BS 1190 21 INCHES RIGHT OF TOP. CRACK LENGTH: L=2.3' W=2.2'. LOCATED & DRILLED INITIAL TAIL CONE SCREW HOLES WITH EXCEPTION OF HOLES AROUND ELEVATOR PUSH ROD CUT OUTS IAW MM 51-40-02 & SIP. TAIL CONE WAS R & R Dec 5, 2025 · N482WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2025091213803Lens · looseOVERHEAD EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS PER AMM 33-51-01.Sep 11, 2025 · N482WN · Boeing 7377H4 · Emergency LightingSDR SWAA2025042125797Sign · detachedMID CABIN OVERHEAD EXIT SIGN FELL OFF. SECURED SIGN AS PER SIPApr 16, 2025 · N482WN · Boeing 7377H4 · Emergency LightingSDR SWAA2025030601774Seal · crackedR/H HORIZONTAL UPPER SLIDER CRACKED<[01] REF ADDED;[02] REMOVED AND REPLACED PER 53-31-31.Mar 4, 2025 · N482WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2025030601773Seal · crackedL/H HORIZONTAL UPPER SLIDER CRACKED<[01] REF ADDED;[02] REMOVED AND REPLACED PER 53-31-31.Mar 4, 2025 · N482WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2025012489193Handle · brokenAFT ENTRY DOOR ASSIST HANDLE BROKEN<[01] ROBBED ASSIST HANDLE FROM FWD LAV AND INSTALLED ON AFT LEFT ENTRY DOOR IAW AMM 52-13-31. FWD LAV ASSIST HANDLE INOP. OK TO CONTINUE PER MEL 25-10-01 SP 1B;[02] REPLACED MISSING FWD LAV ASSIST HANDLE PER CMM 25-42-59.Jan 23, 2025 · N482WN · Boeing 7377H4 · Passenger/Crew DoorsSDR SWAA2025012288475Handle · brokenAFT ENTRY DOOR ASSIST HANDLE BROKEN<[01] ROBBED ASSIST HANDLE FROM AFT LAV AND INSTALLED ON AFT ENTRY DOOR IAW AMM 52-13-31. AFT LAV ASSIST HANDLE INOP. OK TO CONTINUE PER MEL 25-10-01 SP 1B. REPLACED MISSING AFT LAV ASSIST HANDLE PER CMM 25-42-60.Jan 22, 2025 · N482WN · Boeing 7377H4 · Passenger/Crew DoorsSDR SWAA2024080713755Seat Track · crackedCRACK INDICATION ON FLOOR STRUCTURE SEAT TRACK AT BS 727 AND AT LBL 45.5 HOLE POSITION B 2024-405210 CRACK INDICATION ON FLOOR STRUCTURE SEAT TRACK AT BS 727B AND AT LBL 45.5 HOLE POSITION B<[01] PERFORMED REPAIR CATEGORY A LOC ON FLOOR STRUCTURE SEAT TRACK BTJul 18, 2024 · N482WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2024080709054Access Panel · crackedCRACK LEADING EDGE RIB ACCESS PANEL 331B LOCATED LE STA198.23 LT HORIZONTAL STAB 2024-405175<[01] REPLACED RIB LOC ON LEADING EDGE STA198.23 ACCESS PANEL 331B HORIZONTAL STABILIZER LH IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. DWG 186A1001; SHEET 11; RJul 4, 2024 · N482WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2024080709053Rib · crackedCRACK LEADING EDGE RIB ACCESS PANEL 331B LOCATED LE STA188.94 LT HORIZONTAL STAB 2024-405174<[01] REPLACED NEW RIB 188.94 AND FASTENERS LOCATED ON LEADING EDGE HORIZONTAL STABILIZER ACCESS PANEL 331B LH IAW B737-700 SRM 51-40-02 AND DWG 186A1001 SHEET 11 REV: Jul 4, 2024 · N482WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2024080821406Unknown · unknownTHICKNESS MEASUREMENT OF GAP BETWEEN INNER CHORD AND WEB S-18A BS 727 RIGHT SIDE IS 0.024 INCH 2024-405139<[01] FAULT RESOLVED ON OTHER FAULT TTG8Q00UBC80;[02] FAULT RESOLVED ON OTHER FAULT TTG8Q00UBC80 ; RIIJul 2, 2024 · N482WN · Boeing 7377H4 · Standard Practices/StructuresSDR SWAA2024080821405Unknown · unknownTHICKNESS MEASUREMENT OF GAP BETWEEN INNER CHORD AND WEB S-18A BS 727 LEFT SIDE IS 0.037 INCH 2024-405138<[01] FAULT RESOLVED ON OTHER FAULT TTG8Q00UBC7V;[02] FAULT RESOLVED ON OTHER FAULT TTG8Q00UBC7V ; RIIJul 2, 2024 · N482WN · Boeing 7377H4 · Standard Practices/StructuresSDR SWAA2024080707754Frame · crackedCRACK ON FRAME WEB LOCATED BS259.5 BTW STR8L AND STR9L AT PASSENGER CABIN 2024-405134<[01] EQUIPMENT USED P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 08-JAN-25;[02] PERFORMED REPAIR ON FRAME WEB LOCATED BS259.5 BTW STR8L AND STR9L AT PASSENGER CABIN IAW EA 24-Jul 1, 2024 · N482WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2024080719012Stringer · crackedCRACK STRINGER 8 INTERNAL AREA FUEL TANK UPPER POSITION LOC. BTW RIB 19 AND RIB 20 AT LT WING 2024-405124<[01] PERFORMED REPAIR CATEGORY A ON STRINGER 8 INTERNAL AREA FUEL TANK UPPER POSITION LOC. BTW RIB 19 AND RIB 20 AT LT WING IAW 24-157-01864. SEE INDIVIDUJun 29, 2024 · N482WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2024080706185Bolt · wornWEAR ON GIRT BAR FITTING BOLT FWD POSITION AT AFT GALLEY AREA (2 EA) 2024-405056<[01] REPLACED GIRT BAR FITTING BOLT FWD POSITION ENTRY DOOR AT AFT GALLEY AREA (2 EA) IAW B737-700 AMM 25-66-02-400-801.;[02] CORRECTED STEP 1 <BR>REPLACED GIRT BAR FITTING BOLT FJun 27, 2024 · N482WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2024080706183Bolt · wornWEAR ON GIRT BAR FITTING BOLT FWD POSITION AT AFT GALLEY AREA (2 EA) 2024-405217<[01] FAULT WILL RESOLVED ON ANOTHER FAULT DUE TO DUPLICATED DISCREPANCY REPORT. <BR>TTG8Q00U7VJ1;[02] CORRECTED STEP 1 <BR>FAULT WILL RESOLVED ON ANOTHER FAULT DUE TO DUPLICATED DJun 27, 2024 · N482WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2024080705917Stringer · crackedCRACK STRINGER 26L LOCATED BS540 AT FWD CARGO COMPARTMENT 2024-405036<[01] TOOL USED ULTRASONIC THICKNESS EQUIPMENT PN:45MG; SN:430063701; DUE DATE:24-JUL-24.;[02] TOOL USED ON STEP 5: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 210138003; DUE DATE: 11-JUN-2Jun 26, 2024 · N482WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2024080705918Stringer · crackedCRACK STRINGER 24L LOCATED BS540 FWD CARGO COMPARTMENT 2024-405037 CRACK STRINGER 24L LOCATED BS540 FWD CARGO COMPARTMENT<[01] STEP 2. ULTRASONIC EQUIPMENT USED P/N: 45MG; S/N: 2218618T11 AND DUE DATE: 30-NOV-24.;[02] CORRECTED STEP 1. <BR>STEP 2 . ULTRASONIC Jun 26, 2024 · N482WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2024080705916Intercostal · crackedCRACK WEB - INTERCOSTAL LOCATED BS500D TO BS520 AND S-28R FWD CARGO COMPARTMENT 2024-405034<[01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25 AND TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATEJun 26, 2024 · N482WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024080705915Intercostal · crackedCRACK WEB - INTERCOSTAL LOCATED BS 500D TO BS 520 AND S-28L FWD CARGO COMPARTMENT 2024-405035<[01] REPLACED WEB - INTERCOSTAL LOCATED BS 500D TO BS 520 AND S-28L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND SRM 51-40-02. AND DWG 143A7902 REV A Jun 26, 2024 · N482WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024080705556Frame · crackedCRACK FRAME WEB LOCATED STA259.5 AND BETWEEN STR8R TO STR9R AT FWD GALLEY AREA 2024-405014<[01] TOOL USED STEP 5 EDDY CURRENT EQUIPMENT. PN: NORTEC 600D; SN:210138003; DUE DATE: 11-JUN-25;[02] PERFORMED REPAIR ON FRAME WEB LOCATED STA259.5 AND BETWEEN STR 8R TJun 25, 2024 · N482WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2024080705558Stringer · crackedCRACK STRINGER 7L LOCATED BETWEEN STA303.9 TO STA294.5 AT PASSENGER CABIN 2024-405020<[01] STEP 7 TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 200053402; DUE DATE: 24-AUG-24;[02] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DJun 25, 2024 · N482WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2024080705555Support · elongatedELONGATED HOLE SUPPORT ZEE LOCATED BS 887 TO BS 907 AND S-25R AT AFT CARGO COMPARTMENT 2024-405009<[01] REJECTION MISSING FASTENERS SUPPORT ZEE AND RIVET BTW STA 887 TO STA 947.5 STR 25R AT AFT CARGO COMPARTMENT (4 EA) SEE TTG8Q00UW75F;[02] REPLACED SUPPORT ZEJun 25, 2024 · N482WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
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