N925WN

Service difficulty reports · 252

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 = 'N925WN' 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 SWAA2026061508637Fuse · inoperativeEMERGENCY LIGHTS AT RT OVERWING EXIT HATCH INOPERATIVE. REMOVED AND REPLACED THE FUSE AND PERFROMED GOOD OPS TEST IAW AMM 33-51-06-960-804.Jun 2, 2026 · N925WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026061508638Fuse · inoperativeEMERGENCY LIGHTS AT LT OVERWING HATCH INOPERATIVE. REPLACED FUSE, AND PERFORMED GOOD OPS TEST IAW AMM 33-51-06-960-804.Jun 2, 2026 · N925WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026061507012Fan Cowl · crackedNUMBER 2 ENGINE O/B FAN COWL IS CRACKED AT FWD LOWER CORNER 3 INCHES FROM LEADING EDGE. REMOVED AND REPLACED PER AMM 71-11-02.May 27, 2026 · N925WN · Boeing 7377H4 · Nacelle/Pylon, Main FrameSDR SWAA2026061506484Scuff Plate · out of positionFWD SERVICE DOOR SCUFF PLATE AFT VERTICAL HOLES DON'T LINE UP TO AIRCRAFT. LOCATED AND DRILLED FSD REPLACEMENT SCUFF PLATE IAW SRM 51-40-05-0G-0; INSTALLATION WILL BE ACCOMPLISHED ON CUSTOMER CARD TTG8Q003L1XU; STEP 10.May 26, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061504197Attach Angle · crackedRIGHT BS 663, A CRACK FOUND ON VAPOR BARRIER UPPER ATTACH ANGLE AT RBL 25, WL 167.68. REMOVED DAMAGE AND REPAIRED IAW SRM 57-10-10-2R-5.May 18, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061504198Attach Angle · crackedLEFT BS 663, CRACK FOUND ON VAPOR BARRIER UPPER ATTACH ANGLE AT LBL 25, WL 167.68. REMOVED DAMAGE AND REPAIRED IAW SRM 57-10-10-2R-5.May 18, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061503106Fairing · crackedNR 1 ENGINE AFT FAIRING AFT END IS CRACKED. REMOVED; AND REPLACED NR 1 ENGINE AFT FAIRING AFT END TRAILING EDGE ASSY IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG 313A2400 REV:A; DWG 313A2700 REV-.May 14, 2026 · N925WN · Boeing 7377H4 · Nacelle/Pylon, Plate/SkinSDR SWAA2026061598287Seat Track · corrodedCORROSION ON PAX CABIN SEAT TRACK LBL 25 WL 208 STA 500A+10 WELL; STA 500D+10 TOP; STA 500D+10 WELL. REMOVED AND REPLACED SEAT TRACK AT 480-520 LBL25 IAW SRM 51-40-02-0G-0 AND EA 26-153-01350.May 13, 2026 · N925WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026061598289Rib · crackedCRACKED RIB RT INSPAR HORIZ STAB STA 120.30 COMMON TO UPPER RETURN FLANGE AND FWD SPAR. REPAIRED PER EA 26-155-01306. THIS IS A CATEGORY A REPAIR IAW SRM 51-00-06.May 13, 2026 · N925WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2026061597632Rib · crackedRT HORZ STAB L/E 341B 4TH RIB FROM I/B CRACKED AT LE STA 105.26. CRACKED RIB FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN SRM. .REMOVED AND REPLACED RT HORZ STAB L/E 4TH RIB FROM I/B AT L/E STA 105.26 IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWGMay 12, 2026 · N925WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2026061597865Skin · crackedCRACK ON RT LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90. CRACKED WAS FOUND TO BE OUT OF LIMITS; REMOVED DAMAGE AND REPAIRED AS PER SRM 55-10-01-2R-11 REP 11.May 12, 2026 · N925WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2026061597617Baffle · crackedBAFFLE ANGLES CRACKED BS 500C AND BS 400 AFT SIDE OF FRAMES, LBL 25, WL 155. REMOVED AND REPLACED BAFFLE ANGLES IAW SRM 51-40-02-0G-0, AND DWG 143A7505, REV B.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061597628Baffle · crackedBAFFLE ANGLE CRACKED BS 500C FWD SIDE OF FRAME, LBL 25, WL 155. REMOVED AND REPLACED BAFFLE ANGLE IAW SRM 51-40-02-0G-0; AND DWG 143A7505, REV B.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061597457Strap · corrodedCORROSION ON STRAP AT BS 1019-1032 LBL 3 WL 208. REMOVED AND REPLACED STRAP IAW SRM 51-40-02-0G-0 AND DWG 147A5600, SHEET 32, REV B.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061597458Strap · corrodedCORROSION ON STRAP AT BS 1025 RBL 3 WL 208. REMOVED AND REPLACED STRAP IAW SRM 51-40-02-0G-0 AND DWG 147A5730, SHEET 23, REV C.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061597462Floor Support · crackedCRACKED FLOOR SUPPORT AT BS 344 - 360, LBL 11, WL 208. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 141A5400, SHEET 46, REV A.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061597464Floor Support · crackedCRACKED FLOOR SUPPORT, BS 380 - 400, LBL 16, WL 208. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 143A5400, SHEET 109, REV A.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061597465Floor Support · crackedCRACKED FLOOR SUPPORT, BS 380-400, RBL 40, WL 208. EMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 143A5400, SHEET 109, REV A.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061597616Stringer Clip · crackedBS 727B, STRINGER CLIP 5R UPPER CORNER CRACKED. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1106 REV-.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061597623Stringer Clip · crackedBS 727E, STRINGER CLIP 5R UPPER CORNER CRACKED. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1112 REV-.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061597624Stringer Clip · crackedBS 727B STRINGER CLIP 6R UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1106 REV-.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061597625Stringer Clip · crackedBS 727B, STRINGER CLIP 7L UPPER CORNER CRACKED. HFEC INSPECTED STRINGER CLIP IAW NDTM PART 6; 51-00-00 PROCEDURE 23 AND FOUND NO CRACKS PRESENT. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1101 REV-.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061597613Stringer Clip · crackedBS 685, STRINGER CLIP 2L UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 144A1106 REV A.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061597615Stringer Clip · crackedBS 727A, STRINGER CLIP 7L UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1101 REV-.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061597621Stringer Clip · crackedBS 727A, STRINGER CLIP 5L UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1101 REV-.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061597622Stringer Clip · crackedBS 727A STRINGER CLIP 5R UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1101; REV-.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061597461Floor Support · crackedCRACKED INTERCOSTAL AT BS 344-360 BL 0 WL 208<[01] OK TO INSTALL GIVEN FOR STEP 2 ITEM 2;[02] REMOVED AND REPLACED NEW INTERCOSTAL BS344-BS360 BL 0 WL208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A5400 REV:-;[03] VERIFIED; CORRECTIVE ACTION STATEMENT # 2. TASKMay 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061597463Floor Support · crackedCRACKED INTERCOSTAL AT BS 312-328 RBL 31 WL 208<[01] REMOVED AND REPLACED INTERCOSTAL AT BS 312-328 RBL 31 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 141A5400 SHEET 39 REV - DATE: 08/13/96;[02] VERIFIED CORRECTIVE ACTION 1May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061597460Tee Fitting · corrodedCORROSION AT BS 986, RBL 43, WL 208. TASK CARD C/W. REMOVED AND REPLACED PREVIOUS REPAIR TEE FITTING SECTION, RBL14 - RBL50, WL 208 IAW SRM 51-40-02-0G-0 AS SHOWN IN EA 1-753-30047 REV IR ; SRM 53-70-51-2R-4 WITHOUT DEVIATION.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026061597618Stringer Clip · crackedSTA 727E STR CLIP 7L UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1112; REV-May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061597626Stringer Clip · no discrepancySTA 727B STR CLIP 8L UPPER CORNER CRACKED. HFEC INSPECTED STRINGER CLIP AT 727B; S-8L IAW 737 NDTM PART 6; 51-00-00 PROCEDURE 23 AND FOUND NO CRACKS PRESENT.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061597627Stringer Clip · no discrepancySTA 767 STR CLIP 10L UPPER CORNER CRACKED. HFEC INSPECTED STRINGER CLIP AT 767; S-10L IAW 737 NDTM PART 6; 51-00-00 PROCEDURE 23 AND FOUND NO CRACKS PRESENT.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061597629Stringer Clip · crackedSTA 727E STR CLIP 6L UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1112; REV- DATED:09/20/01;[02] VERIFIED ACTION 1 COMPLETE.;[03] CORRECTED MEASUREMENTS TABLE FOR STRINGER LOCATION.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061597630Frame · crackedCRACKED FRAME AT BS 312 LBL 45 WL 284 BETWEEN STR 6L AND STR 5L. COMPLETED PER EA M-22-153-01244 (737-NG - SWA - BS 312 FRAME UPPER CHORD CRACK DAMAGE AT LBL 33 BETWEEN S-5L AND S-6L) CCN TTG8Q01C6MBH;[02] VERIFIED; CORRECTIVE ACTION STATEMENT # 1. PCW ON TAMay 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2026061597459Floor Panel · corrodedCORROSION AT BS 986 RBL 36 WL 208. PREVIOUS REPAIR AND NO LIMITS ALLOWED PART TO BE REMOVED AND REPLACED ON CCN TTG8Q01C4FD9.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026061597471Seat Track · corrodedCORROSION ON PAX CABIN SEAT TRACK RBL 45 WL 208 STA 480+7 WELL; STA 480+7 TOP; STA 500+6 TOP; STA 500A TOP. SEAT TRACK WILL BE REPLACED ON TASK CARD TTG8Q01C4H2B.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026061597474Seat Track · corrodedCORROSION ON PAX CABIN SEAT TRACK RBL 25 WL 208 STA 480+7 WELL; STA 500+6 TOP; STA 500A+17 TOP; STA 500A+18 WELL. SEAT TRACK WILL BE REPLACED ON TASK CARD TTG8Q01C4HKH.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026061597477Seat Track · corrodedCORROSION ON PAX CABIN SEAT TRACK LBL 25 WL 208 STA 500A+10 WELL; STA 500D+10 TOP; STA 500D+10 WELL. UPON FURTHER INVESTIGATION FOUND DAMAGE TO BE AT A PREVIOUS REPAIR. NO ALLOWABLE DAMAGE LIMITS.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026061597470Seat Track · corrodedCORROSION ON PAX CABIN SEAT TRACK LBL 45 WL 208 STA 480+17 TOP; STA 500+8 WELL; STA 500A+15 WELL; STA 500B+18 WELL; STA 500B+17 TOP. SEAT TRACK WILL BE REPLACED ON TASK CARD TTG8Q01C4HKW.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026061597319Stringer Clip · crackedBS 727C STRINGER CLIP 6L UPPER SURFACE CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1103; REV- .May 10, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061597320Stringer Clip · crackedBS 727C STRINGER CLIP 7L UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1103; REV-.May 10, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061597321Stringer Clip · crackedBS 727C STRINGER CLIP 5R CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1103; REV- .May 10, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061597322Stringer Clip · crackedBS 727C STRINGER CLIP 6R UPPER SURFACE CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1103; REV-.May 10, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061597318Stringer Clip · crackedSTA 727C STR CLIP 5L UPPER CORNER CRACKED. MARKED.<[01] REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1103; REV- DATED:09/15/01;[02] VERIFIED ACTION 1 COMPLETE.May 10, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061597014Floor Panel · damagedAFT FLOOR PANEL 242WF HAS MISSING PLIES ON LOWER SURFACE. DUE TO THE EXTENT OF DAMAGE, REPLACED THE AFT FLOOR PANEL 242WF IAW SRM 51-10-02-0G-0, PARA 9, AND AIPC 53-21-00-26, ITEM 195.May 9, 2026 · N925WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026061597013Floor Panel · delaminatedAFT FLOOR PANEL 241AEF UPPER SURFACE DELAMINATED. AFT FLOOR PANEL 241AEF WAS REPAIRED IAW SRM 53-00-50-2R-1.May 9, 2026 · N925WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026061596718Stub Frame · crackedCRACK NOTED ON R1 DOOR CUT OUT STUB FRAME, 0.1 INCH ABOVE SEAL DEPRESSOR, 0.4 INCH FROM FWD EDGE, L: 2.3 INCH. REMOVED DAMAGE FSD STUB FRAME. LOCATED, DRILLED, AND INSTALLED A NEW FSD STUB FRAME AT BS 291 ABOVE SEAL DEPRESSOR IAW SRM 51-40-02-0G-0, AND DWG 1May 8, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026061596492Rib · crackedRT HORZ STAB L/E 341B 3RD RIB FROM I/B CRACKED AT LE STA 95.9. CRACKED RIB FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. REMOVED AND REPLACED RT HORZ STAB L/E 3RD RIB FROM I/B AT L/E STA 95.96 IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWGMay 8, 2026 · N925WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2026061596495Stiffener · crackedRIGHT HORIZONTAL STAB RIB 4 STIFFENER NR 3 IS CRACKED. REPAIRED LOWER SIDE OF STIFFENER #3 AT RIB NR 4 RT HORIZONTAL STABILIZER IAW SRM 55-10-09-2R-5.May 8, 2026 · N925WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2026061596494Rub Strip · crackedNR 3 AFT FLAP FAIRING 542BB O/B RUB STRIP CRACKED. REMOVED AND INSTALLED NEW OTB RUB STRIP ON NR 3 AFT FLAP FAIRING 542BB IAW AMM 20-50-11-910-801 .May 8, 2026 · N925WN · Boeing 7377H4 · Trailing Edge Flaps
Back to N925WN