# Service difficulty reports: N925WN A list on [N925WN](https://openairdocs.org/aircraft/N925WN.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 6 · 252 reports - [SDR SWAA2026061508637](https://openairdocs.org/sdr/SWAA2026061508637.md): Fuse · inoperative · Jun 2, 2026 · N925WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY LIGHTS AT RT OVERWING EXIT HATCH INOPERATIVE. REMOVED AND REPLACED THE FUSE AND PERFROMED GOOD OPS TEST IAW AMM 33-51-06-960-804. - [SDR SWAA2026061508638](https://openairdocs.org/sdr/SWAA2026061508638.md): Fuse · inoperative · Jun 2, 2026 · N925WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY LIGHTS AT LT OVERWING HATCH INOPERATIVE. REPLACED FUSE, AND PERFORMED GOOD OPS TEST IAW AMM 33-51-06-960-804. - [SDR SWAA2026061507012](https://openairdocs.org/sdr/SWAA2026061507012.md): Fan Cowl · cracked · May 27, 2026 · N925WN · Boeing 7377H4 · Nacelle/Pylon, Main Frame > NUMBER 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. - [SDR SWAA2026061506484](https://openairdocs.org/sdr/SWAA2026061506484.md): Scuff Plate · out of position · May 26, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > FWD 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. - [SDR SWAA2026061504197](https://openairdocs.org/sdr/SWAA2026061504197.md): Attach Angle · cracked · May 18, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > RIGHT 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. - [SDR SWAA2026061504198](https://openairdocs.org/sdr/SWAA2026061504198.md): Attach Angle · cracked · May 18, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > LEFT 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. - [SDR SWAA2026061503106](https://openairdocs.org/sdr/SWAA2026061503106.md): Fairing · cracked · May 14, 2026 · N925WN · Boeing 7377H4 · Nacelle/Pylon, Plate/Skin > NR 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-. - [SDR SWAA2026061598287](https://openairdocs.org/sdr/SWAA2026061598287.md): Seat Track · corroded · May 13, 2026 · N925WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings > CORROSION 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. - [SDR SWAA2026061598289](https://openairdocs.org/sdr/SWAA2026061598289.md): Rib · cracked · May 13, 2026 · N925WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib > CRACKED 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. - [SDR SWAA2026061597632](https://openairdocs.org/sdr/SWAA2026061597632.md): Rib · cracked · May 12, 2026 · N925WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin > RT 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; DWG - [SDR SWAA2026061597865](https://openairdocs.org/sdr/SWAA2026061597865.md): Skin · cracked · May 12, 2026 · N925WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin > CRACK 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. - [SDR SWAA2026061597617](https://openairdocs.org/sdr/SWAA2026061597617.md): Baffle · cracked · May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > BAFFLE 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. - [SDR SWAA2026061597628](https://openairdocs.org/sdr/SWAA2026061597628.md): Baffle · cracked · May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > BAFFLE 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. - [SDR SWAA2026061597457](https://openairdocs.org/sdr/SWAA2026061597457.md): Strap · corroded · May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION 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. - [SDR SWAA2026061597458](https://openairdocs.org/sdr/SWAA2026061597458.md): Strap · corroded · May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION 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. - [SDR SWAA2026061597462](https://openairdocs.org/sdr/SWAA2026061597462.md): Floor Support · cracked · May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED 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. - [SDR SWAA2026061597464](https://openairdocs.org/sdr/SWAA2026061597464.md): Floor Support · cracked · May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED 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. - [SDR SWAA2026061597465](https://openairdocs.org/sdr/SWAA2026061597465.md): Floor Support · cracked · May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED 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. - [SDR SWAA2026061597616](https://openairdocs.org/sdr/SWAA2026061597616.md): Stringer Clip · cracked · May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > BS 727B, STRINGER CLIP 5R UPPER CORNER CRACKED. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1106 REV-. - [SDR SWAA2026061597623](https://openairdocs.org/sdr/SWAA2026061597623.md): Stringer Clip · cracked · May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > BS 727E, STRINGER CLIP 5R UPPER CORNER CRACKED. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1112 REV-. - [SDR SWAA2026061597624](https://openairdocs.org/sdr/SWAA2026061597624.md): Stringer Clip · cracked · May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > BS 727B STRINGER CLIP 6R UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1106 REV-. - [SDR SWAA2026061597625](https://openairdocs.org/sdr/SWAA2026061597625.md): Stringer Clip · cracked · May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > BS 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-. - [SDR SWAA2026061597613](https://openairdocs.org/sdr/SWAA2026061597613.md): Stringer Clip · cracked · May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > BS 685, STRINGER CLIP 2L UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 144A1106 REV A. - [SDR SWAA2026061597615](https://openairdocs.org/sdr/SWAA2026061597615.md): Stringer Clip · cracked · May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > BS 727A, STRINGER CLIP 7L UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1101 REV-. - [SDR SWAA2026061597621](https://openairdocs.org/sdr/SWAA2026061597621.md): Stringer Clip · cracked · May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > BS 727A, STRINGER CLIP 5L UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1101 REV-. - [SDR SWAA2026061597622](https://openairdocs.org/sdr/SWAA2026061597622.md): Stringer Clip · cracked · May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > BS 727A STRINGER CLIP 5R UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1101; REV-. - [SDR SWAA2026061597461](https://openairdocs.org/sdr/SWAA2026061597461.md): Floor Support · cracked · May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED 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. TASK - [SDR SWAA2026061597463](https://openairdocs.org/sdr/SWAA2026061597463.md): Floor Support · cracked · May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED 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 1 - [SDR SWAA2026061597460](https://openairdocs.org/sdr/SWAA2026061597460.md): Tee Fitting · corroded · May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Structure > CORROSION 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. - [SDR SWAA2026061597618](https://openairdocs.org/sdr/SWAA2026061597618.md): Stringer Clip · cracked · May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > STA 727E STR CLIP 7L UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1112; REV- - [SDR SWAA2026061597626](https://openairdocs.org/sdr/SWAA2026061597626.md): Stringer Clip · no discrepancy · May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > STA 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. - [SDR SWAA2026061597627](https://openairdocs.org/sdr/SWAA2026061597627.md): Stringer Clip · no discrepancy · May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > STA 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. - [SDR SWAA2026061597629](https://openairdocs.org/sdr/SWAA2026061597629.md): Stringer Clip · cracked · May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > STA 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. - [SDR SWAA2026061597630](https://openairdocs.org/sdr/SWAA2026061597630.md): Frame · cracked · May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Frame > CRACKED 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 TA - [SDR SWAA2026061597459](https://openairdocs.org/sdr/SWAA2026061597459.md): Floor Panel · corroded · May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Floor Panel > CORROSION AT BS 986 RBL 36 WL 208. PREVIOUS REPAIR AND NO LIMITS ALLOWED PART TO BE REMOVED AND REPLACED ON CCN TTG8Q01C4FD9. - [SDR SWAA2026061597471](https://openairdocs.org/sdr/SWAA2026061597471.md): Seat Track · corroded · May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings > CORROSION 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. - [SDR SWAA2026061597474](https://openairdocs.org/sdr/SWAA2026061597474.md): Seat Track · corroded · May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings > CORROSION 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. - [SDR SWAA2026061597477](https://openairdocs.org/sdr/SWAA2026061597477.md): Seat Track · corroded · May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings > CORROSION 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. - [SDR SWAA2026061597470](https://openairdocs.org/sdr/SWAA2026061597470.md): Seat Track · corroded · May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings > CORROSION 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. - [SDR SWAA2026061597319](https://openairdocs.org/sdr/SWAA2026061597319.md): Stringer Clip · cracked · May 10, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > BS 727C STRINGER CLIP 6L UPPER SURFACE CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1103; REV-. - [SDR SWAA2026061597320](https://openairdocs.org/sdr/SWAA2026061597320.md): Stringer Clip · cracked · May 10, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > BS 727C STRINGER CLIP 7L UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1103; REV-. - [SDR SWAA2026061597321](https://openairdocs.org/sdr/SWAA2026061597321.md): Stringer Clip · cracked · May 10, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > BS 727C STRINGER CLIP 5R CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1103; REV-. - [SDR SWAA2026061597322](https://openairdocs.org/sdr/SWAA2026061597322.md): Stringer Clip · cracked · May 10, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > BS 727C STRINGER CLIP 6R UPPER SURFACE CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1103; REV-. - [SDR SWAA2026061597318](https://openairdocs.org/sdr/SWAA2026061597318.md): Stringer Clip · cracked · May 10, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > STA 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. - [SDR SWAA2026061597014](https://openairdocs.org/sdr/SWAA2026061597014.md): Floor Panel · damaged · May 9, 2026 · N925WN · Boeing 7377H4 · Fuselage Floor Panel > AFT 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. - [SDR SWAA2026061597013](https://openairdocs.org/sdr/SWAA2026061597013.md): Floor Panel · delaminated · May 9, 2026 · N925WN · Boeing 7377H4 · Fuselage Floor Panel > AFT FLOOR PANEL 241AEF UPPER SURFACE DELAMINATED. AFT FLOOR PANEL 241AEF WAS REPAIRED IAW SRM 53-00-50-2R-1. - [SDR SWAA2026061596718](https://openairdocs.org/sdr/SWAA2026061596718.md): Stub Frame · cracked · May 8, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Structure > CRACK 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 1 - [SDR SWAA2026061596492](https://openairdocs.org/sdr/SWAA2026061596492.md): Rib · cracked · May 8, 2026 · N925WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib > RT 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; DWG - [SDR SWAA2026061596495](https://openairdocs.org/sdr/SWAA2026061596495.md): Stiffener · cracked · May 8, 2026 · N925WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure > RIGHT 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. - [SDR SWAA2026061596494](https://openairdocs.org/sdr/SWAA2026061596494.md): Rub Strip · cracked · May 8, 2026 · N925WN · Boeing 7377H4 · Trailing Edge Flaps > NR 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. Next page: https://openairdocs.org/aircraft/N925WN/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/aircraft/N925WN/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.