# Service difficulty reports: N411WN, cancelled Sep 29, 2025

A list on [N411WN, cancelled Sep 29, 2025](https://openairdocs.org/deregistered/N411WN-2025-09-29.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 · 265 reports

- [SDR SWAA2025061079856](https://openairdocs.org/sdr/SWAA2025061079856.md): Window · broken · Jun 8, 2025 · N411WN · Boeing 7377H4 · Flight Compartment Windows
  > L1 WINDOW OUTER PANE SHATTERED AT FL390<[01] REMOVED AND REPLACED LT FWD WHCU PER AMM 30-41-11 AND REMOVED AND REPLACED L1 WINDOW PER AMM 56-11-11 BOTH OPS CHECK GOOD. REF LP 2592090 FOR CAT III RECERT.
- [SDR SWAA2024092540554](https://openairdocs.org/sdr/SWAA2024092540554.md): Handle · did not stow · Sep 22, 2024 · N411WN · Boeing 7377H4 · Cargo/Baggage Doors
  > FWD CARGO DOOR HANDLE DIFFICULT TO OPERATE<[01] R/R FWD CARGO DOOR EXTERIOR HANDLE PER AMM 52-31-14
- [SDR SWAA2024090634535](https://openairdocs.org/sdr/SWAA2024090634535.md): Cover · unsecure · Sep 5, 2024 · N411WN · Boeing 7377H4 · Emergency Exits
  > OVERWING EXIT CA SIDE; COVER NEEDS SECURING<[01] RESECURED OVERWING CAP. SIDE EXIT DOOR PER SIP.
- [SDR SWAA2024090332587](https://openairdocs.org/sdr/SWAA2024090332587.md): Light · broken · Aug 30, 2024 · N411WN · Boeing 7377H4 · Emergency Lighting
  > L1 FWD ENTRY DOOR EXIT LT COVER BROKEN OFF<[01] R&R L1 DOOR LOWER EMERGENCY EXIT LT ASSY PER AMM 33-51-01
- [SDR SWAA2024080522695](https://openairdocs.org/sdr/SWAA2024080522695.md): Sensor · split · Aug 4, 2024 · N411WN · Boeing 7377H4 · Trailing Edge Flap Control System
  > SPLIT FLAP LANDING; FLAPS ON LEFT SIDE 1.5 / RIGHT SIDE 2<[01] REMOVED AND REPLACED #6 T/E FLAP SKEW SENSOR PER AMM 27-59-01.
- [SDR SWAA2024020648655](https://openairdocs.org/sdr/SWAA2024020648655.md): Cover · detached · Feb 4, 2024 · N411WN · Boeing 7377H4 · Emergency Lighting
  > FWD SERVICE DOOR LOWER EXIT SIGN COVER OFF<[01] COMPLETED M-21-133-00720<BR><BR>LENS IS TAPED UP WITH CLEAR TAPE IAW M-21-133-00720
- [SDR SWAA2023122835343](https://openairdocs.org/sdr/SWAA2023122835343.md): Girt Bar · loose · Dec 26, 2023 · N411WN · Boeing 7377H4 · Emergency Equipment
  > FORWARD SERVICE DOOR GIRT BAR HOLDER LOOSE.<[01] SECURED FWD SVC DOOR'S GIRT BAR HANGER PER SIP.
- [SDR SWAA2023122134010](https://openairdocs.org/sdr/SWAA2023122134010.md): Girt Bar · out of adjust · Dec 20, 2023 · N411WN · Boeing 7377H4 · Emergency Equipment
  > FWD ENTRY GIRT BAR LOOSE<[01] INSPECTED FWD ENTRY GIRL BAR PER AMM 25-66-01. NO DEFECTS NOTED
- [SDR SWAA2023080786240](https://openairdocs.org/sdr/SWAA2023080786240.md): Light · inoperative · Aug 5, 2023 · N411WN · Boeing 7377H4 · Emergency Lighting
  > OVER WING EXIT LOWER EMERGENCY LIGHTS INOP<[01] RELAMPED RIGHT SIDE OVERWING DOOR INDICATOR LIGHT ASSEMBLY AND TESTED PER AMM 33-51-01-960-801. NO DEFECTS NOTED.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2023080781787](https://openairdocs.org/sdr/SWAA2023080781787.md): Scuff Plate · cracked · Jul 24, 2023 · N411WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FWD CORNER SCUFF PLATE CRACKED<[01] WELDED CRACKED RADIUS OF AFT CARGO BAY; FWD CORNER SCUFF PLATE USING ER4043 ALUMINUM FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 PARAGRAPH 4.B. (2) AND (4). REPAIR REQUIRES DYE PENETRANT INSPECTION.<BR>
- [SDR SWAA2023080781529](https://openairdocs.org/sdr/SWAA2023080781529.md): Scuff Plate · cracked · Jul 23, 2023 · N411WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY AFT CORNER SCUFF PLATE CRACKED<[01] WELDED CRACKED RADIUS OF AFT CARGO BAY; AFT CORNER SCUFF PLATE USING ER4043 ALUMINUM FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 PARAGRAPH 4.B. (2) AND (4). REPAIR REQUIRES DYE PENETRANT INSPECTION.<BR>
- [SDR SWAA2023080779898](https://openairdocs.org/sdr/SWAA2023080779898.md): Stringer · cracked · Jul 18, 2023 · N411WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > FWD CARGO BAY - CRACK ON STRINGER 24L BS 540 (MARKED)<[01] VERIFIED APPLICABILITY IAW SRM 53-30-03-01-1 AND SRM 53-00-03-1A-1;[02] THERE IS NO ALLOWABLE DAMAGE FOR FCB STRINGER CRACK AT BS 540 24L IAW SRM 53-00-03-1A-1. PART TO BE REPAIRED BY REPLACEMENT IAW S
- [SDR SWAA2023080879447](https://openairdocs.org/sdr/SWAA2023080879447.md): Panel · cracked · Jul 17, 2023 · N411WN · Boeing 7377H4 · Fuselage Floor Panel
  > WING CENTER SECTION BREAK PANEL IS CRACKED IN RADIUS NEAR FASTENER BS 540; RBL 1; WL 207<[01] UPDATED PARTS AND MEASUREMENT TABLE;[02] COMPLETED STEP 1;[03] COMPLETED STEP 1 AND VERIFIED MEASURMENT TABLE;[04] REMOVED FLOOR PANEL COMMON TO WING CENTER SECTION B
- [SDR SWAA2023080779744](https://openairdocs.org/sdr/SWAA2023080779744.md): Stringer · cracked · Jul 17, 2023 · N411WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > FWD CARGO BAY - CRACK ON STRINGER 23L BS 540 (MARKED)<[01] EVALUATED CRACK AT FCB STRINGER 23L/H BS 539 DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A FIG 103 DETAIL A;[02] VERIFIED APPLICABILITY FOR STR 23L/H IAW SRM 53-00-03-2R-1 PAR 4; FIG 205.;[03] CUTO
- [SDR SWAA2023080979315](https://openairdocs.org/sdr/SWAA2023080979315.md): Web · cracked · Jul 16, 2023 · N411WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > LT WING TE TRANSITION WEB; AFT LOWER BULB SEAL ANGLE CRACKED; AFT OF PYLON STRUT; MARKED<[01] REMOVED AND REPLACED LT WING TE TRANSITION WEB; AFT LOWER BULB SEAL ANGLE IAW SRM 51-40-02;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2023080987418](https://openairdocs.org/sdr/SWAA2023080987418.md): Angle · cracked · Jul 16, 2023 · N411WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > LT WING TE TRANSITION WEB; AFT LOWER BULB SEAL ANGLE CRACKED; AFT OF PYLON STRUT; MARKED<[01] REMOVED AND REPLACED LT WING TE TRANSITION WEB; AFT LOWER BULB SEAL ANGLE IAW SRM 51-40-02;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2023080979316](https://openairdocs.org/sdr/SWAA2023080979316.md): Web · cracked · Jul 16, 2023 · N411WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > RT WING TE TRANSITION WEB; AFT LOWER BULB SEAL ANGLE CRACKED; AFT OF PYLON STRUT; MARKED<[01] REMOVED AND REPLACED RT WING TE TRANSITION WEB; AFT LOWER BULB SEAL ANGLE IAW SRM 51-40-02;[02] REJECTION: UPPER ATTACH BOLTS ARE LOOSE; SEE STEP 1;[03] COMPLETED STE
- [SDR SWAA2023080987419](https://openairdocs.org/sdr/SWAA2023080987419.md): Angle · cracked · Jul 16, 2023 · N411WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > RT WING TE TRANSITION WEB; AFT LOWER BULB SEAL ANGLE CRACKED; AFT OF PYLON STRUT; MARKED<[01] REMOVED AND REPLACED RT WING TE TRANSITION WEB; AFT LOWER BULB SEAL ANGLE IAW SRM 51-40-02;[02] REJECTION: UPPER ATTACH BOLTS ARE LOOSE; SEE STEP 1;[03] COMPLETED STE
- [SDR SWAA2023080778615](https://openairdocs.org/sdr/SWAA2023080778615.md): Scuff Plate · cracked · Jul 14, 2023 · N411WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY FWD CORNER SCUFF PLATE CRACKED<[01] WELDED CRACKED RADIUS ON FWD CARGO BAY; FWD CORNER SCUFF PLATE USING ER4043 ALUMINUM FILLER ROD LOT NUMBER 1131216 PER SRM 53-30-15-2R-1 PARAGRAPH 4.B. (2) AND (4). REPAIR STILL REQUIRES A DYE PENETRANT INSPECT
- [SDR SWAA2023080978393](https://openairdocs.org/sdr/SWAA2023080978393.md): Skin · cracked · Jul 13, 2023 · N411WN · Boeing 7377H4 · Leading Edge Devices
  > CRACK AROUND THE FASTENER AT NO.1 SLAT LOWER SURFACE OF THE L/E SLAT NOSE SKIN AT ACTUATOR RIBS. MARKED<[01] REMOVED COVE PANELS 525DAB; 525DBB; 525CB IAW SOPM 20-50-01.;[02] REMOVED COVE PANEL 525EB IAW SOPM 20-50-01.;[03] REMOVED SLAT FLEX SKIN IAW SRM 57-42
- [SDR SWAA2023031013272](https://openairdocs.org/sdr/SWAA2023031013272.md): Coffeemaker · faulty · Mar 6, 2023 · N411WN · Boeing 7377H4 · Buffet/Galleys
  > ACRID ODOR AFT SERVICE DOOR AREA; SEEMS TO BE COFFEE MAKER; DISSIPATES WHEN OFF<[01] ACCOMPLISHED CONDITIONAL INSPECTION PER AMM 05-51-56; FOUND SOURCE OF ELECTRICAL SMELL TO BE COMING FROM AFT COFFEE MAKERS. PLACING BOTH AFT COFFEE MAKERS ON MEL. OK TO CONTIN
- [SDR SWAA2022112173733](https://openairdocs.org/sdr/SWAA2022112173733.md): Sign · detached · Nov 19, 2022 · N411WN · Boeing 7377H4 · Emergency Lighting
  > FO SIDE LOWER OVER WING EXIT SIGN FELL OFF / [01] SECURED EXIT SIGN LENS PER AMM 33-51-03
- [SDR SWAA2022072733534](https://openairdocs.org/sdr/SWAA2022072733534.md): Retainer · loose · Jul 24, 2022 · N411WN · Boeing 7377H4 · Escape Slide
  > AFT SLIDE F/O SIDE IS NOT SECURE IN CONTAINER. / [01] FOUND AFT SERVICE DOOR (R2) AFT GIRTH BAR RETAINER TO BE LOOSE; ADJUSTED AFT SERVICE DOOR (R2) AFT GIRTH BAR RETAINER PER S.I.P.
- [SDR SWAA2022072632054](https://openairdocs.org/sdr/SWAA2022072632054.md): Slide · out of position · Jul 22, 2022 · N411WN · Boeing 7377H4 · Escape Slide
  > AFT F/A COMPLAINED BOTH AFT SLIDES ARE FALLING OUT OF CASES / [01] INSPECTED BOTH SLIDES NO DEFECTS NOTED IAW M/M 25-66-01
- [SDR SWAA2022072633933](https://openairdocs.org/sdr/SWAA2022072633933.md): Slide · out of position · Jul 22, 2022 · N411WN · Boeing 7377H4 · Escape Slide
  > AFT F/A COMPLAINED BOTH AFT SLIDES ARE FALLING OUT OF CASES / [01] INSPECTED BOTH SLIDES NO DEFECTS NOTED IAW M/M 25-66-01
- [SDR SWAA2022031181066](https://openairdocs.org/sdr/SWAA2022031181066.md): Slide · out of position · Mar 8, 2022 · N411WN · Boeing 737* · Escape Slide
  > L1 DOOR SLIDE Z FOLD IN CORRECT NEEDS REPOSITION L1 DOOR SLIDE FOLD IN CORRECT NEEDS REPOSITION / [01] CORRECTED ?Z? FOLD IAW AMM25-66-01 AND MT 725-61-06;[02] VERIFIED C/W PER AMM 25-66-01 & MT 725-61-01;[03] C/W
- [SDR SWAA2022020868888](https://openairdocs.org/sdr/SWAA2022020868888.md): Handle · broken · Feb 4, 2022 · N411WN · Boeing 737* · Passenger/Crew Doors
  > FOWARD ENTRY DOOR LOWER HANDLE BROKE; / [01] INSTALLED NEW ASSIST HANDLE PER A.M.M. 52-11-34
- [SDR SWAA2021121350784](https://openairdocs.org/sdr/SWAA2021121350784.md): Bracket · broken · Dec 7, 2021 · N411WN · Boeing 7377H4 · Wing, Attach Fittings
  > LEFT WING DEFLECTION RIB OUTBRD SUPPORT BRACKET BROKE; / [01] REMOVE DAMAGE PER SRM 57-51-02-2R-1.; [02] REMOVE THE LEFT WING DEFLECTION RIB PANEL OUTBOARD SEAL SUPPORT BRACKET WITH 11 SCREWS PER SRM 51-40-02.; [03] C/W DAMAGE REMOVAL INSP AND PERFORMED H.F.E
- [SDR SWAA2021091416776](https://openairdocs.org/sdr/SWAA2021091416776.md): Gauge · damaged · Sep 11, 2021 · N411WN · Boeing 7377H4 · Escape Slide
  > FOUND FWD SERVICE DOOR SLIDE FOAM MISSING FROM PRESSURE GAUGE; / [01] REMOVED FWD SERVICE DOOR SLIDE AND INSTALLED FOAM AND REINSTALLED ORIGINAL SLIDE REF TC 725-61-06-FS AND S.I.P
- [SDR SWAA2021090814805](https://openairdocs.org/sdr/SWAA2021090814805.md): Slide · out of adjust · Sep 4, 2021 · N411WN · Boeing 7377H4 · Escape Slide
  > FWD SVC DOOR EMER. SLIDE NEEDS ADJ.; / [01] ADJUSTED FWD GALLEY SERVICE DOOR SLIDE PER MM 25-666-00
- [SDR SWAA2021081104280](https://openairdocs.org/sdr/SWAA2021081104280.md): Light · faulted · Aug 7, 2021 · N411WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT RH ABOVE FWD CARGO DOOR INOP; 2021-311869 / [01] PERFORMED VISUAL INSPECTION OF THE LIGHT ABOVE FWD CARGO DOOR AND THE LIGHT IN THIS LOCATION IS THE WING ILLUMINATION LIGHT; NOT THE EMERGENCY LIGHT; AND PERFORMED OPERATIONAL TEST OF THE WING I
- [SDR SWAA2021081397440](https://openairdocs.org/sdr/SWAA2021081397440.md): Floor Panel · delaminated · Jul 23, 2021 · N411WN · Boeing 7377H4 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 232AF AT FWD GALLEY AREA; 2021-311843 / [01] TOOL USED HOT BONDER P/N HCS9200B S/N 18165044 DUE DATE 15/FEB/22.; [02] REPAIRED FLOOR PANEL 232AF AT FWD GALLEY AREA AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1; [03] REPAIRED FLOOR PANEL 2
- [SDR SWAA2021081297441](https://openairdocs.org/sdr/SWAA2021081297441.md): Floor Panel · delaminated · Jul 23, 2021 · N411WN · Boeing 7377H4 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 231AF AT FWD GALLEY AREA; 2021-311844 / [01] TOOL USED HOT BONDER P/N HCS9200B S/N 18165044 DUE DATE 15/FEB/22.; [02] TOOL USED: SCALE P/N:SCA-301 S/N:AE-412137 DUE DATE:24-FEB-22; [03] REPAIRED FLOOR PANEL 231AF AT FWD GALLEY AREA AS
- [SDR SWAA2021081297437](https://openairdocs.org/sdr/SWAA2021081297437.md): Floor Panel · delaminated · Jul 23, 2021 · N411WN · Boeing 7377H4 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 222AF AT FWD GALLEY AREA; 2021-311837 / [01] TOOL USED HOT BONDER P/N HCS9200B S/N 18165044 DUE DATE 15/FEB/22.; [02] TOOL USED SCALE P/N SCA-301 S/N AE-412122 DUE DATE 24/FEB/22.; [03] REPAIRED FLOOR PANEL 222AF AT FWD GALLEY AREA AS
- [SDR SWAA2021081297442](https://openairdocs.org/sdr/SWAA2021081297442.md): Floor Panel · delaminated · Jul 23, 2021 · N411WN · Boeing 7377H4 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 222BF AT FWD GALLEY AREA; 2021-311838 / [01] TOOL USED HOT BONDER P/N HCS9200B S/N 18165044 DUE DATE 15/FEB/22.; [02] REPAIRED FLOOR PANEL 222BF AT FWD GALLEY AREA AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1; [03] REPAIRED FLOOR PANEL 2
- [SDR SWAA2021081297438](https://openairdocs.org/sdr/SWAA2021081297438.md): Floor Panel · delaminated · Jul 23, 2021 · N411WN · Boeing 7377H4 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 221BF AT FWD GALLEY AREA; 2021-311840 / [01] TOOL USED HOT BONDER P/N HCS9200B S/N 18165044 DUE DATE 15/FEB/22.; [02] TOOL USED HOT BONDER P/N:HCS9000B S/N:15092096 DUE DATE:14/DEC/21.; [03] TOOL USED SCALE P/N CL5000 S/N AE-408752 DUE
- [SDR SWAA2021081297439](https://openairdocs.org/sdr/SWAA2021081297439.md): Floor Panel · delaminated · Jul 23, 2021 · N411WN · Boeing 7377H4 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 221GF AT FWD GALLEY AREA; 2021-311842 / [01] TOOL USED HOT BONDER P/N HCS9200B S/N 18165044 DUE DATE 15/FEB/2; [02] TOOL USED HOT BONDER P/N:HCS9200B S/N:18165044 DUE DATE:15-FEB-22; [03] TOOL USED SCALE P/N CL5000 S/N AE-408752 DUE DA
- [SDR SWAA2021081297443](https://openairdocs.org/sdr/SWAA2021081297443.md): Floor Panel · delaminated · Jul 23, 2021 · N411WN · Boeing 7377H4 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 241ZF AT AFT GALLEY AREA; 2021-311839 / [01] TOOL USED HOT BONDER P/N HCS9200B S/N 18165044 DUE DATE 15/FEB/22.; [02] REPAIRED FLOOR PANEL 241ZF AT AFT GALLEY AREA AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1; [03] REPAIRED FLOOR PANEL 2
- [SDR SWAA2021081297444](https://openairdocs.org/sdr/SWAA2021081297444.md): Floor Panel · delaminated · Jul 23, 2021 · N411WN · Boeing 7377H4 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 242WF AT AFT GALLEY AREA; 2021-311841 / [01] TOOL USED HOT BONDER P/N HCS9200B S/N 18165044 DUE DATE 15/FEB/22.; [02] TOOL USED SCALE P/N SCA-301 S/N AE-412122 DUE DATE 24/FEB/22.; [03] REPAIRED FLOOR PANEL 242WF AT AFT GALLEY AREA AS
- [SDR SWAA2021081196748](https://openairdocs.org/sdr/SWAA2021081196748.md): Battery Pack · inoperative · Jul 20, 2021 · N411WN · Boeing 7377H4 · Emergency Lighting
  > DONT WORK CORRECTLY LOWER SIDEWALL BATTERY PACK ON EMERGENCY EXIT DOOR AT PASSENGER CABIN (1 EA); 2021-311822 / [01] REPLACED LOWER SIDEWALL BATTERY PACK ON EMERGENCY EXIT DOOR AT PASSENGER CABIN (1 EA) IAW B737-700 AMM 33-51-06-960-805.; [02] REPLACED LOWER
- [SDR SWAA2021081296124](https://openairdocs.org/sdr/SWAA2021081296124.md): Floor Panel · delaminated · Jul 18, 2021 · N411WN · Boeing 7377H4 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 241ADF AT AFT GALLEY AND LAV; 2021-311814 / [01] TOOL USED: HOT BONDER P/N:HCS9200B S/N:15102320 DUE DATE:19-NOV-21; SCALE P/N:SCA-301 S/N:AE-412137 DUE DATE:24-FEB-22; [02] TOOL USED: SCALE P/N:SCA-301 S/N:AE-412125 DUE DATE: 24-FEB-2
- [SDR SWAA2021081294039](https://openairdocs.org/sdr/SWAA2021081294039.md): Floor Panel · delaminated · Jul 13, 2021 · N411WN · Boeing 7377H4 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL J23 PANEL ASSY P/N: 284A6223-1 AT EQUIPMENT EL ECTRONIC COMP; 2021-311795 / [01] TOOL USED: CALIPER PN: 500-464; SN: B17030925. DUE DATE: 06/AUG/21.; [02] TOOL USED: HOT BONDER P/N: HCS9200B SN: 18165044 DUE DATE: 15/FEB/22.; [03] TOOL
- [SDR SWAA2021081194037](https://openairdocs.org/sdr/SWAA2021081194037.md): Floorbeam · elongated · Jul 12, 2021 · N411WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > ELONGATED HOLE BS 294.5 ANGLE - SUPPORT BTW RBL 45 TO RBL 55; FLOOR STRUCTURE AREA AT FWD GALLEY AREA; 2021-311792 / [01] TOOLS USED: POWER PACK P/N: PE1068; S/N: PE0118-94826; DUE DATE: 23-FEB-22; MULTIMETER P/N: 2217-20; S/N: B83B914290479; DUE DATE: 14-APR
- [SDR SWAA2021081392848](https://openairdocs.org/sdr/SWAA2021081392848.md): Fitting · cracked · Jul 9, 2021 · N411WN · Boeing 7377H4 · Passenger/Crew Doors
  > CUSTOMER REQUEST CRACK LOWER FITTING FWD SERVICE DOOR AT FWD GALLEY AREA; 2021-311773 / [01] REPLACED FITTING I.A.W SRM B737-700 51-40-02; SRM B737-700 51-10-02 ITEM 9 AND DWG # 141A6535 REV B; [02] REPLACED FITTING I.A.W SRM B737-700 51-40-02; SRM B737-700 5
- [SDR SWAA2021081292842](https://openairdocs.org/sdr/SWAA2021081292842.md): Strap · cracked · Jul 8, 2021 · N411WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK STRAP LOCATED BS 420 TO BS 440 AND BETWEEN S-27R TO S-26L AT FWD CARGO COMPARTMENT; 2021-311714 / [01] REPLACED STRAP LOCATED BS420 TO BS440 AND BETWEEN S-27R TO S-26L AT FDW CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 AND SRM 51-40-02.; [02] REPLACED
- [SDR SWAA2021081292175](https://openairdocs.org/sdr/SWAA2021081292175.md): Support Angle · cracked · Jul 7, 2021 · N411WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE LOCATED BETWEEN BS 400 AND BS 380 BL 0 AT PASSENGER CABIN; 2021-311691 / [01] REPLACED SUPPORT ANGLE LOCATED BETWEEN BS 400 AND BS 380 BL 0 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02-0G-0. PARAGRAPH 9. AND DWG 143A5400 REV -.; [02] REPLA
- [SDR SWAA2021081292174](https://openairdocs.org/sdr/SWAA2021081292174.md): Web · cracked · Jul 7, 2021 · N411WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 320 LBL47 FWD GALLEY AND LAV; 2021-311689 / [01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND 320 LBL47 FWD GALLEY AND LAV. IAW SRM B737-700 51-10-02 AND DWG 141A5400
- [SDR SWAA2021081292176](https://openairdocs.org/sdr/SWAA2021081292176.md): Strap · corroded · Jul 7, 2021 · N411WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION INNER CHORD STRAP LOCATED BTW BS 294.5 TO BS 312 RBL 51 AND WL 208 AT FWD GALLEY AREA; 2021-311693 / [01] REPLACED INNER CHORD STRAP LOCATED BS 294.5 TO BS 312 RBL 51 AND WL 208 AT FWD GALLEY AREA IAW SRM B737-700 51-10-02 TEM 9 AND DRAWING 141A8310
- [SDR SWAA2021081192177](https://openairdocs.org/sdr/SWAA2021081192177.md): Web · cracked · Jul 7, 2021 · N411WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB LOCATED BTW BS 312 TO BS 328 RBL 29 AND WL 208 AT FWD GALLEY AREA; 2021-311694 / [01] REPLACED WEB LOC. BTW BS 312 TO BS 328 RBL 29 AND WL 208 AT FWD GALLEY AREA IAW SRM B737-700 51-10-02 AND DWG 141A5400 REV -; [02] JOB COMPLETED;RII ACCOMPLISHED.
- [SDR SWAA2021081192173](https://openairdocs.org/sdr/SWAA2021081192173.md): Floorbeam · cracked · Jul 7, 2021 · N411WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACK FLOOR BEAM BS 294.5 RBL 57 FWD GALLEY AND LAV; 2021-311692 / [01] TOOL USED: P/N: NORTEC 600 D; S/N: 210136503; DUE DATE: 05-MAR-22.; [02] PERFORMED PERMANENT REPAIR ON FLOOR BEAM BS 294.5 RBL 57 FWD GALLEY AND LAVATORY AREA IAW B737-700 SRM 53-10-51-2R

Next page: https://openairdocs.org/deregistered/N411WN-2025-09-29/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 = 'N411WN' AND deregistration_id = 'N411WN-2025-09-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N411WN-2025-09-29/reports

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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.
