# Service difficulty reports: N235WN, cancelled Jun 5, 2026

A list on [N235WN, cancelled Jun 5, 2026](https://openairdocs.org/deregistered/N235WN-2026-06-05.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 · 280 reports

- [SDR SWAA2025120441472](https://openairdocs.org/sdr/SWAA2025120441472.md): Battery · no test · Dec 2, 2025 · N235WN · Boeing 7377H4 · Emergency Lighting
  > AFT RIGHT EMERGENCY LIGHTING BATTERY PACK FAILED A CAPACITY CHECK. REMOVED & REPLACED THE BATTERY IAW MM 33-51-06.
- [SDR SWAA2025070387876](https://openairdocs.org/sdr/SWAA2025070387876.md): Lamp · inoperative · Jul 3, 2025 · N235WN · Boeing 7377H4 · Emergency Lighting
  > FWD SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED IAW MM 33-51-04.
- [SDR SWAA2025062785436](https://openairdocs.org/sdr/SWAA2025062785436.md): Lamp · inoperative · Jun 25, 2025 · N235WN · Boeing 7377H4 · Emergency Lighting
  > LEFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] RELAMPED IAW AMM 33-51-03
- [SDR SWAA2025041122644](https://openairdocs.org/sdr/SWAA2025041122644.md): Handle · broken · Apr 8, 2025 · N235WN · Boeing 7377H4 · Flight Compartment Windows
  > F/O PILOT ASSIST HANDLE BROKEN<[01] R&R F/O SEAT ASSIST HANDLE PER AMM 20-50-11
- [SDR SWAA2025020492495](https://openairdocs.org/sdr/SWAA2025020492495.md): Cover · out of adjust · Feb 3, 2025 · N235WN · Boeing 7377H4 · Emergency Lighting
  > PLASTIC EXIT ROW COVER FELL OFF AFTER LANDING<[01] RE-INSTALL PLASTIC EXIT ROW I.A.W AMM 11-32-01.
- [SDR SWAA2024080822699](https://openairdocs.org/sdr/SWAA2024080822699.md): Wire Harness · disconnected · Aug 5, 2024 · N235WN · Boeing 7377H4 · Engine Fuel System Wiring
  > RED BOX ON SHUTDOWN IN #2 ENG. EGT REDLINE LIMIT EXCEEDED ON TAKEOFF. DISCONNECTED A/T AND REDUCED THRUST; NO FURTHER INDICATIONS.<[01] T/S PER FIM 71-06 TASK 805 AND ACCOMPLISHED EA M-21-177-01860. FOUND CJ10 HARNESS; S3; AND S4 EGT PROBES FAILING RESISTANCE
- [SDR SWAA2024080823958](https://openairdocs.org/sdr/SWAA2024080823958.md): Probe · failed · Aug 5, 2024 · N235WN · Boeing 7377H4 · Cylinder Head Temperature (CHT) Indicating System
  > RED BOX ON SHUTDOWN IN #2 ENG. EGT REDLINE LIMIT EXCEEDED ON TAKEOFF. DISCONNECTED A/T AND REDUCED THRUST; NO FURTHER INDICATIONS.<[01] T/S PER FIM 71-06 TASK 805 AND ACCOMPLISHED EA M-21-177-01860. FOUND CJ10 HARNESS; S3; AND S4 EGT PROBES FAILING RESISTANCE
- [SDR SWAA2024062505471](https://openairdocs.org/sdr/SWAA2024062505471.md): Egt Indication · activated · Jun 24, 2024 · N235WN · Boeing 7377H4 · Engine Indicating System
  > ON T/O #2 ENGINE EGT HAD AN EXCEEDENCE; EGT OF 960 FOR 5 SEC'S EGT GAUGE TURNED RED. PULLED POWER BACK & EGT RETURNED TO LIMITS. PER THE ENGINE EXCEEDENCE PAGE THE #2 ENGINE EXCEEDENCE WAS 958 DEGREES FOR 2 SECONDS & FOUND TO BE IN ZONE A ACCOMPLISHED A VISUAL
- [SDR SWAA2024061801469](https://openairdocs.org/sdr/SWAA2024061801469.md): Handle · loose · Jun 14, 2024 · N235WN · Boeing 7377H4 · Passenger/Crew Doors
  > FWD ENTRY DOOR HANDLE RATTLES WHEN DOOR IS CLOSED<[01] RETIGHTEN FWD ENTRY DOOR HANDLE AS REQUIRED REF. AMM 52-11-31.
- [SDR SWAA2024061801470](https://openairdocs.org/sdr/SWAA2024061801470.md): Girt Bar · out of adjust · Jun 14, 2024 · N235WN · Boeing 7377H4 · Emergency Equipment
  > FWD GALLEY SERVICE DOOR; SLIDE GIRT IS NOT PROPERLY PACKED<[01] REPACKED FWD SERVICE DOOR SLIDE GIRT PROPERLY REF. AMM 25-66-00.;[02] REPACKED FWD SERVICE DOOR SLIDE GIRT PROPERLY REF. AMM 25-66-01 AND MT 725-61-06.
- [SDR SWAA2024011639815](https://openairdocs.org/sdr/SWAA2024011639815.md): Light · inoperative · Jan 10, 2024 · N235WN · Boeing 7377H4 · Emergency Lighting
  > RIGHT HAND EMERGENCY EXIT GROUND ILLUMINATION LIGHT IS INOP<[01] RELAMPED R/H EMERGENCY EXIT GROUND ILLUMINATION LIGHT AND PERFORMED GOOD INSTALLATION TEST PER AMM 33-51-04-960-801;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE
- [SDR SWAA2024011639220](https://openairdocs.org/sdr/SWAA2024011639220.md): Battery Pack · inoperative · Jan 9, 2024 · N235WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ASSOCIATED WITH EMERGENCY BATTERY PACK M1669 INOP<[01] REPLACED EMERGENCY EXIT BATTERY PACK M1669 AND PERFORMED GOOD TEST PER AMM 33-51-06-960-806.;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
- [SDR SWAA2024011639217](https://openairdocs.org/sdr/SWAA2024011639217.md): Battery Pack · inoperative · Jan 9, 2024 · N235WN · Boeing 7377H4 · Emergency Lighting
  > MULTIPLE EMERGENCY EXIT LIGHTS ASSOCIATED WITH EMERGENCY BATTERY PACK M1674 INOP<[01] REPLACED BATTERY PACK M1674 AND PERFORMED GOOD TEST PER AMM 33-51-06-960-806.;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
- [SDR SWAA2024011639219](https://openairdocs.org/sdr/SWAA2024011639219.md): Light · inoperative · Jan 9, 2024 · N235WN · Boeing 7377H4 · Emergency Lighting
  > AFT SERVICE DOOR SLIDE LIGHT IS INOP<[01] RELAMPED AFT SERVICE DOOR SLIDE LIGHT AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-04-960-801.;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.<BR>JOB COMPLETE.
- [SDR SWAA2024011737606](https://openairdocs.org/sdr/SWAA2024011737606.md): Shield · corroded · Jan 3, 2024 · N235WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > PERFORM RII BUYBACK OF FWD CARGO AFT SHIELD HAS CORROSION AT BS 500+5 - 500+16; RBL 24; WL 208 [TTG8Q00QAH7R]<[01] UPDATED MEASUREMENTS;[02] PERFORMED RII BUYBACK OF FWD CARGO BAY AFT SHIELD INSTALLATION PER DGW#143A0080 AND SRM 51-40-02. VERIFIED MEASUREMENT
- [SDR SWAA2024011636727](https://openairdocs.org/sdr/SWAA2024011636727.md): Intercostal · corroded · Dec 31, 2023 · N235WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY WEB AT BS 827-847 STRINGER 27 R/H<[01] REMOVED AND REPLACED ACB INTERCOSTAL FROM BS 827 TO BS 847 RBL 6 WL 156 IAW SRM 51-40-02-0G-0 AND DWG# 146A8130 AND DWG # 146A8131;[02] VERIFIED CORRECTIVE ACTION ITEMS; AND MEASUREMENT FIELDS C
- [SDR SWAA2024011633879](https://openairdocs.org/sdr/SWAA2024011633879.md): Scuff Plate · cracked · Dec 19, 2023 · N235WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FORWARD CORNER SCUFF PLATE IS CRACKED<[01] AFT CARGO BAY FORWARD CORNER SCUFF PLATE REPAIRED PER SRM 53-60-15-2R-1.;[02] CORRECTED MEASUREMENT LINE ITEM 3;[03] VERIFIED CORRECTIVE ACTION #1<BR>VERIFIED MEASUREMENTS
- [SDR SWAA2024011633670](https://openairdocs.org/sdr/SWAA2024011633670.md): Floor Panel · pulled · Dec 19, 2023 · N235WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 221CF UPPER SURFACE HAS PULLED STRAND OF FIBERGLASS.<[01] REPAIRED FWD FLOOR PANEL 221CF UPPER SURFACE PULLED STRAND OF FIBERGLASS IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1<BR>VERIFIED MEASUREMENTS
- [SDR SWAA2024011633671](https://openairdocs.org/sdr/SWAA2024011633671.md): Floor Panel · delaminated · Dec 19, 2023 · N235WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 221CF LOWER SURFACE HAS AREAS OF DELAMINATION.<[01] REPAIRED FWD FLOOR PANEL 221CF LOWER SURFACE DELAMINATION IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1<BR>VERIFIED MEASUREMENTS
- [SDR SWAA2024011633672](https://openairdocs.org/sdr/SWAA2024011633672.md): Floor Panel · delaminated · Dec 19, 2023 · N235WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 222AF UPPER SURFACE HAS AREAS OF DELAMINATION.<[01] REPAIRED FWD FLOOR PANEL 222AF UPPER SURFACE DELAMINATION IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1. JOB COMPLETE.
- [SDR SWAA2024011633673](https://openairdocs.org/sdr/SWAA2024011633673.md): Floor Panel · delaminated · Dec 19, 2023 · N235WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 222AF LOWER SURFACE HAS AREAS OF DELAMINATION.<[01] REPAIRED FWD FLOOR PANEL 222AF LOWER SURFACE DELAMINATION IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1. JOB COMPLETE.
- [SDR SWAA2024011633476](https://openairdocs.org/sdr/SWAA2024011633476.md): Frame · cracked · Dec 19, 2023 · N235WN · Boeing 7377H4 · Fuselage Main, Frame
  > STATION 312 FRAME IS CRACKED IN RADIUS ABOVE L1 DOOR CUT-OUT.<[01] THE UPPER CORD OF THE BS312 FRAME WAS REPAIRED PER REF EA M-22-153-01244;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE
- [SDR SWAA2024011633439](https://openairdocs.org/sdr/SWAA2024011633439.md): Support Angle · cracked · Dec 18, 2023 · N235WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > LEFT WING; T/E COVE SEAL SUPPORT ANGLE CRACKED ABOVE #1 PYLON AFT TIP<[01] REMOVED AND REPLACED LEFT WING; T/E COVE SEAL SUPPORT ANGLE ABOVE #1 PYLON AFT TIP IAW SRM 51-40-02 AND AIPC 57-50-00-25.;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREME
- [SDR SWAA2024011633454](https://openairdocs.org/sdr/SWAA2024011633454.md): Scuff Plate · cracked · Dec 18, 2023 · N235WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR AFT CORNER SCUFF PLATE IS CRACKED<[01] AFT CARGO DOOR AFT CORNER SCUFF PLATE REPAIRED PER SRM 53-60-15-2R-1.;[02] CORRECTED MEASUREMENT LINE ITEM 3;[03] VERIFIED CORRECTIVE ACTION #1<BR>VERIFIED MEASUREMENTS
- [SDR SWAA2024011632520](https://openairdocs.org/sdr/SWAA2024011632520.md): Floor Panel · pulled · Dec 16, 2023 · N235WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 231FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231FF 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.;[02] PANEL REPLACED. JOB COMPLETE
- [SDR SWAA2024011632521](https://openairdocs.org/sdr/SWAA2024011632521.md): Floor Panel · pulled · Dec 16, 2023 · N235WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 231MF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231MF 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.;[02] PANEL REPLACED. JOB COMPLETE
- [SDR SWAA2024011632522](https://openairdocs.org/sdr/SWAA2024011632522.md): Floor Panel · pulled · Dec 16, 2023 · N235WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241UF 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.;[02] PANEL REPLACED. JOB COMPLETE
- [SDR SWAA2024011632518](https://openairdocs.org/sdr/SWAA2024011632518.md): Bracket · cracked · Dec 15, 2023 · N235WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > PULLEY SUPPORT BEAM CRACKED ON L-BRACKET AT BS 697; LBL 0.5; WL 207. (MARKED)<[01] STEP 2 COMPLETE OK TO APPLY CONVERSION COAT AND PRIME;[02] STEP 3 COMPLETE;[03] REMOVED AND REPLACED L-BRACKET AT BS 697; LBL 0.5; WL 207 PER REF SRM 51-40-02 AND DWG NBR 273A91
- [SDR SWAA2024011632253](https://openairdocs.org/sdr/SWAA2024011632253.md): Flange · corroded · Dec 15, 2023 · N235WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD R/H MOP SILL VERTICAL FLANGE FROM STA 294 TO STA 330; RBL 54 TO RBL 59; WL 208.9.<[01] REMOVED AND REPLACED ON FWD R/H MOPSILL BS 260 TO BS 360 RBL 59 IAW SRM 51-40-02 AND DWG 141A8310;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEAS
- [SDR SWAA2024011632251](https://openairdocs.org/sdr/SWAA2024011632251.md): Floor Support · cracked · Dec 15, 2023 · N235WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT STA 277+10; BL 0; WL 208.1.<[01] REMOVED AND REPLACED NEW INTERCOSTAL ITEM 141A5410-3 IAW SRM 51-40-02 AND DWG 141A5400;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2024011632393](https://openairdocs.org/sdr/SWAA2024011632393.md): Scuff Plate · cracked · Dec 15, 2023 · N235WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FCB AFT CORNER SCUFF PLATE IS CRACKED<[01] APPLIED A CHEMICAL CONVERSION COATING TO THE BARE ALUMINUM SURFACES PER SOPM 20-43-03; TYPE 2; CLASS A OR C AND SRM 53-30-15-2R-1 AND APPLY TWO LAYERS OF BMS 10-11;TYPE 1 PRIMER TO THE INNER SURFACES OF THE CORNER SCU
- [SDR SWAA2024011631806](https://openairdocs.org/sdr/SWAA2024011631806.md): Floor Panel · pulled · Dec 14, 2023 · N235WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 221AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221AF 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.;[02] PANEL REPLACED. JOB
- [SDR SWAA2024011631807](https://openairdocs.org/sdr/SWAA2024011631807.md): Floor Panel · pulled · Dec 14, 2023 · N235WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 221BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221BF 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.;[02] PANEL REPLACED. JOB
- [SDR SWAA2024011631815](https://openairdocs.org/sdr/SWAA2024011631815.md): Floor Panel · pulled · Dec 14, 2023 · N235WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 221GF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] 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.;[02] VERIFIED CORRECTIVE
- [SDR SWAA2024011631812](https://openairdocs.org/sdr/SWAA2024011631812.md): Floor Panel · pulled · Dec 14, 2023 · N235WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 222CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AREAS OF PULLED STRANDS ON UPPER SKIN OF FWD FLOOR PANEL 222CF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.
- [SDR SWAA2024011631816](https://openairdocs.org/sdr/SWAA2024011631816.md): Floor Panel · pulled · Dec 14, 2023 · N235WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241DF HAS PULLED STRANDS.<[01] DUE TO EXTENT OF THE DAMAGE ON PASSENGER CABIN FLOOR PANEL 241DF FABRICATED NEW PANEL FROM BMS4-17 TYPE 6 LOT#1544951-1; LOCATED AND INSTALLED INSERTS USING BMS5-107 LOT#AK3BA2380A/A; CURED USING HEAT
- [SDR SWAA2024011631820](https://openairdocs.org/sdr/SWAA2024011631820.md): Floor Panel · pulled · Dec 14, 2023 · N235WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241FF HAS PULLED STRANDS.<[01] VERIFIED STEP 1;2 AND THE MEASUREMENT TABLE.;[02] PASSENGER CABIN FLOOR PANEL 241FF WITH PULLED STRANDS WAS BEYOND ECONOMICAL REPAIR. PANEL WAS REPLACED BY FABRICATING A NEW ONE IAW SRM 53-00-50-2R-0 A
- [SDR SWAA2024011631818](https://openairdocs.org/sdr/SWAA2024011631818.md): Floor Panel · pulled · Dec 14, 2023 · N235WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 242CF HAS PULLED INSERT.<[01] VERIFIED STEP 1;2 AND THE MEASUREMENT TABLE.;[02] PASSENGER CABIN FLOOR PANEL 242CF WITH A PULLED INSERT WAS BEYOND ECONOMICAL REPAIR. PANEL WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0
- [SDR SWAA2024011631821](https://openairdocs.org/sdr/SWAA2024011631821.md): Floor Panel · pulled · Dec 14, 2023 · N235WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241AAF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241AAF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS BEYOND ECONOMICAL REPAIR. A NEW PANEL WAS FABRICATED IAW SRM 53-00-50-2R-0 AND BOEING DWG 147A5810 ID: 0008.;[02] VERIFIED CO
- [SDR SWAA2024011631823](https://openairdocs.org/sdr/SWAA2024011631823.md): Floor Panel · pulled · Dec 14, 2023 · N235WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241ADF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ADF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.;[02] VERIFIED FLOOR PANEL 241ADF WAS REPAIRED PER SRM 53-00-50-2R-1.;[03] WORKSCOPE COMPLETE.
- [SDR SWAA2024011631824](https://openairdocs.org/sdr/SWAA2024011631824.md): Floor Panel · pulled · Dec 14, 2023 · N235WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 242TF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242TF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.;[02] VERIFIED FLOOR PANEL 242TF REPAIRED PER SRM 53-00-50-2R-1.;[03] WORKSCOPE COMPLETE.
- [SDR SWAA2024011631827](https://openairdocs.org/sdr/SWAA2024011631827.md): Floor Panel · pulled · Dec 14, 2023 · N235WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 242UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242UF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.;[02] VERIFIED FLOOR PANEL 242UF WAS REPAIRED PER SRM 53-00-50-2R-1.;[03] WORKSCOPE COMPLETE
- [SDR SWAA2024011631828](https://openairdocs.org/sdr/SWAA2024011631828.md): Floor Panel · pulled · Dec 14, 2023 · N235WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242VF UPPER SKIN; AREAS OF PULLED STRANDS; WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED FLOOR PANEL 242VF WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2024011632239](https://openairdocs.org/sdr/SWAA2024011632239.md): Frame · corroded · Dec 14, 2023 · N235WN · Boeing 7377H4 · Fuselage Main, Frame
  > AFT CABIN WET AREA FRAME HAS CORROSION AT FASTENER HOLE; BS 986; LBL 44; WL 208<[01] REMOVED AND REPLACED REPAIR PARTS PER SEM 51-40-02 AS SHOW IN SWA EA#1-753-32297 REV IR (ESR#23-02724);[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.
- [SDR SWAA2024011632244](https://openairdocs.org/sdr/SWAA2024011632244.md): Web · corroded · Dec 14, 2023 · N235WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR CENTER THRESHOLD HAS CORROSION AT BS 440+10 - 480+4; RBL 28; WL 208<[01] REMOVED AND REPLACED THRESHOLD WEB AT FCB BS 440- 492.4; RBL 28; WL 156.IAW SRM 51-40-02.;[02] VERIFIED MEASUREMENTS FIELD
- [SDR SWAA2024011632245](https://openairdocs.org/sdr/SWAA2024011632245.md): Shield · corroded · Dec 14, 2023 · N235WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO AFT SHIELD HAS CORROSION AT BS 500+5 - 500+16; RBL 24; WL 208<[01] REMOVED AND REPLACED AFT SHIELD;IAW DWG#143A0080 AND SRM 51-40-02.;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.
- [SDR SWAA2024011632246](https://openairdocs.org/sdr/SWAA2024011632246.md): Sidewall Support · corroded · Dec 14, 2023 · N235WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 767-727E; RBL 22; WL 156<[01] REMOVED AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02 AN DWG 146A7500.;[02] VERIFIED MEASUERMENT TABLE.;[03] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2024011632243](https://openairdocs.org/sdr/SWAA2024011632243.md): Sidewall Support · corroded · Dec 14, 2023 · N235WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 727D - 744; LBL 22; WL 156<[01] CORRECTION TOM MEASUREMENT #1;[02] REMOVED AND REPLACED LH SIDEWALL SUPPORT FROM BS727 TO BS847;LBL22 WL156;IAW DGW#146A7500 REV A AND SRM 51-40-02.;[03] VERIFIED CORRECTIV
- [SDR SWAA2024011632247](https://openairdocs.org/sdr/SWAA2024011632247.md): Sidewall Support · corroded · Dec 14, 2023 · N235WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 747+9 - 787; LBL 22; WL 157<[01] THIS TASK CARD WILL BE COMPLETED WITH CARD #TTG8Q00QAFFY.;[02] VERIFIED ITEM 1 COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.
- [SDR SWAA2024011632003](https://openairdocs.org/sdr/SWAA2024011632003.md): Frame · corroded · Dec 14, 2023 · N235WN · Boeing 7377H4 · Fuselage Main, Frame
  > FWD CABIN WET AREA FRAME HAS CORROSION AT FASTENER HOLES; BS 294.5; RBL 7; WL 208 CLARIFICATION THIS IS THE BS 294 FLOOR BEAM=FWD CABIN WET AREA FRAME HAS CORROSION AT FASTENER HOLES; BS 294.5; RBL 7; WL 208<[01] TASK CARD IS COMPLETE;[02] FWD CABIN WET AREA F

Next page: https://openairdocs.org/deregistered/N235WN-2026-06-05/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 = 'N235WN' AND deregistration_id = 'N235WN-2026-06-05'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N235WN-2026-06-05/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.