# Service difficulty reports: N423WN, cancelled Feb 18, 2026

A list on [N423WN, cancelled Feb 18, 2026](https://openairdocs.org/deregistered/N423WN-2026-02-18.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 7 · 320 reports

- [SDR SWAA2025120843022](https://openairdocs.org/sdr/SWAA2025120843022.md): Girt Bar · out of position · Dec 5, 2025 · N423WN · Boeing 7377H4 · Emergency Equipment
  > AFT ENTRY DOOR SLIDE GIRT BAR HANGS LOW. REPACKED AFT ENTRY DOOR SLIDE GIRT BAR IAW AMM 25-66-01.
- [SDR SWAA2025071490655](https://openairdocs.org/sdr/SWAA2025071490655.md): Valve · faulty · Jul 11, 2025 · N423WN · Boeing 7377H4 · Brake Anti-Skid Section
  > ANTI-SKID AND PARKING BRAKE LIGHTS ILLUMINATED ON TAKEOFF. REMOVED AND REPLACED ANTI-SKID VALVE PER AMM. 32-42-31. OPS AND LEAK CHECK SATISFACTORY. REF# TTG8Q013P7MC CONDITIONAL INSPECTION. REMOVED AND REPLACED PARKING BRAKE VALVE ON NON-ROUTINE REF. TTG8Q01
- [SDR SWAA2025071490656](https://openairdocs.org/sdr/SWAA2025071490656.md): Door · cracked · Jul 11, 2025 · N423WN · Boeing 7377H4 · Landing Gear Doors
  > LH MLG INNER DOOR CRACKED. REMOVED AND REPLACED LEFT MLG INNER DOOR PER AMM. 32-13-11. ADJUSTMENT AND TEST SATISFACTORY.
- [SDR SWAA2025071090038](https://openairdocs.org/sdr/SWAA2025071090038.md): Slide · out of adjust · Jul 10, 2025 · N423WN · Boeing 7377H4 · Escape Slide
  > FWD ENTRY DOOR SLIDE OUT OF POSITION<[01] C/W ESCAPE SLIDE PACK CHECK AND REPOSITIONED GIRT BAR IAW AMM 25-66-01
- [SDR SWAA2025071089637](https://openairdocs.org/sdr/SWAA2025071089637.md): Holder · loose · Jul 9, 2025 · N423WN · Boeing 7377H4 · Emergency Equipment
  > AFT CARGO DOOR GIRT BAR HOLDER LOOSE<[01] ADJUSTED R2 SERVICE DOOR GIRT BAR HOLDER TENSON PER SIP. PILOT WRITEUP SHOULD OF BEEN FOR R2 NOT AFT CARGO
- [SDR SWAA2025061180253](https://openairdocs.org/sdr/SWAA2025061180253.md): Lamp · inoperative · Jun 10, 2025 · N423WN · Boeing 7377H4 · Emergency Lighting
  > R/H EMERGENCY DOOR WINDOW LIGHT INOP. INSTALLED NEW LAMP ON R/H EMERGENCY DOOR LIGHT PER AMM 33-21-00.
- [SDR SWAA2025050265796](https://openairdocs.org/sdr/SWAA2025050265796.md): Screw · missing · Apr 29, 2025 · N423WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > F/A ADISED- AFT GALLEY SERVICE DOOR(CAPT) - SCREW MISSING ON FLOOR GIRT PLATE<[01] INSTALLED MISSING FASTERNER PER AMM 20-50-11
- [SDR SWAA2025022700128](https://openairdocs.org/sdr/SWAA2025022700128.md): Bulb · inoperative · Feb 27, 2025 · N423WN · Boeing 7377H4 · Emergency Lighting
  > AFT RH EXTERIOR EMERGENCY LIGHT INOP <[01]. RELAMPED AFT R/H SERVICE DOOR; EXTERIOR EMERGENCY LIGHT BULB REF AMM 33-51-04. OPS CHECK GOOD AT THIS TIME.
- [SDR SWAA2025010883853](https://openairdocs.org/sdr/SWAA2025010883853.md): Door · cracked · Jan 8, 2025 · N423WN · Boeing 7377H4 · Landing Gear Doors
  > RIGHT MAIN LANDING GEAR CENTER DOOR CRACKED/BENT HANGAR REQUEST RECORD #3626<[01] OK TO CONTINUE PER CDL 32-10-3. SP1B. AUTH # 231834.;[02] OK TO CONTINUE PER CDL 32-10-3. SP1B. AUTH # 231834.
- [SDR SWAA2024120974795](https://openairdocs.org/sdr/SWAA2024120974795.md): Attach Bolt · loose · Dec 6, 2024 · N423WN · Boeing 7377H4 · Emergency Equipment
  > L2 SERVICE DOOR RAFT COMPARTMENT LOOSE<[01] SECURED L2 SLIDE COMPARTMENT ATTACH BOLTS PER AMM 20-50-11.
- [SDR SWAA2024120974631](https://openairdocs.org/sdr/SWAA2024120974631.md): Girt Bar · out of position · Dec 6, 2024 · N423WN · Boeing 7377H4 · Emergency Equipment
  > L2 GIRT BAR NEED ATTENTION<[01] REPOSITIONED FLAP FOR SLIDE PER AMM 25-66-01. CK GOOD
- [SDR SWAA2024101146532](https://openairdocs.org/sdr/SWAA2024101146532.md): Cable · out of position · Oct 9, 2024 · N423WN · Boeing 7377H4 · Escape Slide
  > FWD SERVICE DOOR ESCAPE SLIDE COVER HAS WIRE CABLE EXTENDING OUTSIDE OF COVER<[01] REPOSITIONED FWD SERVICE DOOR ESCAPE SLIDE COVER<BR>REF. SIP
- [SDR SWAA2024082931046](https://openairdocs.org/sdr/SWAA2024082931046.md): Extinguisher · low pressure · Aug 26, 2024 · N423WN · Boeing 7377H4 · Fire Bottle, Portable
  > COCKPIT HALON FIRE EXTINGUISHER UNDER CHARGED<[01] R&R COCKPIT HALON FIRE EXTINGUISHER PER AMM 26-26-01. <BR>A&P 3125606
- [SDR SWAA2024080723479](https://openairdocs.org/sdr/SWAA2024080723479.md): Slide · dislodged · Aug 6, 2024 · N423WN · Boeing 7377H4 · Escape Slide
  > FWD ENTRY DOOR ESCAPE SLIDE FELL OUT OF CONTAINER<[01] R&R FWD ENTRY SLIDE PER MT#725-61-06-FE.
- [SDR SWAA2024052388696](https://openairdocs.org/sdr/SWAA2024052388696.md): Battery · no test · May 21, 2024 · N423WN · Boeing 7377H4 · Emergency Equipment
  > FWD CABIN MEGAPHONE INOP. REPLACED BATTERIES ON FWD CABIN MEGAPHONE & OPS CKD O.K. PER AMM 25-64-00
- [SDR SWAA2024052187862](https://openairdocs.org/sdr/SWAA2024052187862.md): Anti-Skid Valve · faulty · May 20, 2024 · N423WN · Boeing 7377H4 · Brake Anti-Skid Section
  > ANTI-SKID INOP LIGHT ILLUMINATED COMPLETED QRH<[01] PERFORMED ANTISKID/AUTOBRAKE CONTROL UNITE BITE PER FIM 32-42 TASK 801 FOUND VLV 2 FAULT C/W FIM 32-42 TASK 804 <BR>REMOVED AND REPLACED LEFT INBOARD V7 ANTISKID VALVE PER AMM 32-42-31 OPS CHECK GOOD
- [SDR SWAA2024041574008](https://openairdocs.org/sdr/SWAA2024041574008.md): Hook · loose · Apr 12, 2024 · N423WN · Boeing 7377H4 · Emergency Equipment
  > FLIGHT ATTENDANT REPORTS FWD ENTRY BRACKET FOR SLIDE IS LOOSE<[01] REPLACED RIVET IN GIRT BAR STOW HOOK ON L-1 DOOR PER <BR>MM 25-66-00
- [SDR SWAA2024012444019](https://openairdocs.org/sdr/SWAA2024012444019.md): Handle · loose · Jan 23, 2024 · N423WN · Boeing 7377H4 · Passenger/Crew Doors
  > BOTH GRAB HANDLES ON AFT SERVICE DOOR ARE LOOSE<[01] INSTALLED ASSIST HANDLE IAW AMM 52-41-31-400-802 STEP F (2) SUBTASK 52-41-31-020-008.;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE
- [SDR SWAA2024012443117](https://openairdocs.org/sdr/SWAA2024012443117.md): Battery Pack · no test · Jan 20, 2024 · N423WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1669 FAIL TEST<[01] REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK M1669; PERFORMED GOOD TEST PER AMM 33-51-06-960-805;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE
- [SDR SWAA2024012540626](https://openairdocs.org/sdr/SWAA2024012540626.md): Baffle · cracked · Jan 13, 2024 · N423WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > BAFFLE UNDER L/H FLOOR TO SIDEWALL SUPPORT IS CRACKED AT BS 440-460 LBL 25 WL 156<[01] REMOVED AND REPLACED BAFFLE UNDER L/H FLOOR TO SIDEWALL SUPPORT AT BS 440-460 LBL 25 WL 156 PER REF SRM 51-40-02 AND DWG 143A7500;[02] JOB COMPLETE.;[03] CORRECTED MEASUREME
- [SDR SWAA2024012440711](https://openairdocs.org/sdr/SWAA2024012440711.md): Hinge Bracket · cracked · Jan 13, 2024 · N423WN · Boeing 7377H4 · Fuselage, Door Hinge
  > PANEL 834 DZ AFT ENTRY DOOR LOWER HINGE AFT BRACKET IS CRACKED<[01] REMOVED AND REPLACED AFT ENTRY DOOR PNL 834DZ AFT BRACKET IAW BOEING DWG 411A2119 SHT 72 AND SRM 51-40-02-0G-0;[02] VERIFIED CORRECTIVE ACTION STEP 1. VERIFIED MEASUREMENTS TABLE AND TASK CARD
- [SDR SWAA2024012539765](https://openairdocs.org/sdr/SWAA2024012539765.md): Shield · corroded · Jan 10, 2024 · N423WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD SHIELD AT ACB BS767 - BS787 RBL22 WL157.<[01] REMOVED AND REPLACED ON FWD SHIELD AT ACB BS 767 TO BS 794 RBL 22 IAW SRM 51-40-02 AND DWG 146A0081;[02] VERIFIED COMPLETE<BR>VERIFIED MEASUREMENTS.
- [SDR SWAA2024012439766](https://openairdocs.org/sdr/SWAA2024012439766.md): Sidewall Support · corroded · Jan 10, 2024 · N423WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - BS767 RBL21 WL156.<[01] REMOVED AND REPLACED AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT ANGLE BS 727 - BS 767; RBL 21; WL 156 IAW SRM 51-40-02-0G-0 AND DWG#146A7500.;[02] VERIFIED CORRECTIVE ACTIONS. JOB C
- [SDR SWAA2024012439767](https://openairdocs.org/sdr/SWAA2024012439767.md): Sidewall Support · corroded · Jan 10, 2024 · N423WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - BS767 LBL21 WL156.<[01] REMOVED AND REPLACED ACB FLOOR/SIDEWALL SUPPORT IAW SRM 51-40-02 <BR>& DWG146A7500; BS727-BS847; LBL21; WL156.;[02] VERIFIED CORRECTIVE ACTIONS. JOB COMPLETE.;[03] VERIFIED CORRECTIV
- [SDR SWAA2024012439768](https://openairdocs.org/sdr/SWAA2024012439768.md): Sidewall Support · corroded · Jan 10, 2024 · N423WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FCB BS400 - BS420 RBL22 WL156.<[01] REMOVED CORROSION L=1.0 W=1.0 D=.002 MATERIAL REMAINING.038' MATERIAL ORIGINAL THICKNESS.040' FOUND TO BE WITHING LIMITS PER SRM 53-00-53-1A-2;[02] VERIFIED MEASUREMENTS TABLE
- [SDR SWAA2024012439769](https://openairdocs.org/sdr/SWAA2024012439769.md): Sidewall Support · corroded · Jan 10, 2024 · N423WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FCB BS400 - BS500D LBL22 WL156.<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT FCB BS400-500D LBL22;WL156;IAW SRM 51-40-02.;[02] UPDATED PARTS USAGE;[03] VERIFIED CORRECTIVE ACTION. <BR><BR>VERIFIED MEASUREMENT
- [SDR SWAA2024012439770](https://openairdocs.org/sdr/SWAA2024012439770.md): Sidewall Support · corroded · Jan 10, 2024 · N423WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FCB BS500A - BS500D RBL22 WL156.<[01] REMOVED AND REPLACED FWD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT ANGLE BS500A - BS500D; RBL22; WL156 IAW SRM 51-40-02-0G-0 AND DWG# 143A7500;[02] JOB COMPLETE.
- [SDR SWAA2024012439772](https://openairdocs.org/sdr/SWAA2024012439772.md): Shield · corroded · Jan 10, 2024 · N423WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT SHIELD AT FCB BS500 - BS500A RBL23 WL156.<[01] REMOVED AND REPLACED ON AFT SHIELD AT FCB BS 492 TO BS 500A RBL 23 IAW SRM 51-40-02 AND DWG 143A0080;[02] VERIFIED THE MEASUREMENT TABLE;[03] VERIFIED REPLACEMENT OF THE AFT SHIELD IN THE FWD CARG
- [SDR SWAA2024012639334](https://openairdocs.org/sdr/SWAA2024012639334.md): Skin · cracked · Jan 9, 2024 · N423WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > LH HORIZONTAL STABILIZER LOWER SKIN -.5' CRACK FOUND 10' FROM FWD EDGE AT STA 193.90<[01] ACCOMPLISHED REPAIR PER SRM 55-10-01-2R-11 REPAIR 11;[02] VERIFIED CARD COMPLETE. VERIFIED MEASUREMENT TABLE.
- [SDR SWAA2024012539337](https://openairdocs.org/sdr/SWAA2024012539337.md): Threshold · corroded · Jan 9, 2024 · N423WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION: SUB THRESHOLD; BS793-795; RBL 29-32; WL156; MARKED<[01] REMOVED AND REPLACED SUB THRESHOLD; BS793-795; RBL 29-32; WL156; PER REF SRM 51-40-02 AND DWG 146A8120;[02] VERIFIED CORRECTIVE ACTION. JOB COMPLETE.<BR><BR>VERIFIED MEASUREMENTS.
- [SDR SWAA2024012439433](https://openairdocs.org/sdr/SWAA2024012439433.md): Guide Plate · corroded · Jan 9, 2024 · N423WN · Boeing 7377H4 · Passenger/Crew Doors
  > FWD ENTRY DOOR GUIDE PLATE HAS CORROSION ON LOWER SURFACE<[01] RECEIVED NEW FWD ENTRY DOOR GUIDE PLATE. PLATE TO BE INSTALLED ON TC# TTG8Q00QSVW8;[02] VERIFIED CORRECTIVE ACTION STEP 1. VERIFIED MEASUREMENTS TABLE AND TASK CARD COMPLETE.
- [SDR SWAA2024012938096](https://openairdocs.org/sdr/SWAA2024012938096.md): Panel · cracked · Jan 5, 2024 · N423WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MID CABIN; WING CENTER SECTION; BREAK PANEL IS CRACKED AT BS 540; LBL 1; WL 208<[01] REMOVED AND INSTALLED NEW PANEL BREAK<BR>IAW SRM 51-40-02 & DWG 143A0060<BR>BS 540; LBL 1; WL 208;[02] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2024012938095](https://openairdocs.org/sdr/SWAA2024012938095.md): Panel · cracked · Jan 5, 2024 · N423WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MID CABIN; WING CENTER SECTION; BREAK PANEL IS CRACKED AT BS 540; RBL 1; WL 208<[01] REMOVED AND INSTALLED NEW PANEL BREAK<BR>IAW SRM 51-40-02 & DWG 143A0060<BR>BS 540; RBL 1; WL 208;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
- [SDR SWAA2024012338285](https://openairdocs.org/sdr/SWAA2024012338285.md): Shelf · corroded · Jan 5, 2024 · N423WN · Boeing 7377H4 · Buffet/Galleys
  > G1 GALLEY IS CORRODED ON THE SHELF UNDER THE COFFEE MAKER<[01] PARTIALLY COMPLETED STEPS 1 AND 2.;[02] STEP 2: INSTALLATION(PARTIAL);[03] STEP 2: INSTALLATION(PARTIAL);[04] STEP 2 COMPLETE;[05] PARTIAL STEPS 1 AND 5;[06] REMOVED AND REPLACED G1 GALLEY IAW AMM
- [SDR SWAA2024012537874](https://openairdocs.org/sdr/SWAA2024012537874.md): Stringer · cracked · Jan 4, 2024 · N423WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK FOUND IN FWD CARGO BAY AT STR 25L; AFT OF AFT FASTENER; BS 520+19<[01] TASK COMPLETED;[02] UPDATED STEP 11 TO PARTIAL.;[03] CUTED AND REMOVED THE DAMAGED PART OF THE STRINGER 25L BS 520+19;PEROFERMED HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION OF THE R
- [SDR SWAA2024012437483](https://openairdocs.org/sdr/SWAA2024012437483.md): Floor Panel · pulled · Jan 4, 2024 · N423WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231ZF WITH PULLED UPPER SKIN STRANDS WAS REPLACED BY FABRICATING NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0011.;[02] VERIFIED CORRECTIVE ACTION #1<BR>VERIFIED MEASUREMENTS
- [SDR SWAA2024012437486](https://openairdocs.org/sdr/SWAA2024012437486.md): Floor Panel · pulled · Jan 4, 2024 · N423WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 232RF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] REPLACED FLOOR PANEL 232RF WITH PULLED STRANDS BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0004.;[02] VERIFIED CORRECTIVE ACTION ITEM 1 AND MEASUREMENTS TABLE.
- [SDR SWAA2024012437487](https://openairdocs.org/sdr/SWAA2024012437487.md): Floor Panel · pulled · Jan 4, 2024 · N423WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241BF UPPEER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241BF WITH PULLED UPPER SKIN STRANDS WAS REPLACED BY FABRICATING NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0037.;[02] VERIFIED CORRECTIVE ACTION #1<BR>VERIFIED MEASUREMENTS
- [SDR SWAA2024012437484](https://openairdocs.org/sdr/SWAA2024012437484.md): Floor Panel · pulled · Jan 4, 2024 · N423WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOR PANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] REPLACED FLOOR PANEL 242AF WITH PULLED STRANDS BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0004.;[02] DRAWING NUMBER ENTERED IN ERROR; FABRICATED BOARD IAW DWG 144A5810 ID:0
- [SDR SWAA2024012437488](https://openairdocs.org/sdr/SWAA2024012437488.md): Floor Panel · pulled · Jan 4, 2024 · N423WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 242CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242CF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION 1.<BR>V
- [SDR SWAA2024012437485](https://openairdocs.org/sdr/SWAA2024012437485.md): Floor Panel · pulled · Jan 4, 2024 · N423WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 242DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATE FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION 1.<BR>VE
- [SDR SWAA2024012437033](https://openairdocs.org/sdr/SWAA2024012437033.md): Battery Pack · no test · Jan 2, 2024 · N423WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY BATTERIES PACKS M1674; M1675; M1672 AND M1673FAIL CAPACITY TEST EMERGENCY BATTERIES PACKS M1674 M1675 M1672 AND M1673FAIL CAPACITY TEST<[01] REMOVED AND REPLACED BATTERY PACKS M1672; M1673; M1674 & M1675 PER AMM 33-51-06-960-805.;[02] VERIFIED CORREC
- [SDR SWAA2023113025845](https://openairdocs.org/sdr/SWAA2023113025845.md): Battery Pack · inoperative · Nov 29, 2023 · N423WN · Boeing 7377H4 · Emergency Lighting
  > LH ENTRANCE DOOR; ROW 1 ABC; AND ROW 4 ABC EMERGENCY LIGHTS COME ON MOMENTARILY THEN GO OFF.<[01] REPLACED FWD LH EMERGENCY BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD.
- [SDR SWAA2023062772136](https://openairdocs.org/sdr/SWAA2023062772136.md): Light · failed · Jun 27, 2023 · N423WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT SWITCH IN AFT GALLEY IS ILLUMINATED RED<[01] RESET EMERGENCY EXIT LIGHT SWITCH IN AFT GALLEY; RED LIGHT EXTINGUISHED. OPS CHECK GOOD IAW SIP 33-51-00
- [SDR SWAA2023061960421](https://openairdocs.org/sdr/SWAA2023061960421.md): Floor Panel · cracked · Jun 17, 2023 · N423WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD CARGO COMPARTMENT FLOOR PANEL 120 CF HAS 11.5 CRACK<[01] REMOVED AND REPLACED FORWARD CARGO COMPARTMENT FLOOR PANEL 120CF IN REFERENCE TO AIRCRAFT MAINTENANCE MANUAL 25 - 52 - 01 - 201 - 801 - NG
- [SDR SWAA2023040322831](https://openairdocs.org/sdr/SWAA2023040322831.md): Slide · loose · Mar 31, 2023 · N423WN · Boeing 7377H4 · Escape Slide
  > R2 DOOR SLIDE LOOSE<[01] REPOSITIONED AFT SERVICE DOOR SLIDE AS PER MT 725-61-06
- [SDR SWAA2023032118756](https://openairdocs.org/sdr/SWAA2023032118756.md): Slide · out of rig · Mar 20, 2023 · N423WN · Boeing 7377H4 · Escape Slide
  > L1 SLIDE PACK CAME OUT OF PACK ASSEMBLY<[01] INSTALLED SLIDE PACK PER AMM 25-66-01 AND MT 725-61-06
- [SDR SWAA2022120678709](https://openairdocs.org/sdr/SWAA2022120678709.md): Lens · broken · Dec 6, 2022 · N423WN · Boeing 7377H4 · Emergency Lighting
  > RIGHT WING OUTSIDE EMERGENCY EXIT LIGHT LENS JUST AFT OF THE OVERWING EXIT DOOR LENS BROKEN. / [01] REMOVED AND REPLACED LENS ASSEMBLY PER 33-51-04 AMM AND S.I.P.
- [SDR SWAA2022101459151](https://openairdocs.org/sdr/SWAA2022101459151.md): None · loose · Oct 13, 2022 · N423WN · Boeing 7377H4 · Trailing Edge Flap Control System
  > RIGHT WING O/B AFT FLAP #7 FLAP TRACK LOOSE AT ATTACH POINT. / [01] REMOVED AND REPLACED O/B #7 AFT FLAP TRACK PER AMM 27-51-26.
- [SDR SWAA2022101459153](https://openairdocs.org/sdr/SWAA2022101459153.md): None · loose · Oct 13, 2022 · N423WN · Boeing 7377H4 · Trailing Edge Flap Control System
  > RIGHT WING O/B AFT FLAP #8 FLAP TRACK LOOSE AT ATTACH POINT. / [01] REMOVED AND REPLACED RIGHT WING O/B AFT FLAP #8 FLAP TRACK PER AMM 27-51-26. OPERATIONAL CHECKS GOOD.

Next page: https://openairdocs.org/deregistered/N423WN-2026-02-18/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 = 'N423WN' AND deregistration_id = 'N423WN-2026-02-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N423WN-2026-02-18/reports

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