# Service difficulty reports: N238WN, cancelled Jun 5, 2026

A list on [N238WN, cancelled Jun 5, 2026](https://openairdocs.org/deregistered/N238WN-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 · 273 reports

- [SDR SWAA2025120341772](https://openairdocs.org/sdr/SWAA2025120341772.md): Slide · dislodged · Dec 1, 2025 · N238WN · Boeing 7377H4 · Escape Slide
  > FWD ENTRY DOOR SLIDE FELL OUT OF DOOR COMPARTMENT. REINSTALLED FWD ENTRY IAW AMM 25-66-00 AND TASK CARD 725-61-06.
- [SDR SWAA2025111133130](https://openairdocs.org/sdr/SWAA2025111133130.md): Bracket · out of adjust · Nov 8, 2025 · N238WN · Boeing 7377H4 · Emergency Equipment
  > FORWARD SERVICE DOOR GIRT BAR WILL NOT STAY ARMED. ADJUSTED THE BRACKETS IAW SIP.
- [SDR SWAA2025091113291](https://openairdocs.org/sdr/SWAA2025091113291.md): Girt Bar · no discrepancy · Sep 9, 2025 · N238WN · Boeing 7377H4 · Emergency Equipment
  > FORWARD PROVISIONING DOOR LEFT SIDE GIRT BAR BRACKET ON SLIDE BROKEN. INSPECTED FORWARD SERVICE DOOR GIRT BAR LATCH AND BRACKET ATTACHMENTS. EVERYTHING IS INTACT. ADJUSTED GIRT BAR HOOKS. REF AMM 25-66-00. AC OK FOR SERVICE
- [SDR SWAA2025082909183](https://openairdocs.org/sdr/SWAA2025082909183.md): Lamp · inoperative · Aug 28, 2025 · N238WN · Boeing 7377H4 · Emergency Lighting
  > EMER LIGHT 3D INOPERATIVE. REMOVED AND REPLACED THE LAMPS IAW AMM 33-51-03-960-801-NG
- [SDR SWAA2025081198853](https://openairdocs.org/sdr/SWAA2025081198853.md): Hmu · failed · Aug 5, 2025 · N238WN · Boeing 7377H4 · Fuel Controlling System
  > NR 1 ENGINE FAILED UPON EXITING THE RUNWAY. SHUTDOWN ENG IAW QRH. R&R HMU;FUEL PUMP PACKAGE REF 773-11-00; R&R MW03102 HARNESS PER AMM 71-51-03; R&R J10;J6 HARNESS PER AM 73-21-06 R&R EEC PER AMM 73-21-60; OPS CK GOOD. C/W RII STEPS FOR HMU; FUEL PUMP PACK
- [SDR SWAA2025081100402](https://openairdocs.org/sdr/SWAA2025081100402.md): Pump · failed · Aug 5, 2025 · N238WN · Boeing 7377H4 · Engine Fuel Distribution
  > NR 1 ENGINE FAILED UPON EXITING THE RUNWAY. SHUTDOWN ENG IAW QRH. R&R HMU;FUEL PUMP PACKAGE REF 773-11-00; R&R MW03102 HARNESS PER AMM 71-51-03; R&R J10;J6 HARNESS PER AM 73-21-06 R&R EEC PER AMM 73-21-60; OPS CK GOOD. C/W RII STEPS FOR HMU; FUEL PUMP PACK
- [SDR SWAA2025081100403](https://openairdocs.org/sdr/SWAA2025081100403.md): Wire Harness · failed · Aug 5, 2025 · N238WN · Boeing 7377H4 · Engine Fuel System Wiring
  > NR 1 ENGINE FAILED UPON EXITING THE RUNWAY. SHUTDOWN ENG IAW QRH. R&R HMU;FUEL PUMP PACKAGE REF 773-11-00; R&R MW03102 HARNESS PER AMM 71-51-03; R&R J10;J6 HARNESS PER AM 73-21-06 R&R EEC PER AMM 73-21-60; OPS CK GOOD. C/W RII STEPS FOR HMU; FUEL PUMP PACKA
- [SDR SWAA2025081100404](https://openairdocs.org/sdr/SWAA2025081100404.md): Eec · failed · Aug 5, 2025 · N238WN · Boeing 7377H4 · Fuel Controlling System
  > NR 1 ENGINE FAILED UPON EXITING THE RUNWAY. SHUTDOWN ENG IAW QRH<[01] C/W. R&R HMU;FUEL PUMP PACKAGE REF 773-11-00; R&R MW03102 HARNESS PER AMM 71-51-03; R&R J10;J6 HARNESS PER AM 73-21-06 R&R EEC PER AMM 73-21-60; OPS CK GOOD. C/W RII STEPS FOR HMU; FUEL P
- [SDR SWAA2025031003751](https://openairdocs.org/sdr/SWAA2025031003751.md): Structure · cracked · Mar 9, 2025 · N238WN · Boeing 7377H4 · Leading Edge Devices
  > BIRD STRIKE ON CLIMBOUT. NOTED NO ABNORMAL SMELL IN COCKPIT.AS CLIMB CONTINUED; EGT ON #1 ENGINE CONTINUED TO RISE PAST 860 LARGE EGT SPLIT WITH OTHER ENGINE (+60 DIFF).RETURNED TO FLL THIS WAS AN AIR RETURN TO FLL UNABLE TO UPDATE RESULTING EVENTS DUE TO ERRO
- [SDR SWAA2025022597750](https://openairdocs.org/sdr/SWAA2025022597750.md): Handle · out of adjust · Feb 19, 2025 · N238WN · Boeing 7377H4 · Passenger/Crew Doors
  > L1 DOOR ASSIST HANDLE NEEDS SECURED <[01]. ADJUSTED L1 DOOR ASSIST HANDLE IAW B737-700 AMM 52-11-31-400-802-NG; [02] ADJUSTED L1 DOOR ASSIST HANDLE IAW B737-700 AMM 52-11-31-400-802-NG.
- [SDR SWAA2025022597747](https://openairdocs.org/sdr/SWAA2025022597747.md): Handle · loose · Feb 19, 2025 · N238WN · Boeing 7377H4 · Passenger/Crew Doors
  > L2 DOOR ASSIST HANDLE NEEDS SECURED <[01]. SECURED L2 DOOR ASSIST HANDLE IAW B737-700 AMM 52-13-31-400-802-NG (TOOL# T-0070023-0003); [02] SECURED L2 DOOR ASSIST HANDLE IAW B737-700 AMM 52-13-31-400-802-NG (TOOL# T-0070023-0003).
- [SDR SWAA2025022597751](https://openairdocs.org/sdr/SWAA2025022597751.md): Handle · loose · Feb 19, 2025 · N238WN · Boeing 7377H4 · Galley Doors
  > R1 DOOR AND AIRFRAME SIDE ASSIST HANDLES NEED SECURED <[01]. SECURED R1 DOOR AND AIRFRAME SIDE ASSIST HANDLES IAW B737-700 AMM 52-11-31-400-802-NG (TOOL# T-0070023-0003);[02] SECURED R1 DOOR AND AIRFRAME SIDE ASSIST HANDLES IAW B737-700 AMM 52-11-31-400-802-NG
- [SDR SWAA2024101447207](https://openairdocs.org/sdr/SWAA2024101447207.md): Circuit Breaker · tripped · Oct 10, 2024 · N238WN · Boeing 7377H4 · Equipment/Furnishings Wiring
  > ON DECENT ELECTRICAL SMELL IN AFT GALLEY. SELECTED GALLEY POWER OFF; SMELL DISSIPATED.<[01] C/W CONDITIONAL INSPECTION IAW AMM 05-51-56 & FIM 21-60 TASK 806. NO DEFECTS NOTED; DEACTIVATED AFT GALLEY COFFEE MAKERS AS PRECAUTIONARY. OK TO CONTINUE ON MEL 25-10-0
- [SDR SWAA2024071211614](https://openairdocs.org/sdr/SWAA2024071211614.md): Battery Pack · no test · Jul 12, 2024 · N238WN · Boeing 7377H4 · Emergency Lighting
  > M1673 FAILED CAPACITY CHECK<[01] R&R M1673 BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2024071211612](https://openairdocs.org/sdr/SWAA2024071211612.md): Battery Pack · no test · Jul 12, 2024 · N238WN · Boeing 7377H4 · Emergency Lighting
  > M1675 FAILED CAPACITY CHECK<[01] R&R M1675 BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2024071211613](https://openairdocs.org/sdr/SWAA2024071211613.md): Battery Pack · no test · Jul 12, 2024 · N238WN · Boeing 7377H4 · Emergency Lighting
  > M1672 FAILED CAPACITY CHECK<[01] R&R M1672 BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2024071211591](https://openairdocs.org/sdr/SWAA2024071211591.md): Stop Fitting · cracked · Jul 12, 2024 · N238WN · Boeing 7377H4 · Service Doors
  > FWD SERVICE DOOR AFT LOWER STOP FITTING CRACKED.<[01] REMOVED FWD SERVICE DOOR AND INSTALLED NEW DOOR UP TO AMM TASK 52-41-00 GALLEY SERVICE DOOR INSTALLATION STEP 3.F.(5)(G);[02] VERIFIED REMOVED FWD SERVICE DOOR AND INSTALLED NEW DOOR UP TO AMM TASK 52-41-00
- [SDR SWAA2024052890772](https://openairdocs.org/sdr/SWAA2024052890772.md): B-Nut · loose · May 20, 2024 · N238WN · Boeing 7377H4 · Hydraulic System, Main
  > #2 BRAKE LEAKING HYDRAULIC FLUID<[01] TIGHTENED B-NUT @ MLG BRAKE QUICK DISCONNECT PER AMM 32-41-11 LEAK CHECK GOOD. SERVICED B HYD SYS TO FULL PER AMM 12-12-00
- [SDR SWAA2024032666886](https://openairdocs.org/sdr/SWAA2024032666886.md): Door · cracked · Mar 23, 2024 · N238WN · Boeing 7377H4 · Landing Gear Doors
  > LEFT MLG CENTER GEAR DOOR CRACKED AT LWR FWD ATTACH POINT. CONFIGURED AIRCRAFT FOR GEAR SWING AND PULLED BREAKERS PER AMM 32-00-00; INSTALLED L/H GEAR CENTER DOOR PER AMM 32-13-11 UP TO FINAL ADJUSTMENTS. BONDING JUMPER REQUIRES SEALANT. LOCATED AND DR
- [SDR SWAA2024030559386](https://openairdocs.org/sdr/SWAA2024030559386.md): Module · fluctuates · Mar 3, 2024 · N238WN · Boeing 7377H4 · Flight Environment Data
  > AT FL400 AIRSPEED AND ALTITUDE INDICATIONS BEGAN TO FLUCTUATE AND DISAGREE FLAG. DETERMINED CA SIDE WAS UNRELIABLE/BAD. FO SIDE RELIABLE AND STANDBY RELIABLE. INTERMITTENT ON DESCENT AND ARRIVAL.<[01] R AND R LEFT STATIC AIR DATA MODULE PER AMM 34-21-04. REQUI
- [SDR SWAA2024030458535](https://openairdocs.org/sdr/SWAA2024030458535.md): Module · fluctuates · Mar 2, 2024 · N238WN · Boeing 7377H4 · Air Data Computer
  > FL390 A/S & ALT DISAGREE INDICATIONS WITH A/S & ALT FLUCUATIONS. DETERMINED CA SIDE WAS THE BAD SIDE. INDICATIONS CONTINUED THROUGH DESCENT. NO OVERWEIGHT LANDING.<[01] REMOVED AND REPLACED AIR DATA MODULE ON THE LH CAPT SIDE IAW AMM 34-21-01;[02] I DID NOT RE
- [SDR SWAA2024030458805](https://openairdocs.org/sdr/SWAA2024030458805.md): Module · fluctuates · Mar 2, 2024 · N238WN · Boeing 7377H4 · Air Data Computer
  > FL390 A/S & ALT DISAGREE INDICATIONS WITH A/S & ALT FLUCUATIONS. DETERMINED CA SIDE WAS THE BAD SIDE. INDICATIONS CONTINUED THROUGH DESCENT. NO OVERWEIGHT LANDING.<[01] REMOVED AND REPLACED AIR DATA MODULE ON THE LH CAPT SIDE IAW AMM 34-21-01;[02] I DID NOT RE
- [SDR SWAA2024030457268](https://openairdocs.org/sdr/SWAA2024030457268.md): Lamp · inoperative · Feb 29, 2024 · N238WN · Boeing 7377H4 · Emergency Lighting
  > L/H EMERGENCY EXIT GROUND ILLUMINATION LIGHT INOP<[01] REPLACED LAMP AND PERFORMED GOOD FUNCTIONAL TEST OF L/H EMERGENCY EXIT GROUND ILLUMINATION LIGHT PER AMM 33-51-04-960-801.;[02] VERIFIED CORRECTION ACTION ITEM 1 AND MEASUREMENT FIELD; CARD COMPLETE.
- [SDR SWAA2024030457267](https://openairdocs.org/sdr/SWAA2024030457267.md): Lamp · inoperative · Feb 29, 2024 · N238WN · Boeing 7377H4 · Emergency Lighting
  > L/H OWE EMERGENCY EXIT LOCATOR SIGN HAS INOP BULBS<[01] REPLACED LAMPS AND PERFORMED GOOD FUNCTIONAL CHECK OF L/H OWE EMERGENCY EXIT LOCATOR SIGN PER AMM 33-51-01-960-801.;[02] VERIFIED CORRECTION ACTION ITEM 1 AND MEASUREMENT FIELD; CARD COMPLETE.
- [SDR SWAA2024030456460](https://openairdocs.org/sdr/SWAA2024030456460.md): Battery Pack · inoperative · Feb 26, 2024 · N238WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1670 ARE INOP<[01] OK TO CLOSE SIDEWALL CARPET RISER.;[02] OK TO CLOSE GIVEN.;[03] REPLACED POWER SUPPLY - BATTERY PACK M1670 PER AMM 33-51-06-960-805. GOOD TEST.;[04] VERIFIED ITEM 3 COMPLETE.<BR>VERIFIED ME
- [SDR SWAA2024030453804](https://openairdocs.org/sdr/SWAA2024030453804.md): Scuff Plate · cracked · Feb 20, 2024 · N238WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR AFT CORNER SCUFF PLATE IS CRACKED<[01] REMOVED AND REPAIRED CRACK FCB CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER BAC5975.AND WILL BE INSTALL ON CUSTOMER CARD # TTG8Q00R6FRR.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. COMPLET
- [SDR SWAA2024030551057](https://openairdocs.org/sdr/SWAA2024030551057.md): Hinge Box · corroded · Feb 10, 2024 · N238WN · Boeing 7377H4 · Fuselage, Door Hinge
  > FWD ENTRY DOOR LOWER HINGE BOX IS CORRODED ON UPPER SURFACE COMMON TO OUTBOARD; AFT BOLT HOLE FOR BEARING PLATE<[01] REMOVED CORROSION ON LOWER HINGE BOX FOUND TO BE OUT OF LIMITS REPAIRED BY REPLACEMENT IAW SRM 51-10-02; SRM 53-10-15-1A-1; SRM 51-40-02; SRM 5
- [SDR SWAA2024030449329](https://openairdocs.org/sdr/SWAA2024030449329.md): Intercostal · cracked · Feb 6, 2024 · N238WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > BS 295 INTERCOSTAL AT STR 15L CRACKED; IB RADIUS<[01] REMOVED AND INSTALLED NEW INTERCOSTAL PER SRM 51-40-02 AND DWG 141A8180
- [SDR SWAA2024030548060](https://openairdocs.org/sdr/SWAA2024030548060.md): Former · cracked · Feb 2, 2024 · N238WN · Boeing 7377H4 · Leading Edge Devices
  > L/H FAIRING FORMER I/B OF #2 K-FLAP IS CRACKED AT UPPER FASTENER (MARKED)<[01] REMOVED AND REPLACED LEFT WING FAIRING FORMER ON I/B FIXED L/E; BS 500D IAW SRM 51-40-02 AND DWG 116A3010; DWG 116A3110; DWG149A7101;[02] CORRECTED MEASUREMENT ENTRY #3.
- [SDR SWAA2024030447950](https://openairdocs.org/sdr/SWAA2024030447950.md): Intercostal · cracked · Feb 2, 2024 · N238WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > BS 295 INTERCOSTAL AT STR 16L CRACKED; IB RADIUS; MARKED<[01] REMOVED AND REPLACED INTERCOSTAL ON BS295 TO BS 303.8 STR 16L IAW SRM 51-40-02 AND DWG 141A8180;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.
- [SDR SWAA2024030547290](https://openairdocs.org/sdr/SWAA2024030547290.md): Support Bracket · broken · Feb 1, 2024 · N238WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CABLE ATTACH ANGLE SUPPORT BRACKET BROKEN; BS 685+8; RB 24.5; WL 204.<[01] REMOVED AND REPLACED ATTACH ANGLE SUPPORT BRACKET I.A.W SRM 51-10-02-0G-0; SRM 51-40-02-0G-0 AND DWG 27A9110.;[02] JOB COMPLETE.;[03] JOB COMPLETE
- [SDR SWAA2024030547292](https://openairdocs.org/sdr/SWAA2024030547292.md): Web · corroded · Feb 1, 2024 · N238WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > REJECT; ADDITIONAL CORROSION EXIST ON WEB BS 1016+11; LBL 4; WL208; ADJACENT TO TENSION STRAP ON UPPER SURFACE.<[01] REMOVED AND REPLACED WEB IN TTG8Q00R9MW3;[02] VERIFIED CORRECTIVE ACTIONS STEP 1.
- [SDR SWAA2024030547294](https://openairdocs.org/sdr/SWAA2024030547294.md): Sidewall Support · corroded · Feb 1, 2024 · N238WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO BAY LH FLOOR-TO-SIDEWALL SUPPORT AT WL 156; LBL 24; BS 494; BS 500+4 TO 500A; AND BS 500B+5 TO 500C+11<[01] ALL PROCESS WILL BE CLOSED WITH TASK CARD #TTG8Q00RA74Z.;[02] VERIFIED CORRECTIVE ACTION ITEM 1; MEASUREMENTS TABLE OK; CARD COMP
- [SDR SWAA2024030547295](https://openairdocs.org/sdr/SWAA2024030547295.md): Sidewall Support · corroded · Feb 1, 2024 · N238WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO BAY RH FLOOR-TO-SIDEWALL SUPPORT AT WL 156; RBL 24; BS 500B+14; BS 500C+10; AND BS 500C+14<[01] REMOVED AND REPLACED ON FWD CARGO BAY RH FLOOR-TO-SIDEWALL SUPPORT AT WL 156; RBL 24; BS 500A - 500D. IAW BOEING 737-700 SRM 51-40-02; & DWG
- [SDR SWAA2024030547298](https://openairdocs.org/sdr/SWAA2024030547298.md): Shield · corroded · Feb 1, 2024 · N238WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO DOORWAY AFT SHIELD AT RBL 24; WL 156; BS 500+6; AND BS 500+13 TO 500+18<[01] VERIFIED STEP 2; COMPLETE; STEP 2 IN PARTIAL; OK TO APPLY COAT AND CIC GIVEN.;[02] REMOVED AND REPLACED AFT SHIELD;RBL24;WL156 IAW DWG#143A0080 AND SRM 51-40-02
- [SDR SWAA2024030547296](https://openairdocs.org/sdr/SWAA2024030547296.md): Sidewall Support · corroded · Feb 1, 2024 · N238WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO BAY RH FLOOR-TO-SIDEWALL SUPPORT AT WL 156; RBL 24; BS 414<[01] VERIFIED STEP 3 IN PARTIAL.;[02] REMOVED; FABRICATED AND INSTALLED FWD CARGO BAY RH FLOOR TO SIDEWALL SUPPORT AT WL 156; RBL 24; BS 396 - BS 420 IAW SRM 51-40-02; DGW 143
- [SDR SWAA2024030547300](https://openairdocs.org/sdr/SWAA2024030547300.md): Shield · corroded · Feb 1, 2024 · N238WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION OF FWD CARGO DOORWAY FWD SHIELD AT RBL 24; WL 156; BS 426<[01] REMOVED AND REPLACED ON FWD. CARGO DOORWAY FWD. SHIELD AT WL 156; RBL 24; BS. 420 - BS.440 IAW BOEING 737-700 SRM 51-40-02; & DWG# 143A0080.
- [SDR SWAA2024030547302](https://openairdocs.org/sdr/SWAA2024030547302.md): Sidewall Support · corroded · Feb 1, 2024 · N238WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO BAY LH FLOOR-TO-SIDEWALL SUPPORT AT WL 156; LBL 24; BS 458; AND BS 466 TO 479<[01] REMOVED AND REPLACED LH FLOOR TO SIDEWALL SUPPORT AT LBL24;WL156 FROM BS396 TO BS500D;IAW SRM 51-40-02.;[02] VERIFIED COMPLETE STEP 5; MEASUREMENTS TABLE
- [SDR SWAA2024030547685](https://openairdocs.org/sdr/SWAA2024030547685.md): Sidewall Support · corroded · Feb 1, 2024 · N238WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO LH SIDEWALL SUPPORT SECTION FROM BS 727F TO 787 HAS MULTIPLE CORROSION AROUND NUTPLATE HOLES; WL 150; LBL 21.0<[01] VERIFIED STEP 9 COMPLETE; STEP 10 IN PARTIAL.;[02] REMOVED AND REPLACE (1EA.) ZEE CHANNEL SIDEPLATE AT ACB BETWENN BS 727E+10 - BS 847
- [SDR SWAA2024030547686](https://openairdocs.org/sdr/SWAA2024030547686.md): Sidewall Support · corroded · Feb 1, 2024 · N238WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO RH FLOOR TO SIDEWALL SUPPORT FROM BS 727D TO 767 HAS MULTIPLE CORROSION AROUND NUTPLATE HOLES; WL 150.6; RBL 21.0 [TTG8Q00R9J22]<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT P/N 146A7502-51; LOT#1553581-1 LOCATED AT ACB BETWEEN BS.727 - BS.767
- [SDR SWAA2024030547548](https://openairdocs.org/sdr/SWAA2024030547548.md): Floorbeam · corroded · Feb 1, 2024 · N238WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > WHILE WORKING CUST. CARD TTG8Q00R9ETN CORROSION FOUND ON LOWER FLANGE AT BS986.5 FLOORBEAM AT NUTPLATE HOLE RBL 40 WL 208.<[01] 'REFER TO FAULT TTG8Q00R9ETN WHERE EA 24-153-00319 WAS ADDED AS A SUBTASK.';[02] JOB COMPLETE.
- [SDR SWAA2024030447687](https://openairdocs.org/sdr/SWAA2024030447687.md): Shield · corroded · Feb 1, 2024 · N238WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD AFT CARGO DOOR SHIELD HAS CORROSION IN MULTIPLE PLACES BS 767-787+3; WL 150; RBL 21<[01] REMOVED AND REPLACED FWD AFT CARGO DOOR SHIELD AT WL 150; RBL 21; BS 767 - BS 787+6; IAW SRM 51-40-02 AND DWG 146A0081.;[02] VERIFIED CORRECTIVE ACTION ITEM 1; MEASURE
- [SDR SWAA2024030547091](https://openairdocs.org/sdr/SWAA2024030547091.md): Floorbeam · corroded · Jan 31, 2024 · N238WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION ON BS 986 FLOOR BEAM AT NUTPLATE HOLE RBL 42; WL 208<[01] UPDATED LINE 22 OF MEASUREMENTS TABLE - PHOTOGRAPH IS NOT AVAILABLE OF THE CORROSION.;[02] UPDATED STEP'S 7 AND 8;[03] ACCOPLISHED BS 986 FLOOR BEAM AT NUTPLATE HOLE RBL 42 REPAIR PEER EA#24-1
- [SDR SWAA2024030547092](https://openairdocs.org/sdr/SWAA2024030547092.md): Floorbeam · corroded · Jan 31, 2024 · N238WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION ON BS 986 FLOOR BEAM AT NUTPLATE HOLE LBL 42; WL 208<[01] REPAIRED BS 986 FLOOR BEAM AT NUTPLATE HOLE LBL 42; WL 208 PER REF SRM 53-70-51-2R-6;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2024030547277](https://openairdocs.org/sdr/SWAA2024030547277.md): Web · corroded · Jan 31, 2024 · N238WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT PASSENGER CABIN 1016 WEB HAS CORROSION AT BS 1016 - 1016+16; LBL 6 - 29; WL 208<[01] REMOVED AND INSTALLED NEW SHEAR WEB PER SRM 51-40-02-0G-0 AND DWG#147A5600;[02] VERIFIED STEPS 3;7; COMPLETE.;[03] VERIFIED ALL STEPS AND MEASUREMENT TABLE COMPLETE; CARD
- [SDR SWAA2024030547278](https://openairdocs.org/sdr/SWAA2024030547278.md): Strap · corroded · Jan 31, 2024 · N238WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT PASSENGER CABIN 1016 TENSION STRAP HAS CORROSION AT BS 1016 - 1016+14; LBL 3; WL 208<[01] REMOVED AND REPLACED TENSION STRAP BS 1016; LBL 3; WL 208<BR>IAW SRM 51-40-02 & DWG 147A5600;[02] CORRECTED MEASUREMENT FIELD;[03] JOB COMPLETE.
- [SDR SWAA2024030547283](https://openairdocs.org/sdr/SWAA2024030547283.md): Intercostal · corroded · Jan 31, 2024 · N238WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD PASSENGER CABIN INTERCOSTAL IS CORRODED COMMON TO ATTACH FITTING AT BS 294.5 + 10; LBL 13; WL 208<[01] REMOVED AND INSTALLED ON FWD PASSENGER CABIN INTERCOSTAL BS 294.5 TO BS 312 LBL 13 IAW SRM 51-40-02 AND DWG 141A5600;[02] VERIFIED CORRECTIVE ACTION ENTR
- [SDR SWAA2024022647280](https://openairdocs.org/sdr/SWAA2024022647280.md): Strap · corroded · Jan 31, 2024 · N238WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT PASSENGER CABIN 1016 TENSION STRAP HAS CORROSION AT BS 1016 + 10 - 1016 + 14; RBL 17 -18; WL 208<[01] REMOVED AND REPLACED BS1016 TENSION STRAP AT RBL 17 IAW SRM 51-40-02 AND IAW DGW#147A5730;[02] JOB COMPLETE.
- [SDR SWAA2024030546405](https://openairdocs.org/sdr/SWAA2024030546405.md): Panel · cracked · Jan 30, 2024 · N238WN · Boeing 7377H4 · Wing, Plate/Skin
  > LT WING T/E PANEL 561AB AFT ROW OF FASTENER HOLES HAVE CRACKS AROUND THEM<[01] PANEL 561AB FASTENER HOLES HAVE BEEN REPAIRED IAW SRM 51-70-04-2R-9.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] JOB COMPLETE.
- [SDR SWAA2024030546419](https://openairdocs.org/sdr/SWAA2024030546419.md): Panel · cracked · Jan 30, 2024 · N238WN · Boeing 7377H4 · Wing, Plate/Skin
  > RT WING T/E PANEL 661CB AFT ROW OF FASTENER HOLES HAS HOLES WITH CRACKS AROUND THEM<[01] PANEL 661CB FASTENER HOLES HAVE BEEN REPAIRED IAW SRM 51-70-04-2R-9.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] JOB COMPLETE.

Next page: https://openairdocs.org/deregistered/N238WN-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 = 'N238WN' AND deregistration_id = 'N238WN-2026-06-05'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N238WN-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.