# Service difficulty reports: N231WN

A list on [N231WN](https://openairdocs.org/aircraft/N231WN.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 · 263 reports

- [SDR SWAA2026010859145](https://openairdocs.org/sdr/SWAA2026010859145.md): Pump · failed · Jan 7, 2026 · N231WN · Boeing 7377H4 · Engine Fuel Pump
  > ON TAKEOFF ROLL, NR 1 ENGINE ONLY PRODUCED 80.7% N1 WITH 85% COMMANDED, NR 2 WAS NORMAL. EECS WERE ON. NO CAUTIONS OR WARNINGS. AIRBORNE NR 1 WOULD ONLY PRODUCE 83.3% AT 5000'. WHEN BACK AT THE GATE, NR 1 WOULD NOT SHUT DOWN ON ITS COMMAND TO CUTOFF. IT DID
- [SDR SWAA2025120430768](https://openairdocs.org/sdr/SWAA2025120430768.md): Web · cracked · Nov 1, 2025 · N231WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED WEB, BTW BS 500D - 520, STRINGER 28L, FWD CARGO BAY. REPLACED THE WEB AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7902, SHEET 126, REV A.
- [SDR SWAA2025120430916](https://openairdocs.org/sdr/SWAA2025120430916.md): Support Angle · cracked · Nov 1, 2025 · N231WN · Boeing 7377H4 · Leading Edge Devices
  > CRACKED SUPPORT ANGLE AT AUXILIARY TRACK SLAT 8, INBD, RT WING. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 114A5010, SHEET 6, REV D. MEASUREMENT OF CRACK: 2.022.
- [SDR SWAA2025120433606](https://openairdocs.org/sdr/SWAA2025120433606.md): Tee Angle · perforated · Nov 1, 2025 · N231WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > PERFORATION ON TEE ANGLE, BTW BS540 - 559, RBL 40 IN THE AIR CONDITIONING BAY. PERFORMED REPAIR ON THE TEE ANGLE IAW SRM 57-10-13-2R-3, REPAIR 3.
- [SDR SWAA2025120430765](https://openairdocs.org/sdr/SWAA2025120430765.md): Stringer · corroded · Nov 1, 2025 · N231WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 24R, BS 540, RBL 40, WL 160, IN FWD CARGO. PERFORMED PERMANENT REPAIR ON THE STRINGER IAW SRM 53-00-03-2R-1, REPAIR 1.
- [SDR SWAA2025120430767](https://openairdocs.org/sdr/SWAA2025120430767.md): Angle · cracked · Nov 1, 2025 · N231WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE, BS 663.75 BTW LBL 6.15 & LBL 15.54. IN AIR CONDITIONING BAY. REPLACED THE ANGLEIAW SRM 51-40-02, AND DWG 111A1000, SHEET 190, REV-, AND DWG 111A1000, SHEET 192, REV-.
- [SDR SWAA2025120430766](https://openairdocs.org/sdr/SWAA2025120430766.md): Angle · cracked · Nov 1, 2025 · N231WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE AFT FACE, BS 500D, STR 28L, FWD CARGO BAY, REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7902, SHEET 126, REV A.
- [SDR SWAA2025120430914](https://openairdocs.org/sdr/SWAA2025120430914.md): Support Bracket · cracked · Nov 1, 2025 · N231WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT BRACKET ON PNEUMATIC DUCT LOCATED BS 540, LBL 6 IN AIR CONDITIONING BAY. REPLACED SUPPORT BRACKET ON PNEUMATIC DUCT IAW SOPM 20-50-01, REV 39, AND DWG 212A1101, SHEET 3.
- [SDR SWAA2025120430613](https://openairdocs.org/sdr/SWAA2025120430613.md): Strap · corroded · Oct 31, 2025 · N231WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORRODED STRAP, WL154 BETWEEN BS 794 - 794 + 5 INCHES, RBL 21 IN AFT CARGO BAY. REPLACED THE STRAP AND FASTENERS IAW SRM 51-40-02-0G-0 AND DWG 146A8340, SHEET 21, REV-.
- [SDR SWAA2025120430610](https://openairdocs.org/sdr/SWAA2025120430610.md): Support · corroded · Oct 31, 2025 · N231WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORRODED SUPPORT ZEE, WL 156 BETWEEN BS 727C + 10 INCHES - BS 787 + 10 INCHES, LBL 22, S25L IN THE AFT CARGO BAY. PERFORMED REPAIR ON THE SUPPORT, BS 727+4 TO BS 847 IAW SRM 53-00-53-2R-6, REPAIR 6.
- [SDR SWAA2025120430612](https://openairdocs.org/sdr/SWAA2025120430612.md): Web · corroded · Oct 31, 2025 · N231WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORRODED SHIELD WEB, WL156 BETWEEN BS 767 - 794, RBL 22, S25R IN AFT CARGO. REPLACED THE SHIELD WEB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 146A0081, SHEET 31, REV -.
- [SDR SWAA2025120430614](https://openairdocs.org/sdr/SWAA2025120430614.md): Sill Drain · corroded · Oct 31, 2025 · N231WN · Boeing 7377H4 · Fuselage Main, Structure
  > CORRODED LOWER SILL DRAIN, WL 156, BS 794 - 847, RBL 22, S25R IN THE AFT CARGO BAY. REPLACED THE LOWER SILL DRAIN IAW SRM 51-40-02, AND DWG 146A8340, SHEET 21, REV -.
- [SDR SWAA2025120430617](https://openairdocs.org/sdr/SWAA2025120430617.md): Nut Plate · cracked · Oct 31, 2025 · N231WN · Boeing 7377H4 · Wing, Attach Fittings
  > CRACK RAIL NUT PLATES, LEADING EDGE INTERNAL CAVITY LOCATED OF SS 499, LT WING. REPLACED RAIL NUT PLATES ON LEADING EDGE INTERNAL CAVITY LOCATED OFSS499, LT WING; IAW 51-40-02, DWG 112A4402, SHEET 13, REV - CRACK LENGTH: 0.449 IN.
- [SDR SWAA2025120330615](https://openairdocs.org/sdr/SWAA2025120330615.md): Intercostal · corroded · Oct 31, 2025 · N231WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORRODED WEB, INTERCOSTAL LOCATED WL 154, BS 794 - 847, RBL 21 IN THE AFT CARGO BAY. REPLACED THE WEB - INTERCOSTAL AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 146A8120, SHEET 34, REV -.
- [SDR SWAA2025120330611](https://openairdocs.org/sdr/SWAA2025120330611.md): Support · corroded · Oct 31, 2025 · N231WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED WL 156 BETWEEN BS 727 - 767, RBL 22, S25R IN THE AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE IAW SRM 51-40-02, & DWG 146A7500, SHEET 85, REV A.
- [SDR SWAA2025120430196](https://openairdocs.org/sdr/SWAA2025120430196.md): Rib · cracked · Oct 30, 2025 · N231WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACKED INSPAR RIB, HSS 120.30 29 INCHES FROM SPAR, LT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON INSPAR RIB LOCATED STAB STA 120.30 29 INCHES OF FROM SPAR LT HORIZONTAL STAB IAW B737-700 EA 25-155-03220-WIP1 SUMMARY EA 25-155-03220.
- [SDR SWAA2025120429810](https://openairdocs.org/sdr/SWAA2025120429810.md): Strap · corroded · Oct 29, 2025 · N231WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CORROSION OTBD FRONT SPAR LOWER STRAP OF SS 345, RT WING. REPAIRED OUTBOARD FRONT SPAR LOWER STRAP OFSS 345 AT RT WING IAW EA 25-157-03068-WIP1; EA EA 25-157-03068-WIP2 AND EA 25-157-03068.
- [SDR SWAA2025120429803](https://openairdocs.org/sdr/SWAA2025120429803.md): Stub Frame · cracked · Oct 29, 2025 · N231WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACKED LOWER STUB FRAME, BS 294.5, STR 17R IN THE FWD GALLEY. REPLACED THE STUB FRAME AND FASTENERS IAW SRM 51-40-02-0G, SRM 51-10-02, ITEM 9, DWG 141A8370, SHEET 9, SHEET 10, REV D, DRAWING 141A8430, SHEET 4, REV B, AND DRAWING 141A8380, SHEET 22, REV -.
- [SDR SWAA2025120429812](https://openairdocs.org/sdr/SWAA2025120429812.md): Tie Clip · cracked · Oct 29, 2025 · N231WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED TIE CLIP, BS 277, STR 10R. REPLACED THE TIE CLIP AND FASTENERS IAW SRM 51-40-02, AND SRM 51-10-02, ITEM 9, AND DWG 141A1110, SHEET 17, REV-.
- [SDR SWAA2025120429807](https://openairdocs.org/sdr/SWAA2025120429807.md): Angle · cracked · Oct 29, 2025 · N231WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE, BS 294.5, STR 13L IN THE FWD GALLEY AREA. REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 141A1311, SHEET 1, REV C.
- [SDR SWAA2025120430008](https://openairdocs.org/sdr/SWAA2025120430008.md): Support Angle · cracked · Oct 29, 2025 · N231WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE ON BODY FAIRING SUPPORT STRUCTURE BS 500D, STRINGER 19L LOWER FUSELAGE. REPLACED SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, AND DWG 116A3010, SHEET 39, REV -, DWG 149A7101, SHEET 7, REV -.
- [SDR SWAA2025120429804](https://openairdocs.org/sdr/SWAA2025120429804.md): Access Panel · elongated · Oct 29, 2025 · N231WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > ELONGATED HOLES ON ACCESS PANEL 343BB, RT HORIZONTAL STAB. REPAIRED ACCESS PANEL 343BB, RT HORIZONTAL STAB IAW SRM 51-70-04-2R-9, REPAIR 9.
- [SDR SWAA2025120429806](https://openairdocs.org/sdr/SWAA2025120429806.md): Access Panel · elongated · Oct 29, 2025 · N231WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLES ON ACCESS PANEL 661BB TRAILING EDGE ON THE RT WING. REPAIRED ACCESS PANEL 661BB IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2025120429674](https://openairdocs.org/sdr/SWAA2025120429674.md): Seal Plate · cracked · Oct 28, 2025 · N231WN · Boeing 7377H4 · Nacelle/Pylon Miscellaneous Structure
  > CRACK SEAL PLATE LOCATED ON ACCESS PANEL 434CL ON LT PYLON. REPLACED SEAL PLATE ON ACCESS PANEL 434CL IAW SRM 51-10-02, ITEM 9, AND SRM 51-40-02.
- [SDR SWAA2025120429673](https://openairdocs.org/sdr/SWAA2025120429673.md): Access Panel · elongated · Oct 28, 2025 · N231WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLES ON ACCESS PANEL 561BB TRAILING EDGE ON THE LT WING. REPAIRED THE ACCESS PANEL 561BB TRAILING EDGE, LT WING IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2025120429669](https://openairdocs.org/sdr/SWAA2025120429669.md): Angle · cracked · Oct 28, 2025 · N231WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE, BS 400, S26L, FWD CARGO BAY, REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 2, REV B.
- [SDR SWAA2025120428764](https://openairdocs.org/sdr/SWAA2025120428764.md): Floorbeam · corroded · Oct 26, 2025 · N231WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORRODED FLOORBEAM ANGLE BS 706 LBL 64, WL 208.1. REPLACED THE FLOORBEAM ANGLE AND FASTENERS IAW SRM 51-40-02, & DWG 144A7730, SHEET 7, REV-.
- [SDR SWAA2025120428641](https://openairdocs.org/sdr/SWAA2025120428641.md): Scuff Plate · cracked · Oct 26, 2025 · N231WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON THE FWD SERVICE DOOR CENTER SCUFF PLATE. REPAIRED FWD SERVICE DOOR CENTER SCUFF PLATE AT FWD GALLEY AREA IAW SRM 53-10-15-2R-2, REPAIR 2, AND BAC 5975.
- [SDR SWAA2025120428642](https://openairdocs.org/sdr/SWAA2025120428642.md): Pressure Deck · cracked · Oct 26, 2025 · N231WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK INDICATION ON THE HORIZONTAL PRESSURE DECK WEB, RBL 41, BS 663. CRACK LENGTH: 0.187 INCH. PERFORMED A PERMANENT REPAIR ON THE HORIZONTAL PRESSURE DECK, BS 663 - 675, RBL 30 - 60 IAW SRM 53-40-51-2R-2, REPAIR 2.
- [SDR SWAA2025120428763](https://openairdocs.org/sdr/SWAA2025120428763.md): Floorbeam · cracked · Oct 26, 2025 · N231WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACKED FLOORBEAM, BS 540, RBL 2. REPLACED THE FLOORBEAM IAW SRM 51-10-02, ITEM 9, AND INSTALLED FASTENERS IAW SRM 51-40-02, AND DRAWING 143A5240, SHEET 14. MEASUREMENT OF CRACK: L 0.450 INCH.
- [SDR SWAA2025120428766](https://openairdocs.org/sdr/SWAA2025120428766.md): Angle · cracked · Oct 26, 2025 · N231WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE FLOOR STRUCTURE, BS 695 AND RBL 1. REPLACED ANGLE AND FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02, ITEM 9, AND DWG 273A9110, SHEET 6, REV A.
- [SDR SWAA2025120428470](https://openairdocs.org/sdr/SWAA2025120428470.md): Glowstrip · cracked · Oct 25, 2025 · N231WN · Boeing 7377H4 · Emergency Equipment
  > CRACKED PHOTOLUMINESCENT STRIP ALONG PAX CABIN (12 EA). REPLACED THE PHOTOLUMINESCENT STRIP IAW AMM 33-51-15-400-802.
- [SDR SWAA2025120428475](https://openairdocs.org/sdr/SWAA2025120428475.md): Bear Strap · cracked · Oct 25, 2025 · N231WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CRACK INDICATION ON THE BEAR STRAP IN THE FWD GALLEY DOOR BETWEEN BS 291 - 294.5, S8 & 9R. CRACK LENGTH 0.125 INCH. RII REJECTED STEP 17 DUE TO IAW 5313-I-17254-NG, FWD R1 DOOR BEAR STRAP; - GROUP 2. ENGINEERING WAS CONTACTED FOR REPAIR INSTRUCTIONS TSR-20
- [SDR SWAA2025120428474](https://openairdocs.org/sdr/SWAA2025120428474.md): Stub Frame · cracked · Oct 25, 2025 · N231WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK STUB FRAME, BS 296.5, BTW STRINGERS 8 - 9R UPPER POSITION IN THE FWD GALLEY. REPLACED STUB FRAME & FASTENERS IAW SRM 51-40-02-OG-0, SRM 51-10-02, AND DWG 141A8370, SHEET 9, REV D.
- [SDR SWAA2025120428478](https://openairdocs.org/sdr/SWAA2025120428478.md): Access Panel · damaged · Oct 25, 2025 · N231WN · Boeing 7377H4 · Aerodynamic Fairings
  > ELONGATED HOLES OF ACCESS PANEL 195BL BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 195BL IAW SRM 51-70-05-2R-10, REPAIR 10.
- [SDR SWAA2025120428479](https://openairdocs.org/sdr/SWAA2025120428479.md): Access Panel · elongated · Oct 25, 2025 · N231WN · Boeing 7377H4 · Aerodynamic Fairings
  > ELOGANTED HOLES OF ACCESS PANEL 195AR BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 195AR BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-05-2R-10, REPAIR 10.
- [SDR SWAA2025120428064](https://openairdocs.org/sdr/SWAA2025120428064.md): Access Panel · damaged · Oct 24, 2025 · N231WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > ELONGATED HOLES OF ACCESS PANEL 192AL FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL 192AL IAW SRM 51-70-05-2R-10, REPAIR 10.
- [SDR SWAA2025120428063](https://openairdocs.org/sdr/SWAA2025120428063.md): Access Panel · elongated · Oct 24, 2025 · N231WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > ELONGATED HOLES OF ACCESS PANEL 192AR AT FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL 192AR IAW SRM 51-70-05-2R-10, REPAIR 10.
- [SDR SWAA2025120427826](https://openairdocs.org/sdr/SWAA2025120427826.md): Battery Pack · inoperative · Oct 23, 2025 · N231WN · Boeing 7377H4 · Emergency Lighting
  > INOPERATIVE GALLEY 3 BATTERY PACK. REPLACED GALLEY 3 BATTERY PACK IAW AMM 33-51-06-960-805. INSTALLATION TESTED OK.
- [SDR SWAA2025120427823](https://openairdocs.org/sdr/SWAA2025120427823.md): Skin · cracked · Oct 23, 2025 · N231WN · Boeing 7377H4 · Leading Edge Devices
  > CRACKED LOWER SURFACE SKIN OF LEADING EDGE SLAT 7, AT ACTUATOR LOCATION AROUND FASTENER ON RT WING. FAULT RESOLVED ON OTHER FAULT, TTG8Q015XHC7.;
- [SDR SWAA2025120427822](https://openairdocs.org/sdr/SWAA2025120427822.md): Skin · cracked · Oct 23, 2025 · N231WN · Boeing 7377H4 · Leading Edge Devices
  > CRACKED ON LOWER SURFACE OF LEADING EDGE SLAT 7, NOSE SKIN AT ACTUATOR AROUND FASTENER ON RT WING. PERFORMED PERMANENT REPAIR IAW SRM 57-42-01-2R-8, REPAIR 8.
- [SDR SWAA2025120341943](https://openairdocs.org/sdr/SWAA2025120341943.md): Battery Pack · inoperative · Oct 23, 2025 · N231WN · Boeing 7377H4 · Emergency Lighting
  > INOPERATIVE BATTERY PACK AT FWD GALLEY AREA (2 EA). REPLACED BATTERY PACK AT FWD GALLEY AREA (2 EA) IAW AMM 33-51-06-960-805. INSTALLATION TESTED OK.
- [SDR SWAA2025120427310](https://openairdocs.org/sdr/SWAA2025120427310.md): Skin · cracked · Oct 22, 2025 · N231WN · Boeing 7377H4 · Leading Edge Devices
  > CRACKED LOWER SURFACE OF LEADING EDGE SLAT NR 6 SKIN AT ACTUATOR LOCATION, AROUND FASTENER ON RT WING. PERFORMED PERMANENT REPAIR IAW SRM 57-42-01-2R-8, REPAIR 8.
- [SDR SWAA2025082607422](https://openairdocs.org/sdr/SWAA2025082607422.md): Panel · cracked · Aug 23, 2025 · N231WN · Boeing 7377H4 · Wing, Plate/Skin
  > LEFT WING UPPER O/B FIXED LEADING EDGE PANEL HAS CRACK/ PUNCTURE AT WS 279 L/H WING UPPER O/B FIXED LEADING EDGE PANEL HAS CRACK/ PUNCTURE AT WS 279. LENGTH 2.6 IN. X.100 IN. ACCOMPLISHED PERMANENT REPAIR PER SRM 57-41-01-2R-1 AND SRM 51-70-05.
- [SDR SWAA2025041122309](https://openairdocs.org/sdr/SWAA2025041122309.md): Heating Element · arced · Apr 7, 2025 · N231WN · Boeing 7377H4 · Windshield/Door Rain/Ice Removal
  > R1 WINDOW ARCING UPPER RIGHT WITH SMOKE OUTSIDE WINDSHIELD.<[01] R & R R1 WINDOW IN REF TO AMM 56-11-11. OPS AND LEAK CHECK GOOD. R&R RIGHT FRONT WINDOW HEAT CONTROL IN REF TO AMM 30-41-11. OPS CHECK GOOD
- [SDR SWAA2025020693588](https://openairdocs.org/sdr/SWAA2025020693588.md): Girt Bar · out of adjust · Feb 6, 2025 · N231WN · Boeing 7377H4 · Emergency Equipment
  > AFT ENTRY L2 DOOR SLIDE GIRT NEEDS ADJUSTMENT. VELCRO NOT SECURED.<[01] RE-PACKED AFT ENTRY L2 DOOR SLIDE GIRT REF AMM 25-66-01.
- [SDR SWAA2024071512426](https://openairdocs.org/sdr/SWAA2024071512426.md): Slide · loose · Jul 12, 2024 · N231WN · Boeing 7377H4 · Escape Slide
  > R1 DOOR SLIDE IS LOOSE<[01] REPOSITIONED FS SLIDE PER MT725-61-06 AND AMM25-66-01
- [SDR SWAA2024010937934](https://openairdocs.org/sdr/SWAA2024010937934.md): Web · cracked · Jan 5, 2024 · N231WN · Boeing 7377H4 · Engine Thrust Reverser
  > #1 ENGINE I/B THRUST REVERSER IS CRACKED ON THE AFT WEB TORQUE BOX JUST FORWARD OF THE SECOND FROM UPPER CASCADE LOCATED JUST UNDER T/R STOW SENSOR.<[01] REMOVED AND REPLACED #1 ENGINE I/B THRUST REVERSER IAW AMM 78-31-01. OPS AND LEAK CHECKED GOOD.
- [SDR SWAA2023112222713](https://openairdocs.org/sdr/SWAA2023112222713.md): Handle · loose · Nov 18, 2023 · N231WN · Boeing 7377H4 · Passenger/Crew Doors
  > CUSTOMER WALK ITEM - R2 DOOR ASSIST HANDLE LOOSE.<[01] ADJUSTED R2 DOOR ASSIST HANDLE IAW B737 AMM 25-00-00-100-801;[02] VERIFIED STEP 1
- [SDR SWAA2023112222715](https://openairdocs.org/sdr/SWAA2023112222715.md): Fitting · faulty · Nov 18, 2023 · N231WN · Boeing 7377H4 · Emergency Equipment
  > CUSTOMER WALK ITEM - R2 DOOR FWD GIRT BAR FITTING AFT ATTACH SCREW HAS NO THREAD PROTRUSION.<[01] REMOVED AND REINSTALLED AFT SCREW AT R2 DOOR FWD GIRT BAR FITTING IAW B737 AMM 25-66-02-400-801 AND TESTED GIRT BAR INSTALLATION<BR>WORK DONE BY JUAN RODRIGUEZ;[0

Next page: https://openairdocs.org/aircraft/N231WN/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 = 'N231WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N231WN/reports

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