# Service difficulty reports: N232WN

A list on [N232WN](https://openairdocs.org/aircraft/N232WN.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 · 294 reports

- [SDR SWAA2026072757416](https://openairdocs.org/sdr/SWAA2026072757416.md): Light · inoperative · Jul 22, 2026 · N232WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT AT SEAT 17ABC INOPERATIVE. REMOVED AND REPLACED EMERGENCY AREA LIGHT AT SEAT 17ABC IAW AMM 33-51-03-960-801 OPS CHECK GOOD.
- [SDR SWAA2026062213874](https://openairdocs.org/sdr/SWAA2026062213874.md): Girt Bar · out of adjust · Jun 18, 2026 · N232WN · Boeing 7377H4 · Emergency Equipment
  > AFTER ENTRY GIRT BAR DOES NOT SEAT FIRMLY IN CLIPS. INSPECTED AND CLEANED AFT ENTRY GIRT BAR. OPS CHKD GOOD IAW SIP.
- [SDR SWAA2026061510946](https://openairdocs.org/sdr/SWAA2026061510946.md): Slide · out of position · Jun 10, 2026 · N232WN · Boeing 7377H4 · Escape Slide
  > R2 DOOR ESCAPE SLIDE PROTRUDING FROM SLIDE BOX. TUCKED SLIDE FLAP INTO SLIDE COMPARTMENT IAW SIP
- [SDR SWAA2026050494367](https://openairdocs.org/sdr/SWAA2026050494367.md): Bracket · loose · May 1, 2026 · N232WN · Boeing 7377H4 · Escape Slide
  > FWD SERVICE SLIDE CONTAINER AFT BRACKET IS LOOSE THAT HOLDS GIRT BAR FWD SERVICE DOOR SLIDE CONTAINER AFT BRACKET IS LOOSE THAT HOLDS GIRT BAR. R&R FASTENERS ON BRAKET IAW SRM 51-40-02.
- [SDR SWAA2026021169009](https://openairdocs.org/sdr/SWAA2026021169009.md): Light · inoperative · Feb 9, 2026 · N232WN · Boeing 7377H4 · Emergency Lighting
  > RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. R & R RT OVERWING EMERGENCY EXIT LIGHT BULB AND LENS IAW AMM 33-51-04. OPS CHECKED GOOD.
- [SDR SWAA2025081292284](https://openairdocs.org/sdr/SWAA2025081292284.md): Stringer Clip · cracked · Jul 17, 2025 · N232WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP AT PAX CABIN BS 727B, S7L. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1102 REV -.
- [SDR SWAA2025081292089](https://openairdocs.org/sdr/SWAA2025081292089.md): Strap · corroded · Jul 16, 2025 · N232WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON STRAP AT MID CABIN BS 703, LBL 68, WL 203. REFER TO FAULT TTG8Q013SLHA. EA 25-153-01977.
- [SDR SWAA2025081292091](https://openairdocs.org/sdr/SWAA2025081292091.md): Strap · corroded · Jul 16, 2025 · N232WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON STRAP AT MID CABIN, BS 709, LBL 63, WL 203. REFER TO FAULT TTG8Q013SLHA WHERE EA 25-153-01977 WAS ADDED AS A SUBTASK.
- [SDR SWAA2025081292092](https://openairdocs.org/sdr/SWAA2025081292092.md): Strap · corroded · Jul 16, 2025 · N232WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON STRAP AT MID CABIN, BS 713, LBL 64 - LBL 67, WL 203. REFER TO FAULT TTG8Q013SLHA WHERE EA 25-153-01977 WAS ADDED AS A SUBTASK.
- [SDR SWAA2025081292085](https://openairdocs.org/sdr/SWAA2025081292085.md): Floorbeam · cracked · Jul 16, 2025 · N232WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACKED PANEL BREAK AT PASSENGER CABIN BS 540, LBL 26, WL 208. REPLACED PANEL BREAK IAW SRM 51-40-02, AND BOEING DWG 143A0060 REV:-;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2025081292086](https://openairdocs.org/sdr/SWAA2025081292086.md): Floorbeam · cracked · Jul 16, 2025 · N232WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACKED PANEL BREAK AT PASSENGER CABIN BS 540, LBL 1, WL 208. REPLACED PANEL BREAK PASSENGER CABIN BS540 LBL1 IAW SRM 51-40-02 AND DWG 143A0060 REV-.
- [SDR SWAA2025081292088](https://openairdocs.org/sdr/SWAA2025081292088.md): Strap · corroded · Jul 16, 2025 · N232WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON STRAP AT MID CABIN BS692 LBL68 WL203. REMOVED CORROSION ON STRAP BS 692, LBL 68, WL 203 AND ACCOMPLISHED REWORK OF STRAP IAW EA 25-153-01977.
- [SDR SWAA2025081292087](https://openairdocs.org/sdr/SWAA2025081292087.md): Strap · corroded · Jul 16, 2025 · N232WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON STRAP AT MID CABIN BS718 RBL62 WL203. CORROSION ON STRAP AT MID CABIN BS718 RBL62 WL203 REPAIRED PER EA 25-153-01971-WIP1.
- [SDR SWAA2025081291672](https://openairdocs.org/sdr/SWAA2025081291672.md): Support · corroded · Jul 15, 2025 · N232WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT BULKHEAD SUPPORT BS 947; RBL 20; WL 160. REMOVED AND REPLACED AFT BULKHEAD SUPPORT STA 947. STR 25L-STR 25R IAW SRM 51-40-02; DWG 149A8117 REV:- AND DWG 149A8110 REV:A.
- [SDR SWAA2025081291365](https://openairdocs.org/sdr/SWAA2025081291365.md): Sidewall Support · corroded · Jul 14, 2025 · N232WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO COMPARTMENT R/H FLOOR TO SIDEWALL SUPPORT BS 867+10, 867+15-16, RBL 22, WL 158. REMOVED AND REPLACED ON AFT CARGO COMPARTMENT R/H FLOOR SIDEWALL SUPPORT BS 867 TO 887 IAW SRM 51-40-02, AND 51-40-05 AND DWG 146A7500 REV A.
- [SDR SWAA2025081291379](https://openairdocs.org/sdr/SWAA2025081291379.md): Shield · corroded · Jul 14, 2025 · N232WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO COMPARTMENT AFT SHIELD BS 847-867, RBL 22, WL 157. NO ALLOWABLE DAMAGE GIVEN FOR THIS PART IN SRM 53-00-53-1A-2. REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0, STEP 9. REMOVED DAMAGED SHIELD AND INSTALLED A NEW SHIELD IAW SRM 51-40-02
- [SDR SWAA2025081291349](https://openairdocs.org/sdr/SWAA2025081291349.md): Shield · corroded · Jul 14, 2025 · N232WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO COMPARTMENT SHIELD BS 500+6, 500+10, RBL 22, WL 156. CORROSION FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2. REPAIR BY REPLACEMENT IAW SRM 51-10-02<BR>REMOVED DAMAGED SHIELD IAW SRM 51-40-02. INSTALLED A NEW SHIELD
- [SDR SWAA2025081291350](https://openairdocs.org/sdr/SWAA2025081291350.md): Sidewall Support · corroded · Jul 14, 2025 · N232WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT BS 400-500D, LBL 22, WL 157. SUPPORT HAS MISSING FASTENER AND IS NOT DRILLED AT BS 396, LBL 22, WL 157. DRILLED HOLE AND INSTALLED FASTENER IAW SRM 51-40-05, SRM 51-40-02, AND DWG 143A7500 REV-.
- [SDR SWAA2025081291351](https://openairdocs.org/sdr/SWAA2025081291351.md): Sidewall Support · corroded · Jul 14, 2025 · N232WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT BS 500A-500D; RBL 22; WL 157. REMOVED AND REPLACED SIDEWALL SUPPORT IAW SRM 51-4-02 AND DWG 143A7500 REV-.
- [SDR SWAA2025081291373](https://openairdocs.org/sdr/SWAA2025081291373.md): Shield · corroded · Jul 14, 2025 · N232WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO COMPARTMENT FWD SHIELD BS 767-787, RBL 22, WL 156-157. INSTALLED NEW SHIELD IAW SRM 51-40-02, 51-40-05, AND DWG 146A8127 REV -.
- [SDR SWAA2025081291375](https://openairdocs.org/sdr/SWAA2025081291375.md): Sidewall Support · corroded · Jul 14, 2025 · N232WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO COMPARTMENT L/H FLOOR TO SIDEWALL SUPPORT BS 727+4 - 787+1-10, LBL 22, WL 156. REMOVED AND REPLACED AFT CARGO COMPARTMENT LT FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0, DWG 146A7500 REV:B, DWG 146A7502 REV-, AND SRM 51-40-05-0G
- [SDR SWAA2025081291376](https://openairdocs.org/sdr/SWAA2025081291376.md): Sidewall Support · corroded · Jul 14, 2025 · N232WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO COMPARTMENT R/H FLOOR TO SIDEWALL SUPPORT STA 727+4-767 RBL 22; WL 156. REMOVED OLD AND INSTALLED NEW AFT CARGO COMPARTMENT R/H FLOOR TO SIDEWALL SUPPORT BS A 727+4 - 767 RBL 22; WL 156 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; SRM 51-
- [SDR SWAA2025081291377](https://openairdocs.org/sdr/SWAA2025081291377.md): Sidewall Support · corroded · Jul 14, 2025 · N232WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO COMPARTMENT R/H FLOOR TO SIDEWALL SUPPORT STA 887+4-887+12; 907+2; RBL 22; WL 159. REMOVED AND REPLACED ON AFT CARGO COMPARTMENT R/H FLOOR TO SIDEWALL SUPPORT STA 867 TO 887 PER SRM 51-40-02; 51-40-05 AND BOEING DWG 147A7500REV -.
- [SDR SWAA2025081291378](https://openairdocs.org/sdr/SWAA2025081291378.md): Strap · corroded · Jul 14, 2025 · N232WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO COMPARTMENT FLOOR TIEDOWN STRAP STA 887; BETWEEN FLOOR PANELS 140CF-140DF. REMOVED AND REPLACED SPLICE / TEE ASSY IAW SRM 51-40-05 AND DWG 146A7500 REV A.
- [SDR SWAA2025081291371](https://openairdocs.org/sdr/SWAA2025081291371.md): Seat Track · corroded · Jul 14, 2025 · N232WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK LBL 45 AT STA 616+18 APPROX.; BS 663; BS 663+12 APPROX.; STA 685+12 APPROX. AND AT STA 727A+10 APPROX. WAS FOUND CORRODED ON CROWN. REMOVED CORROSION ON SEAT TRACK BS 540-727 LBL 45 FOUND TO BE OUT OF LIMITS PER SRM 53-00-52-1A-1. REMOVED
- [SDR SWAA2025081291364](https://openairdocs.org/sdr/SWAA2025081291364.md): Seat Track · corroded · Jul 14, 2025 · N232WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK LBL 45 AT STA 540 AND STA 727+12 APPROX. WAS FOUND MECHANICAL DAMAGE ON CROWN. AND AT STA 559+10 APPROX. WAS FOUND CORROSION ON WELL. SEAT TRACK FOUND TO BE OUT OF LIMITS ON FAULT TTG8Q013QT63 AND WILL BE REPLACED ON TTG8Q013QT63.
- [SDR SWAA2025081203486](https://openairdocs.org/sdr/SWAA2025081203486.md): Stringer · cracked · Jul 11, 2025 · N232WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FCB BS535 S-23L WL164. REMOVED DAMAGED STRINGER S-23L BS 540 - BS500D+10; FABRICATED AND INSTALLED NEW STRINGER AND SPLICE AT STRINGER 23L BS 540-BS 500D+10 IAW SRM 53-00-03-2R-1; SRM 51-40-02 DWG143A3210 REV B.
- [SDR SWAA2025081290412](https://openairdocs.org/sdr/SWAA2025081290412.md): Stringer · cracked · Jul 11, 2025 · N232WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FCB BS 535, S-23L, WL164. REMOVED DAMAGED STRINGER S-23L BS 540 - BS500D+10; FABRICATED AND INSTALLED NEW STRINGER AND SPLICE AT STRINGER 23L BS 540-BS 500D+10 IAW SRM 53-00-03-2R-1; SRM 51-40-02 DWG143A3210 REV B.
- [SDR SWAA2025081290413](https://openairdocs.org/sdr/SWAA2025081290413.md): Stringer · cracked · Jul 11, 2025 · N232WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FCB BS535 S-26L WL153. REMOVED DAMAGED STRINGER S-26L BS 540 - BS500D+10; FABRICATED AND INSTALLED NEW STRINGER AND SPLICE AT STRINGER 26L BS 540-BS 500D+10 IAW SRM 53-00-03-2R-1; SRM 51-40-02 DWG143A3230 REV A.
- [SDR SWAA2025081203487](https://openairdocs.org/sdr/SWAA2025081203487.md): Stringer Splice · cracked · Jul 11, 2025 · N232WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FCB BS535 S-26L WL153. REMOVED DAMAGED STRINGER S-26L BS 540 - BS500D+10; FABRICATED AND INSTALLED NEW STRINGER AND SPLICE AT STRINGER 26L BS 540-BS 500D+10 IAW SRM 53-00-03-2R-1; SRM 51-40-02 DWG143A3230 REV A.
- [SDR SWAA2025081290534](https://openairdocs.org/sdr/SWAA2025081290534.md): Plate · cracked · Jul 11, 2025 · N232WN · Boeing 7377H4 · Wing Main, Frame Structure
  > RIGHT WING T/E WIGGLE PLATE AT ORSS 261 IS CRACKED.
- [SDR SWAA2025081290178](https://openairdocs.org/sdr/SWAA2025081290178.md): Scuff Plate · cracked · Jul 10, 2025 · N232WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT FWD CORNER SCUFF PLATE IS CRACKED. REPAIRED FWD CARGO COMPARTMENT FWD CORNER SCUFF PLATE PER SRM 53-30-15-2R-1, SOPM 20-43-03, SOPM 20-41-02;
- [SDR SWAA2025081289830](https://openairdocs.org/sdr/SWAA2025081289830.md): Stub Frame · cracked · Jul 10, 2025 · N232WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK FOUND ON STUB FRAME BS 294.5 +8.5'; ABOVE SEAL DEPRESSOR, BETWEEN S8R AND S9R; LENGTH 1.4'. REMOVED OLD FWD SERVICE DOOR STUB FRAME BS 294 +8.5' IAW SRM 51-40-02-0G-0 AND INSTALLED NEW FWD SERVICE DOOR STUB FRAME IAW SRM 51-40-02-0G-0 AND DWG 141A8370
- [SDR SWAA2025081489485](https://openairdocs.org/sdr/SWAA2025081489485.md): Assist Handle · broken · Jul 9, 2025 · N232WN · Boeing 7377H4 · Service Doors
  > AFT SERVICE DOOR SURROUND ASSIST HANDLE IS BROKEN.
- [SDR SWAA2025081289822](https://openairdocs.org/sdr/SWAA2025081289822.md): Rib · cracked · Jul 9, 2025 · N232WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > L/H HORIZONTAL STAB REMOVABLE L/E; 3RD RIB FROM I/B END IS CRACKED. REMOVED AND REPLACED 3RD RIB FROM I/B END OF L/H HORIZONTAL STAB. L/E IAW SRM 51-40-02-0G-0 PARA. 4.
- [SDR SWAA2025081289823](https://openairdocs.org/sdr/SWAA2025081289823.md): Rib · cracked · Jul 9, 2025 · N232WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > L/H HORIZONTAL STAB REMOVABLE L/E; 4TH RIB FROM I/B END IS CRACKED. REMOVED AND REPLACED 4TH RIB FROM I/B END OF L/H HORIZONTAL STAB. L/E IAW SRM 51-40-02-0G-0 PARA. 4.
- [SDR SWAA2025081289824](https://openairdocs.org/sdr/SWAA2025081289824.md): Rib · cracked · Jul 9, 2025 · N232WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > L/H HORIZONTAL STAB REMOVABLE L/E; 5TH RIB FROM I/B END IS CRACKED. REMOVED AND REPLACED 5TH RIB FROM I/B END OF L/H HORIZONTAL STAB. L/E IAW SRM 51-40-02-0G-0 PARA. 4.
- [SDR SWAA2025081289062](https://openairdocs.org/sdr/SWAA2025081289062.md): Rib · cracked · Jul 8, 2025 · N232WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > RIGHT HORIZONTAL STAB RIB 5 STIFFENER HAS CRACK ON LOWER RADIUS. REPAIRED RT HORIZONTAL STAB RIB 5, STAB STA 129.5 IAW SRM 51-40-2-0G-0 AND SRM 55-10-09-2R-4 REPAIR 4; FIG. 202; DETAIL.
- [SDR SWAA2025081289464](https://openairdocs.org/sdr/SWAA2025081289464.md): Floor Panel · delaminated · Jul 8, 2025 · N232WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 232SF HAS AREAS OF DELAMINATION ON UPPER SKIN. FABRICATED NEW FLOOR PANEL 232SF IAW SRM 53-00-50-2R-0 AND DWG 144A5810 SHEET 159.
- [SDR SWAA2025081289466](https://openairdocs.org/sdr/SWAA2025081289466.md): Floor Panel · delaminated · Jul 8, 2025 · N232WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241AF HAS AREAS OF DELAMINATION ON UPPER SKIN. FLOOR PANEL 241AF WITH AREAS OF UPPER SURFACE DELAMINATION WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810-127.
- [SDR SWAA2025081289467](https://openairdocs.org/sdr/SWAA2025081289467.md): Floor Panel · delaminated · Jul 8, 2025 · N232WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241BF HAS AREAS OF DELAMINATION ON UPPER SKIN. FLOOR PANEL 241BF WITH AREAS OF UPPER SURFACE DELAMINATION WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810-189.
- [SDR SWAA2025081289468](https://openairdocs.org/sdr/SWAA2025081289468.md): Floor Panel · delaminated · Jul 8, 2025 · N232WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 242AF HAS AREAS OF DELAMINATION ON UPPER SKIN. FABRICATION OF NEW 242AF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0-A00938, REPAIR GENERAL.
- [SDR SWAA2025081289469](https://openairdocs.org/sdr/SWAA2025081289469.md): Floor Panel · delaminated · Jul 8, 2025 · N232WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 242BF HAS AREAS OF DELAMINATION ON UPPER SKIN. FABRICATED NEW FLOOR PANEL 242BF IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0122.
- [SDR SWAA2025081289470](https://openairdocs.org/sdr/SWAA2025081289470.md): Floor Panel · delaminated · Jul 8, 2025 · N232WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241EF HAS AREAS OF DELAMINATION ON UPPER SKIN. FLOOR PANEL 241EF WITH AREAS OF DELAMINATION ON UPPER SKIN WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810-129.
- [SDR SWAA2025081289471](https://openairdocs.org/sdr/SWAA2025081289471.md): Floor Panel · delaminated · Jul 8, 2025 · N232WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241FF HAS AREAS OF DELAMINATION ON UPPER SKIN. FLOOR PANEL 241FF WITH AREAS OF UPPER SKIN DELAMINATION WAS REPLACED BY FABRICATING A NEW BOARD IAW SRM 53-00-50-2R-0 AND DWG 144A5810-131.
- [SDR SWAA2025081289472](https://openairdocs.org/sdr/SWAA2025081289472.md): Floor Panel · delaminated · Jul 8, 2025 · N232WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 242CF HAS AREAS OF DELAMINATION ON UPPER SKIN. FLOOR PANEL 242CF WITH AREAS OF UPPER SURFACE DELAMINATION WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0125.
- [SDR SWAA2025081189462](https://openairdocs.org/sdr/SWAA2025081189462.md): Floor Panel · delaminated · Jul 8, 2025 · N232WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 231XF HAS AREAS OF DELAMINATION ON UPPER SKIN. FABRICATED NEW FLOOR PANEL 231XF IAW SRM 53-00-50-2R-0 AND BOEING DRAWING 144A5810 SHEET 126.
- [SDR SWAA2025081189463](https://openairdocs.org/sdr/SWAA2025081189463.md): Floor Panel · delaminated · Jul 8, 2025 · N232WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 231YF HAS AREAS OF DELAMINATION ON UPPER SKIN. FABRICATED NEW FLOOR PANEL 231YF IAW SRM 53-00-50-2R-0 AND BOEING DRAWING 144A5810 SHEET 124..
- [SDR SWAA2025081289061](https://openairdocs.org/sdr/SWAA2025081289061.md): Skin · pulled · Jul 7, 2025 · N232WN · Boeing 7377H4 · Nacelle/Pylon, Plate/Skin
  > L/H ENGINE INLET COWL BARREL SKIN HAS A PULLED THROUGH FASTENER AT 10:00 O'CLOCK POSITION.NR 1 ENGINE INLET COWL WAS REMOVED AND REPLACED ON CARD 7111-E-17062-NG. FAULT WAS ATTACHED TO R/O AND WILL BE CORRECTED WHEN INLET COWL GETS MODIFIED.
- [SDR SWAA2025050667558](https://openairdocs.org/sdr/SWAA2025050667558.md): Lens · displaced · May 4, 2025 · N232WN · Boeing 7377H4 · Emergency Lighting
  > RAMP REPORTS. EMERGENCY LIGHT LENSE DISPLACED AIRCRAFT LEFT AFT<[01] SECURED EMERGENCY LIGHT LENSE REF SIP

Next page: https://openairdocs.org/aircraft/N232WN/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 = 'N232WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N232WN/reports

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