# Service difficulty reports: N923WN

A list on [N923WN](https://openairdocs.org/aircraft/N923WN.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 5 · 246 reports

- [SDR SWAA2026101294290](https://openairdocs.org/sdr/SWAA2026101294290.md): Battery Pack · no test · Oct 6, 2026 · N923WN · Boeing 7377H4 · Emergency Lighting
  > AFT RIGHT EMERGENCY BATTERY PACK M1672 FAILED A CAPACITY CHECK. R & R THE BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026101290539](https://openairdocs.org/sdr/SWAA2026101290539.md): Battery Pack · failed · Oct 6, 2026 · N923WN · Boeing 7377H4 · Emergency Lighting
  > AFT LEFT EMERGENCY BATTERY PACK M1673 FAILED CAPACITY CHECK. R & R THE BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026100508192](https://openairdocs.org/sdr/SWAA2026100508192.md): Seat · out of position · Oct 1, 2026 · N923WN · Boeing 7377H4 · Passenger Compartment Equipment
  > SEAT 14D SEATBACK WILL NOT STAY IN THE UPRIGHT POSITION. SECURED THE SEAT IN UPRIGHT POSITION, OK TO CONTINUE IAW MEL 25-6-02. PER AMM 25-22-00
- [SDR SWAA2026071019230](https://openairdocs.org/sdr/SWAA2026071019230.md): Light · inoperative · Jul 7, 2026 · N923WN · Boeing 7377H4 · Emergency Lighting
  > LEFT OVERWING EXTERIOR EMERGENCY LIGHT INOP. REPLACED THE LAMPS AND PERFORMED SATISFACTORY OPS CHECK OF LT OVERWING EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-04.
- [SDR SWAA2026033083264](https://openairdocs.org/sdr/SWAA2026033083264.md): Battery Pack · failed · Mar 25, 2026 · N923WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT AT ROWS 17ABC; 20ABC; 22ABC; 27ABC; 25DEF AFTER ABOUT 15 SECONDS. REMOVED AND REPLACED BATTERY PACK M1673 AND PERFORMED GOOD TEST OF EXIT LIGHTS AT ROWS 17ABC; 20ABC; 22ABC; 27ABC; 25DEF.
- [SDR SWAA2026033079595](https://openairdocs.org/sdr/SWAA2026033079595.md): Intercostal · cracked · Mar 13, 2026 · N923WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT BS 380-400 RBL 8 WL 208. REQUIRES RII BUYBACK<[01] VERIFIED RII BUYBACK FOR TTG8Q01AR0L2.
- [SDR SWAA2026033075902](https://openairdocs.org/sdr/SWAA2026033075902.md): Floor Support · cracked · Mar 2, 2026 · N923WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT BS 380-400 RBL 8 WL 208. REMOVED AND REPLACED INTERCOSTAL AT BS 380-400 RBL 8 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 143A5400 SHEET 38 REV A.
- [SDR SWAA2026033075893](https://openairdocs.org/sdr/SWAA2026033075893.md): Strap · corroded · Mar 2, 2026 · N923WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON STRAP AT BS 1018 RBL3 WL 208<[01] REMOVED; FABRICATED AND INSTALLED NEW TENSION STRAP BS 1006 - BS11028 RBL3 WL 208 I.A.W SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND BOEING DWGS 147A5730 REV: C; 147A5744 REV: B; PL 147A5744 REV: E.
- [SDR SWAA2026033075903](https://openairdocs.org/sdr/SWAA2026033075903.md): Intercostal · cracked · Mar 2, 2026 · N923WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT BS 380-400 LBL 13 WL 208. NOT ALLOWABLE LIMITS FOUND THEREFORE SRM 51-10-02-0G-0 PAR 9.C REMOVE AND REPLACEMENT OF THE PART IS APPLICABLE; REMOVED CRACKED INTERCOSTAL AT BS 380-400 LBL 13 WL 208 PER SRM 51-40-02; OK TO INSTALL NEW INTE
- [SDR SWAA2026033075904](https://openairdocs.org/sdr/SWAA2026033075904.md): Intercostal · cracked · Mar 2, 2026 · N923WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT BS 380-400 BL 0 WL 208. NOT ALLOWABLE LIMITS FOUND THEREFORE SRM 51-10-02-0G-0 PAR 9.C REMOVE AND REPLACEMENT OF THE PART IS APPLICABLE; REMOVED CRACKED INTERCOSTAL AT BS 380-400 BL 0 WL 208 PER SRM 51-40-02; LOCATED AND DRILLED NEW IN
- [SDR SWAA2026033075900](https://openairdocs.org/sdr/SWAA2026033075900.md): Intercostal · cracked · Mar 2, 2026 · N923WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL, BS 312 - 328, LBL 45, WL 208. REMOVED & REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G-0, & DWG 141A5400, SHEET 26, REV-.
- [SDR SWAA2026033075901](https://openairdocs.org/sdr/SWAA2026033075901.md): Intercostal · cracked · Mar 2, 2026 · N923WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL, BS 328 - 344, LBL 45, WL 208. REMOVED & REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G-0, & DWG 141A5400, SHEET 44, REV -.
- [SDR SWAA2026032775911](https://openairdocs.org/sdr/SWAA2026032775911.md): Support · corroded · Mar 2, 2026 · N923WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION FWD CARGO BAY AFT LOWER BULKHEAD SUPPORT HAS MULTIPLE AREAS AROUND FASTENER HOLES BS500D LBL21 TO RBL21. REMOVED AND INSTALLED NEW FWD CARGO BAY AFT LOWER BULKHEAD SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 143A7902 REV:-.
- [SDR SWAA2026032775912](https://openairdocs.org/sdr/SWAA2026032775912.md): Support Plate · corroded · Mar 2, 2026 · N923WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156<[01] REMOVED AND INSTALLED NEW L/H FLOOR TO SIDEWALL SUPPORT BS 727 TO 847 LBL 22 IAW SRM 51-40-02-0G-0 AND DWG 146A7500 REV:-.
- [SDR SWAA2026032775913](https://openairdocs.org/sdr/SWAA2026032775913.md): Support Plate · corroded · Mar 2, 2026 · N923WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS 727B TO 767 RBL22 WL156. REMOVED AND INSTALLED NEW R/H FLOOR TO SIDEWALL SUPPORT BS 727 TO 847 LBL 22 IAW SRM 51-40-02-0G-0 AND DWG 146A7500 REV-.
- [SDR SWAA2026032775908](https://openairdocs.org/sdr/SWAA2026032775908.md): Seat Track · corroded · Mar 2, 2026 · N923WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON TOP & IN WELL OF PAX CABIN SEAT TRACK LBL 45 BS 500+8 TOP, BS 500A+7 WELL, BS 500B+18 WELL., WL 208. REMOVED CORROSION ON PAX CABIN SEAT TRACK LBL 45 WL 208 AT BS 500+8 ON TOP PER SRM 51-10-02-0G-0. AREA BLENDED IS L4' X W1' X D0.026' FOUND TO B
- [SDR SWAA2026032675894](https://openairdocs.org/sdr/SWAA2026032675894.md): Floorbeam · corroded · Mar 2, 2026 · N923WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR BEAM BS 986 LBL 45 WL 208<[01] REMOVED AND REPLACED DAMAGE UPPER T-CHORD BS 986 RBL1-LBL50 WL 208 I.A.W SRM 51-40-02-0G-0 AS SHOWN IN CC# U152596 DATED 04/27/2020 PER SRM 53-70-51-2R-4 REPAIR 4 WITHOUT ANY DEVIATION.;[02] VERIFIED; CORRECTIV
- [SDR SWAA2026032775638](https://openairdocs.org/sdr/SWAA2026032775638.md): Floor Panel · delaminated · Mar 1, 2026 · N923WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241VF HAS DELAMINATION DAMAGE. THE FLOOR PANEL 241VF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0 AND DWG 146A5810 I.
- [SDR SWAA2026032775640](https://openairdocs.org/sdr/SWAA2026032775640.md): Floor Panel · delaminated · Mar 1, 2026 · N923WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241XF HAS DELAMINATION DAMAGE. THE FLOOR PANEL 241XF WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2026032775646](https://openairdocs.org/sdr/SWAA2026032775646.md): Floor Panel · delaminated · Mar 1, 2026 · N923WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241YF HAS DELAMINATION DAMAGE. FLOOR PANEL 241YF WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2026032775645](https://openairdocs.org/sdr/SWAA2026032775645.md): Floor Panel · delaminated · Mar 1, 2026 · N923WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 242VF HAS DELAMINATION DAMAGE. FLOOR PANEL 242VF WAS REPAIRED PER SRM 53-00-50-2R-1.
- [SDR SWAA2026032775636](https://openairdocs.org/sdr/SWAA2026032775636.md): Floor Panel · delaminated · Mar 1, 2026 · N923WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241AEF HAS DELAMINATION DAMAGE. FLOOR PANEL 241AEF WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2026032775642](https://openairdocs.org/sdr/SWAA2026032775642.md): Floor Panel · delaminated · Mar 1, 2026 · N923WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 242PF HAS DELAMINATION DAMAGE. FLOOR PANEL 242PF REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 AND DWG: 146A5810 DUE TO AMOUNT OF ALL DAMAGE.
- [SDR SWAA2026032775647](https://openairdocs.org/sdr/SWAA2026032775647.md): Floor Panel · delaminated · Mar 1, 2026 · N923WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 242QF HAS DELAMINATION DAMAGE. FLOOR PANEL 242QF WITH DELAMINATION DAMAGE WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 AND BDWG: 146A5810 ID: 0468 DUE TO AMOUNT OF ALL DAMAGE.
- [SDR SWAA2026032775634](https://openairdocs.org/sdr/SWAA2026032775634.md): Floor Panel · delaminated · Mar 1, 2026 · N923WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241ACF HAS DELAMINATION DAMAGE. THE FLOOR PANEL 241ACF WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2026032775639](https://openairdocs.org/sdr/SWAA2026032775639.md): Floor Panel · delaminated · Mar 1, 2026 · N923WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL241WF DELAMINATION DAMAGE. REPLACED THE FLOOR PANEL WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0 AND DRAWING 146A5810 SHEET 471.
- [SDR SWAA2026032775641](https://openairdocs.org/sdr/SWAA2026032775641.md): Floor Panel · delaminated · Mar 1, 2026 · N923WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241ZF HAS DELAMINATION DAMAGE. FLOOR PANEL 241ZF; WITH DELAMINATION DAMAGE; WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2026032775648](https://openairdocs.org/sdr/SWAA2026032775648.md): Floor Panel · delaminated · Mar 1, 2026 · N923WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 242WF HAS DELAMINATION DAMAGE. FLOOR PANEL 242WF WITH DELAMINATION DAMAGE WAS REPLACED WITH A SERVICEABLE FLOOR PANEL IAW SRM 51-10-02-0G-0 PARA. 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.
- [SDR SWAA2026032775633](https://openairdocs.org/sdr/SWAA2026032775633.md): Floor Panel · delaminated · Mar 1, 2026 · N923WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241ABF HAS DELAMINATION DAMAGE. THE FLOOR PANEL 241ABF WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2026032774872](https://openairdocs.org/sdr/SWAA2026032774872.md): Floor Panel · pulled · Feb 27, 2026 · N923WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 231YF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL 231YF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 SHEET 151.
- [SDR SWAA2026032774873](https://openairdocs.org/sdr/SWAA2026032774873.md): Floor Panel · pulled · Feb 27, 2026 · N923WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL 231ZF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 SHEET 160.
- [SDR SWAA2026032774874](https://openairdocs.org/sdr/SWAA2026032774874.md): Floor Panel · debonded · Feb 27, 2026 · N923WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 232SF UPPER SKIN HAS LARGE DISBOND NEAR AFT EDGE OF PANEL. THE FLOOR PANEL 232SF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810.
- [SDR SWAA2026033074852](https://openairdocs.org/sdr/SWAA2026033074852.md): Crossbeam · cracked · Feb 26, 2026 · N923WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACKED CROSSBEAM, BS 540, LBL 2, WL 208. REMOVED AND REPLACED CROSSBEAM IAW SRM 51-40-02-0G-0, & DWG 143A0060, SHEET 46, REV -.
- [SDR SWAA2026033074851](https://openairdocs.org/sdr/SWAA2026033074851.md): Crossbeam · cracked · Feb 26, 2026 · N923WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACKED CROSSBEAM, BS 540, LBL 26, WL 208. REMOVED AND REPLACED CROSSBEAM IAW SRM 51-40-02, PAR 9.C. INSTALLED EWIS PROTECTION PER AMM 20-60-07.
- [SDR SWAA2026033074854](https://openairdocs.org/sdr/SWAA2026033074854.md): Crossbeam · cracked · Feb 26, 2026 · N923WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACKED CROSSBEAM, BS 540, RBL 26, WL 208. REMOVED AND REPLACED THE CROSSBEAM IAW SRM 51-10-02, PAR 9.C.
- [SDR SWAA2026033074497](https://openairdocs.org/sdr/SWAA2026033074497.md): Stringer Splice · corroded · Feb 26, 2026 · N923WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION IN THE E&E BAY, BS 361, WL 147, STRINGER 28L, INBD SIDE OF U SHAPE STRINGER SPLICE. R & R U STRINGER SPLICE BTWN BS 356 - 369, S28L IAW SRM 51-40-02, DWG:140A9101,0029;REV-, & DWG 140A9101,0032, REV-.
- [SDR SWAA2026032674500](https://openairdocs.org/sdr/SWAA2026032674500.md): Stiffener · cracked · Feb 26, 2026 · N923WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > RH HORIZONTAL STAB INSPAR RIB #4 (STA 120.30) AFT STIFFINER IS CRACKED AT LOWER RADIUS<[01] REMOVED; REPAIRED; AND REINSTALLED RIB #4 STA 120.30 PER SRM 55-10-09-2R-5; SRM 51-40-02-0G-0; DWG 182A4001 REV:D; DWG 182A3001 REV: F; AND DWG 182A5304 REV: C. AND DWG
- [SDR SWAA2026032774494](https://openairdocs.org/sdr/SWAA2026032774494.md): Doubler · cracked · Feb 25, 2026 · N923WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > EGPR SURROUND DOUBLER IS CRACKED BS233 WL175 8' ABOVE S-24R. TRIMMED OUT THE DAMAGED, FABRICATED REPAIR PARTS AND INSTALLED ALL REPAIR PARTS AT THE EGPR SURROUND DOUBLER AT BS233 WL175 8' ABOVE S-24R IAW SRM 53-10-15-2R-4, REPAIR 4, PARG 4(B-M).
- [SDR SWAA2026032674310](https://openairdocs.org/sdr/SWAA2026032674310.md): Web · cracked · Feb 25, 2026 · N923WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MAIN CABIN; FOUND HORIZONTAL PREASSURE WEB CRACKED AT STA 673 AND RBL 42 APPRO. MARKED<[01] REMOVED DAMAGE PART OF THE BEADED PRESSURE DECK WEB AND REPAIRED BS 663- BS 674 RBL38-RBL60 WL202;RESTORED FINISHES; APPLIED CIC ALL I.A.W SRM 53-40-51-2R-2 REPAIR 2;
- [SDR SWAA2026033074076](https://openairdocs.org/sdr/SWAA2026033074076.md): Strut · cracked · Feb 24, 2026 · N923WN · Boeing 7377H4 · Nacelle/Pylon, Main Frame
  > NR 1 NACELLE AFT FAIRING STRUCTURE CRACKED AT AFT END. REMOVED & REPLACED THE NR 1 NACELLE STRUT AFT FAIRING TRAILING EDGE ASSY IAW SRM 51-40-05, DWG 313A2400, REV A, & DWG 313A2700, REV-.
- [SDR SWAA2026033074077](https://openairdocs.org/sdr/SWAA2026033074077.md): Strut · cracked · Feb 24, 2026 · N923WN · Boeing 7377H4 · Nacelle/Pylon, Main Frame
  > NUMBER 2 NACELLE AFT FAIRING STRUCTURE CRACKED AT AFT END. REMOVED & REPLACED THE NR 2 NACELLE STRUT AFT FAIRING TRAILING EDGE ASSY IAW SRM 51-40-02, DWG 313A2400, REV A, AND DWG 313A2700, REV-.
- [SDR SWAA2026021369256](https://openairdocs.org/sdr/SWAA2026021369256.md): Seal · cracked · Feb 10, 2026 · N923WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > RIGHT HORIZONTAL STAB, FWD UPPER SLIDING SEAL CRACKED. R & R RT HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL IAW AMM 53-31-31.
- [SDR SWAA2026021369257](https://openairdocs.org/sdr/SWAA2026021369257.md): Seal · cracked · Feb 10, 2026 · N923WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > LEFT HORIZONTAL STAB, FWD UPPER SLIDING SEAL CRACKED. R & R THE LT HORIZONTAL STAB FWD UPPER SLIDING SEAL IAW AMM 53-31-31.
- [SDR SWAA2025031805906](https://openairdocs.org/sdr/SWAA2025031805906.md): Table · loose · Mar 16, 2025 · N923WN · Boeing 7377H4 · Passenger Compartment Equipment
  > TRAY TABLE ON ROW 11 FELL OFF <[01]. RESECURED HARDWARE AT ROW 11 TRAY TABLE PER SIP.
- [SDR SWAA2024122380166](https://openairdocs.org/sdr/SWAA2024122380166.md): Lens · cracked · Dec 22, 2024 · N923WN · Boeing 7377H4 · Emergency Lighting
  > PASSENGER CABIN R1 DOOR EMERGENCY EXIT LOWER LIGHT LENS CRACKED<[01] INSTALLED R1 DOOR EXIT LIGHT LENS PER AMM SIP
- [SDR SWAA2024120974545](https://openairdocs.org/sdr/SWAA2024120974545.md): Scuff Plate · cracked · Dec 6, 2024 · N923WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR FWD CORNER SCUFF PLATE HAS CRACK<[01] REMOVED AND INSTALLED AFT CARGO DOOR FWD CORNER SCUFF PLATE PER AMM 53-11-02. LEAK CHECK GOOD OF FWD CORNER. CRACK WAS REPAIRED BY OUTSIDE VENDOR REFER TO WO P8211770-1 FOR WORK PERFORMED.
- [SDR SWAA2024120574009](https://openairdocs.org/sdr/SWAA2024120574009.md): Scuff Plate · cracked · Dec 4, 2024 · N923WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > REF. TTG8Q00X7P8A; AFT CARGO FWD SCUFF PLATE.<[01] REMOVED AFT CARGO FWD SCUFF PLATE IN REF WITH AMM 53-11-02.;[02] INSTALLED AFT CARGO DOOR FWD SCUFF PLATE. DURING INSTALLATION; SCUFF PLATE CRACKED AGAIN. THIS ITEM WILL REMAIN ON TLD. REF TTG8Q00X7P8A.
- [SDR SWAA2024112671424](https://openairdocs.org/sdr/SWAA2024112671424.md): Battery · inoperative · Nov 24, 2024 · N923WN · Boeing 7377H4 · Emergency Equipment
  > AFT MEGA-PHONE INOP.<[01] REPLACED MEGAPHONE BATTERY IAW AMM 25-64-00. OPS CHECK GOOD.
- [SDR SWAA2024112670560](https://openairdocs.org/sdr/SWAA2024112670560.md): Scuff Plate · cracked · Nov 22, 2024 · N923WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFD CARGO DOOR FWD CORNER SCUFF PLATE HAS CRACK.<[01] REF CW TC 24-153-03177 (N923WN - SWA - INTERNAL NDT INSPECTION OF LOWER FWD CORNER AFT CARGO DOOR BEAR STRAP) FOR NDT COMPLIANCE OF THIS CARD TTG8Q00X7KPE.;[02] CW;[03] PERFORMED TEMPORARY REPAIR OF AFT CAR
- [SDR SWAA2024050980919](https://openairdocs.org/sdr/SWAA2024050980919.md): Battery Pack · inoperative · Apr 30, 2024 · N923WN · Boeing 7377H4 · Emergency Lighting
  > MULTIPLE PAX EMERGENCY LIGHT BATTERY PACKS INOP.<[01] PERFORMED POWER SUPPLY - BATTERY PACK REPLACEMENT AT POSITION M1669 AS PER REF AMM 33-51-06-960-805. TEST FOUND NORMAL.;[02] VERIFIED REMOVED AND REPLACED POWER SUPPLY - BATTERY PACK.<BR>P/N: AD-D717-01-100

Next page: https://openairdocs.org/aircraft/N923WN/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 = 'N923WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N923WN/reports

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