# Service difficulty reports: N298WN

A list on [N298WN](https://openairdocs.org/aircraft/N298WN.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 · 268 reports

- [SDR SWAA2026092845005](https://openairdocs.org/sdr/SWAA2026092845005.md): Switch · damaged · Sep 22, 2026 · N298WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS GUARD ON SWITCH DAMAGED (FLIGHT DECK). REMOVED AND REPLACED THE FLIGHT DECK EMERGENCY LIGHT SWITCH GUARD PER SIP. PERFORMED OPERATIONAL TEST OF THE EMERGENCY LIGHTS PER THE AMM 33-51-00. OPS CHECK GOOD AT THIS TIME.
- [SDR SWAA2026061110081](https://openairdocs.org/sdr/SWAA2026061110081.md): Door · open · Jun 7, 2026 · N298WN · Boeing 7377H4 · Accessory Compartment Doors
  > ON CLIMB OUT VIBRATION NOTED CLIMBING ABOVE FL260, ON POST FLIGHT WALKAROUND NOTICED GROUND POWER DOOR OPEN. PERFORMED AIRFRAME CONDITION INSPECTION IAW AMM 05-51-67. FOUND EXT PWR LEFT OPEN. INSPECTED DOOR WITH NO DAMAGE IN OPENED AND CLOSED POSITIONS NOTED
- [SDR SWAA2026040385368](https://openairdocs.org/sdr/SWAA2026040385368.md): Handle · broken · Apr 1, 2026 · N298WN · Boeing 7377H4 · Passenger/Crew Doors
  > FWD ENTRY DOOR ASSIST HANDLE BROKE OFF. INSTALLED L1 DOOR HANDLE IAW AMM 52-11-31. OK TO CONTINUE ON MEL 25-10-01; SP1B C/W.
- [SDR SWAA2026031980273](https://openairdocs.org/sdr/SWAA2026031980273.md): Sign · broken · Mar 16, 2026 · N298WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT ROW SIGN MID CABIN ATTACHED TO THE CEILING IS BROKEN. REMOVED AND REPLACED MID CABIN CEILING EMERGENCY LIGHT IAW AMM 33-51-01. OPS CHECK GOOD.
- [SDR SWAA2026022573948](https://openairdocs.org/sdr/SWAA2026022573948.md): Counter · odor · Feb 24, 2026 · N298WN · Boeing 7377H4 · Instrument Panel
  > ELECTRICAL ODOR COMING FROM FO YOKE TRIP COUNTER. REMOVED AND REPLACED FO'S TRIP COUNTER IAW MM 33-11-00.
- [SDR SWAA2026012965750](https://openairdocs.org/sdr/SWAA2026012965750.md): Lamp · damaged · Jan 29, 2026 · N298WN · Boeing 7377H4 · Emergency Lighting
  > FWD ENTRY EMERGENCY EXIT LENS HOUSING & LAMP ASSY FOUND DAMAGED. REMOVED & REPLACED IAW AMM 33-51-01-960-802-NG. OPS TESTED GOOD.
- [SDR SWAA2026012764351](https://openairdocs.org/sdr/SWAA2026012764351.md): Sign · detached · Jan 24, 2026 · N298WN · Boeing 7377H4 · Emergency Lighting
  > FWD GALLEY EXIT SIGN FELL DOWN. COMPLIED WITH EA 26-133-00249, REV A.
- [SDR SWAA2025101624569](https://openairdocs.org/sdr/SWAA2025101624569.md): Cover · broken · Oct 15, 2025 · N298WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT COVER BROKEN FWD OF LH OVERWING EXIT DOOR. R & R EMERGENCY EXIT LIGHT COVER FWD OF LH OVERWING EXIT DOOR IAW AMM 33-51-01.
- [SDR SWAA2025092918436](https://openairdocs.org/sdr/SWAA2025092918436.md): Girt Bar · out of position · Sep 26, 2025 · N298WN · Boeing 7377H4 · Emergency Equipment
  > R1 FWD SERVICE DOOR GIRT BAR HANGS LOW. REPACKED CABIN R1 FWD SERVICE DOOR GIRT BAR IAW AMM 25-66-01.
- [SDR SWAA2025092918437](https://openairdocs.org/sdr/SWAA2025092918437.md): Girt Bar · out of position · Sep 26, 2025 · N298WN · Boeing 7377H4 · Emergency Equipment
  > CABIN - L1 FWD ENTRY DOOR GIRT BAR HANGS LOW. REPACKED L-1 DOOR SLIDE GIRT BAR IAW AMM 25-66-01-000-804-NG.
- [SDR SWAA2025090209200](https://openairdocs.org/sdr/SWAA2025090209200.md): Tailpipe · fire · Aug 27, 2025 · N298WN · Boeing 7377H4 · Engine Collector/Tailpipe/Nozzle
  > RAMP TOWER REPORTED POSSIBLE TAIL PIPE FIRE LT ENGINE. NO ABNORMAL INDICATION IN COCKPIT, ON TAXI OUT WITH BOTH ENGINES RUNNING GROUND CONTROL REPORTS TAIL PIPE FLAME AS ACFT APPROACHED TAXIWAY LIMA. CREW SUCH DOWN ENGINE AFTER RECEIVING REPORT. ADDED OIL AFT
- [SDR SWAA2025062081444](https://openairdocs.org/sdr/SWAA2025062081444.md): Flashlight · inoperative · Jun 13, 2025 · N298WN · Boeing 7377H4 · Emergency Equipment
  > FWD L/H WINDSCREEN LOWER FLASHLIGHT INOP <[01]. REMOVED AND REPLACED FWD L/H WINDSCREEN LOWER FLASHLIGHT BATTERY IAW AMM 25-64-00-900-806. OPERATIONAL CHECK WAS 'GOOD'. INSTALLED NEW BATTERY P/N: P4-01-0021.; [02] VERIFIED.
- [SDR SWAA2025061781447](https://openairdocs.org/sdr/SWAA2025061781447.md): Fuse · open · Jun 13, 2025 · N298WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS L1365; L751 ASSOCIATED WITH BATTERY PACK M1668 ARE INOPERATIVE. REPLACED FUSE AT POWER SUPPLY M1668 AND PERFORMED GOOD TEST IAW AMM 33-51-06-960-804 AND WDM 33-51-13.
- [SDR SWAA2025061781446](https://openairdocs.org/sdr/SWAA2025061781446.md): Battery Pack · inoperative · Jun 13, 2025 · N298WN · Boeing 7377H4 · Emergency Lighting
  > ALL EMERGENCY EXIT LIGHTS ASSOCIATED WITH M1670 BATTERY PACK ARE INOP. REMOVED AND REPLACED BATTERY PACK M1670 AND PERFORMED GOOD INSTALLATION TEST; PER AMM 33-51-06-960-805.
- [SDR SWAA2025061781445](https://openairdocs.org/sdr/SWAA2025061781445.md): Fuse · open · Jun 13, 2025 · N298WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT L1365; L751 & L1605 ASSOCIATED WITH M1669 BATTERY PACK ARE INOPERATIVE. REPLACED FUSE AT POWER SUPPLY M1669 AND PERFORMED GOOD TEST IAW AMM 33-51-06-960-804 AND WDM 33-51-13.
- [SDR SWAA2025061781240](https://openairdocs.org/sdr/SWAA2025061781240.md): Battery Pack · inoperative · Jun 13, 2025 · N298WN · Boeing 7377H4 · Emergency Lighting
  > ALL ASSOCIATED LIGHTS INOP WITH M1674 EMERGENCY BATTERY PACK. REMOVED AND REPLACED M1674 EMERGENCY BATTERY PACK AND PERFORMED GOOD OPERATIONAL TEST IAW AMM 33-51-06-960-805.
- [SDR SWAA2025062078296](https://openairdocs.org/sdr/SWAA2025062078296.md): Rib · cracked · Jun 4, 2025 · N298WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACKED ON LOWER AREA OF STIFFENER 2 INSPAR RIB 6, STAB STA 120.30. REPAIRED AT LOWER AREA OF STIFFENER 2 INSPAR RIB 6 STAB STA 120.30 PER SRM 55-10-09-2R-4 REP 4.
- [SDR SWAA2025062078297](https://openairdocs.org/sdr/SWAA2025062078297.md): Rib · cracked · Jun 4, 2025 · N298WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACKED ON LOWER AREA OF STIFFENER 4 INSPAR RIB 6, STAB STA 120.30. REPAIRED AT LOWER AREA OF STIFFENER 4 INSPAR RIB 6 STAB STA 120.30 PER SRM 55-10-09-2R-4 REP 4.
- [SDR SWAA2025061777526](https://openairdocs.org/sdr/SWAA2025061777526.md): Panel · debonded · Jun 2, 2025 · N298WN · Boeing 7377H4 · Aerodynamic Fairings
  > PANEL 193AR INNER SURFACE HAS MULTIPLE DISBONDS. PANEL 193AR WAS REPLACED ON CUSTOMER FAULT TTG8Q010RK8D.
- [SDR SWAA2025062075888](https://openairdocs.org/sdr/SWAA2025062075888.md): Fitting · cracked · May 28, 2025 · N298WN · Boeing 7377H4 · Elevator Structure
  > WHILE REMOVING LT STAB INSPAR RIB AT STAB STA 111.10 FOUND CRACK IN #3 ELEVATOR HINGE RIB FITTING AT FWD FLANGE. <[01] 04 - REPAIRED PER [EA EA-COMPONENT (EA ATTACHED TO A FAULT FOR A TRACKED COMPONENT)] #EA 25-155-01438; [02] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2025061775508](https://openairdocs.org/sdr/SWAA2025061775508.md): Stringer · cracked · May 27, 2025 · N298WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT FWD CABIN BS297 S-7L WL275. THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-00-03-2R-1 REPAIR 1 AND EA 25-153-01407 WITH AN INSPECTION PROGRAM DEFINED IN 25-153-01407-INSP.
- [SDR SWAA2025061775509](https://openairdocs.org/sdr/SWAA2025061775509.md): Frame · cracked · May 27, 2025 · N298WN · Boeing 7377H4 · Fuselage Main, Frame
  > PASSENGER CABIN FED UPPER FRAME BS 312 STR 5L CRACKED. REMOVED DAMAGE ON PASSENGER CABIN FED UPPER FRAME BS 312 STR 5L I.A.W SRM 51-10-02-0G-0 AND M-22-153-01244 CUSTOMER CARD TTG8Q011B7S2. FINAL RESOLUTION ON TTG8Q011B7S2.
- [SDR SWAA2025062075339](https://openairdocs.org/sdr/SWAA2025062075339.md): Intercostal · cracked · May 26, 2025 · N298WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FED INTERCOSTAL CRACKED AT BS295.5 STR16L; WL216. REMOVED AND REPLACED INTERCOSTAL BS 294-BS 303 S16L WL216 PER SRM 51-40-02 AND DWG 141A8180 REV: C. REJECT CORRECTIVE ACTION, TOO SHORT HI LOCK ON INTERCOSTAL BS295.5 STR16L; WL216. REMOVED AND REPLACED 1
- [SDR SWAA2025062074866](https://openairdocs.org/sdr/SWAA2025062074866.md): Sidewall Support · corroded · May 24, 2025 · N298WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MULTIPLE SPOTS OF CORROSION ON FCB RH SIDE FLOOR TO SIDEWALL SUPPORT NUTPLATES BS500A TO BS500D; RBL22;WL156. REMOVED AND REPLACED FCB SIDEWALL SUPPORT<BR>BS 500 TO BS 500D RBL 22 WL 156 IAW SRM 51-40-02 AND DWG 143A7500 REV: -.
- [SDR SWAA2025062074867](https://openairdocs.org/sdr/SWAA2025062074867.md): Sidewall Support · corroded · May 24, 2025 · N298WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MULTIPLE SPOTS OF CORROSION ON FCB LH SIDE FLOOR TO SIDEWALL SUPPORT NUTPLATES BS460 TO BS500D; RBL22;WL156. MULTIPLE SPOTS OF CORROSION ON FCB LH SIDE FLOOR TO SIDEWALL SUPPORT NUTPLATES BS460 TO BS500D LBL22WL156. REMOVED AND REPLACED SIDEWALL SUPPORT BS39
- [SDR SWAA2025062074868](https://openairdocs.org/sdr/SWAA2025062074868.md): Support · corroded · May 24, 2025 · N298WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FCB FLOOR TO AFT BULKHEAD SUPPORT BS500D FROM RBL22 TO LBL22 WL156. REMOVED AND REPLACED FCB FLOOR TO AFT BULKHEAD SUPPORT BS500D RBL22 TO LBL22 WL156 IAW SRM 51-40-02-0G-0 AND DWG 143A9481 REV: -.
- [SDR SWAA2025062074873](https://openairdocs.org/sdr/SWAA2025062074873.md): Sidewall Support · corroded · May 24, 2025 · N298WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON ACB RH SIDE FLOOR TO SIDEWALL SUPPORT AT BS927+3 RBL16 WL156. REMOVED AND REPLACED ON ACB RH FLOOR TO SIDEWALL SUPPORT FROM BS 887 TO BS 947 RBL16 IAW SRM 51-40-02 AND DWG 147A7500 ID: 0011 REV: -.
- [SDR SWAA2025062075333](https://openairdocs.org/sdr/SWAA2025062075333.md): Shield · corroded · May 24, 2025 · N298WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON ACB FWD SHIELD NUTPLATES B767 TO BS787 RBL22 WL156. REMOVED AND REPLACED NEW ON ACB FWD SHIELD BS767 TO BS794 RBL22 IAW SRM 51-40-02 AND DWG 146A0081 ID: 0028 REV: A.
- [SDR SWAA2025061774864](https://openairdocs.org/sdr/SWAA2025061774864.md): Web · corroded · May 24, 2025 · N298WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MULTIPLE SPOT WITH CORROSION ON FCB DOOR CUTOUT SURROUND THRESHOLD BS440+15; 460+3;460+6;BS460+17; RBL29, WL156. REMOVED AND REPLACED SUBTHRESHOLD WEB AT BS440 TO BS496 IAW SRM 51-40-02 AND DWG# 143A8330 ID: 0042 REV: A..
- [SDR SWAA2025061774865](https://openairdocs.org/sdr/SWAA2025061774865.md): Shield · corroded · May 24, 2025 · N298WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MULTIPLE SPOTS OF CORROSION ON FCB FWD SHIELD NUT PLATES BS420 TO BS440 RBL24 WL156. REMOVED AND INSTALLED NEW FCB FWD SHIELD BS420 TO BS440 RBL24 WL156 P/N 143A8126-21 LOT: 1603244-7 IAW 51-40-02-0G-0 AND DWG 143A0080.
- [SDR SWAA2025061776458](https://openairdocs.org/sdr/SWAA2025061776458.md): Shield · corroded · May 24, 2025 · N298WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MULTIPLE SPOTS OF CORROSION ON FCB AFT SHIELD NUTPLATES BS480+13 TO BS500A; RBL22;WL156. REMOVED AND REPLACED FCB AFT SHIELD P/N 143A8126-31 LOT: 1594230-1 BS496 TO BS500A RBL22 WL156 IAW SRM 51-40-02-0G-0 AND DWG 143A0080 REV: -.
- [SDR SWAA2025061775702](https://openairdocs.org/sdr/SWAA2025061775702.md): Support · corroded · May 24, 2025 · N298WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MULTIPLE SPOTS OF CORROSION ON FCB FWD SHIELD NUTPLATES BS 400 TO BS 420, RBL24, WL156. REMOVED AND REPLACED FCB FLOOR TO SIDEWALL SUPPORT BS 400 TO BS 420, RBL24, WL156 IAW SRM 51-40-02 AND DWG# 143A7500 REV-.
- [SDR SWAA2025061774566](https://openairdocs.org/sdr/SWAA2025061774566.md): Seat Track · cracked · May 23, 2025 · N298WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > F/O'S FWD I/B SEAT TRACK CRACKED. REMOVED AND REPLACED F/O'S FWD I/B SEAT TRACK PER AMM 25-11-11-400-801.
- [SDR SWAA2025062073749](https://openairdocs.org/sdr/SWAA2025062073749.md): Rib · cracked · May 21, 2025 · N298WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > SUSPECT CRACK ON UPPER AREA OF STIFFENER 2 INSPAR RIB 5 (STAB STA 110). REPAIRED THE UPPER AREA OF STIFFENER 2 IN SPAR RIB 5 (STAB STA 110) APPLIED A FILLET SEAL; FINISH; AND CIC IAW SRM 55-10-09-2R-4 REP 4. REPAIRED THE L/H HORIZONTAL STAB UPPER AREA OF S
- [SDR SWAA2025062073750](https://openairdocs.org/sdr/SWAA2025062073750.md): Rib · cracked · May 21, 2025 · N298WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACKED ON LOWER AREA OF STIFFENER 3 INSPAR RIB 6. STAB STA 120, LT HORIZONTAL STAB. REPAIRED AT LOWER AREA OF STIFFENER 3 INSPAR RIB 6 STAB STA 120.30 PER SRM 55-10-09-2R-4 REP 4.
- [SDR SWAA2025061773751](https://openairdocs.org/sdr/SWAA2025061773751.md): Support Angle · cracked · May 21, 2025 · N298WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED ON UPPER FLOOR SUPPORT ANGLE AT BS927+4; BL0; WL 208. REMOVED AND REPLACED UPPER SUPPORT ANGLE BETWEEN BS 927 TO BS 947 BL 0 PER SRM 51-40-02-0G-0 AND DWG 147A5400 REV-.
- [SDR SWAA2025061773518](https://openairdocs.org/sdr/SWAA2025061773518.md): Intercostal · cracked · May 21, 2025 · N298WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT FWD WET AREA BS390 RBL41 WL208. REMOVED AND REPLACED ANGLE AT FLOOR STRUCTURE RBL 41 WL 208 BETWEEN BS 380 TO BS 400 PER SRM 51-40-02 AND DWG 143A5400 REV -.
- [SDR SWAA2025061773519](https://openairdocs.org/sdr/SWAA2025061773519.md): Intercostal · cracked · May 21, 2025 · N298WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT FWD WET AREA BS394 LBL13 WL208. REMOVED AND REPLACED THE CRACKED INTERCOSTAL UPPER ANGLE FROM BS-380 TO BS-400; LBL13; WL208 IAW SRM 51-40-02 AND DWG#143A5400 REV:-.
- [SDR SWAA2025061773517](https://openairdocs.org/sdr/SWAA2025061773517.md): Attach Angle · cracked · May 21, 2025 · N298WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED ATTACH ANGLE AT FWD CABIN BS294 RBL54 WL208. REMOVED AND REPLACED ATTACH ANGLE BS 291.5 TO 294 WL 208 RBL 54 PER SRM 51-40-02 AND DWG 141A8310 REV D.
- [SDR SWAA2025061773490](https://openairdocs.org/sdr/SWAA2025061773490.md): Floor Panel · pulled · May 21, 2025 · N298WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241UF UPPER SURFACE HAS AREAS OF PULLED STRANDS. FLOOR PANEL 241UF UPPER SURFACE; WITH AREAS OF PULLED STRANDS; WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.
- [SDR SWAA2025061773509](https://openairdocs.org/sdr/SWAA2025061773509.md): Floor Panel · pulled · May 21, 2025 · N298WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 221FF UPPER SURFACE DELAMINATED. FWD FLOOR PANEL 221FF UPPER SURFACE WITH DELAMINATIONS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.
- [SDR SWAA2025061773500](https://openairdocs.org/sdr/SWAA2025061773500.md): Floor Panel · delaminated · May 21, 2025 · N298WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241YF UPPER SURFACE DELAMINATED. AFT FLOOR PANEL 241YF UPPER SURFACE DELAMINATED WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2025061773512](https://openairdocs.org/sdr/SWAA2025061773512.md): Floor Panel · delaminated · May 21, 2025 · N298WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241AAF UPPER SURFACE DELAMINATED. AFT FLOOR PANEL 241AAF; WITH UPPER SURFACE DELAMINATION; WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0 AND DRAWING 147A5810 SHEET 8.
- [SDR SWAA2025061773502](https://openairdocs.org/sdr/SWAA2025061773502.md): Floor Panel · delaminated · May 21, 2025 · N298WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241ABF UPPER SURFACE DELAMINATED. UPPER SURFACE DELAMINATION ON AFT FLOOR PANEL 241ABF WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2025061773508](https://openairdocs.org/sdr/SWAA2025061773508.md): Floor Panel · delaminated · May 21, 2025 · N298WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 242VF UPPER SURFACE DELAMINATED. AFT FLOOR PANEL 242VF UPPER SURFACE DELAMINATED; WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2025061773496](https://openairdocs.org/sdr/SWAA2025061773496.md): Floor Panel · delaminated · May 21, 2025 · N298WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 222AF UPPER SURFACE DELAMINATED. FWD FLOOR PANEL 222AF WITH UPPER SURFACE DELAMINATED WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2025061773511](https://openairdocs.org/sdr/SWAA2025061773511.md): Floor Panel · delaminated · May 21, 2025 · N298WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241XF UPPER SURFACE DELAMINATED. AFT FLOOR PANEL 241XF WITH UPPER SURFACE DELAMINATED WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2025061773501](https://openairdocs.org/sdr/SWAA2025061773501.md): Floor Panel · delaminated · May 21, 2025 · N298WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241ZF UPPER SURFACE DELAMINATED. AFT FLOOR PANEL 241ZF WITH UPPER SURFACE DELAMINATED WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2025061773503](https://openairdocs.org/sdr/SWAA2025061773503.md): Floor Panel · delaminated · May 21, 2025 · N298WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241ACF UPPER SURFACE DELAMINATED. REPAIRED PER SRM 53-00-50-2R-1-A00939 REPAIR 1 - REPAIR OF DAMAGE TO ONE FACESHEET IN COMPOSITE FLOOR PANELS - PERMANENT.
- [SDR SWAA2025061773506](https://openairdocs.org/sdr/SWAA2025061773506.md): Floor Panel · delaminated · May 21, 2025 · N298WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 242SF UPPER SURFACE DELAMINATED. REPAIRED PER SRM 53-00-50-2R-1-A00939 REPAIR 1.

Next page: https://openairdocs.org/aircraft/N298WN/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 = 'N298WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N298WN/reports

---
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.