# Service difficulty reports: N297WN

A list on [N297WN](https://openairdocs.org/aircraft/N297WN.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 7 · 308 reports

- [SDR SWAA2026102122860](https://openairdocs.org/sdr/SWAA2026102122860.md): Panel · cracked · Oct 17, 2026 · N297WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > RIGHT MLG AFT SHELF PANEL WAS CRACKED. REPLACED FAIRING CAP IAW AMM 57-50-02 & 20-50-11.
- [SDR SWAA2026081024513](https://openairdocs.org/sdr/SWAA2026081024513.md): Girt Bar · unpacked · Aug 6, 2026 · N297WN · Boeing 7377H4 · Emergency Equipment
  > FWD SERVICE DOOR R1 EMERGENCY EXIT SLIDE GIRT BAR HANGS TOO LOW. REPACKED FWD SERVICE DOOR R1 EMERGENCY EXIT SLIDE IAW MT 725-61-06.
- [SDR SWAA2026081046196](https://openairdocs.org/sdr/SWAA2026081046196.md): Slide · out of tolerance · Aug 6, 2026 · N297WN · Boeing 7377H4 · Escape Slide
  > FWD ENTRY DOOR L1 EMERGENCY EXIT SLIDE GIRT BAR HANGS TOO LOW. REPACKED FWD ENTRY DOOR L1 EMERGENCY EXIT SLIDE IAW MT 725-61-06
- [SDR SWAA2026032381201](https://openairdocs.org/sdr/SWAA2026032381201.md): Flap · debonded · Mar 19, 2026 · N297WN · Boeing 7377H4 · Trailing Edge Flaps
  > LEFT WING TRAILING EDGE INBD FLAP HAS DISBONDING ON LOWER SKIN 2 FROM OTBD TRAILING EDGE CORNER 17 AT LONGEST AND 4 AT WIDEST AND SPLIT AT TRAILING EDGE MEASURING 17. REPAIRED LT WING INBD FLAP TRAILING EDGE ON LOWER SKIN 2 INCH FROM OTBD TRAILING EDGE CORNER
- [SDR SWAA2026030976248](https://openairdocs.org/sdr/SWAA2026030976248.md): Sign · broken · Mar 3, 2026 · N297WN · Boeing 7377H4 · Emergency Lighting
  > CEILING EXIT SIGN MID-CABIN BROKEN. R & R CEILING EXIT LIGHT ASSY IAW AMM 33-51-01.
- [SDR SWAA2025110632076](https://openairdocs.org/sdr/SWAA2025110632076.md): Tensioner · loose · Nov 5, 2025 · N297WN · Boeing 7377H4 · Emergency Equipment
  > GALLEY SERVICE DOOR GIRT BAR TENSIONER LOOSE. RESECURED PER SIP.
- [SDR SWAA2025091714766](https://openairdocs.org/sdr/SWAA2025091714766.md): Girt Bar · out of adjust · Sep 15, 2025 · N297WN · Boeing 7377H4 · Emergency Equipment
  > FWD SERVICE DOOR GIRT BAR NEEDS ADJUSTMENT. OK TO CONTINUE ON TLD PER EA M-23-125-01839.
- [SDR SWAA2025070787693](https://openairdocs.org/sdr/SWAA2025070787693.md): Handle · loose · Jul 3, 2025 · N297WN · Boeing 7377H4 · Passenger/Crew Doors
  > AFT ENTRY DOOR HANDLE IS LOOSE. TIGHTENED AFT ENTRY DOOR HANDLE IAW AMM 52-13-31-400-802.
- [SDR SWAA2025070787696](https://openairdocs.org/sdr/SWAA2025070787696.md): Handle · loose · Jul 3, 2025 · N297WN · Boeing 7377H4 · Service Doors
  > FWD SERVICE DOOR HANDLE IS LOOSE. TIGHTENED FWD SERVICE DOOR HANDLE IAW AMM 25-21-35-420-801.
- [SDR SWAA2025070787686](https://openairdocs.org/sdr/SWAA2025070787686.md): Lamp · inoperative · Jul 2, 2025 · N297WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT SLIDE LIGHT IS INOPERATIVE ON RIGHT SIDE OF FUSELAGE. REPLACED EMERGENCY EXIT SLIDE LAMP AT AFT RIGHT SIDE OF FUSELAGE IAW AMM 33-51-04-960-801. OPS TEST GOOD.
- [SDR SWAA2025070780579](https://openairdocs.org/sdr/SWAA2025070780579.md): Baffle · cracked · Jun 11, 2025 · N297WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > DURING OK TO INSTALL SIDEWALL SUPPORT FOUND BUFFLE CRACKED AT FCB STA 400 APPROX. LBL 23 AND WL 156; MARKED<[01] REMOVED AND REPLACED BAFFLE P/N 143A7510-33 LOT 1596926-3 BS TO BS396 TO BS420 LBL23 WL156 IAW SRM 51-40-02-0G-0 AND DWG 143A7505 REV: -.
- [SDR SWAA2025070780208](https://openairdocs.org/sdr/SWAA2025070780208.md): Sign · damaged · Jun 10, 2025 · N297WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT MOUNTED ON PANEL 232YJW IS DAMAGED. REMOVED AND REPLACED EMERGENCY EXIT LIGHT SIGN ON PANEL 232YJW PER AMM 33-51-01-960-802. PANEL 232YJW WILL BE INSTALLED ON CLOSE CARD TTG8Q01099ZV.
- [SDR SWAA2025070780209](https://openairdocs.org/sdr/SWAA2025070780209.md): Lens · damaged · Jun 10, 2025 · N297WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT LENS ON PANEL 232YJW IS DAMAGED. REMOVED AND REPLACED EMERGENCY EXIT LIGHT LENS ON PANEL 232YJW WITH P/N 82000-37709ATS SN/LOT 1439779-1 PER AMM 33-51-01-960-802 3C5C AND 3C10.
- [SDR SWAA2025070780215](https://openairdocs.org/sdr/SWAA2025070780215.md): Stub Frame · cracked · Jun 10, 2025 · N297WN · Boeing 7377H4 · Service Doors
  > 1 CRACK NOTED ON R1 DOOR STUB FRAME, LOCATED 0.7' ABOVE SEAL DEPRESSOR; LENGTH: 2.5'. ENGINEERING TSR REQUIRED. REMOVED AND REPLACED R1 DOOR UPPER STUB FRAME IAW SRM 51-40-02 & DWG 141A8370 REV C, INSTALLED AND ADJUSTED FORWARD UPPER LATCH RECIEVER ON FSD
- [SDR SWAA2025070779843](https://openairdocs.org/sdr/SWAA2025070779843.md): Baffle · cracked · Jun 9, 2025 · N297WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FCB BS440 - BS480; BS500 - BS500D; LBL23 WL156. DURING OK TO INSTALL SIDEWALL SUPPORT FOUND BAFFLE CRACKED AT FCB STA 400 APPROX. LBL 23 AND WL 156; REMOVED AND REPLACED SIDEWALL SUPPORT AT FCB BS 396-BS 500D LBL 23
- [SDR SWAA2025070779844](https://openairdocs.org/sdr/SWAA2025070779844.md): Shield · corroded · Jun 9, 2025 · N297WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT SHIELD AT FCB BS500 - BS500A RBL24 WL156.<[01] REMOVED AND REPLACED FCB SHIELD AT BS500-BS500A RBL 24 WL 156<BR>IAW SRM 51-40-05 IAW SRM 51-40-02 AND DWG 143A0080 REV: C<BR>CARD COMPLETED;[02] VERIFIED CORRECTIVE ACTION
- [SDR SWAA2025070779660](https://openairdocs.org/sdr/SWAA2025070779660.md): Scuff Plate · cracked · Jun 9, 2025 · N297WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR FWD CORNER SCUFF PLATE IS CRACKED. REPAIRED FWD CARGO DOOR FWD CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1 PARAGRAPH 4.B.(2). REFER TO SOPM 20-30-02 AND APPLIED CHEMICAL CONVERSION IAW SOPM 20-43-03; TYPE 2; CLASS A OR C.
- [SDR SWAA2025070780044](https://openairdocs.org/sdr/SWAA2025070780044.md): Support Angle · pulled · Jun 9, 2025 · N297WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > FASTENER HEADS FOR I/B SUPPORT ANGLE PULLED THROUGH ON L/W PANEL 551GB. REPAIRED PER SRM 51-70-04-2R-9-A00753, REPAIR 9 - REPAIR OF DAMAGE TO A FASTENER HOLE WITH LAMINATING RESIN AND CHOPPED FIBER.
- [SDR SWAA2025070779368](https://openairdocs.org/sdr/SWAA2025070779368.md): Floorbeam · cracked · Jun 8, 2025 · N297WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACKED FLOOR BEAM AT FWD CABIN BS294 RBL52 WL208.<[01] FLOOR BEAM 294 WAS REPAIRED IAW B737-7 SRM 53-10-51-2R-16 REPAIR 16 THIS REPAIR IS CATEGORY A.(CATEGORY A REPAIR: A PERMANENT REPAIR FOR WHICH THE INSPECTIONS GIVEN IN THE MAINTENANCE PLANNING DATA (MPD)
- [SDR SWAA2025070779371](https://openairdocs.org/sdr/SWAA2025070779371.md): Support · corroded · Jun 8, 2025 · N297WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB LBL20 BS727B - BS807 WL156.<[01] REMOVED AND REPLACED ACB FLOOR TO SIDEWALL SUPPORT BS727 TO BS847 LBL20 WL156 IAW SRM 51-40-02 AND DWG 146A7500 REV B.;[02] COMPLETE;[03] COMPLETE
- [SDR SWAA2025070779651](https://openairdocs.org/sdr/SWAA2025070779651.md): Support · corroded · Jun 8, 2025 · N297WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB RBL20 BS727A - BS767 WL156.<[01] REMOVED AND REPLACED ACB FLOOR TO SIDEWALL SUPPORT BS727 TO BS767 RBL20 WL156 IAW SRM 51-40-02 AND DWG 146A7500 REV B.;[02] COMPLETE
- [SDR SWAA2025070779654](https://openairdocs.org/sdr/SWAA2025070779654.md): Shield · corroded · Jun 8, 2025 · N297WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD SHIELD AT ACB BS767 - BS787 RBL22 WL156.<[01] REMOVED AND REPLACED ACB FWD SHIELD BS 767-787 RBL 22 WL 156 IAW SRM 51-40-02 AND BOEING DWG 146A0081 REV: A.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2025070779366](https://openairdocs.org/sdr/SWAA2025070779366.md): Floor Support · cracked · Jun 8, 2025 · N297WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT FWD CABIN BS380 - BS400 RBL9 WL208. REMOVED AND REPLACED ANGLE (INTERCOSTAL) IAW B737-7 SRM 51-40-02-0G-0 AND DWG:143A5400 ID:0006 REV: -.
- [SDR SWAA2025070779367](https://openairdocs.org/sdr/SWAA2025070779367.md): Floor Support · cracked · Jun 8, 2025 · N297WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT FWD CABIN BS380 - BS400 RBL41 WL208. REMOVED AND REPLACED CRACKED ANGLE (INTERCOSTAL) IAW B737-7 SRM 51-40-02-0G-0 AND DWG143A5400 ID:0006 REV: -.
- [SDR SWAA2025070779652](https://openairdocs.org/sdr/SWAA2025070779652.md): Tie Down · corroded · Jun 8, 2025 · N297WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON TRACK TIEDOWN AT ACB BS790 LBL17 WL157. ALL STEPS COMPLETE. REMOVED CORROSION ON TRACK TIEDOWN AT ACB BS790 LBL17 WL157; L=6.8' W=1.2' D=0.024' ON THE TOP SURFACE OF THE TRACK AND L=1.8' W=0.8' D=0.043' IN THE BOTTOM SURFACE OF THE TRACK; FOUND
- [SDR SWAA2025070779657](https://openairdocs.org/sdr/SWAA2025070779657.md): Support Angle · corroded · Jun 8, 2025 · N297WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT ACB BS947 RBL12 WL180. REMOVED AND REPLACED AFT BULKHEAD LOWER SUPPORT ANGLE BS947 RBL20 TO LBL10 WL180 IAW SRM 51-40-02-0G-0; IAW SRM 51-40-05-0G-0 AND DWG # 149A8117 REV:C. RII REJECTION OF STEP 2: AFT BU
- [SDR SWAA2025070779658](https://openairdocs.org/sdr/SWAA2025070779658.md): Support Fitting · cracked · Jun 8, 2025 · N297WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED SUPPORT FITTING AT ACB BS947 LBL10 WL180. MARKED<[01] REMOVED AND REPLACED SUPPORT FITTING P/N 149A8113U6 AT ACB BS947 LBL10 WL180 IAW SRM 51-40-02 AND DWG 149A8103 REV D.;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2025070779659](https://openairdocs.org/sdr/SWAA2025070779659.md): Support Angle · cracked · Jun 8, 2025 · N297WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE AT ACB BEHIND WATER SERVICE PANEL BS 918, RBL 10, WL 177. REMOVED AND REPLACED SUPPORT ANGLE P/N 147A7221Y32 AT ACB BEHIND WATER SERVICE PANEL BS 907+11, RBL 7 TO RBL 18 IAW SRM 51-40-02 AND DWG 147A7221 REV D.
- [SDR SWAA2025070778858](https://openairdocs.org/sdr/SWAA2025070778858.md): Floor Panel · pulled · Jun 6, 2025 · N297WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 231FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231FF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.
- [SDR SWAA2025070778860](https://openairdocs.org/sdr/SWAA2025070778860.md): Floor Panel · pulled · Jun 6, 2025 · N297WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 231MF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231MF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2025070778861](https://openairdocs.org/sdr/SWAA2025070778861.md): Floor Panel · pulled · Jun 6, 2025 · N297WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 232DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 232DF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).
- [SDR SWAA2025070778866](https://openairdocs.org/sdr/SWAA2025070778866.md): Floor Panel · pulled · Jun 6, 2025 · N297WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241XF UPPER SKIN HAS AN AREA OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241XF; UPPER SKIN WITH AREAS OF PULLED STRANDS; WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2025070778869](https://openairdocs.org/sdr/SWAA2025070778869.md): Floor Panel · cracked · Jun 6, 2025 · N297WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 242UF LOWER SKIN IS CRACKED AT O/B FWD CORNER. (MARKED)<[01] AFT FLOOR PANEL 242UF; WITH LOWER SKIN CRACK; AT THE O/B FWD CORNER; WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025070778870](https://openairdocs.org/sdr/SWAA2025070778870.md): Floor Panel · pulled · Jun 6, 2025 · N297WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] REPAIRED AFT FLOOR PANEL 242VF UPPER SKIN IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2025070778871](https://openairdocs.org/sdr/SWAA2025070778871.md): Floor Panel · cracked · Jun 6, 2025 · N297WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 242XF UPPER SKIN IS CRACKED NEAR CENTER OF PANEL. (MARKED)<[01] AFT FLOOR PANEL 242XF UPPER SKIN WAS CRACKED NEAR CENTER OF PANEL AND REPAIRED IAW SRM 53-00-50-2R-1;[02] VERIFIED COMPLETE
- [SDR SWAA2025070779082](https://openairdocs.org/sdr/SWAA2025070779082.md): Floor Panel · pulled · Jun 6, 2025 · N297WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 241VF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025070779083](https://openairdocs.org/sdr/SWAA2025070779083.md): Floor Panel · pulled · Jun 6, 2025 · N297WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241WF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 241WF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025070778863](https://openairdocs.org/sdr/SWAA2025070778863.md): Floor Panel · pulled · Jun 6, 2025 · N297WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 232JF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 232JF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1
- [SDR SWAA2025070779086](https://openairdocs.org/sdr/SWAA2025070779086.md): Floor Panel · cracked · Jun 6, 2025 · N297WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 221GF FWD O/B TANG IS CRACKED.<[01] FLOOR PANEL 221GF WITH CRACKED FORWARD TANG WAS REPAIRED IAW SRM 53-00-50-2R-1 AND DWG 141A5810 ID:0181;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2025070779084](https://openairdocs.org/sdr/SWAA2025070779084.md): Floor Panel · pulled · Jun 6, 2025 · N297WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 221BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 221BF WITH AREAS OF UPPER PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1 AND DWG 141A5810 ID:0056;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2025070778878](https://openairdocs.org/sdr/SWAA2025070778878.md): Tee Angle · corroded · Jun 6, 2025 · N297WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION ON BS986 UPPER T-CHORD PREVIOUS REPAIR AT NUTPLATE HOLES AT RBL40 AND RBL43<[01] REMOVED AND REPLACED BS986 UPPER T-CHORD PREVIOUS REPAIR R/H IAW SRM 51-40-02 AS SHOWN IN SWA EA 23-153-02176 REV 1.;[02] REJECT: 2 EA COLLARS MISSING AT REPAIR AREA; BS
- [SDR SWAA2025070778859](https://openairdocs.org/sdr/SWAA2025070778859.md): Floor Panel · pulled · Jun 6, 2025 · N297WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 231JF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 231JF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION STEP 1.
- [SDR SWAA2025070778862](https://openairdocs.org/sdr/SWAA2025070778862.md): Floor Panel · pulled · Jun 6, 2025 · N297WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 232FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 232FF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTIONS STEP 1.
- [SDR SWAA2025070778864](https://openairdocs.org/sdr/SWAA2025070778864.md): Floor Panel · pulled · Jun 6, 2025 · N297WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 241AF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION STEP 1.
- [SDR SWAA2025070778873](https://openairdocs.org/sdr/SWAA2025070778873.md): Door Frame · cracked · Jun 6, 2025 · N297WN · Boeing 7377H4 · Fuselage Main, Structure
  > PASSENGER CABIN FWD ENTRY DOOR STOP FITTING WEB CRACKED BS295 S-16L. REMOVED AND REPLACED ON CABIN FWD ENTRY DOOR FITTING WEB BS295 TO BS303.81 S-16L IAW SRM 51-40-02 AND DWG 141A8180 ID: 0027 REV: C
- [SDR SWAA2025070778875](https://openairdocs.org/sdr/SWAA2025070778875.md): Strap · corroded · Jun 6, 2025 · N297WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > TENSION STRAP CORRODED AT BS1015; BS1017; BS1016+4 AND BS1016+12 RBL3. REMOVED AND REPLACED TENSION STRAP AT RBL 3 IAW SRM 51-40-02 AND DWG# 147A5730 ID: 0023 REV: C.
- [SDR SWAA2025070778874](https://openairdocs.org/sdr/SWAA2025070778874.md): Frame · cracked · Jun 6, 2025 · N297WN · Boeing 7377H4 · Fuselage Main, Frame
  > PASSENGER CABIN FED UPPER FRAME BS 312, STR 5L CRACKED. THIS FAULT WILL BE ACCOMPLISHED ON M-22-153-01244.
- [SDR SWAA2025070778403](https://openairdocs.org/sdr/SWAA2025070778403.md): Pressure Deck · cracked · Jun 5, 2025 · N297WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK FOUND ON HORIZONTAL PRESSURE DECK AT MID PASSENGER CABIN BS663+2 RBL 42 LEN: 0.4'( MARKED)<[01] REPAIRED HORIZONTAL PRESSURE DECK BETWEEN BS 663 TO BS 675 RBL 30 TO RBL 65 PER SRM 53-40-51-2R-2 REP 2;[02] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2025070778854](https://openairdocs.org/sdr/SWAA2025070778854.md): Lens · missing · Jun 5, 2025 · N297WN · Boeing 7377H4 · Emergency Lighting
  > FOUND LEFT EMERGENCY SILDE/OVERWING (LOWER) LIGHT MISSING LENS. REPLACED LEFT EMERGENCY SILDE/OVERWING (LOWER) LIGHT LENS IAW AMM 33-51-04-960-801 STEP 2.F.3.(A)(D).
- [SDR SWAA2025070778855](https://openairdocs.org/sdr/SWAA2025070778855.md): Scuff Plate · corroded · Jun 5, 2025 · N297WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ACD FWD PLATE SCUFF IS CORRODED. RECEIVED NEW SCUFF PLATE P/N 453A2611-1. THIS PART WILL BE INSTALLED ON CARD TTG8Q0130M3D.

Next page: https://openairdocs.org/aircraft/N297WN/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 = 'N297WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N297WN/reports

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