# Service difficulty reports: N249WN

A list on [N249WN](https://openairdocs.org/aircraft/N249WN.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 · 318 reports

- [SDR SWAA2026090898931](https://openairdocs.org/sdr/SWAA2026090898931.md): Slide · out of adjust · Sep 1, 2026 · N249WN · Boeing 7377H4 · Escape Slide
  > R 2 DOOR Z FOLD INCORRECT DRAGS FLOOR. CORRECTED R2 DOOR SLIDE Z FOLD IAW AMM 25-66-00.
- [SDR SWAA2026082448984](https://openairdocs.org/sdr/SWAA2026082448984.md): Lamp · inoperative · Aug 20, 2026 · N249WN · Boeing 7377H4 · Emergency Lighting
  > CREW REPORTS SIDEWALL LIGHT INOP AT ROW 15DEF, REPLACED THE LAMPS IAW AMM 33-51-01.
- [SDR SWAA2026072051578](https://openairdocs.org/sdr/SWAA2026072051578.md): Light · inoperative · Jul 16, 2026 · N249WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY ASILE LIGHT AT 6DEF INOPERATIVE. REMOVED & REPLACED AND PERFORMED GOOD OPS CHECK OF THE EMERGENCY AREA LIGHT AT SEAT ROW 6 DEF IAW AMM 33-51-003-960-801.
- [SDR SWAA2026040183912](https://openairdocs.org/sdr/SWAA2026040183912.md): Sign · detached · Mar 28, 2026 · N249WN · Boeing 7377H4 · Emergency Lighting
  > EXIT SIGN ABOVE COCKPIT FELL OFF. INSTALLED EXIT SIGN ABOVE COCKPIT IAW AMM 33-51-01-960-801, STEP 2.C.
- [SDR SWAA2026033083273](https://openairdocs.org/sdr/SWAA2026033083273.md): Wire · damaged · Mar 25, 2026 · N249WN · Boeing 7377H4 · Light System Wiring
  > EMERGENCY LIGHT ASSEMBLY OVER FWD ENTRY DOOR INOPERATIVE. SPLICED THE WIRE W4142-0059-20 IAW SWPM 20-30-12 AND PERFORMED GOOD FUNCTIONAL CHECK OF EMERGENCY LIGHT IAW AMM 33-51-00-710-801.
- [SDR SWAA2026033179615](https://openairdocs.org/sdr/SWAA2026033179615.md): Strap · corroded · Mar 13, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON ACB STRAP UNDER LOWER SILLWEB BS847 RBL21; WL156. REMOVED AND REPLACED ACB STRAP UNDER LOWER SILL WEB BS 847 RBL21, WL156 IAW SRM 51-40-02-0G-0 & DWG146A8340 REV-.
- [SDR SWAA2026033078876](https://openairdocs.org/sdr/SWAA2026033078876.md): Light · damaged · Mar 11, 2026 · N249WN · Boeing 7377H4 · Emergency Lighting
  > CENTER LINE CEILING EMERGENCY LIGHT BS 623 DAMAGED. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-01-960-802. TESTED GOOD.
- [SDR SWAA2026033078534](https://openairdocs.org/sdr/SWAA2026033078534.md): Web · cracked · Mar 10, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY ANGLE ATTACHED TO THE WEB, BS 827, RBL 19, WL 154 CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02-0G-0, & DWG 146A8120, REV-.
- [SDR SWAA2026033078114](https://openairdocs.org/sdr/SWAA2026033078114.md): Frame · damaged · Mar 9, 2026 · N249WN · Boeing 7377H4 · Fuselage Main, Frame
  > AFT CARGO BAY, BS 767 FRAME HAD AN ELONGATED FASTENER HOLE AT RBL 21, WL 156. FORMED A REPAIR FRAME IAW SRM 53-60-07-2R-2, REPAIR 2, DETAIL 4.D (7), TABLE 202. REPAIRED THE FRAMEIAW SRM 53-60-07-2R-2, REPAIR 2.
- [SDR SWAA2026033077946](https://openairdocs.org/sdr/SWAA2026033077946.md): Web · corroded · Mar 9, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON ACB LOWER SILL WEB BETWEEN BS 794 - 847, RBL 22, WL 156. REMOVED AND REPLACED THE ACB LOWER SILL WEB IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02, DWG 146A8121, REV-, & DWG 146A8120, REV-.
- [SDR SWAA2026033077947](https://openairdocs.org/sdr/SWAA2026033077947.md): Web · corroded · Mar 9, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON ACB LOWER SILL WEB BETWEEN BS 847 - 856, RBL 22, WL 156. REMOVED AND REPLACED THE SILL WEB IAW SRM 51-40-02, AND DWG 146A8120, REV-, & APPLIED CAP SEAL TO THE FASTENERS IAW AMM 51-31-00.
- [SDR SWAA2026033078112](https://openairdocs.org/sdr/SWAA2026033078112.md): Strap · corroded · Mar 9, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON ACD NUTPLATE STRAP BS 794 - 794+7, RBL 20, WL 156. REMODED AND REPLACED THE NUTPLATE STRAP IAW SRM 51-40-02-0G-0, & DWG 146A8340, REV-.
- [SDR SWAA2026033077527](https://openairdocs.org/sdr/SWAA2026033077527.md): Web · corroded · Mar 8, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ACB DOOR SURROUND STRUCTURE CORRODED ON THE LOWER INTERCOSTAL WEB, BS 791, RBL 25, WL 159. REMOVED AND REPLACED THE INTERCOSTAL WEB IAW SRM 51-40-02, & DWG 146A8320, REV D.
- [SDR SWAA2026033077368](https://openairdocs.org/sdr/SWAA2026033077368.md): Strap · corroded · Mar 7, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ACB LWR DOOR SURROUND STRUCTURE SILL STRAP CORRODED ON UPPER SURFACE AT FASTENER HOLE,BS 787 - 827, RBL 25. REMOVED & REPLACED THE SILL STRAP FROM BS 767+7 - 847+15, IAW SRM 51-40-02, DWG 146A8120, REV-, & DWG 146A8340, REV-.
- [SDR SWAA2026033077369](https://openairdocs.org/sdr/SWAA2026033077369.md): Nut Plate · corroded · Mar 7, 2026 · N249WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > ACB LWR DOOR SURROUND STRUCTURE NUTPLATE STRAP CORRODED ON LWR SURFACE AT FASTENER HOLE, BS 784; RBL 25. REMOVED AND INSTALLED THE NUTPLATE STRAP IAW SRM 51-40-02-0G-0, & DWG 146A0081, REV -.
- [SDR SWAA2026033077524](https://openairdocs.org/sdr/SWAA2026033077524.md): Web · corroded · Mar 7, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON THE LOWER SILL WEB BETWEEN BS 787 - 794, RBL 22, WL 156. REMOVED AND REPLACED THE LOWER SILL WEB IAW SRM 51-40-05, AND DWG 146A0081, REV B.
- [SDR SWAA2026040177261](https://openairdocs.org/sdr/SWAA2026040177261.md): Sidewall Support · corroded · Mar 6, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FORWARD CARGO BAY, CORROSION ON RT AFT BODY TO SIDE WALL SUPPORT, BS 500A - 500B, RBL 22, WL 156. REMOVED AND REPLACED THE FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02, SRM 53-00-53-1A-2, & DWG 143A7500, REV -.
- [SDR SWAA2026033177260](https://openairdocs.org/sdr/SWAA2026033177260.md): Support · corroded · Mar 6, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FCB; CORROSION ON LH AFT BODY TO SIDE WALL SUPPORT STA 507-500D LBL22 WL156. REMOVED AND REPLACED FCB FLOOR TO SIDEWALL SUPPORT AT BS 395 - 500D, LBL 22, WL 156 IAW SRM 51-40-05 AND DWG 143A7501 0112, REV A.
- [SDR SWAA2026033077088](https://openairdocs.org/sdr/SWAA2026033077088.md): Sidewall Support · corroded · Mar 6, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON LT FWD BODY TO SIDEWALL SUPPORT, BS 396 - 495, LBL 21, WL 156. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 4.A (2) (A) FIGURE 103, DETAIL D.
- [SDR SWAA2026040176893](https://openairdocs.org/sdr/SWAA2026040176893.md): Angle · cracked · Mar 5, 2026 · N249WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > LEFT WING TRANSVERSE ANGLE, JUST ABOVE AFT PYLON WAS CRACKED IN RADIUS. REMOVED AND REPLACED THE LT WING TRANSVERSE ANGLE IAW SRM 51-40-02 AND DWG 115A2512, REV B.
- [SDR SWAA2026033176736](https://openairdocs.org/sdr/SWAA2026033176736.md): Rail · corroded · Mar 5, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON THE BULKHEAD, BS 489, STRINGERS 26R - 26L, WL 152. REMOVED AND REPLACED FWD CARGO BAY AFT BULKHEAD LOWER RAIL, BS 500D, RBL 24 - LBL 24, WL 152 IAW SRM 51-40-02, & DWG 143A7902, REV C.
- [SDR SWAA2026033076892](https://openairdocs.org/sdr/SWAA2026033076892.md): Stiffener · cracked · Mar 5, 2026 · N249WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > LEFT STABILIZER RIB NR 3, STFFENER NR 3 CRACKED. FOUND DURING AN INSPECTION. REPAIRED THE STIFFENER IAW SRM 55-10-09-2R-4.
- [SDR SWAA2026033076735](https://openairdocs.org/sdr/SWAA2026033076735.md): Intercostal · corroded · Mar 5, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO INTERCOSTAL BETWEEN BS 767 & 787, RBL 25 CORRODED, TWO LOCATIONS. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-05-0G-0, DWG 146A0081, REV-.
- [SDR SWAA2026033076895](https://openairdocs.org/sdr/SWAA2026033076895.md): Floor Support · corroded · Mar 5, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON ACB FLOOR SUPPORT SPLICE AT BS 767+5 WL157. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-10-02 AND DWG 146A7500 REV -.
- [SDR SWAA2026040176612](https://openairdocs.org/sdr/SWAA2026040176612.md): Cover · cracked · Mar 4, 2026 · N249WN · Boeing 7377H4 · Emergency Lighting
  > PLASTIC COVER PLATE ABOVE RT OVERWING EMERGENCY EXIT, CRACKED. REMOVED AND REPLACED THE PLASTIC COVER PLATE RT OVERWING WITH A NEW COVER IAW SRM 51-40-02, AND AMM 52-22-00-400-802.
- [SDR SWAA2026033076730](https://openairdocs.org/sdr/SWAA2026033076730.md): Sidewall Support · corroded · Mar 4, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO SIDEWALL SUPPORT AT LBL 22, BS 727 - 847 WAS CORRODED AT SEVERAL LOCATIONS. REMOVED AND REPLACED SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0, & DWG 146A7500, REV-.
- [SDR SWAA2026033076731](https://openairdocs.org/sdr/SWAA2026033076731.md): Sidewall Support · corroded · Mar 4, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO SIDEWALL SUPPORT AT RBL 22, BS 727 - 767 CORRODED AT SEVERAL LOCATIONS. REMOVED AND REPLACED THE SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0, & DWG 146A7500, REV -.
- [SDR SWAA2026033076732](https://openairdocs.org/sdr/SWAA2026033076732.md): Sidewall Support · corroded · Mar 4, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO SIDEWALL SUPPORT AT BS 727A, LBL 22, WL 155 CORRODED. SIDEWALL SUPPORT RESOLVED ON CUSTOMER CARD TTG8Q01ASTYM.
- [SDR SWAA2026033176435](https://openairdocs.org/sdr/SWAA2026033176435.md): Stringer · cracked · Mar 3, 2026 · N249WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER 25R, BS 535, WL155. REPAIRED IAW EA 26-153-00644. THIS IS A CATEGORY A REPAIR AS DEFINED IN SRM 51-00-06.
- [SDR SWAA2026033176027](https://openairdocs.org/sdr/SWAA2026033176027.md): Floor Panel · pulled · Mar 3, 2026 · N249WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 232RF UPPER SKIN HAS AREAS OF PULLED STRANDS. FLOOR PANEL 232RF WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, AND DWG 144A5810, 0151, DUE TO AMOUNT OF ALL DAMAGE.
- [SDR SWAA2026033176029](https://openairdocs.org/sdr/SWAA2026033176029.md): Floor Panel · pulled · Mar 3, 2026 · N249WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS. FLOOR PANEL 241AF WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0 AND DWG: 144A5810, 0127.
- [SDR SWAA2026033176028](https://openairdocs.org/sdr/SWAA2026033176028.md): Floor Panel · pulled · Mar 3, 2026 · N249WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, & DRAWING 144A5810, SHEET 161.
- [SDR SWAA2026033076436](https://openairdocs.org/sdr/SWAA2026033076436.md): Stringer · cracked · Mar 3, 2026 · N249WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER 26R, BS 535, WL153. REPAIRED STRINGER 26R BTWN BS 500D & 540, AND APPLIED A FILLET SEAL & CIC IAW SRM 53-00-03-2R-1, REPAIR 1.
- [SDR SWAA2026033076437](https://openairdocs.org/sdr/SWAA2026033076437.md): Stringer · cracked · Mar 3, 2026 · N249WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER 23 LT, BS 535, WL164. REPAIRED STRINGER 23L BTWN BS 500D & 540, WL 164. APPLIED A FILLET SEAL AND CIC IAW SRM 53-00-03-2R-1, REPAIR 1.
- [SDR SWAA2026033076020](https://openairdocs.org/sdr/SWAA2026033076020.md): Floor Panel · pulled · Mar 3, 2026 · N249WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 231XF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. FLOOR PANEL 231XF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, & DWG 144A5810, 0126.
- [SDR SWAA2026033076026](https://openairdocs.org/sdr/SWAA2026033076026.md): Floor Panel · debonded · Mar 3, 2026 · N249WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 231ZF LOWER SKIN IS DEBONDED NEAR AFT EDGE. FLOOR PANEL 231ZF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, & DWG 144A5810, SHEET 160.
- [SDR SWAA2026033076021](https://openairdocs.org/sdr/SWAA2026033076021.md): Floor Panel · debonded · Mar 3, 2026 · N249WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241BF UPPER SKIN IS DEBONDED NEAR CENTER OF PANEL. FABRICATION OF A NEW FLOOR PANEL REPLACEMENT HAD BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026033076030](https://openairdocs.org/sdr/SWAA2026033076030.md): Floor Panel · pulled · Mar 3, 2026 · N249WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241DF UPPER SKIN HAD AREAS OF PULLED STRANDS. FLOOR PANEL 241DF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, AND DWG 144A5810, 0128.
- [SDR SWAA2026033076022](https://openairdocs.org/sdr/SWAA2026033076022.md): Floor Panel · pulled · Mar 3, 2026 · N249WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241EF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED A NEW FLOOR PANEL 241EF & REPLACED IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026033076023](https://openairdocs.org/sdr/SWAA2026033076023.md): Floor Panel · pulled · Mar 3, 2026 · N249WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 242AF UPPER SKIN HAD AREAS OF PULLED STRANDS. FLOOR PANEL 242AF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810, SHEET 189.
- [SDR SWAA2026033076031](https://openairdocs.org/sdr/SWAA2026033076031.md): Floor Panel · pulled · Mar 3, 2026 · N249WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 242BF UPPER SKIN HAD AREAS OF PULLED STRANDS. FLOOR PANEL 242BF WAS REPLACED IAW SRM 53-00-50-2R-0, & DWG 144A5810, SHEET 122.;[02] ITEM 1
- [SDR SWAA2026033076025](https://openairdocs.org/sdr/SWAA2026033076025.md): Floor Panel · pulled · Mar 3, 2026 · N249WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 242DF UPPER SKIN HAD AREAS OF PULLED STRANDS. FLOOR PANEL 242DF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, & DWG 144A5810, SHEET 150.
- [SDR SWAA2026033175992](https://openairdocs.org/sdr/SWAA2026033175992.md): Crossbeam · cracked · Mar 2, 2026 · N249WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACKED CROSSBEAM, BS 540, LBL 44, WL 208. REMOVED AND REPLACED CROSSBEAM, BS 540, LBL24 - 45, WL 208, IAW SRM 51-40-02, & DWG 143A5240, REV -.
- [SDR SWAA2026033175999](https://openairdocs.org/sdr/SWAA2026033175999.md): Seat Track · corroded · Mar 2, 2026 · N249WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK LBL 45, BS 480+17, BS 500+8, BS 500A+8, BS 500B+18. THE SEAT TRACK WILL BE REPLACED ON FAULT TTG8Q01AR96P.
- [SDR SWAA2026033075682](https://openairdocs.org/sdr/SWAA2026033075682.md): Scuff Plate · cracked · Mar 2, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY AFT CORNER SCUFF PLATE CRACKED. REPAIRED THE SCUFF PLATE IAW SRM 53-60-15-2R-1.
- [SDR SWAA2026033075681](https://openairdocs.org/sdr/SWAA2026033075681.md): Scuff Plate · cracked · Mar 2, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FWD CORNER SCUFF PLATE CRACKED. AFT CARGO BAY FWD CORNER SCUFF PLATE WAS REPLACED IAW SRM 51-10-02-0G-0, PARAGRAPH 9.
- [SDR SWAA2026033075775](https://openairdocs.org/sdr/SWAA2026033075775.md): Shield · corroded · Mar 2, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON ACD FWD SHIELD WEB BETWEEN BS 767 - 794, RBL 23, WL 156, REMOVED & REPLACED THE SHIELD IAW SRM 51-40-02, AND DWG 146A0081, 0034, REV-.
- [SDR SWAA2026033075776](https://openairdocs.org/sdr/SWAA2026033075776.md): Shield · corroded · Mar 2, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON ACD AFT SHIELD WEB BETWEEN BS 847 - 867, RBL 23, WL 156. REMOVED & REPLACED THE SHIELD IAW SRM 51-40-02, AND DWG 146A0081, 0034, REV-.
- [SDR SWAA2026033075777](https://openairdocs.org/sdr/SWAA2026033075777.md): Threshold Web · corroded · Mar 2, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON ACD SUB THRESHOLD WEB BETWEEN BS 794 - 847, RBL 26, WL 156. REMOVED AND REPLACED THE SUB THRESHOLD WEB IAW SRM 51-10-02-0G-0, PARAGRAPH 9,
- [SDR SWAA2026033075993](https://openairdocs.org/sdr/SWAA2026033075993.md): Threshold Web · corroded · Mar 2, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FCD SUB THRESHOLD WEB BETWEEN BS 440 - 492, RBL 26, WL 156. REMOVED AND REPLACED THE SUB THRESHOLD WEB, IAW SRM 51-40-02-0G-0, & DWG 143A8330, REV A.

Next page: https://openairdocs.org/aircraft/N249WN/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 = 'N249WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N249WN/reports

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