# Service difficulty reports: N919WN

A list on [N919WN](https://openairdocs.org/aircraft/N919WN.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 · 260 reports

- [SDR SWAA2026040284666](https://openairdocs.org/sdr/SWAA2026040284666.md): Bracket · cracked · Mar 30, 2026 · N919WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > BRACKET THAT HOLDS WIRE SUPPORT BRACKET INBOARD OF RH MLG BENT AND CRACKED. REMOVED AND REPLACED BRACKET THAT HOLDS WIRE BRACKET INBOARD OF RT MLG IAW SRM 51-40-02.
- [SDR SWAA2026033084151](https://openairdocs.org/sdr/SWAA2026033084151.md): Brake · failed · Mar 28, 2026 · N919WN · Boeing 7377H4 · Landing Gear Brake System
  > ON T/O AT ROTATION SPEED; LOAD BANG AND SEVERE SHIMMY. STAYED CONFIGURED; GEAR DOWN; FLAPS 1.RETURNED TO KELP AND LANDED FLAPS 40. EMERGENCY VEHICLES INSPECTED A/C ON THE RUNWAY AND TOWED BACK TO GATE<[01] PERFORMED TIRE BURST INSP PER MM 05-51-54<BR>REF 27632
- [SDR SWAA2026033084434](https://openairdocs.org/sdr/SWAA2026033084434.md): Tire · burst · Mar 28, 2026 · N919WN · Boeing 7377H4 · Tire
  > ON T/O AT ROTATION SPEED; LOAD BANG AND SEVERE SHIMMY. STAYED CONFIGURED; GEAR DOWN; FLAPS 1.RETURNED TO KELP AND LANDED FLAPS 40. EMERGENCY VEHICLES INSPECTED A/C ON THE RUNWAY AND TOWED BACK TO GATE<[01] PERFORMED TIRE BURST INSP PER MM 05-51-54<BR>REF 27632
- [SDR SWAA2026011359248](https://openairdocs.org/sdr/SWAA2026011359248.md): Light · inoperative · Jan 8, 2026 · N919WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS AND SIGN OVER FORWARD SERVICE DOOR DO NOT ILLUMINATE. R & R POWER SUPPLY, FUSE TO M1675 & PERFORMED GOOD EMERGENCY LIGHTS. OPS TESTED IAW AMM 33-51-06-960-804, WDM 33-51-12, AND SSM 33-51-11.
- [SDR SWAA2026011359249](https://openairdocs.org/sdr/SWAA2026011359249.md): Light · out of adjust · Jan 8, 2026 · N919WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT INDICATOR LIGHT ASSY FOR FWD ENTRY DOOR MISSING. INSTALLED EMERGENCY EXIT INDICATOR LIGHT ASSY FOR FWD ENTRY DOOR AND PERFORMED GOOD, OPS TESTED PER AMM 33-51-01-960-802.
- [SDR SWAA2026011458386](https://openairdocs.org/sdr/SWAA2026011458386.md): Bulb · inoperative · Jan 6, 2026 · N919WN · Boeing 7377H4 · Emergency Lighting
  > LEFT OVERWING EXIT FWD LOCATOR HAD INOPERATIVE BULBS. BULBS ON LT OVERWING EXIT FWD LOCATOR EMERGENCY EXIT LIGHT WERE REPLACED IAW AMM 33-51-01-960-801; OPS CHECKED GOOD IAW AMM 33-51-01-710-001.
- [SDR SWAA2026011358384](https://openairdocs.org/sdr/SWAA2026011358384.md): Lamp · inoperative · Jan 6, 2026 · N919WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT AISLE LIGHT AT SEAT ROW 14DEF INOP<[01] RELAMPED AND PERFORMED GOOD INSTALLATION TEST OF EMERGENCY EXIT AISLE LIGHT AT SEAT ROW 14DEF IAW AMM 33-51-03-960-801.;[02] VERIFIED; RELAMPED AND PERFORMED GOOD INSTALLATION TEST OF EMERGENCY EXIT AISLE
- [SDR SWAA2026011358385](https://openairdocs.org/sdr/SWAA2026011358385.md): Lamp · inoperative · Jan 6, 2026 · N919WN · Boeing 7377H4 · Emergency Lighting
  > RIGHT OVERWING EXIT AFT LOCATOR SIGN HAS INOPERATIVE BULBS. EMERGENCI LIGHT WAW RELAMPED IAW AMM 33-51-01-960-801, OPS CHECK GOOD IAW AMM SUBTASK 33-51-01-710-001.
- [SDR SWAA2026011358287](https://openairdocs.org/sdr/SWAA2026011358287.md): Battery Pack · inoperative · Jan 5, 2026 · N919WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ASSOCIATED WITH EMERGENCY EXIT BATTERY PACK M1674 DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK M1674 IAW AMM 33-51-06-960-806. PERFORMED A GOOD FUNTIONAL TEST.
- [SDR SWAA2026011454810](https://openairdocs.org/sdr/SWAA2026011454810.md): Scuff Plate · cracked · Dec 22, 2025 · N919WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FSD SCUFF PLATE CRACKED AT CORNER. REPAIRED FSD SCUFF PLATE IAW SRM 53-10-15-2R-2-A01193, REPAIR 2 - SECTION 41.
- [SDR SWAA2026011453062](https://openairdocs.org/sdr/SWAA2026011453062.md): Panel · debonded · Dec 16, 2025 · N919WN · Boeing 7377H4 · Aerodynamic Fairings
  > DEBOND ON OUTER SKIN OF PANEL 193AR. REPAIRED IAW SRM 51-70-05-2R-1-A00732, REPAIR 1.
- [SDR SWAA2026011453063](https://openairdocs.org/sdr/SWAA2026011453063.md): Floor Support · cracked · Dec 16, 2025 · N919WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPORT, FWD CABIN BS 391, RBL 41, WL 208. REMOVED DAMAGED FLOOR SUPPORT AND INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 143A5400 REV-.
- [SDR SWAA2026011452583](https://openairdocs.org/sdr/SWAA2026011452583.md): Stiffener · cracked · Dec 15, 2025 · N919WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > WHILE ACCESSING FOR VAPOR BARRIER FOUND STIFFENER AT BS 663, LBL 27, WL 146 CRACKED. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-40-02, DWG 111A1000, REV A, & DWG 149A7210, REV-.
- [SDR SWAA2026011451959](https://openairdocs.org/sdr/SWAA2026011451959.md): Doubler · cracked · Dec 12, 2025 · N919WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > METAL DOUBLER MOUNTED TO FWD SIDE OF 663 VAPOR BARRIER HAS A CRACK WL 144 RBL 27.6. REMOVED AND REPLACED DOUBLER IAW SRM 51-40-02 AND DWG 111A1000 REV:A AND DWG 111A1001 REV A.
- [SDR SWAA2026011451387](https://openairdocs.org/sdr/SWAA2026011451387.md): Frame · cracked · Dec 11, 2025 · N919WN · Boeing 7377H4 · Fuselage Main, Frame
  > BS 312 FRAME IS CRACKED IN THE RADIUS JUST ABOVE THE L1 DOOR CUT OUT. REMOVED THE CRACK DAMAGE IAW SRM 51-10-02-0G-0. ACCOMPLISHED REPAIR EA M-22-153-01244.
- [SDR SWAA2026011451696](https://openairdocs.org/sdr/SWAA2026011451696.md): Stringer · cracked · Dec 11, 2025 · N919WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > LEFT FWD PAX CABIN BS 295.5, STRINGER 7L CRACKED. REPAIRED IAW SRM 53-00-03-2R-1, EA 25-153-03423-WIP1, AND EA 25-153-03423-WIP2.
- [SDR SWAA2026011451681](https://openairdocs.org/sdr/SWAA2026011451681.md): Attach Angle · cracked · Dec 11, 2025 · N919WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED INTERCOSTAL ATTACH ANGLE, BS 400, LBL 25, WL 155. REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE IAW SRM 51-40-02, & DWG 143A7505-82.
- [SDR SWAA2026011451678](https://openairdocs.org/sdr/SWAA2026011451678.md): Attach Angle · cracked · Dec 11, 2025 · N919WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACK ON FCB FWD INTERCOSTAL ATTACH ANGLE AT BS 500C, LBL 24, WL 155. REMOVED AND REPLACED FWD CARGO BAY FWD INTERCOSTAL ATTACH ANGLE IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHEETS 81 & 82.
- [SDR SWAA2026011451682](https://openairdocs.org/sdr/SWAA2026011451682.md): Attach Angle · cracked · Dec 11, 2025 · N919WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACK ON FCB AFT INTERCOSTAL ATTACHMENT ANGLE AT STA 500C, LBL 24, WL 155. REMOVED AND REPLACED FWD CARGO BAY AFT INTERCOSTAL ATTACH ANGLE IAW SRM 51-40-02 AND DWG 143A7505-82.
- [SDR SWAA2026011451688](https://openairdocs.org/sdr/SWAA2026011451688.md): Threshold Web · corroded · Dec 11, 2025 · N919WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO BAY SUB THRESHOLD WEB AT BS 451 - 485, RBL 28.5, WL 156. REMOVED AND REPLACED THE FWD CARGO BAY SUB-THRESHOLD WEB IAW SRM 51-40-02 AND DWG 143A8330 REV A.
- [SDR SWAA2026011451692](https://openairdocs.org/sdr/SWAA2026011451692.md): Threshold · corroded · Dec 11, 2025 · N919WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY SUB THRESHOLD WEB AT BS 787 - 847, RBL 26, WL 160. REMOVED AND REPLACED AFT CARGO BAY THRESHOLD WEB IAW SRM 51-40-02 AND DWG 146A8340 REV-.
- [SDR SWAA2026011451683](https://openairdocs.org/sdr/SWAA2026011451683.md): Sidewall Support · corroded · Dec 11, 2025 · N919WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO BAY LT AFT BODY TO SIDE WALL SUPPORT BS 489 - 500C, LBL 25, WL 156. REMOVED AND REPLACED THE SIDEWALL SUPPORT FROM BS 489 - 500D, LBL 25, WL 156 IAW SRM 51-40-02-0G-0, SRM 53-00-53-2R-5, DWG 143A7501, & 143A7500.
- [SDR SWAA2026011451684](https://openairdocs.org/sdr/SWAA2026011451684.md): Shield · corroded · Dec 11, 2025 · N919WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO BAY RT AFT BODY TO SIDE WALL SUPPORT BS 510, RBL 25, WL 156, RT AFT SHIELD. REMOVED AND REPLACED THE AFT SHEILD IAW SRM 51-40-02 & DWG 143A0080 REV-.
- [SDR SWAA2026011351693](https://openairdocs.org/sdr/SWAA2026011351693.md): Web · corroded · Dec 11, 2025 · N919WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON ACB UPPER WEB AT BS 827, RBL 65, WL 200. R & R ACB UPPER WEB BS 787 - 847 IAW SRM 51-40-02 & DWG 146A0080, REV A, DWG 146A8111, REV -.AND DWG 146A0083.
- [SDR SWAA2026011451390](https://openairdocs.org/sdr/SWAA2026011451390.md): Floor Support · cracked · Dec 10, 2025 · N919WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT FWD WET AREA BS 284, BL 0, WL 208. THE INTERCOSTAL WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04-1A-1. REMOVED AND REPLACED THE INTERCOSTAL BS 277-294 BL 0 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 141A5400 REV-.
- [SDR SWAA2026011450905](https://openairdocs.org/sdr/SWAA2026011450905.md): Floor Panel · pulled · Dec 10, 2025 · N919WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 242TF UPPER SKIN HAS AREAS OF PULLED STRANDS. 242TF FLOOR PANEL UPPER SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2026011450932](https://openairdocs.org/sdr/SWAA2026011450932.md): Sidewall Support · corroded · Dec 10, 2025 · N919WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT, BS 727B+10 - 787+7, LBL 21, WL 156. REMOVED AND REPLACED THE SIDEWALL SUPPORT BS 727 - 847 IAW SRM 51-40-02, DWG 146A7500, & 146A7502.
- [SDR SWAA2026011451380](https://openairdocs.org/sdr/SWAA2026011451380.md): Skin · damaged · Dec 10, 2025 · N919WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > EXTERNAL GROUND POWER DOOR LOWER CUTOUT HAS A MISSING FASTENER. REPAIRED EXTERNAL POWER DOOR LOWER CUTOUT IAW SRM 53-10-15-2R-4, REPAIR 4.
- [SDR SWAA2026011450934](https://openairdocs.org/sdr/SWAA2026011450934.md): Shield · corroded · Dec 10, 2025 · N919WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY CARGO DOOR CUT-OUT FWD SHIELD AT BS 767+19, RBL 22, WL 156. REMOVED AND REPLACED THE AFT CARGO BAY CARGO DOOR CUT OUT FWD SHIELD IAW SRM 51-40-02, DWG 146A0081, REV A.
- [SDR SWAA2026011451163](https://openairdocs.org/sdr/SWAA2026011451163.md): Stub Frame · cracked · Dec 10, 2025 · N919WN · Boeing 7377H4 · Fuselage Main, Frame
  > ONE CRACK NOTED ON R1 DOOR STUB FRAME, BS 294.5+2, 0.1 INCH ABOVE SEAL DEPRESSOR, WL 267. L: 1 INCH. EVALUATED CRACK ON FSD STUB FRAME AND FOUND TO BE OUT OF ALLOWABLE LIMITS. THE DAMAGED FSD STUB FRAME WAS REMOVED AND INSTALLED NEW UPPER STUB FRAME IAW SRM
- [SDR SWAA2026011451384](https://openairdocs.org/sdr/SWAA2026011451384.md): Floor Support · cracked · Dec 10, 2025 · N919WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPORT, FWD CABIN BS 390, BL 0, WL 208. THE INTERCOSTAL WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04-1A-1. REMOVED AND REPLACED UPPER SECTION IAW SRM 51-40-02-0G-0, AND DWG 143A5400, REV A.
- [SDR SWAA2026011451392](https://openairdocs.org/sdr/SWAA2026011451392.md): Floor Support · cracked · Dec 10, 2025 · N919WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPORT, FWD CABIN BS 394, LBL 14, WL 208. REMOVED THE DAMAGED FLOOR SUPPORT UPPER SECTION AND INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 143A5400, REV-.
- [SDR SWAA2026011451393](https://openairdocs.org/sdr/SWAA2026011451393.md): Floor Support · cracked · Dec 10, 2025 · N919WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPORT, BS 391, RBL 9, WL 208. FOUND TO BE OUT LIMITS IAW SRM 53-00-04-1A-1. REMOVED AND REPLACED UPPER SECTION OF THE FLOOR SUPPORT, BS 380-400, RBL 39, WL 208 IAW SRM 51-40-02-0G-0, AND DWG 143A5400, REV A.
- [SDR SWAA2026011451385](https://openairdocs.org/sdr/SWAA2026011451385.md): Floor Support · cracked · Dec 10, 2025 · N919WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPORT BS 354, BL 0, WL 208. THE FLOOR SUPPORT WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04-1A-1. REMOVED AND REPLACED IAW DWG 141A5400, REV-.
- [SDR SWAA2026011451366](https://openairdocs.org/sdr/SWAA2026011451366.md): Angle · cracked · Dec 10, 2025 · N919WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > WHILE ACCESSING FOR VAPOR BARRIER FOUND ANGLE CRACKED BS 652 LBL 29 WL 144. REMOVED AND REPLACED THE VAPOR BARRIER ANGLE IAW SRM 51-40-02 & DWG 149A7210 REV -.
- [SDR SWAA2026011350917](https://openairdocs.org/sdr/SWAA2026011350917.md): Floorbeam · corroded · Dec 10, 2025 · N919WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM BS 986, RBL 43, WL 208.1. REPAIRED THE FLOORBEAM IAW SRM 53-70-51-2R-6-A00995, REPAIR 6.
- [SDR SWAA2026011350918](https://openairdocs.org/sdr/SWAA2026011350918.md): Floorbeam · corroded · Dec 10, 2025 · N919WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION ON BS 986 FLOORBEAM, LBL 43, WL 208.1. REPAIRED THE FLOORBEAM IAW SRM 53-70-51-2R-6-A00995, REPAIR 6.
- [SDR SWAA2026011350897](https://openairdocs.org/sdr/SWAA2026011350897.md): Floor Panel · pulled · Dec 10, 2025 · N919WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241UF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0, & DWG 146A5810.
- [SDR SWAA2026011350898](https://openairdocs.org/sdr/SWAA2026011350898.md): Floor Panel · pulled · Dec 10, 2025 · N919WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241XF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241XF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2026011350899](https://openairdocs.org/sdr/SWAA2026011350899.md): Floor Panel · pulled · Dec 10, 2025 · N919WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241YF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED IAW SRM 53-00-50-2R-1-A00939, REPAIR 1.
- [SDR SWAA2026011350907](https://openairdocs.org/sdr/SWAA2026011350907.md): Floor Panel · pulled · Dec 10, 2025 · N919WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT 242VF FLOOR PANEL UPPER SKIN DAMAGE WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2026011350915](https://openairdocs.org/sdr/SWAA2026011350915.md): Floor Panel · pulled · Dec 10, 2025 · N919WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 231JF UPPER SKIN HAS AREAS OF PULLED STRANDS. REMOVED AND FABRICATED A NEW FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.
- [SDR SWAA2026011350920](https://openairdocs.org/sdr/SWAA2026011350920.md): Floor Panel · pulled · Dec 10, 2025 · N919WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL 231XF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0, & DWG 144A5810.
- [SDR SWAA2026011350921](https://openairdocs.org/sdr/SWAA2026011350921.md): Floor Panel · pulled · Dec 10, 2025 · N919WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS. R & R THE FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.
- [SDR SWAA2026011350922](https://openairdocs.org/sdr/SWAA2026011350922.md): Floor Panel · pulled · Dec 10, 2025 · N919WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS. R & R IAW SRM 53-00-50-2R-0-A00938.
- [SDR SWAA2026011350924](https://openairdocs.org/sdr/SWAA2026011350924.md): Floor Panel · pulled · Dec 10, 2025 · N919WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241ADF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE AFT FLOOR PANEL 241ADF WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2026011350933](https://openairdocs.org/sdr/SWAA2026011350933.md): Sidewall Support · corroded · Dec 10, 2025 · N919WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT FROM BS 727C+13 - 747+16, RBL 21, WL 156. R & R FLOOR SIDEWALL SUPPORT AT BS 727+4.04 - 767, RBL 21, WL 156 IAW SRM 51-40-02-0G-0 AND DWG 146A7500 SHEET 113 REV -.
- [SDR SWAA2026011350919](https://openairdocs.org/sdr/SWAA2026011350919.md): Strap · corroded · Dec 10, 2025 · N919WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT PAX CABIN FLOOR STRAP AT BS 1016+14, LBL 3, WL 208.2. REPAIRED AFT PAX CABIN FLOOR STRAP AT BS 1016+14, LBL 3, WL 208.2 IAW EA 25-153-03386.
- [SDR SWAA2026011350901](https://openairdocs.org/sdr/SWAA2026011350901.md): Floor Panel · pulled · Dec 10, 2025 · N919WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241AAF UPPER SKIN HAS AREAS OF PULLED STRANDS. REMOVED AND FABRICATED A NEW FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.
- [SDR SWAA2026011350906](https://openairdocs.org/sdr/SWAA2026011350906.md): Floor Panel · pulled · Dec 10, 2025 · N919WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 242UF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED IAW SRM 53-00-50-2R-1-A00939, REPAIR 1.

Next page: https://openairdocs.org/aircraft/N919WN/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 = 'N919WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N919WN/reports

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