# Service difficulty reports: N915WN

A list on [N915WN](https://openairdocs.org/aircraft/N915WN.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 · 259 reports

- [SDR SWAA2026082592093](https://openairdocs.org/sdr/SWAA2026082592093.md): Slide · low pressure · Aug 21, 2026 · N915WN · Boeing 7377H4 · Escape Slide
  > AFT SERVICE DOOR CAPTAIN SLIDE NOT IN GREEN BAND, R & R THE AFT ENTRY DOOR SLIDE IAW MT 725-61-06-AE, AND AMM 25-66-01.
- [SDR SWAA2026080365471](https://openairdocs.org/sdr/SWAA2026080365471.md): Spoiler · delaminated · Jul 31, 2026 · N915WN · Boeing 7377H4 · Spoilers
  > RIGHT WING NR 8 SPOILER PANEL UPPER SURFACE REPAIR DELAMINATED. REMOVED AND REPLACED SPOILER IAW AMM 27-61-11.
- [SDR SWAA2026061511630](https://openairdocs.org/sdr/SWAA2026061511630.md): Unknown · odor · Jun 11, 2026 · N915WN · Boeing 7377H4 · Air Distribution System
  > UNUSUAL ODOR IN COCKPIT, POSSIBLE ELECTRICAL. ACCOMPLISHED ODOR OR FUMES IN CABIN INSPECTION IAW FIM 21-00 806, FOUND NO EVIDENCE OF ODOR THRU OUT CABIN. ACFT OK FOR SERVICE.
- [SDR SWAA2026020366650](https://openairdocs.org/sdr/SWAA2026020366650.md): Lamp · inoperative · Feb 1, 2026 · N915WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS IN THE CABIN ARE INOPERATIVE DURING NIGHT MODE. REPLACED THE LAMPS IN THE NIGHT LIGHT AT BS 727E+10 IAW AMM 33-22-00. EMERGENCY EXIT LIGHTS OPS NORMAL IAW AMM 33-51-00.
- [SDR SWAA2025111333830](https://openairdocs.org/sdr/SWAA2025111333830.md): Seal · cracked · Nov 11, 2025 · N915WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > RT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL HAS VERTICAL CRACKS PARALLEL TO BOTH THE FORWARD AND AFT EDGES. REMOVED AND REPLACED THE STABILIZER TO BODY UPPER FRONT R/H SLIDING SEAL PER AMM 53-31-31.
- [SDR SWAA2025111333828](https://openairdocs.org/sdr/SWAA2025111333828.md): Seal · cracked · Nov 11, 2025 · N915WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > L/H HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL HAS VERTICAL CRACKS PARALLEL TO BOTH THE FORWARD AND AFT EDGES. REMOVED AND REPLACED L/H HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL PER AMM 53-31-31.
- [SDR SWAA2025110631594](https://openairdocs.org/sdr/SWAA2025110631594.md): Battery · inoperative · Nov 4, 2025 · N915WN · Boeing 7377H4 · Emergency Equipment
  > FWD FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FWD EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-64-00. OPS TEST PASS.
- [SDR SWAA2025103130280](https://openairdocs.org/sdr/SWAA2025103130280.md): Light · burned out · Oct 31, 2025 · N915WN · Boeing 7377H4 · Emergency Lighting
  > LEFT EMERGENCY EXIT LATCH; EMERGENCY EXIT LIGHT BURNED OUT. REPLACED EMERGENCY EXIT LIGHT, LT EMERGENCY EXIT LATCH IAW AMM 33-51-04-960-801 STEP 2.F.(1)(2)(3)(A)(B)(D).
- [SDR SWAA2025110330275](https://openairdocs.org/sdr/SWAA2025110330275.md): Light · inoperative · Oct 30, 2025 · N915WN · Boeing 7377H4 · Emergency Lighting
  > INOPERATIVE EXTERNAL EMERGENCY LIGHT AFT SERVICE DOOR AT UPPER FUSELAGE. REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-04-960-801, STEP 2.F. 1, 2, 3, A, B, D, 4. TESTED OK.
- [SDR SWAA2025103025269](https://openairdocs.org/sdr/SWAA2025103025269.md): Support · cracked · Oct 17, 2025 · N915WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ZEE LOCATED BETWEEN BS 727D - 727E, S25L, WL 156. REPLACED SUPPORT ZEE IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 146A7500 SHEET 113 REV- DWG 146A7502 SHEET 27 REV-.
- [SDR SWAA2025110321085](https://openairdocs.org/sdr/SWAA2025110321085.md): Support · corroded · Oct 3, 2025 · N915WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE BETWEEN BS 727 - 767, S25R, WL 156. REPLACED SUPPORT ZEE AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, DWG 146A7500, SHEET 113, REV-, AND DWG 146A7502, SHEET 49, REV-.
- [SDR SWAA2025110331271](https://openairdocs.org/sdr/SWAA2025110331271.md): Support · corroded · Oct 3, 2025 · N915WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE BETWEEN BS 727 - 767, S25R, WL 156. REPLACED THE SUPPORT ZEE AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, DWG 146A7500, SHEET 113, REV-, AND DWG 146A7502, SHEET 49, REV-.
- [SDR SWAA2025103021090](https://openairdocs.org/sdr/SWAA2025103021090.md): Web · cracked · Oct 3, 2025 · N915WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB CEILING AREA, BS 847 TO 867, LBL 19, AFT CARGO BAY. REPLACED WEB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 149A8100, SHEET 1 REV -.
- [SDR SWAA2025103021086](https://openairdocs.org/sdr/SWAA2025103021086.md): Shield · corroded · Oct 3, 2025 · N915WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SHIELD WEB FLOOR STRUCTURE BS 767 TO 794.5, S25R, WL156, AFT CARGO COMPARTMENT. REPLACED SHIELD WEB AND FASTENERS IAW SRM 51-10-02, ITEM 9, AND INSTALLED FASTENERS IAW SRM 51-40-02, AND DRAWING 146A0081, SHEET 37, REV -.
- [SDR SWAA2025103020975](https://openairdocs.org/sdr/SWAA2025103020975.md): Support Bracket · cracked · Oct 3, 2025 · N915WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT BRACKET, BS 947.5, LBL 10 IN THE AFT CARGO COMPARTMENT. REPLACED SUPPORT BRACKET AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 149A8103, SHEET 7, REV A.
- [SDR SWAA2025103020977](https://openairdocs.org/sdr/SWAA2025103020977.md): Angle · cracked · Oct 3, 2025 · N915WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BS 867, LBL 10 IN THE AFT CARGO COMPARTMENT. REPLACED ANGLE LOCATED BS 867, LBL 10 IAW SRM 51-10-02, ITEM 9, AND INSTALLED FASTENERS IAW SRM 51-40-02, AND DRAWING 149A8102, SHEET 17, REV-. MEASUREMENT OF CRACK IS 0.550 INCH.
- [SDR SWAA2025103021084](https://openairdocs.org/sdr/SWAA2025103021084.md): Cargo Track · cracked · Oct 3, 2025 · N915WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK CARGO TRACK RBBL 13.84 BS 727 IN THE AFT CARGO COMPARTMENT. REPAIRED THE CARGO TRACK BTW BS 727D- 787 IAW SRM 53-00-53-2R-3, REPAIR 3, ALTERNATIVE 1 AND 2.
- [SDR SWAA2025103021088](https://openairdocs.org/sdr/SWAA2025103021088.md): Cargo Track · cracked · Oct 3, 2025 · N915WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK CARGO TRACK RBBL 13.84, BS 767 IN THE AFT CARGO COMPARTMENT. REPAIRED THE CARGO TRACK SECTION BS 727D - 787 IAW SRM 53-00-53-2R-3, REPAIR 3, ALTERNATIVE 1 AND ALTERNATIVE 2.
- [SDR SWAA2025103021087](https://openairdocs.org/sdr/SWAA2025103021087.md): Cargo Track · cracked · Oct 3, 2025 · N915WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK CARGO TRACK RBBL 13.84 FRAME 747 AFT CARGO COMPARTMENT. REPAIRED CARGO TRACK RBL 13.84 BTW SECTION BS 727D - 787 IAW SRM 53-00-53-2R-3, REPAIR 3, ALTERNATIVE 1, AND ALTERNATIVE 2.
- [SDR SWAA2025103020730](https://openairdocs.org/sdr/SWAA2025103020730.md): Web · corroded · Oct 2, 2025 · N915WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORRODED WEB, BS 492.4 - 500A, S26R, WL 156 IN THE FWD CARGO BAY. REPLACED THE WEB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A0080, SHEET 23, REV-.
- [SDR SWAA2025103020341](https://openairdocs.org/sdr/SWAA2025103020341.md): Plate · cracked · Oct 1, 2025 · N915WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 297 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 297 AT RT WING IAW SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 115A3712 SHEET 7REV A AND DWG 115A3700 SHEET 41 REV -.
- [SDR SWAA2025110319909](https://openairdocs.org/sdr/SWAA2025110319909.md): Intercostal · cracked · Sep 30, 2025 · N915WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB INTERCOSTAL LOCATED BETWEEN BS 294.5 - 303.9, S16L. PERFORMED A MAJOR REPAIR ON WEB INTERCOSTAL IAW EA 25-153-02714-WIP1, TTG8Q015JTW1 AND EA 25-153-02714, TTG8Q015TCU5.
- [SDR SWAA2025110319913](https://openairdocs.org/sdr/SWAA2025110319913.md): Floorbeam · corroded · Sep 30, 2025 · N915WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROED FLOORBEAM, BS 986.5, RBL 42, WL 208.1. REPAIRED THE FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6.
- [SDR SWAA2025110319914](https://openairdocs.org/sdr/SWAA2025110319914.md): Floorbeam · corroded · Sep 30, 2025 · N915WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION FLOOR BEAM, BS 986.5, LBL 42, WL 208.1. REPAIRED THE FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6.
- [SDR SWAA2025110319906](https://openairdocs.org/sdr/SWAA2025110319906.md): Strap · corroded · Sep 30, 2025 · N915WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORRODED STRAP, FLOOR STRUCTURE LOCATED BETWEEN BS 1016 TO 1040, LBL 4, WL 208.1. REPLACED THE STRAP IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 147A5600, SHEET 32, REV B.
- [SDR SWAA2025110319910](https://openairdocs.org/sdr/SWAA2025110319910.md): Tie Clip · cracked · Sep 30, 2025 · N915WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACK TIE CLIP LOCATED BS 277, STR 10R. REPLACED THE TIE CLIP AND FASTENERS AT BS 277, S10R IAW SRM 51-40-02-0G-0 AND DWG 141A1110 SHEET 18 REV-.
- [SDR SWAA2025103019746](https://openairdocs.org/sdr/SWAA2025103019746.md): Floor Support · cracked · Sep 30, 2025 · N915WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPORT BS 328 - 344, LBL 46 REPLACED THE FLOOR SUPPORT IAW SRM 51-10-02, ITEM 9, AND SRM 51-40-02, DRAWING 141A5400, SHEET 44, REV-.
- [SDR SWAA2025103019745](https://openairdocs.org/sdr/SWAA2025103019745.md): Floor Support · cracked · Sep 30, 2025 · N915WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPORT LOCATED BETWEEN BS 312 - 328, LBL 46. REPLACED FLOOR SUPPORT IAW SRM 51-40-02, SRM 51-10-02, AND DWG 141A5400, SHEET 26, REV-.
- [SDR SWAA2025103019912](https://openairdocs.org/sdr/SWAA2025103019912.md): Strap · corroded · Sep 30, 2025 · N915WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION STRAP FLOOR STRUCTURE LOCATED BETWEEN STA1016 TO STA1040 AND RBL18 WL208.1. REPLACED STRAP FLOOR STRUCTURE IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 147A5730 SHEET 23 REV C.
- [SDR SWAA2025103019744](https://openairdocs.org/sdr/SWAA2025103019744.md): Angle · cracked · Sep 30, 2025 · N915WN · Boeing 7377H4 · Aerodynamic Fairings
  > CRACK ON ANGLE WING TO BODY FARING STRUCTURE BS 500D AT LEVEL STR19L AT LOWER FUSELAGE. REPLACED THE ANGLE IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, AND DWG 116A3010, SHEET 39, REV-.
- [SDR SWAA2025103019747](https://openairdocs.org/sdr/SWAA2025103019747.md): Nut Plate · cracked · Sep 30, 2025 · N915WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ON RAIL NUT-PLATE LOCATED ORSS 286 INTERNAL CAVITY TRAILING EDGE AT LT WING. REPLACED RAIL NUT-PLATE LOCATED ORSS 286 INTERNAL CAVITY TRAILING EDGE AT LT WING IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9.
- [SDR SWAA2025110319524](https://openairdocs.org/sdr/SWAA2025110319524.md): Angle · cracked · Sep 29, 2025 · N915WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE, BS 695, BL 0. REPLACED ANGLE AND FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02, ITEM 9, AND DWG 273A9110, SHEET 6, REV A.
- [SDR SWAA2025110331274](https://openairdocs.org/sdr/SWAA2025110331274.md): Angle · cracked · Sep 29, 2025 · N915WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE, FLOOR STRUCTURE, BS 695, BL 0. REPLACED ANGLE AND FASTENERS IAW SRM 51-40-02-0G-0 SRM 51-10-02 ITEM 9 AND DWG 273A9110, SHEET 6, REV.A.
- [SDR SWAA2025110319520](https://openairdocs.org/sdr/SWAA2025110319520.md): Angle · cracked · Sep 29, 2025 · N915WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE, FLOOR STRUCTURE. BS 695, RBL 24.75. REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, DWG 273A9110, REV A, & DWG 111A6000, SHEET 302, REV-.
- [SDR SWAA2025110319521](https://openairdocs.org/sdr/SWAA2025110319521.md): Angle · cracked · Sep 29, 2025 · N915WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE FLOOR STRUCTURE LOCATED STA695 AND LBL24.75. REPLACED ANGLE LOCATED STA695 AND LBL24.75 CENTER SECTION IAW SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 273A9110 REV A.
- [SDR SWAA2025103019299](https://openairdocs.org/sdr/SWAA2025103019299.md): Handle · deteriorated · Sep 29, 2025 · N915WN · Boeing 7377H4 · Passenger/Crew Doors
  > DETERIORATED HANDLE ON FWD ENTRY DOOR AT FWD GALLEY AREA (2 E/A). REPLACED HANDLE ON FWD ENTRY DOOR AT FWD GALLEY AREA (2 E/A) IAW AMM 52-11-31-400-802 STEP 3.G.(2).
- [SDR SWAA2025110419100](https://openairdocs.org/sdr/SWAA2025110419100.md): Nut Plate · cracked · Sep 28, 2025 · N915WN · Boeing 7377H4 · Wing, Attach Fittings
  > CRACK ON RAIL NUT-PLATE LOCATED OFSS 469 INTERNAL CAVITY LEADING EDGE AT RT WING. REPLACED RAIL NUT PLATE LOCATED OFSS 469 INTERNAL CAVITY LEADING EDGE AT RT WING IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 112A4402, SHEET 13, REV -. CRACK MEASUREMENT I
- [SDR SWAA2025110419095](https://openairdocs.org/sdr/SWAA2025110419095.md): Nut Plate · cracked · Sep 28, 2025 · N915WN · Boeing 7377H4 · Wing, Attach Fittings
  > CRACK ON RAIL NUT-PLATE LOCATED OFSS 369 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT-PLATE LOCATED OFSS 369 INTERNAL CAVITY LEADING EDGE AT LT WING IAW SRM 51-10-02 ITEM 9 AND DWG 112A4402 SHEET:13 REV-.
- [SDR SWAA2025110418986](https://openairdocs.org/sdr/SWAA2025110418986.md): Angle · cracked · Sep 28, 2025 · N915WN · Boeing 7377H4 · Leading Edge Devices
  > CRACK ON ANGLE AUXILIARY TRACK SLAT 8 AT RT WING. REPLACED ANGLE AUXILIARY TRACK SLAT 8 AT RT WING IAW SRM 51-10-02 ITEM 9 & INSTALLED FASTENERS IAW SRM 51-40-02 AND DWG 114A5010; SHEET 16; REV A. AND MEASURE OF CRACK IS 0.750.
- [SDR SWAA2025110418985](https://openairdocs.org/sdr/SWAA2025110418985.md): Angle · cracked · Sep 28, 2025 · N915WN · Boeing 7377H4 · Leading Edge Devices
  > CRACK ON ANGLE AUXILIARY TRACK SLAT 7 AT RT WING (TWO EACH). REPLACED ANGLE AUXILIARY TRACK LOCATED ON SLAT 7 AT RT WING IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9. LENGTH OF CRACK 0.250 INCH.
- [SDR SWAA2025110318984](https://openairdocs.org/sdr/SWAA2025110318984.md): Angle · cracked · Sep 28, 2025 · N915WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACKED ANGLE AUXILIARY TRACK SLAT 6, RT WING. REPLACED THE ANGLE IAW SRM 51-10-02 ITEM 9, AND SRM 51-40-02. DUE TO EVALUATED CRACK ON ANGLE AND NOT FOUND ALLOWABLE DAMAGE IAW SRM-57-42-02-1A-1, ALLOWABLE DAMAGE 1. MEASUREMENT OF CRACK IS L= 2.057.
- [SDR SWAA2025110319098](https://openairdocs.org/sdr/SWAA2025110319098.md): Nut Plate · cracked · Sep 28, 2025 · N915WN · Boeing 7377H4 · Wing, Attach Fittings
  > CRACK ON RAIL NUT-PLATE, OFSS 509 INTERNAL CAVITY LEADING EDGE AT RT WING. REPLACED RAIL NUT-PLATE LOCATED OFSS 509 INTERNAL CAVITY LEADING EDGE AT RT WING IAW SRM 51-10-02 ITEM 9 SRM 51-40-02, AND DWG 112A4402, REV -, SHEET 13. MEASUREMENT OF CRACK IS L: 0
- [SDR SWAA2025103119101](https://openairdocs.org/sdr/SWAA2025103119101.md): Battery Pack · inoperative · Sep 28, 2025 · N915WN · Boeing 7377H4 · Emergency Lighting
  > INOPERATIVE BATTERY PACK BS 603 RT SIDE AT PASSENGER CABIN. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-06-960-805, OPS CHECKED OK.
- [SDR SWAA2025103019099](https://openairdocs.org/sdr/SWAA2025103019099.md): Stub Frame · cracked · Sep 28, 2025 · N915WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK INDICATION ON STUB FRAME BETWEEN BS 294.5 - 296.5, S-8 & 9R AT FWD GALLEY DOOR AREA. CRACK LENGTH 1.375 IN. REPLACED STUB FRAME IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 141A8370, SHEET 9, REV -, SHEET 10, REV D.
- [SDR SWAA2025103019097](https://openairdocs.org/sdr/SWAA2025103019097.md): Nut Plate · cracked · Sep 28, 2025 · N915WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ON RAIL NUT-PLATE LOCATED OFSS 591 INTERNAL CAVITY LEADING EDGE AT RT WING. REPLACED RAIL NUT-PLATE LOCATED OFSS 591 INTERNAL CAVITY LEADING EDGE AT RT WING IAW SRM 51-10-02 ITEM 9 AND DWG: 112A4402 SHEET: 14 REV: -.
- [SDR SWAA2025103019094](https://openairdocs.org/sdr/SWAA2025103019094.md): Nut Plate · cracked · Sep 28, 2025 · N915WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ON RAIL NUT-PLATE LOCATED OFSS 484 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT-PLATE LOCATED OFSS 484 INTERNAL CAVITY LEADING EDGE AT LT WING IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 112A4402, SHEET 13, AND SHEET 14 REV-. MEASURE O
- [SDR SWAA2025110318785](https://openairdocs.org/sdr/SWAA2025110318785.md): Access Panel · delaminated · Sep 27, 2025 · N915WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > DELAMINATED ACCESS PANEL 193AL AT FUSELAGE EXTERIOR, REPAIRED THE ACCESS PANEL 193AL IAW SRM 51-70-05-2R-6, REPAIR 6.
- [SDR SWAA2025103018783](https://openairdocs.org/sdr/SWAA2025103018783.md): Girt Bar · deteriorated · Sep 27, 2025 · N915WN · Boeing 7377H4 · Emergency Equipment
  > DETERIORATED HARDWARE GALLEY GIRT BAR FLOOR BRACKETS. REPLACED HARDWARE GALLEY GIRT BAR BRACKETS IAW AMM 25-66-02-400-801.
- [SDR SWAA2025103018784](https://openairdocs.org/sdr/SWAA2025103018784.md): Girt Bar · deteriorated · Sep 27, 2025 · N915WN · Boeing 7377H4 · Emergency Equipment
  > DETERIORATED HARDWARE AFT ENTRY GIRT BAR FLOOR BRACKETS. REPLACED HARDWARE AFT ENTRY GIRT BAR BRACKETS IAW AMM 25-66-02-400-801.
- [SDR SWAA2025110318660](https://openairdocs.org/sdr/SWAA2025110318660.md): Light · burned · Sep 26, 2025 · N915WN · Boeing 7377H4 · Emergency Lighting
  > BURNED EMERGENCY EXIT LIGHT LEFT SIDE IN PASSENGER CABIN. REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-01-960-801, STEP 2.C, 1, C THRU 2. TESTED OK.

Next page: https://openairdocs.org/aircraft/N915WN/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 = 'N915WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N915WN/reports

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