# Service difficulty reports: N914WN

A list on [N914WN](https://openairdocs.org/aircraft/N914WN.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 · 256 reports

- [SDR SWAA2026101256846](https://openairdocs.org/sdr/SWAA2026101256846.md): Cover · loose · Oct 8, 2026 · N914WN · Boeing 7377H4 · Escape Slide
  > ESCAPE SLIDE PACK COVER LOOSE AFT ENTRY DOOR. REMOVED ADJUSTED & REINSTALLED AFT ENTRY ESCAPE SLIDE IAW AMM 25-66-01.
- [SDR SWAA2026061010645](https://openairdocs.org/sdr/SWAA2026061010645.md): Battery Pack · no test · Jun 10, 2026 · N914WN · Boeing 7377H4 · Emergency Lighting
  > AFT LEFT EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK IAW MM 33-51-06.
- [SDR SWAA2026061010644](https://openairdocs.org/sdr/SWAA2026061010644.md): Battery Pack · no test · Jun 10, 2026 · N914WN · Boeing 7377H4 · Emergency Lighting
  > AFT RT EMERGENCY LIGHTING BATTERY PACK FAILED A CAPACITY CHECK. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK IAW MM 33-51-06.
- [SDR SWAA2025120943260](https://openairdocs.org/sdr/SWAA2025120943260.md): Handle · loose · Dec 5, 2025 · N914WN · Boeing 7377H4 · Passenger/Crew Doors
  > PAX CABIN AFT LEFT DOOR LINING ASSISTANT HANDLE LOOSE. PAX CABIN AFT LEFT DOOR LINING ASSISTANT HANDLE IAW AMM-52-13-31-400-802 STEP 3.G.(2).
- [SDR SWAA2025121039101](https://openairdocs.org/sdr/SWAA2025121039101.md): Access Panel · cracked · Nov 23, 2025 · N914WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACKED ACCESS PANEL 344GB AT RT HORIZONTAL STABILIZER. REPAIRED ACCESS PANEL 344GB AT RT HORIZONTAL STABILIZER IAW SRM 55-20-01-2R-4, REPAIR 4.
- [SDR SWAA2025121039100](https://openairdocs.org/sdr/SWAA2025121039100.md): Access Panel · cracked · Nov 23, 2025 · N914WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACKED ACCESS PANEL 334GB AT LT HORIZONTAL STABILIZER. REPAIRED ACCESS PANEL 334GB AT LT HORIZONTAL STABILIZER IAW SRM 55-20-01-2R-4, REPAIR 4.
- [SDR SWAA2025120939102](https://openairdocs.org/sdr/SWAA2025120939102.md): Access Panel · damaged · Nov 23, 2025 · N914WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > ELONGATED HOLE ON ACCESS PANEL 334GB AT LT HORIZONTAL STABILIZER. REPAIRED ACCESS PANEL 334GB AT LT HORIZONTAL STABILIZER IAW SRM 51-70-04-2R-9, REPAIR 9.
- [SDR SWAA2025121035632](https://openairdocs.org/sdr/SWAA2025121035632.md): Stiffener · cracked · Nov 15, 2025 · N914WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > CRACK ON STIFFENER LOCATED ON STAB STA 129.50 AT FRONT SPAR RT HORIZONTAL STABILIZER. REPLACED STIFFENER ON STAB STA 129.50 AT FRONT SPAR RT HORIZONTAL STABILIZER IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, AND DWG 182A5305, SHEET 1, REV C.
- [SDR SWAA2025121034210](https://openairdocs.org/sdr/SWAA2025121034210.md): Filler · mismanufactured · Nov 11, 2025 · N914WN · Boeing 7377H4 · Wing Main, Frame Structure
  > RIGHT WING OTBD FIXED L/E REPAIR, BTW SS 61.75 & SS 67.53, REPAIR FILLER DOES NOT HAVE THE REQUIRED SIZE IAW EA 1-757-16674. FILLER HAS BEEN ADJUSTED ON RT WING OTBD FIXED L/E IAW EA 1-757-16674 AND EA 57-0485-19, PART 2, STEP 11, FIG 2, AND INSTALLED IAW E
- [SDR SWAA2025121033790](https://openairdocs.org/sdr/SWAA2025121033790.md): Web · cracked · Nov 11, 2025 · N914WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > CRACKED NR 2 VAPOR BARRIER WEB, BS 663.75, RBL 25 MAIN WHEEL WELL. REPAIRED THE VAPOR BARRIER WEB IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2025121034214](https://openairdocs.org/sdr/SWAA2025121034214.md): Floorbeam · cracked · Nov 11, 2025 · N914WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM CRACKED, BS 540, BL 0 - LBL 24.75. REPLACED THE FLOORBEAM IAW SRM 51-40-02-0G-0, AND DWG 143A0060, SHEET 46, REV -..
- [SDR SWAA2025120434212](https://openairdocs.org/sdr/SWAA2025120434212.md): Floorbeam · cracked · Nov 11, 2025 · N914WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM HAS CRACK AT BS 540; BL 0 TO RBL 24.75. REPLACED THE FLOORBEAM IAW SRM 51-40-02-0G-0, DWG 143A5240, SHEET 13, REV -, AND DWG 143A0060, SHEET 46, REV -.
- [SDR SWAA2025121033223](https://openairdocs.org/sdr/SWAA2025121033223.md): Bracket · cracked · Nov 9, 2025 · N914WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ACCESS PANEL 651FB TRAILING EDGE BRACKET RT WING. REPLACED BRACKET ON ACCESS PANEL 651FB TRAILING EDGE BRACKET RT WING IAW SRM 51-40-02 AND SRM 51-10-02. MEASUREMENT OF CRACK: L=0.895".
- [SDR SWAA2025121033220](https://openairdocs.org/sdr/SWAA2025121033220.md): Bracket · cracked · Nov 9, 2025 · N914WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ACCESS PANEL 551FB TRAILING EDGE BRACKET LT WING. REPLACED BRACKET ON ACCESS PANEL 551FB TRAILING EDGE LT WING IAW SRM 51-40-02, SRM 51-20-01, AND DWG 115A2710, SHEET 9, REV A.
- [SDR SWAA2025121033221](https://openairdocs.org/sdr/SWAA2025121033221.md): Access Panel · damaged · Nov 9, 2025 · N914WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLE ACCESS PANEL 651FB TRAILING EDGE LOCATED ON STIFFENER RT WING. REPLACED BEAM ON ACCESS PANEL 651FB TRAILING EDGE LOCATED ON STIFFENER RT WING IAW SRM 51-40-02 AND SRM 51-10-02, PARAGRAPH 9, AND DWG 115A2710 SHEET 9, REV A.
- [SDR SWAA2025121033222](https://openairdocs.org/sdr/SWAA2025121033222.md): Support Angle · cracked · Nov 9, 2025 · N914WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ACCESS PANEL 551GB TRAILING EDGE SUPPORT ANGLE LT WING. REPLACED SUPPORT ANGLE ON ACCESS PANEL 551GB TRAILING EDGE IAW SRM 51-40-02; SRM 51-10-02, AND DWG 115A2714 SHEET:10 REV-.
- [SDR SWAA2025121033217](https://openairdocs.org/sdr/SWAA2025121033217.md): Plate · cracked · Nov 8, 2025 · N914WN · Boeing 7377H4 · Wing Main, Frame Structure
  > CRACKED CORRUGATED PLATE LOCATED TRAILING EDGE IRSS 216 AT LT WING. MEASUREMENT OF CRACK: L 0.800 INCHES. REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE IRSS 216 AT LT WING IAW SRM 51-40-02-0G, SRM 51-10-02-0G, PARAGRAPH 9, AND DWG 115A2713, SHEET 4, REV-.
- [SDR SWAA2025121033218](https://openairdocs.org/sdr/SWAA2025121033218.md): Plate · cracked · Nov 8, 2025 · N914WN · Boeing 7377H4 · Wing Main, Frame Structure
  > CRACK CORRUGATED PLATE ON TRAILING EDGE IRSS 216 AT RT WING. REPLACED CORRUGATED PLATE ON TRAILING EDGE IRSS 216, RT WING IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, AND DWG 115A2781, SHEET 2, REV B.
- [SDR SWAA2025121033219](https://openairdocs.org/sdr/SWAA2025121033219.md): Support Bracket · cracked · Nov 8, 2025 · N914WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK SUPPORT BRACKET LOCATED TRAILING EDGE IRSS139 RT WING. MEASURE OF CRACK SUPPORT BRACKET IS L:1.664 INCHES, AND NOT FOUND ALLOWABLE DAMAGE, SRM 57-51-02-1A-1. SUPPORT BRACKET MUST BE REPLACED. REPLACED SUPPORT BRACKET LOCATED TRAILING EDGE IRSS 139 RT W
- [SDR SWAA2025121033037](https://openairdocs.org/sdr/SWAA2025121033037.md): Angle · cracked · Nov 7, 2025 · N914WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED BILGE ANGLE, BS 867, S26L IN THE AFT CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02-0G-0, 51-10-02-0G-0, STEP 9, AND DWG 149A8102, SHEET 17, REV -. MEASUREMENT OF CRACK: 0.276 IN.
- [SDR SWAA2025121033041](https://openairdocs.org/sdr/SWAA2025121033041.md): Plate · corroded · Nov 7, 2025 · N914WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORRODED BILGE PLATE BTW BS 787 - 796, S25R, WL 156. REPLACED THE BILGE PLATE IAW SRM 51-40-02, AND DWG 146A0081, SHEET 37, REV-.
- [SDR SWAA2025120933039](https://openairdocs.org/sdr/SWAA2025120933039.md): Cargo Track · cracked · Nov 7, 2025 · N914WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK TRACK RBL 13.80 ON BS 767 IN THE AFT CARGO COMPARTMENT. PERFORMED REPAIR ON TRACK, RBL 13.80 ON BS 767 AT AFT CARGO COMPARTMENT IAW SRM 53-00-53-2R-3, REPAIR 3; ALTERNATIVE 1 FIGURE 203.
- [SDR SWAA2025120933040](https://openairdocs.org/sdr/SWAA2025120933040.md): Cargo Track · cracked · Nov 7, 2025 · N914WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK TRACK RBL 13.80 ON BS 727C IN THE AFT CARGO COMPARTMENT. PERFORMED REPAIR ON TRACK LOC. RBL 13.80 ON BS 727C AT AFT CARGO COMPARTMENT IAW SRM 53-00-53-2R-3 REPAIR 3; ALTERNATIVE 1 FIGURE 203.
- [SDR SWAA2025121032243](https://openairdocs.org/sdr/SWAA2025121032243.md): Support · corroded · Nov 5, 2025 · N914WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORRODED LOWER SILL, BTW BS 440 - 492.4, RBL 22, WL 156 IN FWD CARGO BAY. (8 EA). REPLACED THE LOWER SILL IAW SRM 51-40-02, AND DWG 143A8330, SHEET 42, REV A.
- [SDR SWAA2025121046461](https://openairdocs.org/sdr/SWAA2025121046461.md): Web · corroded · Nov 5, 2025 · N914WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SHIELD WEB LOCATED BTW BS 492.4 - 500A, S26R, WL 156 IN FWD CARGO COMPARTMENT. REPLACED SHIELD WEB AND FASTENERS IAW SRM 51-40-02, AND DWG 143A0080, SHEET 39, REV-.
- [SDR SWAA2025121032242](https://openairdocs.org/sdr/SWAA2025121032242.md): Web · corroded · Nov 5, 2025 · N914WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CORROSION SHIELD WEB LOCATED BTW BS 492.4 - 500A, S26R, WL 156 IN FWD CARGO COMPARTMENT. REPLACED THE SHIELD WEB AND FASTENERS BS 492.4 - 500A, S26R, WL 156 IAW SRM 51-40-02, AND DWG 143A0080, SHEET 39, REV-.
- [SDR SWAA2025120432245](https://openairdocs.org/sdr/SWAA2025120432245.md): Support Angle · cracked · Nov 5, 2025 · N914WN · Boeing 7377H4 · Leading Edge Devices
  > CRACK SUPPORT ANGLE ON AUXILIARY TRACK SLAT 8 INBOARD POSITION AT RT WING. REPLACED SUPPORT ANGLE ON AUXILIARY TRACK SLAT 8 INBD POSITION AT RT WING IAW CMM-57-43-01, PAGE 702, STEP 3 C, ITEM 9.
- [SDR SWAA2025121031762](https://openairdocs.org/sdr/SWAA2025121031762.md): Access Panel · delaminated · Nov 4, 2025 · N914WN · Boeing 7377H4 · Wing, Plate/Skin
  > DELAMINATED ACCESS PANEL 542EB AT LT WING. REPLACED BY A NEW ACCESS PANEL 542EB IAW AMM 27-51-18-400-802, STEP 5.G(5).
- [SDR SWAA2025121046456](https://openairdocs.org/sdr/SWAA2025121046456.md): Access Panel · delaminated · Nov 4, 2025 · N914WN · Boeing 7377H4 · Wing, Plate/Skin
  > DELAMINATED ACCESS PANEL 542EB AT LT WING. REPLACED DELAMINATED ACCESS PANEL 542EB DUE TO WAS FOUND OUT OF LIMIT IAW AMM 27-51-18-400-802 STEP 5.G5.
- [SDR SWAA2025121030900](https://openairdocs.org/sdr/SWAA2025121030900.md): Scuff Plate · cracked · Nov 2, 2025 · N914WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED FWD SCUFF PLATE IN THE FWD CARGO BAY CUTOUT. REPAIRED FWD SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, AND BAC 5975.
- [SDR SWAA2025121031135](https://openairdocs.org/sdr/SWAA2025121031135.md): Stiffener · cracked · Nov 2, 2025 · N914WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > FWD CARGO BAY BULKHEAD VERTICAL STIFFENER CRACKED, BS 540, LBL 24.97. REPLACED VERTICAL STIFFENER IAW SRM 51-40-02-0G-0, SRM 51-10-02-G-0, ITEM 9, AND DWG 11A2001, SHEET 113, REV B & DWG 111A2000, SHEET 49, REV -.
- [SDR SWAA2025121031136](https://openairdocs.org/sdr/SWAA2025121031136.md): Stiffener · cracked · Nov 2, 2025 · N914WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > FWD CARGO BAY BULKHEAD VERTICAL STIFFENER CRACKED BS 540, LBL 0.22. REPLACED THE VERTICAL STIFFENER IAW SRM 51-40-02-0G-0, SRM 51-10-02-G-0, ITEM 9, AND DWG 11A2001, SHEET 113, REV B.
- [SDR SWAA2025121031139](https://openairdocs.org/sdr/SWAA2025121031139.md): Gusset · cracked · Nov 2, 2025 · N914WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED GUSSET, BS 500D, S19R IN THE FWD CARGO BAY. REPLACED THE GUSSET IAW SRM 51-40-02-0G-0, AND DWG 143A7902, SHEET 209, REV-.
- [SDR SWAA2025121031140](https://openairdocs.org/sdr/SWAA2025121031140.md): Gusset · cracked · Nov 2, 2025 · N914WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED GUSSET, BS 500D, S19L IN FWD CARGO BAY. INSTALLED GUSSET IAW SRM 51-40-02-0G-0, AND DWG 143A7902, SHEET 209, REV-.
- [SDR SWAA2025121031134](https://openairdocs.org/sdr/SWAA2025121031134.md): Plate · cracked · Nov 2, 2025 · N914WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACKED SEAL PLATE, ACCESS PANEL 333AB AT THE LT HORIZONTAL STAB. REPLACED THE SEAL ON ACCESS PANEL 333AB AT LT HORIZONTAL STAB IAW SRM 51-40-02-0G-0, AND SRM 51-10-02-0G-0, STEP 9.
- [SDR SWAA2025120931138](https://openairdocs.org/sdr/SWAA2025120931138.md): Support Bracket · cracked · Nov 2, 2025 · N914WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACK SUPPORT BRACKET LOCATED BS 540 AT LEVEL RBL 6 AT AIR CONDITIONING. REPLACED SUPPORT SUPPORT BRACKET LOCATED BS 540 AT LEVEL RBL 6 AT AIR CONDITIONING BAY IAW SRM 51-40-02 & DWG 212A1101 SHEET 3 REV -.
- [SDR SWAA2025120931023](https://openairdocs.org/sdr/SWAA2025120931023.md): Rib · cracked · Nov 2, 2025 · N914WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK ON INSPAR RIB LOCATED STAB STA 129.50 AND 28 INCHES OF FROM SPAR AT RT HORIZONTAL STABILIZER. STEP 5 ANND STEP 6. EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 250593109 AND DUE DATE: 06-OCT-26. REPAIRED INSPAR RIB LOCATED STAB STA 129.50 AND 28 I
- [SDR SWAA2025121030757](https://openairdocs.org/sdr/SWAA2025121030757.md): Pressure Deck · cracked · Nov 1, 2025 · N914WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK INDICATION ON THE HORIZONTAL PRESSURE DECK WEB, LBL 31, BS 663 IN MAIN WHEEL WELL. CRACK LENGTH: 0.312 IN. PERFORMED REPAIR ON HORIZONTAL PRESSURE DECK WEB IAW SRM 53-40-51-2R-2, REPAIR 2, FIGURE 203, AND EA 25-153-03155.
- [SDR SWAA2025121030762](https://openairdocs.org/sdr/SWAA2025121030762.md): Skin · corroded · Nov 1, 2025 · N914WN · Boeing 7377H4 · Fluid Service Doors
  > CORROSION ON INTERNAL SKIN TOILET SERVICE DOOR 145AL, LOWER FUSELAGE. PERFORMED REPAIR ON TOILET SERVICE DOOR 145AL AT LOWER FUSELAGE IAW SRM 52-40-01-2R-8, REPAIR 8, FIGURE 202.
- [SDR SWAA2025121030756](https://openairdocs.org/sdr/SWAA2025121030756.md): Stub Frame · cracked · Nov 1, 2025 · N914WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK INDICATION ON STUB FRAME, BETWEEN BS 294.5 - 296.5, S8R - 9R AT THE FWD GALLEY DOOR AREA. CRACK LENGTH: 1.187 IN. REPLACED THE STUB FRAME IAW SRM 51-40-02-0G-0, AND DWG 141A8370, SHEET 10, REV D.
- [SDR SWAA2025121030758](https://openairdocs.org/sdr/SWAA2025121030758.md): Access Panel · cracked · Nov 1, 2025 · N914WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CRACKED ACCESS PANEL 193AR AT FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL 193AR IAW SRM 51-70-05-2R-2, REPAIR 2.
- [SDR SWAA2025121050826](https://openairdocs.org/sdr/SWAA2025121050826.md): Access Panel · cracked · Nov 1, 2025 · N914WN · Boeing 7377H4 · Aerodynamic Fairings
  > CRACKED ACCESS PANEL 193AL, BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL 193AL BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-05-2R-2, REPAIR 2.
- [SDR SWAA2025120430899](https://openairdocs.org/sdr/SWAA2025120430899.md): Support Angle · cracked · Nov 1, 2025 · N914WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE, BS 695, RBL 24.75, WL208.1 IN PASSENGER CABIN. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, DWG 111A6000, SHEET 304, REV -, AND DWG 273A9110, SHEET 6, REV A.
- [SDR SWAA2025120930608](https://openairdocs.org/sdr/SWAA2025120930608.md): Light · broken · Oct 31, 2025 · N914WN · Boeing 7377H4 · Emergency Lighting
  > BROKEN PHOTOLUMINESCENT STRIPS RT AT PASSENGER CABIN ( 6 EA). REPLACED PHOTOLUMINESCENT STRIP IAW AMM-33-51-15-400-802.
- [SDR SWAA2025120930609](https://openairdocs.org/sdr/SWAA2025120930609.md): Light · cracked · Oct 31, 2025 · N914WN · Boeing 7377H4 · Emergency Lighting
  > CRACKED PHOTOLUMINESCENT STRIPS LT IN PASSENGER CABIN (5 EA). REPLACED PHOTOLUMINESCENT STRIP AT LT PASSENGER CABIN (5 EA) IAW AMM-33-51-15-400-802
- [SDR SWAA2025121030190](https://openairdocs.org/sdr/SWAA2025121030190.md): Vapor Barrier · cracked · Oct 30, 2025 · N914WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > CRACK VAPOR BARRIER WEB, BS 663.75, BTW RBL 25 - 35. REPAIRED THE VAPOR BARRIER WEB IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2025072895488](https://openairdocs.org/sdr/SWAA2025072895488.md): Pcu · faulty · Jul 25, 2025 · N914WN · Boeing 7377H4 · Rudder Control System
  > DURING CLIMB OUT AT 14000 AND AGAIN AT 16000 FT THE RUDDER KICKED LEFT WITHOUT PILOT INPUT. OCCURRED AGAIN AT FL370 APPROX 30 MINUTES LATER. AUTOPILOT DID NOT DISENGAGE<[01] REMOVED AND REPLACED MAIN RUDDER PCU PER AMM 27-21-91. ALL OPS CHECKS NORMAL.;[02] REM
- [SDR SWAA2025071691134](https://openairdocs.org/sdr/SWAA2025071691134.md): Lens · damaged · Jul 13, 2025 · N914WN · Boeing 7377H4 · Emergency Lighting
  > OVERHEAD EMERGENCY EXIT SIGN DAMAGED BY PASSENGER. FOUND FWD LENS OF CENTER AISLE OVERHEAD EXIT SIGN BY EMERGENCY EXIT ROW CAME LOOSE. RESECURED LENS TO HOUSING PER SIP.
- [SDR SWAA2025060276130](https://openairdocs.org/sdr/SWAA2025060276130.md): Lamp · inoperative · May 29, 2025 · N914WN · Boeing 7377H4 · Emergency Lighting
  > R/H OVER WING EMERGENCY LIGHT INOP. <[01] R/R R/H OVERWING EMERGENCY EXIT LAMP PER AMM 33-51-04. OPS CHECK GOOD.
- [SDR SWAA2025050565143](https://openairdocs.org/sdr/SWAA2025050565143.md): Light · broken · Apr 29, 2025 · N914WN · Boeing 7377H4 · Emergency Lighting
  > FOUND AFT R2 DOOR LOWER EMERGENCY EXIT LIGHT ASSY BROKEN.<[01] REMOVED + REPLACED R2 DOOR LOWER EMERGENCY EXIT LIGHT ASSY IAW AMM 33-51-01; OPS CHECK GOOD.;[02] REMOVED + REPLACED R2 DOOR LOWER EMERGENCY EXIT LIGHT ASSY IAW AMM 33-51-01; OPS CHECK GOOD.

Next page: https://openairdocs.org/aircraft/N914WN/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 = 'N914WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N914WN/reports

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