# Service difficulty reports: N569WN

A list on [N569WN](https://openairdocs.org/aircraft/N569WN.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 · 253 reports

- [SDR SWAA2026061509885](https://openairdocs.org/sdr/SWAA2026061509885.md): Stiffener · cracked · Jun 6, 2026 · N569WN · Boeing 7377CT · Fuel Storage
  > CENTER FUEL TANK VERTICAL STIFFENER IS CRACKED. BS 540, LBL 24 ON THE TOP 6 INCHES BELOW THE BOTTOM OF THE CABIN FLOOR PANEL. REF TTG8Q01CKAZ4. REMOVED AND REPLACED LBL 24.97 VERTICAL STIFFENER IAW EA 26-157-01545.
- [SDR SWAA2026061009723](https://openairdocs.org/sdr/SWAA2026061009723.md): Stiffener · cracked · Jun 6, 2026 · N569WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CENTER FUEL TANK VERTICAL STIFFENER IS CRACKED. STA 540, LBL 24 ON THE TOP 6 INCHES BELOW THE BOTTOM OF THE CABIN FLOOR PANEL. AIRCRAFT TO BE FERRIED TO PAE FOR REPAIR.
- [SDR SWAA2026060909230](https://openairdocs.org/sdr/SWAA2026060909230.md): Door · cracked · Jun 5, 2026 · N569WN · Boeing 7377CT · Landing Gear Doors
  > RIGHT MLG CENTER DOOR CRACKED. REMOVED RT CTR & INNER DOOR ASSY IAW AMM 32-13-11, OK TO CONTINUE SERVICE PER CDL 32-10-3XD AUTHORIZATION 322696. REPLACED RT GEAR SHOCK STRUT CENTER AND INNER DOOR AND ADJUSTMENT, AND FIT CLEARANCE CHECK GOOD IAW AMM 32-13-1
- [SDR SWAA2026060909228](https://openairdocs.org/sdr/SWAA2026060909228.md): Door · cracked · Jun 5, 2026 · N569WN · Boeing 7377CT · Landing Gear Doors
  > LEFT MLG CENTER DOOR CRACKED.<[01] REMOVER LT MLG CENTER AND INNER DOOR PER AMM 32-13-11. OK TO CONTINUE PER CDL 32-10-3XC. AUTHORIZATION NR 322695. REPLACED LT GEAR SHOCK STRUT CENTER AND INNER DOOR AND ADJUSTMENT AND FIT CLEARANCE CHECK GOOD IAW AMM 32-1
- [SDR SWAA2026060909265](https://openairdocs.org/sdr/SWAA2026060909265.md): Light · damaged · Jun 5, 2026 · N569WN · Boeing 7377CT · Emergency Lighting
  > PASSENGER CABIN SEAT ROW 1DEF PHOTOLUMINESCENT STRIP HAS MOISTURE UNDER CLEAR LENS. REMOVED AND REPLACED PHOTO STRIP PER AMM 33-51-15.
- [SDR SWAA2026060809275](https://openairdocs.org/sdr/SWAA2026060809275.md): Stiffener · cracked · Jun 5, 2026 · N569WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CENTER FUEL TANK VERTICAL STIFFENER IS CRACKED. STA 540; LBL 24 ON THE TOP 6 INCHES BELOW THE BOTTOM OF THE CABIN FLOOR PANEL. AIRCRAFT TO BE FERRIED TO PAE FOR REPAIR.
- [SDR SWAA2026060207887](https://openairdocs.org/sdr/SWAA2026060207887.md): Screw · worn · May 30, 2026 · N569WN · Boeing 7377CT · Emergency Lighting
  > RH OVERWING ESCAPE SLIDE LIGHT LENS HAS 1 SCREW THAT SPINS AND WILL NOT COME OUT SUSPECT BAD NUT PLATE. UPON FURTHER INVESTIGATION FOUND SCREW TO BE WORN. SCREW REPLACED PER AMM 20-50-11.
- [SDR SWAA2026060207758](https://openairdocs.org/sdr/SWAA2026060207758.md): Wire · damaged · May 30, 2026 · N569WN · Boeing 7377CT · Light System Wiring
  > OVERWING ESCAPE LIGHT AT RT WAS INOPERATIVE. REMOVED DAMAGED WIRING BETWEEN OVERWING EXIT LIGHT ASSEMBLY L7 AND D11076 AND INSTALLED NEW WIRING PER WDM 33-51-13 AND SWPM 20-61-28 AND SWPM 20-30-12. PERFORMED FUNCTIONAL TEST OF RIGHT OVERWING EXIT ESCAPE LIGHT
- [SDR SWAA2026060207757](https://openairdocs.org/sdr/SWAA2026060207757.md): Battery Pack · inoperative · May 30, 2026 · N569WN · Boeing 7377CT · Emergency Lighting
  > EMERGENCY LIGHTS ASSOCIATED WITH EMERGENCY LIGHTS BATTERY PACK M2335 ARE INOPERATIVE. REMOVED AND REPLACED M2335 EMERGENCY LIGHTS BATTERY PACK AND CHARGER AND PERFORMED SATISFACTORY INSTALLATION TEST PER AMM 33-51-06-960-806 AND AMM 33-51-06-960-805.
- [SDR SWAA2026060208281](https://openairdocs.org/sdr/SWAA2026060208281.md): Charger · inoperative · May 30, 2026 · N569WN · Boeing 7377CT · Emergency Lighting
  > EMERGENCY LIGHTS ASSOCIATED WITH EMERGENCY LIGHTS BATTERY PACK M2335 ARE INOPERATIVE. REMOVED AND REPLACED M2335 EMERGENCY LIGHTS BATTERY PACK AND CHARGER AND PERFORMED SATISFACTORY INSTALLATION TEST PER AMM 33-51-06-960-806 AND AMM 33-51-06-960-805.
- [SDR SWAA2026060202871](https://openairdocs.org/sdr/SWAA2026060202871.md): Intercostal · cracked · May 13, 2026 · N569WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > FOUND CRACKED FASTENER HOLE DURING NDI ON AFT INTERCOSTAL CLIP AT BS 663 STR 15R. NEW CLIP WAS FABRICATED PER SWA EA 26-153-01321 AND INSTALLED PER EA 26-153-01207.
- [SDR SWAA2026060202869](https://openairdocs.org/sdr/SWAA2026060202869.md): Bracket · corroded · May 13, 2026 · N569WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CORROSION ON AFT DOG BONE BRACKET BS 663.75, STR 18 R/H. AFT DOG BONE BRACKET BS 663.75, STR 18R WAS FOUND TO HAVE CORROSION. AFT DOG BONE BRACKET AT BS 663.75 STR 18R IS INSTALLED ON FAULT TTG8Q01C6509 EA 26-153-01207-WIP2 STEP 26; PER SB 737-53-1397 FIG
- [SDR SWAA2026060202870](https://openairdocs.org/sdr/SWAA2026060202870.md): Fitting · corroded · May 13, 2026 · N569WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CORROSION WAS FOUND ON RT KICK FITTING. CUSTOMER CARD TTG8Q01C1KDT WIP 1 STEP 26 ACCOMPLISHES SB 737-53-1397 FIGURE 173 INSPECTIONS AND DOES NOT ALLOW ANY CORROSION. FIGURE 179 REPLACES THE KICK FITTING ON CUSTOMER CARD TTG8Q01C6509 WIP 2 ON STEP 8. VERIFIED
- [SDR SWAA2026060293856](https://openairdocs.org/sdr/SWAA2026060293856.md): Fitting · cracked · Apr 29, 2026 · N569WN · Boeing 7377CT · Fuselage Main, Structure
  > RH PICKLEFORK FRAME FITTING AT S-18A IS CRACKED FROM FASTENER TO EDGE OF FITTING (SECOND FASTENER DOWN ON AFT SIDE OF FITTING. REMOVED AND REPLACED RT PICKLE FORK FRAME IAW SRM 51-40-02-0-G-0 AND SB 737-53-1397.
- [SDR SWAA2026010557151](https://openairdocs.org/sdr/SWAA2026010557151.md): Trim Motor · failed · Dec 31, 2025 · N569WN · Boeing 7377CT · Stabilizer Control System
  > MAIN STAB TRIM FAIL AFTER DEPARTURE. R & R STAB TRIM MOTOR IAW AMM 27-41-71. PERFORMED STAB TRIM MOTOR TEST IAW AMM 27-41-71, TESTED GOOD. PERFORMED STAB TRIM MOTOR AUTOPILOT TEST IAW AMM 22-11-81 TEST GOOD, ACFT OK FOR SERVICE
- [SDR SWAA2025080697686](https://openairdocs.org/sdr/SWAA2025080697686.md): Handle · broken · Aug 2, 2025 · N569WN · Boeing 7377CT · Service Doors
  > FWD SERVICE DOOR BULKHEAD ASSISST HANDLE BROKEN. TIGHTENED ASSISST HANDLE PER CMM 25-21-71.
- [SDR SWAA2025072895258](https://openairdocs.org/sdr/SWAA2025072895258.md): Slide · out of position · Jul 24, 2025 · N569WN · Boeing 7377CT · Escape Slide
  > AFT ENTRY DOOR SLIDE PARTIALLY PULLED OUT<[01] REPOSITIONED AFT ENTRY DOOR SLIDE PER AMM 25-66-01 AND MT 725-61-06 WITH NO DEFECTS NOTED. AC OK FOR SERVICE
- [SDR SWAA2024120271900](https://openairdocs.org/sdr/SWAA2024120271900.md): Seal · cracked · Nov 26, 2024 · N569WN · Boeing 7377CT · Horizontal Stabilizer Miscellaneous Structure
  > LEFT HORIZONTAL UPPER FORWARD SLIDER SEAL AND TRACK IS CRACKED; BUCKLED.<[01] OK TO CONTINUE PER CDL 55-10-1. AUTHORIZATION # 225145.;[02] REMOVED AND REPLACED FWD. MID; INNER TRACK STRIP P/N 181A8030U57 PER SRM 51-40-02.;[03] C/W STEPS 1-3.;[04] REPLACED LH H
- [SDR SWAA2024120273333](https://openairdocs.org/sdr/SWAA2024120273333.md): Track · buckled · Nov 26, 2024 · N569WN · Boeing 7377CT · Horizontal Stabilizer Miscellaneous Structure
  > LEFT HORIZONTAL UPPER FORWARD SLIDER SEAL AND TRACK IS CRACKED; BUCKLED.<[01] OK TO CONTINUE PER CDL 55-10-1. AUTHORIZATION # 225145.;[02] REMOVED AND REPLACED FWD. MID; INNER TRACK STRIP P/N 181A8030U57 PER SRM 51-40-02.;[03] C/W STEPS 1-3.;[04] REPLACED LH H
- [SDR SWAA2024112771594](https://openairdocs.org/sdr/SWAA2024112771594.md): Seal · cracked · Nov 26, 2024 · N569WN · Boeing 7377CT · Horizontal Stabilizer Miscellaneous Structure
  > RIGHT HORIZONTAL LOWER FORWARD SLIDER SEAL IS CRACKED; BUCKLED.<[01] REPLACED RH HORIZONTAL STAB LOWER FWD SLIDER SEAL PER AMM 53-31-31.;[02] VERIFIED REPLACED RH HORIZONTAL STAB LOWER FWD SLIDER SEAL PER AMM 53-31-31;[03] RII IS C/W. VERIFIED REPLACED RH HORI
- [SDR SWAA2024112161314](https://openairdocs.org/sdr/SWAA2024112161314.md): Panel · cracked · Nov 15, 2024 · N569WN · Boeing 7377CT · Passenger/Crew Doors
  > FED UPPER FWD COVE PANEL IS CRACKED<[01] REMOVED AND REPLACED FED REVEAL PANEL PER SOPM 20-50-01; SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND DWG:141A8220.;[02] REMOVED AND REPLACED FED REVEAL PANEL PER SOPM 20-50-01; SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND DWG:
- [SDR SWAA2024112559994](https://openairdocs.org/sdr/SWAA2024112559994.md): Battery Pack · inoperative · Nov 14, 2024 · N569WN · Boeing 7377CT · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ASSOCIATED WITH M1670 BATTERY PACK ARE INOP.<[01] REMOVE AND REPLACED BATTERY PACK M1670 AND PERFORMED GOOD TEST IAW AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.;[03] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.
- [SDR SWAA2024112556238](https://openairdocs.org/sdr/SWAA2024112556238.md): Stiffener · cracked · Nov 3, 2024 · N569WN · Boeing 7377CT · Horizontal Stabilizer Structure
  > RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB AT STABILIZER STATION 111.10 3RD VERTICAL STIFFENER IS CRACKED.<[01] REMOVED DAMAGE FROM 3RD VERTICAL STIFFENER AND WEB AT STABILIZER INSPAR RIB STA 111.1 PER SRM 55-10-09-2R-4 PARA. 4. B (1) - (2).<BR><BR>INSTALLED
- [SDR SWAA2024112555555](https://openairdocs.org/sdr/SWAA2024112555555.md): Radome · delaminated · Oct 31, 2024 · N569WN · Boeing 7377CT · Aerodynamic Fairings
  > PER CUSTOMER REQUEST; FOUND NOSE RADOME DELAMINATED AT THE VERY TIP MARKED<[01] REMOVED DAMAGED RADOME BOOT AND FOUND A DELAMINATION IN THE COMPOSITE AT THE DISCREPANT LOCATION IAW AMM 53-52-00-000-802 PARAGRAPH 4.C(1-2).;[02] VERIFIED CORRECTIVE ACTION 1;[03]
- [SDR SWAA2024112555322](https://openairdocs.org/sdr/SWAA2024112555322.md): Skin · corroded · Oct 31, 2024 · N569WN · Boeing 7377CT · Fuselage Main, Plate/Skin
  > CORROSION ON EXTERNAL LOWER FUSELAGE SKIN COMMON TO ATC ANTENNA STA 351.50-357.50; BLO; WL 149.<[01] REPAIRED LWR SKIN COMMON TO ATC ANTENNA IAW EA 24-153-03031;[02] VERIFIED CORRECTIVE ACTION
- [SDR SWAA2024112554736](https://openairdocs.org/sdr/SWAA2024112554736.md): Panel · cracked · Oct 30, 2024 · N569WN · Boeing 7377CT · Cargo Compartments
  > CRACKED PANEL BREAK AT BS540; LBL25-LBL45; WL208.<[01] REMOVED DAMAGED PANEL; BRAKE ASSY IAW SRM 51-40-02.<BR>INSTALLED NEW PANEL; BRAKE ASSY IAW SRM 51-40-02 AND DWG 143A0060 REV: A.;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.
- [SDR SWAA2024112554362](https://openairdocs.org/sdr/SWAA2024112554362.md): Attach Angle · cracked · Oct 28, 2024 · N569WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CRACKED ATTACH ANGLE AT MID CABIN BS690 RBL1 WL206. MARKED<[01] REMOVED AND REPLACED ATTACH ANGLE (BRACKET) AT BS BS690 RBL 1 WL 206 PER SRM 51-40-02-0G-0 AND BOEING DWG 273A9111.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2024112554176](https://openairdocs.org/sdr/SWAA2024112554176.md): Seat Track · corroded · Oct 28, 2024 · N569WN · Boeing 7377CT · Fuselage Internal Mounting Structure
  > CORROSION ON PAX CABIN SEAT TRACK RBL25 BS554; BS562; BS661; BS712CROWN. WL208. MARKED<[01] REMOVED CORROSION FROM CABIN SEAT TRACK ON RBL25 BS552.5 3'X.70'X.015' ON WELL. BS556.5 8'X.70'X.007' ON WELL. BS661 11'X.70'X.011' ON WELL. BS709 4'X.50'X.015' ON WELL
- [SDR SWAA2024112554363](https://openairdocs.org/sdr/SWAA2024112554363.md): Stiffener · cracked · Oct 28, 2024 · N569WN · Boeing 7377CT · Horizontal Stabilizer Structure
  > RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 111.10; 4TH VERTICAL STIFFENER IS CRACKED.<[01] REMOVED DAMAGE FROM 4TH VERTICAL STIFFENER AND WEB AT STABILIZER INSPAR RIB STA 111.1 PER SRM 55-10-09-2R-4 PARA. 4. B (1) - (2).<BR><BR>INSTALLE
- [SDR SWAA2024112554360](https://openairdocs.org/sdr/SWAA2024112554360.md): Panel · cracked · Oct 28, 2024 · N569WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CRACKED PANEL BREAK AT MID CABIN BS540 RBL1 WL208.<[01] REMOVED AND REPLACED PANEL BREAK AT BS540 RBL1 TO RBL24 WL 208 PER SRM 51-40-02-0G-0 AND BOEING DWG 143A0060 REV. A.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2024112554366](https://openairdocs.org/sdr/SWAA2024112554366.md): Skin · corroded · Oct 28, 2024 · N569WN · Boeing 7377CT · Fuselage Main, Plate/Skin
  > CORROSION ON EXTERNAL FUSELAGE SKIN UNDER VERTICAL STAB BS1016 - BS1033 LBL12 TO RBL12 WL308. MARKED<[01] COMPLETED CARD;[02] ACCOMPLISHED PER EA 24-153-03047-;[03] VERIFIED CORRECTIVE ACTION
- [SDR SWAA2024112553950](https://openairdocs.org/sdr/SWAA2024112553950.md): Rib · cracked · Oct 27, 2024 · N569WN · Boeing 7377CT · Horizontal Stabilizer Structure
  > LEFT HORIZONTAL STAB REMOVABLE L/E 331B RIB #4 CRACKED<[01] TASK COMPLETE:<BR>REMOVED CRACKED #4 RIB ON L/E 331B AND REPLACED WITH NEW (PN: 186A1304-1 LOT: 1582297-1) IAW SRM 51-40-02-0G-0 AND DWG 186A1001.;[02] CORRECTION TO ACTION 1; INCORRECT DRAWING LISTED
- [SDR SWAA2024112553951](https://openairdocs.org/sdr/SWAA2024112553951.md): Rib · cracked · Oct 27, 2024 · N569WN · Boeing 7377CT · Horizontal Stabilizer Structure
  > RIGHT HORIZONTAL STAB REMOVABLE L/E 341B RIB #5 CRACKED<[01] TASK COMPLETE:<BR>REMOVED CRACKED #5 RIB ON L/E 341B AND REPLACED WITH NEW (PN: 186A1305-2 LOT: 1582412-2) IAW SRM 51-40-02-0G-0 AND DWG 186A1001.;[02] CORRECTION TO ACTION 1; INCORRECT DRAWING LISTE
- [SDR SWAA2024092039256](https://openairdocs.org/sdr/SWAA2024092039256.md): Battery Pack · inoperative · Sep 19, 2024 · N569WN · Boeing 7377CT · Emergency Lighting
  > LH EMERGENCY EXIT OVERWING LIGHTS INOP<[01] R&R EMERGENCY LIGHT BATTERY PACK FOR OVERWING EXIT DOOR PER AMM 33-51-06. OPS CHECK GOOD.
- [SDR SWAA2024082227525](https://openairdocs.org/sdr/SWAA2024082227525.md): Lamp · inoperative · Aug 19, 2024 · N569WN · Boeing 7377CT · Emergency Lighting
  > LH OVERWING EMERGENCY EXIT LIGHT INOPERATIVE.<[01] RELAMPED LH OVERWING EMERGENCY EXIT LIGHT IAW AMM 33-51-04.
- [SDR SWAA2024070507848](https://openairdocs.org/sdr/SWAA2024070507848.md): Battery Pack · no test · Jul 2, 2024 · N569WN · Boeing 7377CT · Emergency Lighting
  > EMX LIGHT BATT/POWER SUPPLY M01673 FAILS TO ILLUMINATE LIGHTS<[01] 01 - REMOVED AND REPLACED EMX BATTERY PACK AND POWER SUPPLY M01673 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)];[02] 01 - REMOVED AND REPLACED EMX BATTERY
- [SDR SWAA2024070507844](https://openairdocs.org/sdr/SWAA2024070507844.md): Handle · loose · Jul 2, 2024 · N569WN · Boeing 7377CT · Emergency Equipment
  > AFT SERVICE DOOR ASSIST HANDLE A/C SIDE IS LOOSE<[01] TIGHTENED AFT SERVICE DOOR ASSIST HANDLE A/C SIDE PER AMM 20-50-11
- [SDR SWAA2024062705429](https://openairdocs.org/sdr/SWAA2024062705429.md): Lamp · inoperative · Jun 25, 2024 · N569WN · Boeing 7377CT · Emergency Lighting
  > AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] RE LAMPED SLIDE LIGHT IAW AMM 33-51-04. OPS CHECK GOOD
- [SDR SWAA2024061903258](https://openairdocs.org/sdr/SWAA2024061903258.md): Bracket · loose · Jun 19, 2024 · N569WN · Boeing 7377CT · Emergency Equipment
  > FORWARD ENTRY DOOR GIRT BAR STOWAGE BRACKET LOOSE<[01] RESECURED FWD ENTRY DOOR FWDGIRT BAR BRACKET REF AMM 25-66-02.
- [SDR SWAA2024052387864](https://openairdocs.org/sdr/SWAA2024052387864.md): Slide · partial deploy · May 20, 2024 · N569WN · Boeing 7377CT · Escape Slide
  > FORWARD SERVICE DOOR SLIDE PARTIALLY DEPLOYED/UNPACKED<[01] REINSTALLED FWD SERVICE DOOR SLIDE; FOUND IT NOT PARTIALLY DEPLOYED AND FOUND NO DAMAGE INSTALLED PER MT 725-61-06 OPS CHECK GOOD.;[02] CW
- [SDR SWAA2023121830941](https://openairdocs.org/sdr/SWAA2023121830941.md): Skin · handler error · Dec 11, 2023 · N569WN · Boeing 7377CT · Fuselage Main, Plate/Skin
  > PROVO TRUCK COLLIDED WITH CAPT SIDE ENTRY AFT DOOR<[01] REPAIRED ON EA 23-153-03617 (N569WN - SWA - REPAIR - SECTION 47 FUSELAGE SKIN DAMAGE BETWEEN STA 914 - 937 AND BETWEEN STR 20L AND 21L) [TTG8Q00QBG9R]
- [SDR SWAA2023121830942](https://openairdocs.org/sdr/SWAA2023121830942.md): Stringer · cracked · Dec 11, 2023 · N569WN · Boeing 7377CT · Fuselage Main, Longeron/Stringer
  > REF TO LP 2398631 FOUND DAMAGE CAUSED BY PROVO TRUCK IN BETWEEN STATIONS 914-937 AND STRINGERS S-20L & S-21L LENGTH OF 7-12/32 AND WIDTH OF 15-8/32 13/64TH DEEP FOUND SHEAR TIE AT STATION 927 CRACKED BETWEEN STRINGERS S-20L & S-21L<[01] REPAIRED PER EA 23-153-
- [SDR SWAA2023101710911](https://openairdocs.org/sdr/SWAA2023101710911.md): Light · inoperative · Oct 15, 2023 · N569WN · Boeing 7377CT · Emergency Lighting
  > AREA EMERGENCY LIGHT AT ROW 6FED INOP<[01] RELAMPED AREA EMERGENCY LIGHT AT ROW 6FED REF AMM 33-51-03. OPS CHK GOOD.
- [SDR SWAA2023072481094](https://openairdocs.org/sdr/SWAA2023072481094.md): Lens · broken · Jul 20, 2023 · N569WN · Boeing 7377CT · Emergency Lighting
  > FWD ENTRY DOOR LOWER EXIT SIGN LENS BROKEN.<[01] R+R FWD ENTRY DOOR LOWER EXIT SIGN LENS PER AMM 33-51-01.
- [SDR SWAA2023052450847](https://openairdocs.org/sdr/SWAA2023052450847.md): Light · inoperative · May 21, 2023 · N569WN · Boeing 7377CT · Emergency Lighting
  > AFT R/H SIDE EMERGENCY SLIDE LIGHT INOP<[01] RELAMPED AFT R/H SIDE EMERGENCY SLIDE LIGHT PER AMM 33-51-04.
- [SDR SWAA2023051749156](https://openairdocs.org/sdr/SWAA2023051749156.md): Light · out of adjust · May 15, 2023 · N569WN · Boeing 7377CT · Emergency Lighting
  > FWD RIGHT SIDE ILLUMINATION STRIP LIFTING.<[01] APPLIED DOUBLE SIDE TAPE TO ILLUMINATES STRIP PER SIP.
- [SDR SWAA2023051548481](https://openairdocs.org/sdr/SWAA2023051548481.md): Battery Pack · inoperative · May 13, 2023 · N569WN · Boeing 7377CT · Emergency Lighting
  > FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP<[01] REMOVED AND REPLACED FWD ENTRY DOOR BATTERY PACK IAW AMM 33-51-06 OPS CHECK GOOD AT THIS TIME
- [SDR SWAA2023031515943](https://openairdocs.org/sdr/SWAA2023031515943.md): Strip · loose · Mar 11, 2023 · N569WN · Boeing 7377CT · Emergency Lighting
  > FLOOR LIGHTING PHOTOLUMENESCENT STRIP AT FWD CABIN COMING LOOSE.<[01] RESECURED STRIP PER AMM 33-51-15
- [SDR SWAA2022120277578](https://openairdocs.org/sdr/SWAA2022120277578.md): Battery Pack · inoperative · Dec 2, 2022 · N569WN · Boeing 7377CT · Emergency Lighting
  > ENEMERGENCY LIGHTS AT SEAT 6C; 8D; 9A AND 12A INOPERATIVE. REPLACED BATTERY PACK AND CHARGER ASSEMBLY IAW AMM 33-51-06, OPS CHECKED GOOD.
- [SDR SWAA2022120277656](https://openairdocs.org/sdr/SWAA2022120277656.md): Charger · inoperative · Dec 2, 2022 · N569WN · Boeing 7377CT · Emergency Lighting
  > ENEMERGENCY LIGHTS AT SEAT 6C; 8D; 9A AND 12A INOPERATIVE. REPLACED BATTERY PACK AND CHARGER ASSEMBLY PER AMM 33-51-06;OPS CHECK GOOD

Next page: https://openairdocs.org/aircraft/N569WN/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 = 'N569WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N569WN/reports

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