# Service difficulty reports: N567WN

A list on [N567WN](https://openairdocs.org/aircraft/N567WN.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 5 · 225 reports

- [SDR SWAA2026092324437](https://openairdocs.org/sdr/SWAA2026092324437.md): Assist Handle · loose · Sep 19, 2026 · N567WN · Boeing 7377CT · Passenger/Crew Doors
  > FORWARD GALLEY R1 DOOR ASSIST HANDLE LOOSE. SECURED THE ASSIST HANDLE IAW CMM 25-31-03.
- [SDR SWAA2026042792357](https://openairdocs.org/sdr/SWAA2026042792357.md): Battery Pack · no test · Apr 24, 2026 · N567WN · Boeing 7377CT · Emergency Lighting
  > EMERGENCY BATTERY PACK AT 14 DEF M1669 FAILED CAPACITY CHECK. R&R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026040987817](https://openairdocs.org/sdr/SWAA2026040987817.md): Lamp · inoperative · Apr 9, 2026 · N567WN · Boeing 7377CT · Emergency Lighting
  > AFT. OF L2 DOOR EXTERIOR EMERGENCY LIGHTS INOP<[01] RELAMPED L2 EXTERIOR EMERGENCY LIGHT AND CHECK GROUND WIRES. PER AMM 33-51-04. REMOVED AND REPLACED L2 DOOR SLIDE EMERGENCY LIGHT BATTERY PACK AND CHARGER ASSY PER AMM 33-51-06.
- [SDR SWAA2025121652036](https://openairdocs.org/sdr/SWAA2025121652036.md): Girt Bar · out of adjust · Dec 13, 2025 · N567WN · Boeing 7377CT · Emergency Equipment
  > FWD SERVICE DOOR GIRT HANGING LOW. SECURED THE GIRT BAR IAW AMM 25-66-01.
- [SDR SWAA2025051268286](https://openairdocs.org/sdr/SWAA2025051268286.md): Lamp · inoperative · May 7, 2025 · N567WN · Boeing 7377CT · Emergency Lighting
  > EMERGENCY LIGHT AT SEAT ROW 14ABC INOPERATIVE.<[01] REMOVED AND REPLACED EMERGENCY LIGHT LAMP AT SEAT ROW 14ABC. REF AMM 33-51-01. OPERATIONAL CHECK GOOD.
- [SDR SWAA2025051268285](https://openairdocs.org/sdr/SWAA2025051268285.md): Lamp · inoperative · May 7, 2025 · N567WN · Boeing 7377CT · Emergency Lighting
  > EMERGENCY LIGHT AT SEAT ROW 6DEF INOPERATIVE.<[01] REMOVED AND REPLACED EMERGENCY LIGHT LAMP AT SEAT ROW 6DEF. REF AMM 33-51-01. OPERATIONAL CHECK GOOD.
- [SDR SWAA2025031304356](https://openairdocs.org/sdr/SWAA2025031304356.md): Seat Back · out of adjust · Mar 12, 2025 · N567WN · Boeing 7377CT · Passenger Compartment Equipment
  > SEATS RECLINING AT EMERGENCY EXIT ROW 12D; 12F. ADJUSTED 12D; 12F SEAT RECLINE REF AMM 25-22-00
- [SDR SWAA2025021094370](https://openairdocs.org/sdr/SWAA2025021094370.md): Slide · out of position · Feb 9, 2025 · N567WN · Boeing 7377CT · Escape Slide
  > R2 DOOR ESCAPE SLIDE DRAGS ON THE FLOOR<[01]. PROPERLY INSTALLED R2 DOOR ESCAPE SLIDE IAW AMM 25-66-01-400-801;[02] VERIFIED CORRETIVE ACTION ENTRY 1.
- [SDR SWAA2025021093811](https://openairdocs.org/sdr/SWAA2025021093811.md): Battery Pack · no test · Feb 6, 2025 · N567WN · Boeing 7377CT · Emergency Lighting
  > EMERGENCY LIGHTS RELATED TO BATTERY PACK M2355 FAIL TEST<[01] REPLACED EMERGENCY BATTERY PACK M2335; PERFORMED GOOD EMEREGENCY LIGHT TEST PER AMM 33-51-06-960-805;[02] VERIFIED CORRECTIVE ACTION. CARD COMPLETE.
- [SDR SWAA2025021093812](https://openairdocs.org/sdr/SWAA2025021093812.md): Light · inoperative · Feb 6, 2025 · N567WN · Boeing 7377CT · Emergency Lighting
  > FWD ESCAPE EMEREGENCY LIGHT OUTSIDE FWD MAIN ENTRY DOOR INOP (L731)<[01] INSTALLED NEW LIGHT AT FWD ESCAPE EMEREGENCY OUTSIDE FWD MAIN ENTRY DOOR; PERFORMED GOOD TEST PER AMM 33-51-04-960-801.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
- [SDR SWAA2025021091146](https://openairdocs.org/sdr/SWAA2025021091146.md): Scuff Plate · missing · Jan 29, 2025 · N567WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > AFT AND FWD SCUFF PLATES (CORNERS) MISSING AT FWD CARGO BAY<[01] 01 - REMOVED AND REPLACED PER [AMM 53-11-02-420-801-NG (CARGO DOOR SCUFF PLATE - INSTALLATION - PERMANENT)];[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2025021088431](https://openairdocs.org/sdr/SWAA2025021088431.md): Floorbeam · cracked · Jan 22, 2025 · N567WN · Boeing 7377CT · Fuselage Main, Floor Beam
  > CRACKED PANEL BREAK BS 540 BL 0 - RBL 25 WL 207 (MARKED)<[01] REMOVED AND REPLACED PANEL BREAK AT BS540 BL0-RBL25 WL207 PER SRM 51-40-02 AND DWG:143A0060 REV:A;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2025021088432](https://openairdocs.org/sdr/SWAA2025021088432.md): Floorbeam · canning · Jan 22, 2025 · N567WN · Boeing 7377CT · Fuselage Main, Floor Beam
  > CRACKED PANEL BREAK BS 540 BL 0 - LBL 25 WL 207 (MARKED)<[01] REMOVED AND REPLACED PANEL BREAK AT BS540 BL0-LBL25 WL207 PER SRM 51-40-02 AND DWG:143A0060 REV:A;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2025021088206](https://openairdocs.org/sdr/SWAA2025021088206.md): Seat Track · corroded · Jan 21, 2025 · N567WN · Boeing 7377CT · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK LBL 24.75 BS500A+8; BS500A+11; BS500A+14.5; BS500A+17; BS500D+9.5; BS 520+5.5 TO BS520+11 WL 208 (MARKED)<[01] BS 480 TO BS 520 LBL25 SEAT TRACK WILL REPLACE DUE TO MECHANICAL DAMAGE ACCORDING TO CUST# TTG8Q00Y9C8F.<BR>UPON FURTHER INVE
- [SDR SWAA2025021088212](https://openairdocs.org/sdr/SWAA2025021088212.md): Seat Track · corroded · Jan 21, 2025 · N567WN · Boeing 7377CT · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK LBL 45.5 BS480+16.5; BS500A+5; BS500A+8; BS500B+16; BS500B+18.5; BS00D+9.5 WL 208 (MARKED)<[01] SEAT TRACK WILL REPLACE DUE TO MECHANICAL DAMAGE ACCORDING TO CUSTOMER # TTG8Q00Y9C43.;[02] VERIFIED ITEM 1
- [SDR SWAA2025021087806](https://openairdocs.org/sdr/SWAA2025021087806.md): Skin · cracked · Jan 20, 2025 · N567WN · Boeing 7377CT · Horizontal Stabilizer, Plate/Skin
  > CRACK ON RH LOWER HORIZONTAL STABILIZER SKIN AT STAB STA 193.90; 18.5' FROM FWD EDGE;.35' IN LENGTH (MARKED) <[01]. REPAIRED R/H HORIZONTAL STAB LOWER SKIN AT STAB STA 193.90 IAW SRM 55-10-01-2R-11 REPAIR 11.; [02] VERIFIED ACTION ITEMS AND TASK CARD COMPLETE
- [SDR SWAA2025021087557](https://openairdocs.org/sdr/SWAA2025021087557.md): Web · cracked · Jan 19, 2025 · N567WN · Boeing 7377CT · Wing Miscellaneous Structure
  > RIGHT WING T/E UPPER SURFACE PANEL AT ORSS 276; TRANSVERSE WEB IS CRACKED AT O/B UPPER FASTENER<[01] REMOVED R/W T/E UPPER SURFCE PANEL TRANSVERSE WEB AT ORSS 276 IAW SRM 51-40-02-OG-0 PARA. 4.;[02] VERIFIED ITEM 1
- [SDR SWAA2025021087563](https://openairdocs.org/sdr/SWAA2025021087563.md): Rib · cracked · Jan 19, 2025 · N567WN · Boeing 7377CT · Wing, Rib/Bulkhead
  > L-CLIP COMMON TO L/W I/B SIDE OF DEFLECTION CONTROL RIB AND UPPER SURFACE PANEL ORSS 271 IS CRACKED <[01]. REMOVED AND REPLACED L- CLIP COMMON TO L/W I/B SIDE OF DEFLECTION CONTROL RIB AND UPPER SURFACE PANEL AT ORSS 271 IAW SRM 51-40-02-0G-0 PARA. 4.;[02] VER
- [SDR SWAA2025021187233](https://openairdocs.org/sdr/SWAA2025021187233.md): Panel · debonded · Jan 18, 2025 · N567WN · Boeing 7377CT · Leading Edge Devices
  > RIGHT WING L/E PANEL 621HB HAS DISBOND AT I/B FWD CORNER<[01] 04 - REPAIRED PER [SRM 51-70-05-2R-6-A00737 (REPAIR 6 - REPAIR OF DAMAGE TO THE EDGEBAND OF A HONEYCOMB PANEL - AIRFRAME - PERMANENT)];[02] VERIFEID CORRECTIVE ACTION 1
- [SDR SWAA2025021087434](https://openairdocs.org/sdr/SWAA2025021087434.md): Rib · cracked · Jan 18, 2025 · N567WN · Boeing 7377CT · Horizontal Stabilizer, Spar/Rib
  > LEFT HORIZONTAL STAB REMOVABLE L/E 331B RIB #3 IS CRACKED<[01] 1. KENNETH RUDIO (TECHNICIAN); 24-JAN-2025 22:07 UTC<BR>REMOVED AND REPLACED L/H HORIZONTAL STAB. L/E #3 RIB IAW SRM 51-40-02-0G-0 PARA. 4.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREM
- [SDR SWAA2025021087435](https://openairdocs.org/sdr/SWAA2025021087435.md): Rib · cracked · Jan 18, 2025 · N567WN · Boeing 7377CT · Horizontal Stabilizer, Spar/Rib
  > LEFT HORIZONTAL STAB REMOVABLE L/E 331B RIB #5 IS CRACKED<[01] REMOVED AND REPLACED L/H HORIZONTAL STAB. L/E #5 RIB IAW SRM 51-40-02-0G-0 PARA. 4.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
- [SDR SWAA2025021087226](https://openairdocs.org/sdr/SWAA2025021087226.md): Floor Panel · pulled · Jan 18, 2025 · N567WN · Boeing 7377CT · Fuselage Floor Panel
  > FLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231XF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.
- [SDR SWAA2025021087227](https://openairdocs.org/sdr/SWAA2025021087227.md): Floor Panel · pulled · Jan 18, 2025 · N567WN · Boeing 7377CT · Fuselage Floor Panel
  > FLOOR PANEL 231YF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231YF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] ADDED PART INSTALL INFO.
- [SDR SWAA2025021087224](https://openairdocs.org/sdr/SWAA2025021087224.md): Floor Panel · pulled · Jan 18, 2025 · N567WN · Boeing 7377CT · Fuselage Floor Panel
  > FLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231ZF; WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] JOB COMPLETE.
- [SDR SWAA2025021087228](https://openairdocs.org/sdr/SWAA2025021087228.md): Floor Panel · pulled · Jan 18, 2025 · N567WN · Boeing 7377CT · Fuselage Floor Panel
  > FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241AF UPPER SKIN; WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] JOB COMPLETE.
- [SDR SWAA2025021087230](https://openairdocs.org/sdr/SWAA2025021087230.md): Floor Panel · pulled · Jan 18, 2025 · N567WN · Boeing 7377CT · Fuselage Floor Panel
  > FLOOR PANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242AF; UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] JOB COMPLETE.
- [SDR SWAA2025021087229](https://openairdocs.org/sdr/SWAA2025021087229.md): Floor Panel · pulled · Jan 18, 2025 · N567WN · Boeing 7377CT · Fuselage Floor Panel
  > PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 241DF 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 144A5810 ID:0128.;[02] JOB COMPLETE.
- [SDR SWAA2025021086864](https://openairdocs.org/sdr/SWAA2025021086864.md): Threshold · corroded · Jan 17, 2025 · N567WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > FWD CARGO SUBTHRESHOLD HAS CORROSION IN MULTIPLE AREAS<[01] UPON FURTHER INVESTIGATION; FOUND TO BE OUT OF LIMIT AS PER SRM 53-30-15-1A-1. REPAIR BY REPLACEMENT.;[02] UPDATED STEP 4;[03] UPDATED STEP 5;[04] REPLACED FWD CARGO BAY SUB THRESHOLD IAW SRM 51-40-02
- [SDR SWAA2025021086866](https://openairdocs.org/sdr/SWAA2025021086866.md): Pressure Deck · cracked · Jan 17, 2025 · N567WN · Boeing 7377CT · Fuselage Main, Structure
  > CRACK IN LH HORIZONTAL PRESSURE DECK BS 672 WL 202 LBL35. CRACK IS.650 INCHES IN LENGTH. MARKED IN RED INK.<[01] REPAIRED LH HORIZONTAL PRESSURE DECK WEB AT BS 663 TO BS 675 LBL 30 TO LBL 60 PER SRM 53-40-51-2R-2 REPAIR 2 FIG. 202.;[02] TASK CARD COMPLETED.;[
- [SDR SWAA2025021086867](https://openairdocs.org/sdr/SWAA2025021086867.md): Pressure Deck · cracked · Jan 17, 2025 · N567WN · Boeing 7377CT · Fuselage Main, Structure
  > CRACK IN RH HORIZONTAL PRESSURE DECK BS 664.5 WL 202 RBL 43. CRACK IS.250 INCHES LONG AND MARKED IN RED INK.<[01] REMOVED THE DAMAGE PART OF THE WEB AT BS 663.75 - 6BS75; RBL38 - 60; WL 202; PER SRM 53-40-51-2R-2 PAR. 4. C. FIG. 202.<BR><BR>INSTALLED REPAIR R
- [SDR SWAA2025021086862](https://openairdocs.org/sdr/SWAA2025021086862.md): Web · corroded · Jan 17, 2025 · N567WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > AFT CARGO SUBTHRESHOLD WEB HAVE CORROSION MULTIPLE AREAS.<[01] REMOVE AND REMPLACE AFT CARGO SUBTHRESHOLD WEB SRM 51-40-02 DWG 146A8340 ID:0024 REV: A;[02] REMOVED AND REMPLACED AFT CARGO SUBTHRESHOLD WEB BETWEEN BS 794 TO BS 847 PER SRM 51-40-02 DWG 146A8340
- [SDR SWAA2025021086863](https://openairdocs.org/sdr/SWAA2025021086863.md): Strap · corroded · Jan 17, 2025 · N567WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > AFT CARGO BAY TENSION STRAP HAS CORROSION APPROX BS802; RBL25.<[01] CORROSION ON TENSION STRAP AT ACB BS 806; RBL 25 IN L=2' X W=1' X D=0.030' FROM ORIGINAL THICKNESS 0.100' THEREFORE FOUND TO BE OUT OF LIMITS; TENSION STRAP WILL BE REPAIRED BY REPLACEMENT OF
- [SDR SWAA2025021086500](https://openairdocs.org/sdr/SWAA2025021086500.md): Scuff Plate · cracked · Jan 16, 2025 · N567WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > AFT CARGO FWD SCUFF PLATE IS CRACKED <[01]. WELDED THE CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 PARA 4.B.(4). REFERRED TO BAC 5975. EQUIPMENT USED; WELDING MACHINE I.D. 10583; CAL DATE 01/2025; APPLIED CHEMICAL CONVE
- [SDR SWAA2025021086861](https://openairdocs.org/sdr/SWAA2025021086861.md): Vapor Barrier · cracked · Jan 16, 2025 · N567WN · Boeing 7377CT · Wing Miscellaneous Structure
  > CRACKED VAPOR BARRIER IN THE MAIN WHEEL WELL BS663 LBL15 WL147. MARKED <[01]. CRACKED VAPOR BARRIER BS663 LBL15 WL147 WAS REPAIRED IAW SRM 51-70-04-2R-10;[02] VERIFIED CORRECTIVE ACTION.
- [SDR SWAA2025021086319](https://openairdocs.org/sdr/SWAA2025021086319.md): Doubler · damaged · Jan 15, 2025 · N567WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CUSTOMER REQUEST: DOUBLER AT BS 407 BETWEEN S-1 AND S-2L REQUIRES REMOVAL AND REPAIR DOUBLER AT BS 407 STR 1 - STR 2L/H <[01]. `THE DAMAGE WAS REPAIRED PER EA 25-153-00120. CONTINUED AIRWORTHINESS REQUIREMENTS ARE TRACKING ON EA 25-153-00120-DTI.' ENSURE THE
- [SDR SWAA2024102148684](https://openairdocs.org/sdr/SWAA2024102148684.md): Girt Bar · unsecure · Oct 15, 2024 · N567WN · Boeing 7377CT · Emergency Equipment
  > R1 DOOR SLIDE GIRT IS NOT SECURED WITH VELCRO<[01] RE-SECURED R1 DOOR SLIDE GIRT WITH VELCRO PER AMM 25-66-01.
- [SDR SWAA2024102148674](https://openairdocs.org/sdr/SWAA2024102148674.md): Bracket · cracked · Oct 15, 2024 · N567WN · Boeing 7377CT · Fuselage Main, Keel
  > KEEL BEAM ACCESS PANEL 192E FWD RH ATTACH HANGAR BRACKET IS CRACKED.<[01] REMOVED AND REPLACED KEEL BEAM ACCESS PANEL 192E FWD R/H ATTACH HANGER BRACKET PER SRM 51-40-02
- [SDR SWAA2024081926753](https://openairdocs.org/sdr/SWAA2024081926753.md): Battery Pack · inoperative · Aug 16, 2024 · N567WN · Boeing 7377CT · Emergency Lighting
  > LEFT OVERWING EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED LEFT OVERWING EMERGENCY LIGHTS PSU BATTERY PACK. TEST OK. REF AMM. 33-51-06.
- [SDR SWAA2024040470177](https://openairdocs.org/sdr/SWAA2024040470177.md): Sign · broken · Apr 3, 2024 · N567WN · Boeing 7377CT · Emergency Lighting
  > AFT CEILING EMERGENCY EXIT SIGN BROKEN<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-01-960-802-NG (EXIT SIGN - LIGHT ASSEMBLY REPLACEMENT - PERMANENT)]
- [SDR SWAA2023030810769](https://openairdocs.org/sdr/SWAA2023030810769.md): Handle · loose · Feb 28, 2023 · N567WN · Boeing 7377CT · Passenger/Crew Doors
  > PER CUSTOMER WALK- L-1 DOOR AFT ASSIST HANDLE LOOSE.<[01] SECURED L-1 DOOR AFT ASSIST HANDLE AS PER AMM 25-21-31-420-802;[02] VERIFIED 1.
- [SDR SWAA2023030810774](https://openairdocs.org/sdr/SWAA2023030810774.md): Fitting · loose · Feb 28, 2023 · N567WN · Boeing 7377CT · Escape Slide
  > CUSTOMER WALK - R-2 DOOR AFT GIRT BAR FLOOR FITTING LOOSE.<[01] RESECURED R 2 DOOR AFT GIRT BAR FLOOR FITTING AS PER REF B737AMM 25-66-01-000-804;[02] VERIFIED 1.
- [SDR SWAA2023030810503](https://openairdocs.org/sdr/SWAA2023030810503.md): Light · inoperative · Feb 27, 2023 · N567WN · Boeing 7377CT · Emergency Lighting
  > R2 DOOR EXTERIOR EMERGENCY LIGHT INOP.<[01] RECONNECTED R2 DOOR EXTERIOR EMERGENCY LIGHT AS PER REF B737 AMM 33-51-04-960-801. TEST OK.;[02] VERIFIED STEP#1
- [SDR SWAA2023030809602](https://openairdocs.org/sdr/SWAA2023030809602.md): Battery Pack · failed · Feb 23, 2023 · N567WN · Boeing 7377CT · Emergency Lighting
  > SEVERAL EMERGENCY LIGHTS FAILED OPERATIONAL TEST THROUGHOUT THE CABIN.<[01] REMOVED AND REPLACED AT LOCATIONS M1673; M1670 AND M1669 PERFORMED OPERATIONAL TEST NORMAL AS PER REF B737 AMM 33-51-06-960-805;[02] CORRECTION FOR STEP # 1 REMOVED AND REPLACED EMERGE
- [SDR SWAA2023030805304](https://openairdocs.org/sdr/SWAA2023030805304.md): Panel · cracked · Feb 21, 2023 · N567WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > LH HORIZONTAL STABILIZER PANEL 333AT TRACK ASSY FOUND CRACKED<[01] REMOVED PANEL 333AT AT LT HORIZONTAL STABILIZER FOR ACCESS TO DAMAGE IN AS PER B 737-700 SRM 51-40-02-0G-0;[02] REMOVED KEYWORD TRACK AT LT HORIZONTAL STABILIZER OF UPPER SIDE FOR DAMAGE IN AS
- [SDR SWAA2023030805302](https://openairdocs.org/sdr/SWAA2023030805302.md): Seat · cracked · Feb 16, 2023 · N567WN · Boeing 7377CT · Flight Compartment Equipment
  > COCKPIT 1ST OBS SEAT BOTTOM CRACKED ON RIGHT LWR SURFACE. 8-50<[01] REMOVED FLIGHT DECK 1ST OBS. SEAT AS PER B737 AMM 25-1102-000-801;[02] ACCOMPLISHED REPAIR DOUBLER TO 1ST OBSERVER SEAT AS PER EA-M-22-125-00561; WORK T/C: TTG8Q00HW8W5.;[03] VERIFIED AND INSP
- [SDR SWAA2023030802149](https://openairdocs.org/sdr/SWAA2023030802149.md): Battery · inoperative · Feb 11, 2023 · N567WN · Boeing 7377CT · Emergency Equipment
  > FWD LH WINDSCREEN: BATTERIES AT EMERGENCY FLASHLIGHTS DO NOT WORK (2 EACH)<[01] FLASHLIGHT BATTERIES AT FWD LH WINDSCREEN REMOVED AND REPLACED IAW CMM 25-60-02;[02] VERIFIED STEP 1.
- [SDR SWAA2023030802152](https://openairdocs.org/sdr/SWAA2023030802152.md): Battery · inoperative · Feb 11, 2023 · N567WN · Boeing 7377CT · Emergency Equipment
  > AFT LH WINDSCREEN: BATTERIES AT EMERGENCY FLASHLIGHTS DO NOT WORK (2 EACH)<[01] FLASHLIGHT BATTERIES AT AFT LH WINDSCREEN REMOVED AND REPLACED IAW CMM 25-60-02;[02] VERIFIED STEP 1.
- [SDR SWAA2023030800909](https://openairdocs.org/sdr/SWAA2023030800909.md): Track · corroded · Feb 8, 2023 · N567WN · Boeing 7377CT · Fuselage Internal Mounting Structure
  > F/O FWD I/B SEAT TRACK HAS CORROSION ON LWR SURFACE. 8-36<[01] RECEIVED PART; NEW TRACK INSTALLED ON TASK CARD TTG8Q001YDLC.;[02] VERIFIED 1;
- [SDR SWAA2023030800907](https://openairdocs.org/sdr/SWAA2023030800907.md): Track · corroded · Feb 8, 2023 · N567WN · Boeing 7377CT · Fuselage Internal Mounting Structure
  > CAPT. FWD O/B SEAT TRACK HAS CORROSION ON LWR SURFACE. 8-35<[01] RECEIVED PART; NEW TRACK INSTALLED ON TASK CARD TTG8Q001YDLC;[02] VERIFIED 1;
- [SDR SWAA2023030800908](https://openairdocs.org/sdr/SWAA2023030800908.md): Track · corroded · Feb 8, 2023 · N567WN · Boeing 7377CT · Fuselage Internal Mounting Structure
  > F/O FWD O/B SEAT TRACK HAS CORROSION ON LWR SURFACE. 8-34<[01] RECEIVED PART; NEW SEAT TRACK INSTALLED ON TASK CARD TTG8Q001YDLC.;[02] PARTS TRANS ACTION;[03] FINAL INSPECTION; RECEIVED NEW SEAT TRACK. WILL BE INSTALL ON TTG8Q001YDLC.

Next page: https://openairdocs.org/aircraft/N567WN/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 = 'N567WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N567WN/reports

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