# Service difficulty reports: N486WN

A list on [N486WN](https://openairdocs.org/aircraft/N486WN.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 7 · 328 reports

- [SDR SWAA2026101639244](https://openairdocs.org/sdr/SWAA2026101639244.md): Radome · cracked · Oct 12, 2026 · N486WN · Boeing 7377H4 · Aerodynamic Fairings
  > RADOME CRACKED AT 6 OCLOCK POSITION, R & R THE NOSE RADOME IAW AMM 53-52-00.
- [SDR SWAA2026101270866](https://openairdocs.org/sdr/SWAA2026101270866.md): Slide · unsecure · Oct 9, 2026 · N486WN · Boeing 7377H4 · Escape Slide
  > ESCAPE SLIDE PACK COVER LOOSE (AFT SERVICE DOOR) AFT SERVICE DOOR SLIDE UNSECURE. SECURED AFT SERVICE DOOR SLIDE IAW MT 725-61-06. ACFT OK FOR SERVICE.
- [SDR SWAA2026072770155](https://openairdocs.org/sdr/SWAA2026072770155.md): Stub Frame · cracked · Jul 7, 2026 · N486WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > BS 616 RH STUB BEAM STRAP 2EA LOWER FWD AND FWD-MIDDLE FASTENER HOLES WITH CRACKS IN AFT DIRECTION NOTED DURING OHEC INSP TTG8Q01BLV7Z STEP 19(C)1), AND 2). DISPLACED BS 616 R/H STUB BEAM TO FOM IAW SRM 51-40-02-0G-0 INSTALLED 100% PERMANENT FASTENERS (14) WIT
- [SDR SWAA2026072764870](https://openairdocs.org/sdr/SWAA2026072764870.md): Attach Angle · cracked · Jul 2, 2026 · N486WN · Boeing 7377H4 · Wing, Attach Fittings
  > LEFT WING TRAILING EDGE TRANSVERSE WEB ABOVE #1 PYLON AFT TIP O/B ATTACH ANGLE CRACKED. REMOVED AND REPLACED LEFT WING TRAILING EDGE TRANSVERSE WEB ABOVE #1 PYLON AFT TIP O/B ATTACH ANGLE IAW SRM 51-40-02. VERIFIED CORRECTIVE ACTION
- [SDR SWAA2026072272060](https://openairdocs.org/sdr/SWAA2026072272060.md): Plate · cracked · Jul 2, 2026 · N486WN · Boeing 7377H4 · Wing Main, Frame Structure
  > CRACKED WIGGLE PLATE ON RT WING AT RSS 240. REMOVED AND REPLACED WIGGLE PLATE ON RT WING AT RSS 240 IAW SRM 51-40-02-0G-0 AND AIPC 57-50-00-22.
- [SDR SWAA2026072723597](https://openairdocs.org/sdr/SWAA2026072723597.md): Stiffener · cracked · Jul 1, 2026 · N486WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > LH HORIZONTAL STABILIZER RIB 2, STAB STA 101.9, 1ST STIFFENER IS CRACKED AT LOWER END. REPAIRED THE LT HORIZONTAL STAB RIB, 1ST STIFFENER AT LOWER END IAW SRM 55-10-09-2R-5.
- [SDR SWAA2026072206805](https://openairdocs.org/sdr/SWAA2026072206805.md): Plate · cracked · Jul 1, 2026 · N486WN · Boeing 7377H4 · Wing Main, Frame Structure
  > CRACKED WIGGLE PLATE ON RT WING UNDER PANEL 651EB AT RSS 226. REMOVED AND REPLACED WIGGLE PLATE IAW SRM 51-40-02-0G-0, AND AIPC 57-50-00-22.
- [SDR SWAA2026072205274](https://openairdocs.org/sdr/SWAA2026072205274.md): Seat Track · corroded · Jul 1, 2026 · N486WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > PASSENGER CABIN SEAT TRACK LBL 25 CORRODED, BS 727B+3 ON TOP, BS 727E+4 ON TOP, BS 827 ON TOP, WL 208, SRM 53-00-52-1A-1 IS APPLICABLE ALLOWABLE DAMAGE. REMOVED CORROSION ON CABIN SEAT TRACK LBL 25 AT BS 727B + 3 IAW SRM 51-10-02-0G-0, AREA BLENDED IS L2'
- [SDR SWAA2026072258105](https://openairdocs.org/sdr/SWAA2026072258105.md): Scuff Plate · cracked · Jul 1, 2026 · N486WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED. AFT CARGO BAY AFT SCUFF PLATE REPAIRED IAW SRM 53-60-15-2R-1.
- [SDR SWAA2026072202304](https://openairdocs.org/sdr/SWAA2026072202304.md): Stiffener · cracked · Jul 1, 2026 · N486WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > RT HORIZONTAL STAB RIB 5 (STAB STA 129.5) 2ND STIFFENER HAS DENT WITH CRACK IN MIDDLE OF STIFFENER. REPAIRED PER SRM 55-10-09-2R-5 AND EA 26-155-01893.
- [SDR SWAA2026072283613](https://openairdocs.org/sdr/SWAA2026072283613.md): Stiffener · cracked · Jul 1, 2026 · N486WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > RIGHT HORIZONTAL STAB RIB 5 (STAB STA 129.5) 3RD STIFFENER HAS DENT WITH CRACK IN MIDDLE OF STIFFENER. REFER TO FAULT TTG8Q01CZG6D WHERE EA 26-155-01893 WAS ADDED AS A SUBTASK.
- [SDR SWAA2026072211040](https://openairdocs.org/sdr/SWAA2026072211040.md): Scuff Plate · cracked · Jun 29, 2026 · N486WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD SERVICE DOOR SCUFFPLATE IS CRACKED. COMPLETED STEP 8. REMOVED FSD SCUFF PLATE IAW AMM 53-11-01-000-801. WELDED IAW SRM 53-10-15-2R-2 STEP 4.B.(3). REFERRED TO SOPM 20-30-03. PT INSPECTED WELDED AREA IAW SOPM 20-20-02. NO CRACKS NOTED. REINSTALLED SCUFF
- [SDR SWAA2026033083345](https://openairdocs.org/sdr/SWAA2026033083345.md): Battery Pack · inoperative · Mar 25, 2026 · N486WN · Boeing 7377H4 · Emergency Lighting
  > RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE REMOVED AND REPLACED THE RT OVERWING BATTERY PACK IAW AMM 33-51-06-960-805.
- [SDR SWAA2026033077860](https://openairdocs.org/sdr/SWAA2026033077860.md): Stringer · cracked · Mar 8, 2026 · N486WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > BS 1016 AFT PRESSURE BULKHEAD, STRINGER 13R CRACKED AT RBL 3.45. REPAIRED IAW EA 26-153-00643.
- [SDR SWAA2026033076808](https://openairdocs.org/sdr/SWAA2026033076808.md): Pressure Blkhd · cracked · Mar 4, 2026 · N486WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD HAD A CRACK INDICATION, EMANATING FROM RIVET AT STRINGER 7R LOWER GROUP OF FIVE, CLOSEST TO APEX. APPROX. 1/8' LONG. REJECTED STEP 43 FOR EDGE MARGIN IS OUT OF LIMITS OF -1 FILLER AND -2 FILLER. REFABRICATED -1 AND -2 REPAIR PARTS TO M
- [SDR SWAA2026033075818](https://openairdocs.org/sdr/SWAA2026033075818.md): Pressure Blkhd · cracked · Mar 3, 2026 · N486WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD HAD A CRACK INDICATION EMANATING FROM RIVET AT STRINGER 7R LOWER GROUP OF FIVE CLOSEST TO APEX. APPROX. 1/8' LONG. IAW PART 6, 51-00-00, PROCEDURE 23.
- [SDR SWAA2026021068627](https://openairdocs.org/sdr/SWAA2026021068627.md): Sign · wrong part · Feb 7, 2026 · N486WN · Boeing 7377H4 · Emergency Lighting
  > PSU`S 9ABC, 14ABC, 14DEF, AND 15DEF LIGHT ILLUMINATION TO AFT CABIN EXIT SIGN IAW DWG DG307-142007C.
- [SDR SWAA2026011660914](https://openairdocs.org/sdr/SWAA2026011660914.md): Flashlight · inoperative · Jan 13, 2026 · N486WN · Boeing 7377H4 · Emergency Equipment
  > FWD LOWER F/A FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED IAW AMM 25-64-00-SWA-807-NG-01.
- [SDR SWAA2025082206124](https://openairdocs.org/sdr/SWAA2025082206124.md): Slide · out of position · Aug 20, 2025 · N486WN · Boeing 7377H4 · Escape Slide
  > L1 DOOR SLIDE HANGS TOO LOW. RESECURED CABIN L1 DOOR SLIDE GIRT BAR IAW AMM 25-66-01.
- [SDR SWAA2024120473111](https://openairdocs.org/sdr/SWAA2024120473111.md): Idg · slow · Dec 1, 2024 · N486WN · Boeing 7377H4 · Alternator-Generator Drive
  > N1 & N2 SLOW TO REDUCE BELOW 45% N1 WHEN RETARDING THRUST LEVER. TAKES APPROX 30 SECS TO REDUCE TO IDLE. ( #1 ENGINE)<[01] R&R #1 ENG IDG PER [AMM 24-11-11-401-NG (INTEGRATED DRIVE GENERATOR (IDG) - REMOVAL/INSTALLATION - PERMANENT)]. NO HELP.;[02] R&R #1 ENG
- [SDR SWAA2024120473951](https://openairdocs.org/sdr/SWAA2024120473951.md): Hmu · slow · Dec 1, 2024 · N486WN · Boeing 7377H4 · Alternator-Generator Drive
  > N1 & N2 SLOW TO REDUCE BELOW 45% N1 WHEN RETARDING THRUST LEVER. TAKES APPROX 30 SECS TO REDUCE TO IDLE. ( #1 ENGINE)<[01] R&R #1 ENG IDG PER [AMM 24-11-11-401-NG (INTEGRATED DRIVE GENERATOR (IDG) - REMOVAL/INSTALLATION - PERMANENT)]. NO HELP.;[02] R&R #1 ENG
- [SDR SWAA2024120473952](https://openairdocs.org/sdr/SWAA2024120473952.md): Pump · slow · Dec 1, 2024 · N486WN · Boeing 7377H4 · Alternator-Generator Drive
  > N1 & N2 SLOW TO REDUCE BELOW 45% N1 WHEN RETARDING THRUST LEVER. TAKES APPROX 30 SECS TO REDUCE TO IDLE. ( #1 ENGINE)<[01] R&R #1 ENG IDG PER [AMM 24-11-11-401-NG (INTEGRATED DRIVE GENERATOR (IDG) - REMOVAL/INSTALLATION - PERMANENT)]. NO HELP.;[02] R&R #1 ENG
- [SDR SWAA2024111960633](https://openairdocs.org/sdr/SWAA2024111960633.md): Flashlight · inoperative · Nov 16, 2024 · N486WN · Boeing 7377H4 · Emergency Equipment
  > FA FORWARD; EMERGENCY FLASHLIGHT INOP<[01] INSPECTED PER AMM 25-64-00. NO DEFECTS FOUND. OPS CK NORMAL.
- [SDR SWAA2024101748468](https://openairdocs.org/sdr/SWAA2024101748468.md): Cover · damaged · Oct 14, 2024 · N486WN · Boeing 7377H4 · Escape Slide
  > FWD RIGHT EMERGENCY EXIT SLIDE COVER HAS VERY SHARP CORNER RIGHT SIDE<[01] SMOOTHED CORNER PER AMM 25-00-00
- [SDR SWAA2024090433238](https://openairdocs.org/sdr/SWAA2024090433238.md): Sign · broken · Sep 1, 2024 · N486WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT SIGN IN 12 F BROKEN. R & R EMERGENCY EXIT SIGN IN ROW 12F PER MM 33-51-01
- [SDR SWAA2024081425275](https://openairdocs.org/sdr/SWAA2024081425275.md): Slide · out of adjust · Aug 13, 2024 · N486WN · Boeing 7377H4 · Escape Slide
  > C/R. L2 DOOR SLIDE HITS THRESHOLD<[01] THIS ITEM WAS ACCOMPLISHED ON MT 725-61-06.;[02] VERIFIED STEP:1
- [SDR SWAA2024081425280](https://openairdocs.org/sdr/SWAA2024081425280.md): Slide · out of adjust · Aug 13, 2024 · N486WN · Boeing 7377H4 · Escape Slide
  > C/R. R2 DOOR SLIDE HITS THRESHOLD.<[01] THIS ITEM WAS ACCOMPLISHED ON MT 725-61-06.;[02] VERIFIED STEP:1
- [SDR SWAA2024081914305](https://openairdocs.org/sdr/SWAA2024081914305.md): Panel · cracked · Jul 19, 2024 · N486WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STABILIZER - LWR T/E MID BALANCE PANEL CRACKED AT I/B HINGE TIP.<[01] REMOVED AND REPLACED LEFT HORIZONTAL STABILIZER MID BALANCE PANEL PER AMM 27-31-41-401-NG AND ACCOMPLISHED BALANCE PANEL TEST.<BR>TORQUE WRENCH B/C 14066 CAL DUE DATE 07/11/2
- [SDR SWAA2024081914307](https://openairdocs.org/sdr/SWAA2024081914307.md): Skin · cracked · Jul 19, 2024 · N486WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND AT DENT. CRACK LENGTH: 0.15' CRACK FOUND AT DENT ON L/H HORIZONTAL STABILIZER L/E SKIN L/E STA 254.02+7.5'. CRACK LENGTH: 0.15'<[01] RECEIVED NEW L/H HORIZONTAL STABILIZER L/E PANEL (MPN#186A1001-15; PO#2074280). PART TO BE INSTALLED ON TTG8Q001T
- [SDR SWAA2024081514304](https://openairdocs.org/sdr/SWAA2024081514304.md): Handle · worn · Jul 19, 2024 · N486WN · Boeing 7377H4 · Passenger/Crew Doors
  > L1 DOOR INTERIOR HANDLE MECHANISM CONTROL CAM WORN AT TRACK..<[01] REMOVED AND REPLACED L1 DOOR INTERIOR HANDLE MECHANISM CONTROL CAM PER REF CMM 52-16-12.;[02] VERIFIED AND INSPECTED STEP#1.
- [SDR SWAA2024081412099](https://openairdocs.org/sdr/SWAA2024081412099.md): Support · corroded · Jul 13, 2024 · N486WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SPOTS ON AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT ZEE RAIL B.S. 727+11' - B.S. 807 LBL. 21' W.L. 156.<[01] (FINAL) REMOVED; LOCATED/DRILLED AND INSTALLED NEW L/H ZEE CHANNEL PER B737-700 SRM 51-40-02-0G-0 AND DWG# 146A7500.;[02] (CORRECTION ST
- [SDR SWAA2024081412100](https://openairdocs.org/sdr/SWAA2024081412100.md): Support · corroded · Jul 13, 2024 · N486WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > COROSION SPOTS ON AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT ZEE RAIL B.S. 727+15' -B.S. 767 RBL. 21' W.L. 156.<[01] (FINAL) REMOVED; LOCATED/DRILLED AND INSTALLED NEW R/H FWD Z CHANNEL AT AFT CARGO COMPARTMENT PER B737-700 SRM 51-40-02-0G-0; SRM 51-40-05
- [SDR SWAA2024081411842](https://openairdocs.org/sdr/SWAA2024081411842.md): Intercostal · cracked · Jul 12, 2024 · N486WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACKED AT STR15L STA.294.5<[01] JOB WAS ACCOMPLISHED ON EA 24-153-02000 FAULT # TTG8Q00USB2D;[02] VERIFIED STEP 1
- [SDR SWAA2024081911322](https://openairdocs.org/sdr/SWAA2024081911322.md): Nut Plate · corroded · Jul 11, 2024 · N486WN · Boeing 7377H4 · Horizontal Stabilizer Structure
  > LEFT HORIZONTAL STAB. REAR SPAR AT ELEVATOR RIB STA 121.59 SUPPORT STRUCTURE WITH ONE CORRODED NUTPLATE.<[01] REMOVED AND REPLACED NUTPLATE FROM LEFT HORIZONTAL STABILIZER REAR SPAR AT ELEVATOR RIB STA 121.59 SUPPORT STRUCTURE PER B737-700 SRM 51-40-02-0G-0.;[
- [SDR SWAA2024081510545](https://openairdocs.org/sdr/SWAA2024081510545.md): Handle · out of adjust · Jul 9, 2024 · N486WN · Boeing 7377H4 · Passenger/Crew Doors
  > L1 DOOR INTERIOR HANDLE MECHANISM CONTROL CAM HAS EXCESSIVE PLAY.<[01] L1 DOOR INTERIOR HANDLE MECHANISM CONTROL CAM WITH PLAY WILL BE ACCOMPLISHED ON T/C TTG8Q00UPBW9.;[02] VERIFIED STEP#1.
- [SDR SWAA2024081510773](https://openairdocs.org/sdr/SWAA2024081510773.md): Scuff Plate · cracked · Jul 9, 2024 · N486WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO FWD SCUFF PLATE CRACKED<[01] RECEIVED SERVICEABLE AFT CARGO COMPARTMENT FWD SCUFF PLATE (146A8341-7; PO#2043476). PART TO BE INSTALLED ON TTG8Q001TL82.;[02] VERIFIED STEP # 1
- [SDR SWAA2024081610345](https://openairdocs.org/sdr/SWAA2024081610345.md): Drain · corroded · Jul 8, 2024 · N486WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > WATER DRAIN AT FUSELAGE BELLY HAS CORROSION AROUND IT; BETWEEN STA 967 AND STA 986.5<[01] JOB WAS ACCOMPLISHED ON FAULT TTG8Q00UDWRD;[02] VERIFIED STEP 1
- [SDR SWAA2024081610341](https://openairdocs.org/sdr/SWAA2024081610341.md): Bracket · cracked · Jul 8, 2024 · N486WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > KEEL BEAM UNDER PANEL #192E HAS TWO BROKEN BRACKETS<[01] REMOVED AND REPLACED PANEL SUPPORT BRACKETS 2E/A AT KEEL BEAM FWD AREA STA 546.26 IN REF B737-700 SRM 51-40-02-0G-0.;[02] CORRECTION: REMOVED AND REPLACED PANEL SUPPORT BRACKETS 2E/A AT KEEL BEAM FWD ARE
- [SDR SWAA2024081610343](https://openairdocs.org/sdr/SWAA2024081610343.md): Skin · damaged · Jul 8, 2024 · N486WN · Boeing 7377H4 · Wing, Plate/Skin
  > L/W L/E LWR SURFACE HAS ELONGATED HOLE I/B OF SLAT #3 ANTI ICE T DUCT<[01] APPLIED REPAIR ON L/W L/E LWR SURFACE AT ELONGATED HOLE I/B OF SLAT #3 PER B737 SRM 51-70-04-2R-9 TOOL USED TEMPERATURE CONTROLLER ID:160354 CALIBRATION DUE 03-07-25 MATERIAL USED PO#14
- [SDR SWAA2024081410533](https://openairdocs.org/sdr/SWAA2024081410533.md): Doubler · cracked · Jul 8, 2024 · N486WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND AT RT SIDE HORIZONTAL STABILIZER LOWER SKIN STAB STA 193.90 I/B OF RIB I/B ROW; 17' FROM T/E. CRACK LENGTH 1' APPROX. CRACK FOUND AT RT SIDE HORIZONTAL STABILIZER LOWER SKIN STAB STA 193.90 I/B OF RIB I/B ROW 17' FROM T/E. CRACK LENGTH 1' APPROX.<[
- [SDR SWAA2024081310104](https://openairdocs.org/sdr/SWAA2024081310104.md): Floor Panel · delaminated · Jul 7, 2024 · N486WN · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL #231ZF DELAMINATED<[01] RECEIVED FLOOR PANEL 231ZF (P# 144A5810-160) PANEL WILL BE CLOSED ON TTG8Q00U34ZE.;[02] VERIFIED STEP#1.
- [SDR SWAA2024081516410](https://openairdocs.org/sdr/SWAA2024081516410.md): Doubler · cracked · Jul 6, 2024 · N486WN · Boeing 7377H4 · Service Doors
  > EXT PWR RECEPTACLE SKIN CRACKED<[01] REMOVED AND REPLACED EGPR DOUBLER AT R/H FUSELAGE SKIN REF B737-700 SRM 51-40-02-0G-0 AND DWG# 141A3702.;[02] VERIFIED STEP 1
- [SDR SWAA2023101108887](https://openairdocs.org/sdr/SWAA2023101108887.md): Light · inoperative · Oct 7, 2023 · N486WN · Boeing 7377H4 · Emergency Lighting
  > FWD SERVICE DOOR OUTSIDE EMERGENCY LIGHT IS INOP.<[01] RELAMPED FWD SERVICE DOOR SLIDE EMERGENCY LIGHT IAW AMM 33-51-04. OPS CK GOOD.
- [SDR SWAA2023071878624](https://openairdocs.org/sdr/SWAA2023071878624.md): Girt Bar · out of adjust · Jul 14, 2023 · N486WN · Boeing 7377H4 · Emergency Equipment
  > FORWARD SERVICE DOOR GIRT BAR BRACKET (RIGHT) LOOSE<[01] SECURE GIRT BAR BRACKET I.A.W. 25-66-00 OPS CHECK GOOD
- [SDR SWAA2023050129427](https://openairdocs.org/sdr/SWAA2023050129427.md): Battery Pack · inoperative · Apr 19, 2023 · N486WN · Boeing 7377H4 · Emergency Lighting
  > FWD L/H EMERGENCY LIGHT BATTERY M1675 WILL NOT HOLD CHARGE<[01] REMOVED BATTERY PACK AT M1675 IAW AMM 33-51-06-960-805 STEP 4.E.(1) UP TO (4).;[02] OK TO INSTALL BATTERY PACK AT M1675;[03] INSTALLED NEW BATTERY PACK AT M1675 IAW AMM 33-51-06-960-805 STEP 4E.(5
- [SDR SWAA2022111670386](https://openairdocs.org/sdr/SWAA2022111670386.md): Attach Angle · cracked · Nov 12, 2022 · N486WN · Boeing 7377H4 · Wing, Attach Fittings
  > RT WING; FWD ATTACH ANGLE CRACKED FOR PANEL 651AT ATTACH CHANEL RT WING FWD ATTACH ANGLE CRACKED FOR PANEL 651AT ATTACH CHANEL / [01] REMOVED AND REPLACED ANGLE BRACKET IAW SRM 51-40-04
- [SDR SWAA2022101057500](https://openairdocs.org/sdr/SWAA2022101057500.md): Power Supply · popped · Oct 7, 2022 · N486WN · Boeing 7377H4 · Emergency Lighting
  > DURING PREFLIGHT FOUND C/B POPPED P18-3A10 CB; PASSENGER EMER CHGR L AFT / [01] R/R 2EA AFT AND 2EA LEFT POWER SUPPLY AND BATRY PACK IAW AMM 33-51-06
- [SDR SWAA2022101058190](https://openairdocs.org/sdr/SWAA2022101058190.md): Battery Pack · popped · Oct 7, 2022 · N486WN · Boeing 7377H4 · Emergency Lighting
  > DURING PREFLIGHT FOUND C/B POPPED P18-3A10 CB; PASSENGER EMER CHGR L AFT / [01] R/R 2EA AFT AND 2EA LEFT POWER SUPPLY AND BATRY PACK IAW AMM 33-51-06
- [SDR SWAA2022091974499](https://openairdocs.org/sdr/SWAA2022091974499.md): Hook · loose · Sep 15, 2022 · N486WN · Boeing 7377H4 · Escape Slide
  > R1 GALLEY GIRT BAR HOLDER LOOSE / [01] ADJUSTED HOOKS PER SIP.OPS NORMAL.
- [SDR SWAA2022082946517](https://openairdocs.org/sdr/SWAA2022082946517.md): Bracket · bent · Aug 26, 2022 · N486WN · Boeing 7377H4 · Escape Slide
  > GIRT BAR BRACKET BENT ON FWD SERVICE DOOR / [01] INSPECTED AND PERFORMED OPS CK OF FWD SERVICE GIRT BAR BRACKET PER AMM 25-66-00. NO DEFECTS NOTED.

Next page: https://openairdocs.org/aircraft/N486WN/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 = 'N486WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N486WN/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.