# Service difficulty reports: N286WN

A list on [N286WN](https://openairdocs.org/aircraft/N286WN.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 · 295 reports

- [SDR SWAA2026092188951](https://openairdocs.org/sdr/SWAA2026092188951.md): Light · broken · Sep 15, 2026 · N286WN · Boeing 7377H4 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHT ASSEMBLY FOR AISLE BROKEN REPLACED OVERHEAD EMERGENCY LIGHT ASSEMBLY IAW AMM 33-51-01. OPS CHKD GOOD.
- [SDR SWAA2026061004193](https://openairdocs.org/sdr/SWAA2026061004193.md): Skin · corroded · May 18, 2026 · N286WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON LOWER FUSELAGE SKIN AT BS 400+6'- 400+15' BTW STR 27L- 26L. IAW EA 26-153-01372; THE REWORK IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITH AN INSPECTION THRESHOLD DEFINED IN EA 26-153-01372-DTI.
- [SDR SWAA2026061003731](https://openairdocs.org/sdr/SWAA2026061003731.md): Scuff Plate · cracked · May 17, 2026 · N286WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO AFT CORNER SCUFF PLATE CRACKED. REMOVED AND REPLACED CRACKED SCUFF PLATE IAW AMM 53-11-02-020-801 AND AMM 53-11-02-420-801.
- [SDR SWAA2026061003734](https://openairdocs.org/sdr/SWAA2026061003734.md): Fairing · corroded · May 17, 2026 · N286WN · Boeing 7377H4 · Aerodynamic Fairings
  > CORROSION FOUND ON LOWER FUSELAGE AT BS 440+14, STRINGER 26L; NEAR LOW RANGE RADIO ALTIMETER ANTENNA AREA. REPLACED (FAIRING ASSY; NUT PLATE ASSEMBLIES; COVER PLATE) IAW AMM 34-33-11 AND DWG 143A3230, REV A.
- [SDR SWAA2026061003735](https://openairdocs.org/sdr/SWAA2026061003735.md): Fairing · corroded · May 17, 2026 · N286WN · Boeing 7377H4 · Aerodynamic Fairings
  > CORROSION FOUND ON LOWER FUSELAGE AT STA 400+7, STRINGER 26L; NEAR LOW RANGE RADIO ALTIMETER ANTENNA AREA. REPLACED THE FAIRING ASSY; NUT PLATE ASSEMBLIES; COVER PLATE IAW AMM 34-33-11 AND DWG 143A3230, REV A.
- [SDR SWAA2026060303736](https://openairdocs.org/sdr/SWAA2026060303736.md): Skin · corroded · May 17, 2026 · N286WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON LOWER FUSELAGE SKIN AT STA 440+6 IN; BETWEEN STRINGERS 26L AND 27L; NEAR LOW RANGE RADIO ALTIMETER ANTENNA AREA (MARKED)<[01] AS PER EA 26-153-01399; THE REPAIR IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITH AN INSPECTION THRESHOLD DE
- [SDR SWAA2026060303725](https://openairdocs.org/sdr/SWAA2026060303725.md): Attach Angle · cracked · May 16, 2026 · N286WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > LH 663 VAPOR BARRIER UPPER ATTACH ANGLE CRACKED LBL 11. REMOVED FASTENERS AS REQUIRED COMMON TO REPAIR BSTA. 663 UPPER ATTACH ANGLE LEFT SIDE; VAPOR BARRIER PER SRM 51-40-02-0G-0;[02] ALL STEPS C/W. REPAIRED LH 663 VAPOR BARRIER UPPER ATTACH ANGLE LBL 11 PE
- [SDR SWAA2026040786179](https://openairdocs.org/sdr/SWAA2026040786179.md): Floorboard · cracked · Apr 3, 2026 · N286WN · Boeing 7377H4 · Fuselage Floor Panel
  > CREW REPORTS FWD CARGO METAL FLOORBOARD CRACKED. OK TO CONTINUE PER MEL 25-16-01 SP1B. R &R FWD CENTER. FLOORBOARD IAW AMM 25-52-10.
- [SDR SWAA2026030976578](https://openairdocs.org/sdr/SWAA2026030976578.md): Scuff Plate · cracked · Mar 4, 2026 · N286WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK MEASURING 0.5 IN. ON DENT MEASURING L=0.625; W=0.5; D=0.054, ON THE FWD CARGO SCUFF PLATE. R & R THE SCUFF PLATE IAW AMM 53-11-01, & 53-11-02,
- [SDR SWAA2025110330548](https://openairdocs.org/sdr/SWAA2025110330548.md): Ring · engaged · Oct 31, 2025 · N286WN · Boeing 7377H4 · Emergency Equipment
  > GIRT BAR FORWARD SERVICE DOOR LOOSE. INSTALLED GIRT BAR STOP RELEASE RING IAW AMM 25-66-01. OPS CHECKED GOOD.
- [SDR SWAA2025101523864](https://openairdocs.org/sdr/SWAA2025101523864.md): Lamp · inoperative · Oct 12, 2025 · N286WN · Boeing 7377H4 · Emergency Lighting
  > LEFT OVERWING EXIT SIGN SIDEWALL LIGHT INOPERATIVE. R & R LEFT OVERWING EXIT SIGN LAMP IAW AMM 33-51-04. OPS CHECKED GOOD.
- [SDR SWAA2025042126532](https://openairdocs.org/sdr/SWAA2025042126532.md): Elec Connector · dirty · Apr 20, 2025 · N286WN · Boeing 7377H4 · Flight Control System Wiring
  > WITH LAP LEVER TO 25; FLAP INDICATOR SHOWED SPLIT FLAP CONDITION WITH 1 NEEDLE AT 0 AND THE OTHER AT.5. RAN QRH FOR TRAILING EDGE FLAP ASYMMETRY. FLAPS OPERATED APPROX. 5-6 TIMES NO NEEDLE SPLIT NO FAULTS...WRITING A TIZZY FOR FIRST LEG TO MX TO REPLACE THE #
- [SDR SWAA2025010382230](https://openairdocs.org/sdr/SWAA2025010382230.md): Slide · loose · Jan 1, 2025 · N286WN · Boeing 7377H4 · Escape Slide
  > CREW REPORTS ANTS LH ESCAPE SLIDE HARDWARE LOOSE<[01] VERIFIED HARDWARE SECURE PER AMM 25-66-01
- [SDR SWAA2024070908947](https://openairdocs.org/sdr/SWAA2024070908947.md): Slide · out of adjust · Jul 4, 2024 · N286WN · Boeing 7377H4 · Escape Slide
  > CUSTOMER WALK - L2 DOOR SLIDE SKIRT HITS THRESHOLD WHEN CLOSING<[01] READJUSTED THE GIRT Z-FOLD ON L2 DOOR SLIDE REF 'TASK CARD '725-61-06 (REM/INST - SLIDE REMOVAL AND INSTALLATION) [TTG8Q00UDDC3]' FOR WORK ACCOMPLISHED.;[02] VERIFIED STEP 1<BR>AUDIT C/W REF
- [SDR SWAA2024070908953](https://openairdocs.org/sdr/SWAA2024070908953.md): Slide · out of adjust · Jul 4, 2024 · N286WN · Boeing 7377H4 · Escape Slide
  > CUSTOMER WALK - R2 DOOR SLIDE SKIRT HITS THRESHOLD WHEN CLOSING<[01] REFER TO TASK CARD '725-61-06 (REM/INST - SLIDE REMOVAL AND INSTALLATION) [TTG8Q00UDCAY]' FOR WORK ACCOMPLISHED.;[02] CORRECTION STEP 1. READJUSTED THE GIRT Z-FOLD ON R2 DOOR SLIDE REF TASK C
- [SDR SWAA2024070908946](https://openairdocs.org/sdr/SWAA2024070908946.md): Bulb · burned out · Jul 4, 2024 · N286WN · Boeing 7377H4 · Emergency Lighting
  > CUSTOMER WALK - SEVERAL BULBS BURNT OUT ON EMER EXIT SIGN ON AFT GALLEY OUTBD SIDE<[01] RELAMPED BULBS ON EMER EXIT SIGN ON AFT GALLEY OUTBD SIDE AS PER B737 AMM 33-51-01-960-801. OPERATIONAL TEST PASSED.;[02] VERIFIED STEP 1.
- [SDR SWAA2024070906475](https://openairdocs.org/sdr/SWAA2024070906475.md): Fuse · inoperative · Jun 27, 2024 · N286WN · Boeing 7377H4 · Emergency Lighting
  > MULTIPLE PAX EMERGENCY LIGHTS INOP<[01] REPLACED FUSES ON BATTERY PACK M1669 I/A/W B737 AMM 33-51-06-960-804. OPS CHECK PASSED.;[02] VERIFIED STEP 1.
- [SDR SWAA2024070903575](https://openairdocs.org/sdr/SWAA2024070903575.md): Seat Track · corroded · Jun 19, 2024 · N286WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > FLIGHT DECK FIRST OFFICER FWD SEAT TRACK I/B HAS CORROSION.<[01] RECEIVED SERVICEABLE TRACK FOR FIRST OFFICER FWD SEAT TRACK I/B. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD '753-330-00-01Y (INSTALL FLIGHT COMPARTMENT COMPONENTS) [TTG8Q003DFWN]' STEP 12;[02
- [SDR SWAA2024070903576](https://openairdocs.org/sdr/SWAA2024070903576.md): Seat Track · corroded · Jun 19, 2024 · N286WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > FLIGHT DECK FIRST OFFICER FWD SEAT TRACK O/B HAS CORROSION.<[01] RECEIVED SERVICEABLE TRACK FOR FIRST OFFICER FWD SEAT TRACK O/B. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD '753-330-00-01Y (INSTALL FLIGHT COMPARTMENT COMPONENTS) [TTG8Q003DFWN]' STEP 12;[02
- [SDR SWAA2024070903577](https://openairdocs.org/sdr/SWAA2024070903577.md): Seat Track · corroded · Jun 19, 2024 · N286WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > FLIGHT DECK CAPTAIN FWD SEAT TRACK I/B HAS CORROSION.<[01] RECEIVED SERVICEABLE TRACK FOR CAPTAIN FWD SEAT TRACK I/B. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD '753-330-00-01Y (INSTALL FLIGHT COMPARTMENT COMPONENTS) [TTG8Q003DFWN]' STEP 12;[02] VERIFIED S
- [SDR SWAA2024070903574](https://openairdocs.org/sdr/SWAA2024070903574.md): Seat Track · corroded · Jun 19, 2024 · N286WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > FLIGHT DECK CAPTAIN FWD SEAT TRACK O/B HAS CORROSION.<[01] RECEIVED SERVICEABLE TRACK FOR CAPTAIN FWD SEAT TRACK O/B. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD '753-330-00-01Y (INSTALL FLIGHT COMPARTMENT COMPONENTS) [TTG8Q003DFWN]' STEP 12;[02] VERIFIED S
- [SDR SWAA2024070900662](https://openairdocs.org/sdr/SWAA2024070900662.md): Web · cracked · Jun 12, 2024 · N286WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK FOUND AT UNDERLYING STRUCTURE OF EXISTING FLIGHT DECK FLOOR WEB AT STA 260; RBL 4 ADJACENT TO PRODUCTION FASTENER HOLE. CRACK FOUND AT UNDERLYING STRUCTURE OF EXISTING FLIGHT DECK FLOOR WEB REPAIR. ESR #9349<[01] ACCOMPLISHED EA 24-153-01612;[02] VERIFIE
- [SDR SWAA2024070999343](https://openairdocs.org/sdr/SWAA2024070999343.md): Floor Panel · cracked · Jun 8, 2024 · N286WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL BREAK ASSEMBLY AT STA 540 FROM BL 0 TO LBL 24.75 FOUND CRACKED.<[01] WORK ACCOMPLISHED ON FAULT #TTG8Q00TSRFU;[02] VERIFIED STEP 1 <BR>AUDIT PER MPM 52-02-02;[03] CORRECTION: UPDATED MEASUREMENT TABLE;[04] VERIFIED STEP 3;[05] AUDIT C/W PER MPM 52.
- [SDR SWAA2024070998871](https://openairdocs.org/sdr/SWAA2024070998871.md): Floor Panel · cracked · Jun 6, 2024 · N286WN · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL BREAK CRACKED AT STA.540 LBL 1.<[01] REMOVED AND REPLACED CABIN FLOOR PANEL BREAK ASSY AT STA.540 LBL 1. AS PER REF B737 SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1 <BR>AUDIT PER MPM52-02-02
- [SDR SWAA2024070998872](https://openairdocs.org/sdr/SWAA2024070998872.md): Floor Panel · cracked · Jun 6, 2024 · N286WN · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL BREAK CRACKED AT STA.540 RBL 1.<[01] REMOVED AND REPLACED CABIN FLOOR PANEL BREAK ASSY AT STA.540 RBL1 AS PER REF B737 SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1<BR>AUDIT PER MPM 52-02-02
- [SDR SWAA2024070391723](https://openairdocs.org/sdr/SWAA2024070391723.md): Rib · cracked · May 30, 2024 · N286WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > L/H HORIZONTAL STAB RIB #3 CRACKED AT STIFFENER #3 LWR RADIUS. STA. 111.10.<[01] REMOVED CRACK DAMAGE AND ACCOMPLISHED REPAIR AT L/H HORIZ. STAB RIB 3 AT STIFFENER # 3 LWR RADIO AS PER SRM 51-10-02-0G-0;SRM 55-10-09-2R-4;[02] CORRECTING STEP #1 REMOVED CRACK
- [SDR SWAA2024070391724](https://openairdocs.org/sdr/SWAA2024070391724.md): Rib · cracked · May 30, 2024 · N286WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > L/H HORIZONTAL STAB RIB #3 CRACKED AT STIFFENER #4 LWR RADIUS. STA. 111.10.<[01] REMOVED CRACK DAMAGE AND ACCOMPLISHED REPAIR AT L/H HORIZ; STAB. RIB 3 AT STRIFFENER # 4 LOWER RADIUS AS PER REF B737 SRM 51-10-02-0G-0 AND SRM 55-10-09-2R-4;[02] VERIFIED STEP 1
- [SDR SWAA2024070391725](https://openairdocs.org/sdr/SWAA2024070391725.md): Rib · cracked · May 30, 2024 · N286WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > R/H HORIZONTAL STAB RIB #1 CRACKED AT STIFFENER #3 LWR RADIUS. STA. 92.70.<[01] REMOVED CRACK DAMAGE AND ACCOMPLISHED REPAIR AT R/H STABILIZER RIB #1; STIFFENER #3 LOWER RADIUS AS PER SRM 51-10-02-0G-0; SRM 51-40-02-0G-0 AND SRM 55-10-09-2R-4.;[02] COMPLETED S
- [SDR SWAA2024070991110](https://openairdocs.org/sdr/SWAA2024070991110.md): Bracket · corroded · May 29, 2024 · N286WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CORROSION **LEFT W/W LT & RT ENGINES FIRE EXTINGUISHERS BOTTLES' SUPPORT BRACKETS AT AROUND FASTENERS HOLES MKD DOTS<[01] REMOVED AND REPLACED LT & RT FIRE EXTINGUISHERS BOTTLES' SUPPORT BRACKET AT WEEL WELL AS PER B737-700 SRM 51-40-02-0G-0; DWG# 364A4403.;[0
- [SDR SWAA2024070990661](https://openairdocs.org/sdr/SWAA2024070990661.md): Retainer · cracked · May 28, 2024 · N286WN · Boeing 7377H4 · Wing Main, Frame Structure
  > LEFT WING FIXED T/E REAR SPAR DEFLECTION CONTROL RIB PANEL LOWER T/EHORIZONTAL BULB SEAL RETAINER O/B ATTACHED CLIP CRACKED @ FASTENER HEAD MKD DOT<[01] REMOVED AND REPLACED LT WING FIXED T/E REAR SPAR DEFLECTOR CONTROL RIB PANEL LOWER O/B CLIP REF B737-700 SR
- [SDR SWAA2024070990655](https://openairdocs.org/sdr/SWAA2024070990655.md): Retainer · cracked · May 28, 2024 · N286WN · Boeing 7377H4 · Wing Main, Frame Structure
  > RIGHT WING FIXED T/E REAR SPAR DEFLECTION CONTROL RIB PANEL LOWER VERTICAL SEAL RETAINER CRACKED @ FASTENER HEAD MKD DOT<[01] REMOVED AND REPLACED SEAL RETAIN AT RIGHT WING FIXED T/E REAR SPAR DEFLECTION CONTROL RIB PANEL PER REF B 737 SRM 51-40-02-0G-0.;[02]
- [SDR SWAA2024070990654](https://openairdocs.org/sdr/SWAA2024070990654.md): Vapor Barrier · cracked · May 28, 2024 · N286WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > R/H WHEEL WELL AT VAPOR BARRIOR; VERTICAL SUPPORT STIFFENER CRACKED.<[01] REMOVED AND REPLACED STIFFENER AT R/H WHEEL WELL VAPOR BARRIER RBL 25 REF B737-700 SRM 51-40-02-0G-0 AND DWG# 111A1000.;[02] VERIFIED STEP 1. AUDIT C/W PER MPM 52.02.02.
- [SDR SWAA2024070390663](https://openairdocs.org/sdr/SWAA2024070390663.md): Support Angle · cracked · May 28, 2024 · N286WN · Boeing 7377H4 · Aerodynamic Fairings
  > R/H WING-TO-BODY ACCESS PANEL 191AR AS SUPPORT ANGLE CRACKED<[01] REMOVED AND REPLACED NEW SUPPORT ANGLE AT R/H WING-TO-BODY ACCESS PANEL 191AR PER REF B 737 SRM 51-40-02-0G-0 AND DWG 116A3110.;[02] VERIFIED STEP 1. AUDIT C/W PER MPM 52.02.02.
- [SDR SWAA2024052287861](https://openairdocs.org/sdr/SWAA2024052287861.md): Slide · loose · May 20, 2024 · N286WN · Boeing 7377H4 · Escape Slide
  > AFT LEFT SERVICE DOOR SLIDE LOOSE<[01] LOOSE SCREWS SECURED; ON SLIDE. REF MM 25-66-01
- [SDR SWAA2024050782776](https://openairdocs.org/sdr/SWAA2024050782776.md): Girt Bar · damaged · May 5, 2024 · N286WN · Boeing 7377H4 · Emergency Equipment
  > AFT SVC DOOR SLIDE GRIT BAR MISSING STOP-RINGE<[01] 01 - REMOVED AND REPLACED PER [AMM 25-66-01-000-804-NG (ESCAPE SLIDE GIRT BAR INSTALLATION - PERMANENT)]
- [SDR SWAA2024042979360](https://openairdocs.org/sdr/SWAA2024042979360.md): Slider · cracked · Apr 26, 2024 · N286WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > L/H HORIZONTAL STAB UPPER FORWARD SLIDERL CRACKED<[01] R&R L/H HORIZONTAL STAB UPPER FORWARD SLIDER. IAW AMM 53-31-31
- [SDR SWAA2024040369286](https://openairdocs.org/sdr/SWAA2024040369286.md): Girt Bar · loose · Mar 31, 2024 · N286WN · Boeing 7377H4 · Emergency Equipment
  > L2 DOOR SLIDE GIRT BAR LOOSE ON ATTACHMENT<[01] RESECURED L2 DOOR SLIDE GIRT BAR REF AMM 25-66-01. NO FURTHER DEFECTS NOTED.
- [SDR SWAA2024032567454](https://openairdocs.org/sdr/SWAA2024032567454.md): Slide · detached · Mar 25, 2024 · N286WN · Boeing 7377H4 · Escape Slide
  > L2 DOOR SLIDE FELL OFF<[01] INSTALLED L2 DOOR SLIDE PER MT 725-61-06. A/C OK FOR SVC
- [SDR SWAA2024013046014](https://openairdocs.org/sdr/SWAA2024013046014.md): Slide · out of adjust · Jan 28, 2024 · N286WN · Boeing 7377H4 · Escape Slide
  > FORWARD SERVICE DOOR SLIDE PACK SAGGING<[01] DETERMINED SLIDE IS PROPERLY PACKED WITHOUT REMOVING SLIDE FROM DOOR. PER AMM 25-66-01
- [SDR SWAA2024011842008](https://openairdocs.org/sdr/SWAA2024011842008.md): Lens · detached · Jan 17, 2024 · N286WN · Boeing 7377H4 · Emergency Lighting
  > CEILING EMERGENCY EXIT SIGN LENS DETACHED<[01] RE-ATTACHED EMERGENCY EXIT SIGN LENS COVER PER S.I.P.
- [SDR SWAA2023120125523](https://openairdocs.org/sdr/SWAA2023120125523.md): Pump · faulty · Nov 28, 2023 · N286WN · Boeing 7377H4 · Hydraulic Pump (Electric/Engine), Main
  > B ELEC HYDRAULIC PUMP CREATED A FLOOR VIBRATION AT MID CABIN FLOOR ASSOCIATED LOUD NOISE AS WELL. FLIGHT ATTENDANT REPORTED AN ELECTRICAL SMELL AT MID AND AFT CABIN.<[01] REMOVED AND REPLACED B SYSTEM EMDP ASSY IAW AMM 29-11-21. OPS/LEAK CHECK GOOD.
- [SDR SWAA2023090898067](https://openairdocs.org/sdr/SWAA2023090898067.md): Seat · out of adjust · Sep 8, 2023 · N286WN · Boeing 7377H4 · Passenger Compartment Equipment
  > PASSENGER CABIN: SEAT 11E RECLINES INTO THE EMERGENCY EXIT LANE.<[01] ADJUSTED HYDRO-LOCK PER AMM 25-22-00;[02] C/W INSPECTION PER AMM 25-22-00.
- [SDR SWAA2023071978645](https://openairdocs.org/sdr/SWAA2023071978645.md): Wire · shorted · Jul 15, 2023 · N286WN · Boeing 7377H4 · Hydraulic Power System Wiring
  > AT CRUISE; HYDRAULIC B SYSTEM PRESSURE INDICATED ZERO AND THEN FLUCTUATED FROM 0 TO 1400. NO LIGHTS ILLUMINATED AND QUANTITY WAS 90%. FLAPS EXTENDED NORMALLY. NO OTHER ISSUES. PRESSURE BACK TO 3100 UPON LANDING. HAS HISTORY NEEDS FURTHER T/S WITH FEILD TECH<[0
- [SDR SWAA2023031014446](https://openairdocs.org/sdr/SWAA2023031014446.md): Megaphone · loose · Mar 9, 2023 · N286WN · Boeing 7377H4 · Emergency Equipment
  > MEGA HONE HANDLE LOOSE WILL NOT TIGHTEN<[01] REPLACED MEGA-PHONE IAW 25-64-00
- [SDR SWAA2023030210409](https://openairdocs.org/sdr/SWAA2023030210409.md): Battery Pack · inoperative · Feb 27, 2023 · N286WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK M01675 L/H FWD ENTRY LIGHT IS INOP<[01] REMOVED AND REPLACED LH FWD EMERGENCY LIGHT BATTERY PACK M01675 IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD;[02] VERIFIED STEP 1<BR>AUDIT CW
- [SDR SWAA2023013095711](https://openairdocs.org/sdr/SWAA2023013095711.md): Battery Pack · no test · Jan 27, 2023 · N286WN · Boeing 7377H4 · Emergency Lighting
  > CABIN EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY TEST AT POSITIONS M1670; M1672; M1673; M1674; AND M1675<[01] REMOVED AND REPLACED CABIN EMERGENCY LIGHT BATTERY PACKS AT POSITIONS M1670; M1672; M1673; M1674; AND M1675 PER AMM 33-51-06 AND ENG DWG 33500005
- [SDR SWAA2023013095721](https://openairdocs.org/sdr/SWAA2023013095721.md): Seal · cracked · Jan 27, 2023 · N286WN · Boeing 7377H4 · Horizontal Stabilizer Structure
  > RH HORIZONTAL STABILIZER UPPER SLIDING SEAL CRACKED<[01] R&R RH HORIZONTAL STABILIZER UPPER SLIDING SEAL. IAW AMM 53-31-31
- [SDR SWAA2022113076291](https://openairdocs.org/sdr/SWAA2022113076291.md): Panel · damaged · Nov 29, 2022 · N286WN · Boeing 7377H4 · Fuselage Main, Structure
  > ELONGATED HOLES FOUND ON 193B PANEL AT THE FOLLOWING LOCATIONS. 4, 5, 6, 7, 8, 10, 13, 16, 19, 20, 24, 25, 30, 31, AND 33. C/W EO 5351-I-14108-NG.
- [SDR SWAA2022061314739](https://openairdocs.org/sdr/SWAA2022061314739.md): Connector · inoperative · Jun 3, 2022 · N286WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT SIGN AT R1 DOOR INOP. / [01] SECURED CONNECTOR D40042P FOR OVERDOOR EXIT SIGN L1063 AT FORWARD RIGHT DOORWAY LINING. LAMP TEST PERFORMED NORMAL. REF B737 AMM TASK 33-51-01-960-801.;[02] VERIFIED STEP 1
- [SDR SWAA2022061314734](https://openairdocs.org/sdr/SWAA2022061314734.md): Battery Pack · failed · Jun 2, 2022 · N286WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY BATTERY PACK M1868 FAILED OPS TEST. / [01] REMOVED AND REPLACED BATTERY PACK POS. M1868 AS PER REF. B737 AMM 33-51-06-960-805. PERFORMED OPS CHECK AND FOUND NORMAL;[02] VERIFIED STEP 1

Next page: https://openairdocs.org/aircraft/N286WN/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 = 'N286WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N286WN/reports

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