# Service difficulty reports: N235SW

A list on [N235SW](https://openairdocs.org/aircraft/N235SW.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 3 · 136 reports

- [SDR HKGA20251220001](https://openairdocs.org/sdr/HKGA20251220001.md): Unknown · odor · Dec 20, 2025 · N235SW · Emb EMB120ER · Air Distribution System
  > WHILE AT 28K ALTITUDE, CREW TURNED PACKS ON HIGH (HEAT), AFTER 20MIN RT PACK FAILED INDICATION ILLUMINATED, CREW FOLLOWED QRH. ABOUT A MIN LATER WITH PACKS ON LOW SETTING, CREW STARTED GETTING SMOKE. CREW FOLLOWED QRH FOR SMOKE BUT SMOKE DIDN’T EVAC FAST ENOUG
- [SDR HKGA202510041001](https://openairdocs.org/sdr/HKGA202510041001.md): Fitting · chafed · Oct 1, 2025 · N235SW · Emb EMB120ER · Hydraulic System, Main
  > LOSS OF GREEN HYDRAULIC SYSTEM PRESSURE, RESULTING IN EMERGENCY PROCEDURES. EMERGENCY DECLARED AND GEAR WERE EXTENDED AND LOCKED. SMOKE APPEARED IN COCKPIT OF GEAR WAS DOWN AND LOCKED. INSPECTED AIRCRAFT AN FOUND ENGINE DRIVEN PUMP PRESSURE LINE ELBOW FITTING
- [SDR HKGA20230623001](https://openairdocs.org/sdr/HKGA20230623001.md): Engine · failed · Jun 23, 2023 · N235SW · Emb EMB120ER · Engine (Turbine/Turboprop)
  > DURING TAKEOFF, LH ENG T6 OVER HEAT, ENGINE WAS SHUT DOWN AS A PRECAUTION. SMOKE WAS PRESENT IN THE COCKPIT. UPON WALKAROUND OIL WAS PRESENT ON THE EXTERIOR OF ENGINE COWING. MAINTENANCE PERFORMED A BORESCOPE AND IDENTIFIED OIL IN THE COMBUSTION CHAMBER WITH P
- [SDR HKGA20201201001](https://openairdocs.org/sdr/HKGA20201201001.md): Unknown · vapor · Dec 1, 2020 · N235SW · Emb EMB120ER · Air Distribution System
  > SHORTLY AFTER TAKEOFF FROM KACK THE CREW NOTICED WHAT SEEMED TO BE SMOKE OR FOG COMING FROM BEHIND THE GLARESHIED ON THE CAPTAINS SIDE. THE CREW DONNED THEIR OXYGEN MASKS, DECLARED AN EMERGENCY, AND RETURNED BACK TO KCAK AND LANDED WITHOUT FURTHER ISSUE. KCA
- [SDR HKGA20191022011](https://openairdocs.org/sdr/HKGA20191022011.md): Skin · corroded · Oct 22, 2019 · N235SW · Emb EMB120ER · Wing, Plate/Skin
  > RH WING UPPER SURFACE SKIN BETWEEN RIBS 22-23 HAS CORROSION AT MIDDLE VORTEX GENERATOR INSTALLED REPAIR (PER EMB ETD 2019-120-129256)
- [SDR HKGA20191022010](https://openairdocs.org/sdr/HKGA20191022010.md): Shear Tie · cracked · Oct 22, 2019 · N235SW · Emb EMB120ER · Wing, Attach Fittings
  > FOUND CRACKED SHEAR TIE WHILE INSTALLING DOUBLER AT LH WING FUEL TANK RIB 21 FWD OF THE AFT STIFFENER. INSTALLED NEW SHEAR TIE (REF EMB120 SRM 51-40-02 REV 58)
- [SDR HKGA20191022009](https://openairdocs.org/sdr/HKGA20191022009.md): Shear Tie · cracked · Oct 22, 2019 · N235SW · Emb EMB120ER · Wing, Attach Fittings
  > LH WING RIB 15 2ND FROM THE FWD SHEAR TIE IS CRACKED. INSTALLED NEW SHEAR TIE (REF EMB120 SRM 51-40-02 REV 58)
- [SDR HKGA20191022008](https://openairdocs.org/sdr/HKGA20191022008.md): Shear Tie · cracked · Oct 22, 2019 · N235SW · Emb EMB120ER · Wing, Attach Fittings
  > LH WING RIB 15 2ND FROM THE AFT SHEAR TIE IS CRACKED. INSTALLED NEW SHEAR TIE (REF EMB120 SRM 51-40-02 REV 58).
- [SDR HKGA20191022007](https://openairdocs.org/sdr/HKGA20191022007.md): Shear Tie · cracked · Oct 22, 2019 · N235SW · Emb EMB120ER · Wing, Attach Fittings
  > LH WING RIB 16 2ND FROM THE AFT SHEAR TIE IS CRACKED. INSTALLED NEW SHEAR TIE (REF EMB120 SRM 51-40-02 REV 58)
- [SDR HKGA20191022006](https://openairdocs.org/sdr/HKGA20191022006.md): Stringer · cracked · Oct 22, 2019 · N235SW · Emb EMB120ER · Wing, Longeron/Stringer
  > LH LOWER WING STRINGER FWD OF 551BB AT RIB 16 IS CRACKED. REPAIRED AND INSTALLED STRINGER (IAW EMB120 SRM 58-20-03 FIG 202, EMBRAER ETD 019-120-121013)
- [SDR HKGA20191022005](https://openairdocs.org/sdr/HKGA20191022005.md): Shear Tie · cracked · Oct 22, 2019 · N235SW · Emb EMB120ER · Wing, Attach Fittings
  > LH WING INTERNAL RIB 19 AFT MOST UPPER SKIN TO RIB SHEAR CLIP IS CRACKED. INSTALLED NEW SHEAR TIE (REF EMB120 SRM 51-40-02 REV 58)
- [SDR HKGA20191022004](https://openairdocs.org/sdr/HKGA20191022004.md): Shear Tie · cracked · Oct 22, 2019 · N235SW · Emb EMB120ER · Wing, Attach Fittings
  > LH WING INTERNAL RIB 19, 3RD UPPER SKIN TO RIB SHEAR CLIP FROM FRONT SPAR IS CRACKED. INSTALLED NEW SHEAR CLIP (REF EMB120 SRM 51-40-02 REV 58).
- [SDR HKGA20191022003](https://openairdocs.org/sdr/HKGA20191022003.md): Shear Tie · cracked · Oct 22, 2019 · N235SW · Emb EMB120ER · Wing, Attach Fittings
  > LH WING INTERNAL RIB 19 FWD MOST UPPER SKIN TO RIB SHEAR CLIP IS CRACKED. INSTALLED NEW SHEAR CLIP (REF EMB120 SRM 51-40-02 REV 58)
- [SDR HKGA20191022002](https://openairdocs.org/sdr/HKGA20191022002.md): Mount · cracked · Oct 22, 2019 · N235SW · Emb EMB120ER · APU Cowling/Containment
  > APU COWL RH UPPER MOUNT FITTING, LOWER SUPPORT STRUCTURE IS CRACKED. INSTALLED NEW SUPPORT STRUCTURE (REF EMB120 SRM 51-25-00 REV 58)
- [SDR HKGA20191022001](https://openairdocs.org/sdr/HKGA20191022001.md): Seat Track · corroded · Oct 22, 2019 · N235SW · Emb EMB120ER · Fuselage, Seat/Cargo Attach Fittings
  > RH SEAT TRACK BETWEEN FRAMES 14-15 HAS CORROSION. INSTALLED NEW SEAT TRACK (REF EMB120 AMM 53-01-05 REV 44).
- [SDR HKGA201910108027](https://openairdocs.org/sdr/HKGA201910108027.md): Floorbeam · bent · Oct 8, 2019 · N235SW · Emb EMB120ER · Fuselage Main, Floor Beam
  > FUSELAGE, FLOOR BEAM 36 UPPER FLANGE IS BENT LEFT OF BL0. INSTALLED NEW FLOOR BEAM (REF EMB120 SRM 51-40-02 REV 58).
- [SDR HKGA201910108026](https://openairdocs.org/sdr/HKGA201910108026.md): Floorbeam · bent · Oct 8, 2019 · N235SW · Emb EMB120ER · Fuselage Main, Floor Beam
  > FUSELAGE FLOOR BEAM 33 UPPER FLANGE IS BENT LEFT OF BL0. INSTALLED NEW FLOOR BEAM (REF EMB120 SRM 51-40-02 REV 58).
- [SDR HKGA201910108025](https://openairdocs.org/sdr/HKGA201910108025.md): Stop Fitting · corroded · Oct 8, 2019 · N235SW · Emb EMB120ER · Passenger/Crew Doors
  > PAX DOOR, INTERNAL BACK UP FITTING FOR AFT LOWER STOP FITTING IS CORRODED (WITH DOOR CLOSED). MATCH DRILLED NEW INTERNAL BACKUP FITTING, INSTALLED NEW INTERNAL BACKUP FITTING (IAW EMB120 SRM 51-25-00, 51-40-02 REV 58). INSTALLED AFT LOWER STOP FITTING HAND RAI
- [SDR HKGA201910108024](https://openairdocs.org/sdr/HKGA201910108024.md): Skin · corroded · Oct 8, 2019 · N235SW · Emb EMB120ER · Passenger/Crew Doors
  > PAX DOOR OUTER SKIN, INNER SURFACE HAS A SPOT OF CORROSION AFT OF FWD FRAME BETWEEN BEAMS 5 & 6 (WITH PAX DOOR CLOSED). REPAIR FILLER FROM 2024-T3.404" (PER ETD 2019-120-111246 REV 1). INSTALLED REPAIR (PER ETD 2019-120-111246 REV 1).
- [SDR HKGA201910108023](https://openairdocs.org/sdr/HKGA201910108023.md): Attach Angle · chafed · Oct 8, 2019 · N235SW · Emb EMB120ER · Wing, Attach Fittings
  > RH WING LEADING EDGE ATTACH ANGLE RIB AT INBOARD SIDE OF NACELLE IS CHAFED IN MULTIPLE AREAS. LOCATED AND DRILLED NEW ATTACH ANGLE AND INSTALLED NUTPLATES (IAW EMB120 SRM 51-40-02 REV 58). INSTALLED NEW L/E ATTACH ANGLE (IAW EMB120 SRM 51-40-02 REV 58).
- [SDR HKGA20191008022](https://openairdocs.org/sdr/HKGA20191008022.md): Skin · cracked · Oct 8, 2019 · N235SW · Emb EMB120ER · Wing, Center Box
  > RH NACELLE FLAP TRAILING EDGE LOWER SKIN ATTACH FLANGE IS CRACKED. LOCATED AND DRILLED NEW RH NACELLE FLAP TRAIILING EDGE LOWER SKIN ATTACH FLANGE (IAW EMB120 SRM 51-40-04 REV 58). INSTALLED ATTACH FLANGE (IAW EMB120 SRM 51-40-02 REV 58).
- [SDR HKGA201910108021](https://openairdocs.org/sdr/HKGA201910108021.md): Rib · cracked · Oct 8, 2019 · N235SW · Emb EMB120ER · Nacelle/Pylon, Main Frame
  > RH NACELLE FLAP TRAILING EDGE STUB RIB BETWEEN THE IB AND CENTER RIB IS CRACKED. LOCATED AND DRILLED NEW STUB RIB (IAW EMB120 SRM 51-40-03 REV 58). INSTALLED NEW STUB RIB (REF EMB120 CPM 51-40-02 REV 58).
- [SDR HKGA201910108020](https://openairdocs.org/sdr/HKGA201910108020.md): Frame · cracked · Oct 8, 2019 · N235SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/Rib
  > LH NACELLE FRAME 10 WEB IS CRACKED ON IB SIDE LOWER CORNER. COMPLETED REPAIR STEPS OF REPAIR PROCEDURE (REF EMB ETD 2019-120-099295 REV A).
- [SDR HKGA20191008019](https://openairdocs.org/sdr/HKGA20191008019.md): Rib · cracked · Oct 8, 2019 · N235SW · Emb EMB120ER · Wing Main, Frame Structure
  > RH NACELLE FLAP INTERNAL TRAINING EDGE STUB RIB AFT OF LOWER SKIN ACCESS HOLE IS CRACKED & HAS ENLARGED FASTENER HOLES. MATCHDRILLED NEW STUB RIB (REF EMB120 SRM 51-25-00 REV 58). INSTALLED NEW STUB RIB (REF EMB120 SRM 51-40-02 REV 58).
- [SDR HKGA201910108018](https://openairdocs.org/sdr/HKGA201910108018.md): Door · chafed · Oct 8, 2019 · N235SW · Emb EMB120ER · Nacelle/Pylon, Main Frame
  > RH NACELLE COWL DOOR 423 INNER SKIN IS CHAFFED THROUGH AT THE UPPER FWD CORNER OF THE OIL FILL DOOR. C/W REPAIR (ETD 2019-120-10557).
- [SDR HKGA201910108017](https://openairdocs.org/sdr/HKGA201910108017.md): Doubler · chafed · Oct 8, 2019 · N235SW · Emb EMB120ER · Nacelle/Pylon, Plate/Skin
  > RH NACELLE COWL DOOR 424 INNER SKIN EXISTING REPAIR DOUBLER IS CHAFFED. FABRICATED REPAIR DOUBLER, INSTALLED REPAIR DOUBLER (IAW EMB120 ETD 2019-120-105571).
- [SDR HKGA201910108016](https://openairdocs.org/sdr/HKGA201910108016.md): Doubler · cracked · Oct 8, 2019 · N235SW · Emb EMB120ER · Nacelle/Pylon, Plate/Skin
  > RH NACELLE COWL DOOR 424 INNER SKIN IS CRACKED BELOW HOLD OPEN ROD STOWAGE BRACKET. FABRICATED REPAIR DOUBLER, INSTALLED REPAIR DOUBLER (IAW EMB120 ETD 2019-120-105571).
- [SDR HKGA201910108015](https://openairdocs.org/sdr/HKGA201910108015.md): Support · cracked · Oct 8, 2019 · N235SW · Emb EMB120ER · APU Cowling/Containment
  > APU COWL LH UPPER MOUNT FITTING, LOWER SUPPORT STRUCTURE IS CRACKED AT RIVET HOLE. MATCH DRILLED NEW SUPPORT (IAW EMB120 SRM 51-25-00 REV 58). INSTALLED NEW SUPPORT (IAW EMB120 SRM 51-40-02 REV 58).
- [SDR HKGA201910108014](https://openairdocs.org/sdr/HKGA201910108014.md): Support · buckled · Oct 8, 2019 · N235SW · Emb EMB120ER · APU Cowling/Containment
  > APU COWL RH LOWER MOUNT FITTING, UPPER SUPPORT STRUCTURE IS BUCKLED. MATCH DRILLED NEW SUPPORT (IAW EMB120 SRM 51-25-00 REV 58). INSTALLED NEW SUPPORT (IAW EMB120 SRM 51-40-02 REV 58).
- [SDR HKGA2019101080](https://openairdocs.org/sdr/HKGA2019101080.md): Intercostal · cracked · Oct 8, 2019 · N235SW · Emb EMB120ER · Fuselage Miscellaneous Structure
  > INTERCOSTAL BETWEEN FRAMES 39-40, STRINGER 3R IS CRACKED. LOCATED AND DRILLED NEW INTERCOSTAL (IAW EMB120 SRM 51-40-04 REV 58). INSTALLED INTERCOSTAL AND SUPPORT BRACKET BETWEEN FRAMES 39-40 STR3R (IAW EMB120 SRM 51-40-02 REV 58).
- [SDR HKGA201910108012](https://openairdocs.org/sdr/HKGA201910108012.md): Floor Support · corroded · Oct 8, 2019 · N235SW · Emb EMB120ER · Fuselage Miscellaneous Structure
  > FUSELAGE, CENTER LONGITUDINAL FLOOR BEAM UPPER SURFACE HAS AREAS OF CORROSION AND MISSING SURFACE PROTECTION FR 38-40. MIN REMAINING THICKNESS NOTED ON FWD FLOOR BEAM UPPER SURFACE FOUND TO BE.038" (REF EMB NDI 51-00-04 REV 3). PERFORMED MATCH DRILL OF LONGIT
- [SDR HKGA201910108011](https://openairdocs.org/sdr/HKGA201910108011.md): Floor Support · corroded · Oct 8, 2019 · N235SW · Emb EMB120ER · Fuselage Miscellaneous Structure
  > FUSELAGE, RH LONGITUTINAL FLOORBEAM UPPER SURFACE HAS AREAS OF CORROSION AND MISSING SURFACE PROTECTION BETWEEN FR 38-42. MIN REMAINING THICKNESS.027" (REF EMB NDI 51-00-04 REV 3). DRILLED NEW FAILSAFE (IAW EMB120 SRM 51-26-00 REV 58). INSTALLED NEW FAILSAFE
- [SDR HKGA201910108010](https://openairdocs.org/sdr/HKGA201910108010.md): Floor Support · bent · Oct 8, 2019 · N235SW · Emb EMB120ER · Fuselage Miscellaneous Structure
  > LH FLOOR SUPPORT BETWEEN FRAMES 28-29 IS BENT AND CREASED. LOCATED AND DRILLED NEW FLOOR SUPPORT (IAW EMB120 SRM 51-40-04 REV 58). INSTALLED PULLEY BRACKET (PER EMB120 SRM 51-40-02 REV 58).
- [SDR HKGA201910108009](https://openairdocs.org/sdr/HKGA201910108009.md): Floor Support · corroded · Oct 8, 2019 · N235SW · Emb EMB120ER · Fuselage Miscellaneous Structure
  > LEFT LONGITUDINAL FLOORBEAM PPER SILL HAS AREAS OF CORROSION BETWEEN FRAMES 20-22. MATCHDRILLED NEW FLOORBEAM UPPER SILL (REF EMB120 SRM 51-25-00 REV 58). INSTALLED NEW UPPER SILL (REF EMB120 SRM 51-40-02 REV 58)
- [SDR HKGA201910108008](https://openairdocs.org/sdr/HKGA201910108008.md): Failsafe · corroded · Oct 8, 2019 · N235SW · Emb EMB120ER · Fuselage Main, Structure
  > FRAME 17 FAILSAFE BETWEEN STRINGERS 20R-21R HAS CORROSION. MIN REMAINING THICKNESS.027" (REF EMB NDI 51-00-04 REV 3). DRILLED NEW FAILSAFE (IAW EMB120 SRM 51-26-00 REV 58). INSTALLED NEW FAILSAFE (IAW EMB120 SRM 51-40-02 REV 58).
- [SDR HKGA201910108007](https://openairdocs.org/sdr/HKGA201910108007.md): Floor Support · corroded · Oct 8, 2019 · N235SW · Emb EMB120ER · Fuselage Miscellaneous Structure
  > LEFT LONGITIDUNAL FLOORBEAM UPPER SILL BETWEEN FRAMES 15-16 HAS AREAS OF CORROSION. MATCHDRILLED NEW UPPER SILL (PER EMB120 51-40-02 REV 58). INSTALLED NEW UPPER SILL (PER EMB120 51-40-02 REV 58).
- [SDR HKGA201910108006](https://openairdocs.org/sdr/HKGA201910108006.md): Floor Support · corroded · Oct 8, 2019 · N235SW · Emb EMB120ER · Fuselage Miscellaneous Structure
  > RH LONGITUDINAL FLOORBEAM UPPER SILL BETWEEN FRAMES 13-15 HAS AREAS OF CORROSION. MATCHDRILLED NEW FLOORBEAM UPPER SILL (REF EMB120 SRM 51-25-00 REV 58). INSTALLED NEW UPPER SILL (REF EMB120 SRM 51-40-02 REV 58).
- [SDR HKGA201910108005](https://openairdocs.org/sdr/HKGA201910108005.md): Floor Support · corroded · Oct 8, 2019 · N235SW · Emb EMB120ER · Fuselage Miscellaneous Structure
  > CENTER LONGITUDINAL FLOORBEAM UPPER STILL BETWEEN FRAMES 13-16 HAS AREAS OF CORROSION. REMOVED CORROSION ON CENTER FLOORBEAM UPPER SILL BETWEEN FR 13-16 (IAW EMB120 CPM 51-14-00 REV 10). REMAINING THICKNESS.030 (IAW EMB120 SRM 53-10-10, 53-00-00 REV 58). MATC
- [SDR HKGA201910108004](https://openairdocs.org/sdr/HKGA201910108004.md): Skin · corroded · Oct 8, 2019 · N235SW · Emb EMB120ER · Wing, Plate/Skin
  > LH WING UPPER SKIN HAS CORROSION AFT OF THE VORTEX GENERATOR AT RIB 23. NOMINAL THICKNESS.080" OUT OF LIMITS (REF EMB120 SRM 57-20-01 AND 57-00-01 REV 58). CUTOUT BLENDED AREA (IAW EMB120 SRM 57-20-01 REV 58). LAYED OUT AND FABIRCATED DOUBLER FROM.080" 2024T
- [SDR HKGA201910108003](https://openairdocs.org/sdr/HKGA201910108003.md): Skin · corroded · Oct 8, 2019 · N235SW · Emb EMB120ER · Wing, Plate/Skin
  > LH WING UPPER SKIN HAS CORROSION AFT OF VORTEX GENERATOR BETWEEN RIBS 22 AND 23. NOMINAL THICKNESS.080" OUT OF LIMITS (REF EMB120 SRM 57-20-01 AND 57-00-01 REV 58). CUTOUT BLENDED AREA (IAW EMB120 SRM 57-20-01 REV 58). LAYED OUT AND FABIRCATED DOUBLER FROM.0
- [SDR HKGA201910108002](https://openairdocs.org/sdr/HKGA201910108002.md): Attach Angle · chafed · Oct 8, 2019 · N235SW · Emb EMB120ER · Leading Edge Devices
  > LH WING LEADING EDGE ATTACH ANGLE RIB AT INBOARD SIDE OF NACELLE IS CHAFED IN MULTIPLE AREAS. MATCHDRILLED NEW LEADING EDGE ATTACH (REF EMB120 SRM 51-25-00 REV 58). INSTALLED NEW LEADING EDGE ATTACH (REF EMB120 SRM 51-40-02 REV 58). APPLIED SURFACE PROTECTION
- [SDR HKGA201910108001](https://openairdocs.org/sdr/HKGA201910108001.md): Skin · corroded · Oct 8, 2019 · N235SW · Emb EMB120ER · Wing, Plate/Skin
  > LH WING UPPER SKIN HAS CORROSION AFT OF THE VORTEX GENERATOR AT RIB 21. FABRICATED REPAIR DOUBLER AND FILLER PIECE FROM 2024-T3.080" (PER ETD 2019-120-101457). INSTALLED DOUBLER AND VORTEX GENERATOR (PER 2019-120-101457). APPLIED CAP SEAL TO FASTENERS WITHIN
- [SDR HKGA20180201001](https://openairdocs.org/sdr/HKGA20180201001.md): Tube · ruptured · Jan 31, 2018 · N235SW · Emb EMB120ER · Pneumatic Distribution System
  > SHORTLY AFTER TAKEOFF, THE PILOTS TURNED THE BLEEDS TO NORMAL IAW AFTER TAKEOFF CHECKLIST AND RECEIVED A RED LT DUCT LEAK ANNUNCIATION. PERFORMED THE QRH PROCEDURES AND RETURNED TO THE AIRPORT. MAINTENANCE TROUBLESHOT THE ISSUE TO THE LEFT CROSS BLEED TUBE A
- [SDR HKGA20171207008](https://openairdocs.org/sdr/HKGA20171207008.md): Relay · intermittent · Dec 7, 2017 · N235SW · Emb EMB120ER · Landing Gear Retraction/Extension System
  > DURING APPROACH THE LANDING GEAR DID NOT EXTEND WHEN THE GEAR HANDLE WAS PLACED IN THE DOWN POSITION. THE FLIGHT CREW BEGAN EMERGENCY PROCEDURES AND ACTIVATED THE ELECTRICAL OVERRIDE SYSTEMS AND THE GEAR EXTENDED AND THE FLIGHT CREW RECEIVED THREE GOOD DOWN AN
- [SDR SWIA201439815](https://openairdocs.org/sdr/SWIA201439815.md): Wire · broken · Nov 3, 2014 · N235SW · Emb EMB120ER · Light System Wiring
  > EMERGENCY FLOOR STRIP INOPERATIVE. REPAIRED BROKEN WIRES. OPS CHECKED GOOD.
- [SDR SWIA201439570](https://openairdocs.org/sdr/SWIA201439570.md): Connector · failed · Oct 19, 2014 · N235SW · Emb EMB120ER · Light System Wiring
  > EMERGENCY LIGHTS ARE INOPERATIVE. R & R EMERGENCY LIGHT CONNECTORS. OPS CHECKED GOOD.
- [SDR SWIA201439342](https://openairdocs.org/sdr/SWIA201439342.md): Door · failed · Sep 23, 2014 · N235SW · Emb EMB120ER · Landing Gear Door Retract Section
  > RT MLG WOULD NOT RETRACT AFTER TAKEOFF, RETURNED TO THE FIELD. R & R RT MLG FORWARD OTBD DOOR. SWUNG GEAR SEVERAL TIMES. OPS CHECK GOOD.
- [SDR SWIA201438600](https://openairdocs.org/sdr/SWIA201438600.md): Lens · missing · Jun 29, 2014 · N235SW · Emb EMB120ER · Emergency Lighting
  > SECOND WHITE LIGHT BACK ON EMERGENCY LIGHT FLOOR STRIP MISSING LENS. ATTACHED A LENS COVER TO 2ND WHITE LIGHT BACK ON EMERGENCY LIGHT FLOOR STRIP. 2014NM060066
- [SDR SWIA201438023](https://openairdocs.org/sdr/SWIA201438023.md): Acm · failed · Jun 8, 2014 · N235SW · Emb EMB120ER · Cabin Cooling System
  > CABIN FILLED WITH SMOKE. REMOVED AND REPLACED RT ACM IAW AMM.
- [SDR SWIA201437379](https://openairdocs.org/sdr/SWIA201437379.md): Lamp · burned out · Apr 23, 2014 · N235SW · Emb EMB120ER · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHT IN CABIN IS BURNED OUT. REPLACED THE LAMP.

Next page: https://openairdocs.org/aircraft/N235SW/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 = 'N235SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N235SW/reports

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