# Service difficulty reports: N920SW

A list on [N920SW](https://openairdocs.org/aircraft/N920SW.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 4 · 167 reports

- [SDR SWIA202266123](https://openairdocs.org/sdr/SWIA202266123.md): None · cracked · Jul 12, 2022 · N920SW · Cndair CL6002B19 · Window/Windshield System
  > TRANSFER FROM EAML 947626: RIGHT (FO SIDE) WINDSHIELD CRACKED AFTER ARCHING WAS OBSERVED DURING THE DESCENT ( FLIGHT #5615 - FILED CLOSED) REPLACED RIGHT (FO SIDE) WINDSHIELD IN REFERENCE TO CRJ200 AMM. 56-11-01 AND TASK CARD 56-220-1000-SKY. OPERATIONAL
- [SDR SWIA202158614](https://openairdocs.org/sdr/SWIA202158614.md): Retainer · corroded · May 28, 2021 · N920SW · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > MAIN AVIONICS DOOR SEAL RETAINER TRACK HAS MULTIPLE AREAS OF CORROSION. (FILED CLOSED) REMOVED AND REPLACED ALL FOUR MAIN AVIONICS DOOR SEAL RETAINER SEGMENTS IN REF TO SRM 51-42-06.
- [SDR SWIA202158613](https://openairdocs.org/sdr/SWIA202158613.md): Track · cracked · May 27, 2021 · N920SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR FORWARD TRACK, LOWER SUPPORT BRACKET AT FS 574.00, WL 77.61 IS CRACKED. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR FORWARD TRACK, LOWER SUPPORT BRACKET AT FS 574.00, WL 77.61 IN REF TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA202158612](https://openairdocs.org/sdr/SWIA202158612.md): Support Angle · cracked · May 27, 2021 · N920SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR CUTOUT, UPPER BEAM AFT SUPPORT ANGLE IS CRACKED. FS 621.00 AT WL 115.08. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR CUTOUT, UPPER BEAM AFT SUPPORT ANGLE IN REF TO SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED M-337.
- [SDR SWIA202158615](https://openairdocs.org/sdr/SWIA202158615.md): Skin · corroded · May 26, 2021 · N920SW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR HAS CORRODED FASTENERS ON THE LOWER AFT CORNER AND UPPER FORWARD CORNERS OF THE INNER SKIN. (FILED CLOSED) REMOVED AND REPLACED CORRODED FASTENERS ON THE LOWER AFT CORNER AND UPPER FORWARD CORNERS OF THE SERVICE DOOR INNER SKIN IN REF TO SRM
- [SDR SWIA202156302](https://openairdocs.org/sdr/SWIA202156302.md): Nut · loose · Feb 17, 2021 · N920SW · Cndair CL6002B19 · Engine Thrust Reverser
  > RIGHT REV UNLOCKED IN FLIGHT, FLIGHT 5038 - FILED CLOSED. PLEASE REFERENCE AML 581409. THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 22323893 WITH THE FOLLOWING CORRECTIVE ACTION: BEFORE RIGGING THE RT ENGINE STOW MICRO SWITCH, FOUND THE JAM NUTS LOOSE CAUSI
- [SDR SWIA202051279](https://openairdocs.org/sdr/SWIA202051279.md): Bpsu · failed · Jun 29, 2020 · N920SW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > WHEN CONFIGURING FOR APPROACH AND LAND INTO DENVER FLAPS FAIL CAUTION MESSAGE WHEN SELECTING FLAP 8. FLAPS WERE AT 0 FOR APPROACH, LANDED AT 42700 LBS AND AT 100 PFM VSI. FLIGHT 5791. INSTALLED NEW RH BPSU IN REF WITH AMM. OPS CHECK GOOD AT THIS TIME. F
- [SDR SWIA2019122647104](https://openairdocs.org/sdr/SWIA2019122647104.md): Engine · failed · Dec 22, 2019 · N920SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > DURING CLIMB-OUT, LOSS OF NR 1 ENGINE AND LOUD BANG. ENGINE ITT WAS IN THE RED FOR ABOUT 15-20 SECONDS WITH NEEDLE FLUTTERING AT THE BOTTOM OF THE GAUGE. N1 AND N2 SPOOLED DOWN DURING THE FAILURE. CREW WAS NOT ABLE TO IDENTIFY ANY MESSAGES. AFTER ENGINE RESTAR
- [SDR SWIA2019080946177](https://openairdocs.org/sdr/SWIA2019080946177.md): Gusset · corroded · Jul 31, 2019 · N920SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON GUSSET ATTACHED TO FRAME 364 AT STR 26L. (C-CHECK) RO: 08/07/2019 REMOVED AND REPLACED GUSSET ATTACHED TO FRAME 364 AT STR 26L IAW SRM.
- [SDR SWIA2019080946172](https://openairdocs.org/sdr/SWIA2019080946172.md): Gusset · corroded · Jul 31, 2019 · N920SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON GUSSET ATTACHED TO FRAME 364 AT STR 26R. (C-CHECK) RO: 08/07/2019 REPLACED GUSSET ATTACHED TO FRAME 364 AT STR 26R IAW SRM.
- [SDR SWIA2019080946176](https://openairdocs.org/sdr/SWIA2019080946176.md): Angle · corroded · Jun 13, 2019 · N920SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON ANGLE ATTACHED TO AFT SIDE OF FRAME 364. (C-CHECK) RO: REMOVED AND REPLACED ATTACH ANGLE TO FRAME AT FS364 STGR 25L - STGR 25R IAW SRM.
- [SDR SWIA2019080946175](https://openairdocs.org/sdr/SWIA2019080946175.md): Floorbeam · corroded · Jun 13, 2019 · N920SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR BEAM AT FS 574 IS CORRODED AT THE L/H FLOOR SILL. (C-CHECK) REMOVED CORROSION ON FLOOR BEAM LOCATED AT FS574.00. C/W ALL STEPS OF REO.
- [SDR SWIA2019080946174](https://openairdocs.org/sdr/SWIA2019080946174.md): Floorbeam · cracked · Jun 13, 2019 · N920SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > BOTH INBOARD AND OUTBOARD CLIPS ON THE BL9L FLOOR BEAM, AT THE FS280.00 BULKHEAD, ARE CRACKED. (C-CHECK) REPLACED INBOARD AND OUTBOARD CLIPS ON THE BL9L FLOOR BEAM, AT THE FS280.00 IAW REO.
- [SDR SWIA2019080946173](https://openairdocs.org/sdr/SWIA2019080946173.md): Fairing · chafed · Jun 6, 2019 · N920SW · Cndair CL6002B19 · Trailing Edge Flaps
  > L/H FLAP STUB FAIRING IS CHAFED. (C-CHECK) REMOVED AND REPLACED L/H FLAP STUB FAIRING IAW SRM.
- [SDR SWIA2018110945157](https://openairdocs.org/sdr/SWIA2018110945157.md): Sensor · out of adjust · Oct 17, 2018 · N920SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > ON TAKEOFF NOSE GEAR DID NOT COME UP. LANDED WITHOUT INCIDENT. (FLT#5517) FO: 10/18/2018 CLOSED ADJUSTED NLG OLEO EXTENDED/CENTERED SENSOR IAW AMM. PERFORMED FULL STRUT SERVICE OF NLG IAW AMM.
- [SDR SWIA2018101845157](https://openairdocs.org/sdr/SWIA2018101845157.md): Not Reported · malfunctioned · Oct 17, 2018 · N920SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > ON TAKEOFF NOSE GEAR DID NOT COME UP. LANDED WITHOUT INCIDENT. (FLT 5517) FO: 10/18/2018 WORK IN PROGRESS.
- [SDR SWIA2018102545137](https://openairdocs.org/sdr/SWIA2018102545137.md): Sensor · out of adjust · Oct 15, 2018 · N920SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE WARNING SHORTLY AFTER GEAR SELECTED UP FOLLOWED BY NOSE DOOR WARNING MESSAGE. THE NOSE GEAR WAS STILL SHOWING DOWN AND LOCKED. COMPLIED WITH QRH FOR GEAR DISAGREE UNTIL MANUAL RELEASE HANDLE STEP. BOTH HYDRAULIC 3B AND 2B PUMPS SELECTED ON. MESSA
- [SDR SWIA201743484](https://openairdocs.org/sdr/SWIA201743484.md): Floorbeam · corroded · Jun 22, 2017 · N920SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM ANGLE CORRODED OUT OF LIMITS FWD AT BS 280 BETWEEN LBL 9 AND RBL 9. REMOVED AND REPLACED THE FWD FLOORBEAM ANGLE IAW SRM.
- [SDR SWIA201743490](https://openairdocs.org/sdr/SWIA201743490.md): Bracket · corroded · Jun 20, 2017 · N920SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > PASSENGER DOOR SILL ANGLE. BOTH MOUNT BRACKETS FOR THE DOOR HARNESS BLOW OUT. INBD SIDE OF THE ANGLE. REMOVED AND REPLACED THE BRACKETRS IAW SRM.
- [SDR SWIA201743489](https://openairdocs.org/sdr/SWIA201743489.md): Door Sill · corroded · Jun 19, 2017 · N920SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT DOOR SILL BS 310 - 349 HAS CORROSION. REMOVED AND INSTALLED A NEW DOOR SILL ANGLE IAW AMM.
- [SDR SWIA201743488](https://openairdocs.org/sdr/SWIA201743488.md): Door Sill · corroded · Jun 19, 2017 · N920SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT DOOR SILL BS 319.7 - 349 HAS CORROSION. REMOVED DOOR SILL LOWER ANGLE AND INSTALLED A NEW ANGLE IAW SRM.
- [SDR SWIA201743487](https://openairdocs.org/sdr/SWIA201743487.md): Intercostal · corroded · Jun 16, 2017 · N920SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR INTERCOSTAL (HINGE SIDE OF DOOR) UNDER PANEL 832ER HAS CORROSION. INSTALLED A NEW INTERCOSTAL IAW SRM.
- [SDR SWIA201743486](https://openairdocs.org/sdr/SWIA201743486.md): Skin · chafed · Jun 16, 2017 · N920SW · Cndair CL6002B19 · Ailerons
  > RIGHT AILERON LOWER INBOARD FIXED LEADING EDGE SKIN CHAFED. REPAIRED IAW REO.
- [SDR SWIA201743485](https://openairdocs.org/sdr/SWIA201743485.md): Skin · chafed · Jun 16, 2017 · N920SW · Cndair CL6002B19 · Ailerons
  > RH AILERON LOWER OUTBOARD FIXED LEADING EDGE CHAFED. REPAIRED IAW REO.
- [SDR SWIA201541315](https://openairdocs.org/sdr/SWIA201541315.md): Floor Panel · cracked · May 29, 2015 · N920SW · Cndair CL6002B19 · Fuselage Floor Panel
  > FLOOR PANEL 222FLW CRACKED AT SCREW HOLE. REPAIRED THE COCKPIT FLOOR PANEL IAW EA.
- [SDR SWIA201541317](https://openairdocs.org/sdr/SWIA201541317.md): Bulkhead Web · damaged · May 24, 2015 · N920SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BS 621 AFT PRESSURE BULKHEAD FWD SIDE, DEFECTS NOTED AT RBL 27.50, RBL 18.00, RBL 9.50, LBL 18.00, LBL 27.50, LBL 36.20 BETWEEN WL 120.43 AND WL 73.50. REPAIRED THE PRESSURE BULKHEAD IAW REO.
- [SDR SWIA201541314](https://openairdocs.org/sdr/SWIA201541314.md): Skin · gouged · May 24, 2015 · N920SW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR OUTER SKIN GOUGED AT EXTERNAL HANDLE CUT OUT. REPAIRED SERVICE DOOR OUTER SKIN GOUGES AT EXTENAL HANDLE CUT OUT IAW EA.
- [SDR SWIA201541312](https://openairdocs.org/sdr/SWIA201541312.md): Door Sill · cracked · May 24, 2015 · N920SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND CRACK ON CARGO DOOR SILL AT FS 589. REPAIRED THE DOOR SILL IAW REO.
- [SDR SWIA201541313](https://openairdocs.org/sdr/SWIA201541313.md): Skin · dented · May 23, 2015 · N920SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP LOWER SKIN HAS A DENT INBD SIDE. DAMAGE WAS REMOVED, REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM.
- [SDR SWIA201541311](https://openairdocs.org/sdr/SWIA201541311.md): Skin · damaged · May 23, 2015 · N920SW · Cndair CL6002B19 · Elevator, Plate/Skin
  > LIGHTNING STRIKE FOUND ON RT ELEVATOR T/E INBD SIDE. REPAIRED THE RT ELEVATOR T/E SKIN IAW REO.
- [SDR SWIA201541310](https://openairdocs.org/sdr/SWIA201541310.md): Door Frame · dented · May 23, 2015 · N920SW · Cndair CL6002B19 · Fuselage Main, Structure
  > PAX DOOR FRAME DENTED AT FS 349, BY THE CAM FITTING. REPAIRED THE DOOR FRAME IAW REO.
- [SDR SWIA201541316](https://openairdocs.org/sdr/SWIA201541316.md): Handle · gouged · May 22, 2015 · N920SW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR INNER DOOR HANDLE HAS SEVERAL AREAS THAT CONTAIN CHAFED AND GOUGED. REPAIRED THE SERVICE DOOR INNER HANDLE IAW STS EA.
- [SDR SWIA201541308](https://openairdocs.org/sdr/SWIA201541308.md): Rib · corroded · May 22, 2015 · N920SW · Cndair CL6002B19 · Spoilers
  > LT SPOILERON INBD RIB HAS CORRODED HARDWARE. R & R CORRODED HARDWARE IAW SRM.
- [SDR SWIA201541307](https://openairdocs.org/sdr/SWIA201541307.md): Pcu · corroded · May 22, 2015 · N920SW · Cndair CL6002B19 · Spoilers
  > RT FLIGHT SPOILER OTBD PCU HAS CORRODED HARDWARE. REMOVED CORROSION FROM THE RT FLIGHT SPOILER OTBD PCU ATTACH HARDWARE IAW SRM.
- [SDR SWIA201541306](https://openairdocs.org/sdr/SWIA201541306.md): Attach Fitting · corroded · May 22, 2015 · N920SW · Cndair CL6002B19 · Spoilers
  > RT SPOILERON OTBD FITTING ATTACH RIB HAS CORRODED HARDWARE. REMOVED CORROSION FROM THE RT SPOILERON OTBD FITTING ATTACH RIB IAW SRM.
- [SDR SWIA201541305](https://openairdocs.org/sdr/SWIA201541305.md): Bolt · corroded · May 22, 2015 · N920SW · Cndair CL6002B19 · Spoilers
  > RT SPOILERON PCU'S HAVE CORRODED HARDWARE. REMOVED CORROSION FROM THE RT SPOILERON PCU CONNECTING HARDWARE IAW SRM.
- [SDR SWIA201541304](https://openairdocs.org/sdr/SWIA201541304.md): Fitting · corroded · May 22, 2015 · N920SW · Cndair CL6002B19 · Wing, Attach Fittings
  > RT WING T/E FITTING, OTBD OF SPOILERON, HAS CORRODED HARDWARE. REMOVED CORROSION FROM THE CONNECTING HARDWARE ON THE RT WING T/E FITTING OTBD OF THE SPOILERON IAW SRM.
- [SDR SWIA201541303](https://openairdocs.org/sdr/SWIA201541303.md): Attach Fitting · corroded · May 22, 2015 · N920SW · Cndair CL6002B19 · Ailerons
  > RT AILERON INBD AND OTBD ATTACH FITTING BOLT RETAINERS HAVE CORRODED HARDWARE. REMOVED CORROSION FROM THE RT AILERON INBD AND OTBD ATTACH FITTING BOLT RETAINERS HARDWARE IAW SRM.
- [SDR SWIA201541309](https://openairdocs.org/sdr/SWIA201541309.md): Floor Panel · cracked · May 21, 2015 · N920SW · Cndair CL6002B19 · Fuselage Floor Panel
  > FLOOR PANEL 222WZ CRACKED. REPAIRED THE FLOOR PANEL IAW EA.
- [SDR SWIA201440241](https://openairdocs.org/sdr/SWIA201440241.md): Wire · chafed · Nov 30, 2014 · N920SW · Cndair CL6002B19 · Fire Protection System Wiring
  > LEFT JET OVERHEAT FAIL. REPAIRED CHAFED WIRES TO LT ENGINE LOOP A & LOOP B IAW ESPM. OPS CHECKED FIRE DETECTION SYSTEM - GOOD IAW AMM.
- [SDR SWIA201438712](https://openairdocs.org/sdr/SWIA201438712.md): Battery Pack · inoperative · Jul 13, 2014 · N920SW · Cndair CL6002B19 · Emergency Equipment
  > F/A FLASHLIGHT INOPERATIVE. INSTALLED NEW BATTERIES.
- [SDR SWIA201438621](https://openairdocs.org/sdr/SWIA201438621.md): Line · failed · Jul 8, 2014 · N920SW · Cndair CL6002B19 · Hydraulic System, Main
  > ACFT LOST ALL FLUID IN NR 1 HYDRAULIC SYSTEM. REPLACED HYDRAULIC LINE AND NR 1 EDP IAW AMM.
- [SDR SWIA201437260](https://openairdocs.org/sdr/SWIA201437260.md): Lamp · burned out · Apr 24, 2014 · N920SW · Cndair CL6002B19 · Emergency Lighting
  > NR 2 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. REPLACED LAMP.
- [SDR SWIA2014032836852](https://openairdocs.org/sdr/SWIA2014032836852.md): Bulb · burned out · Mar 26, 2014 · N920SW · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT EXIT SIGN FORWARD OF GALLEY SERVICE DOOR HAS 1 LIGHT BULB BURNED OUT. REPLACED BULB.
- [SDR SWIA201436826](https://openairdocs.org/sdr/SWIA201436826.md): Lamp · burned out · Mar 20, 2014 · N920SW · Cndair CL6002B19 · Emergency Lighting
  > TWO EMERGENCY EXIT LIGHTS BURNED OUT IN GALLEY, REPLACED LAMPS.
- [SDR SWIA201436762](https://openairdocs.org/sdr/SWIA201436762.md): Door · binding · Mar 17, 2014 · N920SW · Cndair CL6002B19 · Service Doors
  > THE GALLEY SERVICE DOOR IS DIFFICULT TO OPEN AND CLOSE. REPLACED THE GALLEY SERVICE DOOR LIFT DEVICE IAW AMM.
- [SDR SWIA201436227](https://openairdocs.org/sdr/SWIA201436227.md): Light · inoperative · Feb 2, 2014 · N920SW · Cndair CL6002B19 · Emergency Lighting
  > ONE OF THE LIGHT BULBS ON THE EMERGENCY EXIT SIGN NEXT TO SERVICE DOOR IS BURNED OUT. FLT 6415 RELAMPED.
- [SDR SWIA201335535](https://openairdocs.org/sdr/SWIA201335535.md): Relay · faulty · Dec 9, 2013 · N920SW · Cndair CL6002B19 · AC Power Distribution System
  > AC ESS BUS CAUTION MESSAGE ON & EMERGENCY LIGHT ON STATUS MESSAGE. FLT 5549 REPLACED THE AC ESS TRANSFER RELAY K1X10.
- [SDR SWIA201335297](https://openairdocs.org/sdr/SWIA201335297.md): Post · cracked · Nov 1, 2013 · N920SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACK ON FS 409+128 VERTICAL POST OTBD AFT RADIUS AT RBL18.00 WL71.00. C-CHECK REPLACED CRACKED POST AT 409+128 RBL 18 IAW REO.
- [SDR SWIA201335296](https://openairdocs.org/sdr/SWIA201335296.md): Drag Angle · cracked · Nov 1, 2013 · N920SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE CRACKED. C-CHECK REPAIRED PAX DOOR AFT DRAG ANGLE IAW REO.

Next page: https://openairdocs.org/aircraft/N920SW/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 = 'N920SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N920SW/reports

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