# Service difficulty reports: N418SW, cancelled Nov 30, 2022

A list on [N418SW, cancelled Nov 30, 2022](https://openairdocs.org/deregistered/N418SW-2022-11-30.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 · 144 reports

- [SDR SWIA2018082144957](https://openairdocs.org/sdr/SWIA2018082144957.md): Engine · seized · Aug 2, 2018 · N418SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > DURING DESCENT, LEFT ENGINE SEIZED IN FLIGHT, AURAL WARNING, ENGINE SHUT DOWN. R & R THE LT ENGINE IAW AMM. OPS AND LEAK CHECKED GOOD.
- [SDR SWIA2018041044533](https://openairdocs.org/sdr/SWIA2018041044533.md): Frame · corroded · Mar 20, 2018 · N418SW · Cndair CL6002B19 · Fuselage Main, Frame
  > BS 333 FRAME CORRODED BETWEEN STRINGERS 25L AND 26R. REMOVED CORROSION IAW REO AND SRM.
- [SDR SWIA2018041044532](https://openairdocs.org/sdr/SWIA2018041044532.md): Seat Track · corroded · Mar 14, 2018 · N418SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED LBL 9, BS 574 TO 621. BLENDED THE CORROSION IAW SRM AND REO.
- [SDR SWIA2018041044523](https://openairdocs.org/sdr/SWIA2018041044523.md): Floor Support · damaged · Mar 14, 2018 · N418SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SUPPORT, BETWEEN BS 559 - 559+16 FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM AND REO.
- [SDR SWIA2018041044531](https://openairdocs.org/sdr/SWIA2018041044531.md): Floor Support · corroded · Mar 11, 2018 · N418SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FLOOR SUPPORT, BS 559+80 TO 621 HAS CORROSION. REPLACED THE FLOOR SUPPORT IAW REO.
- [SDR SWIA2018041044530](https://openairdocs.org/sdr/SWIA2018041044530.md): Intercostal · corroded · Mar 11, 2018 · N418SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL CORRODED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM.
- [SDR SWIA201844529](https://openairdocs.org/sdr/SWIA201844529.md): Intercostal · corroded · Mar 11, 2018 · N418SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL AND ATTACH AND CORRODED. REMOVED CORROSION IAW SRM.
- [SDR SWIA2018041044528](https://openairdocs.org/sdr/SWIA2018041044528.md): Intercostal · corroded · Mar 11, 2018 · N418SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL 60031902413 AND ITS ATTACH ANGLE CORRODED. REMOVED AND REPLACED THE PAX DOOR INTERCOSTAL AND ATTACH ANGLE IAW SRM.
- [SDR SWIA201844527](https://openairdocs.org/sdr/SWIA201844527.md): Intercostal · corroded · Mar 11, 2018 · N418SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CORRODED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM.
- [SDR SWIA2018041044526](https://openairdocs.org/sdr/SWIA2018041044526.md): Strap · corroded · Mar 11, 2018 · N418SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM HAS CORROSION AT RIGHT SIDE BS 559. REMOVED AND REPLACED THE FLOORBEAM STRAP IAW SRM.
- [SDR SWIA2018041044525](https://openairdocs.org/sdr/SWIA2018041044525.md): Floor Support · corroded · Mar 11, 2018 · N418SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SUPPORT BS 559 TO 559+80 CORRODED. BLENDED THE CORROSION IAW REO.
- [SDR SWIA2018041044524](https://openairdocs.org/sdr/SWIA2018041044524.md): Door Sill · corroded · Mar 10, 2018 · N418SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL CORRODED. REMOVED AND REPLACED THE DOOR SILL IAW SRM.
- [SDR SWIA2017122944113](https://openairdocs.org/sdr/SWIA2017122944113.md): Windshield · cracked · Dec 28, 2017 · N418SW · Cndair CL6002B19 · Flight Compartment Windows
  > RECEIVED A RIGHT WINDSHIELD HEAT CAUTION - RIGHT WINDSHIELD CRACKED. RAN QRH AND MANUALLY CONTROLLED PRESSURIZATION, HOWEVER THE NUMBERS WERE TOO HIGH IN THE CABIN. DECLARED AN EMERGENCY AND DID A QUICK DESCENT AND DIVERTED. (FLT 4668) FO: 12/28/2017 CLOSED. R
- [SDR SWIA201641987](https://openairdocs.org/sdr/SWIA201641987.md): Skin · chafed · Feb 27, 2016 · N418SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > RIGHT APRON SKIN HAS CHAFING BETWEEN BS 529 - 554 AT WL 51-58. REPAIRED IAW REO.
- [SDR SWIA201641985](https://openairdocs.org/sdr/SWIA201641985.md): Panel · corroded · Feb 25, 2016 · N418SW · Cndair CL6002B19 · Passenger/Crew Doors
  > DOOR PANEL 832BR HAS CORROSION AROUND THE FASTENER HOLES. REPLACED PAX DOOR PANEL 832BR IAW SRM.
- [SDR SWIA201641984](https://openairdocs.org/sdr/SWIA201641984.md): Skin · dented · Feb 23, 2016 · N418SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SKIN DENTED LOCATED EIGHT INCHES AFT OF BS 640 BETWEEN STRINGERS 22 - 23R. PERFORMED PERMANENT REPAIR, SECTION 1 IAW EA.
- [SDR SWIA201641986](https://openairdocs.org/sdr/SWIA201641986.md): Vane · chafed · Feb 21, 2016 · N418SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE CHAFED AT CENTER L/E CAP. REPLACED RT INBD FLAP VANE CENTER CAP IAW SRM AND STS EA.
- [SDR SWIA201641983](https://openairdocs.org/sdr/SWIA201641983.md): Isolator · cracked · Feb 20, 2016 · N418SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT 621 BULKHEAD ISOLATOR CRACKED. R & R THE ISOLATOR IAW SRM.
- [SDR SWIA201641982](https://openairdocs.org/sdr/SWIA201641982.md): Isolator · cracked · Feb 20, 2016 · N418SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > ISOLATOR CRACKED ON FWD SIDE OF FS 621. R & R THE ISOLATOR, AT FS 621, LBL 27 IAW SRM.
- [SDR SWIA201641981](https://openairdocs.org/sdr/SWIA201641981.md): Floor Panel · cracked · Feb 19, 2016 · N418SW · Cndair CL6002B19 · Fuselage Floor Panel
  > RIGHT TRU FLOOR CRACK AT FS 193.00. COMPLIED WITH PERMANENT REPAIR, TYPE II, OF RT TRU FLOOR IAW REO.
- [SDR SWIA201641854](https://openairdocs.org/sdr/SWIA201641854.md): Filter · contaminated · Feb 2, 2016 · N418SW · Cndair CL6002B19 · Cabin Cooling System
  > LT PACK HI TEMP FOLLOWED BY SMOKE TOILET MESSAGE. R & R LT PRSOV FILTER IAW CMM. OPS CHECK GOOD.
- [SDR SWIA201641767](https://openairdocs.org/sdr/SWIA201641767.md): Fan · smoke · Jan 18, 2016 · N418SW · Cndair CL6002B19 · Air Distribution Fan
  > RETURN TO FIELD FOR SMOKE IN THE LAV. R & R LAVATORY EXHAUST FAN IAW AMM. OPS CHECK GOOD.
- [SDR SWIA201540493](https://openairdocs.org/sdr/SWIA201540493.md): Battery Pack · discharged · Jan 3, 2015 · N418SW · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. CHARGED BATTERIES AND ALL EMERGENCY LIGHTS ILLUMINATE NORMALLY.
- [SDR SWIA201439281](https://openairdocs.org/sdr/SWIA201439281.md): Wire · disconnected · Sep 11, 2014 · N418SW · Cndair CL6002B19 · Light System Wiring
  > BOTTOM LEFT INTERIOR EMERGENCY LIGHT INOPERATIVE. REPAIRED A LOOSE CONNECTION.
- [SDR SWIA201438005](https://openairdocs.org/sdr/SWIA201438005.md): Light · inoperative · Jun 5, 2014 · N418SW · Cndair CL6002B19 · Emergency Lighting
  > RT OVERWING EMERGENCY LIGHT NR 6 INOPERATIVE. R & R RT OVERWING EMERGENCY LIGHT NR 6 IAW AMM.
- [SDR SWIA201437931](https://openairdocs.org/sdr/SWIA201437931.md): Overheat Sensor · failed · May 27, 2014 · N418SW · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > DURING CLIMB OUT, RECEIVED A RT WING OVERHEAT MESSAGE. COMPLIED WITH QRH AND RETURNED TO DEPARTURE. R & R RT WING OVERHEAT SENSOR AND CONTROL SENSOR WITH SERVICEABLE UNITS IAW AMM.
- [SDR SWIA201437136](https://openairdocs.org/sdr/SWIA201437136.md): Structure · cracked · Apr 12, 2014 · N418SW · Cndair CL6002B19 · APU Cowling/Containment
  > THE APU ENCLOSURE CRACKED ALONG SIDE THE WELD DURING INSTALLATION. C-CHECK, WELDED CRACK ON APU ENCLOSURE IAW REO.
- [SDR SWIA201437138](https://openairdocs.org/sdr/SWIA201437138.md): Structure · delaminated · Apr 11, 2014 · N418SW · Cndair CL6002B19 · Fuselage Main, Structure
  > L/E PANEL 630KL HAS SEPARATION OF THE SHROUD TO L/E SKIN. DELAMINATION. C-CHECK, REBONDED SEPARATION OF THE SHROUD TO L/E SKIN IAW REO.
- [SDR SWIA201437137](https://openairdocs.org/sdr/SWIA201437137.md): Structure · delaminated · Apr 11, 2014 · N418SW · Cndair CL6002B19 · Fuselage Main, Structure
  > L/E PANEL 630JL HAS SEPARATION OF THE SHROUD TO L/E SKIN, DELAMINATION. C-CHECK, REBONDED SEPARATION OF THE SHROUD TO L/E SKIN IAW REO.
- [SDR SWIA201437140](https://openairdocs.org/sdr/SWIA201437140.md): Skin · gouged · Apr 7, 2014 · N418SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP INSIDE PANEL 584AB GOUGE IN SKIN IN BETWEEN ACTUATOR FITTING. C-CHECK, BLENDED GOUGE SMOOTH IAW REO.
- [SDR SWIA201437139](https://openairdocs.org/sdr/SWIA201437139.md): Skin · gouged · Apr 7, 2014 · N418SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP INSIDE PANEL 584CB GOUGE IN SKIN IN BETWEEN ACTUATOR FITTING. C-CHECK, BLENDED GOUGE SMOOTH IAW REO.
- [SDR SWIA201437141](https://openairdocs.org/sdr/SWIA201437141.md): Vane · chafed · Apr 3, 2014 · N418SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE L/E CENTER CAP CHAFED BEYOND PERMANENT LIMITS. C-CHECK, REPLACED RT INBD FLAP VANE L/E CENTER CAP IAW SRM.
- [SDR SWIA201437144](https://openairdocs.org/sdr/SWIA201437144.md): Stiffener · cracked · Apr 2, 2014 · N418SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT SIDE OUTER FUSELAGE VERTICAL STIFFENER HAS CRACK AT FS 473.15. C-CHECK, REMOVED AND INSTALLED NEW VERTICAL STIFFNER IAW SRM.
- [SDR SWIA201437143](https://openairdocs.org/sdr/SWIA201437143.md): Stiffener · cracked · Apr 2, 2014 · N418SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > OUTSIDE FUSELAGE VERTICAL STIFFENER HAS CRACK AT RADIUS AT BS 461, RT SIDE. C-CHECK, R & R VERTICAL STIFFENER IAW SRM.
- [SDR SWIA201437142](https://openairdocs.org/sdr/SWIA201437142.md): Vane · chafed · Apr 2, 2014 · N418SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RT WING INBD FLAP VANE CHAFED ON INBD L/E. C-CHECK, BLENDED RT WING INBD FLAP VANE CHAFE ON INBD L/E IAW REO.
- [SDR SWIA201437146](https://openairdocs.org/sdr/SWIA201437146.md): Skin · chafed · Apr 1, 2014 · N418SW · Cndair CL6002B19 · Ailerons
  > LT AILERON HAS CHAFING ON UPPER L/E SHROUD IN VARIOUS AREAS. C-CHECK, CHAFED LT AILERON UPPER L/E WAS BLENDED IAW REO.
- [SDR SWIA201437145](https://openairdocs.org/sdr/SWIA201437145.md): Lever · chafed · Apr 1, 2014 · N418SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FORWARD PULL IN LEVER IS CHAFED. C-CHECK, REMOVED CHAFE ON PAX DOOR PULL IN LEVER IAW REO.
- [SDR SWIA201437153](https://openairdocs.org/sdr/SWIA201437153.md): Structure · chafed · Mar 31, 2014 · N418SW · Cndair CL6002B19 · Landing Gear Doors
  > LEFT MLG DOOR, THE INBD FWD INNER CORNER BY THE BRUSH ASSY HAS CHAFING. C-CHECK, REPAIRED IAW REO AND SRM.
- [SDR SWIA201437152](https://openairdocs.org/sdr/SWIA201437152.md): Arm · chafed · Mar 31, 2014 · N418SW · Cndair CL6002B19 · Landing Gear Door Retract Section
  > LEFT MLG DOOR, THE WING TO DOOR BELLCRANK LEVER/ARM HAS CHAFING ON LOWER AFT SECTION. C-CHECK, BLENDED CHAFING ON LT MLG DOOR, WING TO DOOR BELLCRANK LEVER ARM LOWER AFT SECTION IAW REO.
- [SDR SWIA201437151](https://openairdocs.org/sdr/SWIA201437151.md): Structure · chafed · Mar 31, 2014 · N418SW · Cndair CL6002B19 · Landing Gear Doors
  > RT MLG DOOR, THE INBD FWD CORNER OF INNER DOOR BY THE BRUSH ASSY HAS CHAFING. C-CHECK, REPAIRED IAW REO AND SRM.
- [SDR SWIA201437150](https://openairdocs.org/sdr/SWIA201437150.md): Bellcrank · chafed · Mar 31, 2014 · N418SW · Cndair CL6002B19 · Landing Gear Door Retract Section
  > RIGHT MLG DOOR, WING TO BELL CRANK ASSY LEVER/ARM, THE FWD ATTACH POINT HAS CHAFING. C-CHECK, BLENDED CHAFING ON RT MLG DOOR, WING TO DOOR BELLCRANK ASSY LEVER ARM, FWD ATTACH POINT IAW REO.
- [SDR SWIA201437149](https://openairdocs.org/sdr/SWIA201437149.md): Panel · chafed · Mar 31, 2014 · N418SW · Cndair CL6002B19 · Standard Practices/Structures
  > CHAFE ON PANEL 599BB. C-CHECK, BLENDED CHAFED AREA ON PANEL 599BB IAW REO.
- [SDR SWIA201437148](https://openairdocs.org/sdr/SWIA201437148.md): Vane · chafed · Mar 31, 2014 · N418SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RT WING INBD FLAP VANE CHAFED ON OTBD L/E. C-CHECK, R & R WITH NEW RT WING INBD FLAP VANE OTBD FLAP VANE SKIN IAW SRM.
- [SDR SWIA201437147](https://openairdocs.org/sdr/SWIA201437147.md): Rib · cracked · Mar 31, 2014 · N418SW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > LT WING BATTERY RIB HAS CRACK AT UPPER EDGE. C-CHECK, TRIMMED OUT DAMAGE TO LEFT BATTERY RIB IAW REO.
- [SDR SWIA201333765](https://openairdocs.org/sdr/SWIA201333765.md): Light · inoperative · Jun 21, 2013 · N418SW · Cndair CL6002B19 · Emergency Lighting
  > SERVICE DOOR EMERGENCY EXIT IS BURNED OUT. SERVICE RELAMPED.
- [SDR SWIA201333633](https://openairdocs.org/sdr/SWIA201333633.md): Control Unit · failed · Jun 5, 2013 · N418SW · Cndair CL6002B19 · Landing Gear Steering System
  > LOST DIRECTIONAL CONTROL WITH NOSE WHEEL STEERING AND RUDDER IMPUTS. ACFT VEERED HARD TO THE RT. NO CAUTION MESSAGE WAS RECEIVED, AFTER STOPPING, NOSE WHEEL STEERING WOULD NOT REENGAGE WITH SWITCH AND STEERING INOP CAUTION MESSAGE APPEARED. REPLACED HCU DUE
- [SDR SWIA201232176](https://openairdocs.org/sdr/SWIA201232176.md): Light · inoperative · Nov 15, 2012 · N418SW · Cndair CL6002B19 · Emergency Lighting
  > LIGHT ON EXIT SIGN NEAR SERVICE DOOR BURNED OUT. (FLT 5649) RELAMPED EXIT SIGN.
- [SDR SWIA201231463](https://openairdocs.org/sdr/SWIA201231463.md): Skin · damaged · Aug 8, 2012 · N418SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DAMAGE FROM A BIRD STRIKE FOUND ON NOSE OF AIRCRAFT BETWEEN THE TRU ACCESS DOORS. (FLT 4566) REPLACED SKIN IN REFERENCE TO CRJ200 SRM.
- [SDR SWIA201231393](https://openairdocs.org/sdr/SWIA201231393.md): Tire · blown · Jul 24, 2012 · N418SW · Cndair CL6002B19 · Tire
  > RIGHT OUTBOARD MAIN TIRE WAS BLOWN AND FLAT. (FLT 6222) REPLACED NR 3 AND 4 MAIN LANDING GEAR WHEEL ASSEMBLIES AND NR 4 WHEEL SPEED TRANSDUCER. P/N: 5010571-1, S/N OFF: SEP04-6652, P/N: 5010571-1, S/N OFF: SEP11-0859.
- [SDR SWIA201231261](https://openairdocs.org/sdr/SWIA201231261.md): Light · inoperative · Jul 11, 2012 · N418SW · Cndair CL6002B19 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHT NEAR ROW 8 IS OUT. (FLT 5514) RELAMPED EMERGENCY LIGHT.

Next page: https://openairdocs.org/deregistered/N418SW-2022-11-30/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 = 'N418SW' AND deregistration_id = 'N418SW-2022-11-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N418SW-2022-11-30/reports

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