# Service difficulty reports: N423SW, cancelled Mar 6, 2023

A list on [N423SW, cancelled Mar 6, 2023](https://openairdocs.org/deregistered/N423SW-2023-03-06.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 · 130 reports

- [SDR SWIA2020061847643](https://openairdocs.org/sdr/SWIA2020061847643.md): Fitting · damaged · Jul 3, 2018 · N423SW · Cndair CL6002B19 · Horizontal Stabilizer Miscellaneous Structure
  > PER CUSTOMER REQUEST, REMOVE HORIZONTAL STAB STATIONARY FITTING HARDWARE TO VERIFY HOLE DIAMETER. (C-CHECK) RO 7/27/2018 VERIFIED HOLES DIAMETER ON HORIZONTAL STAB STATIONARY FITTING AND REAMED AND UP SIZE HOLES AND INSTALLED NEW HARDWARE PER REO AND COMPLIED
- [SDR SWIA2018073144929](https://openairdocs.org/sdr/SWIA2018073144929.md): Vane · chafed · Jun 22, 2018 · N423SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LT INBOARD FLAP - FLAP VANE CHAFED AT 2 LOCATIONS ON TOP TRAILING EDGE (CHAFES LOCATED AT 49" AND 54" FROM INBOARD SIDE OF VANE). (C-CHECK) RO: 07/28/2018 BLENDED OUT DAMAGE IAW REO AND SRM.
- [SDR SWIA2018073144928](https://openairdocs.org/sdr/SWIA2018073144928.md): Coaming · chafed · Jun 16, 2018 · N423SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR COAMING IS CHAFED AT LOWER FWD END. (C-CHECK) RO: 07/28/2018 INSTALLED 2 EA CARGO DOOR COAMING IAW SRM AND REO. OPS TEST AND LEAK CHECK GOOD AT THIS TIME. NO DEFECTS NOTED.
- [SDR SWIA2018073144921](https://openairdocs.org/sdr/SWIA2018073144921.md): Hinge · damaged · Jun 14, 2018 · N423SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > REPLACE PAX DOOR HINGE FUSELAGE SIDE DUE TO OUT OF LIMITS ELONGATED HOLES. (C-CHECK) RO: 07/28/2018 INSTALLED NEW/SERVICEABLE PASSENGER DOOR HINGE FUSELAGE SIDE IAW REO. LEAK CHECK GOOD AT THIS TIME.
- [SDR SWIA2018073144927](https://openairdocs.org/sdr/SWIA2018073144927.md): Frame · corroded · Jun 12, 2018 · N423SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 605.00 FRAME HAS 2 AREAS OF CORROSION ON FWD SIDE OF FRAME BETWEEN STR 27 AND 23L. (C-CHECK) RO: 07/28/2018 REMOVED AND INSTALLED A NEW FS 605.00 FRAME BETWEEN STRINGER 27 AND STRINGER 23L IAW REO. COMPLIED WITH PRESSURIZATION LEAK CHECK, GOOD.
- [SDR SWIA2018073144926](https://openairdocs.org/sdr/SWIA2018073144926.md): Aileron · chafed · Jun 9, 2018 · N423SW · Cndair CL6002B19 · Ailerons
  > RT AILERON ALONG LOWER LEADING EDGE IS CHAFED. (C-CHECK) RO: 07/28/2018 REMOVED DAMAGE ON RT AILERON ALONG LOWER LEADING EDGE IAW REO.
- [SDR SWIA2018073144925](https://openairdocs.org/sdr/SWIA2018073144925.md): Aileron · chafed · Jun 9, 2018 · N423SW · Cndair CL6002B19 · Ailerons
  > RT AILERON ALONG UPPER LEADING EDGE IS CHAFED. (C-CHECK) RO: 07/28/2018 REMOVED AND REPLACED R/H AILERON UPPER LEADING EDGE IAW REO.
- [SDR SWIA2018073144924](https://openairdocs.org/sdr/SWIA2018073144924.md): Vane · chafed · Jun 9, 2018 · N423SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT WING INBOARD FLAP VANE LEADING EDGE CHAFED INBOARD OF THE INBOARD SLIDING VANE ACTUATOR ATTACHMENT. (C-CHECK) RO: 07/28/2018. REPLACED RT INBD FLAP VANE CAP IAW SRM.
- [SDR SWIA2018073144923](https://openairdocs.org/sdr/SWIA2018073144923.md): Vane · chafed · Jun 9, 2018 · N423SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT WING INBOARD FLAP VANE LEADING EDGE CHAFED OUTBOARD OF THE OUTBOARD SLIDING VANE ACTUATOR ATTACHMENT. (C-CHECK) RO: 07/28/2018 REMOVED CHAFE DAMAGE IAW REO AND SRM.
- [SDR SWIA2018073144922](https://openairdocs.org/sdr/SWIA2018073144922.md): Vane · chafed · Jun 9, 2018 · N423SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT WING INBOARD FLAP VANE LEADING EDGE CHAFED OUTBOARD OF THE MIDDLE SLIDING VANE ACTUATOR ATTACHMENT. (C-CHECK) RO: 07/28/2018 REMOVED CHAFE DAMAGE IAW REO AND SRM.
- [SDR SWIA2017101743746](https://openairdocs.org/sdr/SWIA2017101743746.md): Warning Message · false activation · Sep 11, 2017 · N423SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE. WOW INPUT CAUTION MESSAGE, STEERING INOPERATIVE, WOW OUTPUT FAIL STATUS MESSAGES POSTED. MESSAGES CLEARED AND OPS CHECKED GOOD.
- [SDR SWIA201642287](https://openairdocs.org/sdr/SWIA201642287.md): Strut · chafed · Jun 13, 2016 · N423SW · Cndair CL6002B19 · Landing Gear Door Retract Section
  > LEFT MLG DOOR LOWER CONTROL ARM CHAFED AT INBD END. REMOVED AND INSTALLED NEW SERVICEABLE LT MLG DOOR STRUT, IAW AMM. OPS CKS GOOD.
- [SDR SWIA201642286](https://openairdocs.org/sdr/SWIA201642286.md): Panel · corroded · Jun 11, 2016 · N423SW · Cndair CL6002B19 · Doors
  > PANEL 832CR HAS CORROSION AROUND THE FASTENER HOLES. R & R WITH NEW PANEL 832CR, PN: 600-31902-295 IAW SRM.
- [SDR SWIA201642285](https://openairdocs.org/sdr/SWIA201642285.md): Panel · corroded · Jun 11, 2016 · N423SW · Cndair CL6002B19 · Doors
  > PANEL 832CL HAS CORROSION AROUND THE FASTENER HOLES. R & R PANEL 832CL, PN: 600-31902-295 IAW SRM.
- [SDR SWIA201642096](https://openairdocs.org/sdr/SWIA201642096.md): A/C Pack · leaking · May 3, 2016 · N423SW · Cndair CL6002B19 · Cabin Cooling System
  > LEFT 14TH DUCT WARNING WITH SYS OFF, RED FLOW BAR ON LT COWL/PYLON. FOLLOWED QRH AND MSG DID NOT EXTINGUISH. DIVERTED, DECLARED EMERGENCY. HOT AIR LEAK COMING FROM FWD OF THE LT PACK. THE HOT AIR IS BLOWING ON THE 14TH STAGE LOOP CAUSING WARNING MESSAGE. R
- [SDR SWIA201541136](https://openairdocs.org/sdr/SWIA201541136.md): Battery Pack · discharged · Apr 17, 2015 · N423SW · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS ARE INOPERATIVE. CHARGED EMERGENCY LIGHT BATTERIES. ALL LIGHTS OPS CHECKED GOOD IAW AMM.
- [SDR SWIA201439496](https://openairdocs.org/sdr/SWIA201439496.md): Proximity Sensor · damaged · Oct 14, 2014 · N423SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE. NOSE GEAR DOORS. RETURNED TO FIELD. NOSE GEAR PROXIMITY SWITCH HAD BEEN DAMAGED.
- [SDR SWIA201439261](https://openairdocs.org/sdr/SWIA201439261.md): Bracket · bent · Sep 8, 2014 · N423SW · Cndair CL6002B19 · Main Landing Gear Attach Section
  > AFTER TAKE OFF WHEN RETRACTING THE LANDING GEAR THE NOSE GEAR DID NOT RETRACT. RECEIVED A GEAR DISAGREE WARNING MESSAGE AND NOSE DOOR OPEN WARNING MESSAGE. FOLLOWED QRH AND LANDED. R & R THE BENT NLG OLEO CENTERED/EXTENDED PROXIMITY SENSOR, PSI4GA, BRACKET
- [SDR SWIA201439206](https://openairdocs.org/sdr/SWIA201439206.md): Acm · overtemp · Aug 24, 2014 · N423SW · Cndair CL6002B19 · Cabin Cooling System
  > RETURNED TO DEPARTURE DUE TO A RT PACK HIGH TEMP. R & R RIGHT ACM.
- [SDR SWIA201439150](https://openairdocs.org/sdr/SWIA201439150.md): Bracket · broken · Aug 18, 2014 · N423SW · Cndair CL6002B19 · Main Landing Gear
  > GEAR DISAGREE. RETURNED TO THE FIELD. CLOSED, R & R NLG WOW SENSOR BRACKET IAW CMM. ADJUSTED NLG WOW SENSOR IAW CMM. OPS CHECKED GOOD. PERFORMED LANDING GEAR EXTENSION/RETRACTION OPERATIONAL CHECK IAW AMM. NO DEFECTS NOTED.
- [SDR SWIA201438914](https://openairdocs.org/sdr/SWIA201438914.md): Structure · damaged · Jul 8, 2014 · N423SW · Cndair CL6002B19 · Fuselage Main, Structure
  > MULTIPLE DENTS FOUND ON FUSELAGE SKIN AT BS 654.5 - 682 BETWEEN STRINGERS 16 -18L. ACFT OUT OF SERVICE, REPAIRED FRAME, INSTALLED DOUBLER AND REPAIRED STRINGERS 17L AND 18L IAW REO.
- [SDR SWIA201438134](https://openairdocs.org/sdr/SWIA201438134.md): Bulb · inoperative · Jun 10, 2014 · N423SW · Cndair CL6002B19 · Emergency Lighting
  > SERVICE DOOR FLOOR LEVEL LIGHTED EMERGENCY EXIT SIGN HAS AN INOPERATIVE BULB. REPLACED THE BULB IAW AMM.
- [SDR SWIA201437822](https://openairdocs.org/sdr/SWIA201437822.md): Connector · broken · May 21, 2014 · N423SW · Cndair CL6002B19 · Light System Wiring
  > EMERGENCY EXIT LIGHT FOR WARDROBE HAS A BROKEN WIRE CONNECTOR. REPLACED WIRE CONNECTOR IAW ESPM AND AMM.
- [SDR SWIA201437823](https://openairdocs.org/sdr/SWIA201437823.md): Structure · cracked · May 16, 2014 · N423SW · Cndair CL6002B19 · APU Cowling/Containment
  > APU ENCLOSURE HAS SEVERAL CRACKS AT SPOT WELDS. CLEAN AND WELDED CRACKS IN APU ENCLOSURE IAW EA.
- [SDR SWIA201437835](https://openairdocs.org/sdr/SWIA201437835.md): Floorbeam · cracked · May 15, 2014 · N423SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > ANGLE UNDER FLOORBOARD AT BS 484, LBL 36, CRACKED. C-CHECK, REPAIRED ANGLE IAW REO.
- [SDR SWIA201437834](https://openairdocs.org/sdr/SWIA201437834.md): Floorbeam · cracked · May 15, 2014 · N423SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > ANGLE UNDER FLOORBOARD AT BS 484, RBL 27, CRACKED, C-CHECK, REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE IAW STANDARD REPAIR.
- [SDR SWIA201437833](https://openairdocs.org/sdr/SWIA201437833.md): Floor Panel · corroded · May 15, 2014 · N423SW · Cndair CL6002B19 · Fuselage Floor Panel
  > LEFT PRESSURE FLOOR DOUBLER BS 409+128 - 473.15 HAS FOUR AREAS OF CORROSION. C-CHECK, REMOVED CORROSION IAW REO.
- [SDR SWIA201437832](https://openairdocs.org/sdr/SWIA201437832.md): Floor Panel · corroded · May 15, 2014 · N423SW · Cndair CL6002B19 · Fuselage Floor Panel
  > LEFT PRESSURE FLOOR DOUBLER BS 473.15 - 513 HAS THREE AREAS OF CORROSION. C-CHECK, REMOVED CORROSION IAW REO.
- [SDR SWIA201437831](https://openairdocs.org/sdr/SWIA201437831.md): Floor Panel · corroded · May 15, 2014 · N423SW · Cndair CL6002B19 · Fuselage Floor Panel
  > LEFT PRESSURE FLOOR DOUBLER BS 513-559 HAS FIVE AREAS OF CORROSION. C-CHECK, REMOVED CORROSION IAW REO.
- [SDR SWIA201437830](https://openairdocs.org/sdr/SWIA201437830.md): Web · corroded · May 15, 2014 · N423SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT PRESSURE FLOOR WEB, BS 441, CORRODED AT NUTPLATE. C-CHECK, REMOVED CORROSION IAW REO.
- [SDR SWIA201437829](https://openairdocs.org/sdr/SWIA201437829.md): Web · corroded · May 15, 2014 · N423SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT PRESSURE FLOOR WEB BS 460 CORRODED AT NUTPLATE. C-CHECK, REMOVED CORROSION IAW REO.
- [SDR SWIA201437828](https://openairdocs.org/sdr/SWIA201437828.md): Web · corroded · May 15, 2014 · N423SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT PRESSURE FLOOR WEB BS 540 CORRODED AT NUTPLATE. C-CHECK, REMOVED CORROSION IAW REO.
- [SDR SWIA201437827](https://openairdocs.org/sdr/SWIA201437827.md): Web · corroded · May 15, 2014 · N423SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT PRESSURE FLOOR WEB, BS 548, CORRODED AT NUTPLATE, C-CHECK, REMOVED CORROSION IAW REO.
- [SDR SWIA201437826](https://openairdocs.org/sdr/SWIA201437826.md): Floor Panel · corroded · May 15, 2014 · N423SW · Cndair CL6002B19 · Fuselage Floor Panel
  > RT PRESSURE FLOOR DOUBLER BS 409+128-473.15 HAS FOUR AREAS OF CORROSION. C-CHECK REMOVED CORROSION IAW REO.
- [SDR SWIA201437825](https://openairdocs.org/sdr/SWIA201437825.md): Floor Panel · corroded · May 15, 2014 · N423SW · Cndair CL6002B19 · Fuselage Floor Panel
  > RIGHT PRESSURE FLOOR DOUBLER BS 473.15-513 HAS THREE AREAS OF CORROSION. C-CHECK REMOVED CORROSION IAW REO.
- [SDR SWIA201437824](https://openairdocs.org/sdr/SWIA201437824.md): Floor Panel · corroded · May 15, 2014 · N423SW · Cndair CL6002B19 · Fuselage Floor Panel
  > RIGHT PRESSURE FLOOR DOUBLER BS 513-559 HAS FOUR AREAS OF CORROSION. C-CHECK, REMOVED CORROSION IAW REO.
- [SDR SWIA201437840](https://openairdocs.org/sdr/SWIA201437840.md): Frame · corroded · May 13, 2014 · N423SW · Cndair CL6002B19 · Fuselage Main, Frame
  > LOWER FRAME SECTION AT BS 333 IS CORRODED BEYOND LIMITS. C-CHECK, REPLACED LOWER FRAME SECTION IAW SRM.
- [SDR SWIA201437839](https://openairdocs.org/sdr/SWIA201437839.md): Frame · failed · May 13, 2014 · N423SW · Cndair CL6002B19 · Fuselage Main, Frame
  > LOWER FRAME SECTION AT BS 349 IS BEYOND LIMITS. C-CHECK, INSTALLED NEW LOWER FRAME SECTION IAW SRM.
- [SDR SWIA201437838](https://openairdocs.org/sdr/SWIA201437838.md): Frame · failed · May 13, 2014 · N423SW · Cndair CL6002B19 · Fuselage Main, Frame
  > LOWER FRAME SECTION AT BS 319.7 IS BEYOND LIMITS. C-CHECK, INSTALLED NEW LOWER FRAME SECTION IAW SRM.
- [SDR SWIA201437837](https://openairdocs.org/sdr/SWIA201437837.md): Window Frame · cracked · May 13, 2014 · N423SW · Cndair CL6002B19 · Fuselage Main, Structure
  > POSSIBLE CRACK ON WINDSHIELD CENTER POST LEFT LOWER ANGLE FITTING. C-CHECK, REPLACED POST IAW SRM.
- [SDR SWIA201437836](https://openairdocs.org/sdr/SWIA201437836.md): Angle · cracked · May 13, 2014 · N423SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 625, ANGLE IS CRACKED S14L. C-CHECK, REPLACED ANGLE IAW SRM.
- [SDR SWIA201437846](https://openairdocs.org/sdr/SWIA201437846.md): Skin · corroded · May 11, 2014 · N423SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LOWER AFT FUSELAGE SKIN HAS CORROSION AT SEVERAL FASTENERS FROM BS 559+88 - 559 +112 AT LOWER CENTERLINE. C-CHECK, REMOVED CORROSION IAW EA.
- [SDR SWIA201437845](https://openairdocs.org/sdr/SWIA201437845.md): Skin · gouged · May 11, 2014 · N423SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE SKIN HAS A GOUGE AT BS 691, S20L. C-CHECK, REPAIRED SKIN IAW EA.
- [SDR SWIA201437844](https://openairdocs.org/sdr/SWIA201437844.md): Hinge Fitting · gouged · May 11, 2014 · N423SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > NR 6 LUG IS GOUGED ON PASSENGER DOOR PIANO HINGE. C-CHECK, BLENDED OUT GOUGE DAMAGE IAW REO.
- [SDR SWIA201437843](https://openairdocs.org/sdr/SWIA201437843.md): Vane · chafed · May 11, 2014 · N423SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE INBD L/E IS CHAFED. C-CHECK, BLENDED OUT CHAFE IAW REO.
- [SDR SWIA201437842](https://openairdocs.org/sdr/SWIA201437842.md): Vane · chafed · May 11, 2014 · N423SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE CENTER L/E IS CHAFED. C-CHECK, SKIN CAP REPLACED IAW REO.
- [SDR SWIA201437841](https://openairdocs.org/sdr/SWIA201437841.md): Vane · chafed · May 11, 2014 · N423SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE OTBD L/E IS CHAFED. C-CHECK, BLENDED OUT DAMAGED AREA IAW REO.
- [SDR SWIA201437850](https://openairdocs.org/sdr/SWIA201437850.md): Skin · gouged · May 9, 2014 · N423SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR SKIN AROUND HANDLE, HAS THREE GOUGES. TWO AT FWD AREA OF HANDLE AND ONE AT AFT END. C-CHECK, REPAIRED GOUGES IAW GREO.
- [SDR SWIA201437849](https://openairdocs.org/sdr/SWIA201437849.md): Vane · chafed · May 9, 2014 · N423SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT WING INBD FLAP VANE UPPER L/E OF VANE CHAFED, JUST INBD OF FLAP VANE, INBD SLIDING ACTUATOR. C-CHECK, REPLACED LEFT WING INBD FLAP VANE INBD L/E IAW SRM.
- [SDR SWIA201437848](https://openairdocs.org/sdr/SWIA201437848.md): Vane · chafed · May 9, 2014 · N423SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT WING INBD FLAP VANE-UPPER L/E OF VANE CHAFED JUST OTBD OF FLAP VANE OTBD SLIDING ACTUATOR, C-CHECK, BLENDED OUT DAMAGED AREA IAW REO.

Next page: https://openairdocs.org/deregistered/N423SW-2023-03-06/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 = 'N423SW' AND deregistration_id = 'N423SW-2023-03-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N423SW-2023-03-06/reports

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