# Service difficulty reports: N427SW, cancelled Mar 8, 2023

A list on [N427SW, cancelled Mar 8, 2023](https://openairdocs.org/deregistered/N427SW-2023-03-08.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 · 162 reports

- [SDR SWIA2019120246802](https://openairdocs.org/sdr/SWIA2019120246802.md): Coalescer Bag · odor · Dec 2, 2019 · N427SW · Cndair CL6002B19 · Humidity Control System
  > SMOKE TOILET CAUTION MESSAGE ON ARRIVAL. SUSPECT APU IS AT FAULT BECAUSE IT APPEARED WHEN I TURNED IT ON AND DISAPPEARED WHEN I TURNED IT OFF. FLIGHT 3844 CLOSED TROUBLE SHOT SMOKE IN CABIN IAW FIM. FOUND APU TO BE OVER SERVICED. PROPERLY SERVICED APU IAW A
- [SDR SWIA2019102246551](https://openairdocs.org/sdr/SWIA2019102246551.md): Proximity Sensor · failed · Oct 21, 2019 · N427SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > NOSE GEAR FAILED TO RETRACT ON TAKEOFF. MADE NORMAL LANDING AND TAXIED TO THE GATE. FLT # 3892 CLOSEDTROUBLE SHOT LANDING GEAR SYSTEM. ADJUSTED LEFT AND RIGHT WEIGHT OFF WHEELS PROX SENSORS IAW AMM. PERFORMED EXTENSION AND RETRACTION CHECK PER IAW AMM. OPS
- [SDR SWIA2018121245370](https://openairdocs.org/sdr/SWIA2018121245370.md): Skin · damaged · Nov 30, 2018 · N427SW · Cndair CL6002B19 · Ailerons
  > RIGHT AILERON ASSEMBLY €“ UPPER LEADING EDGE FOUND TO BE OUT OF LIMITS. (C-CHECK) RO: 12/11/2018 REMOVED AND REPLACED RH AILERON UPPER LEADING EDGE SKIN IAW SRM.
- [SDR SWIA2018121245369](https://openairdocs.org/sdr/SWIA2018121245369.md): Attach Bracket · corroded · Nov 17, 2018 · N427SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > THE FRAME TO FLOOR BEAM ATTACH BRACKET (€ŒT€? FITTING) AT FS 319.0 HAS CORROSION. (C-CHECK) RO: 12/11/2018 REMOVED AND REPLACED FRAME TO FLOOR BEAM ATTACH BRACKET (€ŒT€? FITTING) AT FS 319.0 IAW SRM.
- [SDR SWIA2018121245368](https://openairdocs.org/sdr/SWIA2018121245368.md): Door Sill · corroded · Nov 17, 2018 · N427SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > THE SERVICE DOOR FWD SILL FROM FS310.0 TO FS319.0 HAS CORROSION. (C-CHECK) RO: 12/11/2018 REMOVED AND REPLACED FLOOR SILL IAW SRM.
- [SDR SWIA2018121245367](https://openairdocs.org/sdr/SWIA2018121245367.md): Attach Angle · corroded · Nov 17, 2018 · N427SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FOUND CORRODED SPLICE ANGLE ATTACHED TO THE LH SIDE OF LOWER FRAME SPLICE @ FS.605. (C-CHECK) RO: 12/11/2018 REMOVED AND REPLACED SPLICE ANGLE AT FS 605.00 ON THE LH SIDE IAW SRM.
- [SDR SWIA2018121245366](https://openairdocs.org/sdr/SWIA2018121245366.md): Drain · corroded · Nov 14, 2018 · N427SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON THE FORWARD PASSENGER DOOR LOWER SILL DRAIN TUBE SUPPORT BRACKET. LOCATED ON THE LOWER SIDE OF THE DOOR SILL. FS312.00 (C-CHECK) RO: 12/11/2018 REMOVED AND REPLACED DRAIN TUBE BRACKET IAW SRM.
- [SDR SWIA2018121245365](https://openairdocs.org/sdr/SWIA2018121245365.md): Pressure Deck · corroded · Nov 13, 2018 · N427SW · Cndair CL6002B19 · Fuselage Main, Structure
  > LEFT HAND UPPER SURFACE OF PRESSURE FLOOR SILL HAS CORROSION MARKED FROM FS 445.0 TO 559.0. (C-CHECK) RO: 12/11/2018 BLENDED THE LEFT HAND UPPER SURFACE OF PRESSURE FLOOR SILL FROM FS 445.0 TO 559.0. COMPLIED WITH ALL STEPS OF THE REPAIRS IAW REO AND SRM.
- [SDR SWIA2018121245364](https://openairdocs.org/sdr/SWIA2018121245364.md): Pressure Deck · corroded · Nov 13, 2018 · N427SW · Cndair CL6002B19 · Fuselage Main, Structure
  > RIGHT HAND UPPER SURFACE OF PRESSURE FLOOR SILL HAS CORROSION MARKED FROM FS 445.0 TO 559.0. (C-CHECK) RO: 12/11/2018 BLENDED 11 EA LOCATIONS ON RIGHT HAND UPPER SURFACE OF PRESSURE FLOOR SILL FROM FS 445.0 TO 559.0. COMPLIED WITH ALL STEPS OF THE REPAIRS IAW
- [SDR SWIA2018121245363](https://openairdocs.org/sdr/SWIA2018121245363.md): Floor Support · corroded · Nov 11, 2018 · N427SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT SIDE SILL BETWEEN FS559-FS559+80 HAS SEVERAL SPOTS OF CORROSION. (C-CHECK) RO: 12/11/2018 REPLACED 2EA SECTIONS OF RH FLOOR SILL FROM FS559 TO FS559+80 IAW REO AND SRM.
- [SDR SWIA2018121245362](https://openairdocs.org/sdr/SWIA2018121245362.md): Vane · chafed · Nov 10, 2018 · N427SW · Cndair CL6002B19 · Trailing Edge Flaps
  > REPLACE LH INBOARD FLAP VANE L/E SKIN, CENTER LOCATION DUE TO OUT OF LIMITS CHAFE DAMAGE. (C-CHECK) RO: 12/11/2018 REMOVED AND REPLACED LH INBOARD FLAP VANE L/E SKIN, CENTER LOCATION IAW SRM.
- [SDR SWIA2018121245361](https://openairdocs.org/sdr/SWIA2018121245361.md): Vane · chafed · Nov 10, 2018 · N427SW · Cndair CL6002B19 · Trailing Edge Flaps
  > REPLACE LH INBOARD FLAP VANE L/E SKIN, OUTBOARD LOCATION DUE TO OUT OF LIMITS CHAFE DAMAGE. (C-CHECK) RO: 12/11/2018 REMOVED AND REPLACED LH INBOARD FLAP VANE L/E SKIN, OUTBOARD LOCATION IAW SRM.
- [SDR SWIA2018121245360](https://openairdocs.org/sdr/SWIA2018121245360.md): Hinge · corroded · Nov 10, 2018 · N427SW · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > LAVATORY SERVICE DOOR ( 196AR) UPPER AND LOWER HINGES CORRODED. (C-CHECK) RO: 12/11/2018 REPLACED THE AFT LAVATORY SERVICE DOOR WITH NEW UPPER AND LOWER HINGES IAW SRM.
- [SDR SWIA2018121245358](https://openairdocs.org/sdr/SWIA2018121245358.md): Skin · scratched · Nov 9, 2018 · N427SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > ABOVE AFT CARGO DOOR A/C OUTER SKIN THERE IS DEEP SCRATCHES. (C-CHECK) RO: 12/11/2018 REMOVED CARGO DOOR A/C OUTER SKIN SCRATCHES IAW SRM. NO DEFECTS NOTED.
- [SDR SWIA2018121245357](https://openairdocs.org/sdr/SWIA2018121245357.md): Intercostal · corroded · Nov 9, 2018 · N427SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AVIONICS BETWEEN FS 349.0 TO FS 364.0 HAS CORROSION AT INTERCOSTAL ON STR 26 R. (C-CHECK) RO: 12/11/2018 REPLACED INTERCOSTAL AT FS349 TO FS364 NEAR STR26R IAW SRM. PRESSURIZATION LEAK CHECK GOOD.
- [SDR SWIA2018121245356](https://openairdocs.org/sdr/SWIA2018121245356.md): Intercostal · corroded · Nov 9, 2018 · N427SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AVIONICS BAY IN BETWEEN FS 364 AND FS 349.0 AT STR 26L INTERCOSTAL HAS CORROSION. (C-CHECK) RO: 12/11/2018 INSTALLED NEW SERVICABLE L/H LATCH PIN INTERCOSTAL BETWEEN FS349.00-FS364.00 AND BETWEEN STGE 26L TO STGR 27 IAW SRM, LEAK CHECK GOOD.
- [SDR SWIA2018121245355](https://openairdocs.org/sdr/SWIA2018121245355.md): Frame · corroded · Nov 9, 2018 · N427SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 394.0 AVIONICS BAY AFT FRAME HAS CORROSION. (C-CHECK) RO: 12/11/2018 REMOVED CORROSION FROM LOWER FRAME AT FS394.0 IAW SRM. PRESSURE CHECKS GOOD.
- [SDR SWIA2018121245354](https://openairdocs.org/sdr/SWIA2018121245354.md): Frame · corroded · Nov 9, 2018 · N427SW · Cndair CL6002B19 · Fuselage Main, Frame
  > AVIONICS BAY LOWER FRAME AT FS 349.0 HAS CORROSION. (C-CHECK) RO: 12/11/2018 REMOVED AND REPLACED 349 FRAME IAW SRM. ALL CHECKS OKAY.
- [SDR SWIA2018121245353](https://openairdocs.org/sdr/SWIA2018121245353.md): Threshold · corroded · Nov 9, 2018 · N427SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR THRESHOLD CORRODED. (C-CHECK) RO: 12/11/2018 INSTALLED NEW SERVICE DOOR STEP PLATE P/N 601R38957-31 IAW REO.
- [SDR SWIA2018121245352](https://openairdocs.org/sdr/SWIA2018121245352.md): Fitting · gouged · Nov 7, 2018 · N427SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LH OVERWING EMERGENCY DOOR FITTINGS GOUGED 2EA. (C-CHECK) RO: 12/11/2018 REMOVED DAMAGE FROM THE LH EMERGENCY DOOR FITTINGS 2EA. IAW REO.
- [SDR SWIA2018121245351](https://openairdocs.org/sdr/SWIA2018121245351.md): Fitting · gouged · Nov 7, 2018 · N427SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RH OVERWING EMERGENCY DOOR FITTINGS GOUGED 2EA. (C-CHECK) RO: 12/11/2018 REMOVED DAMAGE FROM THE RH EMERGENCY DOOR FITTINGS 2EA. IAW REO.
- [SDR SWIA2018121245350](https://openairdocs.org/sdr/SWIA2018121245350.md): Stringer · dented · Nov 6, 2018 · N427SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > DENT FOUND BETWEEN STR 21L AND 22L, 1 1/8" ABOVE 22L, 5.5" FORWARD OF FS 589.00. (C-CHECK) RO: 12/11/2018 COMPLIED WITH PERMANENT REPAIR OF DENT FOUND AT FS 589.00 AND ADDITIONAL DENT FOUND AT FS 580.00 IAW REO.
- [SDR SWIA2017103143931](https://openairdocs.org/sdr/SWIA2017103143931.md): Flap · failed · Oct 30, 2017 · N427SW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAIL. EMERGENCY DECLARED. (FLT 4871). CLOSED. RESET IAW FIM.
- [SDR SWIA201642837](https://openairdocs.org/sdr/SWIA201642837.md): Skin · chafed · Nov 6, 2016 · N427SW · Cndair CL6002B19 · Ailerons
  > RIGHT AILERON PANEL 699BB IS CHAFED. INSTALLED A NEW PANEL IAW SRM.
- [SDR SWIA201642836](https://openairdocs.org/sdr/SWIA201642836.md): Bracket · corroded · Nov 3, 2016 · N427SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR LOWER SILL BRACKET CONNECTORS HAVE CORROSION. REMOVED AND REPLACED 2 EACH PAX DOOR LOWER SILL BRACKETS CONNECTORS IAW SRM.
- [SDR SWIA201440286](https://openairdocs.org/sdr/SWIA201440286.md): Visor · failed · Nov 23, 2014 · N427SW · Cndair CL6002B19 · Fuselage Structure (General)
  > VISOR PANEL 326AR FAILED GAP CHECK, C-CHECK, RECOUNTERED VISOR PANEL 326AR REF REO. GAP CHECKS GOOD.
- [SDR SWIA201440285](https://openairdocs.org/sdr/SWIA201440285.md): Step · cracked · Nov 20, 2014 · N427SW · Cndair CL6002B19 · Passenger/Crew Doors
  > CRACK ON PAX DOOR FWD SIDE PANEL BOTTOM STEP. REPAIRED PAX DOOR BOTTOM STEP, PERFORMED NDT, NO DEFECTS NOTED. FABRICATED AND INSTALLED REPAIR AND RESTORED FINISH IAW EA.
- [SDR SWIA201440284](https://openairdocs.org/sdr/SWIA201440284.md): Frame · corroded · Nov 20, 2014 · N427SW · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION FOUND BS 333 FRAME LOWER FLANGE BETWEEN S25L - 26R. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS AND RESTORED FINISH IAW EA.
- [SDR SWIA201440283](https://openairdocs.org/sdr/SWIA201440283.md): Floorbeam · cracked · Nov 16, 2014 · N427SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280 FLOORBEAM IS CRACKED LBL 11. THE FLOORBEAM REPAIRED IAW REO.
- [SDR SWIA201440282](https://openairdocs.org/sdr/SWIA201440282.md): Floorbeam · corroded · Nov 15, 2014 · N427SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM BS 353, RBL 44. BLENDED CORROSION AND FOUND TO BE IN LIMITS IAW REO.
- [SDR SWIA201440281](https://openairdocs.org/sdr/SWIA201440281.md): Structure · damaged · Nov 14, 2014 · N427SW · Cndair CL6002B19 · Fuselage Main, Structure
  > UPON REMOVAL OF FASTENERS FOR CORROSION REMOVAL FOUND ONE HOLE ELONGATED LOCATED ON LOWER AFT FUSELAGE, BS 559.47, RIGHT OF STR 27. REPAIRED.
- [SDR SWIA201440280](https://openairdocs.org/sdr/SWIA201440280.md): Floor Support · corroded · Nov 13, 2014 · N427SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT BS 353 LBL 44. REMOVED CORROSION AND FOUND WITHIN LIMITS IAW REO.
- [SDR SWIA201440279](https://openairdocs.org/sdr/SWIA201440279.md): Trunnion · cracked · Nov 13, 2014 · N427SW · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > RT MLG TRUNNION WAS FOUND CRACKED. REPAIRED THE TRUNNION IAW REO.
- [SDR SWIA201440278](https://openairdocs.org/sdr/SWIA201440278.md): Trunnion · cracked · Nov 13, 2014 · N427SW · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > LT TRUNNION WAS FOUND CRACKED. REPAIRED THE LT TRUNNION IAW REO.
- [SDR SWIA201440277](https://openairdocs.org/sdr/SWIA201440277.md): Stringer · corroded · Nov 13, 2014 · N427SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 26L HAS CORROSION ON FLANGE AT FS 326 APPROXIMATELY, C-CHECK, BLENDED CORROSION. FOUND TO BE OUT OF LIMITS. CUT AND REMOVED DAMAGED SECTION OF STRINGER 26L FROM FS 325-FS 340 AND INSTALLED NEW STRINGER SECTION IAW SRM. COMPLIED WITH ST CARD. MAJOR
- [SDR SWIA201440276](https://openairdocs.org/sdr/SWIA201440276.md): Floor Support · corroded · Nov 13, 2014 · N427SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT HAS CORROSION AT FS 409.44 APPROXIMATELY, LBL 44. FLOOR SUPPORT REPAIRED IAW REO.
- [SDR SWIA201440275](https://openairdocs.org/sdr/SWIA201440275.md): Floor Support · corroded · Nov 13, 2014 · N427SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT HAS CORROSION AT BS 409.87 LBL 44. REPAIRED IAW REO. UT INSPECTION REF NDTM. NO DEFECTS FOUND.
- [SDR SWIA201440274](https://openairdocs.org/sdr/SWIA201440274.md): Floor Support · corroded · Nov 13, 2014 · N427SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT HAS CORROSION AT BS 409.126 RBL 44. REMOVED CORROSION AND FOUND WITHIN LIMITS.
- [SDR SWIA201440273](https://openairdocs.org/sdr/SWIA201440273.md): Floor Support · corroded · Nov 13, 2014 · N427SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT HAS CORROSION ON UPPER AND LOWER SURFACES AT NUTPLATE AT FS 319, RBL 44. REMOVED CORROSION IAW SRM AND FOUND TO BE WITHIN LIMITS IAW REO.
- [SDR SWIA201440272](https://openairdocs.org/sdr/SWIA201440272.md): Floorbeam · cracked · Nov 13, 2014 · N427SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM ANGLE AT BS 280, RBL 11 IS CRACKED. R & R THE FLOORBEAM ANGLE.
- [SDR SWIA201440271](https://openairdocs.org/sdr/SWIA201440271.md): Floor Support · corroded · Nov 13, 2014 · N427SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT FLOOR SUPPORT IS CORRODED IN SEVERAL PLACES FROM BS 559 TO 559+16. FLOOR SUPPORT REPAIRED IAW REO, AND FOUND WITHIN LIMITS.
- [SDR SWIA201440270](https://openairdocs.org/sdr/SWIA201440270.md): Floor Support · corroded · Nov 13, 2014 · N427SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT RT FLOOR SUPPORT HAS CORROSION UNDER OTBD MATING SURFACE OF AFT RT CARGO FLOOR PANEL 282HRF. BLENDED CORROSION IAW REO.
- [SDR SWIA201440269](https://openairdocs.org/sdr/SWIA201440269.md): Floorbeam · cracked · Nov 13, 2014 · N427SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM CRACKED, BS 409+96, RBL 27. REPLACED THE CRACKED FLOORBEAM IAW SRM. PERMANENT REPAIR IAW EA.
- [SDR SWIA201440268](https://openairdocs.org/sdr/SWIA201440268.md): Hinge · chafed · Nov 12, 2014 · N427SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR FUSELAGE MOUNTED HINGE HAS FIVE LUGS WITH MINOR CHAFE. PAX DOOR HINGE REPAIRED IAW REO.
- [SDR SWIA201440267](https://openairdocs.org/sdr/SWIA201440267.md): Hinge · chafed · Nov 12, 2014 · N427SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR MOUNTED HINGE HALF HAS3 LUGS WITH CHAFED. BLENDED THE HINGE AND FOUND TO BE IN LIMITS IAW REO.
- [SDR SWIA201440265](https://openairdocs.org/sdr/SWIA201440265.md): Vane · damaged · Nov 12, 2014 · N427SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LT INBD FLAP VANE L/E SKIN, CENTER, WS 103 DAMGED. INSTALLED NEW FABRICATED CENTER CAP ONTO LT INBD FLAP VANE IAW SRM & EA.
- [SDR SWIA201440264](https://openairdocs.org/sdr/SWIA201440264.md): Vane · damaged · Nov 12, 2014 · N427SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RT INBD FLAP VANE L/E SKIN, CENTER, WS 98.509 DAMAGED. INSTALLED NEW FABRICATED CENTER CAP ONTO RT INBD FLAP VANE, IAW SRM AND EA.
- [SDR SWIA201440263](https://openairdocs.org/sdr/SWIA201440263.md): Structure · chafed · Nov 12, 2014 · N427SW · Cndair CL6002B19 · Landing Gear Doors
  > LEFT MLG DOOR FWD EDGE CHAFED. BLENDED CHAFE IAW SRM AND FOUND TO BE WITHIN LIMITS. REPAIRED IAW REO.
- [SDR SWIA201440262](https://openairdocs.org/sdr/SWIA201440262.md): Structure · chafed · Nov 12, 2014 · N427SW · Cndair CL6002B19 · Landing Gear Doors
  > RT MLG DOOR AFT EDGE IS CHAFED. CHAFE BLENDED IAW SRM AND FOUND WITHIN LIMITS IAW SRM. REPAIRED IAW EA.
- [SDR SWIA201440261](https://openairdocs.org/sdr/SWIA201440261.md): Floor Support · corroded · Nov 12, 2014 · N427SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT UPPER SURFACE OF PRESSURE FLOOR SUPPORT FROM BS 420 - 535 HAS CORROSION. REPAIRED RT UPPER SURFACE OF PRESSURE FLOOR SUPPORT IAW REO. NO LEAKS NOTED.

Next page: https://openairdocs.org/deregistered/N427SW-2023-03-08/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 = 'N427SW' AND deregistration_id = 'N427SW-2023-03-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N427SW-2023-03-08/reports

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