# N427SW: 2001 Bombardier CL-600-2B19, registration cancelled 2023-03-08

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 8, 2023
- Status when cancelled: Valid registration
- Airframe: [Bombardier CL-600-2B19](https://openairdocs.org/model/bombardier-cl-600-2b19) (registry code 1390008)
- Engine: [GE CF34 series](https://openairdocs.org/engine/ge-cf34-series) (registry code 30015)
- Data sheets: [TCDS A21EA-1](https://openairdocs.org/tcds/A21EA-1) (OpenAirDocs)
- Serial number: 7497
- Year built: 2001
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 5, 2001
- Certificate issued: October 18, 2017
- Last registry action: June 8, 2020
- Mode S code: A51745
- Owner when cancelled: [Skywest Airlines Inc](https://openairdocs.org/faa-owner/SKYWEST%20AIRLINES%20INC)
- Location: [Saint George, UT](https://openairdocs.org/faa-place/UT/Saint%20George)
- Owner type: Corporation
- Owner's area on the map: 37.0461° N, 113.5573° W: Placed by OpenAirDocs at the center of ZIP code 84790, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N427SW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=427SW
- Page: https://openairdocs.org/deregistered/N427SW-2023-03-08

From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Bombardier CL-600-2B19: https://openairdocs.org/model/bombardier-cl-600-2b19.md

## Service difficulty reports (162, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR SWIA2019120246802](https://openairdocs.org/sdr/SWIA2019120246802), Dec 2, 2019: COALESCER BAG. ODOR. 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 CLOSE
- [SDR SWIA2019102246551](https://openairdocs.org/sdr/SWIA2019102246551), Oct 21, 2019: PROXIMITY SENSOR. FAILED. 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 W
- [SDR SWIA2018121245370](https://openairdocs.org/sdr/SWIA2018121245370), Nov 30, 2018: SKIN. DAMAGED. 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 SR
- [SDR SWIA2018121245369](https://openairdocs.org/sdr/SWIA2018121245369), Nov 17, 2018: ATTACH BRACKET. CORRODED. 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 BRA
- [SDR SWIA2018121245368](https://openairdocs.org/sdr/SWIA2018121245368), Nov 17, 2018: DOOR SILL. CORRODED. 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), Nov 17, 2018: ATTACH ANGLE. CORRODED. 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 T
- [SDR SWIA2018121245366](https://openairdocs.org/sdr/SWIA2018121245366), Nov 14, 2018: DRAIN. CORRODED. 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 REM
- [SDR SWIA2018121245365](https://openairdocs.org/sdr/SWIA2018121245365), Nov 13, 2018: PRESSURE DECK. CORRODED. 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 PRES
- [SDR SWIA2018121245364](https://openairdocs.org/sdr/SWIA2018121245364), Nov 13, 2018: PRESSURE DECK. CORRODED. 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 UPPE
- [SDR SWIA2018121245363](https://openairdocs.org/sdr/SWIA2018121245363), Nov 11, 2018: FLOOR SUPPORT. CORRODED. 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 IA
- [SDR SWIA2018121245362](https://openairdocs.org/sdr/SWIA2018121245362), Nov 10, 2018: VANE. CHAFED. 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
- [SDR SWIA2018121245361](https://openairdocs.org/sdr/SWIA2018121245361), Nov 10, 2018: VANE. CHAFED. 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
- [SDR SWIA2018121245360](https://openairdocs.org/sdr/SWIA2018121245360), Nov 10, 2018: HINGE. CORRODED. 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
- [SDR SWIA2018121245358](https://openairdocs.org/sdr/SWIA2018121245358), Nov 9, 2018: SKIN. SCRATCHED. 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), Nov 9, 2018: INTERCOSTAL. CORRODED. 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 
- [SDR SWIA2018121245356](https://openairdocs.org/sdr/SWIA2018121245356), Nov 9, 2018: INTERCOSTAL. CORRODED. 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 BE
- [SDR SWIA2018121245355](https://openairdocs.org/sdr/SWIA2018121245355), Nov 9, 2018: FRAME. CORRODED. 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), Nov 9, 2018: FRAME. CORRODED. 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), Nov 9, 2018: THRESHOLD. CORRODED. 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), Nov 7, 2018: FITTING. GOUGED. 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), Nov 7, 2018: FITTING. GOUGED. 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), Nov 6, 2018: STRINGER. DENTED. 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
- [SDR SWIA2017103143931](https://openairdocs.org/sdr/SWIA2017103143931), Oct 30, 2017: FLAP. FAILED. FLAP FAIL. EMERGENCY DECLARED. (FLT 4871). CLOSED. RESET IAW FIM.
- [SDR SWIA201642837](https://openairdocs.org/sdr/SWIA201642837), Nov 6, 2016: SKIN. CHAFED. RIGHT AILERON PANEL 699BB IS CHAFED. INSTALLED A NEW PANEL IAW SRM.
- [SDR SWIA201642836](https://openairdocs.org/sdr/SWIA201642836), Nov 3, 2016: BRACKET. CORRODED. 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), Nov 23, 2014: VISOR. FAILED. VISOR PANEL 326AR FAILED GAP CHECK, C-CHECK, RECOUNTERED VISOR PANEL 326AR REF REO. GAP CHECKS GOOD.
- [SDR SWIA201440285](https://openairdocs.org/sdr/SWIA201440285), Nov 20, 2014: STEP. CRACKED. 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 FINIS
- [SDR SWIA201440284](https://openairdocs.org/sdr/SWIA201440284), Nov 20, 2014: FRAME. CORRODED. 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), Nov 16, 2014: FLOORBEAM. CRACKED. FS 280 FLOORBEAM IS CRACKED LBL 11. THE FLOORBEAM REPAIRED IAW REO.
- [SDR SWIA201440282](https://openairdocs.org/sdr/SWIA201440282), Nov 15, 2014: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM BS 353, RBL 44. BLENDED CORROSION AND FOUND TO BE IN LIMITS IAW REO.
- [SDR SWIA201440281](https://openairdocs.org/sdr/SWIA201440281), Nov 14, 2014: STRUCTURE. DAMAGED. 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), Nov 13, 2014: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT BS 353 LBL 44. REMOVED CORROSION AND FOUND WITHIN LIMITS IAW REO.
- [SDR SWIA201440279](https://openairdocs.org/sdr/SWIA201440279), Nov 13, 2014: TRUNNION. CRACKED. RT MLG TRUNNION WAS FOUND CRACKED. REPAIRED THE TRUNNION IAW REO.
- [SDR SWIA201440278](https://openairdocs.org/sdr/SWIA201440278), Nov 13, 2014: TRUNNION. CRACKED. LT TRUNNION WAS FOUND CRACKED. REPAIRED THE LT TRUNNION IAW REO.
- [SDR SWIA201440277](https://openairdocs.org/sdr/SWIA201440277), Nov 13, 2014: STRINGER. CORRODED. 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
- [SDR SWIA201440276](https://openairdocs.org/sdr/SWIA201440276), Nov 13, 2014: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT HAS CORROSION AT FS 409.44 APPROXIMATELY, LBL 44. FLOOR SUPPORT REPAIRED IAW REO.
- [SDR SWIA201440275](https://openairdocs.org/sdr/SWIA201440275), Nov 13, 2014: FLOOR SUPPORT. CORRODED. 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), Nov 13, 2014: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT HAS CORROSION AT BS 409.126 RBL 44. REMOVED CORROSION AND FOUND WITHIN LIMITS.
- [SDR SWIA201440273](https://openairdocs.org/sdr/SWIA201440273), Nov 13, 2014: FLOOR SUPPORT. CORRODED. 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), Nov 13, 2014: FLOORBEAM. CRACKED. FLOORBEAM ANGLE AT BS 280, RBL 11 IS CRACKED. R & R THE FLOORBEAM ANGLE.
- [SDR SWIA201440271](https://openairdocs.org/sdr/SWIA201440271), Nov 13, 2014: FLOOR SUPPORT. CORRODED. 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), Nov 13, 2014: FLOOR SUPPORT. CORRODED. 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), Nov 13, 2014: FLOORBEAM. CRACKED. FLOORBEAM CRACKED, BS 409+96, RBL 27. REPLACED THE CRACKED FLOORBEAM IAW SRM. PERMANENT REPAIR IAW EA.
- [SDR SWIA201440268](https://openairdocs.org/sdr/SWIA201440268), Nov 12, 2014: HINGE. CHAFED. PAX DOOR FUSELAGE MOUNTED HINGE HAS FIVE LUGS WITH MINOR CHAFE. PAX DOOR HINGE REPAIRED IAW REO.
- [SDR SWIA201440267](https://openairdocs.org/sdr/SWIA201440267), Nov 12, 2014: HINGE. CHAFED. 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), Nov 12, 2014: VANE. DAMAGED. 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), Nov 12, 2014: VANE. DAMAGED. 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), Nov 12, 2014: STRUCTURE. CHAFED. 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), Nov 12, 2014: STRUCTURE. CHAFED. 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), Nov 12, 2014: FLOOR SUPPORT. CORRODED. 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.

All 162: https://openairdocs.org/deregistered/N427SW-2023-03-08/reports.md

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