# N809CA: 2000 Bombardier CL-600-2B19, registration cancelled 2023-11-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 3, 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: 7366
- Year built: 2000
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 4, 2000
- Certificate issued: November 18, 2016
- Last registry action: September 15, 2023
- Mode S code: AB037F
- Owner when cancelled: [Skywest Airlines Inc](https://openairdocs.org/faa-owner/SKYWEST%20AIRLINES%20INC)
- Location: [St George, UT](https://openairdocs.org/faa-place/UT/St%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/N809CA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=809CA
- Page: https://openairdocs.org/deregistered/N809CA-2023-11-03

From the FAA registry file of November 5, 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 (180, newest 50)

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

- [SDR SWIA202266699](https://openairdocs.org/sdr/SWIA202266699), Oct 31, 2022: NONE. FAULT MESSAGE. LEFT FIRE FAIL CAUTION MESSAGE CAME ON AND OFF TWICE INFLIGHT. PERFORMED QRH. (FLIGHT #5336 FILED CLOSED) T/S L/H FIRE FAIL CAUTION MSG, FOUND ENGINE NACELLE AN
- [SDR SWIA202265554](https://openairdocs.org/sdr/SWIA202265554), May 3, 2022: NONE. FAILED. GEAR DISAGREE WARNING MESSAGE. NOSE GEAR STUCK DOWN. RAN QRH AND ALL 3 GEARS CAME DOWN WITH THE MANUAL RELEASE HANDLE. (FLIGHT 5454 - FILED CLOSED) THIS DISCREP
- [SDR SWIA2020033149779](https://openairdocs.org/sdr/SWIA2020033149779), Mar 10, 2020: NUT PLATE. BROKEN. PANEL 571LL ON L/H WING HAS ONE BROKEN NUTPLATE. (C CHECK) RO 3/27/2020 REMOVED BROKEN NUTPLATE AND INSTALLED NEW P/N NAS1789-3 NUTPLATE IAW CRJ 200 SRM.
- [SDR SWIA2020033149770](https://openairdocs.org/sdr/SWIA2020033149770), Feb 27, 2020: FITTING. BROKEN. AVIONICS BAY DOOR FWD R/H NYLON GUIDE FITTING BROKEN. (C CHECK) RO 3/27/2020 REMOVED BROKEN AVIONICS BAY DOOR FWD R/H NYLON GUIDE FITTING. LOCATED AND DRILLED N
- [SDR SWIA2020033049586](https://openairdocs.org/sdr/SWIA2020033049586), Feb 26, 2020: ANGLE. CRACKED. *ANGLE ATTACHED TO TOP AFT EDGE OF FRAME AT FS 682 IS CRACKED BETWEEN STGR25R AND STGR26R. (C CHECK) RO 3/27/2020 REPAIRED ANGLE ATTACHED TO TOP AFT EDGE OF FRA
- [SDR SWIA2020033049584](https://openairdocs.org/sdr/SWIA2020033049584), Feb 25, 2020: FITTING. CRACKED. *R/H WINDSHIELD SIDE POST AFT LWR CLIP (FITTING) IS CRACKED. (C CHECK) RO 3/27/2020 REMOVED AND REPLACED R/H WINDSHIELD SIDE POST FITTING REFERENCE CRJ 200 SRM 
- [SDR SWIA2020033049583](https://openairdocs.org/sdr/SWIA2020033049583), Feb 25, 2020: FITTING. CRACKED. *L/H WINDSHIELD SIDE POST AFT LWR CLIP (FITTING) IS CRACKED. (C CHECK) RO 3/27/2020 REMOVED AND REPLACED CRACKED L/H WINDSHEILD SIDE POST AFT LOWER FITTING WITH
- [SDR SWIA2020033049582](https://openairdocs.org/sdr/SWIA2020033049582), Feb 24, 2020: FRAME. CRACKED. FS 605.0 FRAME FLANGE LEFT HAND SIDE, JUST OVER AFT CARGO DOOR HAS SUSPECT CRACK AT RIVET LOCATION JUST ABOVE AND BELOW STR 9. (MARKED) (C CHECK) RO 3/27/2020 R
- [SDR SWIA2020033049581](https://openairdocs.org/sdr/SWIA2020033049581), Feb 20, 2020: RIB. DAMAGED. RH INBOARD FLAP VANE LEADING EDGE INBOARD RIB REQUIRES REPLACEMENT (C CHECK) RO 3/27/2020 REMOVED AND REPLACED AND RESTORED FINISH ON RH INBOARD FLAP VANE LEADI
- [SDR SWIA2020033149753](https://openairdocs.org/sdr/SWIA2020033149753), Feb 19, 2020: CHANNEL. CORRODED. CORROSION FOUND ON AVIONICS BAY DOOR POSITION SENSOR MOUNTING CHANNEL AT FS.364.00, STGR 27. (MARKED) (C CHECK) RO 3/27/2020 REMOVED CORROSION FROM AVIONICS BAY
- [SDR SWIA2020033049580](https://openairdocs.org/sdr/SWIA2020033049580), Feb 19, 2020: FLOOR SKIN. CRACKED. *PRESSURE FLOOR SKIN IS CRACKED AT 2EA LOCATIONS AT APPROX FS 461 BETWEEN BL0 AND LBL 9 AND BL0 TO RBL9. SUSPECT AREAS ARE MARKED WITH RED GREASE PENCIL. (C CHE
- [SDR SWIA2020033049579](https://openairdocs.org/sdr/SWIA2020033049579), Feb 19, 2020: FRAME SPLICE. CORRODED. CORROSION FOUND ON UPPER SPLICE ANGLE FOR LOWER FRAME SECTOR AT FS.364.00 AND STGR 27. (MARKED) (C CHECK) RO 3/27/2020 REMOVED CORROSION ON UPPER SPLICE ANGLE F
- [SDR SWIA2020033049578](https://openairdocs.org/sdr/SWIA2020033049578), Feb 17, 2020: FITTING. CRACKED. *AFT LINTEL CLIP IS POSSIBLY CRACKED. FLAGGED (C CHECK) RO 3/27/2020 REMOVED AND REPLACED AFT LINTEL CLIP REF. CRJ-200 SRM AND BOMBARDIER DWG. PRESSURE CHECK GO
- [SDR SWIA2020033149764](https://openairdocs.org/sdr/SWIA2020033149764), Feb 13, 2020: NOT REPORTED. CORRODED. *FS559.00+80 €“ 559.00+112 STGR 26L €“ 26R CORROSION AROUND SEVERAL FASTENERS (MARKED) (C CHECK) RO 3/27/2020 REPAIRED CORROSION DAMAGE AT FS559+80 TO FS574 S
- [SDR SWIA2020033149752](https://openairdocs.org/sdr/SWIA2020033149752), Feb 13, 2020: FLOOR SUPPORT. CORRODED. AFT CARGO APPROX.€¦ FS.559.00+118 TO FS. 621.00 LEFT HAND LBL 27.00 FLOOR BEAM HAS NUMEROUS SPOTS OF CORROSION (MARKED) (C CHECK) RO 3/27/2020 COMPLIED WITH RE
- [SDR SWIA2020033149751](https://openairdocs.org/sdr/SWIA2020033149751), Feb 13, 2020: HINGE. CORRODED. *RUDDER CENTER HINGE AREA, UPPER AND LOWER GROUND STUD AND HARDWARE ON RUDDER, CORRODED (MARKED, OUT OF SCOPE) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW 
- [SDR SWIA2020033149750](https://openairdocs.org/sdr/SWIA2020033149750), Feb 13, 2020: SEAT TRACK. CORRODED. THE SEAT TRACK AT RBL9.00 FROM FS409.00+128 TO FS559.00 HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C CHECK) RO 3/27/2020 BLENDED SEAT TRACK AT RBL9 FS409+12
- [SDR SWIA2020033149749](https://openairdocs.org/sdr/SWIA2020033149749), Feb 13, 2020: SEAT TRACK. CORRODED. THE SEAT TRACK AT LBL9.00 FROM FS409.00+128 TO FS559.00 HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C CHECK) RO 3/27/2020 REMOVED CORRODED SET TRACK LBL BETW
- [SDR SWIA2020033149748](https://openairdocs.org/sdr/SWIA2020033149748), Feb 13, 2020: STAND OFF. CORRODED. * THE LH FLOOR SILL HAS 3EA ELECTRICAL STANDOFFS THAT ARE CORRODED BETWEEN FS409.00+64 TO FS409.00+80. (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND REPLACED 3 EA
- [SDR SWIA2020033049576](https://openairdocs.org/sdr/SWIA2020033049576), Feb 13, 2020: BRACKET. CRACKED. *FS621.00 - 625.30 STGR APPROX. 14R ANGLE CRACKED (MARKED) (C CHECK) RO 3/27/2020 REMOVED CRACKED ANGLE BRACKET FROM FS. 625.30 STRINGER 14R AND INSTALLED NEW A
- [SDR SWIA2020033049575](https://openairdocs.org/sdr/SWIA2020033049575), Feb 13, 2020: BRACKET. CRACKED. *FS621.00 - 625.30 STGR APPROX. 14L ANGLE CRACKED (MARKED) (C CHECK) RO 3/27/2020 REMOVED CRACKED ANGLE BRACKET FROM FS. 625.3.0 STRINGER 14L AND INSTALLED NEW 
- [SDR SWIA2020033049574](https://openairdocs.org/sdr/SWIA2020033049574), Feb 13, 2020: FRAME. CORRODED. FRAME AT L/H FS 513 WL73 (FLOOR LEVEL) HAS SMALL AREA OF CORROSION. (C CHECK) RO 3/27/2020 REMOVED CORROSION ON FRAME @ FS.513 WL.73. FOUND TO BE OUT OF LIMITS.
- [SDR SWIA2020033049570](https://openairdocs.org/sdr/SWIA2020033049570), Feb 13, 2020: DOOR SILL. CRACKED. *FRAME FROM PAX DOOR UPPER SILL TO STGR 0 AT FS 333 IS CRACKED. (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED A NEW FRAME @ FS.333.00 FROM PAX DOOR UPPER SILL TO
- [SDR SWIA2020033049568](https://openairdocs.org/sdr/SWIA2020033049568), Feb 13, 2020: INTERCOSTAL. CORRODED. *CORROSION FOUND ON INTERCOSTAL AFT OF AVIONICS BAY DOOR ON R/H SIDE OF STGR27. (C CHECK) RO 3/27/2020 REMOVED AND REINSTALLED A NEW INTERCOSTAL AT STRG 27 RH F
- [SDR SWIA2020033049566](https://openairdocs.org/sdr/SWIA2020033049566), Feb 13, 2020: INTERCOSTAL. CORRODED. *CORROSION FOUND ON INTERCOSTAL AFT OF AVIONICS BAY DOOR ON L/H SIDE OF STGR27. (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED A NEW INTERCOSTAL AFT OF AVIONICS B
- [SDR SWIA2020033049563](https://openairdocs.org/sdr/SWIA2020033049563), Feb 13, 2020: STRINGER CLIP. CRACKED. FWD CABIN - APPROX.€¦ FS280.00 STGR 3 €“ STRINGER CLIP HAS SIGNS OF A CRACK AND WORKING RIVETS (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED A NEW FWD
- [SDR SWIA2020033049560](https://openairdocs.org/sdr/SWIA2020033049560), Feb 13, 2020: PANEL. CORRODED. THE RH FLOOR SILL PANEL HAS MULTIPLE LOCATIONS OF CORROSION FROM FS409.00+128 TO FS559.00. (MARKED) (C CHECK) RO 3/27/2020 BLENDED MULTIPLE AREAS OF CORROSION F
- [SDR SWIA2020033049559](https://openairdocs.org/sdr/SWIA2020033049559), Feb 13, 2020: NOT REPORTED. CORRODED. *FS559.00 STGR 26L €“ 26R HAS CORROSION ON FASTENERS AND AROUND THE FASTENERS(MARKED) (C CHECK) RO 3/27/2020 REPAIRED FS559.00 STR26L -26R REFERENCING REO. ALL
- [SDR SWIA2020033049556](https://openairdocs.org/sdr/SWIA2020033049556), Feb 13, 2020: FLOORBEAM. CORRODED. THE FLOORBEAM AT LBL9.00 FROM FS409.00 TO FS409.00+128 HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C CHECK) RO 3/27/2020 REMOVED CORROSION FROM FLOOR BEAM AT
- [SDR SWIA2020033149776](https://openairdocs.org/sdr/SWIA2020033149776), Feb 12, 2020: HINGE FITTING. GOUGED. *LH SPOILERON THIRD HINGE FITTING GOUGED ON THE OUTBD UPPER AFT EDGE (MARKED) (C CHECK) RO 3/27/2020 REMOVED GOUGE ON THE LH SPOILERON THIRD HINGE FITTING OUTBD
- [SDR SWIA2020033149747](https://openairdocs.org/sdr/SWIA2020033149747), Feb 12, 2020: SEAT TRACK. CHAFED. *NUMEROUS AREAS OF CHAFEING, FRETTING, AND CORROSION ON SEAT RAIL FROM FS409 TO FS409+128 AT RBL9 (C CHECK) RO 3/27/2020 REPLACED SEAT RAIL FROM FS409 TO FS409+
- [SDR SWIA2020033149746](https://openairdocs.org/sdr/SWIA2020033149746), Feb 12, 2020: SEAT TRACK. CHAFED. *NUMEROUS AREAS OF CHAFEING, FRETTING, AND CORROSION ON SEAT RAIL FROM FS364 TO FS409 AT RBL9. (C CHECK) RO 3/27/2020 BLENDED SEAT TRACK AT RBL 9.00 FROM FS 364
- [SDR SWIA2020033149745](https://openairdocs.org/sdr/SWIA2020033149745), Feb 12, 2020: FASTENER. CORRODED. *RH SPOILERON BOTH PCU, BOTTOM ATTACH HARDWARE CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE AT BOTTOM ATTACH POINT AT RH SPOILERO
- [SDR SWIA2020033149744](https://openairdocs.org/sdr/SWIA2020033149744), Feb 12, 2020: FASTENER. CORRODED. *RH FLIGHT SPOILER BOTH PCU, BOTTOM ATTACH HARDWARE CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE ON BOTTOM ATTACHING OINTS ON RH 
- [SDR SWIA2020033149743](https://openairdocs.org/sdr/SWIA2020033149743), Feb 12, 2020: NUT. CORRODED. *RH SPOILERON HINGES ATTACH HARDWARE NUTS CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND REPLACED THE HARDWARE WITH NEW ON THE RH SPOILERON HINGE ATTACH P
- [SDR SWIA2020033149742](https://openairdocs.org/sdr/SWIA2020033149742), Feb 12, 2020: NUT. CORRODED. *RH FLIGHT SPOILER HINGES ATTACH HARDWARE NUTS CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE ON RH FLIGHT SPOILER HINGES REF CRJ20
- [SDR SWIA2020033149741](https://openairdocs.org/sdr/SWIA2020033149741), Feb 12, 2020: NUT. CORRODED. *RH OUTBD GROUND SPOILER INBD/OUTBD HINGE ATTACH HARDWARE NUTS CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND REPLACED THE ATTACHING HARDWARE ON THE RIGHT
- [SDR SWIA2020033149740](https://openairdocs.org/sdr/SWIA2020033149740), Feb 12, 2020: NUT. CORRODED. *RH INBD GROUND SPOILER OUTBD HINGE ATTACH HARDWARE NUT CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND REPLACED HARDWARE OF THE RH INBOARD GROUND SPOILER 
- [SDR SWIA2020033149739](https://openairdocs.org/sdr/SWIA2020033149739), Feb 12, 2020: FASTENER. CORRODED. *LH SPOILERON BOTH PCU, BOTTOM ATTACH HARDWARE CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE ON LH INBOARD SPOILER PCU BOTTOM ATTA
- [SDR SWIA2020033149738](https://openairdocs.org/sdr/SWIA2020033149738), Feb 12, 2020: FASTENER. CORRODED. *LH FLIGHT SPOILER BOTH PCU, BOTTOM ATTACH HARDWARE CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE AT BOTTOM ATTACHING POINTS OF TH
- [SDR SWIA2020033149737](https://openairdocs.org/sdr/SWIA2020033149737), Feb 12, 2020: NUT. CORRODED. *LH SPOILERON HINGES ATTACH HARDWARE NUTS CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE (NUTS) ON LH SPOILERON END HINGES REF CRJ2
- [SDR SWIA2020033149736](https://openairdocs.org/sdr/SWIA2020033149736), Feb 12, 2020: NUT. CORRODED. *LH FLIGHT SPOILER HINGES ATTACH HARDWARE NUTS CORRODED (MARKED) (C CHECK) RO 3/27/2020 LEFT FLIGHT SPOILER CENTER HINGES HARDWARE REMOVED AND REPLACED WITH NEW
- [SDR SWIA2020033149735](https://openairdocs.org/sdr/SWIA2020033149735), Feb 12, 2020: NUT. CORRODED. *LH OUTBD GROUND SPOILER HINGES ATTACH HARDWARE NUTS CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE (NUTS) ON LH OUTBOARD GROUND SP
- [SDR SWIA2020033149734](https://openairdocs.org/sdr/SWIA2020033149734), Feb 12, 2020: NUT. CORRODED. *LH INBD GROUND SPOILER HINGES ATTACH HARDWARE NUTS CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE (NUTS) ON LH INBOARD GROUND SPOI
- [SDR SWIA2020033049554](https://openairdocs.org/sdr/SWIA2020033049554), Feb 12, 2020: FRAME. CORRODED. AFT CARGO APPROX.€¦ FS.574.00 LEFT HAND STGR 25 TO STGR 18 - FRAME HAS NUMEROUS SPOTS OF CORROSION (MARKED) (C CHECK) RO 3/27/2020 REPLACED AFT CARGO APPROX FS
- [SDR SWIA2020033049553](https://openairdocs.org/sdr/SWIA2020033049553), Feb 12, 2020: DOOR SILL. CORRODED. *R/H FLOOR SILL HAS 4EA AREAS OF CORROSION BETWEEN FS310 AND FS319.70. AREAS MARKED WITH RED GREASE PENCIL. (C CHECK) RO 3/27/2020 REMOVED AND REPLACE RH FLOOR 
- [SDR SWIA2020033049551](https://openairdocs.org/sdr/SWIA2020033049551), Feb 12, 2020: DOOR SILL. CORRODED. AFT CABIN APPROX. FS 559.00 TO 559.00 +96 RIGHT HAND FLOOR SILL BL 42.90 HAS NUMEROUS SPOTS OF CORROSION (MARKED) (C CHECK) RO 3/27/2020 REPLACED AFT CABIN APPR
- [SDR SWIA2020033049550](https://openairdocs.org/sdr/SWIA2020033049550), Feb 12, 2020: STRAP. CORRODED. AFT CABIN APPROX. FS 559.00 RIGHT HAND RBL 42.90 TO RBL27.00- INTERCOSTAL STRAP HAS SIGNS OF CORROSION (MARKED) (C CHECK) RO 3/27/2020 REPLACED AFT CABIN APPROX
- [SDR SWIA2020033049548](https://openairdocs.org/sdr/SWIA2020033049548), Feb 12, 2020: PLATE. CORRODED. THE PLATE UNDER THE TRANSMITTER ANTENNA NO.2 HAS CORROSION. (MARKED) (C CHECK) RO 3/27/2020 REMOVED CORROSION FROM PLATE UNDER TRANSMITTER ANTENNA #2 REF CRJ 20
- [SDR SWIA2020033149772](https://openairdocs.org/sdr/SWIA2020033149772), Feb 11, 2020: TRIM PANEL. CRACKED. CREW ESCAPE HATCH TRIM ASSY CRACKED IN SEVERAL AREAS (C CHECK) RO 3/27/2020 REPAIRED THE CREW ESCAPE HATCH TRIM ASSEMBLY USING PO# 24268 PER BOMBARDIER REO.

All 180: https://openairdocs.org/deregistered/N809CA-2023-11-03/reports.md

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