# N907SW: 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: 7511
- Year built: 2001
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 22, 2001
- Certificate issued: November 17, 2017
- Last registry action: August 20, 2020
- Mode S code: AC8AD2
- 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/N907SW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=907SW
- Page: https://openairdocs.org/deregistered/N907SW-2023-03-08

From the FAA registry file of October 28, 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 (159, newest 50)

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

- [SDR SWIA202159606](https://openairdocs.org/sdr/SWIA202159606), Jul 19, 2021: ENGINE. UNCONTROLLABLE. LEFT ENGINE DID NOT RESPOND TO THRUST LEVER MOVEMENT. LEFT ENGINE APR FIRED. EVEN IN SHUTOFF POSITION ENGINE STILL WAS RUNNING. RAN SEVERE ENGINE DAMAGE IN FLIG
- [SDR SWIA202054338](https://openairdocs.org/sdr/SWIA202054338), Nov 12, 2020: BRACKET. CRACKED. CARGO COMPARTMENT FWD CARGO DOOR TRACK LOWER U CHANNEL ATTACH BRACKET CRACKED, MARKED. C-CHECK RO 11/23/2020. REMOVED AND INSTALLED NEW FWD CARGO DOOR TRACK LOW
- [SDR SWIA202054339](https://openairdocs.org/sdr/SWIA202054339), Nov 11, 2020: FRAME. CORRODED. FS 589.0 FRAME AT STR 26L TO AT 26R HAS CORROSION ON FWD SIDE. C-CHECK RO 11/23/2020. REMOVED CORROSION ON FS 589 FRAME AT STGR 26L TO STGR 26R, REF CRJ200 SRM,
- [SDR SWIA202054337](https://openairdocs.org/sdr/SWIA202054337), Nov 11, 2020: ANGLE. CRACKED. RT 280 CROSSBEAM CLIPS ARE CRACKED AROUND RBL 9 FLOORBEAM. C-CHECK RO 11/23/2020. REMOVED AND INSTALLED NEW RT 280 CROSSBEAM CLIPS AT RBL 9 FLOORBEAM, REF CRJ20
- [SDR SWIA202054336](https://openairdocs.org/sdr/SWIA202054336), Nov 11, 2020: ANGLE. CRACKED. LT 280 CROSSBEAM CLIPS ARE CRACKED AROUND LBL 9 FLOORBEAM. C-CHECK RO 11/23/2020. REMOVED AND INSTALLED NEW LT 280 CROSSBEAM CLIPS AT LBL 9 FLOORBEAM, REF CRJ20
- [SDR SWIA202054335](https://openairdocs.org/sdr/SWIA202054335), Nov 11, 2020: STRAP. CORRODED. LT TOP STRAP AT FS 559.0 FROM LBL 27 TO SILL HAS CORROSION. C-CHECK RO 11/23/2020. REMOVED CORROSION AT LT TOP STRAP AT FS 559.00 LBL 27 TO SILL, REF CRJ200 SRM
- [SDR SWIA202054342](https://openairdocs.org/sdr/SWIA202054342), Nov 9, 2020: RIVET. GOUGED. FS 621 BULKHEAD FWD SIDE HAS 4 GOUGES RIVET HEADS AT APPROXIMATELY WL 87 & RBL 9, RBL 18, RBL 27, RBL 36, MARKED. C-CHECK RO 11/23/2020. REMOVED AND INSTALLED N
- [SDR SWIA202054341](https://openairdocs.org/sdr/SWIA202054341), Nov 9, 2020: ISOLATOR. LOOSE. FS 621 BULKHEAD FWD SIDE HAS 3 ISOLATORS LOOSE, MARKED. C-CHECK RO 11/23/2020. REPLACED 6 EA SOLID RIVETS ON FS 621 BULKHEAD FWD SIDE HAS 3 ISOLATORS, REF CRJ20
- [SDR SWIA202054340](https://openairdocs.org/sdr/SWIA202054340), Nov 9, 2020: ISOLATOR. BENT. FS 621 BULKHEAD FWD SIDE HAS 14 ISOLATOR BRACKETS BENT/DEFORMED, MARKED. C-CHECK RO 11/23/2020. REMOVED AND REPLACED 14 EA ISOLATOR BRACKET ASSEMBLY FROM FWD SI
- [SDR SWIA202054334](https://openairdocs.org/sdr/SWIA202054334), Nov 9, 2020: SKIN. CORRODED. WING PLANK LAND AT 610AB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON RT WING PLANK LAND AT 610AB, REF REO, FOUND TO BE WITHIN LI
- [SDR SWIA202054333](https://openairdocs.org/sdr/SWIA202054333), Nov 9, 2020: SKIN. CORRODED. WING PLANK LAND AT 640BB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON RT WING PLANK LAND AT 640BB, REF REO, FOUND TO BE WITHIN LI
- [SDR SWIA202054332](https://openairdocs.org/sdr/SWIA202054332), Nov 9, 2020: SKIN. CORRODED. WING PLANK LAND AT 640CB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON RT WING PLANK LAND AT 640CB, REF REO, FOUND TO BE WITHIN LI
- [SDR SWIA202054331](https://openairdocs.org/sdr/SWIA202054331), Nov 9, 2020: SKIN. CORRODED. WING PLANK LAND AT 640EB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON RT WING PLANK LAND AT 640EB, REF REO, FOUND TO BE WITHIN LI
- [SDR SWIA202054330](https://openairdocs.org/sdr/SWIA202054330), Nov 9, 2020: SKIN. CORRODED. WING PLANK LAND AT 650AB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON RT WING PLANK LAND AT 650AB, REF REO, FOUND TO BE WITHIN LI
- [SDR SWIA202054329](https://openairdocs.org/sdr/SWIA202054329), Nov 9, 2020: SKIN. CORRODED. WING PLANK LAND AT 650BB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON RT WING PLANK LAND AT 650BB, REF REO, FOUND TO BE WITHIN LI
- [SDR SWIA202054328](https://openairdocs.org/sdr/SWIA202054328), Nov 9, 2020: SKIN. CORRODED. WING PLANK LAND AT 510AB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 510AB, REF REO, FOUND TO BE WITH IN L
- [SDR SWIA202054327](https://openairdocs.org/sdr/SWIA202054327), Nov 9, 2020: SKIN. CORRODED. WING PLANK LAND AT 510BB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 510BB, REF REO. FOUND TO BE WITH IN L
- [SDR SWIA202054326](https://openairdocs.org/sdr/SWIA202054326), Nov 9, 2020: SKIN. CORRODED. WING PLANK LAND AT 540AB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 540AB, REF REO, FOUND TO BE WITHIN LI
- [SDR SWIA202054325](https://openairdocs.org/sdr/SWIA202054325), Nov 9, 2020: SKIN. CORRODED. WING PLANK LAND AT 540BB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 540BB, REF REO, FOUND TO BE WITH IN L
- [SDR SWIA202054324](https://openairdocs.org/sdr/SWIA202054324), Nov 9, 2020: SKIN. CORRODED. WING PLANK LAND AT 540CB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 540CB, REF REO, FOUND TO BE WITHIN LI
- [SDR SWIA202054323](https://openairdocs.org/sdr/SWIA202054323), Nov 9, 2020: SKIN. CORRODED. WING PLANK LAND AT 540DB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 540DB, REF REO, FOUND TO BE WITHIN LI
- [SDR SWIA202054322](https://openairdocs.org/sdr/SWIA202054322), Nov 9, 2020: SKIN. CORRODED. WING PLANK LAND AT 540EB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 540EB, REF REO, FOUND TO BE WITHIN LI
- [SDR SWIA202054321](https://openairdocs.org/sdr/SWIA202054321), Nov 9, 2020: SKIN. CORRODED. WING PLANK LAND AT 540FB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 540FB, REF REO, FOUND TO BE WITHIN LI
- [SDR SWIA202054320](https://openairdocs.org/sdr/SWIA202054320), Nov 9, 2020: SKIN. CORRODED. WING PLANK LAND AT 550AB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 550AB, REF REO, FOUND TO BE WITHIN LI
- [SDR SWIA202054319](https://openairdocs.org/sdr/SWIA202054319), Nov 9, 2020: SKIN. CORRODED. WING PLANK LAND AT 550CB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 550CB, REF REO, FOUND TO BE WITHIN LI
- [SDR SWIA202054318](https://openairdocs.org/sdr/SWIA202054318), Nov 9, 2020: SKIN. CORRODED. WING PLANK LAND AT 550DB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 550DB, REF REO, FOUND TO BE WITHIN LI
- [SDR SWIA202054317](https://openairdocs.org/sdr/SWIA202054317), Nov 9, 2020: SKIN. CORRODED. WING PLANK LAND AT 550EB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 550EB, REF REO, FOUND TO BE WITH IN L
- [SDR SWIA202054316](https://openairdocs.org/sdr/SWIA202054316), Nov 9, 2020: SKIN. CORRODED. WING PLANK LAND AT 550FB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 550FB, REF REO. FOUND TO BE WITHIN LI
- [SDR SWIA202054315](https://openairdocs.org/sdr/SWIA202054315), Nov 9, 2020: SKIN. CORRODED. WING PLANK LAND AT 550HB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 550HB, REF REO. FOUND TO BE WITH IN L
- [SDR SWIA202054314](https://openairdocs.org/sdr/SWIA202054314), Nov 9, 2020: BULKHEAD. GOUGED. FS 621 BULKHEAD FWD SIDE HAS 3 GOUGES AT APPROXIMATELY WL 103 & RBL 18, RBL 27, RBL 36, MARKED. C-CHECK RO 11/23/2020. BLENDED OUT DAMAGE TO A SMOOTH SURFACE AT
- [SDR SWIA202054343](https://openairdocs.org/sdr/SWIA202054343), Nov 7, 2020: VANE. CHAFED. LT INBOARD FLAP VANE TRAILING EDGE MID UPPER SIDE HAS CHAFING DAMAGE. C-CHECK RO 11/23/2020. REMOVED THE CHAFE DAMAGE FROM THE LT INBOARD FLAP VANE UPPER TRAILI
- [SDR SWIA202054313](https://openairdocs.org/sdr/SWIA202054313), Nov 7, 2020: VANE. CHAFED. RT INBOARD FLAP VANE LEADING EDGE INBOARD SIDE HAS CHAFING DAMAGE. C-CHECK RO 11/23/2020. REMOVED CHAFE DAMAGE FROM RT INBOARD FLAP VANE LEADING EDGE, INBOARD S
- [SDR SWIA202054312](https://openairdocs.org/sdr/SWIA202054312), Nov 7, 2020: VANE. CHAFED. LT INBOARD FLAP VANE LEADING EDGE OUTBOARD SIDE HAS CHAFING DAMAGE. C-CHECK RO 11/23/2020. REMOVED CHAFE DAMAGE ON LT INBOARD FLAP VANE LEADING EDGE OUTBOARD SI
- [SDR SWIA2019012945470](https://openairdocs.org/sdr/SWIA2019012945470), Dec 23, 2018: STIFFENER. CHAFED. THE REAR PRESSURE BULKHEAD, VERTICAL STIFFENER AT THE CENTER, IS CHAFED IN THE UPPER PORTION OF ITS HEIGHT, ON THE AFT LEG SURFACE AND AFT CORNER. (C-CHECK) RO:
- [SDR SWIA201845472](https://openairdocs.org/sdr/SWIA201845472), Dec 18, 2018: FLOOR SKIN. DENTED. PRESSURE FLOOR SKIN DENT FS516 RBL13. (C-CHECK) RO:01/25/2019 PRESSURE FLOOR SKIN DENT AT FS516 RBL13 IAW REO.
- [SDR SWIA2019012945463](https://openairdocs.org/sdr/SWIA2019012945463), Dec 18, 2018: FLOOR SKIN. DENTED. PRESSURE FLOOR SKIN DENT FS501 RBL15 (C-CHECK) RO:01/25/2019 REPAIRED DENT IAW SRM.
- [SDR SWIA2019012945468](https://openairdocs.org/sdr/SWIA2019012945468), Dec 17, 2018: BUTTSTRAP. CORRODED. FLOOR BUTTSTRAP AT FS559.00 FROM LBL27-LBL43 HAS EXFOILIATED CORROSION. (C-CHECK) RO:01/25/2019 REPAIRED FLOOR BUTTSTRAP AT FS559.00 FROM LBL27-LBL43 IAW REO.
- [SDR SWIA2019012945467](https://openairdocs.org/sdr/SWIA2019012945467), Dec 16, 2018: STRAP. CORRODED. RT SIDE STRAP AT FS559.00 BETWEEN RBL 27.0 TO RBL 41.75 IS CORRODED. (C-CHECK) RO:01/25/2019 REPAIRED RT SIDE STRAP AT FS 559.00 BETWEEN RBL 27.0 TO RBL 41.75 I
- [SDR SWIA2019012945469](https://openairdocs.org/sdr/SWIA2019012945469), Dec 15, 2018: FLOORBEAM. CORRODED. FLOORBEAM CAP - INBOARD AND OUTBOARD FLANGES ARE CORRODED AROUND THE FASTENER HOLES. LBL27, FS569.5 €“ FS621.00. (C-CHECK) RO:01/25/2019 REMOVED AND REPLACED F
- [SDR SWIA2019012945466](https://openairdocs.org/sdr/SWIA2019012945466), Dec 15, 2018: FRAME. CORRODED. SEVERAL AREAS OF CORROSION ON FRAME AT FS589 BETWEEN STRG 21L AND 23L. (C-CHECK) RO:01/25/2019 REPAIRED DAMAGED AREA OF FRAME AT FS589 BETWEEN STR 21L AND STR 2
- [SDR SWIA2019012945474](https://openairdocs.org/sdr/SWIA2019012945474), Dec 14, 2018: DOOR SILL. CORRODED. LT PRESSURE FLOOR SILL HAS CORROSION IN MULTIPLE PLACES BETWEEN FS 409+128 €“ FS 559 (C-CHECK) RO:01/25/2019 REMOVED CORROSION FROM LT PRESSURE FLOOR SILL IN M
- [SDR SWIA2019012945471](https://openairdocs.org/sdr/SWIA2019012945471), Dec 14, 2018: FLOORBEAM. CORRODED. RBL 9 FLOORBEAM FS 409.00+48 TO 409.00 +112 APPROX. HAS CORROSION. (C-CHECK) RO:01/25/2019 REPAIRED RBL 9 FLOORBEAM AT FS409.00+48 TO FS409+112 IAW REO.
- [SDR SWIA2019012945462](https://openairdocs.org/sdr/SWIA2019012945462), Dec 8, 2018: VANE. DAMAGED. REPLACE LT INBOARD FLAP CENTER VANE CAP. (C-CHECK) RO:01/25/2019 REPLACED LT IB FLAP CENTER VANE CAP WITH NEW P/N 601R14303-51 IAW REO.
- [SDR SWIA2019012945473](https://openairdocs.org/sdr/SWIA2019012945473), Dec 5, 2018: HINGE. SCRATCHED. PAX DOOR HINGE FUSELAGE SIDE HAS MULTIBLE SCRATCH'S AND NICKS. (C-CHECK) RO:01/25/2019 / REMOVED AND REPLACED WITH NEW FUSELAGE SIDE PAX DOOR HINGE IAW REO.
- [SDR SWIA2019012945465](https://openairdocs.org/sdr/SWIA2019012945465), Dec 5, 2018: PANEL. CHAFED. LEFT HAND AILERON LOWER FIXED LEADING EDGE PANELS HAVE CHAFES. (C-CHECK) RO:01/25/2019 LT AILERON INBD LEADING EDGE PANEL REMOVED AND REPLACED WITH NEW PANEL (P
- [SDR SWIA2019012945464](https://openairdocs.org/sdr/SWIA2019012945464), Dec 3, 2018: STRAP. CORRODED. STRAP AT FS349.00 STR 3L HAS CORROSION AT MULTIPLE PLACES. (C-CHECK) RO:01/25/2019REMOVED AND INSTALLED NEW STRAP AT FS349.00 STGR 3L IAW SRM.
- [SDR SWIA201743181](https://openairdocs.org/sdr/SWIA201743181), Apr 4, 2017: SKIN. DENTED. LEFT SIDE OF FUSELAGE SKIN HAS A DENT BETWEEN BS 605 AND 621, STRINGERS 21 - 22L. PERFORMED PERMANENT REPAIR IAW REO AND SRM.
- [SDR SWIA201440415](https://openairdocs.org/sdr/SWIA201440415), Dec 12, 2014: VANE. UNSECURE. RIGHT RAM AIR EXHAUST DUCT VANE IS MISSING ADHESIVE, C-CHECK, RO 12/13/14, CLEANED AND REAPPLIED ADHESIVE TO RT RAM AIR EXHAUST DUCT VANE IAW REO.
- [SDR SWIA201440411](https://openairdocs.org/sdr/SWIA201440411), Dec 12, 2014: VANE. UNSECURE. LEFT RAM AIR EXHAUST DUCT VANE IS MISSING ADHESIVE. CLEANED AND REAPPLIED ADHESIVE TO LT RAM AIR EXHAUST DUCT VANE IAW REO.
- [SDR SWIA201440403](https://openairdocs.org/sdr/SWIA201440403), Dec 9, 2014: NUT. UNSECURE. CO-PILOTS AILERON CONTROL COLUMN HAS CLICKING. RETORQUED COPILOTS CONTROL COLUMN NUT ON FWD SIDE OF THE CONTROL WHEEL SHAFT REF REO AND AMM.

All 159: https://openairdocs.org/deregistered/N907SW-2023-03-08/reports.md

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20080219833119I](https://openairdocs.org/incident/20080219833119I), Feb 19, 2008: Cndair CL6002B19 (N907SW), Peoria, IL, No damage. (-23) The aircraft departed pia (Peoria, IL) for ord (chicago, IL) and returned to pia due to a nose wheel steering indication disagree annunciation. The crew…
- [Incident 20080218833109I](https://openairdocs.org/incident/20080218833109I), Feb 18, 2008: Cndair CL6002B19 (N907SW), Springfield, IL, No damage. (-23) The aircraft departed spi (Springfield, IL) for ord (chicago, IL) and returned to spi due to a nose wheel steering indication disagree annunciation. The…

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