# N863AS: 2001 Bombardier CL-600-2B19, registration cancelled 2023-01-25

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 25, 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: 7487
- Year built: 2001
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 11, 2001
- Certificate issued: October 2, 2017
- Last registry action: October 1, 2020
- Mode S code: ABDA0D
- 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/N863AS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=863AS
- Page: https://openairdocs.org/deregistered/N863AS-2023-01-25

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 (168, newest 50)

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

- [SDR SWIA202265531](https://openairdocs.org/sdr/SWIA202265531), Apr 24, 2022: NONE. DELAMINATED. RH WINDOW DELAMINATION ON EDGE WITH VERTICAL LENGTH OF 8" AND HORIZONTAL LENGTH OF 4". (FLIGHT 5848 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITE
- [SDR SWIA202052767](https://openairdocs.org/sdr/SWIA202052767), Sep 23, 2020: HEAT SHIELD. CRACKED. APU HEAT SHIELD HAS A CRACK AT THE 6 O' POSITION. FILED CLOSED (9/23/2020). REMOVED AND REPLACED APU EXHAUST HEAT SHIELD, IN REF TO CRJ200 AMM.
- [SDR SWIA2020071451337](https://openairdocs.org/sdr/SWIA2020071451337), Jun 26, 2020: SEAT TRACK. CORRODED. CABIN FLOOR SEAT TRACK AT RBL9 FROM FS559.00+3-FS559.00+85 IS CORRODED. (C-CHECK) RO 7/10/2020 REMOVED CORROSION ON CABIN FLOOR SEAT TRACK AT RBL9 FROM FS559.00
- [SDR SWIA2020071451322](https://openairdocs.org/sdr/SWIA2020071451322), Jun 18, 2020: STRAP. CORRODED. EVIDENCE OF CORROSION FOUND ON STRAP AT FS 333, BETWEEN STR 25L AND 26L. (C-CHECK) RO 7/10/2020 REPAIRED DAMAGED AREA PER REO. LEAK CHECK GOOD. COMPLIED WITH TA
- [SDR SWIA2020071451321](https://openairdocs.org/sdr/SWIA2020071451321), Jun 18, 2020: SKIN. DENTED. FUSELAGE SKIN BETWEEN FS589-FS605, STR 21L-22L IS DENTED. (C-CHECK) RO 7/10/2020 DRESSED OUT DENT ON FUSELAGE SKIN BETWEEN FS589-FS605, STR 21L-22L REF REO. EVA
- [SDR SWIA2020071451320](https://openairdocs.org/sdr/SWIA2020071451320), Jun 18, 2020: SKIN. DENTED. FUSELAGE SKIN BETWEEN FS700-FS718, STR 14L-15L IS DENTED. (C-CHECK) RO 7/10/2020 HAND DRESSED DENTS (2EA) ON THE FUSELAGE SKIN BETWEEN FS700-FS718, STR 14L-15L 
- [SDR SWIA2020071451319](https://openairdocs.org/sdr/SWIA2020071451319), Jun 18, 2020: SKIN. DENTED. FUSELAGE SKIN BETWEEN FS589-FS605, STR 24R-26R IS DENTED. (C-CHECK) RO 7/10/2020 HAND DRESSED DENTS (3EA) LOCATED AT FUSELAGE SKIN BETWEEN FS589-FS605, STR 24R-
- [SDR SWIA2020071451318](https://openairdocs.org/sdr/SWIA2020071451318), Jun 15, 2020: FRAME. CHAFED. FRAME AT FS654.5 IS CHAFED THROUGH JUST FORWARD OF THE APU EXHAUST PORT. (C-CHECK) RO 7/10/2020 REPAIRED FRAME AT FS654.5 JUST FORWARD OF THE APU EXHAUST PORT R
- [SDR SWIA2020071451336](https://openairdocs.org/sdr/SWIA2020071451336), Jun 14, 2020: SEAT TRACK. CORRODED. SEAT TRACK AT FS 559+80 - FS 574.0 RBL 9 HAS CORROSION. (C-CHECK) RO 7/10/2020 REMOVED AND REPLACED CARGO TIE DOWN TRACKS AT FS559.00+80 - FS574.00 RBL 9 DUE TO
- [SDR SWIA2020071451335](https://openairdocs.org/sdr/SWIA2020071451335), Jun 14, 2020: SEAT TRACK. CORRODED. SMALL PIECE OF SEAT TRACK AT FS 559+112-FS 574.0 LBL 27 HAS CORROSION. (C-CHECK) RO 7/10/2020 FABRICATED NEW SEAT TRACK USING N126-2075, PO TX3728 PER REO.
- [SDR SWIA2020071451317](https://openairdocs.org/sdr/SWIA2020071451317), Jun 14, 2020: SEAT TRACK. CORRODED. SEAT TRACK CAP RBL 27 AT FS 559+112 TO JUST AFT OF FS 559.0 HAS CORROSION. (C-CHECK) RO 7/10/2020 REMOVED AND REPLACED SEAT TRACK CAP AT RBL27 FROM FS559.00-FS5
- [SDR SWIA2020071451316](https://openairdocs.org/sdr/SWIA2020071451316), Jun 14, 2020: SEAT TRACK. CORRODED. SEAT TRACK SUPPORT CAP RBL 9 JUST FWD OF FS 574.0 TO FS 621.0 HAS CORROSION. (C-CHECK) RO 7/10/2020 REMOVE CORROSION FROM SEAT TRACK SUPPORT CAP ON RBL 9 FWD OF
- [SDR SWIA2020071451315](https://openairdocs.org/sdr/SWIA2020071451315), Jun 14, 2020: SEAT TRACK. CORRODED. SEAT TRACK SUPPORT CAP FROM FS 559.0 TO FS 574.0 RBL 9 HAS CORROSION. (C-CHECK) RO 7/10/2020. REMOVED AND REPLACED SEAT TRACK SUPPORT CAP FROM FS559.00 TO FS574
- [SDR SWIA2020071451314](https://openairdocs.org/sdr/SWIA2020071451314), Jun 13, 2020: DOOR SILL. CORRODED. CORROSION ON LEFT HAND FLOOR SILL AT FS 349. (C-CHECK) RO 7/10/2020 REPAIRED LT FLOOR SILL AT FS 349 REF REO. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA2020071451313](https://openairdocs.org/sdr/SWIA2020071451313), Jun 12, 2020: PANEL. CORRODED. RT PRESSURE FLOOR SILL PANEL HAS SEVERAL AREA OF CORROSION BETWEEN FS 499 AND FS 559. (C-CHECK) RO 7/10/2020 REPAIRED THE RT PRESSURE FLOOR SILL PANEL BETWEEN F
- [SDR SWIA2020071451312](https://openairdocs.org/sdr/SWIA2020071451312), Jun 12, 2020: STRAP. CORRODED. STRAP AT FS 559 HAS CORROSION BETWEEN APPROXIMATE LBL33 AND LBL44. (C-CHECK) RO 7/10/2020 BLENDED CORROSION, REF SRM. NDT MEASURED THICKNESS AND FOUND PART TO B
- [SDR SWIA2020071451311](https://openairdocs.org/sdr/SWIA2020071451311), Jun 12, 2020: PANEL. CORRODED. LT PRESSURE FLOOR SILL PANEL HAS SEVERAL AREA OF CORROSION BETWEEN FS 409+112 AND FS 559. (C-CHECK) RO 7/10/2020 REPAIRED THE LT PRESSURE FLOOR SILL PANEL BETWE
- [SDR SWIA2020071451310](https://openairdocs.org/sdr/SWIA2020071451310), Jun 12, 2020: INTERCOSTAL. CORRODED. THE PAX DOOR INTERCOSTAL DD5 AFT HAS CORROSION. (C-CHECK) RO 7/10/2020 REMOVED THE CORROSION FROM THE PAX DOOR INTERCOSTAL AFT DD5 REF SRM. BLENDED AREA FOUND T
- [SDR SWIA2020071451309](https://openairdocs.org/sdr/SWIA2020071451309), Jun 11, 2020: HINGE BRACKET. CHAFED. RUDDER LOWER CENTER HINGE BRACKET ON VERTICAL STABILIZER IS CHAFED ON TOP SURFACE JUST FORWARD OF THE SPHERICAL BEARING. (C-CHECK) RO 7/10/2020 BLENDED CHAFE ON
- [SDR SWIA2020071451308](https://openairdocs.org/sdr/SWIA2020071451308), Jun 11, 2020: HINGE BRACKET. CHAFED. RUDDER UPPER CENTER HINGE BRACKET ON VERTICAL STABILIZER IS CHAFED ON TOP SURFACE JUST FORWARD OF THE SPHERICAL BEARING. (C-CHECK) RO 7/10/2020 BLENDED CHAFE ON
- [SDR SWIA2020071451307](https://openairdocs.org/sdr/SWIA2020071451307), Jun 10, 2020: RETAINER. CORRODED. UPON PROVIDED ACCES TO TREATMANT OF CORROSION DAMAGE ON SERVICE DOOR SEAL LWR AFT CORNER RETAINER FOUND CORROSION DAMAGE AT DOOR FRAME LWR AFT PAN SECTION. (C-C
- [SDR SWIA2020071451306](https://openairdocs.org/sdr/SWIA2020071451306), Jun 10, 2020: FITTING. CRACKED. CLIP AT STR14R, FS621-FS625, IS CRACKED. (C-CHECK) RO 7/10/2020 REMOVED AND INSTALLED NEW CLIP AT STGR 14R BETWEEN FS621 AND FS625 REF SRM AND REO. SEE CONTINUA
- [SDR SWIA2020071451305](https://openairdocs.org/sdr/SWIA2020071451305), Jun 10, 2020: FITTING. CRACKED. CLIP AT STR14L, FS621-FS625, IS CRACKED. (C-CHECK) RO 7/10/2020 REMOVED AND INSTALLED NEW CLIP AT STGR 14L BETWEEN FS621 AND FS625 REF CSRM AND REO. SEE CONTINU
- [SDR SWIA2020071451304](https://openairdocs.org/sdr/SWIA2020071451304), Jun 10, 2020: INTERCOSTAL. CRACKED. INTERCOSTAL / CLIP COMMON TO THE SKIN AT STR14L, FS621-FS625, IS CRACKED. (C-CHECK) RO 7/10/2020 REMOVED AND INSTALLED CLIP/INTERCOSTAL COMMON TO THE OUTER SKIN
- [SDR SWIA2020071451325](https://openairdocs.org/sdr/SWIA2020071451325), Jun 9, 2020: STOP FITTING. CRACKED. PASSENGER DOOR PULL-IN LEVER TORQUE TUBE STOP FITTING CORRODED AND APPEARS CRACKED. (C-CHECK) RO 7/10/2020 REPLACED PASSENGER DOOR LOWER TORQUE TUBE STOP FITTIN
- [SDR SWIA2020071451324](https://openairdocs.org/sdr/SWIA2020071451324), Jun 9, 2020: BRACKET. CRACKED. PASSENGER DOOR SUPPORT WHEEL SYSTEM CABLE BRACKET AT BOTTOM OF STAIRS APPEARS CRACKED. (C-CHECK) RO 7/10/2020 REMOVED CRACKED SUPPORT WHEEL CABLE BRACKET ASSY O
- [SDR SWIA2020071451323](https://openairdocs.org/sdr/SWIA2020071451323), Jun 9, 2020: DRAG ANGLE. CRACKED. PASSENGER DOOR SUSPECT CRACK AT THE AFT STAIR DRAG ANGLE. (C-CHECK) RO 7/10/2020 REPLACED THE CRACKED AFT STAIR DRAG ANGLE REF SRM.
- [SDR SWIA2020071451303](https://openairdocs.org/sdr/SWIA2020071451303), Jun 9, 2020: INTERCOSTAL. CRACKED. CLIP COMMON TO THE SKIN AT STR13L, FS621-FS625, IS CRACKED. (C-CHECK) RO 7/10/2020 REMOVED AND INSTALLED CLIP/INTERCOSTAL COMMON TO THE OUTER SKIN AT STR13L BET
- [SDR SWIA2020071451302](https://openairdocs.org/sdr/SWIA2020071451302), Jun 9, 2020: FORMER. CORRODED. PASSENGER DOOR FORMER AT FS329.50 BETWEEN DD5 AND DD4 CORRODED. (C-CHECK) RO 7/10/2020 REMOVED THE CORROSION FROM THE PAX DOOR FORMER AT FS329.50 BETWEEN INTERC
- [SDR SWIA2020071451301](https://openairdocs.org/sdr/SWIA2020071451301), Jun 9, 2020: INTERCOSTAL. CORRODED. PASSENGER DOOR MIDDLE INTERCOSTAL AT DD2 CORRODED. (C-CHECK) RO 7/10/2020 REMOVED THE CORROSION FROM THE PAX DOOR INTERCOSTAL MID DD2 REF SRM. BLENDED AREA FOUN
- [SDR SWIA2020071451300](https://openairdocs.org/sdr/SWIA2020071451300), Jun 9, 2020: INTERCOSTAL. CORRODED. PASSENGER DOOR MIDDLE INTERCOSTAL AT DD3 CORRODED. (C-CHECK) RO 7/10/2020 REMOVED THE CORROSION FROM THE PAX DOOR INTERCOSTAL MID DD3 REF SRM. BLENDED AREA FOUN
- [SDR SWIA2020071451299](https://openairdocs.org/sdr/SWIA2020071451299), Jun 9, 2020: INTERCOSTAL. CORRODED. PASSENGER DOOR MIDDLE INTERCOSTAL AT DD4 CORRODED. (C-CHECK) RO 7/10/2020 REMOVED THE CORROSION FROM THE PAX DOOR INTERCOSTAL MID DD4 REF SRM. BLENDED AREA FOUN
- [SDR SWIA2020071451298](https://openairdocs.org/sdr/SWIA2020071451298), Jun 9, 2020: INTERCOSTAL. CORRODED. PASSENGER DOOR AFT INTERCOSTAL AT DD4 CORRODED. (C-CHECK) RO 7/10/2020 REMOVED THE CORROSION FROM THE PAX DOOR INTERCOSTAL AFT DD4 REF SRM. BLENDED AREA FOUND T
- [SDR SWIA2020071451297](https://openairdocs.org/sdr/SWIA2020071451297), Jun 9, 2020: INTERCOSTAL. CORRODED. PASSENGER DOOR CLIP FOR FWD INTERCOSTAL AT DD6, AND AT APPROX FS320 CORRODED. (C-CHECK) RO 7/10/2020 REMOVED AND INSTALLED NEW PAX DOOR CLIP / CLEAT COMMON TO I
- [SDR SWIA2020071451334](https://openairdocs.org/sdr/SWIA2020071451334), Jun 8, 2020: SKIN. CORRODED. EXTERNAL SKIN IS CORRODED AT APPROX FS559+96-559+112, STR26L-26R. (C-CHECK) RO 7/10/2020 BLENDED CORROSION, REF SRM 51-21-06. FOUND TO BE OUT OF LIMITS. NO ALLO
- [SDR SWIA2020071451333](https://openairdocs.org/sdr/SWIA2020071451333), Jun 8, 2020: SKIN. CORRODED. EXTERNAL SKIN IS CORRODED AT APPROX FS559+44, STR25L-25R. (C-CHECK) RO 7/10/2020 BLENDED CORROSION ON EXTERNAL SKIN AT FS 559+44 BETWEEN STR 25L-25R REF SRM. BL
- [SDR SWIA2020071451332](https://openairdocs.org/sdr/SWIA2020071451332), Jun 8, 2020: FASTENER. CORRODED. RT INBOARD GROUND SPOILER ACTUATOR LINK HAS CORRODED HARDWARE. (C-CHECK) RO 7/10/2020 REMOVED AND REPLACED THE RT INBD GROUND SPOILER ACTUATOR LINK HARDWARE REF
- [SDR SWIA2020071451331](https://openairdocs.org/sdr/SWIA2020071451331), Jun 8, 2020: FASTENER. CORRODED. RT OUTBOARD GROUND SPOILER ACTUATOR LINK HAS CORRODED HARDWARE. (C-CHECK) RO 7/10/2020 REMOVED AND REPLACED RT OTBD GROUND SPOILER LINK HARDWARE REF AMM. ALL CH
- [SDR SWIA2020071451330](https://openairdocs.org/sdr/SWIA2020071451330), Jun 8, 2020: FASTENER. CORRODED. LT INBOARD GROUND SPOILER ACTUATOR LINK HAS CORRODED HARDWARE. (C-CHECK) RO 7/10/2020 REMOVED AND REPLACED LT I/B GROUND SPOILER ACTUATOR LINK HARDWARE IAW AMM.
- [SDR SWIA2020071451329](https://openairdocs.org/sdr/SWIA2020071451329), Jun 8, 2020: FLOOR SUPPORT. CORRODED. SERVICE DOOR SURROUND STRUCTURE: UPPER FLOOR SUPPORT ANGLE HAS CORROSION. (C-CHECK) RO 7/10/2020 REMOVED 2 EACH SOLID FASTENERS WITH CORROSION AT THE SERVICE DO
- [SDR SWIA2020071451327](https://openairdocs.org/sdr/SWIA2020071451327), Jun 8, 2020: PLATE. CORRODED. PASSENGER DOOR SURROUND STRUCTURE: AFT ANCHOR, SERRATED MOUNTING PLATE HAS CORROSION ON ITS OUTBOARD SIDE. (C-CHECK) RO 7/10/2020 REMOVED DAMAGED SERRATED MOUNT
- [SDR SWIA2020071451296](https://openairdocs.org/sdr/SWIA2020071451296), Jun 8, 2020: SKIN. CORRODED. EXTERNAL SKIN IS CORRODED AT APPROX FS559+34, STR26L. (C-CHECK) RO 7/10/2020 BLENDED CORROSION, REF SRM 51-21-06. FOUND REMAINING MATERIAL TO BE OUT OF LIMITS, 
- [SDR SWIA2020071451295](https://openairdocs.org/sdr/SWIA2020071451295), Jun 8, 2020: FLOOR SUPPORT. CORRODED. PASSENGER DOOR SURROUND STRUCTURE: LOWER FLOOR SUPPORT ANGLE HAS CORROSION AROUND FASTENERS. (C-CHECK) RO 7/10/2020 REMOVED CORROSION FROM PAX DOOR FLOOR SUPPOR
- [SDR SWIA2020071451294](https://openairdocs.org/sdr/SWIA2020071451294), Jun 8, 2020: RETAINER. CORRODED. SERVICE DOOR: LOWER SEAL RETAINER IS CORRODED. (C-CHECK) RO 7/10/2020 REMOVED CORROSION DAMAGE FROM SERVICE DOOR SILL LWR AFT CORNER RETAINER REF SRM. BLENDED A
- [SDR SWIA2020071451293](https://openairdocs.org/sdr/SWIA2020071451293), Jun 8, 2020: ANGLE. CORRODED. SERVICE DOOR INTERNAL STRUCTURE: CLIP INSIDE LIGHTENING CUT-OUT JUST AFT OF THE INNER HANDLE ACCESS AREA HAS CORROSION. (C-CHECK) RO 7/10/2020 BLENDED CORROSION
- [SDR SWIA2020071451292](https://openairdocs.org/sdr/SWIA2020071451292), Jun 8, 2020: SKIN. GOUGED. CARGO DOOR INTERNAL STRUCTURE: HAS LIGHT GOUGING, AND SOME CORROSION, ON THE RIVET TAILS AND STRUCTURE BELOW THE HANDLE MECHANISM. (C-CHECK) RO 7/10/2020 ORDER 
- [SDR SWIA2020071451291](https://openairdocs.org/sdr/SWIA2020071451291), Jun 7, 2020: SKIN. DENTED. LEFT WING, LOWER WING PLANK, INBD OF WS50 AND FORWARD OF THE WING TANK ACCESS HOLES, APPEARS TO BE DENTED. (C-CHECK) RO 7/10/2020 REPAIRED LT LOWER WING PLANK I
- [SDR SWIA2019050145817](https://openairdocs.org/sdr/SWIA2019050145817), May 1, 2019: UPLOCK ROLLER. FAILED. GEAR DISAGREE NOSE GEAR DID NOT GO DOWN. CYCLED GEAR HANDLE PER QRH AND ALL GEAR DOWN AND LOCKED. (FLT#5529) FO: 05/01/2019 CLOSED REMOVED AND REPLACED NLG UPLO
- [SDR SWIA2019050145818](https://openairdocs.org/sdr/SWIA2019050145818), May 1, 2019: UPLOCK ROLLER. SLOW. EXTENDED GEAR AT 180 KTS, RECEIVED GEAR DISAGREE WARNING MESSAGE. AFTER ABOUT 20 SECONDS, THE GEAR INDICATED DOWN BEFORE WE COULD EVEN START THE QRH PROCEDURE. 
- [SDR SWIA2019040545663](https://openairdocs.org/sdr/SWIA2019040545663), Mar 23, 2019: LINE. LEAKING. ENGINE TWO LOW OIL PRESSURE IN FLIGHT. ENGINE SHUT DOWN IN FLIGHT ACCOMPLISHED. (FLT#5223) REMOVED AND REPLACED OIL SUPPLY LINE IAW AMM. NO LEAKS NOTED AFTER EN

All 168: https://openairdocs.org/deregistered/N863AS-2023-01-25/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 20101118055169I](https://openairdocs.org/incident/20101118055169I), Nov 18, 2010: Bombardier CL-600-2B19 (N863AS), Mnneapolis, MN, Substantial damage. On climb out from msp at 300 feet AGL struck a bird with right wing resulting in wing leading edge damage. Aircraft returned and landed. Pilot was warned of…
- [Incident 20021103036619I](https://openairdocs.org/incident/20021103036619I), Nov 3, 2002: Cndair CL6002B19 (N863AS), Evansville, IN. (-23) On 11/03/02 asoa flight 4156 advised of smoke in the aft cabin after turning on the APU bleed air. Declared an emergency. The aircraft landed without…

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