# N866AS: 2001 Bombardier CL-600-2B19, registration cancelled 2023-07-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 30, 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: 7517
- Year built: 2001
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 24, 2001
- Certificate issued: October 2, 2017
- Last registry action: March 24, 2023
- Mode S code: ABE532
- 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/N866AS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=866AS
- Page: https://openairdocs.org/deregistered/N866AS-2023-07-30

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 (165, newest 50)

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

- [SDR SWIA2019111246758](https://openairdocs.org/sdr/SWIA2019111246758), Nov 12, 2019: PRESSURE SWITCH. FAILED. ABORTED TAKE OFF. LOW FUEL PRESSURE CAUTION MSG. FLT OR GROUND SPOILER MASTER CAUTION WARNING. BRAKE TEMPS LEFT 3/2 RIGHT 3/2. BELOW 80 KIAS. FLIGHT # 5037 CLOS
- [SDR SWIA2018111345262](https://openairdocs.org/sdr/SWIA2018111345262), Oct 20, 2018: FRAME. CORRODED. FS589.00, STGR27 AND STGR26R €“ FRAME SHOWS SIGNS OF CORROSION ON THE FWD SIDE. (C-CHECK) RO: 11/12/2018REPLACED CORRODED FRAME SECTION AT FS 589.00 @STGR 20L 
- [SDR SWIA2018111345258](https://openairdocs.org/sdr/SWIA2018111345258), Oct 20, 2018: BULKHEAD WEB. CRACKED. FS.280.00 LOWER WEB HAS CRACKS AT LBL9 AND RBL9. (C-CHECK) RO: 11/12/2018 COMPLIED WITH REPAIR OF THE FS280 BULKHEAD WEB. PERFORMED ALL STEPS IAW REO.
- [SDR SWIA2018111345261](https://openairdocs.org/sdr/SWIA2018111345261), Oct 18, 2018: STRINGER. CRACKED. CLIP ON THE UPPER SIDE OF STGR3L, FS282.00 IS CRACKED. (C-CHECK) RO: 11/12/2018 REMOVED AND INSTALLED NEW CLIP ON THE UPPER SIDE OF STGR3L, FS282.00. IAW SRM. P
- [SDR SWIA2018111345260](https://openairdocs.org/sdr/SWIA2018111345260), Oct 18, 2018: DOUBLER. CORRODED. CORROSION ON DOUBLER FOR THE PASSENGER DOOR LOWER SILL FS349.00. (C-CHECK) RO: 11/12/2018 REMOVED CORROSION FROM DOUBLER LOCATED UNDER FLOOR SILL JUST AFT OF PA
- [SDR SWIA2018111345259](https://openairdocs.org/sdr/SWIA2018111345259), Oct 15, 2018: SKIN. DENTED. DENT IN FUSELAGE SKIN AT FS639.00 JUST BELOW STGR2R. (C-CHECK) RO: 11/12/2018 DRESSED BACK DENT IN FUSELAGE SKIN AT FS639.00 JUST BELOW STGR2R IAW REO.
- [SDR SWIA201844132](https://openairdocs.org/sdr/SWIA201844132), Jan 10, 2018: BRACKET. FAILED. GEAR DISAGREE NOSE GEAR WOULD NOT RETRACT. (FLT#2944) CLOSED REMOVED AND REPLACED BRACKET IAW AMM. SWUNG GEAR OPS GOOD.
- [SDR SWIA201744067](https://openairdocs.org/sdr/SWIA201744067), Dec 14, 2017: BRACKET. DAMAGED. NOSE GEAR DISAGREE. REMOVED AND REPLACED THE NR 2 WOW AND CENTERED HARNESS ASSY IAW AMM. OPS CHECKED GOOD. REMOVED AND REPLACED CENTERING SENSOR BRACKET IAW CMM
- [SDR SWIA201743582](https://openairdocs.org/sdr/SWIA201743582), Jul 31, 2017: CONTROL UNIT. FAILED. FLAP FAIL, RETURNED TO THE FIELD. EMERGENCY DECLARED. REPLACED THE FLAP LEVER AND FECU. AND RERIGGED THE RIGHT BPSU. SYSTEM OP CHECKS GOOD.
- [SDR SWIA201743256](https://openairdocs.org/sdr/SWIA201743256), May 1, 2017: CARBON SEAL. LEAKING. SMOKE IN THE COCKPIT AND A SMOKE CARGO WARNING MESSAGE. DIVERTED. REMOVED AND REPLACED THE NR 1 CARBON SEAL. LEAK CHECKED AND OIL CONSUMPTION CHECKED GOOD.
- [SDR SWIA2017050243256](https://openairdocs.org/sdr/SWIA2017050243256), May 1, 2017: UNKNOWN. SMOKE. SMOKE IN COCKPIT AND SMOKE CARGO WARNING MESSAGE, DIVERTED. OPEN.
- [SDR SWIA201642833](https://openairdocs.org/sdr/SWIA201642833), Oct 22, 2016: PANEL. CHAFED. PANEL 684BB CHAFED ON FWD EDGE. REPAIRED IAW EA.
- [SDR SWIA201642831](https://openairdocs.org/sdr/SWIA201642831), Oct 22, 2016: PLATE. CRACKED. CARGO SKIN PROTECTIVE PLATE HAS CRACKS AROUND FASTENER HOLES. ( LOCATED & DRILLED HOLES ON NEW CARGO PROTECTIVE PLATE IAW SRM.
- [SDR SWIA201642832](https://openairdocs.org/sdr/SWIA201642832), Oct 21, 2016: SKIN. WORN. RIGHT NACELLE CORE COWL HAS WEAR AT LATCH AREA CAUSED BY BLOCKER DOOR. FABRICATED AND INSTALLED REPAIR PLATE IAW CMM. BLENDED NR 6 BLOCKER DOOR TO OBTAIN THE CO
- [SDR SWIA201541442](https://openairdocs.org/sdr/SWIA201541442), Sep 25, 2015: LANDING GEAR. MALFUNCTIONED. GEAR DISAGREE MESSAGE WITH WOW MESSAGE. RETURNED TO DEPARTURE. SERVICED NLG, BLED SYSTEM. OPS CHECKED GOOD.
- [SDR SWIA201541008](https://openairdocs.org/sdr/SWIA201541008), Apr 7, 2015: WARNING MESSAGE. FALSE ACTIVATION. "RT REV UNLOCKED" CAUTION MSG IN FLIGHT. COMPLIED WITH QRH PROCEDURE ON EMER1-16, LANDED NEAREST SUITABLE AIRPORT. TROUBLESHOT RIGHT THRUST REVERSER UNLOCK MESS
- [SDR SWIA201439820](https://openairdocs.org/sdr/SWIA201439820), Nov 5, 2014: TUBE. DAMAGED. SERVICE DOOR CONVOLEX DAMAGED. C-CHECK, R & R CONVOLEX TUBING WITH NEW, IAW REO.
- [SDR SWIA201439879](https://openairdocs.org/sdr/SWIA201439879), Oct 31, 2014: PICCOLO TUBE. CHAFED. LEFT WING OTBD PICCOLO TUBE HAS CHAFING FROM L/E RIB BETWEEN 530JZ AND 530KZ. C-CHECK, REPAIRED CHAFE ON OTBD PICCOLO TUBE IAW STS EA.
- [SDR SWIA201439878](https://openairdocs.org/sdr/SWIA201439878), Oct 31, 2014: PICCOLO TUBE. DAMAGED. LT WING OTBD PICCOLO TUBE HAS DRILL START 38.5" FROM OTBD EDGE. C-CHECK, CLEANED AND WELDED DRILL START IAW STS EA.
- [SDR SWIA201439877](https://openairdocs.org/sdr/SWIA201439877), Oct 31, 2014: PICCOLO TUBE. DENTED. LT WING OTBD PICCOLO TUBE HAS A DENT 38.5" FROM OTBD EDGE. C-CHECK, REPAIRED DENT IN OTBD PICCOLO TUBE IAW STS EA.
- [SDR SWIA201439876](https://openairdocs.org/sdr/SWIA201439876), Oct 31, 2014: PICCOLO TUBE. GOUGED. LEFT WING OTBD PICCOLO TUBE HAS GOUGE NEAR WELD AT INBD FLANGE. C-CHECK, REPAIRED GOUGE ON INBD FLANGE IAW STS EA.
- [SDR SWIA201439875](https://openairdocs.org/sdr/SWIA201439875), Oct 23, 2014: SKIN. GOUGED. FUSELAGE SKIN, LOWER FORWARD AREA, RT LOWER DME ANTENNA FOOT PRINT HAS A MINOR GOUGE. C-CHECK, REPAIRED LWR FUSELAGE BETWEEN FS 409.0+48 & 409.00+64, S25R-S26R 
- [SDR SWIA201439874](https://openairdocs.org/sdr/SWIA201439874), Oct 23, 2014: SKIN. GOUGED. ON FUSELAGE SKIN LOWER FORWARD AREA, LT LOWER DME ANTENNA FOOT PRINTS HAS MINOR GOUGES 2 LOCATIONS. C-CHECK, REPAIRED LWR FUSELAGE BETWEEN FS 409.0+48 & 409.00+
- [SDR SWIA201439873](https://openairdocs.org/sdr/SWIA201439873), Oct 23, 2014: SKIN. NICKED. FWD LOWER CORNER OF PAX DOOR CUT OUT HAS NICKS. C-CHECK, BLENDED FWD LOWER CORNER FUSELAGE SKIN AT PAX DOOR CUT OUT TO A SMOOTH FINISH, IAW STS EA.
- [SDR SWIA201439872](https://openairdocs.org/sdr/SWIA201439872), Oct 22, 2014: HINGE. GOUGED. PAX DOOR MOUNTED PIANO HINGE HALF HAS WEAR GROOVES AND GOUGES ON LUGS 12 LOCATIONS SEEN WITH DOOR OPENED AND CLOSED. BLENDED DAMAGED AREA TO A SMOOTH FINISH, IA
- [SDR SWIA201439871](https://openairdocs.org/sdr/SWIA201439871), Oct 22, 2014: HINGE. GOUGED. FUSELAGE MOUNTED PAX DOOR PIANO HINGE HALF HAS A GOUGE ON LUG, 6TH FROM AFT END. C-CHECK, BLENDED DAMAGED AREA TO A SMOOTH FINISH, IAW REO.
- [SDR SWIA201439870](https://openairdocs.org/sdr/SWIA201439870), Oct 20, 2014: FLOOR SUPPORT. CORRODED. RIGHT FUSELAGE FLOOR ANGLE HAS CORROSION AT FS529.00, RBL 47. C-CHECK, CORROSION ON RT FLOOR ANGLE AT FS 529.00, RBL 47, WAS BLENDED IAW REO.
- [SDR SWIA201439869](https://openairdocs.org/sdr/SWIA201439869), Oct 20, 2014: FLOOR SUPPORT. CORRODED. RIGHT FUSELAGE FLOOR ANGLE HAS CORROSION AT FS 499 TO 513, RBL 47. C-CHECK, CORROSION ON RT FLOOR ANGLE AT FS 499 TO FS 513, RBL 47, WAS BLENDED IAW REO.
- [SDR SWIA201439868](https://openairdocs.org/sdr/SWIA201439868), Oct 20, 2014: FLOOR SUPPORT. CORRODED. RIGHT FUSELAGE FLOOR ANGLE HAS CORROSION AT FS 473.15 RBL 47. REMOVED CORROSION BY BLENDING IAW REO.
- [SDR SWIA201439867](https://openairdocs.org/sdr/SWIA201439867), Oct 20, 2014: FLOOR SUPPORT. CORRODED. RIGHT FUSELAGE FLOOR ANGLE HAS CORROSION AT FS 461, RBL 47. BLENDED OUT CORROSION IAW REO.
- [SDR SWIA201439866](https://openairdocs.org/sdr/SWIA201439866), Oct 20, 2014: FLOOR SUPPORT. CORRODED. RIGHT FUSELAGE FLOOR ANGLE HAS CORROSION AT FS449.85, RBL 47. C-CHECK CORROSION ON RIGHT FLOOR ANGLE AT FS 449.85, RBL 47, WAS BLENDED IAW REO.
- [SDR SWIA201439865](https://openairdocs.org/sdr/SWIA201439865), Oct 20, 2014: FLOOR SUPPORT. CORRODED. LEFT FUSELAGE FLOOR ANGLE HAS CORROSION AT FS 544, LBL47. C-CHECK, BLENDED CORROSION IAW REO.
- [SDR SWIA201439864](https://openairdocs.org/sdr/SWIA201439864), Oct 20, 2014: FLOOR SUPPORT. CORRODED. LEFT FUSELAGE FLOOR ANGLE HAS CORROSION AT AFT SIDE OF FS 513. C-CHECK, CORROSION ON LEFT FLOOR ANGLE AFT OF FS 513 WAS BLENDED IAW REO.
- [SDR SWIA201439863](https://openairdocs.org/sdr/SWIA201439863), Oct 20, 2014: FLOOR SUPPORT. CORRODED. LEFT FLOOR ANGLE HAS CORROSION AT FS499 TO 513 LBL47. C-CHECK, CORROSION ON LT FLOOR ANGLE FS 499-FS 513 AT LBL 47 WAS BLENDED IAW REO.
- [SDR SWIA201439862](https://openairdocs.org/sdr/SWIA201439862), Oct 20, 2014: FLOOR SUPPORT. CORRODED. LEFT FUSELAGE FLOOR ANGLE CORRODED AT FS461, LBL 47. C-CHECK, REMOVED CORROSION ON LT FUSELAGE FLOOR ANGLE AT FS 461, LBL47 IAW REO.
- [SDR SWIA201439861](https://openairdocs.org/sdr/SWIA201439861), Oct 20, 2014: FLOOR SUPPORT. CORRODED. LEFT FUSELAGE FLOOR ANGLE CORRODED AT BS 449.85, LBL 47. REMOVED CORROSION BY BLENDING IAW REO.
- [SDR SWIA201439840](https://openairdocs.org/sdr/SWIA201439840), Oct 20, 2014: SEAT TRACK. CORRODED. LEFT FUSELAGE SEAT TRACK CORRODED AT BS 559+112 LBL 9. REPLACED THE SEAT TRACK IAW REO.
- [SDR SWIA201439839](https://openairdocs.org/sdr/SWIA201439839), Oct 20, 2014: SEAT TRACK. CORRODED. RT FUSELAGE SEAT TRACK CORRODED BS 559+80 - 559+96. R & R THE SEAT TRACK SECTION IAW REO.
- [SDR SWIA201439838](https://openairdocs.org/sdr/SWIA201439838), Oct 20, 2014: SEAT TRACK. CORRODED. LEFT FUSELAGE SEAT TRACK CORRODED AT BS 559+80 - 559+96 LBL 9. R & R THE SEAT TRACK SECTION IAW REO.
- [SDR SWIA201439837](https://openairdocs.org/sdr/SWIA201439837), Oct 20, 2014: SEAT TRACK. CORRODED. LEFT FUSELAGE SEAT TRACK CORRODED AT BS 612 - 617 LBL 9. R & R THE SEAT TRACK SECTION, IAW REO AND SRM.
- [SDR SWIA201439836](https://openairdocs.org/sdr/SWIA201439836), Oct 20, 2014: FLOOR SUPPORT. CORRODED. RT FUSELAGE FLOOR SUPPORT IS CORRODED AROUND NUTPLATE HOLE BS 605 - 621. REMOVED CORROSION IAW REO.
- [SDR SWIA201439835](https://openairdocs.org/sdr/SWIA201439835), Oct 20, 2014: FLOOR SUPPORT. CORRODED. RT FLOOR SUPPORT BS 559+80 - 559+112 IS CORRODED. CORROSION WAS BLENDED AND FOUND WITHIN LIMITS IAW REO AND SRM.
- [SDR SWIA201439834](https://openairdocs.org/sdr/SWIA201439834), Oct 20, 2014: LINE. CRACKED. APU FUEL LINE HAS A CRACKED WELD AT SUPPORT BRACKET INSIDE PRESSURE BOX. C-CHECK, REINFORCED FUEL LINES FUEL PRESSURE BOX IAW REO.
- [SDR SWIA201439833](https://openairdocs.org/sdr/SWIA201439833), Oct 19, 2014: ATTACH ANGLE. GOUGED. AFT CARGO FLOORBEAM ATTACHMENT TO THE BS 621 PRESSURE BULKHEAD AT LBL27 HAS GOUGE. C-CHECK, REPAIRED AFT CARGO FLOOR RAIL FITTING ON FS 621 LBL 27.00 IAW REO.
- [SDR SWIA201439832](https://openairdocs.org/sdr/SWIA201439832), Oct 19, 2014: ANGLE. CRACKED. FS 484, RBL 36, OTBD CLIP IS CRACKED. C-CHECK, INSTALLED REPAIR ANGLE IAW REO.
- [SDR SWIA201439860](https://openairdocs.org/sdr/SWIA201439860), Oct 18, 2014: LINK. CHAFED. LEFT ENGINE BLOCKER BLOCKER DOOR LINKS HAVE CHAFE DAMAGE AT FORWARD END. REPAIRED DAMAGE ON LT ENG BLOCKER DOOR LINKS IAW REO.
- [SDR SWIA201439831](https://openairdocs.org/sdr/SWIA201439831), Oct 18, 2014: POST. CRACKED. VERTICAL POST AT FS 409+128, RBL 18 OBD SIDE IS CRACKED. C-CHECK R & R THE VERTICAL POST AT FS409+128, RBL18 OTBD IAW REO.
- [SDR SWIA201439830](https://openairdocs.org/sdr/SWIA201439830), Oct 18, 2014: BULKHEAD WEB. CRACKED. CRACK NOTED ON FS 621 BULKHEAD WEB, FWD FACE, ALONG HEEL LINE AT RBL27.5, APPROXIMATELY WL90. C-CHECK, INSTALLED ALL REPAIR PARTS IAW REO.
- [SDR SWIA201439829](https://openairdocs.org/sdr/SWIA201439829), Oct 18, 2014: SKIN. CHAFED. RT AILERON UPPER SKIN SHROUD CHAFED IN 2 LOCATION, BOTH SIDES OF OTBD HINGE. C-CHECK, BLENDED RT AILERON UPPER SKIN SHROUD IN 2EA LOCATIONS, BOTH SIDES OF OTBD 
- [SDR SWIA201439828](https://openairdocs.org/sdr/SWIA201439828), Oct 18, 2014: SKIN. CHAFED. LEFT AILERON UPPER SKIN SHROUD CHAFED IN 2 LOCATION, INBD OF INBD HINGE AND OTBD OF CENTER HINGE. C-CHECK, BLENDED THE LT AILERON UPPER SKIN SHROUD, 2EA, CHAFES

All 165: https://openairdocs.org/deregistered/N866AS-2023-07-30/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB CEN11IA379](https://openairdocs.org/ntsb/CEN11IA379), Jun 7, 2011: Bombardier CL-600-2B19 (N866AS), Milwaukee, WI, incident, minor damage. Probable cause: The failure of the right main landing gear (MLG) to extend normally, which resulted from the combination of a slightly worn uplock pin, the operation of the hydraulic pumps below their specified…

## FAA accident and incident reports (3)

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 20170501004679I](https://openairdocs.org/incident/20170501004679I), May 1, 2017: Bombardier Inc CL-600-2B19 (N866AS), West Chicago, IL, No damage. On may 1, 2017, American airlines flight #2936, a CRJ-700, N866AS, operated by skywest airlines (swia) was scheduled to operate from Chicago, IL (kord) to…
- [Incident 20110606028379I](https://openairdocs.org/incident/20110606028379I), Jun 6, 2011: Bombardier Inc CL-600-2B19 (N866AS), Milwaukee, WI, Minor damage. On June 6, 2011, at 2132 central daylight time (CDT), N866AS, serial number 7517, a Bombardier CL-600-2B19 (CRJ-200), registered to atlantic south east…
- [Incident 20050511014449I](https://openairdocs.org/incident/20050511014449I), May 11, 2005: Cndair CL6002B19 (N866AS), Akron, OH, Minor damage. (-23) Asoa flt 4562 landing at rwy 1 @cak blew inbd rt MLG tire on touch down. Tire fragments opened a 6 in. Gash on the rt inbd flap bottom. Aircraft taxied…

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