# N652BR: 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: 7429
- Year built: 2000
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 20, 2000
- Certificate issued: January 26, 2017
- Last registry action: September 30, 2023
- Mode S code: A89451
- 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/N652BR
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=652BR
- Page: https://openairdocs.org/deregistered/N652BR-2023-11-03

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 (155, newest 50)

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

- [SDR SWIA202266736](https://openairdocs.org/sdr/SWIA202266736), Nov 4, 2022: NONE. FAILED. D:GEAR DISAGREE WARNING MESSAGE AFTER SELECTING GEAR UP ABOVE SPEED 200KTS. GEAR RETRACTION SPEED LIMIT EXCEEDED. / C: MEL 32-30-1 / CAT A DUE WITHIN 1 FLIGHT D
- [SDR SWIA2021091561081](https://openairdocs.org/sdr/SWIA2021091561081), Sep 14, 2021: A/C PACK. FAILED. WHILE CLIMBING THROUGH 23000 FT RIGHT PACK TURNED OFF. RAN CHECKLISTS AND DESCENDED TO 15000. DO TO THE TERRAIN AND NOT BEING ABLE TO GET LOWER THE PASSENGER MA
- [SDR SWIA2021072659748](https://openairdocs.org/sdr/SWIA2021072659748), Jul 12, 2021: SKIN. DAMAGED. AIRCRAFT SUSTAINED DAMAGE TO THE FUSELAGE SKIN BETWEEN FS 265.00 - FS 280.00 BETWEEN STR 25L AND STR 26L (FILED CLOSED) REPAIRED DAMAGE TO FUSELAGE SKIN BETWEEN
- [SDR SWIA202159747](https://openairdocs.org/sdr/SWIA202159747), Jul 12, 2021: SKIN. DAMAGED. AIRCRAFT SUSTAINED DAMAGE TO THE FUSELAGE SKIN AND REPAIR DOUBLER AT FS 235.00, BETWEEN STR 25L - STR 26L (FILED CLOSED) REPAIRED DAMAGE TO FUSELAGE SKIN BETWEE
- [SDR SWIA2021062591000](https://openairdocs.org/sdr/SWIA2021062591000), Jun 25, 2021: APU. SHUTDOWN. APU INFLIGHT SHUTDOWN WHILE ENROUTE. SINGLE GENERATOR. VERIFIED APU INTAKE DOOR CLOSED AND ALL MX ACTION HAS BEEN COMPLIED WITH. REACTIVATED APU PER MEL 49-10-1
- [SDR SWIA202158148](https://openairdocs.org/sdr/SWIA202158148), May 12, 2021: BRACKET. BENT. GEAR DISAGREE EMERGENCY MESSAGE. NOSE GEAR REMAINED DOWN. RAN QRH AND EXTENDED ALL GEAR SUCCESSFULLY AND COMPLETED RTF. (FLIGHT 5289 - FILED CLOSED) FOUND NOSE 
- [SDR SWIA202053019](https://openairdocs.org/sdr/SWIA202053019), Oct 4, 2020: HEAT SHIELD. CRACKED. APU HEAT EXHAUST SHIELD HAS A CRACK BETWEEN THE 7 O`CLOCK AND 8 O`CLOCK POSITION. FILED CLOSED RO 10/5/2020. REMOVED AND REPLACED APU HEAT EXHAUST SHIELD, IN RE
- [SDR SWIA2020060950959](https://openairdocs.org/sdr/SWIA2020060950959), May 29, 2020: SKIN. DENTED. FUSELAGE SKIN DENT LABELED 18 BETWEEN FS654.50 & FS672.20 AND STR 1R - STR 2R REQUIRES REPAIR. (C-CHECK) RO 4/27/2020 REPAIRED FUSELAGE SKIN DENT LABELED 18 BET
- [SDR SWIA2020060950958](https://openairdocs.org/sdr/SWIA2020060950958), May 17, 2020: BULKHEAD. DAMAGED. WHILE PERFORMING REPLACEMENT OF RBL 18 VERTICAL POSTS (INBOARD AND OUTBOARD) AT FS 409+128, FOUND 4 EACH HOLES ELONGATED ON BULKHEAD WEB AND 1 EACH DENT. (C-CHE
- [SDR SWIA2020060950957](https://openairdocs.org/sdr/SWIA2020060950957), May 15, 2020: SKIN. DENTED. DENTS FOUND IN MULTIPLE LOCATIONS ON TOP SIDE OF FUSELAGE BETWEEN FS 621.00 AND FS 755.00 PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED
- [SDR SWIA2020060950956](https://openairdocs.org/sdr/SWIA2020060950956), May 14, 2020: FLOOR SUPPORT. WORN. FLOORBEAM CAP FROM FS569 TO FS621 LBL27 (P/N 601R35031-3) REQUIRES REPLACEMENT. (C-CHECK) RO 4/27/2020 REMOVED THE DAMAGED BEAM CAP FROM FS569 TO FS621 LBL27 (P
- [SDR SWIA2020060950946](https://openairdocs.org/sdr/SWIA2020060950946), May 13, 2020: STRAP. WORN. RT STRAP FS559.0 RBL 40 AND 27 APPROX REQUIRES REPLACEMENT. (C-CHECK) RO 4/27/2020 ORDERED AND RECEIVED, DRILLED AND LOCATED NEW PART, INSTALLED NEW STRAP ON TH
- [SDR SWIA2020060950955](https://openairdocs.org/sdr/SWIA2020060950955), May 9, 2020: POST. CRACKED. FS 409+128 LBL 18.0 OUTBD VERTICAL POST AFT RADIUS IS CRACKED. (C-CHECK) RO 4/27/2020 REMOVED 2 EA PLATES ATTACHED TO VERTICAL STIFFENER FS 409+128 LBL18 AT WL 
- [SDR SWIA2020060950954](https://openairdocs.org/sdr/SWIA2020060950954), May 9, 2020: STIFFENER. CRACKED. FS 409+128 BL 0.0 RT VERTICAL POST UPPER STIFFENER IS CRACKED. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED RT VERTICAL POST AT BL 0.0 FS 409.00+128 INSTALLED RE
- [SDR SWIA2020060950953](https://openairdocs.org/sdr/SWIA2020060950953), May 9, 2020: POST. CRACKED. FS 409+128 RBL 18.0 INBD AND OUTBD VERTICAL POST HAVE CRACKS IN AFT RADIUS. (C-CHECK) RO 4/27/2020 REMOVED AND INSTALLED NEW FS 409+128 RBL 18.0 INBD AND OUTBD 
- [SDR SWIA2020060950972](https://openairdocs.org/sdr/SWIA2020060950972), May 8, 2020: STOP FITTING. CHAFED. THE AVIONICS BAY DOOR CUTOUT SURROUND FWD RT STOP FITTING IS CHAFED. (C-CHECK) RO 4/27/2020 REPLACED AVIONICS BAY DOOR CUTOUT SURROUND FWD RT STOP FITTING REF S
- [SDR SWIA2020060950971](https://openairdocs.org/sdr/SWIA2020060950971), May 8, 2020: STOP FITTING. CHAFED. THE AVIONICS BAY DOOR CUTOUT SURROUND FWD LT STOP FITTING IS CHAFFED. (C-CHECK) RO 4/27/2020 FOUND TO BE OUT LIMITS REF SRM. REMOVED AND REPLACED NEW AVIONICS B
- [SDR SWIA2020060950965](https://openairdocs.org/sdr/SWIA2020060950965), May 8, 2020: FITTING. CRACKED. THE AVIONICS BAY DOOR SURROUND AFT LT GUIDE FITTING IS BROKEN/CRACKED. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED WITH NEW1 EACH AFT LT GUIDE FITTING ON AVIONI
- [SDR SWIA2020060950952](https://openairdocs.org/sdr/SWIA2020060950952), May 8, 2020: FRAME. CORRODED. THE FRAME AT FS349.00 HAS CORROSION FROM STRINGER 26R TO 26L. (C-CHECK) RO 4/27/2020 BLENDED OUT CORROSION ON LOWER FRAME SECTION AT FS349 FROM STR 26R TO 26L. 
- [SDR SWIA2020060950974](https://openairdocs.org/sdr/SWIA2020060950974), May 7, 2020: STRAP. CORRODED. RT STRAP FS559.0 LBL 40 AND 27 APPROX HAS CORROSION. (C-CHECK) RO 4/27/2020 REMOVED CORROSION AND RT STRAP FS559.0 WAS FOUND TO BE OUT OF LIMITS REF SRM. REPLAC
- [SDR SWIA2020060950967](https://openairdocs.org/sdr/SWIA2020060950967), May 7, 2020: SEAT TRACK. CORRODED. THE SEAT TRACK SECTION FROM APPROX FS559.00 TO FS559.00+80 AT RBL9.00 HAS MULTIPLE LOCATIONS OF CORROSION. (C-CHECK) RO 4/27/2020 FOUND TO BE OUT OF LIMITS REF 
- [SDR SWIA2020060950966](https://openairdocs.org/sdr/SWIA2020060950966), May 7, 2020: SEAT TRACK. CORRODED. FS559.00+112 - 574.00 (APPROXIMATE) AT RBL9 SEAT TRACK CORRODED AROUND FASTENERS. (C-CHECK) RO 4/27/2020 FOUND TO BE OUT OF LIMITS REF SRM 53-61-49. REMOVED AND
- [SDR SWIA2020060950962](https://openairdocs.org/sdr/SWIA2020060950962), May 7, 2020: FLOOR SKIN. CRACKED. THE PRESSURE FLOOR SKIN BETWEEN LBL 9.00 AND BL 0 AT APPROX FS 461.00 HAS 2EA CRACKS. (C-CHECK) RO 4/27/2020 REPAIRED REF REO. WEIGHT OF PARTS REMOVED IS 0.06LB
- [SDR SWIA2020060950951](https://openairdocs.org/sdr/SWIA2020060950951), May 7, 2020: PANEL. CORRODED. THE RT PRESSURE FLOOR SILL PANEL HAS MULTIPLE LOCATIONS OF CORROSION FROM FS409.00+128 TO FS559.00. (C-CHECK) RO 4/27/2020 REPAIRED RT PRESSURE FLOOR SILL BETWE
- [SDR SWIA2020060950950](https://openairdocs.org/sdr/SWIA2020060950950), May 7, 2020: PANEL. CORRODED. THE LT PRESSURE FLOOR SILL PANEL HAS MULTIPLE LOCATIONS OF CORROSION FROM FS409.00+128 TO FS559.00. (C-CHECK) RO 4/27/2020 REPAIRED LT PRESSURE FLOOR SILL BETWE
- [SDR SWIA2020060950949](https://openairdocs.org/sdr/SWIA2020060950949), May 7, 2020: FLOOR SKIN. CRACKED. THE PRESSURE FLOOR SKIN BETWEEN RBL 9.00 AND BL 0 AT APPROX FS461.00 HAS 2EA CRACKS. (C-CHECK) RO 4/27/2020 REPAIRED REF REO. WEIGHT OF PARTS REMOVED IS 0.05LBS
- [SDR SWIA2020060950947](https://openairdocs.org/sdr/SWIA2020060950947), May 7, 2020: CROSSBEAM. CORRODED. THE CROSSBEAM CAP AT FS559.00+48 BETWEEN RBL27.00 AND RBL9.00 HAS CORROSION. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED THE FLOOR SUPPORT PLATE. REF SRM, DRAWI
- [SDR SWIA2020060950945](https://openairdocs.org/sdr/SWIA2020060950945), May 7, 2020: STRAP. CORRODED. LT STRAP FS559.0 LBL 35 AND 27 HAS CORROSION. (C-CHECK) RO 4/27/2020 REMOVED CORROSION ON LT STRAP AT FS559 BETWEEN LBL27 - LBL35 REF SRM. LT STRAP AT FS 559.00
- [SDR SWIA2020060950944](https://openairdocs.org/sdr/SWIA2020060950944), May 7, 2020: BRACKET. CRACKED. LT FS 484 INBRD PULLEY ANGLE BRACKET IS CRACKED UPPER CORNER. (C-CHECK) RO 4/27/2020 REMOVED AT LT FS 484 INBRD PULLEY ANGLE BRACKET. REF SRM. FABRICATED LT FS4
- [SDR SWIA2020060950943](https://openairdocs.org/sdr/SWIA2020060950943), May 7, 2020: BRACKET. CRACKED. LT FS 484 OUTBRD PULLEY ANGLE BRACKET IS CRACKED UPPER CORNER. (C-CHECK) RO 4/27/2020 REMOVED AT LT FS 484 OUTBRD PULLEY ANGLE BRACKET. REF SRM. FABRICATED LT F
- [SDR SWIA2020060950942](https://openairdocs.org/sdr/SWIA2020060950942), May 7, 2020: FLOOR SUPPORT. CORRODED. RT FLOORBEAM FS 409.00+128 TO 599.0 RBL 9 HAS CORROSION. (C-CHECK) RO 4/27/2020 REMOVED THE CORROSION, ENSURED REMAINING MATERIAL THICKNESS (NDT) - FOUND OUT OF
- [SDR SWIA2020060950941](https://openairdocs.org/sdr/SWIA2020060950941), May 7, 2020: DOUBLER. CORRODED. RT GALLEY INBRD FWD DOUBLER PLATE HAS CORROSION AROUND NUTPLATE HOLE. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED FWD DOUBLER PLATE AT FS295 AND RBL 4.25 REF SR
- [SDR SWIA2020060950940](https://openairdocs.org/sdr/SWIA2020060950940), May 7, 2020: DOUBLER. CORRODED. RT GALLEY INBRD AFT DOUBLER PLATE HAS CORROSION AROUND NUTPLATE HOLE. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED AFT DOUBLER PLATE AT FS324 AND RBL 4.25 REF SR
- [SDR SWIA2020060950939](https://openairdocs.org/sdr/SWIA2020060950939), May 7, 2020: DOUBLER. CORRODED. RT GALLEY OUTBRD DOUBLER PLATE APPROX FS 319 RBL 35 HAS CORROSION AROUND NUTPLATE HOLE. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED O/B DOUBLER PLATE AT FS319 A
- [SDR SWIA2020060950938](https://openairdocs.org/sdr/SWIA2020060950938), May 7, 2020: FLOORBEAM. CORRODED. RT FLOORBEAM HAS CORROSION FS409.00+05 TO 409.00+121 RBL 9. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED THE RT FLOORBEAM AT RBL 9 BETWEEN FS409.00+05 TO 409.00+
- [SDR SWIA2020060950937](https://openairdocs.org/sdr/SWIA2020060950937), May 7, 2020: FLOORBEAM. CORRODED. LT FLOORBEAM HAS CORROSION FS409.00+05 TO 409.00+121 LBL 9. (C-CHECK) RO 4/27/2020 BLENDED CORROSION ON LT FLOOR BEAM AT FS409.00+05 TO FS409.00+121 REF. FOUND 
- [SDR SWIA2020060950936](https://openairdocs.org/sdr/SWIA2020060950936), May 7, 2020: DOOR SILL. CORRODED. SERVICE DOOR SILL HAS CORROSION RT FS 319- 349. (C-CHECK) RO 4/27/2020 FOUND TO BE OUT OF LIMITS REF SRM. REMOVED AND REPLACED NEW MID SUPPORT ANGLE P/N 601R383
- [SDR SWIA2020060950935](https://openairdocs.org/sdr/SWIA2020060950935), May 7, 2020: SEAT TRACK. CORRODED. FS559.00+112 - 574.00 (APPROXIMATE) AT LBL9 SEAT TRACK CORRODED AROUND FASTENERS. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED SEAT TRACK FROM FS559+112 -FS574 L
- [SDR SWIA2020060950934](https://openairdocs.org/sdr/SWIA2020060950934), May 7, 2020: SEAT TRACK. CORRODED. FS559.00+112 - 621.00 SEAT RAIL BEAM CAP AT LBL27 CORRODED IN NUMEROUS AREAS. (C-CHECK) RO 4/27/2020 REMOVED CORROSION FROM SEAT RAIL BEAM CAP AT LBL27 FS559.00
- [SDR SWIA2020060950970](https://openairdocs.org/sdr/SWIA2020060950970), May 2, 2020: CONNECTING ROD. CHAFED. RT MLG LWR/OTBD DOOR CONNECTING ROD CHAFED ON AFT FACE OF INBD END OF ROD, AT PIVOT MEMBER CONNECTION POINT. (C-CHECK) RO 4/27/2020 REMOVED RT MLG DOOR STRUT. R
- [SDR SWIA2020060950969](https://openairdocs.org/sdr/SWIA2020060950969), May 2, 2020: CONNECTING ROD. CHAFED. RT MLG UPPER/INBD DOOR CONNECTING ROD CHAFED ON AFT FACE OF LWR END OF ROD, AT PIVOT MEMBER CONNECTION POINT. (C-CHECK) RO 4/27/2020 REPLACED RT MLG DOOR PUSH/P
- [SDR SWIA2020060950968](https://openairdocs.org/sdr/SWIA2020060950968), May 1, 2020: SUPPORT. CHAFED. CENTER VERTICAL SUPPORT POST (AFT SIDE) REAR PRESS BULKHEAD FS 621.00, BL 0.00, IS CHAFED FROM MECHANICAL CONTACT WITH 10TH STAGE BLEED AIR SOV APROX 10' FROM T
- [SDR SWIA2020060950964](https://openairdocs.org/sdr/SWIA2020060950964), May 1, 2020: ATTACH FITTING. CRACKED. FOUND CRACKED ATTACHING (CLIP) AFT R/H SIDE OF REAR PRESS BULKHEAD FS 621.00, THAT ATTACHES TO FS 625.00 BY COMMON INTERCOSTAL, AT APROX STR 14R LEVEL, AFT EQUI
- [SDR SWIA2020060950963](https://openairdocs.org/sdr/SWIA2020060950963), May 1, 2020: ATTACH FITTING. CRACKED. FOUND CRACKED ATTACHING (CLIP) AFT LT SIDE OF REAR PRESS BULKHEAD FS 621.00, THAT ATTACHES TO FS 625.00 BY COMMON INTERCOSTAL, AT APROX STR 14L LEVEL, AFT EQUIP
- [SDR SWIA2020060950973](https://openairdocs.org/sdr/SWIA2020060950973), Apr 30, 2020: STRINGER. GOUGED. SMALL SECTION OF STRINGER ATTACHED TO AFT PRESSURE BULKHEAD FS 621.00 THAT SPANS FROM THE AFT CARGO DOOR AFT TRACK OTBD TO FS 621.00, FOUND GOUGED/BENT FROM PRO
- [SDR SWIA2020060950961](https://openairdocs.org/sdr/SWIA2020060950961), Apr 30, 2020: ATTACH ANGLE. CRACKED. (AFT) ATTACHING ANGLE (BOTTOM SIDE) AT FS 621.00 AND COMMON TO THE PRESSURE BULKHEAD, FOR ATTACHMENT OF THE CARGO DOOR CAM TRACK SUPPORT ASSY FOUND CRACKED. (C-
- [SDR SWIA2020060950933](https://openairdocs.org/sdr/SWIA2020060950933), Apr 29, 2020: SKIN. DENTED. RT FUSELAGE SKIN HAS DENT OUTBOARD OF NLG AFT GEAR DOOR HINGE POINT APPROX FS 232 / BL 8 RT. (C-CHECK) RO 4/27/2020 REPAIRED THE DENT AT THE RT FUSELAGE SKIN, O
- [SDR SWIA2020060950932](https://openairdocs.org/sdr/SWIA2020060950932), Apr 28, 2020: SKIN. CHAFED. LT INBOARD FLAP VANE SKIN L/E IS CHAFED OUTBOARD OF PANEL 584FT. (C-CHECK) RO 4/27/2020 REPLACED LT INBOARD FLAP VANE SKIN L/E OUTBOARD SECTION WITH NEW PN 601R
- [SDR SWIA2020060950931](https://openairdocs.org/sdr/SWIA2020060950931), Apr 28, 2020: SKIN. CHAFED. LT INBOARD FLAP VANE SKIN L/E IS CHAFED OUTBOARD OF PANEL 584ET. (C-CHECK) RO 4/27/2020 REPLACED LT INBOARD FLAP VANE SKIN L/E CENTER SECTION WITH NEW PN 601R14
- [SDR SWIA2020060950930](https://openairdocs.org/sdr/SWIA2020060950930), Apr 28, 2020: SKIN. CHAFED. RT INBOARD FLAP VANE SKIN IS CHAFED OUTBOARD OF PANEL 684FT. (C-CHECK) RO 4/27/2020 REPLACED RT INBOARD FLAP VANE SKIN OUTBOARD OF PANEL 684FT PN 601R14303-44S 

All 155: https://openairdocs.org/deregistered/N652BR-2023-11-03/reports.md

## FAA accident and incident reports (1)

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 20030923029889I](https://openairdocs.org/incident/20030923029889I), Sep 23, 2003: Cndair CL6002B19 (N652BR), Peoria, IL. (-23) Just after V2, the crew received a anti-skid warning. On gear retraction the nose went up and the mains remained down with "gear disagree" caption. Other…

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