# N8477R: 2001 Bombardier CL-600-2B19, registration cancelled 2023-03-04

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 4, 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: 7477
- Year built: 2001
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 19, 2001
- Certificate issued: November 25, 2019
- Last registry action: July 18, 2022
- Mode S code: AB9D37
- 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/N8477R
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8477R
- Page: https://openairdocs.org/deregistered/N8477R-2023-03-04

From the FAA registry file of November 3, 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 (52, newest 50)

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

- [SDR REXA2015041500410](https://openairdocs.org/sdr/REXA2015041500410), Apr 15, 2015: LIGHT. INOPERATIVE. OVERHEAD INDICATION LIGHTS ARE FLASHING. R & R 1K1WA & 2K1WA IN JB3 IAW EESPM 20-22-00 & IAW AMM 24-01-03. OPERATIONS CHECKED GOOD.
- [SDR REXA2015031000312](https://openairdocs.org/sdr/REXA2015031000312), Mar 10, 2015: BATTERY PACK. INOPERATIVE. F/A FLASHLIGHT IS NOT WORKING. R & R BATTERY PACK FOR F/A FLASHLIGHT, PN P4-01-0021 IAW CMM 25-60-02. OPS CHECK GOOD, OK FOR SERVICE.
- [SDR REXA2015030100279](https://openairdocs.org/sdr/REXA2015030100279), Mar 1, 2015: LIFE VEST. UNSERVICEABLE. INFANT LIFE VEST BAG TORN. R & R ONE INFANT LIFE VEST IAW PA 25-096A.
- [SDR REXA2014110100902](https://openairdocs.org/sdr/REXA2014110100902), Oct 29, 2014: SKIN. DENTED. PERMANENT REPAIR OF 2 DENTS IN THE LT FUSELAGE SKIN AT FS 589.00 - 605.00, STRINGER 20L - 21L AS SHOWN IN FIG 1. THE DENTS MEASURE 3.875 INCHES X 1.0 INCHES X .
- [SDR REXA2014092701002](https://openairdocs.org/sdr/REXA2014092701002), Sep 27, 2014: UNKNOWN. ODOR. FROM MM02 APU DEACTIVATED FUEL SMELL ON START. OPERATE APU 5 TO 10 MIN CHECK CABIN & FLIGHT DECK DIDNT NOTE FUEL SMELL. REMOVED APU ENCLOSURE VISUALLY. INSPECTE
- [SDR REXA2014092500990](https://openairdocs.org/sdr/REXA2014092500990), Sep 25, 2014: UNKNOWN. ODOR. FUEL SMELL UPON APU START. PLACED APU ON MEL 49-10-11. DEACTIVATED APU IAW MEL. MM02 UPDATED & PLACARD INSTALLED.
- [SDR REXA2014081600764](https://openairdocs.org/sdr/REXA2014081600764), Aug 13, 2014: SKIN. DENTED. FUSELAGE SKIN AT APPROX FS 674 BETWEEN STRINGER 24R & 25R TO BE DENTED OUTWARD 0.75 INCHES X 0.63 INCHES WITH A 0.125 INCH PUNCTURE IN THE CTR. REPAIRED IAW EA 
- [SDR REXA2014080900806](https://openairdocs.org/sdr/REXA2014080900806), Aug 9, 2014: BULB. INOPERATIVE. AFT CEILING EMERGENCY FLOODLIGHT INOPERATIVE. R & R BULB IAW AMM 33-51-16.
- [SDR REXA2014041800388](https://openairdocs.org/sdr/REXA2014041800388), Apr 18, 2014: LIGHT. INOPERATIVE. 2ND FROM AFT EMERGENCY FLOOR TRACK STRIP INOPERATIVE. R & R EMERGENCY FLOOR TRACK LIGHT STRIP IAW AMM 33-51-01.
- [SDR REXA2014032500323](https://openairdocs.org/sdr/REXA2014032500323), Mar 25, 2014: CYLINDER. ERODED. GEAR DISAGREE ON TAKEOFF, NOSE DOOR OPEN MASTER WARNINGS, WITH NOSE DOOR RED, STEERING INOPERATIVE CAUTION, WOW INPUT CAUTION & WOW OUTPUT STATUS MSG. COMPLIED 
- [SDR REXA2014032300322](https://openairdocs.org/sdr/REXA2014032300322), Mar 23, 2014: WIRE HARNESS. FAULTY. UPON GEAR RETRACTION WE RECEIVED THE FOLLOWING MSG'S. GEAR DISAGREE WOW OUTPUT FAIL NOSE DOOR OPEN WOW INPUT STEERING INOPERATIVE. PERFORMED QRH, GEAR LOCKED DO
- [SDR REXA2014020700194](https://openairdocs.org/sdr/REXA2014020700194), Feb 7, 2014: PUMP. FAILED. HYDRAULIC SYS 3 LOW PRESSURE ILLUMINATED DURING GEAR EXTENSION. EMERGENCY NON-NORMAL CHECK LIST PERFORMED. SYS 3 FLUID LEVEL AT 0, UNEVENTFUL LANDING. MANUAL LA
- [SDR REXA2013110802251](https://openairdocs.org/sdr/REXA2013110802251), Nov 8, 2013: STARTER. FAILED. AIR CREW REPORTED, APU HIGH EGT, RPM 6-7, FLAME ERUPTED OUT OF TAIL PIPE. R & R APU STARTER IAW AMM 49-41-07. OP CHECKED GOOD.
- [SDR REXA2013110301792](https://openairdocs.org/sdr/REXA2013110301792), Nov 3, 2013: SMOKE GOGGLES. MISSING. OBSERVER SMOKE GOGGLES MISSING. REPLACED SMOKE GOGGLES IAW AMM 35-11-15.
- [SDR REXA2013101801164](https://openairdocs.org/sdr/REXA2013101801164), Oct 14, 2013: FRAME. CORRODED. MAINTENANCE FOUND CORROSION ON THE LOWER FRAME SECTOR AT FS 605 AS SHOWN IN FIG 1. THE MATERIAL LOSS AFTER BLENDING MEASURES A MAXIMUM OF .018" IN THE WEB OF TH
- [SDR REXA2013100901161](https://openairdocs.org/sdr/REXA2013100901161), Oct 8, 2013: BULKHEAD. CRACKED. FS 621 BULKHEAD FWD FACE AROUND LINTEL FITTING CRACKED. REPAIRED IAW REO 601R-53-61-1230.
- [SDR REXA2013100601152](https://openairdocs.org/sdr/REXA2013100601152), Oct 4, 2013: BULKHEAD. CHAFED. FORWARD FACE OF BS 621 BULKHEAD HAS MULTIPLE SCREW CHAFES AND RIVET HEADS SCRATCHED. REPAIRED IAW REO 601R-53-61-2155.
- [SDR REXA2013060301050](https://openairdocs.org/sdr/REXA2013060301050), Jun 3, 2013: INDICATION SYS. FLUCTUATES. ON FINAL WITH FLAPS SET TO 45 DEG THE ED1 FLAP INDICATOR FLUCTUATED BETWEEN 43 DEG AND 45 DEG. THE F/CTL SNOPTIC PAGE SHOWED THE LT FLAP AT 43 DEG AND THE RT FL
- [SDR REXA2013041200742](https://openairdocs.org/sdr/REXA2013041200742), Apr 12, 2013: LIFE VEST. UNSERVICEABLE. FLIGHT ATTENDANT LIFE VEST TORN. REMOVED AND REPLACED FLIGHT ATTENDANT LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2012090901327](https://openairdocs.org/sdr/REXA2012090901327), Sep 9, 2012: STRAP. BROKEN. FLIGHT ATTENDANT FLASHLIGHT SEAL IS BROKEN. REMOVED AND REPLACED FLIGHT ATTENDANT FLASHLIGHT HOLDER STRAP.
- [SDR REXA2012090601319](https://openairdocs.org/sdr/REXA2012090601319), Sep 6, 2012: CHARGER. INOPERATIVE. FORWARD EXTERIOR EMERGENCY LIGHT SERVICE EXIT AND PASSENGER EXIT INOPERATIVE. TROUBLESHOOT TO CHARGER. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT CHARGER. OPS CH
- [SDR REXA2012071401151](https://openairdocs.org/sdr/REXA2012071401151), Jul 14, 2012: LIGHT. INOPERATIVE. MAIN CABIN DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE.
- [SDR REXA2012070601048](https://openairdocs.org/sdr/REXA2012070601048), Jul 6, 2012: CONTROL PANEL. FAILED. AILERON TRIM STUCK, WILL NOT MOVE IN EITHER DIRECTION. REMOVED AND REPLACED AILERON/RUDDER TRIM CONTROL PANEL IAW AMM 27-12-10. OPS CHECKED GOOD.
- [SDR REXA2012061100831](https://openairdocs.org/sdr/REXA2012061100831), Jun 11, 2012: BULB. INOPERATIVE. LEFT AFT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT BULB IAW AMM 33-51-21. OPS CHECKS GOOD.
- [SDR REXA2012060100681](https://openairdocs.org/sdr/REXA2012060100681), May 26, 2012: VANE. CHAFED. LEFT INBOARD FLAP VANE ACTUATOR CHAFED 0.2 INCHES BY 0.050 INCHES BY 0.002 INCH DEEP AND 0.25 INCH BY 0.1 INCH BY 0.003 INCH DEEP. REPAIRED IAW REO 601R-57-52-1
- [SDR REXA2012052900680](https://openairdocs.org/sdr/REXA2012052900680), May 26, 2012: SKIN. GOUGED. LEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT IS GOUGED IN TWO PLACES AT WS 136.676, 0.006 INCH DEEP IN THE CRITICAL AREA AT HOLE NR 8. REPAIRED IAW REO 60
- [SDR REXA2012030200299](https://openairdocs.org/sdr/REXA2012030200299), Mar 2, 2012: THERMAL SWITCH. DEFECTIVE. ABORTED T/O AFTER DEPARTURE ON CLIMBOUT WING OVERHEAT MASTER WARNING IN STBY MODE (RIGHT WING). RETURNED TO DTW. REMOVED AND REPLACED RT WING BACKUP OVHT THERMA
- [SDR REXA2012030100320](https://openairdocs.org/sdr/REXA2012030100320), Mar 1, 2012: THERMAL SWITCH. DEFECTIVE. AIR RETURN FOR WING OVERHEAT MASTER WARNING IN STBY MODE (RIGHT WING). RETURNED TO DTW. REMOVED AND REPLACED RT WING BACKUP OVHT THERMAL SWITCH. SYSTEM OPS CHEC
- [SDR REXA201200144](https://openairdocs.org/sdr/REXA201200144), Jan 25, 2012: BATTERY. DISCHARGED. CAPT FLASHLIGHT NOT BLINKING. REMOVED AND REPLACED CAPT FLASHLIGHT BATTERY IAW AMM 25-60-00.
- [SDR REXA201200133](https://openairdocs.org/sdr/REXA201200133), Jan 21, 2012: TRANSMITTER. FAULTY. UNSCHEDULED LANDING FOR MULTIPLE INDICATIONS STARTING WITH SPEED SNAKE COVERING ENTIRE SCREEN AT 300 KIAS, THE FLAPS GOING OUT AND IN SEVERAL TIMES, SOMETIMES O
- [SDR REXA201200130](https://openairdocs.org/sdr/REXA201200130), Jan 20, 2012: ECU. MALFUNCTIONED. UNSCHEDULED LANDING. LEVEL OFF AT FL300: FLAPS EXTENDED ON THEIR OWN FLUCTUATING BTW 2 DEG AND 20 DEG MONENTARY HYD PUMP 2B CAUTION, THEN FLAPS DEGRADED STATUS 
- [SDR REXA201100951](https://openairdocs.org/sdr/REXA201100951), Dec 9, 2011: CHARGER. DEFECTIVE. LT/RT CENTER EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY. NO FIX. REMOVED AND REPLACED BATTERY CHARGER ASSY NR 3 PER CRJ 2
- [SDR REXA201100783](https://openairdocs.org/sdr/REXA201100783), Oct 26, 2011: FIRE LOOP. DIRTY. WING OVHT MASTER WARNING WHILE OPERATING IN "STBY" MODE PER MEL (RIGHTSIDE) MESSAGE CAME ON 3X DURING CLIMBOUT ONLY OPERATED NORMALLY ON GROUND LEVEL FLIGHT. CL
- [SDR REXA201100740](https://openairdocs.org/sdr/REXA201100740), Oct 20, 2011: RETAINING NUT. LOOSE. FLIGHT CONTROLS NOT RETURNING TO NEUTRAL DURING FLIGHT CONTROL CHECK AILERON CONTROL WHEEL IS BINDING. RE-TORQUED RETAINING NUTS IN AILERON CONTROL WHEEL IAW PA
- [SDR REXA201100724](https://openairdocs.org/sdr/REXA201100724), Oct 14, 2011: CONTROL SWITCH. BROKEN. ON DEPT, REC'D THE LEFT WING OVERHEAT DURING CLIMBOUT. FOLLOWED QRH. FROM THEN ON, LT WING ANTI-ICE WAS EXTREMELY SLOW TO HEAT. FOUND BROKEN TANG IN WING A/I CT
- [SDR REXA201100707](https://openairdocs.org/sdr/REXA201100707), Oct 14, 2011: SHUTOFF VALVE. FAULTY. WING OVHT WARNING MESSAGE IN FLIGHT WHILE OPERATING IN STBY MODE IN ACCORDANCE WITH MEL 30-12-31. REMOVED AND REPLACED RT 14TH STAGE BLEED AIR SOV IAW AMM 30-12
- [SDR REXA201100656](https://openairdocs.org/sdr/REXA201100656), Sep 29, 2011: SKIN. CORRODED. RT WING LOWER PLANK FUEL ACCESS CUTOUT HOLE NR 1 AT WS 54.897 HAS MINOR CORROSION IN THE NON-CRITICAL AREA. CORROSION APPROX 4.5 W X .002 D. REPAIRED IAW BOMBAR
- [SDR REXA201100652](https://openairdocs.org/sdr/REXA201100652), Sep 25, 2011: SKIN. CORRODED. RT WING LOWER PLANK FUEL ACCESS CUTOUT HOLE NR 1 AT WS 54.897 HAS MINOR CORROSION IN THE NON-CRITICAL AREA. CORROSION APPROX 4.5W X .002D. REPAIRED IAW BOMBARDI
- [SDR REXA201100585](https://openairdocs.org/sdr/REXA201100585), Sep 25, 2011: SILL. CORRODED. RT PRESSURE FLOOR SILL HAS 2 AREAS OF CORROSION AT FS 508 & FS 516. REPAIRED IAW BOMBARDIER REO 601R-53-41-666.
- [SDR REXA201100655](https://openairdocs.org/sdr/REXA201100655), Sep 17, 2011: BULKHEAD. GOUGED. REAR PRESSURE BULKHEAD AT FS 621 LBL 14 & 23, 3.0" UP FROM FLOOR, BULKHEAD GOUGED FROM SCREW APPROX .250 X .020 AND .015. REPAIRED IAW BOMBARDIER REO 601R-53-61
- [SDR REXA201100654](https://openairdocs.org/sdr/REXA201100654), Sep 17, 2011: BULKHEAD. GOUGED. AFT FUSELAGE PRESSURE BULKHEAD AT FS 621 RBL 42.0 & 3.0" UP FROM FLOOR, BULKHEAD GOUGED FROM SCREW .250 X .035 DEEP. REPAIRED IAW BOMBARDIER REO 601R--53-61 420
- [SDR REXA201100653](https://openairdocs.org/sdr/REXA201100653), Sep 17, 2011: ANGLE. CORRODED. FS 280 FWD "J" ANGLE CORRODED BETWEEN LBL 9 AND RBL 9. REPAIRED IAW SRM 51-40-11, 51-42-06, 51-21-11, 51-23-00.
- [SDR REXA201100651](https://openairdocs.org/sdr/REXA201100651), Sep 17, 2011: ANGLE. CORRODED. FS 280 AFT "J" ANGLE CORRODED BETWEEN LBL 9 AND RBL 9. REPAIRED FS 280.00 AFT J-ANGLE IAW BOMBARDIER REO 601R-53-11-926 AND BOMBARDIER SERVICE CORPORATION STAND
- [SDR REXA201100401](https://openairdocs.org/sdr/REXA201100401), Jun 19, 2011: ENGINE. MALFUNCTIONED. LT ENGINE OIL PRESS FLUX. REMOVED AND REPLACED LT ENGINE IAW CRJ AMM 71-00-00, OP CHECK GOOD. OK FOR SERVICE.
- [SDR REXA201100400](https://openairdocs.org/sdr/REXA201100400), Jun 17, 2011: SCAVENGE PUMP. MALFUNCTIONED. NR 1 ENGINE OIL WARNING MESSAGE. REMOVED AND REPLACED LUBE AND SCAVENGE PUMP IAW AMM 79-21-01.
- [SDR REXA201000179](https://openairdocs.org/sdr/REXA201000179), Oct 4, 2010: STRUCTURE. DAMAGED. LEFT AND RIGHT AILERON STATIC DISCHARGE BASES AT WS 370.7 WERE FOUND WITH CRACKING. THE LEFT AILERON DAMAGE IS ON BOTH THE INBOARD AND OUTBOARD FACES WITH CRACK
- [SDR REXA201000120](https://openairdocs.org/sdr/REXA201000120), Aug 30, 2010: WARNING SYSTEM. MALFUNCTIONED. GEAR DISAGREE ON APPROACH NOSE - GREEN BOTH MAINS RED. C/W GEAR SWING AND PA#05-018A, NO DEFECTS NOTED. OK FOR SERVICE.
- [SDR REXA201000091](https://openairdocs.org/sdr/REXA201000091), Jun 7, 2010: RVDT. MALFUNCTIONED. NOSE WHEEL STEERING MESSAGE DURING CRUISE. FOLLOWED QRH AND RETURNED TO DTW. MAINTENANCE REMOVED AND REPLACED THE LT RVDT IAW AMM 32-51-20.
- [SDR REXA200500119](https://openairdocs.org/sdr/REXA200500119), Sep 12, 2005: WARNING LIGHT. ILLUMINATED. GEAR DISAGREE WARNING MESSAGE AND GEAR DISAGREE AURAL WARNING AFTER TAKEOFF. PERFORMED QUICK REFERENCE HANDBOOK (QRH) AND WAS SUCCESSFUL ON LANDING GEAR DOWN. R
- [SDR REX2002F00004](https://openairdocs.org/sdr/REX2002F00004), Jun 12, 2002: PLUG. LEAKING. WHEN POWER WAS REDUCED ON FINAL APPROACH, THE RT ENGINE OIL PRESSURE WARNING ILLUMINATED. THE FLIGHT CREW DECLARED AN EMERGENCY AND SHUTDOWN RT ENGINE USING THE

All 52: https://openairdocs.org/deregistered/N8477R-2023-03-04/reports.md

## Other aircraft with N8477R

- [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N8477R-undated): Robinson Helicopter R22 ALPHA, S/N 0395

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