# N8423C: 2000 Bombardier CL-600-2B19, registration cancelled 2019-04-10 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 10, 2019 - 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: 7423 - Year built: 2000 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 11, 2000 - Certificate issued: October 18, 2000 - Last registry action: June 13, 2018 - Mode S code: AB8A0B - Owner when cancelled: [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N8423C - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8423C - Page: https://openairdocs.org/deregistered/N8423C-2019-04-10 From the FAA registry file of November 12, 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 (56, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR REXA2013112502275](https://openairdocs.org/sdr/REXA2013112502275), Nov 25, 2013: PROXIMITY SENSOR. MISINSTALLED. FLAP FAILURE OCCURRED DURING APPROACH WHILE EXTENDING FLAPS. FLAPS INDICATED FAILURE AT 27 DEGREES AT 170 KTS AT -5 C. FOUND DAMAGE TO RT NR 3 FLAP ACTUATOR FRO - [SDR REXA2013080601560](https://openairdocs.org/sdr/REXA2013080601560), Aug 6, 2013: SIGN. INOPERATIVE. GALLEY EMERGENCY EXIT SIGN INOPERATIVE. R & R LIGHTED FLOOR LEVEL SIGN IAW AMM 33-51-10. OPS CHECKED GOOD. - [SDR REXA2013051600664](https://openairdocs.org/sdr/REXA2013051600664), May 15, 2013: STRINGER SPLICE. BENT. VERTICAL STABILIZER STRINGER EXTENSION SPLICE IS BENT JUST AFT OF MID SPAR 43.75 ON THE UPPER EDGE OF THE FUSELAGE SKIN. REPAIRED IAW SRM 51-42-06. - [SDR REXA2013051700666](https://openairdocs.org/sdr/REXA2013051700666), May 14, 2013: FLOOR SUPPORT. CORRODED. AFT CARGO COMPARTMENT FLOOR SUPPORT STRUCTURE CORRODED AT FS 559+112 TO FS 621, LBL 28, WL 72.5. REPAIRED IAW BOMBARDIER REO 601R-53-61-3778. - [SDR REXA2013041100738](https://openairdocs.org/sdr/REXA2013041100738), Apr 11, 2013: RESERVOIR. FAILED. FLIGHT 3259, DURING CLIMBOUT, RECEIVED HYD 3 LO PRESS CAUTION FOLLOWED BY GEAR DISAGREE WARNING 20 - 30 SECONDS LATER. GEAR RETRACTED AND BOTH MESSAGES WENT AWA - [SDR REXA2013033100604](https://openairdocs.org/sdr/REXA2013033100604), Mar 31, 2013: HYDRAULIC SYSTEM. CONTAMINATED. FLIGHT 4168 (RIC TO CVG) HAD HYDRAULIC SYSTEM 3 LOW PRESSURE CAUTION CAME ON AND GEAR DISAGREE AFTER TAKEOFF. LOW PRESSURE SHOWING 100% QUANTITY. THE CREW STATE - [SDR REXA2013030200431](https://openairdocs.org/sdr/REXA2013030200431), Mar 2, 2013: LIFE VEST. UNSERVICEABLE. CAPTAIN'S LIFE VEST BAG TORN. REMOVED AND REPLACED CAPTAINS LIFE VEST IAW AMM 25-61-03. - [SDR REXA2013012500193](https://openairdocs.org/sdr/REXA2013012500193), Jan 25, 2013: LIFE VEST. DAMAGED. OBSERVERS LIFE VEST HAS A HOLE IN BAG. REMOVED & REPLACED OBSERVER'S LIFE VEST IAW AMM 25-61-03. - [SDR REXA2013010900122](https://openairdocs.org/sdr/REXA2013010900122), Jan 9, 2013: LIFE VEST. UNSERVICEABLE. INFANT LIFE VEST BAG TORN PAST 2 INCHES. REMOVED AND REPLACED LIFE VEST IAW AMM 25-61-03. - [SDR REXA2012121201764](https://openairdocs.org/sdr/REXA2012121201764), Dec 12, 2012: ESCAPE ROPE. DISCONNECTED. EMERGENCY ESCAPE ROPE DISCONNECTED IN FLIGHT DECK. CONNECTED FLIGHT DECK EMERGENCY ESCAPE ROPE PER CRJ 200 AMM 25-63-01. ALL CHECKS GOOD. - [SDR REXA2012111501683](https://openairdocs.org/sdr/REXA2012111501683), Nov 15, 2012: WARNING SYSTEM. ACTIVATED. DURING GEAR RETRACTION RECEIVED A GEAR DISAGREE MESSAGE AND A HYDRAULIC SYSTEM CAUTION FOR 3B, ON TAKEOFF OUT OF DTW, ON FLIGHT 4416. CREW DID NOT DECLARE AN EM - [SDR REXA2012111101513](https://openairdocs.org/sdr/REXA2012111101513), Nov 7, 2012: CHANNEL. DAMAGED. AFT CENTER POST CHANNEL HAS ELONGATED HOLE BEHIND WINDSHIELD CENTERPOST LOWER FITTING. REPAIRED IAW SRM 51-40-11/51-42-21/51-25-06/51-25-16/51-21-11. - [SDR REXA2012102201415](https://openairdocs.org/sdr/REXA2012102201415), Oct 22, 2012: MECHANISM. DEFECTIVE. MAIN CABIN DOOR WILL NOT OPEN. FOUND INNER HANDLE RETENTION MECHANISM BINDING. REMOVED AND REPLACED MCD INNER HANDLE RETENTION MECHANISM SHAFT BEARING AND SPRIN - [SDR REXA2012093001375](https://openairdocs.org/sdr/REXA2012093001375), Sep 30, 2012: LIGHT. INOPERATIVE. ORANGE STRIP OF EMERGENCY TRACK FLOOR LIGHTS INDICATION AN EXIT AS ROW 1 INOP INSTALLED NEW STRIP IAW AMM 33-50-00. OPS CHECK GOOD. - [SDR REXA2012062701025](https://openairdocs.org/sdr/REXA2012062701025), Jun 27, 2012: PDU. FAILED. LEFT THRUST REVERSER INOPERATIVE. REMOVED AND REPLACED LEFT THRUST REVERSER PDU IAW AMM 78-32-03. OPS CHECKED GOOD. OK FOR SERVICE. - [SDR REXA2012062301015](https://openairdocs.org/sdr/REXA2012062301015), Jun 23, 2012: BULB. INOPERATIVE. RIGHT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT SIDE EMERGENCY LIGHT BULB IAW AMM 33-51-06. OPS CHECKED NORMAL. OK FOR SERVICE. - [SDR REXA2012062301014](https://openairdocs.org/sdr/REXA2012062301014), Jun 23, 2012: BULB. INOPERATIVE. FIRST AND THIRD EMERGENCY CEILING LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED OVERHEAD CABIN CEILING EMERGENCY LIGHT BULBS NR 2 AND 3 IAW AMM 33-51-16. OPS CHE - [SDR REXA2012062101005](https://openairdocs.org/sdr/REXA2012062101005), Jun 21, 2012: LIGHT. INOPERATIVE. ROW 1 ORANGE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT IAW AMM 33-51-01. - [SDR REXA2012060700819](https://openairdocs.org/sdr/REXA2012060700819), Jun 7, 2012: LIGHT. INOPERATIVE. LEFT EMERGENCY LIGHT NR 2 AND RT EMERGENCY LIGHT NR 3 EXTERIOR INOPERATIVE. REMOVED AND REPLACED LT NR 2 AND RT NR 3 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. - [SDR REXA2012040800484](https://openairdocs.org/sdr/REXA2012040800484), Apr 8, 2012: BULB. INOPERATIVE. PAX DOOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED FWD PAX DOOR EMERGENCY LIGHT BULB IAW AMM 33-51-00. OK FOR SERVICE. - [SDR REXA201200094](https://openairdocs.org/sdr/REXA201200094), Jan 4, 2012: MOTOR. FAULTY. PAX DOOR WILL NOT FULLY DEPLOY. REMOVED AND REPLACED PAX DOOR POWER ASSIST MOTOR ASSY IAW CRJ AMM 52-11-08. OPS CHECK SATISFACTORY AT THIS TIME. PLACARD REMOVED - [SDR REXA201100920](https://openairdocs.org/sdr/REXA201100920), Dec 9, 2011: YOKE. MALFUNCTIONED. F/O CONTROL YOKE HAS LOTS OF FRICTION ON USE VERY HARD TO MOVE. PERFORMED OPS CHECK OF AILERON CONTROL SYSTEM IAW CRJ AMM 27-11-00. ALL CHECKED GOOD. WILL NOT D - [SDR REXA201100791](https://openairdocs.org/sdr/REXA201100791), Oct 28, 2011: WIRE HARNESS. FAILED. GEAR DISAGREE AFTER T/O NOSE GEAR WOULD NOT COME UP RAN QRH DID 2 CYCLES ON GEAR AT 180 KTS NO MOVEMENT ON NOSE GEAR LANDED AT 46,800 LBS SLOWLY TOUCHED NOSE WH - [SDR REXA201100571](https://openairdocs.org/sdr/REXA201100571), Sep 22, 2011: BEAM. CRACKED. FS 280 TRANSVERSE BEAM WEB CRACKED OTBD OF LBL 9 AND RBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-926 REV B. - [SDR REXA201100583](https://openairdocs.org/sdr/REXA201100583), Sep 20, 2011: BULKHEAD. CHAFED. CHAFE ON FS 621 BULKHEAD AT LBL 18 IS CHAFED OUT OF LIMITS AT .022 DEEP. REPAIRED IAW BOMBARDIER REOS 601R-53-61-4205 REV A AND 601R-53-61-2155. - [SDR REXA201100582](https://openairdocs.org/sdr/REXA201100582), Sep 20, 2011: POST. DAMAGED. FOUND FS 409.00+128 VERTICAL POST RBL 18.0 O/B SIDE HAS INDICATION NOTED APPROX .2" IN LENGTH 50 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS, FAILED NDT INSPECTION - [SDR REXA201100581](https://openairdocs.org/sdr/REXA201100581), Sep 20, 2011: SILL. CORRODED. CORROSION AROUND NUTPLATE HOLE AT LBL 45 FS 439.00 JUST FWD OF LT OVERWING EMERGENCY EXIT CUTOUT ON SILL. REPAIRED IAW BOMBARDIER CRJ-200 SRM 51-21-06 AND REO 6 - [SDR REXA201100580](https://openairdocs.org/sdr/REXA201100580), Sep 20, 2011: BULKHEAD. DAMAGED. FWD FACE OF 621 BULKHEAD 12" ABOVE FLOOR HAS DAMAGED RIVETS AT RBL 9, 18, 27, AND 36. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155. - [SDR REXA201100579](https://openairdocs.org/sdr/REXA201100579), Sep 20, 2011: BULKHEAD. SCRATCHED. FWD FACE OF 621 BULKHEAD IS CHAFED 30" ABOVE FLOOR AT RBL18, 27, 36 APPROX .25 X .25 X .005. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155. - [SDR REXA201100578](https://openairdocs.org/sdr/REXA201100578), Sep 20, 2011: BULKHEAD. SCRATCHED. FWD FACE OF 621 BULKHEAD HAS A SCRATCH 36" ABOVE FLOOR BETWEEN RBL 36 AND 42 APPROX 1"L X .003D. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155. - [SDR REXA201100577](https://openairdocs.org/sdr/REXA201100577), Sep 20, 2011: BULKHEAD. SCRATCHED. 621 BULKHEAD HAS TWO SCRATCHES APPROX 27 FROM TOP 2 OTBD RBL 9 APPROX 1.5L X.005D. REPAIRED IAW BOMBARDIER REO 601R-53-61-4197. - [SDR REXA201100576](https://openairdocs.org/sdr/REXA201100576), Sep 20, 2011: BULKHEAD. SCRATCHED. FWD FACE OF 621 BULKHEAD HAS TWO SCRATCHES 2 INBD OF LBL 18 2 FROM TOP APPROX .500L X .003D. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155. - [SDR REXA201100575](https://openairdocs.org/sdr/REXA201100575), Sep 20, 2011: BULKHEAD. CHAFED. FWD FCU OF 621 BULKHEAD IS CHAFED AT LBL18 AND 27, 30 INCHES ABOVE FLOOR APPROX .25 X .25 X .005. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155. - [SDR REXA201100574](https://openairdocs.org/sdr/REXA201100574), Sep 20, 2011: POST. DAMAGED. FOUND FS 409.00+128 VERT POST BL 0.0 LT SIDE HAS INDICATION NOTED APPROX .2" IN LENGTH 50 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS. REPAIRED IAW BOMBARDIER REO - [SDR REXA201100573](https://openairdocs.org/sdr/REXA201100573), Sep 20, 2011: SKIN. CHAFED. FOUND THE LT FUSELAGE SIDE SKIN TO BE CHAFED FROM F/S 700 TO F/S 755 BETWEEN STR 9 & 12, 2 EA AREAS COMMON TO THE PYLON T/E REPAIR IAW REO601R-53-61-269. - [SDR REXA201100560](https://openairdocs.org/sdr/REXA201100560), Sep 18, 2011: POST. DAMAGED. FOUND FS 409.00 + 128 VERTICAL POST LBL 18.0, O/B SIDE HAS INDICATION NOTED APPROX .2 IN LENGTH, 50 PERCENT FSH AT WL 69.0 AFT FLANGE. REPAIRED IAW REO 601R-53- - [SDR REXA201100650](https://openairdocs.org/sdr/REXA201100650), Sep 16, 2011: SKIN. CORRODED. RT WING PLANK IS CORRODED AT ACCESS HOLE NR 15 (650 GB). DAMAGE REMOVED FROM AFT CRITICAL AREA IS .003. NO DAMAGE REPORTED IN FWD CRITICAL AREA. REPAIRED IAW BO - [SDR REXA201100649](https://openairdocs.org/sdr/REXA201100649), Sep 16, 2011: SKIN. CORRODED. RT WING PLANK IS CORRODED AT ACCESS HOLE NR 13 (650 EB). DAMAGE REMOVED IN FWD CRITICAL AREA IS .004 AND AFT CRITICAL AREA IS .004. REPAIRED IAW BOMBARDIER REO - [SDR REX2011F00000](https://openairdocs.org/sdr/REX2011F00000), Sep 16, 2011: SKIN. CORRODED. RT WING PLANK IS CORRODED AT ACCESS HOLE 13 (650 EB). DAMAGE REMOVED IN FWD CRITICAL AREA IS .004 AND AFT CRITICAL AREA IS .004. REPAIRED IAW BOMBARDIER REO 601 - [SDR REXA201100590](https://openairdocs.org/sdr/REXA201100590), Sep 16, 2011: SKIN. CORRODED. RT WING PLANK IS CORRODED AT ACCESS HOLE NR 10 (650 BB). DAMAGE REMOVED FROM FWD CRITICAL AREA IS .003 AND AFT CRITICAL AREA IS .001. REPAIRED IAW BOMBARDIER RE - [SDR REXA201100589](https://openairdocs.org/sdr/REXA201100589), Sep 16, 2011: SKIN. CORRODED. RT WING PLANK IS CORRODED AT ACCESS HOLE NR 9 (650 AB). DAMAGE REMOVED IN FWD CRITICAL AREA IS .008 AND AFT CRITICAL AREA IS .004. REPAIRED IAW BOMBARDIER REO 6 - [SDR REXA201100588](https://openairdocs.org/sdr/REXA201100588), Sep 16, 2011: SKIN. CORRODED. RT WING PLANK IS CORRODED AT ACCESS HOLE NR 7 (640 EB). DAMAGE REMOVED IN FWD CRITICAL AREA IS .004 AND AFT CRITICAL AREA IS .004. REPAIRED IAW BOMBARDIER REO 6 - [SDR REXA201100587](https://openairdocs.org/sdr/REXA201100587), Sep 16, 2011: SKIN. CORRODED. RT WING PLANK IS CORRODED AT ACCESS HOLE NR 6 (640 DB). DAMAGE REMOVED IN FWD CRITICAL AREA IS .004 AND AFT CRITICAL AREA IS .007. REPAIRED IAW BOMBARDIER REO 6 - [SDR REXA201100586](https://openairdocs.org/sdr/REXA201100586), Sep 16, 2011: SKIN. CORRODED. RT WING PLANK IS CORRODED AT ACCESS HOLE NR 4 (640 AB). DAMAGE REMOVED IN FWD CRITICAL AREA IS .009 AND AFT CRITICAL AREA IS .007. REPAIR IAW BOMBARDIER REO 601 - [SDR REXA201100553](https://openairdocs.org/sdr/REXA201100553), Sep 15, 2011: SKIN. DENTED. THE FUSELAGE SKIN AT FS 654-672 BETWEEN S-14L-S-15L HAS A 2 X 2 PROTRUDING DENT . WHEN INVESTIGATED THE DENT WAS FOUND TO HAVE AN OIL-CANNING CONDITION. PERMANE - [SDR REXA201100163](https://openairdocs.org/sdr/REXA201100163), Mar 6, 2011: FLAP. OBSTRUCTED. FLAPS FAIL REMOVED SNOW AND PERFORMED OPS CHECK IAW RIL 1871. NO DEFECTS NOTED MAINT IS ON SIGHT AND FLAP WELLS ARE FULL OF SNOW. MAINT HAS TO APPLY HEAT TO RES - [SDR REXA201000067](https://openairdocs.org/sdr/REXA201000067), May 2, 2010: SWITCH. FAULTY. REJECTED TAKEOFF DUE TO WOW INPUT CAUTION MESSAGE AT APPROX 115 KIAS. HIGHEST BTMS WAS 08 ON RT OUTBOARD BRAKE. REMOVED AND REPLACED WOW SWITCH PS12GA IAW AMM 3 - [SDR REXA201000027](https://openairdocs.org/sdr/REXA201000027), Feb 22, 2010: ANTI-ICE SYSTEM. FAILED. LONG TAXI OUT AND DEICE PROCESS, TOOK ABOUT AN HOUR OF MORE. GIVEN TAKE OFF CLEARANCE FROM 3L IN DTW. LINING UP, HELD THE BRAKES, POWERED UP THE ENGINES, AND TU - [SDR REXA200900089](https://openairdocs.org/sdr/REXA200900089), Aug 6, 2009: FLAP. FAILED. FLAPS FAIL AT ZERO ON GROUND. C/W AD 2009-06-12 WOULD NOT RESET. - [SDR REXA100900049](https://openairdocs.org/sdr/REXA100900049), May 11, 2009: FLAP SYSTEM. MALFUNCTIONED. 5/11/2009 ACFT 8423C FLIGHT NR 2132 MCI/MSP, ON APPROACH WHEN FLAPS SELECTED DOWN FAILED AT 20 DEGREES. FLIGHT CREW REPORTED TO MAINTENANCE THAT THEY MISTAKENLY All 56: https://openairdocs.org/deregistered/N8423C-2019-04-10/reports.md ## Other aircraft with N8423C - [Cancelled 1981-04-09](https://openairdocs.org/deregistered/N8423C-1981-04-09): Piper PA-28-235, S/N 28-7610077. Owner: [Baker Beatrice J](https://openairdocs.org/faa-owner/BAKER%20BEATRICE%20J), [Norwalk, CA](https://openairdocs.org/faa-place/CA/Norwalk) - [Cancelled 1950-04-13](https://openairdocs.org/deregistered/N8423C-1950-04-13): Cessna 195, S/N 7313. Owner: [C A T Inc](https://openairdocs.org/faa-owner/C%20A%20T%20INC), [Dover, DE](https://openairdocs.org/faa-place/DE/Dover) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain, except the copies of manufacturers’ service documents, which belong to their rights holders.