# N8972E: 2004 Bombardier CL-600-2B19, registration cancelled 2023-07-07 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 7, 2023 - Exported to: South Africa - Status when cancelled: Valid registration - Airframe: [Bombardier CL-600-2B19](https://openairdocs.org/model/bombardier-cl-600-2b19) (registry code 1390008) - Engine: [GE CF34-3B1](https://openairdocs.org/engine/ge-cf34-3b1) (registry code 30070) - Data sheets: [TCDS A21EA-1](https://openairdocs.org/tcds/A21EA-1), [TCDS E15NE](https://openairdocs.org/tcds/E15NE) (OpenAirDocs) - Serial number: 7972 - Year built: 2004 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 1, 2006 - Certificate issued: May 19, 2023 - Last registry action: May 19, 2023 - Mode S code: AC61F8 - Owner when cancelled: [Gold Coast Aviation](https://openairdocs.org/faa-owner/GOLD%20COAST%20AVIATION) - Location: [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale) - Owner type: Corporation - Owner's area on the map: 26.1860° N, 80.1727° W: Placed by OpenAirDocs at the center of ZIP code 33309, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N8972E - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8972E - Page: https://openairdocs.org/deregistered/N8972E-2023-07-07 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 (58, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR REXA2016033000443](https://openairdocs.org/sdr/REXA2016033000443), Mar 30, 2016: BATTERY PACK. DISCHARGED. UPPER EMER EXIT LIGHTED SIGN ON FWD WARDROBE INOPERATIVE. R & R BATTERY PACK AT LOCATION STATION 309L IAW AMM 33-51-04. OPERATIONS CHECKED GOOD. - [SDR REXA2016012100081](https://openairdocs.org/sdr/REXA2016012100081), Jan 21, 2016: MOUNT BRACKET. BROKEN. RIGHT WW CONNECTOR MOUNTING BRACKET FOR J110 J112 IS BROKEN. REMOVED & INSTALLED SERVICEABLE CONNECTOR MOUNTING BRACKET FOR J110 J112 IAW SRM 51-42-21, ESPM 20- - [SDR REXA2016012000073](https://openairdocs.org/sdr/REXA2016012000073), Jan 20, 2016: SUPPORT. CRACKED. AIRCRAFT GND POWER RECEPTACLE SUPPORT IS CRACKED AT INBD AFT SIDE. THE EXTERNAL GND POWER RECEPTACLE SUPPORT WAS REPLACED IAW SRM 51-42-06 & 51-42-21. RT DOOR W - [SDR REXA2016012000069](https://openairdocs.org/sdr/REXA2016012000069), Jan 20, 2016: DOOR SILL. CORRODED. LEFT SIDE SILL FS 574.00 - 621 HAS MINOR CORROSION AROUND NUTPLATES. MINOR CORROSION WAS REPAIRED ON LT SIDE SILL BY PERFORMING REO 601R-53-61-1574, REV B. REMO - [SDR REXA2016012000068](https://openairdocs.org/sdr/REXA2016012000068), Jan 20, 2016: STRUCTURE. DAMAGED. RIGHT FUEL BOOST PUMP CUT OUT LAND SURFACE HAS AN INDICATION .1"" LONG BY 50% FSH. FAILED NDT INSPECTION. RT FUEL & BOOST PUMP WAS REMOVED, REINSTALLED & OPERAT - [SDR REXA2016011900071](https://openairdocs.org/sdr/REXA2016011900071), Jan 19, 2016: GLOWSTRIP. DELAMINATED. EMERGENCY LIGHT TRACK HAS 5 PIECES THAT ARE DELAMINATED. THE TWO FWD PIECES LT & RT PIECES AFT & PIECE JUST FWD OF THE AFT & LT. INSTALLED NEW PHOTO LUMINESCENT - [SDR REXA2016011800074](https://openairdocs.org/sdr/REXA2016011800074), Jan 18, 2016: HANDLE. DAMAGED. AVIONICS DOOR HANDLE HOUSING HAS INDICATION ALL AROUND THE BASE OF HANDLE SHAFT, APPROX 90% FSH FAILED NDT. AVIONICS DOOR HANDLE WAS REPAIRED BY REMOVING & REIN - [SDR REXA2016011700086](https://openairdocs.org/sdr/REXA2016011700086), Jan 17, 2016: POST. DAMAGED. FS 409.0+128, VERTICAL POST, BL 0.0 AT WL 69, HAS AN INDICATION IN THE AFT FLANGE RADIUS OF BOTH LT POST .265"" LONG BY 70% FSH & RT POST .260"" BY 65% FSH. FAI - [SDR REXA2016011700080](https://openairdocs.org/sdr/REXA2016011700080), Jan 17, 2016: SEAT TRACK. ERODED. RIGHT FLOOR SEAT RAILS NR 1, 2 & 5 ERODED. REPLACED RT FLOOR SEAT RAIL SECTIONS NR 1 & 2 WITH SERVICEABLE SEAT RAILS. FABRICATED SEAT RAIL SECTION NR 5 & INSTAL - [SDR REXA2016011600125](https://openairdocs.org/sdr/REXA2016011600125), Jan 16, 2016: POST. DAMAGED. FS 409.0+128, VERTICAL POST RBL 18 AT WL 69, HAS AN INDICATION IN THE AFT FLANGE RADIUS OF BOTH THE INBD POST .250" LONG BY 57% FSH & OTBD POST .250" LONG BY 50 - [SDR REXA2016011600085](https://openairdocs.org/sdr/REXA2016011600085), Jan 16, 2016: POST. DAMAGED. FS 409.0+128, VERTICAL POSTS, LBL 18 AT WL 69, HAS AN INDICATION IN THE AFT FLANGE RADIUS OF BOTH THE OTBD POST .250"" LONG X 60% FSH & INBD POST .247"" LONG BY - [SDR REXA2016011600082](https://openairdocs.org/sdr/REXA2016011600082), Jan 16, 2016: ANGLE. CORRODED. PASSENGER DOOR LOWER SILL, SILL MOUNT ANGLE PN 601R31527-221 IS CORRODED AROUND PROX SENSOR. R & R PAX DOOR LOWER SILL MOUNT ANGLE PN 601R31527-221 IAW SRM 51-4 - [SDR REXA2016011600067](https://openairdocs.org/sdr/REXA2016011600067), Jan 16, 2016: SKIN. CORRODED. LOWER LT WING ACCESS HOLE NR 1, PANEL 540BB, HAS CORROSION ON CUT OUT, IN CRITICAL & NON-CRITICAL AREA. PERFORMED REPAIR ON LOWER LT WING ACCESS HOLE NR 1 PANEL - [SDR REXA2016011400078](https://openairdocs.org/sdr/REXA2016011400078), Jan 14, 2016: SEAT TRACK. ERODED. LEFT SIDE SEAT RAIL NR 5 ERODED FS 409.0+128 - FS 439. REPAIRED LT SIDE SEAT RAIL NR 5 CORROSION FS 409.0+128 - FS 439 IAW EA 253-03929 & SRM 51-40-11. - [SDR REXA2016011200079](https://openairdocs.org/sdr/REXA2016011200079), Jan 12, 2016: SEAT TRACK. ERODED. LEFT FLOOR SEAT RAILS NR 1, 2, 4 & 5 ERODED. REMOVED CORRODED SEAT RAILS NR 2, FS 364 - 394.00 & INSTALLED NEW SEAT RAIL PN 601R31032-15 IAW AMM 53-01-11-400-80 - [SDR REXA2016011200070](https://openairdocs.org/sdr/REXA2016011200070), Jan 12, 2016: SUPPORT. DAMAGED. REAR CARGO DOOR TRACK SUPPORT STRUCTURE PN 601R35050-64 IS CUT & CHAFED FROM FWD BALANCE SPRING CABLE. REPAIRED REAR CARGO DOOR TRACK SUPPORT STRUCTURE PN 601R3 - [SDR REXA2016011100084](https://openairdocs.org/sdr/REXA2016011100084), Jan 11, 2016: ANGLE. CRACKED. AFT EQUIPMENT BAY RT SIDE, FS 621 - 625 OBLIQUE ANGLE CRACKED. REMOVED CRACKED OBLIQUE ANGLE & REPLACED WITH SERVICEABLE OBLIQUE ANGLE, PN 601-35012-52, IAW SRM - [SDR REXA2016011100083](https://openairdocs.org/sdr/REXA2016011100083), Jan 11, 2016: ANGLE. CRACKED. AFT EQUIPMENT BAY LT SIDE FS 621 - 625 OBLIQUE ANGLE CRACKED. REMOVED CRACKED OBLIQUE ANGLE & REPLACED WITH SERVICEABLE OBLIQUE ANGLE PN 601-35012-51 IAW SRM 51 - [SDR REXA2016011100077](https://openairdocs.org/sdr/REXA2016011100077), Jan 11, 2016: FLOOR SUPPORT. CORRODED. CARGO BAY, FLOOR SUPPORT RAIL AT LBL 24.0, FS 590 - 621 HAS MINOR CORROSION AROUND THE NUTPLATES. REPLACED FLOOR CAP PN 601R35031-263. REINSTALLED FILLER STRIP - [SDR REXA2016011000076](https://openairdocs.org/sdr/REXA2016011000076), Jan 10, 2016: ATTACH FITTING. CRACKED. FS 280, RBL 9 INBD ATTACH CLIP IS CRACKED. R & R FS 280.00, RBL 9 CLIP PN 601R31113-58 IAW SRM 51-40-11 & 51-42-21. - [SDR REXA2016011000075](https://openairdocs.org/sdr/REXA2016011000075), Jan 10, 2016: ANGLE. CORRODED. FS 280, FWD J ANGLE IS CORRODED AROUND FASTENER HOLES. LOCATED, DRILLED & INSTALLED NEW FS 280 FWD J ANGLE IN PLACE OF DAMAGED FWD J ANGLE PN 600-34017-351 IAW - [SDR REXA2016010800072](https://openairdocs.org/sdr/REXA2016010800072), Jan 8, 2016: CHANNEL. CRACKED. CARGO DOOR FWD TRACK LOWER AFT C CHANNEL IS CRACKED. R & R CHANNEL 601R35050-25 IAW SRM 51-42-06. - [SDR REXA2015111701067](https://openairdocs.org/sdr/REXA2015111701067), Nov 17, 2015: LIFE VEST. UNSERVICEABLE. INFANT LIFE VEST SEAL BROKEN. R & R INFANT LIFE VEST IAW AMM 25-61-03. - [SDR REXA2015110901056](https://openairdocs.org/sdr/REXA2015110901056), Nov 9, 2015: BRACKET. BENT. GEAR DISAGREE ON TAKEOFF. NOSE GEAR REMAINED IN DOWN POSITION. RAN QRH & DID NOT FIX ISSUE. NOSE DOOR MSG ALSO DISPLAYED. DEFERRED LG RETRACTION SYS IAW MEL 32- - [SDR REXA2015091200857](https://openairdocs.org/sdr/REXA2015091200857), Sep 12, 2015: BATTERY PACK. DISCHARGED. ALL EMER LIGHTS INOPERATIVE DURING TEST. R & R EMER BATTERY PACKS 1, 2, 3 & 4 IAW AMM 33-51-04. OPERATIONS CHECKED GOOD. - [SDR REXA2015072400737](https://openairdocs.org/sdr/REXA2015072400737), Jul 24, 2015: CONTROL UNIT. FAILED. FLAPS FAIL CAUTION MESSAGE RECEIVED AT CRUISE ALTITUDE OF 30,000 FEET. THE EVENT OCCURRED WITH THE FLAPS FULLY RETRACTED AT 0* INFLIGHT WITH AN EICAS POSITION O - [SDR REXA2015072000127](https://openairdocs.org/sdr/REXA2015072000127), Jul 17, 2015: SKIN. DENTED. DURING PAINT, FOUND A DENT IN THE LT RUDDER SKIN. THE DENT MEASURE 7.00” X 2.00” X 0.038” DEEP. REPAIRED IAW EA CRJ255-03564. - [SDR REXA2015071700720](https://openairdocs.org/sdr/REXA2015071700720), Jul 17, 2015: SKIN. DAMAGED. DURING PAINT, MX FOUND A DENT, CREASE IN LT SIDE OF RUDDER SKIN BETWEEN RS 136.9 & 142.63, MEASURING 1" LONG & 2" WIDE X .038 DEEP, DEFERRED IAW EA CRJ253-03563 - [SDR REXA2015070200654](https://openairdocs.org/sdr/REXA2015070200654), Jul 2, 2015: BRACKET. DEFECTIVE. NOSE DOOR & NOSE GEAR ON GEAR UP DISAGREE MASTER WARNING, NOSE GEAR STAYED DOWN & LOCKED, MAIN GEAR WAS NORMAL. REPLACED NLG SENSOR BRACKET. REPLACED TARGET BRA - [SDR REXA2015050700469](https://openairdocs.org/sdr/REXA2015050700469), May 7, 2015: CLAMP. MISSING. LEFT OVERWING EMER ROPE MISSING C CLAMP. REPLACED LT D CLIP ON EMER ROPE IAW AMM 25-63-04. OK FOR SERVICE. - [SDR REXA2015050100456](https://openairdocs.org/sdr/REXA2015050100456), May 1, 2015: GLOWSTRIP. DEGRADED. CABIN EMER FLOOR PHOTO LUMINESCENT STRIP DEGRADED AT SEAT 3 - 5C. R & R PHOTO LUMINESCENT STRIP IAW AMM 33-51-01. - [SDR REXA2015020900191](https://openairdocs.org/sdr/REXA2015020900191), Feb 9, 2015: OXYGEN MASK. INOPERATIVE. OBSERVERS OXYGEN MASK IS INOPERATIVE. DEFERRED OBSERVERS OXYGEN SYS IAW MEL 35-10-01 PLACARD INSTALLED. R & R WITH SERVICEABLE OXY MASK IAW AMM 35-11-12. LEAK & - [SDR REXA2015020300173](https://openairdocs.org/sdr/REXA2015020300173), Feb 3, 2015: BATTERY. WEAK. NUMBER 4 EMER LIGHT BATTERY WEAK. R & R NR 4 EMER LIGHT BATTERY. OPERATIONS CHECKED GOOD IAW AMM 33-51-04. - [SDR REXA2015020300172](https://openairdocs.org/sdr/REXA2015020300172), Feb 3, 2015: LENS. MISSING. AFT CEILING EMER EXIT SIGN BLUE LENS COVER MISSING. INSTALLED BLUE LENS COVER ON CEILING EMER EXIT SIGN AFT SIDE IAW AMM 33-51-14. - [SDR REXA2014092500997](https://openairdocs.org/sdr/REXA2014092500997), Sep 25, 2014: CABLE. FRAYED. DURING PA52-059 FOUND PAX DOOR MOTOR CABLE FRAYED & WORN BEYOND LIMITS. R & R THE PAX DOOR MOTOR CABLE IAW AMM 52-11-08-04 & AMM 52-11-09-04. OPERATIONS CHECKED - [SDR REXA2014072800745](https://openairdocs.org/sdr/REXA2014072800745), Jul 28, 2014: ENGINE. MALFUNCTIONED. ACFT EXPERIENCED INFLIGHT SHUTDOWN OF THE RT ENG. RT ENG OIL PRESS WARNING MSG & RT ENG OIL PRESS INDICATIONS WERE <30 PSI & DECREASING, FLUCTUATING. REDUCED RT - [SDR REXA2014052700525](https://openairdocs.org/sdr/REXA2014052700525), May 27, 2014: PSEU. FAULTY. GEAR DISAGREE WARNING MSG CLIMBING THROUGH FL 210. FOUND CODE A02 FAIL ON PSEU ON LEG NR 1. PERFORMED OPERATIONS CHECK AFTER REMOVAL & REPLACEMENT OF PSEU IAW A - [SDR REXA2011012300010](https://openairdocs.org/sdr/REXA2011012300010), Jan 21, 2014: BULKHEAD. CRACKED. FUSELAGE STATION 621 BULKHEAD CRACKED AT LINTEL FITTING UPPER SIDE. REPAIRED IAW REO 601R-53-61-1230. - [SDR REXA2013121302402](https://openairdocs.org/sdr/REXA2013121302402), Dec 13, 2013: FLAP. FAILED. FLAPS FAIL CAUTION MESSAGE. DEFERRED, PERFORMED TROUBLESHOOTING IAW FIM REV 45, IAW AD 2009-06-12 PARAGRAPH H 6 I AMOC DATED JULY 22, 2013 & PA AD 27-052N. SEE - [SDR REXA2013121002295](https://openairdocs.org/sdr/REXA2013121002295), Dec 10, 2013: LIFE VEST. UNSERVICEABLE. FIRST OFFICER`S LIFE VEST BAG TORN. R & R FIRST OFFICER'S LIFE VEST IAW AMM 25-61-03. - [SDR REXA2013121002294](https://openairdocs.org/sdr/REXA2013121002294), Dec 10, 2013: LIFE VEST. UNSERVICEABLE. FLIGHT ATTENDANT'S LIFE VEST BAG TORN. R & R FLIGHT ATTENDANT’S LIFE VEST IAW AMM 25-61-03. - [SDR REXA2013080601562](https://openairdocs.org/sdr/REXA2013080601562), Aug 6, 2013: FLASHLIGHT. INOPERATIVE. F/O EMERGENCY FLASHLIGHT INOPERATIVE. - [SDR REXA2013042900644](https://openairdocs.org/sdr/REXA2013042900644), Apr 28, 2013: ANGLE. CRACKED. FS 559 SEMI PRESSURE BULKHEAD CAP ANGLE FOUND CRACKED AT LBL 18 AND RBL 18. REPAIRED IAW BOMBARDIER REO 601R-53-41-260 AND 601R-53-41-609 AND PA 53-025. - [SDR REXA2012091901353](https://openairdocs.org/sdr/REXA2012091901353), Sep 19, 2012: BPSU. FAILED. WHEN CREW ATTEMPTED TO EXTEND FLAPS AT 162 KIAS A FLAPS FAIL MESSAGE WAS RECEIVED AND THE FLAPS WERE STUCK AT ZERO DEGREES. THE FLIGHT THEN DIVERTED TO EWR FOR - [SDR REXA2012091101336](https://openairdocs.org/sdr/REXA2012091101336), Sep 11, 2012: DOOR. OUT OF POSITION. RIGHT EMERGENCY EXIT DOOR CAUTION MESSAGE INTERMITTENTLY ON IN FLIGHT. INSTALLED EMERGENCY EXIT DOORS INTO THEIR CORRECT RESPECTIVE POSITION. OPS CHECKED GOOD, - [SDR REXA2012091201093](https://openairdocs.org/sdr/REXA2012091201093), Sep 5, 2012: BULKHEAD. CHAFED. FS 621 BULKHEAD CHAFED AT WL120.43 AND LBL40. REPAIRED IAW REO 601R-53-61-2155 AND 601R-53-61-4633. - [SDR REXA2012051800755](https://openairdocs.org/sdr/REXA2012051800755), May 18, 2012: BPSU. MALFUNCTIONED. FLAPS FAIL CAUTION MSG ON CLIMB AT 0. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H) (6) (I). AMOC DATED MARCH 27, 2009 TR# - [SDR REXA2012042200558](https://openairdocs.org/sdr/REXA2012042200558), Apr 22, 2012: ECU. MALFUNCTIONED. FLAPS FAIL AT 0 IN CRUISE (RESET GOOD). REPLACED LT FECU. ALL OPS CHECKS GOOD. NO JAM CODES. - [SDR REXA2012042000542](https://openairdocs.org/sdr/REXA2012042000542), Apr 20, 2012: LIGHT. BROKEN. EMERGENCY LIGHT NEAR THE FLOOR BY THE MAIN CABIN DOOR BROKEN. REPLACED LIGHT ASSY W/SERVICEABLE. ALL CHECKS GOOD. - [SDR REXA2012040100455](https://openairdocs.org/sdr/REXA2012040100455), Apr 1, 2012: TRIM SYSTEM. MALFUNCTIONED. AILERON TRIM WILL NOT TRIM LEFT. CYCLED AILERON CIRCUIT BREAKER IAW AMM 27-12-01. OP CHECKED GOOD, OK FOR SERVICE. All 58: https://openairdocs.org/deregistered/N8972E-2023-07-07/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 20110704014559I](https://openairdocs.org/incident/20110704014559I), Jul 4, 2011: Bombardier Inc CL-600-2B19 (N8972E), Brainerd, MN, Minor damage. Immediately after touchdown this aircraft struck two deer. Flap damage occurred on left inboard and outboard flaps. Damage occurred on main landing gear door. --- 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.