# N447CA: 2001 Bombardier CL-600-2B19, registration cancelled 2025-12-09

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 9, 2025
- 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: 7552
- Year built: 2001
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 20, 2001
- Certificate issued: December 8, 2022
- Last registry action: September 22, 2023
- Mode S code: A564D1
- Owner when cancelled: [Frontera Flight Holdings Inc](https://openairdocs.org/faa-owner/FRONTERA%20FLIGHT%20HOLDINGS%20INC)
- Location: [Dover, DE](https://openairdocs.org/faa-place/DE/Dover)
- Owner type: Corporation
- Owner's area on the map: 39.1815° N, 75.4736° W: Placed by OpenAirDocs at the center of ZIP code 19901, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N447CA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=447CA
- Page: https://openairdocs.org/deregistered/N447CA-2025-12-09

From the FAA registry file of November 7, 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 (78, newest 50)

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

- [SDR ASOA2012122102696](https://openairdocs.org/sdr/ASOA2012122102696), Dec 17, 2012: LIGHT. INOPERATIVE. EMERGENCY LIGHTING AT ROW 11D DAMAGED. R & R EMERGENCY FLOOR TRACK LIGHTING AT ROW 11 D IAW AMM 33-51-01 OPS CHECK GOOD NO FURTHER DEFECTS NOTED AT THIS TIME. S
- [SDR ASOA201201575](https://openairdocs.org/sdr/ASOA201201575), May 7, 2012: DRAG ANGLE. CRACKED. PAX DOOR AFT DRAG ANGLE CRACKED. R & R THE AFT DRAG ANGLE IAW SRMS 51-42-06, 51-42-10, AND 51-42-13.
- [SDR ASOA201201537](https://openairdocs.org/sdr/ASOA201201537), May 2, 2012: ANGLE. CORRODED. SERVICE DOOR LOWER SILL ANGLE HAS MULTIPLE AREAS OF CORROSION FROM FS 319.00 THROUGH 349.00. REMOVED SILL IAW SRM 51-42-21. FABRICATED AND INSTALLED SILL ANGLE 
- [SDR ASOA201201535](https://openairdocs.org/sdr/ASOA201201535), May 2, 2012: WEB. CRACKED. DURING EXTERNAL DETAILED INSPECTION FOR CRACKING OF THE UPPER & LOWER WEB OF ENGINE SUPPORT BEAM BETWEEN FS 625 & FS 640, FOUND 3 CRACKS AROUND FASTENER HOLES I
- [SDR ASOA201201487](https://openairdocs.org/sdr/ASOA201201487), May 1, 2012: FLOORBEAM. CORRODED. FLOORBEAM AT FS 349.00 FROM RBL 27 THRU 45 HAS MULTIPLE AREAS OF CORROSION. REPAIRED.
- [SDR ASOA201201474](https://openairdocs.org/sdr/ASOA201201474), Apr 30, 2012: DRAG ANGLE. CRACKED. PAX DOOR AFT DRAG ANGLE CRACKED. REPAIRED.
- [SDR ASOA201201448](https://openairdocs.org/sdr/ASOA201201448), Apr 27, 2012: ANGLE. CORRODED. PASSENGER DOOR HAS A CRACKED ANGLE AT HANDLE MOUNTING ASSY. REMOVED ANGLE FROM HANDLE MOUNTING ASSY, LOCATED, DRILLED AND INSTALLED NEW ANGLE AT THE ORIGINAL LO
- [SDR ASOA201201472](https://openairdocs.org/sdr/ASOA201201472), Apr 26, 2012: FLOOR SUPPORT. CORRODED. FLOOR SILL AND GALLEY SUPPORT PLATE FROM FS 310.00 THRU 319.00 CORRODED AT RBL42.00-45.00. LOCATED, DRILLED AND INSTALLED NEW SILL AND SUPPORT IAW SRM 51-40-11 
- [SDR ASOA201201429](https://openairdocs.org/sdr/ASOA201201429), Apr 26, 2012: FLOORBEAM. CORRODED. PASSENGER COMPARTMENT FLOORBEAM AT FS 349.00 FROM RBL 27 - 45 HAS MULTIPLE AREAS OF CORROSION. REPAIRED FLOORBEAM IAW REO 601R-53-21-2307, STEPS 1-11.
- [SDR ASOA201201427](https://openairdocs.org/sdr/ASOA201201427), Apr 26, 2012: ANGLE. CORRODED. SERVICE DOOR LOWER SILL ANGLE HAS MULTIPLE AREAS OF CORROSION FROM FS 319.00 - 349.00. REMOVED AND REPLACED SILL ANGLE IAW SRM 51-42-21.
- [SDR ASOA201201425](https://openairdocs.org/sdr/ASOA201201425), Apr 26, 2012: CARGO TRACK. CORRODED. CARGO TRACK AT FS 559+86 - 559+90 RBL 9 CORRODED. REMOVED CARGO TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW CARGO SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR ASOA201201423](https://openairdocs.org/sdr/ASOA201201423), Apr 26, 2012: CARGO TRACK. CORRODED. CARGO TRACK AT FS 559+80 - 559+96, LBL 27 CORRODED. REMOVED CORRODED CARGO TRACK IAW AMM 51-01-11. INSTALLED NEW CARGO TRACK IAW AMM 51-01-11-400-802.
- [SDR ASOA201201421](https://openairdocs.org/sdr/ASOA201201421), Apr 26, 2012: CARGO TRACK. CORRODED. CARGO TRACK AT FS 559+112 TO FS 570 LBL 9, CORRODED. REMOVED CORRODED CARGO TRACK IAW AMM 53-01-11. INSTALLED NEW CARGO TRACK IAW AMM 53-01-11-400-802.
- [SDR ASOA201201419](https://openairdocs.org/sdr/ASOA201201419), Apr 26, 2012: ATTACH FITTING. CRACKED. PRESSURE BULKHEAD AFT FACE INTERCOSTAL ATTACH FITTINGS AT STRINGERS 12, 13 AND 14 CRACKED. INSTALLED ATTACH FITTINGS IAW REO 601R-53-61-985.
- [SDR ASOA201201407](https://openairdocs.org/sdr/ASOA201201407), Apr 25, 2012: BRACKET. CRACKED. CO-PILOTS WINDSHIELD POST BOTTOM FWD AND AFT BRACKETS ARE CRACKED. R & R FWD & AFT CO-PILOT WINDSHIELD POST BOTTOM BRACKETS IAW SRM 51-42-21.
- [SDR ASOA201201470](https://openairdocs.org/sdr/ASOA201201470), Apr 24, 2012: VENT. CHAFED. PASSENGER DOOR VENT FLAP HAS SEVERAL CHAFES ON INNER SURFACE. DEEPEST CHAFE IS APPROX .180"D. AFTER REMOVAL OF PAINT, FOUND CHAFE TO BE .090 DEEP AND IN REPAIRA
- [SDR ASOA201201374](https://openairdocs.org/sdr/ASOA201201374), Apr 24, 2012: ANGLE. CRACKED. LEFT FS 621-625 OBLIQUE ANGLE IS CRACKED. INSTALLED NEW SERVICEABLE LT OBLIQUE ANGLE IAW SRM 51-42-21. REPAIR CLASSIFIED AS MINOR.
- [SDR ASOA201201372](https://openairdocs.org/sdr/ASOA201201372), Apr 24, 2012: CONNECTOR. MISSING. FOUND MISSING CONNECTOR ON EMERGENCY LIGHT AND ON WIRE AT FS 409. INSTALLED NEW CONNECTOR ON EMERGENCY LIGHT IAW ESPM 20-17-10. OPS TESTED GOOD IAW AMM 33-51-00
- [SDR ASOA201201370](https://openairdocs.org/sdr/ASOA201201370), Apr 24, 2012: WEB. CRACKED. PASSENGER DOOR AFT WEB IS CRACKED IN RADIUS BETWEEN STEPS 832CT AND 832DT AND BETWEEN FIXED STEP AND 832CT. R & R PAX DOOR AFT WEB IAW SRM'S 51-42-06 AND 51-42-
- [SDR ASOA201201368](https://openairdocs.org/sdr/ASOA201201368), Apr 24, 2012: WEB. CRACKED. PASSENGER DOOR AFT WEB IS CRACKED IN RADIUS BETWEEN STEPS 832AT AND 832BT. INSTALLED NEW PAX DOOR AFT WEB IAW SRM'S 51-42-06 AND 51-42-10.
- [SDR ASOA201201366](https://openairdocs.org/sdr/ASOA201201366), Apr 24, 2012: WEB. CRACKED. PASSENGER DOOR FWD WEB IS CRACKED IN RADIUS BETWEEN FIXED STEP AND 832BT. REMOVED DAMAGE IAW SRM 52-00-31 AND 51-12-00. COMPLIED WITH SRM 51-12-00 PERFORMED LPI
- [SDR ASOA201201330](https://openairdocs.org/sdr/ASOA201201330), Apr 23, 2012: STIFFENER. CRACKED. FS 409+128 BULKHEAD LBL 18 POST FAILS NDT WITH A CRACK INDICATION GREATER THAN 50 PERCENT SCREEN HEIGHT APPROX .100 LONG IN OTBD AFT RADIUS. REMOVED POST IAW SR
- [SDR ASOA201201328](https://openairdocs.org/sdr/ASOA201201328), Apr 23, 2012: SUPPORT BEAM. CRACKED. DURING EXTERNAL DETAILED INSPECTION THE UPPER & LOWER WEB OF THE ENGINE SUPPORT BEAM BETWEEN FS 625 & FS 640, FOUND 3 CRACKS AROUND FASTENER HOLES IN UPPER WEB 
- [SDR ASOA201200062](https://openairdocs.org/sdr/ASOA201200062), Jan 6, 2012: DRAG ANGLE. CRACKED. AFT DRAG ANGLE ON PASSENGER DOOR CRACKED NEAR DOOR ASSIST PULLEY BRACKET. CONFIRMED CRACK TO BE .975 LONG, FOUND WITHIN LIMITS IAW REO 601R-52-11-1360 REV A.
- [SDR ASOA201200053](https://openairdocs.org/sdr/ASOA201200053), Jan 5, 2012: DRAG ANGLE. CRACKED. NR 3 AFT DRAG ANGLE ON PAX DOOR CRACKED NEAR ASSIST PULLEY BRACKET. R & R AFT DRAG ANGLE, ON THE PAX DOOR IAW SRMS 51-42-06, 51-42-10 & 51-42-13.
- [SDR ASOA201102171](https://openairdocs.org/sdr/ASOA201102171), Nov 13, 2011: WEB. CRACKED. CRACK INDICATION NOTED AT FS 559, RBL 9, WL 58.70 ON WEB APPROX .10 IN LENGTH 53 PERCENT FSH, FAILED NDT. C/W EC/TC REO 601R-53-41-260 & REO 601R-53-41-260, REV
- [SDR ASOA201102166](https://openairdocs.org/sdr/ASOA201102166), Nov 12, 2011: BULKHEAD WEB. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HS INDICATION NOTED AT LBL 27.50, WL 130 APPROX .5" IN LENGTH 100 PERCENT FSH FAILED NDT INSPECTION. LEAK CHECK OF AIR CONDITIO
- [SDR ASOA201102158](https://openairdocs.org/sdr/ASOA201102158), Nov 8, 2011: ISOLATOR. BROKEN. PRESSURE BULKHEAD IN CARGO BAY HAS 3 BROKEN ISOLATORS. REMOVED CARGO COVER CAP PN LXA5028A FROM FS 565 TO FS 621 117.50 FOR ACCESS. INSTALLED RT CARGO SIDEWALL 
- [SDR ASOA201102128](https://openairdocs.org/sdr/ASOA201102128), Nov 8, 2011: BULKHEAD. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS CRACK INDICATION NOTED AT LBL 27.50, WL 130 APPROX .5" IN LENGTH 100 PERCENT FSH FAILED NDT INSPECTION.
- [SDR ASOA201102127](https://openairdocs.org/sdr/ASOA201102127), Nov 8, 2011: WEB. CRACKED. CRACK INDICATION NOTED AT FS 559, RBL 9, WL 58.70 ON WEB APPROX 10 IN LENGTH 53 PERCENT FULL SCREEN HEIGHT. FAILED NDT.
- [SDR ASOA201101801](https://openairdocs.org/sdr/ASOA201101801), Sep 26, 2011: GROUND WIRE. UNSECURE. RT FORWARD PART OF CABIN EMERGENCY FLOOR LIGHT NOT ATTACHED TO GROUND. SECURED NEW FLOOR LIGHT TRACK COVER IAW AMM 33-51-01, CKS GOOD. (SDR CLOSED)
- [SDR ASOA201101369](https://openairdocs.org/sdr/ASOA201101369), Jul 24, 2011: LAMP. BURNED OUT. FUSELAGE LT 2ND FROM FRONT EXTERNAL EMERGENCY LIGHT INOP. RELAMPED FUSELAGE LT 2ND FROM FRONT EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21. RELAMPED FUSELAGE LT 2N
- [SDR ASOA201101239](https://openairdocs.org/sdr/ASOA201101239), Jun 28, 2011: DOOR. BINDING. CABIN DOOR JAMMING UP DURING OPENING AND CLOSING, MAY CAUSE PROBLEM IN THE EVENT ON EVACUATION. INSPECTED MAIN CABIN DOOR LINKAGES AND ROD ENDS FOR DEFECTS, NO 
- [SDR ASOA201101148](https://openairdocs.org/sdr/ASOA201101148), Jun 9, 2011: DOOR. BINDING. MAIN CABIN DOOR IS STICKING SHUT AND IS DIFFICULT TO OPEN. PERFORMED OPS TEST ON PAX DOOR IAW AMM 52-11-00. (CLOSED)
- [SDR ASOA201101118](https://openairdocs.org/sdr/ASOA201101118), Jun 3, 2011: DOOR. BINDING. F/A HAS TROUBLE OPENING DOOR. PERFORMED OPERATION TEST ON PAX DOOR IAW AMM 52-11-00.
- [SDR ASOA201101081](https://openairdocs.org/sdr/ASOA201101081), May 29, 2011: DOOR. BINDING. PASSENGER DOOR DIFFICULT TO OPEN. PERFORMED PASSENGER DOOR INSPECTION. CHECK IAW IAW AMM 52-11-00. NO DEFECTS NOTED. (CLOSED)
- [SDR ASOA201001681](https://openairdocs.org/sdr/ASOA201001681), Oct 28, 2010: DOOR. BINDING. ARRIVING AT GATE, F/A COULD NOT OPEN PASSENGER DOOR. RAMP ALSO COULD NOT OPEN PASSENGER DOOR. OPENED DOOR AND OPS CHECKED GOOD IAW AMM 52-11-01, MX READY. (CLOS
- [SDR ASOA201001185](https://openairdocs.org/sdr/ASOA201001185), Aug 25, 2010: BULB. BURNED OUT. RT WING EMERGENCY LIGHT INOP. R & R RT WING EMERGENCY LIGHT BULB IAW AMM 33-51-21. OPS CHECK GOOD , NO DEFECTS NOTED AT THIS TIME.
- [SDR ASOA201000775](https://openairdocs.org/sdr/ASOA201000775), May 19, 2010: POST. CRACKED. TWO INDICATIONS FOUND DURING INSP OF FS 409.0+128 VERTICAL POST AT RBL 18.0 1 ON I/B CHANNEL APPROX .312" LONG 100% FSH, 1 ON O/B CHANNEL APPROX .20" LONG 70% F
- [SDR ASOA201000636](https://openairdocs.org/sdr/ASOA201000636), Apr 26, 2010: DOOR. BINDING. F/A REPORTS THE PAX DOOR IS DIFFICULT TO OPEN/CLOSE. PERFORMED OPS CK OF PAX DOOR. NO FAULTS FOUND AT THIS TIME OK FOR SERVICE IAW AMM 52-11-00. (CLOSED)
- [SDR ASOA201000473](https://openairdocs.org/sdr/ASOA201000473), Apr 1, 2010: LIGHT. INOPERATIVE. RT WING EMERGENCY EXIT (2) LIGHTS INOP FWD OF OVERWING EXIT. REPLACED BULBS (2) CK OK IAW AMM 53-12-10.
- [SDR ASOA201000286](https://openairdocs.org/sdr/ASOA201000286), Feb 20, 2010: SMOKE DETECTOR. DIRTY. SMOKE TOILET CAUTION MESSAGE SHORTLY AFTER TAKEOFF. COMPLIED WITH QRH. NO SMOKE OR FIRE FOUND. CAUTION MESSAGE DISSAPPEARED AFTER 5 MINUTES. REMOVED DUST PARTIC
- [SDR ASOA201000046](https://openairdocs.org/sdr/ASOA201000046), Jan 11, 2010: WARNING MESSAGE. FALSE ACTIVATION. SMOKE TOILET ON DEPARTER (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED AS A PRECAUTION) ( LAVATORY SMOKE DETECTION SYS ). PERFORMED OPS CK IAW AMM
- [SDR ASOA200901332](https://openairdocs.org/sdr/ASOA200901332), Nov 28, 2009: SIGN. INOPERATIVE. EMERGENCY EXIT SIGN ON SIDE WARDROBE INOP.
- [SDR ASOA200901227](https://openairdocs.org/sdr/ASOA200901227), Nov 2, 2009: ATTACH FITTING. CRACKED. LT FS 625 CLIP CRACKED. REMOVED AND REPLACED LT FS 625 IAW SRM 51-42-21. FOR WORK ACCOMPLISHED.
- [SDR ASOA200901228](https://openairdocs.org/sdr/ASOA200901228), Nov 2, 2009: ATTACH FITTING. CRACKED. RT FS 625 CLIP CRACKED.
- [SDR ASOA200901223](https://openairdocs.org/sdr/ASOA200901223), Oct 31, 2009: FLOORBEAM. CRACKED. FS 280.00 TRANSVERSE FLOOR BEAM CLIP JUST OTBD OF RBL-9 IS CRACKED. REMOVED AND REPLACED OTBD CLIP AT RBL 9, SRM 51-40-11 AND 51-42-21.
- [SDR ASOA200901222](https://openairdocs.org/sdr/ASOA200901222), Oct 31, 2009: FLOORBEAM. CRACKED. FS 280.00 TRANSVERSE FLOORBEAM CRACKED AT THE RT FLOORBEAM MEMBER AT RBL-9 AT LWR FLANGE RADIUS. CUT OUT DAMAGED AREA AND REMOVED EXISTING FASTENERS IN REPAIR A
- [SDR ASOA200901220](https://openairdocs.org/sdr/ASOA200901220), Oct 31, 2009: SEAT TRACK. CORRODED. SEAT TRACK CORRODED JUST FWD OF FS 621 AT LBL 9. REMOVED AND REPLACED SECTION OF SEAT TRACK JUST FWD OF FS 621 AT LBL 9 IAW SRM 51-40-00.
- [SDR ASOA200901219](https://openairdocs.org/sdr/ASOA200901219), Oct 31, 2009: FRAME. CRACKED. RT FS 621 FRAME CRACKED AT FLOOR SILL. WORK ACCOMPLISHED IAW EC/TC REO 601R-53-61-117 ON W/O 137143.

All 78: https://openairdocs.org/deregistered/N447CA-2025-12-09/reports.md

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