# N486CA: Bombardier CL-600-2B19, registration cancelled 2011-11-02 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 2, 2011 - Exported to: Bermuda - Status when cancelled: Valid registration - Airframe: [Bombardier CL-600-2B19](https://openairdocs.org/model/bombardier-cl-600-2b19) (registry code 1390008) - Data sheets: [TCDS A21EA-1](https://openairdocs.org/tcds/A21EA-1) (OpenAirDocs) - Serial number: 7707 - Type of aircraft: Fixed wing multi engine - Certificate issued: February 9, 2011 - Last registry action: February 9, 2011 - Mode S code: A5FF16 - Owner when cancelled: [Trust N695br N696br N697br](https://openairdocs.org/faa-owner/TRUST%20N695BR%20N696BR%20N697BR) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.7236° N, 75.5412° W: Placed by OpenAirDocs at the center of ZIP code 19801, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N486CA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=486CA - Page: https://openairdocs.org/deregistered/N486CA-2011-11-02 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 (17) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CHQA200900042](https://openairdocs.org/sdr/CHQA200900042), Feb 1, 2009: PRIORITY VALVE. INOPERATIVE. FLIGHT 5584 IAH TO MOB - DURING APPROACH WHEN THE LANDING GEAR WAS EXTENDED THE MAIN GEAR EXTENDED NORMALLY BUT THE NOSE LANDING GEAR STILL INDICATED UP AND LOC - [SDR CHQA200900033](https://openairdocs.org/sdr/CHQA200900033), Jan 24, 2009: TRIM SYSTEM. MALFUNCTIONED. FLIGHT 5635, MAF TO IAH - ON CLIMB-OUT FLIGHT CREW RECEIVED STAB TRIM AND MACH TRIM MESSAGES. THE QRH WAS FOLLOWED AND BOTH TRIMS WERE RE-ENGAGED, BUT UPON TRIM - [SDR CHQA200800161](https://openairdocs.org/sdr/CHQA200800161), Aug 6, 2008: LINE. CHAFED. FLIGHT 5723, SDF TO IAH. DURING CRUISE THE CREW RECEIVED A NR1 HYDRAULIC SYSTEM LOW PRESSURE MSG AND THE HYDRAULIC SYNOPTIC PAGE INDICATED ZERO QUANTITY. THE FL - [SDR CHQA200800009](https://openairdocs.org/sdr/CHQA200800009), Jan 17, 2008: PRESSURE VALVE. STUCK. IAH TO MOB - WHILE CLIMBING THROUGH 1,500 FEET, CREW RECEIVED RIGHT PACK HIGH PRESSURE CAUTION MESSAGE ACCOMPANIED BY FAULT LIGHT INDICATION ON RIGHT PACK BUTTO - [SDR CHQA200700033](https://openairdocs.org/sdr/CHQA200700033), Jul 2, 2007: LOOP. INOPERATIVE. FLIGHT 3288 - IAH-CHS - RECEIVED LT 14TH STAGE BLEED LEAK MESSAGE ON THE EICAS. DECLARED AN EMERGENCY. MAINTENANCE TROUBLE SHOT AND FOUND A FAULTY 14TH STAGE BL - [SDR COMA0660683](https://openairdocs.org/sdr/COMA0660683), Dec 5, 2006: STEP. CRACKED. DURING CABIN DOOR INSPECTION FOUND UPPER STEP CRACKED, RT SIDE. REMOVED DAMAGE AND REPAIRED IAW REO 601R-52-11-279. - [SDR COMA0660682](https://openairdocs.org/sdr/COMA0660682), Dec 4, 2006: FLOOR SUPPORT. CRACKED. LEFT FWD OUTBOARD FLOOR SUPPORT ANGLE BRACKET AT FS 280 BETWEEN GALLEY AND COCKPIT IS CRACKED. INSTALLED NEW ANGLE BRACKET IAW SRM 51-42-21. - [SDR COMA0660681](https://openairdocs.org/sdr/COMA0660681), Dec 4, 2006: ANGLE. CRACKED. LEFT FWD INBOARD FLOOR SUPPORT ANGLE BRACKET AT FS 280 BETWEEN GALLEY AND COCKPIT IS CRACKED. INSTALLED NEW ANGLE BRACKET IAW SRM 51-42-21. - [SDR COMA0660454](https://openairdocs.org/sdr/COMA0660454), Jul 22, 2006: PSEU. FAULTY. DURING CVG APPROACH RECEIVED A LANDING GEAR DISAGREE CAUTION, ABORTED APPROACH, THEN LANDED WITHOUT INCIDENT ON SECOND ATTEMPT.REPLACED THE PROXIMITY SENSING EL - [SDR COMA0660452](https://openairdocs.org/sdr/COMA0660452), Jul 21, 2006: PRIORITY VALVE. FAULTY. DURING AZO APPROACH RECEIVED A NOSE GEAR DOOR AND GEAR DISAGREE WARNING, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE NOSE LANDIN - [SDR COMA0660344](https://openairdocs.org/sdr/COMA0660344), May 12, 2006: DUCT. UNSECURE. FLIGHT 5235 - DISPLAY TEMP DISPLAYED ON CAPTAIN SIDE PFD AND MFD. FOUND CAPTAIN SIDE PLENUM DUCT OFF. RESECURED PLENUM DUCT. - [SDR COMA0560726](https://openairdocs.org/sdr/COMA0560726), Dec 15, 2005: WARNING LIGHT. ILLUMINATED. FLIGHT 5342 - FOUND RT THRUST REVERSER UNLOCKED MESSAGE. - [SDR COMA0560670](https://openairdocs.org/sdr/COMA0560670), Dec 4, 2005: WARNING LIGHT. HOT START. FLIGHT 5746 - RT T/R UNLOCK WARNING. DEFERRED MAINTENANCE PER MEL. - [SDR COMA0560313](https://openairdocs.org/sdr/COMA0560313), May 20, 2005: CONTROL UNIT. MALFUNCTIONED. FLIGHT 5651 AUTO PILOT DISCONNECT WARNING AND PITCH DOWN AND LOSS OF 500 FT. REPLACED THE HSTCU. - [SDR COMA0360101](https://openairdocs.org/sdr/COMA0360101), Feb 13, 2003: CONNECTOR. FLIGHT 5829 EMERGENCY FLOOR PATH LIGHTING FWD SECTION IS INOP.CLEANED ELECTRICAL CONNECTIONS - SYSTEM TEST NORMAL. - [SDR COMA0360036](https://openairdocs.org/sdr/COMA0360036), Jan 19, 2003: WIRE. FLIGHT 5852 LEFT ENGINE REVERSER UNLOCKED WARNING MESSAGE.REPAIRED CHAFED WIRE AT T/R WIRE HARNESS. - [SDR COMA0260714](https://openairdocs.org/sdr/COMA0260714), Dec 13, 2002: FLAP. FLIGHT 5115 FLAPS FAILED AT 26 DEGREES DURING TAXI.ADJUSTED FLAP RIGGING TO C/W M/M LIMITS. ## Other aircraft with N486CA - [Registered now](https://openairdocs.org/aircraft/N486CA): Textron 182T, S/N 18283302, built 2025 --- 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.